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TURKISH AIRLINES A320 Full Flight Simulator Technical Specification

1. cece eeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeee 80 13 QUALITY OF CONSTRUCTION AND SAFETY REQUIREMENTS 82 13 1 MATERIAL PARTS PROCESSES AND FINISHES nnsannnnnnennnnennennnnnnnne 82 E A SLANG Farts snra a a 82 KE Ne A REGAIN Panse a eaa iiaa EAE 82 13 1 3 Non Metallic Parts s 20 s0sisiccstcthcenctsioietstelaiecctalasadsiateiedstalbiadsiebeccstabeness 82 13 1 4 Flammable EN 82 E AE GET 83 13 1 6 Guaranteed Weight eege 83 TAS WIIN ee E A E se 25e Sseaaseeseee 83 13 2 INTERCHANGEABILITY amp IRURERLACEMENT 83 13 3 Ee 84 E Se Ee TE 84 KE EN le EE 84 13 3 3 L calisation WANKING CC 84 13 4 Calle lee M ce rererere nocent renoneer reet eae eatre rert oee petia Fer ratie 84 13 3 5 UE EE Ee 84 13 3 6 ue EEN 84 E Sets Safety ln E 84 13 3 8 Motion System Control Forces Simulated Gvstems eee 85 13 4 HEALTH AND SAFETY QUALIFICATION REQUIREMENTS 5 85 13 4 1 STIS EE 85 13 4 2 Emergency gt er See ee 85 13 4 3 Emergency Power Off scicccctseseccseseueccdbeeueuccedeuecededeneuceesebeccdeueneucuedebescneuet 85 13 4 4 Fire Protection EE 85 13 4 5 EMC Electro Magnetic Compatibility cccceeeeeeeeeeeeeeeeeeeeeeeeeeeees 86 14 SCHEDULE AND PROJECT FOLLOW UP a ssssssnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnna 87 14 AUTHOROTIES HE ese E E ENN 87 14 2 IN PLANT THY S EOLLOWUID 87 14 3 PROGRESS EE UE 87 14 4 UPDATE OF SELLER S SPECIFICATION AA 88 15 ACCEPTANCE EN 89 E Fag eS
2. 10 6 2 Motion System Diagnostics The motion system shall be designed to detect memorise display and print every malfunction which may occur during its operation even erratic or fugitive failures The error messages shall be duplicated simultaneously on the On Line Diagnostic Refer to paragraph 12 The Seller shall provide complete documentation of motion diagnostic tool 10 6 3 Alignment Procedure e The Seller shall provide built in testing capability for trouble shooting and automatic alignment purposes through the motion cabinet processor e Current and back up calibration shall be maintained and saved on the host computer e All adjustment and tuning tools shall be automatic and menu driven e Calibration parameters shall be printable e This procedure shall enable the recovery of system performance after the change of a component servo motor servo amplifier electronic boards e A motion actuator control shall be manually or automatically driven either individually jack or in group e All significant signal values voltages positions inputs shall be monitored and printable Page 73 of 102 3 Turkish Airlines A320 Full Flight Simulator Technical Specification 11 VISUAL SYSTEM 11 1 GENERAL The entire Visual System is part of the FFS Consequently all the requirements detailed in each chapter of this FS specification shall apply The Seller design shall also comply with the specific requirements d
3. minimum requirements as level D refer to chapter 1 Sound simulation shall correlated with visual cues 4 4 2 Sound tuning and evolution Individual volume adjustment shall be possible for each sound audio warning sound ATIS by means of an appropriate Hardware or Software process without any need for equipment dismount The Seller shall provide some sound and voices spares minimum 30 of sound system capability useable without any sound affectation restriction and shall ensure that the addition of sounds or voices shall be done along the sound generation chain through an easy to use procedure All necessary tools for recording and analysing purposes licenses and procedures shall be provided 4 4 3 Sound controls Aircraft systems generated sounds volume shall be always set to nominal value Communications sounds volume shall be tuned by cockpit controls In the same time environmental sounds volume shall be controlled through IOS by 2 ways Page 32 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification e Variable control 80 volume position shall correspond to the nominal level of the simulated sound e Discrete control global mute function Specific functions e During freeze only environmental sounds shall be muted e During repositioning all sounds shall be muted 4 4 4 Flight compartment ambient noise level The acceptable acoustic noise level in the crew and instructor areas as meas
4. TURKISH AIRLINES A320 Full Flight Simulator Technical Specification 30 July 2008 Turkish Airlines A320 Full Flight Simulator Technical Specification TABLE OF CONTENTS 1 GENERAL REQUIREMENTS Zeene 10 2 CUSTOMISATION ORGANISATION ccccccccceeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeees 11 2 1 GENERAL CUSTOMISATION PRINCIPLE nnnsssnnnnennnnnnnseennnnrnrnnnrernsnnnnnrnnnne 11 2 2 HARDWARE CUSTOMISATION PRINCIPLE sssssannnnnnnnsnesnennnnnnnerensnnnnnnnnnne 11 2 3 SOFTWARE CUSTOMISATION DRINCIDILE 11 2 4 AIC COMPUTER CUSTOMISATION geet gegeeteeggekeekereegg Eed 11 3 AIRCRAFT SIMULATION WE 12 3 1 GENERAL en eee ee EEE ee EEE EERE 12 3 2 EIS 2 SOFTWARE DATA LOADING E 12 3 3 EGPWS eege Ce RE 13 Sr EAS WS MOG eironi ninina ataa aaaea a iaasa aA 13 3 3 2 Electronic Mountain E 13 3 3 2 1 Detailed Functions ti picauiaciteentiants tien anteater ee 13 SA FMGG SOREN Sea eee sore ner Saree nee eer Tate rere Toe noe meer 14 34 1 FMS Files L adiN EE 14 3 4 2 F M Preparation Copvlload 14 3 4 2 1 General e E 14 E Link With a ie i le ee a ee ee ee ee ee ee 15 3 4 3 FM COBY LO AG 6 ccnsccsssdodstctctocapniadasstcdeies ctnindnasdnbaieastatetnssintedvsshateteanteiataaicns 16 3 4 3 1 General Performance EE 16 5S We Is LinK With OS seoce peopesas 16 3 5 ATIMS PRE FANS CONEIGURATION 16 SC UNO CUCM ON ee 16 3 5 2 AOC Applications cicsisaiciicterccdsedenssnantsscctcnssadcnsieasdsaccedsaaadsasaniasoeccosa tonics
5. e Any simulation software can be edited compiled linked and debugged in background with the change and configuration control support in multi users environment e Navigation data compiler and instructor station pages compiler can be used for consultation or production e User shall keep access to any Network facility Background shall not interfere with the training capabilities of the simulation and operation of the FS start stop in any case 8 2 COMPUTER PROGRAM SYSTEM FS SOFTWARE 8 2 1 General All the software components shall be identified and specified in the FS control file Software components include processes tools databases visual navigation interface software scripts Multi versions customisation shall also be referenced and defined in the FS control file Several FS control files at least the number of available configurations min 6 shall be kept on the disk and user shall have the capability of selecting one of these files for loading simulation Specific configuration of computers for simulation purpose shall be described in a document provided by Seller specific directories links environment parameters All the software components shall be written in standard language like C ADA FORTRAN In the case of non standard software components Seller shall provide a complete list of these components 8 2 2 FS Real Time Executive Programs All Programs shall be written to perform the real tim
6. PERFORMANCE The performance of the motion system shall be such that flight deck movement will give correct and realistic cues to the flight crew in all normal and abnormal manoeuvres and no anomalies shall exist between visual and motion cues In addition to motion cues directly induced by the flight crew the motion system shall also respond to and give the appropriate cues of buffet atmospheric turbulence runway roughness landing impact fuselage flexure engine vibrations etc Page 71 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification The performance shall comply with civil aviation authorities highest requirements FAA and JAA JAR STD 1 A Ammendment3 10 5 SAFETY REQUIREMENTS In the case of the main building power supply is lost or in the event of any failure switch off or combination of failures malfunctions or switch off electrical systems included the computers the electric motion system shall be smoothly decelerated to rest in a level position without shock or damage to equipment or staff Flight compartment door shall incorporate an interlock switch which will de energise the motion system if the door is opened when motion is in use The Drawbridge shall be provided with a sliding gate with an incorporated switch de energising the actuator of the bridge and the motion if the gate is opened A safety system shall be provided in order to prevent actuation of the bridge if somebody is w
7. e The concept of modularity for boards shall apply to the equipment configuration thereby eliminating inters cabinet wiring e Each rack in the cabinets shall have their individual power supplies and circuits barkers e The back panel wiring shall be easily accessible for signal testing or wiring modifications Wiring modifications shall not necessitate interface chassis dismounting All cooling fans shall be easily accessible Cooling fans shall be equipped with filters Air Conditioning to the Flight Compartment shall be filtered Each Cabinet shall have lighting for maintenance Each Cabinet shall be equipped with Anti Static Wrist Straps for board replacement 8 3 4 Accessibility to Boards LRUs and A C Components For maintenance purposes access to all boards LRU s and A C components shall be made clear and easy 8 3 5 Expansion Capacity e Input output channels shall have 30 spare channels of each signal type on the installed PCBs e Spare connectors shall be available on the I O back plane to enable wiring of the provisioned spare I O e In addition a further 30 of PCB slots shall be provided for subsequent expansion e The ARINC 429 system shall have an average of 30 spare buses available on the installed PCBs Page 67 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification e In addition there shall be 30 spare slots available for installation of extra ARINC PCBs e All pins of th
8. print of the list of versions Definition modification and print list of tests and test sets for one version Definition modification and print list of tests for a tests set Execution of all the tests of a version Execution of a group of tests of a version Print the inputs of all the tests of a version Page 64 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification The execute function of a group will output a list of the tests with an automatic flagging for tests in and out of tolerances A 5 Library management This function is used to e Define the contents of the aircraft results e Define all automatism for tests and documentation creation such as pre defined snapshots init conditions output parameters list general chapters Operating procedure The creation of a new test and of its QTG documentation shall be as much automatic as possible using e Pre defined snapshots for first and subsequent initialisations e Standard lists of recorded printed and driven parameters e Standard pages lay outs and contents for the documentation e Propositions of aeroplane parameters for initialisation and inputs when the test is based on an aeroplane test the operator having the possibility to override it The operator can Activate a test from the work station Activate a group of tests from the work station Activate a test from the instructor station screen Activate a group of tests from the i
9. refer to paragraph 3 1 customisation shall enable the FS to reflect all the A C simulated versions as defined in chapter 1 The A C computer customisation shall automatically select and activate the proper A C computer configuration at simulation loading without any operator intervention Page 11 of 102 D Turkish Airlines A320 Full Flight Simulator Technical Specification 3 AIRCRAFT SIMULATION 3 1 GENERAL The simulation shall be based on the principle of the full representation of the flight characteristics of the various systems and the environment of the aircraft by means of logical and mathematical models issued from the aircraft manufacturer data package In particular simulated systems shall operate as the real A C ones with the same performances results and redundancy Seller shall provide substitution simulation each time information is missing in the data package In the following A C computers shall mean the representation of real A C computers whatever the solution chosen by Seller Stimulation simulation rehosting retargeting Seller shall include all necessary computer equipment and simulation model to complete the A C representation Concerning the Main A C Computers Seller shall propose and explain his solutions to represent the A C at the level defined in chapter 1 All the Circuit Breakers CBs shall be fully simulated Seller solutions shall comply with the A C computer customisation refer to paragrap
10. 1 Page 37 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 6 FLIGHT COMPARTMENT 6 1 GENERAL The interior of the simulator cockpit shall conform to the full scale replica of the aircraft cockpit Aircraft cockpit shall be simulated from the bulkhead forward of the rudder pedals to the bulkhead forward of the rest compartment In the simulator cockpit Seller shall integrate all A C Equipment and A C Parts according to Airbus Standard 1 6 DPE refer to Summary and to the simulation requirements refer to paragraph 3 Seller shall inform in detail how much of the cockpit panels instruments and components will be provided from Airbus how much of these items will be replicated or simulated rehosted retargeted etc by the manufacturer List of all these items will be given by part numbers description and quantities by the Full Flight Simulator parts catalogue supplied by the technical specification where the design and functionality of the device explained in detail Seller shall propose a means to easily verify that the replication of the cockpit compartment dimensions and layout of the A C are in accordance with Airbus Standards This process of verification of the simulator cockpit versus to the A C cockpit dimensions shall be demonstrated during in plant Acceptance In particular THY shall be allowed to measure the windshield and crew seats position the pilots eye position XYZ co ordinates and angle
11. 1 All Equipment required for QTG tests shall be provided and permanently installed especially accelerometers recorder if needed and appropriate wiring Electrically driven powered Drawbridge system shall be provided Solid covers under the cabin shall be fixed securely and light proofed They shall not generate vibration on motion use They permit easily access to underneath parts when opened They shall be enough airtight to comply with the fire suppression system requirements A lighting of the underneath compartment shall be provided The FS shall be programmed and instrumented in such a manner that the characteristics buffet modes can be edited measured and compared to aeroplane data 10 2 AXIS OF MOTION The motion system shall be capable of providing motion in six degrees of freedom Seller shall specify in his proposal the maximum excursions of individual and simultaneous movement and response The system shall operate smoothly quietly and without hunting and shall have no adverse effect on the control loading system or the visual system 10 3 WEIGHT INCREASE ALLOWANCE In addition to inherent weight of the cockpit and personnel therein sufficient margin shall be available within the motion system to enable mounted visual system components The addition of visual components on the Flight Compartment shall not replace restraints on guaranteed motion performance acceleration and displacement on any axes 10 4
12. 16 3 5 3 AOCNOS INNS MACS EE EE EE 17 3 5 3 1 Impending Messages Window 2 2 2 2 0 2000sceseeeeeeeeeee eects 18 3 5 3 2 AOC Menu Page AAA 18 3 5 3 3 AOC REPLY Page 22 icncamsnnnnnce ana anacnnkeakaie 20 3 6 WEATHER RADAR eet 21 3 6 1 Ground Mapping Function lt icrcsncnasavexanccvcerincia Eege Ee Er EEAeCeE 21 3 6 2 Cloud Model Definition eege 21 3 6 3 Cloud Model Modttcatton 21 3 6 4 Cloud ee EE 21 3 6 5 Link WEN Eeer 22 Se CAS a EENE EEE NEEE REEE NEEE ENRERE 23 Bele Lee 23 3 7 11 TCAS aiport traffic eene eenegen eebe 23 3 7 1 2 MCAS Ee Ee in Tee sassvserserrercsnarssaxneenteceiberbeesneedesevanerseansbaxneeeds 24 3 7 2 Bu Are LE 26 3 7 3 Scenario and Airport Traffic Modification ccceeeeeeeeeeeeeeeeeeeeeeeeees 26 3 8 SYSTEM WITH PARTIAL SIMULATION SPECIFIC REQUIREMENTS 26 3 8 1 External Ee ln Te EE 26 3 8 2 Air Conditioning And Cabin Pressurisation e 26 3 8 9 Ele thical POW E 26 Page 2 of 102 Turkish Airlines D g A320 Full Flight Simulator Technical Specification 3 8 4 Oxygen System crew and passengers 26 3 8 5 Communication Gvstems 27 3 8 5 1 General communication 27 Soo EE 27 3 8 6 Flight Recorder System ennenen ennnen 28 3 8 7 Window Heat EE 28 3 8 8 Cir it Breaks aide ee 28 3 8 9 Windscreen Wipers And Rain Repellent Gvstem 28 38 10 TEE 28 39 WAL EC ent LE 28 THE IOS MALFUNCTION PAGES SHALL BE CUSTOMISED ACCORDING TO A C VE
13. 8 4 2 FS Power Supplies DC power supplies shall be selected to operate at no more than 60 of their nominal rating When possible the Seller shall use power supplies of the same manufacturer Monitoring circuits shall report to the system controller the failing items Refer to paragraph 12 e Power supplies shall be monitored by the online diagnostic system e All the current and voltage values shall be displayed e Al power supplies shall be connected with plugs no terminal bars and the output voltages shall be adjustable e All FS main electrical supplies including visual system shall be controlled and monitored via the power supply cabinet located in the computer room e Each interface chassis shall be powered by its own power supplies No interconnection shall be allowed Page 68 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 9 DIGITAL CONTROL LOADING SYSTEM 9 1 GENERAL DESCRIPTION Seller shall provide Electric Digital Control Loading systems with responsive and repeatable electro mechanical actuators to simulate the static and dynamic control forces deflections of all applicable primary flight controls and selected secondary controls of those expected by the pilots in the actual aircraft Control Loading System shall comply with the Airbus Standard 1 6 Data Parts and Equipment defined in paragraph 1 General Requirements which have to be considered as the reference 9 2 HA
14. 95 17 4 2 Consumable Spare E 95 17 5 OPERATION AND MAINTENANCE TRAINING 95 17 5 1 Hardware Training 8 people 96 17 5 2 Software Training ee EE 96 18 RELIABILITY ee ENEE EENEG 97 18 1 RELIABILITY REQUIREMENTS onnnnnnnnnnnnnnnnnnnnnnnnnnnnnrrnnnrnrrrrrrrrrrrnnnrrrrrrrrnnnna 97 18 2 RELIABILITY DEMONSGTRATION 98 Real LEE 99 19 1 DEBRIEFING STATION E 99 19 1 1 GENERAL LAYOUT eee nen ene eee oe 99 lee 99 19 1 2 1 Cockpit Environment video sound replay sssssssnnnnnneneennnnnnnnnene 99 19 1 2 2 Aircraft external 3D AT 100 19 1 2 3 Replayed instrument A 100 19 1 2 4 Navigation charts and graphs 100 19 1 2 5 E e Ou 101 19 1 2 6 Navigation through the simulator session recorded file 101 19 13 CONFIDENTIALITY Seriene e aeeaiei ei S 101 19 1 3 1 Deletion of Simulator session recorded le 101 19 1 3 2 Data e EE 101 E RK 101 192 SPARE COMPUT E 102 19 3 SPARE SOFTWARE DEVELOPMENT EACHOITIN 102 194 TEST BENCH ME 102 19 5 ELECTRONIC BEE 102 SUMMARY Page 8 of 102 D Turkish Airlines A320 Full Flight Simulator Technical Specification This Technical Specification describes Turkish Airlines minimum requirements for an A320 Full Flight Simulator without Visual System FS Seller will specify in a detailed Technical Specification how these requirements are fulfilled Seller will produce more particularly a Compliance Matrix to match the herein Turkish Airlines Technical Specification to
15. Clock and logic sequence shall be simulated 3 8 7 Window Heat The window heating shall be simulated only to the extent that the controls and indicators operate as in the actual aircraft 3 8 8 Circuit Breakers All the circuit breakers shall be fully simulated 3 8 9 Windscreen Wipers And Rain Repellent System The windscreen wipers shall be simulated only to the extent that the control switches are active on visual displays and sound system under instructor weather condition control The aircraft rain repellent system control shall be installed as applicable to the cockpit Operation of the rain repellent system shall not be simulated 3 8 10 Sensors Due to the use of A C equipment simulation refer to paragraph 3 1 the Seller shall take a special attention to this part of simulation In particular sensors shall be fully simulated including errors and deviations each time that these effects affect equipment behaviour Consequently simulated equipment shall take into account these sensor errors and compute the same correction as the real ones whenever necessary Relative sensor position shall also be taken into account to improve computation results 3 9 MALFUNCTIONS The Malfunctions list is defined within the Airbus document EAMLFFFS For each malfunction causes and consequences are detailed The IOS malfunction pages shall be customised according to A C version selected at FFS launching In case of Data Pa
16. Page 89 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 15 2 4 Schedule The last part of the ATM shall be sent to THY for approval not later than three months before the In Plant Acceptance period Updated ATM and functional analysis document shall be sent to THY for approval not later than one month before the In Plant Acceptance The ATM and the functional analysis document shall be updated in accordance with modifications implemented to the FFS 15 3 REGULATORY AUTHORITIES QUALIFICATION TEST GUIDE 15 3 1 Documents The manufacturer shall provide a complete set of Qualification Test Guide QTG for each A C version with final data and within the time schedule as described in chapter 14 1 The QTG shall include all the tests required by the Authorities and shall be produced in accordance with the Authorities official documents referenced in the chapter in the chapter 1 The manufacturer shall implement the test system with digitalised aircraft data for all tests required in the list of validation test If the aircraft manufacturer did not provide digitalised data the simulator manufacturer shall digitalise the data manually All the documentation needed to carry out the Master QTG shall be provided e The layout of this documentation will be checked and shall be suitable to THY The tool will allow some modifications if necessary and the documents must be clear easily readable and convenient e Dat
17. SIMULATION 4 5 1 Navaids Data base The FS database shall be worldwide It will be created with a Navaids Database using ARINC 424 xx format This format shall be defined upon contract signature and by default it shall be the format valid at that time Since THY uses military airfields for domestic flights as well military airfields used for commercial operations in Turkey should also be added into the navigation database from other sources Page 33 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification All parameters defined by the ARINC 424 xx format shall be taken in account to provide a realistic simulation of the navaids 4 5 2 Navaids Processing It shall be possible to process at any time any Navaid when the A C is within range On some airport landing strips there are two runways with the same ILS DME frequency In that case during approach the ILS DME of the opposite runway shall be automatically failed without any action on IOS In the same way the recovery of this failed ILS DME shall be automatic as soon as an approach is performed on its runway A magnetic variation calculation program shall be used for all points of the earth 4 5 3 Navaids Failure It shall be possible to fail all or part of multiple installations The name and type of any failed navaid shall appear on the Instructor Operating Station A list of airport in use navaids shall be proposed by default when navaid failure
18. These stowage facilities shall be able to withstand the maximum accelerations and vibrations produced by the motion system without dislodging or causing damage to their content e Service outlets Sufficient service outlets shall be provided in all simulator area each cabinet under platform visual platform computer area HPU Page 41 of 102 3 Turkish Airlines A320 Full Flight Simulator Technical Specification 7 INSTRUCTOR OPERATING STATION IOS 7 1 GENERAL As a Man Machine Interface IOS shall comply with the general requirements below It shall be designed to be user friendly and self explanatory to the non familiar Instructor Allow the Instructor to operate in a fully forward style Forward Facing concept FFIOS and capable of giving him freedom to move in the cockpit should he desire with all the controls within his reach The IOS environment shall conform to basic instructor operation needs in terms of ergonomics accessibility to different devices lighting visibility of crew and cockpit comfort of use etc The access to crew seats must be easy and simple The instructor must have an easy access to central pedestal The IOS shall not interfere with a normal use of the complete aircraft cockpit configuration IOS pages shall be customised depending on A C versions engine versions and units more generally any model customisation Limits and units will be based on the model configuration loaded Safety the
19. Turkish Airlines A320 Full Flight Simulator Technical Specification e Maintenance Mode This mode shall be applicable only to the permanent FMPrep The COPY TEMPORARY button shall be replaced by a COPY PERMANENT button with the same capabilities but stores the new FMPrep in the permanent window at the bottom of the list A REMOVE PERMANENT button shall allow to remove a selected permanent FMPrep In addition it shall be possible to modify the FMPrep names and the FMPrep order in the list 3 4 3 FM Copy Load 3 4 3 1 General Performance The purpose is to provide the user with the facilities to Copy store or Load reload FM parameters as defined in paragraph 3 4 2 1 This function will cause the FMGC to internally store or reload the data The complete store reload process shall not take more than 5 seconds 3 4 3 2 Link with IOS FM Copy Load functions shall be directly accessible through the IOS pages e FM COPY e FMLOAD 3 5 ATIMS PRE FANS CONFIGURATION 3 5 1 Introduction The Air Traffic and Information Management System ATIMS in Pre FANS A configuration comprises Airline Operational Control AOC 3 5 2 AOC Applications A full simulation shall be provided for AOC applications listed below This means that the interface between cockpit and ground station IOS shall be fully simulated The Seller shall provide e A solution to load all AOC files via the network applications and datab
20. axis Range of movements of the seat shall allow the instructor to have a proper view on crew s operations and cockpit flight instruments The seat shall also be fitted with 2 writing surfaces with raised edges one at each side of the seat They shall be at least A4 format They shall be fitted with penholders and a recess for small objects spectacles 2 book storage areas one at each side of the seat They shall be large and deep enough to allow the instructor to stow FCOM sized manual as well as A4 student files 1 telephone storage under the left armrest refer to paragraph 6 6 Suitable reading lights adjustable in position and brightness Page 43 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 7 2 3 2 Observer Seats Two observer seats shall be provided with upholstered and adjustable armrests and movable on rails fitted into the floor with the same displacement capability as instructor s one Their track shall comply with the general ergonomic requirements and allow the observers to the best field of view considering the primary objectives for the Instructor 7 2 4 Pushbuttons Panels and Controls Located on the Instructor Seat Following devices shall be located on the Forward Faced IOS seat at a convenient position so as to be easily accessible by the instructor in accordance with overall objectives in terms of ergonomics Hardware Push Buttons shall be located on the ar
21. deactivation shall remove immediately all effects linked to this scenario only one scenario shall be selected at the same time e Intruders shall be graphically represented on the IOS MAP with the same shape and colours than on ND e Collision time shall be displayed on IOS TCAS page and collision time shall not exceed 90 seconds e An AIRPORT TRAFFIC button shall be displayed to control a popup menu allowing the following choices Heavy traffic 10 aircraft Medium traffic 5 aircraft Light traffic 1 aircraft Off No aircraft 3 7 3 Scenario and Airport Traffic Modification A user friendly software utility shall be provided to create modify TCAS scenario 3 8 SYSTEM WITH PARTIAL SIMULATION SPECIFIC REQUIREMENTS The following systems shall be simulated according to the following restrictions 3 8 1 External Lighting External lighting such as navigational lights landing lights shall be simulated in relation to electrical loads and visual display when these are significant Controls shall be located and shall function as in the aircraft 3 8 2 Air Conditioning And Cabin Pressurisation The aircraft air conditioning and cabin pressurisation systems shall be simulated to the extent that flight compartment control and indicators function as per Aircraft Data The simulated air conditioning and cabin pressurisation systems shall not have effect on the FS flight compartment 3 8 3 Electrical Power The installa
22. including as a minimum Previous and new configurations display FMS loading in progress FMS loading complete FMS loading fail problem detected during loading In this case the seller shall provide a solution to reload FMS 4 The ability to load the both FMS at the same time 5 The maximum loading time shall not exceed the loading time for 1 FMS when using the MDDU 6 The FMS Loading back up solution shall be to use the MDDU as on aircraft FMS updates shall also be available by Multi Disk Driver At the end of the simulation loading an automatic check shall be provided to guaranty the consistency between FMS files loaded and FMS files selected within A C version Loading time of FMS files to the rehosted FMGC should not exceed loading time with Portable Data Loader to the H W FMGC 3 4 2 F M Preparation Copy Load 3 4 2 1 General Performance The purpose is to provide the user with the facility to load the FMGC with any FM Preparation FMPrep that would have been previously inserted through the Captain or F O MCDU Page 14 of 102 K Turkish Airlines A320 Full Flight Simulator Technical Specification F M Preparation COPY LOAD PERMANENT TEMPORARY NETWORK IMPORT FMPrep FMPrep FMPrep 1 XXX 1 LFBO LFPO 1 ZZZYYYYYY XXX 2 YYY 2 YYY Created 02 10 3 ZZZ 14 55 PA N 50 FMPrep maximum COPY TEMPORARY The FMPrep shall mean and include all MCDU data pages as entered during cockpit preparation
23. list inventory e Technical Publications Refer to paragraph 17 1 e Documentation associated to Seller software production Refer to paragraph 8 2 4 4 e Cross reference list of cockpit equipment and or FS equipment such as power supplies interface addresses computer addresses system diagrams numbers e UO Systems diagrams e Wiring list for chassis cable and subassemblies Full sub assembly technical documentation referenced part lists Hardware Software functional diagram and component location diagrams System Maintenance Manuals Maintenance Operating Manuals Safety Manual Periodic Maintenance Manual Mechanical assembly drawings Fault isolation manual Trouble shooting and test and adjustment procedures Mount dismount procedure save backup procedures Part list and assembly list to include part number vendor part number and code localisation and quantity Software Procedures Manual Software User Manuals Software Design Documents Malfunctions Definition Document Instructor Manual 12 4 6 Motion And Control Loading System Seller shall provide all necessary tools to maintain the system e Leg dismounting tools and equipment temporary stand e Special mechanical tools equipment etc e The general design of Electro Mechanical Control Loading system shall be modular and the parts shall be replaceable between channel where applicable Page 80 of 102 Turkish Airlines A320 Full Fligh
24. main training centre network Tools to program this bridge shall be supplied e An Ethernet connection plug compatible with THY s Ethernet equipment 8 1 5 Spare Capacities Computers and interface shall have at the end of the project the following spare capacities while simulation is running real time tools included Real Time adjustment and debugging tool Real Time data survey tool FS performance test system e 50 spare memory e 50 spare time in all the computer elements and peripherals CPU memory buses internal external buses etc e 30 spare computer busses bandwidth e 30 equipped spare in the interface and 30 of expansion capability e 50 spare disk space the disks shall enable to store at least three releases of the complete software and data for all A C versions Seller shall provide a specific tool demonstrating that the above requirements are fulfilled Simulation shall be monitored so that it is stopped in the following cases e Should any synchronous or asynchronous task aborts e Should any synchronous task overruns the basic cycle time e Should any arithmetic exception appears e Should the execution time of an asynchronous task is exceeded 8 1 6 Software Development Facility A capability shall be provided to support multi background operations during normal operation of the FS including following items Page 61 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification
25. minutes A smoke available indicator shall be provided at the Instructor Operation Station The instructor shall have the possibility to stop smoke generation at any time even if malfunction is still inserted A message shall be displayed on the integrated display outside the FFS during smoke exercise The smoke generator agent shall be be non toxic and harmless to personal equipment The smoke shall be dissipated from the cockpit rapidly by cockpit exhaust fans outside the building This smoke evacuation system shall not generate audible noise level in the cockpit able to disturb the training The visual mirror compartment shall be smoke proof in order to avoid any cockpit smoke propagation and visual display quality degradation The exhaust fans shall stop if running when smoke is generated For safety hot pieces of smoke generator shall be clearly indicated Internal temperature of oil boiler shall be indicated An off line command of the smoke generator shall be provided Seller shall provide a suitable device to avoid cockpit smoke generation from triggering the FS premises smoke detection system Refer to paragraph 13 4 4 Page 36 of 102 3 Turkish Airlines A320 Full Flight Simulator Technical Specification 5 TOLERANCES Final acceptance tolerances for the objective tests must meet the most restrictive tolerances defined in the list of tests which are included in the authorities official documents referenced in the chapter
26. of all slides and or opening of all doors to be toggled from a page by respective single buttons or individually by touching each slide or door A close doors in sequence facility shall be added on this page with an appropriate period A function Cabin ready shall be added to the same page refer to paragraph 3 8 5 2 Cabin Ready info shall also displayed on ECAM 7 2 6 11 Navigation Maps The A C displacement shall be visualised on dedicated page MAP The map shall be centred on runway on A C position MOVING MAP The map scale shall be variable 10 20 40 80 160 or 320 NM The scale reference shall always be easily visible Following parameters shall be permanently visualised and adjustable A C position latitude longitude altitude heading IAS Repositioning shall also be possible by touching the required position on the screen with the finger or by selecting the navaid at which the FS shall be positioned A C position altitude heading and IAS shall be slewable The slew process shall be applied so that the simulation reaches the desired values in a smooth manner Radio Aids shall appear on the map with colour code and type in accordance with ND symbolism Preset snapshots shall appear on the map with numbering conform to their selection order Weather storm selection and control shall be in accordance with Weather radar requirement chapter ref 3 6 Page 50 of 102 3 Turkish Airlines A320 Full F
27. person e date Page 90 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification e data package references used for the answer e The list of FFS program modified and the revision level Data base updating will be made by Seller with information sent by THY DRs shall be considered as ready for recheck RFR when THY has received the information and the updated programs are available to load into the FFS The Seller shall indicate estimated dates to solve DRs in the database 15 5 IN PLANT ACCEPTANCE e First an initial Fly out by THY pilots shall be performed before In plant acceptance to ensure that simulator is enough mature to begin in plant acceptance Without this green light in plant acceptance can t be performed e In Plant Acceptance shall be conducted using ATM QTG and the Aircraft Acceptance procedure and conducted in two phases gt Hardware Acceptance gt Functional Acceptance In accordance with the analysis and data THY will have the possibility to perform some complementary tests during acceptance period 15 5 1 Hardware Acceptance Of FFS THY shall perform hardware acceptance considering the following requirements e FFS should be compliant with the Technical Specification of the FFS e Hardware configuration of the FFS should reflect the changes agreed during the progress meetings and Interface Control Document meeting e All the components used on the FFS shall be brand new e Fun
28. simulated to the extent that related controls visual and audio indications and speakers are operable within the flight compartment 3 8 5 2 CIDS Cabin Ready The Cabin Ready function shall simulate the actions on CABIN READY Pushbutton situated on the Forward Attendant Panel It shall be simulated to cover the two following modes in accordance with the CIDS logic 3 8 5 2 1 Link with IOS The CABIN READY memo shall be simulated according to IOS refer to paragraph7 3 4 10 selection through two control buttons e AUTO MANUAL e ON OFF 3 8 5 2 1 1 Automatic mode Default mode The CABIN READY memo shall be automatically displayed e 5 minutes after door closed and slides armed This delay shall be applied only after Gate Parking repositioning e During Approach and Landing phases The CABIN READY memo shall be displayed after Flaps extended to 2 and gear down selected 3 8 5 2 1 2 Manual mode After selection of the MANUAL mode the ON OFF button shall become active greyed in AUTO mode and emulate the activation forward cabin ready control by the flight attendance 3 8 5 2 1 3 Cockpit Voice Recorder Cockpit Voice recorder panel shall be installed as in the aircraft Volume level indication and erase logic shall be simulated Page 27 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 3 8 6 Flight Recorder System The flight recorder panel shall be installed as in the aircraft
29. the FFS performance and operation as required in the QTG Qualification Test Guide part of the authorities official documents referenced in the paragraph 1 General Requirements The system consists of the following e A1 Aircraft data management Aero engine flight control etc A2 Test management A3 Documentation management A4 Aircraft type management FS A5 Library management A1 Aircraft data management This function will enable the management of the aeroplane reference tests provided on data files by the aeroplane manufacturer including at least Page 63 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification e Creation of a data base of aeroplane tests for all aeroplane simulated versions e Addition deletion replacement of aeroplane reference tests in this data base e Display the aeroplane parameters of the selected test on a graphic screen and print them to a file or a printer e Identification display and print of the list of aeroplane parameters used e Identification of the tests versus the aeroplane version A2 Test management This function will be used to e Create modify and delete FFS tests e Run tests and print results to a file or a printer both must be available e Create and modify all documentation related to the test and necessary for the QTG document and print to a file or printer e Print the test technical contents parameters used outputs pro
30. the same training session for the same reason the failure time will then be equal to the entire training session time Erratic failures The FS shall be considered not meeting the requirements if glitches occur repeatedly during the training periods Such glitches are defined as transient interruption in normal FS performances not traceable to malfunctions If at any time the reliability is below this standard the Seller shall correct design deficiencies on an expected basis Page 97 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 18 2 RELIABILITY DEMONSTRATION For a period of 90 consecutive days the FS shall perform in accordance with the reliability objectives of chapter 18 Computation procedure At the end of the first 90 days the reliability rate will be computed In case the requirement is met the demonstration period will be deemed complete In case it is not met the period will be extended by the necessary amount of days to reach the requirement on 90 consecutive days Until the reliability demonstration is complete a Field Service Engineer employed by the Seller shall be stationed at THY s FS site Refer to paragraph 17 2 The demonstration period shall begin on Seller completion of the following Final acceptance complete FS Approval given by Authorities at the Level defined in paragraph 1 FS Hardware and Software configuration stabilised Page 98 of 102 Turkish Airl
31. whole design of IOS and aft compartment shall comply with the general rules of Health and Safety refer to paragraph 13 4 The AFT cabin layout including instructor seat s configuration one IOS Screen on each armrest and rails location shall be defined and agreed between THY and Seller during design reviews at the beginning of the project Seller shall present at Preliminary and Detailed Reviews a general 3D mocked up layout to THY for agreement 7 2 INSTRUCTOR STATION LAYOUT 7 2 1 Hadrware Layout The layout of IOS shall be oriented towards Forward Facing concept FFIOS which means that all the important IOS functions shall be controlled by the instructor while seated on the IOS seat whatever its position in the cabin The final configuration of IOS seat and the aft cabin layout including IOS controls means screens and buttons Ergonomics issues Seat s displacement capabilities in the different axis Miscellaneous equipment such as ACP lights control switches telephone book stowage and working surface shall be defined after having reviewed the different Seller s proposed solutions and mutually agreed at Design Review Page 42 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 7 2 2 Screens IOS will have set of two 2 high resolution full colour flat touch screens Their dimension and image quality must be such that simultaneous text and graphics shall be clearly legible from Instru
32. wrist strap 12 4 2 Cockpit Instructor seats shall be interchangeable and easy to install remove Instructor seats shall be equipped with interchangeable seat covers 12 4 3 Aircraft Boxes Airflow to aircraft boxes shall be monitored any deficiency shall be signalled to the On line Diagnostic system Wiring shall be easily accessible for modification and or replacement Full A C box plugs shall be wired to a dedicated patch panels Local circuit breakers shall be provided for A C boxes removal 12 4 4 Visual System Stowing devices for remote control boxes shall be mounted in suitable places inside the cockpit Page 79 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 12 4 5 Computerised Documentation Seller shall provide computerised documentation together with two complete paper sets of documentation including hardware software and tools Seller shall provide processed technical documentation on the PC stations and accessible printable from the FS engineering terminal The computerised documentation shall be easy to access search annotate and shall include revision control The Seller shall provide the means to consult implement and modify the documentation data and database organisation THY and Seller shall agree on the software documentation format at the beginning of the project The documentation shall be structured to provide the maintenance engineer with e Documentation
33. 1 TCAS Environment 3 7 1 1 TCAS airport traffic This shall represent a realistic traffic environment around any airport It shall consist of up to 10 aircraft flying realistic approaches and departure routes and holding patterns Page 23 of 102 D Turkish Airlines A320 Full Flight Simulator Technical Specification 3 7 1 2 TCAS scenarios definition Each scenario shall include intruder s which shall have predefined path and type as described in the following table TYPE IOS page title INTRUDER INITIAL ACTION REQUIRED BY TCAS TYPE INTRUDER THE CREW POSITION NON ADVISORIES TRAFFIC 1 Proximate traffic PROXIMATE TRAFFIC Mode C Same level Right No action needed SAME LEVEL RIGHT transponder P REANA TANOACTTUDE DATA f ModeA weem Ro TRAFFIC ADVISORIES E ABOVE LEFT transponder Traffic Adivisory no Altitude TA CONFLICT Mode A Forward same level Action required Data and potential collision NO ALTITUDE DATA transponder FORWARD SAME LEVEL E Traffic Adivisory no Bearing TA NO BEARING DATA Mode C Below left No action needed aa es LEFT transponder 5 Traffic Advisory Mode C Mode S Aft below No action needed ANELON transponder RESOLUTION ADVISORIES Z O O S O RESOLUTION ADVISORIES Preventive Resolution RA PREVENTIVE Mode C Mode S Forward same level Maintain current flight path Advisory MAINTAIN V S transponder FORNARI SAME Goen 6 This scenario includes two intruders coming from the same position but with diffe
34. 2 minutes If no FM loading required during the launch phase Refer to paragraph 3 4 1 e Efficient check facility e Simple and rapid aircraft version identification along with automatic display of main options on the IOS e Use of only one memory support for all versions implementation e Identification between various modules source code executable code loader defined with THY Discrete input programming shall be used for version consistency verification Full cockpit lighting shall be provided during the hardware and software version change 12 1 3 Air Conditioning The Seller shall provide airflow sensors in all sensitive areas so as to detect any ventilation failure that could induce hardware equipment failure These sensors shall be signalled and clearly identified 12 1 4 Overheat Detection A two level overheat detection system shall be installed e When the temperature reaches the first level it will activate an aural alarm and alert on line diagnostic system e When the temperature reaches the second level it will disconnect the main input connector in the power cabinet shutting down the simulator 12 2 ON LINE DIAGNOSTICS 12 2 1 General The Seller shall provide a powerful on line monitoring and diagnostic test which continuously monitors the whole FS and gives all the information necessary for maintenance and repair All interface boards and electronic sub assemblies shall contain local intelligence to repo
35. 3 Page 57 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 7 2 6 36 Radio Chatter messages Refer to chapter 4 5 4 7 2 6 37 Simulator Session Recording control page A specific IOS page shall be provided as per described in paragraph Hata Ba vuru kayna bulunamadi 7 3 USER S GUIDE A User s Guide paper and interactive PC CDROM shall be provided by the Seller e This document shall be designed so as to help the Instructor in a logical step by step procedure through out the preparation and performance of a training session e This document shall cover in particular safety aspects pertinent details about the Motion and CLS controls a chronological list of all OS accessible screens and functions e This document content shall be defined in common with THY so as to comply with THY procedures It must be ready about one month before the FS Factory acceptance e This document shall be updated to reflect all FS evolutions until final RFT Page 58 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 8 COMPUTER INTERFACE AND POWER SUPPLIES FS hardware and software components shall comply essentially with the following factors e Integrity e Reliability e Maintainability e Flexibility e Safety 8 1 FS COMPUTER COMPLEX AND PERIPHERALS The manufacturer shall offer a computing unit using recognised non proprietary standards for architecture internal and exte
36. 6 TELEPHONE AND BOOM SET KEE 39 Page 3 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 6 6 1 Telephone sas cinceateneivtntenicd ete cnanihiiet A 39 G02 ele un 40 6 7 WALKWAY PLATFORM DRAWBRIDGE ssassnnnssssssssnnrrrrirrenrnnrrtrrrrrrnnnnrrrrrent 40 G Rn el 41 7 INSTRUCTOR OPERATING STATION lOS 0 EEN 42 Al Sl EE 42 7 2 INSTRUCTOR STATION LAYOUT socsssssccisiscccccsansissteiccstecesectssibindsiethencsccdeaces 42 7 2 1 TV Ee EE 42 EE 43 Te FFIOS SEa EE 43 e oe lx e Eer 43 1 2 3 2 Observer eege EECH EEN 44 7 2 4 Pushbuttons Panels and Controls Located on the Instructor Seat 44 7 2 4 1 Hardware Push Buttons Panels nnnnnnnnenennnnnnnnnnnenennnnrnnnnnrnnennnn nna 44 7 2 4 2 Simulator and Motion amp C L Emergency Stop Buttons 44 7 2 4 3 AIC Communication F AMG lisstaxstanitinscudchinanasemanansuunabetiampabaniueananiiabanes 44 i 2 AA SOUNG CONO EE 44 7 2 4 5 Overhead Light Switch EEN 44 7 246 Lighting CM EN 45 ge ae Wy EE E 45 7 2 4 8 COCK with Stop WATCH RE 45 7 2 4 9 Controls for Monitor Brightness and Contrast ce eeeeeeeeeeeeeeee 45 7 2 5 Controls not Located on the Instructor Seat ccccceeeeeeceeeeeeeeeeeeeees 45 7 2 5 1 Flight Compartment Air Conditioning Control 45 7 2 5 2 Remote Control Box for IO 45 7 2 6 Functions Controllable From The Touch screens Pages 45 7 2 6 1 Fr ez de E 46 He EAM ROSE
37. 6 32 Electronic Mountain EE 57 T 2039 ICAS SCSI MIG neer diepaianitunabin beobanianabandioes 57 112 0 04 W ather RAGAN screscrescsverceasscacnnecsscepearssasaeacsrenibenssasseadueedaneesmecasarnerens 57 7 2 6 35 ATIMS messages CON E 57 7 2 6 36 Radio Chatter messages ise cc ce oa sted sae os tae eae eee 58 7 2 6 37 Simulator Session Recording control page 58 7 9 USER S GUIDE eegene eege 58 8 COMPUTER INTERFACE AND POWER SUPP LIEGS cceeeeeeeeeeeeeeeeeeees 59 8 1 FS COMPUTER COMPLEX AND PERIPHERALS eeeeeeeeeeeeeeeeeeeees 59 8 1 1 Computers TE 59 812 PEnpheralS pzs ne E ceaeunnnse 59 8 1 3 Operating EE E 60 8 1 4 Ee 61 8 1 5 Spare ee 61 8 1 6 Software Development Face 61 8 2 COMPUTER PROGRAM SYSTEM FS SGOETITWARE 62 8 2 k General rene E 62 8 2 2 FS Real Time Executive Programs e eeen 62 8 2 9 Sim lation ele EE 62 8 2 4 Utility Program And Software Control 62 8 2 4 1 FS Support Programs EE 62 8 2 4 2 FFS performance test system veccscccseeecsssceeecc eevee stoestoustensteystoueteestenecen 63 8 2 4 3 Software control change and configuration Control 66 8 2 4 4 Software supply and documentation 66 8 9 INTERFACE eee eee ee eee ene een ae ae ee ee 67 8 3 eae G2 E 67 8 3 2 Printed Circuits Boards Aesembles ENEE 67 8 3 3 System Config ratioN a ege d e dE dE dee 67 8 3 4 Accessibility to Boards LRUs and A C Components 67 6 9 0 Expansion Capacity cient ciate ieee
38. Autopilot e All A C systems 15 6 ON SITE ACCEPTANCE Before the On Site Acceptance e The Seller should guarantee that the simulator status shall be at least at the level of In Plant Acceptance and DR status generated during In Plant Acceptance shall be on offer e All the software programs shall be compiled from the on site available current source in order to generate the code that will be used for the final acceptance and for the starting of training This task shall be jointly performed between the Seller and THY 15 6 1 On Site Acceptance On Site Acceptance shall be conducted to e Verify all the results of In Plant Acceptance after reinstallation of the simulator at THY s site Therefore In Plant Acceptance test phase to be repeated On Site Check the DR status offered by the Seller Check if any new DRs generated during reinstallation of the FFS Run the QTGs by the Seller and evaluate them Verify that any defects occurred during transportation and installation of FFS Subjectively evaluate the simulator by THY Pilot s tests Check the FFS prior to the Regulatory Authorities Certification 15 6 2 DR Clearence After RFT After the RFT date or the FFS approval THY will give the priority to each pending DRs Seller shall clear all the DRs within 6 months after RFT Any software updated to solve DRs shall be delivered with documents clearly identifying the update contents 15 6 3 Regulatory Authority Approval S
39. Except for landing gear flaps and spoilers the rest of the aircraft surfaces don t have to be dynamically animated 19 1 2 3 Replayed instruments Following instruments shall be represented and animated as per the aircraft in synchronisation with the other windows e PFD including all FMA messages CM1 and CM2 sides e ND CM1 and CM2 sides e SD and EWD including all ECAM messages e Engine throttles panel e Slats Flaps panel e Speed brakes panel e Landing Gear panel e Surfaces position and stick moves shall be represented and animated The information relative to all the cockpit switches and controls activated by the crew during the simulator session has not been deemed necessary 19 1 2 4 Navigation charts and graphs 19 1 2 4 1 Navigation charts A representation of navigation charts shall be displayed Those charts shall be the same as those used by the crew in cockpit and shall be geo referenced so that the system switches from one chart to another according to the aircraft geographical position and the phase of flight The continuous track of the aircraft as well as the aircraft symbol shall be displayed at their proper location in the chart Page 100 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 19 1 2 4 2 6 2 4 2 Graphs Three types of graphs shall be provided e Approach plot showing lateral and vertical deviation versus ILS e Runway Plot showing lateral deviation versus runway
40. G 1 FAIL ENG 2 FAIL ENG 1 FIRE MASTER RESET ENG 2 FIRE WIND WINDSHEAR SPEED UP X 4 7 2 6 Functions Controllable From The Touch screens Pages The graphical interface shall be easy to use and utilising latest display methodologies and graphics The interface shall be designed in order to permit the instructor to find out easily and quickly when searching a particular function For this purpose a Master Index page shall be provided that will give access to each instructional feature specific page Training pages will be determined by THY at the time of the related freeze date of the project Most important training page such as Airport Select Weather Visual Navaids A C Loads Repositioning Runway conditions Services Freezes and Resets as well as Recording control icon shall be accessible from any page through permanent icons Page 45 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification The colour scheme shall be consistent and sensible so as to facilitate user s comprehension All graphical icons shall be sized and located on screen so as to prevent inadvertent selection Automatic boxes shall appear automatically further to instructor action such as parameters modifying or other selection i e left right up down etc request Those boxes shall not hide essential information on page The box dedicated to parameter setting shall propose both e A graphical alphanumerical keyboard for direct di
41. MESGAOES Figure 6 AOC Menu Page The functions of the impending window are described in paragraph 3 5 3 1 The CLEAR FOR NEW SESSION button shall clear all the previous AOC communications Reset of the impending messages and AOC LOG page contents 3 5 3 3 AOC LOG Page The AOC LOG page shall contain functions as per shown in figure 7 AOC LDG annie fait fda TIME Det St AU DUT REGUE Figure 7 AOC Log page The AOC LOG button from any other AOC page shall select this page It shall display the complete history of current AOC communication in chronological order including uplink and downlink messages Page 19 of 102 D Turkish Airlines A320 Full Flight Simulator Technical Specification The Message descriptions shall be displayed on one row For the downlink messages listed refer to paragraph 3 5 2 a REPLY button shall be displayed This button when pressed in shall call the AOC REPLY page refer to paragraph 3 5 3 4 This REPLY button shall be provided with the following functions e For the downlink messages requiring an answer F PLN init WXR VOICE contact FREE TEXT the REPLY shall flash until the appropriate answer is sent to the A C e For the downlink reports without answer requirement a DESCRIPTION button shall replace the REPLY button Pressing this button shall permit to display the entirely message 3 5 3 3 AOC REPLY Page The AOC REPLY page shall contain function
42. N A E A A N AET 46 1 20 39 e 47 Fc E 48 1 20 09 Eelere 48 T206 EE 48 FG Fe NAVAS E E E E 49 7 2 6 8 ell in ee 49 7 2 6 9 Nose Wheel Steering function 22 2 cseeeceeeeeeeeeeeeeeeeees 49 7 26 10 DOOTS CABIN EE geed aoc cee co 50 7 2 0 11 Navigation MEDS sue 50 7 2 6 12 Permanent visualisation of parameters nnsnnsssesessnnnrnreereeenenn nna 51 7 2 6 13 SNADSMOU RECA iicetncccstiiecccascoedsiodidestandeoataoadisssaediatenadarstaaeealendes 51 7 2 6 14 Environment conditions Dre set EE 52 Vol a Hard Re 52 7 2 6 16 Position ts sosscca ceiceed coscaedcasicend EEN oasne cantceatosedectecs 52 EE 53 T20 Ve EEN 54 7 2 6 19 Flight conditions EE 55 7 2 6 20 A Q LoadiNg EEN 55 7 2 6 21 Crash Indication Ee EE EE Een 55 Page 4 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification T 2622 E 55 TAG e erence tee eter e eee teeter errr E rere terre re 56 7 2 6 24 PIC SUIS cesses se tars oceest oars oc estnsarsodees onrdocstnsatsedesonboostccederbantoceeteouades 56 7 26 25 Quick Set 0 EE 56 7 2 0 20 Help Ee e ME 56 7 2 6 27 Maintenance function 6 00c00cceecscnesssacecesesasenesessseseceeadenssenasesececedes 56 7 2 6 28 Maintenance mode accessg 56 7 2 0 29 LESSON PIAS wssasreaczecrciendeaczeadinessseosaestuaveeacaseineeanieasaevineenareeene 57 EE E VIRAL PINTE EE 57 7 2 6 31 F M Preparation COPY LOAD u cc c2s ccccccscccosssnasseantenctoaesaascassdnncses 57 7 2
43. OUND AIR WHEELS CHOCKS PUSHBACK NOSE LEFT PUSHBACK CENTER PUSHBACK NOSE RIGHT AIRCRAFT ON JACKS ENGINE QUICK START ENGINE COLD Page 47 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification e APU QUICK START e ADIRS FAST ALIGN instantaneous IRS alignment e SPEED UP pop up menu shall be displayed and selections of X2 and X4 shall be available Once speed up function has been engaged ground speed acceleration shall occur smoothly in order to prevent spurious effect i e sudden acceleration on PFD SPEED UP X2 and X4 functions shall be toggle type press once shall activate the selected function press again shall deactivate it 7 2 6 4 Airports It shall be possible to select the desired airport by its international code Special feature shall be provided to facilitate airport selection in helping to find the ICAO code The default airport shall be customised and automatically selected at simulation loading depending on the operation site All airports contained in the FMGC Navigation database shall be available A generic model shall be used when no specific model is associated 7 2 6 5 Weather e Ground level TEMPERATURE refer to paragraph 4 1 3 e Sea and ground level BAROMETRIC PRESSURE refer to chapter 4 1 3 e SURFACE WIND refer to paragraph 4 1 1 e Six different three dimensional WINDSHEARS refer to paragraph 4 1 1 1 e TURBULENCE level selectable by percentage refer to p
44. RDWARE REQUIREMENTS 9 2 1 Power Requirements Control Loading System will be powered via UPS therefore main power box of the control loading system shall be separate from motion main power 9 2 2 Start of Electro Mechanical Actuator The starting of Electro Mechanical Actuator shall be controlled locally and remotely from the motion cabinet and IOS 9 2 3 Failure Detection The following features will be monitored by means of software checks PCB operational status including an independent hardware watchdog function Excessive position error between demanded and actual control positions Excessive control velocity error Excessive control force Excessive control power Control loading programs not running Loss of power supply Any of these conditions will immediately isolated the system by removing power to ensure operator and user safety 9 2 4 Reset Failures reset shall be possible from push buttons located on IOS and motion cabinet 9 2 5 Safety Requirements To minimise possible hazardous conditions especially at initial conditions and in case of catastrophic failures both easy on and rapid isolation features shall be incorporated When the control loading actuators are isolated from electrical supplies the flight controls can be positioned anywhere within the actuator stroke to facilitate access to both pilot stations and to instrument panels For maintenance purposes safety inhibit switches shall be available on the
45. RSION SELECTED AT FFS LAUNCHING ucosncstansniedincatenstecaneratmatacatadeenaienabaeetocadncameatacaianetedione 28 3 10 OEB IMPLEMENTATION HEN TN E EE 28 ENVIRONMENT SIMULATION cccccccccsssscceseseccseeecseeecseeeeaeeeenaueeeneeeneaeeees 29 GR Bo EE 29 A Alle WINGS ANG TIUMBUIBINIGE rosies 29 4 1 1 1 Windshear and microburst cxieecveccvececencsees vest vesevanesbecdsansbussessebsavoesvmense 29 4 1 1 2 KN e 30 4 1 13 Ri H OS EEN 30 4 1 1 4 Effects selection and e e e 31 41 2 ale elen pee ee ee eee E E 31 4 1 3 Temperature And Atmosphere Pressure 31 he RI AN EE 31 4 21 RUNWAY E 31 4 2 2 Runway le EE 32 4 3 TERRAIN PS Eeer 32 44 SOUND SIMULATION WE 32 4 5 NAVIGATION AND COMMUNICATION ENVIRONMENT SIMULATION 33 45s Navaids Lieler 33 4 5 2 Nav ids PC SSM e E 34 45 3 Navaids ar lt ee ee ee ee 34 4 5 4 Communication ZEIEN gded ere egen 34 4 5 5 RT and ATC Radio e E 34 4 5 6 ATIS Simulation 0 ceccccccceeececeeceeeceeeceeseeeeeceeseeseeeaeeeeeesanseeseesaneees 35 4 5 6 1 General poertormance A 35 4 5 6 2 Links with e ee ace cee ec cies cic aun neds 35 4 5 6 3 ATIS message modification nnee 35 4 6 TEEN EECH Eeer ege 36 TOLERANCES EE 37 FLIGHT COMPARTMENT eege egeeee Zeene 38 6 1 GENERAL EE 38 6 2 FLIGHT COMPARTMENT GENERAL ARHRANGEMENT 38 e EIN eer 38 6 4 VENTILATION AND AIR CONDITIONING occ ccc eccceeeeeceeeeeeeeeeeeeaneeees 39 6 5 INTERIOR NOSE LEVEL eege Ee EEGENEN 39 6
46. Seller Technical Specification Seller Technical Specification which will include notably a detailed description of the hardware and software of the FS configuration together with all necessary diagrams schematics photographs general layout motion envelope with 3 LCoS projectors visual system with minimum 180 X40 collimated mirror Three hard and soft copies of the Technical Specification shall be sent to Turkish Airlines Definitions THY THY means Turkish Airlines Inc Seller Seller means FS manufacturer Flight Simulator FS Flight Simulator or FS means the flight simulator including optic system and integrated with A320 Aircraft Data Package Aircraft Parts and Aircraft Equipment FS can be integrated with any Level D Visual System Full Flight Simulator FFS Full Flight Simulator or FFS means FS integrated with level D Visual System DPE DPE means A320 Aircraft Data Package Aircraft Parts and Aircraft Equipment This Technical Specification has been generated by modifying AIRBUS Standard A320 Full Flight Simulator Specification Page 9 of 102 D Turkish Airlines A320 Full Flight Simulator Technical Specification 1 GENERAL REQUIREMENTS Airbus A320 FS shall be based on Airbus standard 1 6 THY will have the capability to configure the FS to 2 standard models listed below e A320 232 V2527 AN A320 214 CFM56 5B4 FS will have e Re target Re hosted FMGC e Simu
47. Station Special motion cues shall be simulated for these runway types Page 31 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 4 2 2 Runway Conditions The runway conditions will be those required by the authorities official documents referenced in the chapter 1 They shall be available from IOS Representative braking stopping and directional effects for these runway conditions shall be simulated All visually available runway conditions of IG shall be controlled by IOS 4 3 TERRAIN PROFILE Terrain profile shall give a realistic reproduction of the ground altitude variations in the vicinity of the simulated airports and on runways and taxiways There shall be cross talk from visual computer to the host computer to ensure correlation between environment profile and visual profile 4 4 SOUND SIMULATION Sound simulation must meet Level D standard as defined in the Authorities official documents referenced in the chapter 1 All necessary tools for recording and analysing purposes licenses and procedures shall be provided to THY 4 4 1 Sound fidelity Sound simulation shall be correlated with the whole simulation and shall include all real cockpit audible sounds Sound shall be at an appropriate level through adequately baffled speakers at appropriate locations to give proper directional effect to each source of significant sound Particular attention shall be put on environmental sounds with
48. THY s basic requirements for the Visual System parameters setting shall be decided during the project and ICD Page 74 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 12 OPERATION AND MAINTENANCE 12 1 OPERATION FS versions are defined in the Chapter 1 General Requirements Tools additional equipment panels shall be designed to facilitate assembly disassembly with the maximum of safety 12 1 1 Start Up and Shut Down Procedures FS start up and shut down operation shall be described step by step in a document provided by Seller Each step shall be covered in terms of action normal abnormal result corrective procedure e Total time from the commencement of start up from power off to all systems operating will be less than 10 minutes Computer boot time 7 minutes Simulator start time 3 minutes e FS real time load shall be capable of being launched from the terminals in the computer room and the cockpit e For user information appropriate status messages reporting each major step of simulation loading should be displayed on these terminals e The host and sub systems computers will have clearly defined initialising and loading routines e FS will be provided with an interlocked power up procedure e Loading FS software at simulation start shall be carried out with minimum of steps and from only one device at a time e FS control file refer to paragraph 8 2 1 and airline s co
49. WEE 89 15 2 ACCEPTANCE TEST MANUAL ATM 2 22 202000c0ccccccccccccecceecscssceees 89 15 2 1 Acceptance E TTC 89 Eo Ee E 89 15 23 e 89 Ve 2 SCN EE 90 15 3 REGULATORY AUTHORITIES QUALIFICATION TEST GUIDE 90 T93 la pl e NIS aae E A E danas tea sbue A ansqgasdaiaanadiea sais 90 15 3 2 Hardware Facilities For QTG Tests 90 15 4 DISCREPANCY REPORTS esoe 90 15 5 IN PLAN T ACCEPTANCE E 91 15 5 1 Hardware Acceptance Of EES 91 Page 7 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 15 5 2 F nctional Acceptance sicer r iE 91 15 6 ON SITEACCEP TANCE canicas naniii edd e niai 92 15 6 1 On Site Acceptance cccccccccceeeeseeeeeeeeeeeeeeaeseeeeeeeeeeeeeeeeseeeeeeeeeeseees 92 15 6 2 DR Clearence After E 92 15 6 3 Regulatory Authority Approval AAA 92 16 ON SITE INSTALLATION WEN 93 16 1 FACILITY REQUIREMENTS ease sett ease ee EES 93 16 2 INSTALLATION iterate eee 93 16 3 EEN 93 17 TECHNICAL SUP POR sisiascissctisanciiaes vencvansvenciaes vencvansvenchaesvancvansvenchaasvancvassueesbacaue 94 17 1 TECHNICAL PUBLICAT ION n nnnnnnnnnnnnnnnnnnnnnnnnnnnrrnrrrrrrnrrrrrrrrrrrrrrnrrrrrrrrrnr renn 94 171 1 Ge ee EE 94 17 2 FIELD SERVICE ENGINEER ssosieuctccncesceceedecencreceesnensesonsteecesbaceedecenccseenencdancs 94 17 3 SPARE PARTS MAINTENANCE TOOLS AND TEST EQUIPMENT 94 17 4 SIMULATOR LIFE CYCLE SUPPORT DARAMATERG 95 Ke RR E an
50. a quick wiring portion replacement solution shall be provided e If fibre optic cables should be used spare fibre optic cables shall be routed and equipped with the connectors 13 2 INTERCHANGEABILITY amp LRU REPLACEMENT All parts having the same manufacturers part number shall be physically and functionally interchangeable with respect to the equipment performance and FS installation Access to LRU Line Replaceable Unit Instruments boards computers etc for operational purpose shall be made clear and easy for replacement Duration of this replacement shall be within a reasonable time In the Maintenance manuals the duration of LRU replacement shall be mentioned in minutes All inter unit connections shall be by means of plugs and sockets all of which shall be identified in such a manner as to facilitate interchange and to avoid the possibility of misconnection It shall be possible to replace the Captain and F O aircraft stick from the cockpit side Connectors and their related cables shall be long enough to allow THY maintenance crew to install and remove LRUs easily Page 83 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 13 3 MARKINGS 13 3 1 General Configuration of all the LRUs shall be frozen before the final acceptance The Seller shall provide a database file easily accessible read write print including the designation names P N S N and the localisation for LRUs The Seller
51. a that need to be compared shall be easily comparable in the simplest way without using several documents e The test outputs shall also be of a convenient use for reading and tolerance check since the data references are overplotted scales will be adjusted for the best and easiest reading and survey e The test description shall explain how the test has been programmed i e which parameters are driven and which ones are checked with or without tolerance applied e All the technical justification from the Data package supplier about the QTG tests that have Discrepancy Reports raised by The Authorities or THY shall be inserted as a rationale in the Master QTG document either in the test description or in the introduction as a general statement In this case the general statement shall list the tests concerned and each test description shall refer to the rationale reference 15 3 2 Hardware Facilities For QTG Tests All the test equipment for QTG tests shall be provided and installed permanently on the FFS The Seller shall provide a list of these tools and equipment 15 4 DISCREPANCY REPORTS Discrepancy Reports DR raised during In Plant and On Site Acceptance period shall be listed in a data base THY will access this data base through a stand alone computer and a computer included in the FFS computer complex without any limitation This database shall include the following information about the DRs at least e name of responsible
52. abase For this purpose10 of suitable airports will be selected by THY during the project In the vicinity of these airports all EGPWS functions will be operative with full correlation between environment profile and EGPWS terrain database For airports where visual profile is not correlated with EGPWS terrain database EGPWS terrain detection function and terrain display on ND s shall be automatically inhibited when visibility is greater than 300m This automatic inhibition shall be de selectable with IOS For the installation of RAAS and SAM in the future inhibit switches shall be offered as provision as necessary 3 3 2 Electronic Mountain An icon will be available on the instructor station to activate the EGPWS on request Refer to paragraph 7 2 6 32 When EGPWS activated the radio altitude will decrease The only effects in the cockpit will be e The radio altitude value change on the PFD s e The GPWS aural and visual warning 3 3 2 1 Detailed Functions e This icon shall not be operational when the aircraft is on ground e The function shall be de activated either by pulling back on the side stick or by reselecting the icon When the function is de activated the radio altitude will return gradually to normal operation e The radio altitude shall drop down to 30 feet maximum and remain at this value in order to prevent unwanted crash in case of insufficient or no pilot action e Nocorrelation with the visual system is r
53. ail completely or partially any NAVAID and to reset it on demand refer to paragraph 4 5 3 It shall be possible also to pre arm NAVAID failure triggering on conditions as per any regular system malfunction refer to paragraph 7 2 6 17 7 2 6 8 Communications This panel allows the instructor to control communication using aircraft channels for a MECH CALL b ATT CALL SELCAL VHF 1 SELCAL VHF2 SELCAL VHF3 SELCAL HF1 SELCAL HF2 PRIVATE INTERPHONE TO CM1 CM2 and Instructor A potentiometer shall be provided to control STATIC NOISE gt O OO J Q 7 2 6 9 Nose Wheel Steering function The Nose Wheel Steering function shall respect the following logic a Automatic Default NWS DISC symbol on right hand side of upper ECAM Automatically displayed When aircraft parked at gate and during pushback Automatically removed e When Pushback completed and parking brake applied e f aircraft repositioned away from a gate position Page 49 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification b Manual When the aircraft is on ground and stopped the NWS DISC symbol may be displayed removed according to IOS selection Button to be grayed when aircraft moving Thus 2 pushbuttons are required to control Manual Auto and Connect Disconnect modes 7 2 6 10 Doors Cabin ready A doors control facility shall be available through IOS pages It shall show slides and doors Arming
54. aining Level C No Impact on Training e Guarantee of the Seller to keep the prices of the spare parts unchanged as long as 5 years after the contract signature will effect THY s preference positively e The Special Tools and Equipment needed for operating and maintaining the FS Refer to paragraphs 12 1 12 4 6 e Electronic Parts Catalogue EPC shall be provided e Warranty for the whole simulator complex shall be minimum 3 years e The Repair Turn around time 3 weeks in total for normal repair excluding transportation e The AOG procedure for critical parts the delivery time to THY site shall not exceed 36 hours 17 4 SIMULATOR LIFE CYCLE SUPPORT PARAMATERS 17 4 1 Preventative Maintenance Seller shall provide a list of preventative maintenance items with their frequency and the man hour to accomplish each task in a predicted time period 17 4 2 Consumable Spare Cost Seller shall provide a list and the quantity of consumable spare parts which shall be used for preventative maintenance of the simulator during the longest maintenance cycle Longest maintenance cycle refers to the longest frequency of the maintenance items 17 5 OPERATION AND MAINTENANCE TRAINING THY general requirements for the training is as follows Following the completion of the courses THY maintenance personnel shall be capable of operating maintaining the FFS within the Reliability target allow for standard software operation and troubleshootin
55. alking on it Motion and Drawbridge control shall be separated bridge could be raised lowered with motion at rest e The Drawbridge control buttons shall be located in the Flight Compartment and at the Drawbridge access Lighting and audible warning shall be provided during engagement and disengagement of both motion and drawbridge system Motion on lighting indication warning shall be provided below the flight compartment whenever the motion is on Detectable critical malfunctions which shall cut motion system electric power must include e Abnormal response of one of the actuators e Power supply failure e Simulation program not iterating e Actuators limits reached e Control loading not ready or in maintenance e Emergency shutdown mode e Doors open bridge not retracted The motion and CLS status motion ready CLS ready Motion inhibits doors open shall be displayed on the On Line Diagnostic refer to paragraph 12 2 The motion inhibit RESET function of the IOS shall control emergency doors mains door access bridge gate seats not in safety position and overhead kit panel if needed In the event of an erroneous computation the motion program shall automatically limit the acceleration of the cabin motion to avoid injuries for the people on board A back up device i e Drawbridge Battery will enable drawbridge extension after motion settlement with emergency electrical supply for safety interlocks In the even
56. an ATIS messages shall be provided 4 5 6 2 Links with IOS The ATIS message program page shall allow the instructor to select by ICAO the desired airport All ATIS message parameters shall be controllable on that page This page shall include the following 4 functions e ATIS OVERRIDE validation of ATIS parameter set e ATIS TO CURRENT WHEATHER copy of weather conditions into ATIS parameters e ATIS NOT AVAILABLE When selected this message will be broadcast instead of the ATIS information Supplemental messages to the ATIS broadcast shall be provided and selectable by the instructor A status page shall be displayed upon request to list all the pre programmed ATIS messages 4 5 6 3 ATIS message modification A software utility for ATIS messages modifications shall be provided Male or female voice broadcasting will be randomly selectable Page 35 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 4 6 SMOKE GENERATION Subject to the instructor selection smoke shall be introduced into the cockpit in conjunction with a simulated fire Two smoke sources shall be simulated and selectable independently from the Instructor station e Air conditioning smoke e Electrical smoke Smoke shall be non toxic and harmless to personal and equipment Realistic aircraft smoke sources shall be provided in relation with malfunction definition Preparation phase smoke system shall be available in less than 5
57. angement shall be identified by a suitable sleeve crimp tag or ink stamped marker The designation shall consist of a suitable code developed by the SELLER 13 3 6 Firmware All the Firmware will be identified with own P N and revision 13 3 7 Safety Marking All FS devices which may present a danger for user or maintenance personnel shall be suitably protected and signalled Electro Static sensitive devices shall be clearly marked Page 84 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 13 3 8 Motion System Control Forces Simulated Systems All assemblies subassemblies and replaceable units shall be clearly labelled Each designation shall correspond to the one used on system diagram engineering drawing and maintenance manuals Mechanical components of different channels within the control loading frame will be colour coded as an aid to identification 13 4 HEALTH AND SAFETY QUALIFICATION REQUIREMENTS 13 4 1 General The Simulator shall be designed to meet safety regulations of EU standards All the health and safety information markings and instruction shall be easily readable 13 4 2 Emergency Exits In the flight compartment the following emergency devices shall be provided e Emergency exit door s e Two escape knot ropes or rope ladder s 13 4 3 Emergency Power Off Emergency Power off controls shall be clearly indicated in accordance with safety regulations and the minimu
58. anumeric TEXT IOS UP Free text keyboard shall be displayed to generate free text DELAY MCDU DN Delay Report Informs the ground of an en REPORT route delay Flight plan parameters shall be at minimum Departure Airport SID waypoints airways STAR Arrival airport Alternate Airports Weather actual and ATIS reply information shall be correlated with corresponding weather airport simulator parameters refer to paragraph 7 2 4 14 In addition a set of 5 predefined weather actual messages METAR standard shall also be proposed For weather forecast request a set of 5 predefined weather forecast messages TAF standard shall be proposed in weather reply page By default 1 set of predefined weather messages shall be pre selected standard environment Only if ATIS application is available 3 5 3 AOC IOS Interface Specific AOC pages shall be provided on the IOS to simulate the communication between the ground and the aircraft For each AOC page the following permanent buttons shall be provided Page 17 of 102 K Turkish Airlines A320 Full Flight Simulator Technical Specification AOC Menu to call the AOC main menu page If not selected This page shall be selected by a dedicated icon on the instructor station refer to paragraph 7 2 4 37 AOC Log to call the AOC Log page This button shall flash at the reception of a downlink message from the aircraft and until the message is answered The message shall also come up au
59. aragraph 4 1 1 3 e RUNWAY conditions refer to paragraph 4 2 2 e RUNWAY types refer to paragraph 4 2 1 e Icing condition refer to paragraph 4 1 2 e Predictive Windshear selection refer to paragraph 4 1 1 1 e Microburst selection refer to paragraph 4 1 1 1 7 2 6 6 Visual The visual pages shall be adapted to the visual system installed on these FS A customisation process due to the different visual systems installed on the different FS shall be available for these pages They shall give access to e All functions corresponding to image feature and visual display performance e All other possibilities supplied with the chosen visual Following VISUAL categories shall be controllable through an IOS page a CAVOK b CAT c CAT II d CAT III e CAT IIIB Page 48 of 102 3 Turkish Airlines A320 Full Flight Simulator Technical Specification f Zero 2000FT 20Km h 600FT 4Km i 400FT 2Km j 800FT 6Km Visibility shall be customised according to THY needs and standard values available for US and EU rules Maintenance activation mode e Instructor station will provide functions for maintenance activation of visual maintenance controller disconnection of IGE from host and reverse connection e The login to this function shall be protected by a password 7 2 6 7 Navaids Lists of stored NAVAIDS shall be available Selection of a NAVAID shall automatically give QDM and distance It shall be possible to f
60. ariation or more generally any aircraft configuration leading to dangerous bumps on motion system an automatic freeze shall occur just prior to the effective crash Crash indication shall appear automatically after a crash A crash Inhibit button shall be available to override the above conditions 7 2 6 22 ATIS The ATIS page shall be provided with functions as described in paragraph 4 5 6 Page 55 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 7 2 6 23 SMOKE SMOKE generator and extraction fan controls shall be provided through a dedicated IOS page Smoke generation controls shall be disabled in the case the Smoke Power switch is OFF 7 2 6 24 A C Status Model identification A C version and options indications shall appear on a special page This page is automatically displayed on one screen after FS loading 7 2 6 25 Quick Set Up A Quick Set Up facility shall be provided in order to save instruction time in terms of take off data insertion on the IOS At least 30 different Quick Set Up shall be available on IOS Activating Quick Set Up shall initialise the simulator with all corresponding quick set data It means a Airport name and runway in use b Repositioning type c ATIS information d Runway status surface and conditions e Environment conditions including Wind gradient f A C load g Visual conditions h Runway lighting Quick set up contents shall be initialised with tak
61. ase The applications and database shall be directly issued from the AOC A C floppy disks as defined in A320 Std 1 6 Standard Equipment List e A dedicated connector in the ATSU cabinet in order to plug an A C Portable Data Loader All AOC applications shall be available through the MCDU For the AOC applications not listed in the table below but available through the MCDU a message NOT SUPPORTED BY SIMULATION shall be displayed in the IOS AOC LOG page Flight ops Transmission ASSOCIATED MESSAGE INTENT application Initiated on DOWNLINK AND UPLINK MESSAGES Page 16 of 102 D Turkish Airlines A320 Full Flight Simulator Technical Specification reports the ground ground speed gt 0 Automatic Automatic Automatic DN IN Report IN A C on ground at gate at eege Automatic DN Return IN Report Return In A C has returned to the terminal without taking off F PLAN init MCDU DN F PLAN init Ground sends a flight plan and IOS request See performance data to UP F PLAN INIT SE WXR MCDU DN WXR Request The crew initiates a specific Actual Forecast weather request downlink for UP WXR information specifics airports Actual Forecast ATIS MCDU DN ATIS Request UP The crew initiates a specific ATIS information ATIS request downlink for specifics airports VOICE MCDU DN Voice Contact The crew can be contacted by CONTACT IOS UP Voice Contact the operations via a specific media VHF HF MCDU On IOS an alph
62. ate all pin programming available on the aircraft These pin programmed functions shall be implemented for each model and shall be activated by soft buttons on IOS Page 10 of 102 D Turkish Airlines A320 Full Flight Simulator Technical Specification 2 CUSTOMISATION ORGANISATION 2 1 GENERAL CUSTOMISATION PRINCIPLE Each customised version that requires reloading FS should be identified by a dedicated name Reloading for customised version shall be available after verification of the requested configuration The operable current load shall also be displayed on the information window above the flight compartment door such like A320 CFM56 5B4 load is in progress or Flight In Progress A C Version etc THY will be able to easily modify this message 2 2 HARDWARE CUSTOMISATION PRINCIPLE e A320 214 CFM56 5B4 to from A320 232 V2527 A5 Conversion Timing Seller shall propose the suitable solution if required for the entire conversion of A320 214 CFM56 5B4 from to A320 232 V2527 A5 versions within 15 minutes 2 3 SOFTWARE CUSTOMISATION PRINCIPLE Software code duplication shall be avoided and the naming convention for all modules and codes shall be done properly that the software can be easily maintained Seller shall provide a document stating his customisation principles and provide a list of all customisation flags Impacted and read only files shall be listed 2 4 AIC COMPUTER CUSTOMISATION The A C computer
63. ated aircraft e The communication stations shall be automatically activated in accordance with the A C position and the selected frequency The Seller shall provide a user friendly means to alleviate the Instructor workload Page 34 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification e By proposing on IOS a predefined list of typical ATC messages These messages will be inserted within the frame of overall ATC messages when selected by the Instructor e The Instructor shall be able to communicate without any need of frequency selection The instructor will also be allowed to communicate directly through the ACP e Seller shall take special care in voice quality simulation e An user friendly utility shall be provided to add modify delete predefined messages 4 5 6 ATIS Simulation 4 5 6 1 General performance An ATIS simulation system shall be provided It shall be possible to associate ATIS facility with communication and navigation system All ATIS broadcast parameters shall be able to be initialised individually for any pre selected Airport and runway Without initialisation the messages shall be updated automatically in accordance with the meteorological and visual conditions the runway status and the radio aids status selected at the Instructor Operating Station The frame of the messages shall be in accordance with the geographical position of the airport For that reason American and Europe
64. ay the performance of software by Timing system or and individual modules Providing access to all common data base variables Providing access to interface assignments e Parameters record feature This feature must allow to record up to 30 parameters easily selectable on common data by an operator in maintenance mode The rate from 0 1 to 1s and the duration up to 30 minutes of recording can be easily selectable by an operator in maintenance mode The result must be provided on file accessible by network The format of recording can be ASCII data record engineering format One column by parameter First row will contain parameters label and unit Any other optimised format to be agreed by THY e Real time adjustment and debugging tools at source level These tools will be used for the debugging of running tasks Access to code with step by step stop points facilities at source level Access to local and common data Dynamic suppress of module call e Real time data survey tool that permits to survey a list of data for a period of a certain number of cycles and to stop this process after an event The list of data the number of cycles and the event shall be easily modifiable by THY The buffer including these data shall be easily displayed analysed and printed 8 2 4 2 FFS performance test system Seller shall propose a fully integrated FFS performance test system enabling objective evaluation of
65. b The list of armed malfunctions with corresponding arming conditions c The list of radio aid failed with corresponding type of failure in case of partial failure d The list of anomalies simulator doors status bridge status status of engine fit and ISIS Stand By Instrument panel fit e The list of ATIMS messages refer to 3 5 3 7 2 6 19 Flight conditions It shall be possible to display on one page any information describing the flight conditions Displayed parameters shall be e Atmosphere parameters e A C weights e flight parameters All frequencies selected by the flight crew on RMPs shall appear as well with their type VHF 1 HF2 etc 7 2 6 20 A C Loading Following parameters shall be displayed and adjustable on the same page e A C weights gross weight zero fuel weight e CG location and ZFWCG e Fuel quantity per tank The fuel tanks shall be symbolised accurately to the aircraft drawing A fuel balance function shall be available The instructor shall be able to select several complete pay load pre sets setting automatically all the parameters described above to pre determined values in accordance with instructor s syllabi s 7 2 6 21 Crash Indication A visual indication on IOS shall inform the instructor that e landing rate of sink is too high e an A C part other than landing gear hits the ground In case of explosive crash determined by the ground impact force excessive altitude v
66. be able to leave the FS by means of knot ropes or rope ladders from the rear door of the flight compartment or a separate emergency exit Refer to paragraph 13 4 2 The entrance door of the flight compartment shall be fitted with a shuttered drawbridge observation window Plus a view peephole Dimensioned drawings of flight compartment platform total FS envelop drawbridge gate etc must be provided by the Seller prior to contract signature Page 40 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification International safety regulations shall be respected for emergency exit Refer to paragraph 13 4 2 In particular the drawbridge shall be equipped with 2 warning lights one must be visible from the walkway platform the other one must be visible from the base of the FS refer to paragraph 10 5 On normal drawbridge and motion operation lighting and audio warning must be provided Lighting and audible warning shall be provided during engagement and disengagement of both motion and drawbridge system 6 8 MISCELLANEOUS e Coat space with minimum 5 coat hooks shall be provided inside the flight compartment e Stowage facilities shall be provided for 5 brief cases and manuals Visual system remote control box if necessary Antiseptic spray holder and antiseptic paper supply device for oxygen masks Kleenex type papers container device Dustbin shall be provided at a convenient location
67. ce ee 67 8 3 6 Softcopy Of Firmware tedgetieegetudete dier e rgeeggiedengiegedrge gege gdegedrgegegedeg g i 68 8 3 7 Interface INPUT OUTPUT spare time nnnononnnnenneeneeeeeeeenneenennnneennenneene 68 8 4 POWER SUPPLIES eee eee een ence eee ee ee 68 8 4 1 Main Pwer SUP el 68 8 4 1 1 General E 68 8 4 1 2 ET le EE 68 8 4 2 FS Power Supplies EE EE EE EE EE 68 Page 5 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 9 DIGITAL CONTROL LOADING SYSTEM oc ccceccccceeeeeeeeeeeeeeeeeeeeeeeeeeeeeneeeeeees 69 9 1 GENERAL DESCRIPTION WE 69 9 2 HARDWARE REQUIREMENT S angst aeterte siet eeeeetu ees etc 69 9 2 1 Power Requirements ic sciiccoiarossennsistectadendassaseassteadieaacosciassdsadnanaseactesedunicns 69 9 2 2 Start of Electro Mechanical Achuator 69 9 2 3 Fallure DetEctUON srra a 69 Oa A D T E SE E wees anasavenmees apes aeassvasaeasnertibesaevase 69 9 2 5 Safety Requirements srs sadcestecsecatanenceators ieee tesa neoatesaiecataieneatoss eeateeneeetaeed 69 9 2 6 Recording ET 70 10 MOTION SYST TEM ssssssnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn nnmnnn nnna 71 10 1 GENERAL DESCRIP HON MEN 71 EECHER Etage EE 71 10 3 WEIGHT INCREASE ALLOWWANCE 71 190 4 E Te GE 71 10 5 SAFETY REQUIREMEN ME 72 10 6 TESTING AND ALIGNMENT iesssasesccsstccassccasisedaccnasadecdecsasssdaadebscdociececdessabances 73 10 601 QT Goie EE 73 10 6 2 Motion System Diagnostics get
68. ced e Communication links with main computer e Graphic computers e Touch Screen device All cables must easily be swappable IOS monitor and or touch screen device shall be designed for quick interchange Page 78 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 12 3 4 Computer Complex The Seller shall provide the full diagnostic package for computer complex according to the installed configuration A clear customised procedure shall be provided for testing the installed configuration Seller shall provide a diagnostic tool for FS network 12 3 5 Sound Off line diagnostic shall be provided in order to check the system All Loud speakers shall be individually checked 12 3 6 Smoke Generator The Seller shall provide off line control so as to check the correct operation of the smoke generation 12 4 MAINTENANCE FEATURES 12 4 1 Electronics The chassis wiring shall be directly accessible for signal measurements and or modifications All adjustments and test point shall be directly accessible Extension boards shall be provided where necessary The interface chassis shall not need any dismounting in case of wiring modification Each electronic cabinet inside the cockpit shall be equipped with sufficient lighting Anti static protection Each location where anti static protection required shall be equipped with suitable plug connected to the electrical ground and shall be equipped with anti static
69. centre line e Departure Plot 19 1 2 5 Events management Two types of events shall be considered 19 1 2 5 1 Marked events The insertion of the marked events will be done by two different ways By direct access 3 colored hardware buttons Via an IOS debrief page showing 3 colored pushbuttons The same colour will appear on associated events on above mentioned events list 19 1 2 5 2 Automatic simulation events The list of limited auto simulation events repositioning Flight Freeze release and malfunction may be revised to include possible additional simulator events such as Windshear or Wind insertion The THY and the Seller shall agree it during Design Review The instructor shall be able to display the list of all marked and simulation events at the end of the simulator session before debriefing 19 1 2 6 Navigation through the simulator session recorded file The user shall be able to access directly any period of the simulator session recorded file through a sliding bar running on the simulator session flight profile or by selecting a recorded event 19 1 3 CONFIDENTIALITY 19 1 3 1 Deletion of Simulator session recorded file There should be a way to show in a demonstrative way to the trainees attending the debrief session that the simulator session recorded file has effectively been erased with all its content at the end of the debriefing session 19 1 3 2 Data protection The operation of star
70. ckage evolution during the project THY reserves the right to update the above document accordingly 3 10 OEB IMPLEMENTATION UTILITY The Seller shall implement an OEB reminder function within the FWS with the following requirements e The Seller shall supply an offline tool and procedures to define and update an OEB flag database This database shall contain the list of ECAM message s for which OEB is are active and applicability of the OEB to procedure and or status information e This modification of the OEB flag database shall carried engineering type population not by trainees or instructors Therefore a simple text file type interface is sufficient e The identification of the applicable ECAM message in the OEB flag database shall be done using standard ATA reference FWC message ident so that no internal knowledge of the implementation of the FWC is required by the end user Page 28 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 4 ENVIRONMENT SIMULATION 4 1 ATMOSPHERE The IOS shall be able to allow at the beginning of each flight the setting of the weather situations of the departure destination and alternate airports with a smooth transition of the visual weather situation as well as enroute weather parameters The following meteorological items Wind Visibility Clouds Temperature Dew point Altimeter setting Windshear Microburst Thunderstorm and ligh
71. consider as major criterion the general Reliability of the FS The Seller shall build the FS from components of known reliability and in such a manner as to reduce the time required for trouble shooting repair and maintenance The Seller shall particularly provide the Spare Parts in adequate quantity and design efficient Special Tools and or Diagnostic means to allow for swift interventions of THY maintenance personnel The Seller shall ensure conformity of the FS to the following reliability criteria 18 1 RELIABILITY REQUIREMENTS The reliability requirement is based on two criteria the Availability rate and the mean time between failures MTBF The FS shall be capable of performing all functions in accordance with this Specification with an Availability rate not less than 99 and a MTBF of at least 100 hours during its entire lifetime The FS shall be used on an average of 20h per day 7 days per week during its entire lifetime The formula for the Availability rate is the ratio Accomplished Training Time x100 Accomplished Training Time Failure time Definitions Accomplished Training Time means the amount of time that Training has been performed without failure Failure Time starts whenever a specific part or the entire FS does not meet the training requirements Failure time stops when the failure is cured and the FS is ready for training again Should the FS be found to be inoperative more than 3 times during
72. ctionality of all items should be as expected e Finishing installation and the quality of any item should be compliant with the Technical Specification e All the A C Components P N should be compliant with the P N agreed during the progress meetings This acceptance shall concern essentially Computer complex and interface systems Motion and C L system Cockpit assembly Instructor station A C Computers Verification of Cockpit replication Miscellaneous manufacture and assembly 15 5 2 Functional Acceptance During the acceptance period the configuration of software to be tested shall have THY s agreement It will be in accordance with the frozen data package functional analysis and QTG All QTG tests must be presented before acceptance with a complete set of test cases already recorded on the simulator Automated tests shall be available on simulator and results shall be automatically compared with test data issued within the DP The simulator functionality shall be tested according to the ATM and QTG Page 91 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification THY shall also be able to fly the simulator with the Aircraft Acceptance procedure of the A C manufacturer which used during A C deliveries and test the following subject accordingly e FFS handling e Malfunctions in the models or their simulation e The whole flight loop Flight Controls Aerodynamics Engines Flight Qualities
73. ctor working distances even if tilted No less than 15 inches They shall be tilting and swivelling The touch surface technology shall be hard surface touch sensitive device It shall also accurate enough to ensure the best correlation between the touch surface and the screen display This correlation shall be reliable enough in order to prevent frequent calibration In the case the calibration is eventually needed it shall be easily operated through a dedicated page on maintenance mode Both screens shall have adjustable contrast and brightness controls capable of completely dimming the displayed image Automatic screen saver function shall be provided Both screens shall be able to work in total independent operation they shall have the same capabilities refer to paragraph 7 2 6 and it shall be possible to display the same page on both screens 7 2 3 FFIOS Seat Seller shall provide 1 one instructor and 2 two observer seats as defined in the following The seats shall be fitted with interchangeable seat covers and suitable seat belts 7 2 3 1 Instructor Seat The design of the seats shall comply with the general requirements stated in paragraph 7 1 in particular The seat position shall be able to Move along the rails fitted into the floor Move vertically Swivel Recline backrest Seat s pan adjustment It shall be electrically motorised along the vertical up down and horizontal aft fwd
74. d the Seller shall send an updated schedule and Progress Reports to THY Page 87 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification Progress Reports which will inform THY about the status of the manufacturing phase of FS shall show the progress of the tasks since the previous ones task progress compared to the initial schedule encountered problems and their possible incidence on the schedule These Progress Reports shall be maintained for each version of the FS up to the Final Acceptance 14 4 UPDATE OF SELLER S SPECIFICATION The Seller s specification shall be permanently updated to take into account modifications agreed upon between the Seller and THY during the entire project Page 88 of 102 3 Turkish Airlines A320 Full Flight Simulator Technical Specification 15 ACCEPTANCE 15 1 GENERAL FFS acceptance shall be conducted in the following two phases e In Plant Acceptance Ref 15 5 e On Site Acceptance Ref 15 6 Seller shall conduct an internal test and acceptance in accordance with the Acceptance Test Manual ATM approved by THY Following Seller s successful completion of the tests The FFS shall be offered for THY s In Plant Acceptance THY will start the acceptance only when the FFS is stable fully functional and complete with hardware and software components If there is any unsatisfactory ATM test result in Seller internal acceptance a written report including the list of fa
75. d Lightning 2 STORM 2 42 000 ft 50 X 50 NM Rain and Lightning 3 STORM 3 35 000 ft 100 X 100 NM Rain and Lightning 4 COLD FRONT 1 31 000 ft 150 X 150 NM Rain 5 COLD FRONT 2 20 000 ft 50 X50 NM_ Rain 6 SHOWERS 1 16 000 ft 50 X50 NM_ Rain 7 SQUALLS 18 000 ft 100 X 100 NM Hail 8 SNOW 16 000 ft 100 X 100 NM Snow 9 RAIN 12 000 ft 50 X50 NM_ Rain 10 STORM 4 20 000 ft 100 X 100 NM Rain and Lightning 3 6 3 Cloud Model Modification A software utility shall be provided to allow modification in width thickness and intensity of each individual cloud model 3 6 4 Cloud Model Effects Following cloud model effects shall be simulated e Realistic 3D visual representation with full correlation with ND radar image e Visibility linked to cloud models and special visual effects such as thunder rain lightning e Motion turbulence e Realistic wind parameters display on ND Direction Speed e Environmental sound lightning sound which may be heard at high altitudes and the high speeds shall be realistic as on ground lightning sound and in air sound differs e Perturbations in communications Page 21 of 102 D Turkish Airlines A320 Full Flight Simulator Technical Specification All these effects shall be correlated with respect to the aircraft position and selected clouds models At cloud model activation or deactivation the effects will be dynamically and progressively inserted or remove
76. d in order to prevent any spurious perception to operating crew 3 6 5 Link With IOS A specific IOS weather radar page will enable cloud models selection and control through following icons e Cloud model selection The 10 cloud models will be displayed with a reduced scale Selected cloud model shall be graphically represented on the IOS map display in grey scale Only one cloud model will be selected at the same time It will be possible to activate both windshear microburst and cloud model e Cloud models activation deactivation Cloud model will be activated or deactivated through this icon When active the cloud model will be displayed on IOS map page with correct shape and colours in accordance with ND display Pressing same button de activates the cloud model that returns to the same state than it was prior to its activation e Cloud models removal Further to a cloud model selection a button key shall be available on page to allow instructor to remove completely cloud model and its effects in IOS as well as in the simulation e Cloud models position After cloud model selection or activation its position will be determined on IOS map by a direct touch repositioning Its default position will be the A C position e Cloud models rotation When selected an arrow in a dial will enable to rotate the cloud model e Wind effect A wind function will allow or inhibit motion of the cloud model through wind direction and speed The
77. d vendors simulation specific compilers specific handlers simulation tools must be provided with the sources and the associated documentation design document and user manual computerised Page 66 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 8 3 INTERFACE 8 3 1 General The interface system shall take advantage of state of the art techniques in electronic components technology and shall be capable of meeting the high speed response and accuracy needed by the simulation The interface system computers buses interface cards shall permit to build fault tolerant system for the motion system in order to have maximum safety The causality links concerning the behaviour between all the interface components computers buses cards shall be established explained and supplied Hardware updating Seller shall keep the same revision level for all identical boards when applying hardware and firmware upgrade Seller shall supply modified computer diagnostics accordingly 8 3 2 Printed Circuits Boards Assemblies e All boards shall contain local intelligent circuits for controlling the board main functions and report malfunctions Refer to paragraph 12 e All adjustment and tuning for all FS boards shall be automatic and or menu driven e Board locations shall be displayed on the back of cabinet door or on any convenient place where maintenance crew can easily see 8 3 3 System Configuration
78. de Vertical speed IAS A C load e Flight Plan All A C systems shall be reconfigured to be similar to their status at memorisation time All malfunctions that were active at memorisation shall be re inserted including failed navaids At the end of the recall the simulator shall be in flight freeze status Means shall be provided to the instructor as reminder of landing gear flaps speed brakes stabiliser trim and engine throttle positions in order to set the cockpit in the configuration existing at the time of SNAPSHOT before releasing simulation Page 51 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 7 2 6 14 Environment conditions pre set 7 2 6 14 1 Airports It shall be possible to prepare different sets of environment conditions dedicated to one or several airports departure destination or alternate airports Conditions shall be simulated when the A C is located below 10000ft and less than 50 N M from the corresponding airport These environment conditions shall be defined by the following e The airport code and runway in use weather conditions runway conditions visual conditions ATIS specific parameters e an activation de activation key This operation can be repeated for each desired airport It shall be possible to modify any of those settings at any time 7 2 6 14 2 En Route It shall be possible to prepare a set of environment conditions dedicated to the En Route part of
79. de refer to chapter 1 be chosen by the operator Validation or de validation of one or several customised options shall be available at simulation start e On completion of the start up sequence the simulator will be ready for training e The motion and control loading system will include key operated switches to prevent unauthorised start up and operation e Date and time entries shall be managed on a battery protected internal clock system e Incase of one Instructor s station screen failure it shall be possible to operate the IOS without performances down grading e There shall be an easy and quick mean for the operator to identify the loaded aircraft version through the automatic display of main selected options and to check the hardware consistency e There shall be a file including simulation operation history Information about loaded configuration date and time of start simulator control file release selected aircraft model and options Detected errors during real time running software exceptions overruns context I O errors etc Stop configuration date and time reason 12 1 2 Multiversions The Simulator shall be capable of featuring different versions Page 75 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification The following features shall be available e Quick program loading total time for selection loading identification and all systems initialisation shall not exceed
80. e computation and input output at processing rates sufficient to implement all simulated systems within the specified tolerances and shall offer the following supervisory functions e Scheduling of FS software modules Loading interface controller file Performance monitoring and error reporting Symbolic access to all data base variables Loading executing and freezing simulation programs Input output requests 8 2 3 Simulation Programs The simulation will be structured in independent modules to make modifications and adjustments easier 8 2 4 Utility Program And Software Control An extensive package of utility software shall be supplied to provide a powerful capability for convenient programming program modification debugging and software control 8 2 4 1 FS Support Programs Seller shall propose Page 62 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification e Instructor Station page compiler This compiler shall enable a user to modify add or delete pages e Radio station data maintenance utilities These utilities shall enable a user to modify add delete list or print all types of radio data Automatic update by Arinc 424 data source shall be made available The data which has been modified to align Visual Runways shall be able to masked to protect aligned data during automatic update e Performance evaluation utilities These utilities shall enable a user to monitor in a non intrusive w
81. e connectors of the aircraft components and all spare I O channels in the interface boards shall be fully wired to the disconnect boxes 8 3 6 Softcopy Of Firmware Softcopy of all firmware micro programs used in the boards shall be provided 8 3 7 Interface INPUT OUTPUT spare time The I O hardware spare time will be sufficient to process more transfers during the simulation cycles without simulation disturbance This spare time capacity will be more than 50 and calculated at the end of the on site acceptance Spare time will be effective for each cycle Interface bus monitoring tool for maintenance purposes shall be provided General design documentation shall be provided to describe the architecture and the software components of the interface 8 4 POWER SUPPLIES 8 4 1 Main Power Supply 8 4 1 1 General The Seller s design shall comply with the Safety requirements stated in paragraph 13 4 A power distribution cabinet preferably located in the computer room that shall distribute and control the whole FS power The FS On Line Diagnostics shall monitor main power output When single phase loads are used the Seller shall arrange to balance the difference load between phases within a limit of 15 8 4 1 2 Insulation An insulation transformer if required by the End User s main power supply type shall be provided and installed by the Seller The transformer shall be wired so as to isolate the FS from the main power supply
82. e off data in accordance with the training syllabi 7 2 6 26 Help function This function shall display explanations on how to use the IOS 7 2 6 27 Maintenance function This function shall be provided for maintenance personnel and enable to display e various parameters for use during software integration e any flight test A C referenced and FS curves parameter versus time or parameter versus parameter e Parameter plot of any parameters selected an IOS among a list of parameters defined by THY several plots shall be possible on one page 7 2 6 28 Maintenance mode access The access to all IOS pages dedicated to maintenance purpose shall be protected by a password Page 56 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 7 2 6 29 Lesson plans The Lesson Plan Feature shall be made available During a lesson plan session all other IOS facilities shall be operated normally and the instructor shall be able to quit the lesson plan at any stage of the lesson The system shall be able to manage at least 75 lesson plans per engine type The progressive evolution into a lesson plan shall be monitoring the set of automatic manual items which will be shown along a static time line and altitude The customisation process shall be applied in order to load automatically by default the lesson plans related to the version and the customer s 7 2 6 30 Virtual Printer The aim of the virtual print
83. edia used shall have hot spare One control console for each computer shall exist Floppy disk if necessary CD ROM unit with CD write capability for long safe backup Magnetic tapes capacity 1 tape to store an entire back up of one fully used disk Graphic colour printer Graphic visual display possibility of hard colour copies Means allowing parameters recording and printing e e e e e po e 8 1 3 Operating Systems Each computer operating system shall offer Efficient real time processing Large memory management Interactive terminal support Extensive multiple batch capabilities Complete administration features for operating survey and management Report of all the detected Computer Hardware firmware OS errors on each dedicated system console and memorised on a unique error centralised file e Dating of each Computer errors hardware firmware OS e Software diagnostics to analyse errors The system administrator privileges will be dedicated only to the administration and the maintenance of the computer system hardware Operating system software No simulation programs installation utilisation maintenance shall require to be system administrator A survey of all growing Operating System files shall exist with an easy means to administrate them The space disk dedicated to the Operating System will be totally separated from the space disk dedicated for simulation software utilities simulation programs real time exec
84. eller shall provide technical support to THY for Regulatory Authority Approval following the period of On Site acceptance Page 92 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 16 ON SITE INSTALLATION After signing the contract Seller shall visit the simulator bay of THY s Flight Training Centre and verify that FS can be installed to this bay During this visit the other details of Facility Requirement shall be discussed and mutually agreed 16 1 FACILITY REQUIREMENTS The Facility Requirements shall be supplied to THY by the technical specification of the Seller This document shall include details of all necessary requirements of installation such as The FS Operating Envelope dimensions Power Supplies cooling water and air supply requirements installation dimensions of Computer room Specifications of THY supplied environmental logistics etc Complete drawings and circuit diagrams where applicable used in the manufacture of assemblies and floor loading shall be provided The Seller shall specify the units that require heat dissipation or air conditioning and provide technical data 16 2 INSTALLATION The Seller shall advise THY of any special requirements such as reinforced concrete base dynamic floor loads cooling electrical power fixation of the drawbridge All the special installation requirements shall be described with the Seller s proposal THY will be advised immediately of a
85. emperature for Electronic cabinets Air conditioning air outlets Real time and main programs failures Operator dialogue shall be provided through the console by means of menu Every malfunction shall be analysed memorised and displayed Network failures shall be monitored Error reporting format shall describe Time for beginning and end of failure Device int board circuit breaker PSU sensor location channel type of error Current Failures shall be easily processed e Only current failures shall be displayed printable after a Reset e Total current failure shall be displayed e All failures shall be memorised archived in order to be displayed printed at any time e Convenient facilities shall be provided for archive research date location failure type e Access at the latest failures shall easy and quick Masking e Unwanted or known errors should be maskable by operator e Incase of masked item a warning shall inform operator indicating the masked item e A current mask list shall be saved and restore Page 77 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification i Sound and external contact relay alarms shall be provided for Abnormal Motion CLS stop Abnormal Interface Processor stop Abnormal program abort Smoke temperature A C failure Air Conditioner Computer room ambient temperature too high A push button shall permit to inhibit the alarm sound and external The in
86. equested Page 13 of 102 D Turkish Airlines A320 Full Flight Simulator Technical Specification 3 4 FMGC THY prefers the re targeted rehosted solution for FMGC system simulation 3 4 1 FMS Files Loading Note The following requirements can be suitable for FMS2 according to their respective characteristics The solution shall be applicable inside the scope of each FM Principle Seller shall provide a way to load all FMS files via the network Software Operational Program OPC AMI Performance Data Base Magnetic Variation Data Base Navigation Data Base The process of FMS loading shall be provided with the following features 1 Automatic mode The ability to load and to control the loading for any A C version during normal training phases Version changes In this case the process of FMS loading shall be fully automatic If the new aircraft version does not request new FMS files configuration the FMS shall not be reloaded and User shall be advised 2 Manual mode The ability to load and to control the FMS loading when the simulation is running The FMS loading process shall be initiated with the choice for one or both FMS through the main start menu displayed on the simulation control console In addition the loading menu shall propose the capability to display the FMS current configuration 3 For features 1 or 2 the ability to generate reports during the FMS loading The operator shall be advised on FMS loading status
87. er is to reduce the abusive paper consumption but without breaking the communication protocol between the printer and the systems connected The choice between the real printer and virtual printer is made on the Instructor Station Toggle ON OFF The virtual printer virtual mode selection sends the printed text in a wastebasket file in the host computer This mode shall be the default mode at simulation start The real printer selection shall permit the use of the printer using the ARINC 740 protocol 7 2 6 31 F M Preparation COPY LOAD The F M Preparation Copy Load IOS page shall be provided as per described in 3 4 2 2 7 2 6 32 Electronic Mountain The Seller shall provide the means to introduce the Electronic Mountain from the IOS as required in paragraph 3 3 2 To activate the electronic mountain function an IOS interface shall be programmed in accordance with the following constraints e Anew CRT page EGPWS SCENARIO will be created that will be dedicated to this feature e This page should be easily accessible by the user through an index facility available on the dedicated master index page when applicable 7 2 6 33 TCAS scenario The TCAS scenario page shall be provided as per described in paragraph 3 7 2 7 2 6 34 Weather Radar The Weather IOS radar page shall be provided as described in paragraph 3 6 5 7 2 6 35 ATIMS messages control The AOC IOS interface shall be provided as per described in paragraph 3 5
88. escribed in the Technical Specification of the Visual System All available features of the Visual System shall be integrated to the FS such as available cloud density selection via IOS available different levels of runway contamination etc 11 2 OPTICS The minimum uninterrupted available FOV shall be 180 degrees horizontally by 40 degrees vertically with a vertical distribution of minimum 20 20 in respect of the pilot eye point position Wider FOV will be preferable All the mechanical Support Structures Visual Enclosure Collimating Mirror Back Projection Screen and Alignment spherical Reference Equipment shall be available for installation of any 180 X40 or wider Projection System of a Visual System The Seller shall find a solution to keep the Mirror Cell clean against the dust 11 3 CUSTOMISED AIRPORT MODEL ALIGNMENT The Seller shall provide an automatic tool to align all customised airport models This system shall allow for automatic adjustment of all available radio aids within the airfield area of related customised airport model All the runways defined in one customised scene shall be adjusted automatically The control details of visual system features shall be discussed during the ICD meetings and the number of customised visual scenes to be aligned shall be decided The visual system features shall be available at all airfields They shall not be specific to limited airfields 11 4 PARAMETERS SETTING
89. function is selected 4 5 4 Communication Stations Seller shall provide realistic ATC Radio Chatter in cockpit Radio Chatter shall consist of typical communication exchanges between ATC and all aircraft The instructor will do ATC traffic simulation only for the simulated aircraft e The communication stations shall be automatically activated in accordance with the A C position and the selected frequency e The Radio Chatter shall be specific to the above airports e Seller shall provide a user friendly means to alleviate the Instructor workload By proposing on IOS a predefined list of typical ATC messages These messages will be inserted within the frame of overall ATC messages when selected by the Instructor The Instructor shall be able to communicate without any need of frequency selection The instructor will also be allowed to communicate directly through the ACP e Seller shall take special care in voice quality simulation e An user friendly utility shall be provided to add modify delete predefined messages 4 5 5 RT and ATC Radio Chatter RT Chatter and ATC communications shall be simulated in accordance with IATA document Simulated Air and Ground Traffic Environment for Flight Training level II Seller shall provide realistic ATC Radio Chatter in cockpit e Radio Chatter shall consist of typical communication exchanges between ATC and all aircraft The instructor will do ATC traffic simulation only for the simul
90. g the simulator to the board replacement level The training course shall be completed before the Ready for Training THY shall be able to modify the training course syllabus according to her own requirements after contract signing Therefore e An initial syllabus containing details of each module s training objective outline and practical access requirements shall be submitted to THY e Details of the syllabus and the training schedule will be discussed between THY and Seller before the Training Freeze Date Page 95 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification The training course content shall cover at least the following subjects Page 96 of 102 17 5 1 Hardware Training 8 people Power up procedures FS general architecture and daily operation Trouble Shooting Procedures Maintenance Procedures Preventative amp Corrective On the Job Training for Trouble shooting and tuning 17 5 2 Software Training 6 people Operating System e Software update and modification procedures e Revision Control System e Back up Procedures Real time loop s w architecture software design Host peripherals dialogs interface Monitoring debugging tools IOS Software architecture page building tools Tools and Compilers QTG tools Turkish Airlines A320 Full Flight Simulator Technical Specification 18 RELIABILITY The Seller in his design and during the manufacturing phases shall
91. gramming e Print lists of tests with summary information The test driver will enable e Plotting both aeroplane reference parameters and FFS results on the same graph e Plotting both FS results and aeroplane reference envelope based on the aeroplane figure and on the tolerance value e An automatic flagging of the FS results compared to tolerance enabled in e An automatic calculation of all values submitted to tolerance check as well as all intermediate figures calculated or measured and used for the final result A3 Documentation management This function is used to create modify and print the whole documentation necessary for the Qualification Test Guide necessary to the certification including general chapters and documentation specific to the tests print function at least Some chapters will be automatically generated via a dedicated function This function will ensure that the Table of Contents and the Revision LOG are in accordance with the test data and modifications A 4 Aircraft type management FS On the same physical device different versions may exist they correspond to e A type of aircraft A320 CFM IAE different type e Ora type of checks not intended for certification but for engineering e Or new type of A C provision The Aircraft type function will be used for the management of groups of tests and of different aeroplane versions for one FS including e Addition or deletion of a version
92. h 2 4 and the following statements e All variables of ICD s logical sheets mathematics models etc included in datapackage shall be easily identifiable e All A C pin programming shall be selectable and activated through software variables and controlled via IOS e Notwithstanding IOS inputs no spurious effects on A C computers shall appear e Provisional Hardware and Software Input Output including wiring shall be installed to allow future updates e Main A C computer reset function shall be provided at the IOS refer to paragraph 7 2 6 2 to perform an individual computer quick re initialisation to restore normal operation in accordance with current FS conditions The reset shall not be hampered by the A C conditions flight phases engines off ground flight etc e Any Each A C computer interface shall be software controlled even if two are connected together Use of Industrial off the shelf standards Better or at least same timeframe revision capability as the real A C boxes Better overall revision cost than the real A C box ARINC 610B functionality shall be applied 3 2 EIS 2 SOFTWARE DATA LOADING In order to ease the update of DMCs and DUs the Seller shall provide a solution to upload DMCs and DUs with new EIS2 software version through a user friendly system However A C HMI reproduction is not a requirement The system shall be able to identify P N and S N of each LRU along with their currently loaded ElS2 s
93. hibition shall be light signalled j Diagnostic Guidance e Online help facilities shall be provided and corrective action shall be suggested e A cross reference data base facility shall be provided for each failure failure label address device location and schematic number k The on line diagnostic shall readily show the motion and CLS status motion ready CLS ready motion inhibit 12 3 OFF LINE DIAGNOSTICS 12 3 1 Interface A convenient interface diagnostic tool shall be provided in order to read and modify any value of any selected data ARINC digital and analog This program shall operate from the engineering terminal Error reporting shall work as previously described for the On Line Diagnostic It shall permit to read record and survey all input output data It shall permit off line to modify all transfer values Output of object programs and data memory of chassis processors shall be available 12 3 2 Motion and CLS The diagnostic programs one for motion and one for CLS shall be initiated through the motion cabinet processor The diagnostics shall be dynamic and automatic and shall detect any failure and miscalibration The Seller shall provide built in testing capability for trouble shooting and automatic calibration purposes 12 3 3 Instructor Station The Seller shall provide a suitable off line diagnostic utility in order to trouble shoot of IOS problems It shall determine the subassembly to be repla
94. iling tests and actions in progress to solve them with a schedule shall be submitted to THY THY shall evaluate the status of the simulator and then decide whether to join In Plant Acceptance During the acceptance period Seller shall inform THY about the hardware changes which may effect the result of the previously completed chapters of the acceptance 15 2 ACCEPTANCE TEST MANUAL ATM 15 2 1 Acceptance Test Manual The ATM shall be submitted to THY for his approval prior to In Plant Acceptance The ATM shall include checks for FFS systems quality of construction safety features and diagnostic facilities Each Test shall have 3 control check box one for the Seller own checks one for In Plant Acceptance of THY and one for On Site Acceptance 15 2 2 Scope The ATM shall permit checking of the various components of the FFS in particular All A C systems Computer complex and interface systems Motion and C L system Visual control system Sound system Simulation software including micro programs in the interface computers All software included in the FFS All Software diagnostic tools 15 2 3 Content The ATM shall include all ATA Chapters of A C systems and simulator systems and permit through a selection of significant tests checking of the simulation mathematical models Test conditions and sequences to be carried out shall be very precise The ATM should reflect the changes agreed during progress meetings
95. ines A320 Full Flight Simulator Technical Specification 19 OPTIONS 19 1 DEBRIEFING STATION The Seller shall propose and integrate a debriefing system fulfilling the requirements hereafter 19 1 1 GENERAL LAYOUT The debriefing station shall be preferably composed by 2 screens in order to allow good legibility on the various windows that are the functional components of the debrief station application The geographic distribution of those windows in the 2 screens shall be modifiable off line but frozen during the debrief session However the size of those windows should be adjustable as per user s request during the debrief session Audio speakers shall be properly located in order to ensure a good hearing of the cockpit sounds and shall include a potentiometer to control the volume 19 1 2 WINDOWS The different windows that compose the debriefing station application are e The CRM video replay e The 3D aircraft external view e The replayed instruments e The navigation charts and graphs e The event management window e The navigation through the simulator session recorded file Of course all those windows shall be perfectly synchronized during the replay 19 1 2 1 Cockpit Environment video sound replay 19 1 2 1 1 Video One single camera is enough for record replay of cockpit video This camera shall be located at the rear of cockpit and record a wide angle view of the flight deck including crew interactions Addit
96. ional cameras installed shall be located so that they don t interfere with the real aircraft cockpit environment The whole solution camera s type and locations will be mutually reviewed and agreed by THY and Seller during Design Phase The quality of replayed video shall be at a good level of resolution with a sampling of images allowing fluidity of the replay Numeric video with black and white pictures is sufficient The camera shall be able to show a good result in low luminosity cockpit environment i e night flights 19 1 2 1 2 Sound Recorded sounds shall be synchronised with the video and shall be limited to the Page 99 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification sounds recorded from the intercom as well as a cockpit sound The sound volume shall be controllable through a hardware potentiometer A digital audio mixer preset to generic reproduction should allow to mix several channels trainees voice cockpit sound instructor comments and radio communication or to select one or more if necessary to improve reproduction 19 1 2 2 Aircraft external 3D view The window shall show the aircraft from an external view and the environmental visual scene It shall be very useful in particular to show flight events such as tail strikes The visual environment may remain generic providing that the navigation charts see paragraph 6 2 4 1 are enough accurate and displays the track of the aircraft
97. ish Airlines A320 Full Flight Simulator Technical Specification 7 2 4 6 Lighting Controls For Instructor s working table a fix reading light that is flexible and intensity adjustable shall be provided Light colouring shall be selectable between red and white 7 2 4 7 Telephone It shall be preferentially located under the left armrest refer to paragraph 6 6 7 2 4 8 Clock with stop watch 7 2 4 9 Controls for Monitor Brightness and Contrast 7 2 5 Controls not Located on the Instructor Seat 7 2 5 1 Flight Compartment Air Conditioning Control 7 2 5 2 Remote Control Box for IOS A remote control box to be used by the instructor when seated in pilot seats shall be provided The receiving set shall be included in the IOS There shall be a limited number of functions available Wireless data link is preferred in case of hardware wiring the cable length shall be long enough to allow operation from Crew seats The RCB push buttons surface shall be concave in order to permit easy use when in darkness They shall be real push buttons with integrated lighting First action on push button shall set the function second action shall reset the function except for Eng Start not applicable Brightness shall be controllable Functions and arrangement are described in figure below BRIGHTNESS MOT EMER OFF ENGINE START TO IEINAL APPROACH 1 APPROACH 2 TOTAL FREEZE POS ALT FREEZE RELEASE FREEZE CAVOK CAT CAT Il CAT Ill EN
98. ity Implement the same software tools environment described in paragraph 8 2 4 to develop and maintain all the software Multi user development environment capacity Back up and restore all the disks with an integrated tool 19 4 TEST BENCH As an option the Seller shall propose a micro processed test bench of industrial standard capable of dynamic testing and control of all digital and analogue interface boards This technique shall permit trouble shooting down to chip level The Seller shall provide all necessary software tools needed to develop modify and implement new test programs 19 5 ELECTRONIC FLIGHT BAG Seller shall propose a provision of hardware as an option where Electronic Flight Folder can easy be mounted in the future By the provision THY will be able to integrate Displays in the FLYSMART architecture easily when required Page 102 of 102
99. kish Airlines A320 Full Flight Simulator Technical Specification 13 4 5 EMC Electro Magnetic Compatibility Proven design techniques and procedures will be applied to minimise the cause and effects of electro magnetic interference The choice of materials and construction methods will ensure inherent attenuation of electro magnetic interference enabling EMC requirements to be met without compromising other functional aspects Compliance with applicable standards will ensure the European Union EU EMC Directive and Federal Communication Commission FCC are required Page 86 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 14 SCHEDULE AND PROJECT FOLLOW UP The project will be followed according to the complete specification with major rules defined in this chapter 14 1 AUTHOROTIES QTG Upon requirement of THY Seller shall provide technical assistance during the initial approval of each version of the FS by the JAA Seller shall present at Preliminary and Detailed Review an example of the QTG documentation to THY for agreement The QTG documentation will be available at the authorities and THY s facility before In Plant Acceptance including e The complete general part e The complete tests description part e The complete aeroplane references part e The FS results for tests which can be run in the Fixed Base Simulator confiration The final QTG documentation shall be available at
100. l not be used Flammable impregnating or potting compounds when enclosed in fire resistant containers are excluded from this requirement Page 82 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 13 1 5 Finishes Materials that are subject to corrosion in salt or other atmospheric conditions likely to occur during service shall be avoided wherever possible When such materials are used they shall be protected against corrosion in a manner that will in no way detract from their appearance or the performance requirements of this specification Interior finishes materials and colour schema shall be agreed by THY Exterior finishes of the cockpit shall be based on the exterior markings drawing which shall be supplied as part of the data provided by THY 13 1 6 Guaranteed Weight The Seller shall specify to THY prior to the placing of a contract a guaranteed maximum weight and floor loading for all major components Such weight shall be quoted on the relevant general assembly drawing The Seller shall immediately advise THY of any major weight loading changes which may occur during the design of the equipment 13 1 7 Wiring e Power and signal cables shall be separated e Cable stress shall be avoided e All inter wiring between Chassis and subassemblies shall be done with cables and plugs e Wherever the wiring shall be weakened due to frequent wiring stress mobile parts or numerous part changes
101. lated EFCS e Simulated FWC FS shall be designed and approved without any restriction for certification as Level D In compliance with e JAR STD 1A Amendment 3 And e FAA AC 120 40 B THY prefers FS to meet also the proposed draft documents of JAA and FAA such as draft AC120 40C In case JAR and or FAA Advisory Circular change until the contract sign the contract shall define the valid reference The FFS will be used for ZFTT Zero Flight Time Training i e the based training performed on real A C will be replaced by a simulator session For that purpose in addition to level D conformity a specific attention will be taken concerning AIC representatively to the taxi take off circling approach and landing phases Additional tests and data necessary for the base training phase simulation motion sound ground handling special effect will be provided through the data package and shall be implemented by the Seller e ARINC Report 434 Requirements The requirements of Arinc Report 434 shall be considered as a reference addition to THY Technical Specification Seller shall meet this requirement as well Upgrade capability Seller shall design the FS to allow future hardware and or software expansion while maintaining the architecture unchanged In his Technical Specification Seller shall explain the limits and the solutions in respect of expansion Note Seller shall provide the necessary hardware and software to integr
102. light Simulator Technical Specification APPROACH A C path shall be visualised on selected runway LOC and G S beams If A C is outside normal path with acceptable error a flashing indication shall appear Parameters visualisation and adjustment described in MAP above shall also be available In addition an approach speed plot shall be provided to display the current A C speed vertical scale versus time horizontal scale showing the deviation with the VAPP as defined in MCDU PERF APP page RTO PLOT PAGE A C track on the Runway and stopping distance shall be displayed on the RTO plot page 7 2 6 12 Permanent visualisation of parameters The following parameters shall be permanently visualised on the lower part of each IOS page GROSS WEIGHT GROSS WEIGHT CG HEADING LATITUDE LONGITUDE ALTITUDE IAS SURFACE WIND and FLIGHT PHASE 7 2 6 13 Snapshot Recall SNAPSHOT function shall be available to memorise an A C situation that may subsequently be recalled The instructor shall be able to memorise at least 10 different snapshot situations identified by their chronological sequence number This number shall appear clearly on the map at the exact position where the corresponding memorisation occurred RECALL function shall permit the instructor to choose among snapshot previously memorised in order to reposition the aircraft in the same configuration as it was at memorisation for following parameters A C co ordinates Altitu
103. ll be selectable from the IOS at 3 various levels e Low level Approach e Intermediate level e High level Cruise At each level wind speed and direction shall be modifiable within realistic limits Wind vectors shall be interpolated between these levels A standard wind gradient shall be proposed as a default selection For cruise purposes wind vectors shall be selectable at various identified positions and altitudes A random function activated on request shall be available to set a range of variation around the average values of wind speed and heading 4 1 1 3 Turbulence Turbulence shall be available from the Instructor Operating Station percentage control Page 30 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification A turbulence level between 0 and light turbulence will be set as default For the realism of the simulation when cloud selected and A C is in cloud randomised light level turbulence will be applied automatically Dryden turbulence associated with FAA AC 120 41 wind fields shall be simulated Free air low and high frequency turbulence clear air turbulence CAT shall be simulated Turbulence level shall depend on wind type selected surface wind wind field microburst Turbulence level between low and 0 shall be set as default during simulation activation for the realism of the simulation 4 1 1 4 Effects selection and logic Winds and turbulence shall produce appro
104. ls used except where functional or magnetic properties will be affected shall be either corrosion resistant or shall be suitably treated to resist corrosion in conditions to which the FS will be subjected when in storage or during service Steel parts shall be corrosion resistant except where such treatment will prevent compliance with the performance requirements of this specification Aluminium alloy parts shall be protected against corrosion by either anodic or chemical film except where such protection will prevent compliance with the performance requirements of this specification Contact of dissimilar metals shall be avoided whenever possible When contact of metals is necessary for electrical conduction the use of metals of similar electromotive force value is required When contact of dissimilar metal is unavoidable and electrical conduction is not required an electrical insulation shall be provided by non metallic washers or a suitable protective film having the proper insulating qualities 13 1 3 Non Metallic Parts Materials which are nutrients for fungi including wood shall be avoided insofar as practicable Non metals used shall be moisture resistant and flame retarding Where wood is used for panelling it shall be covered on both surfaces with sheet material which will be securely and continuously bonded 13 1 4 Flammable Materials Materials which will support combustion or which are capable of causing an explosion shal
105. m locations shall be e Computer room e At the IOS which could be easily accessible by the instructor e Motion control cabinet e Visual platform All FS devices shall be designed to meet safety regulations colour form and label In case of FS emergency power off in absence of opposite safety regulation e The motion returns to the rest position and immediately the drawbridge is extended e Anemergency lighting shall be provided for at least 15 minutes in the flight compartment The whole FS is powered off including all devices down stream the UPS The telephone system is still operational The maintenance call on IOS station is still operational and easy to locate The maintenance call located on computer room is still operational 13 4 4 Fire Protection The Fire protection System shall comply with the EU Safety rules and also with the insurance regulations The Seller shall provide and install e A detection system A fire suppression system A CO2 manual extinguisher near the flight compartment exit A control panel with back up battery An interface to the end user building fire suppression system This system shall also be integrated with the visual system Detection of the visual projectors and the visual IG cabinet shall also connected to the FS systems Activation of any detector will activate audible and visual alarms and shut down the simulator air conditioning system and the main power Page 85 of 102 Tur
106. mpartment area Page 38 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification All equipment cabinets lighting shall be provided with an on off control 6 4 VENTILATION AND AIR CONDITIONING The flight compartment shall be air conditioned A thermostatic control shall regulate the temperature inside the flight compartment in Celsius Seller shall provide and install an Air Conditioning Unit ACU Chilled water dependent Seller shall ensure that the selected ACU model have technical support in terms of Spare Parts and Maintenance in Turkey The ACU shall include an air processing unit connected to a distribution circuit by means of two separate groups of flexible ducts The air processing unit shall provide cold air for instruments and electronic equipment hot air and cold air for the flight compartment The air distribution circuit shall not be the aircraft circuit as this one can only give a good air conditioning in the real aircraft ventilation conditions The ACU shall enable the air in the flight compartment to be changed at least once every two minutes The flight compartment ventilation shall also be filtered Instructor shall be able to set the flight compartment temperature between 18 C and 22 C by means of a thermostat located in the flight compartment These conditions will be held with all seats occupied in the flight compartment with the entrance door closed and all covers fitted Moistu
107. mrests and shall be designed in order to prevent inadvertent selections Integrated lighting logic for the push buttons shall be designed in order to display the status of the process at any time 7 2 4 1 Hardware Push Buttons Panels Hardware push buttons shall be provided in order to control e The most frequently used at least 12 functions of the IOS THY will provide the list of them at the time of the related freeze date e Control loading system e Motion and draw bridge system 7 2 4 2 Simulator and Motion amp C L Emergency Stop Buttons Both emergency stop buttons shall be located at a convenient position so as to prevent inadvertent selection e Motion amp C L Emergency stop button refer to functional description paragraph 10 5 SAFETY REQUIREMENTS e One simulator emergency stop button refer to functional description paragraph 13 4 3 Emergency Power Off 7 2 4 3 A C Communication Panel An ACP box will be used for communication between instructor and pilots This shall include a boom set and a handmic with facility sockets located at a convenient position of Instructor Seat 7 2 4 4 Sound Control A C cockpit sound volume shall be controlled by both discrete and variable controls refer to paragraph 4 4 7 2 4 5 Overhead Light Switch The Overhead light switch acts as a two way switch with another one located near the entrance door These switches control the rear compartment lights Page 44 of 102 Turk
108. n 17 2 FIELD SERVICE ENGINEER The Seller shall provide during the entire Demonstration period Refer to paragraph 18 2 the assistance of a qualified and experienced Field Service Engineer FSE The Seller shall assign the FSE to e Assist to THY s maintenance teams in their daily operations e Provide the complementary on the job training e Assist THY s maintenance teams in troubleshooting and repairing the defects that could arise during the above period e Liase with the in house Seller s engineers to ease operational problems solving e Update the Seller provided Technical Publications on the critical maintenance procedures For example C L alignment backup restore of computers disks 17 3 SPARE PARTS MAINTENANCE TOOLS AND TEST EQUIPMENT The Seller shall be responsible for defining and describing his Policy in this proposal how Seller shall meet the Reliability objectives set up in paragraph 18 This shall include e The itemised list of Spare Parts based on the quantities installed on the FS Page 94 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification e All Recommended spare parts list shall be provided e Recommended spares package shall be quoted separately and the list prise of each item will be clearly discernible e The Recommended Spares Listing RSL should include the impact of component failures on STD operations Level A Unsuitable for Training Level B May Impact Tr
109. nstructor station screen Tests can be executed in a fully automatic way or in a manual way In the latter case the pilot must execute as accurately as possible the required manoeuvre to reproduce the aircraft test When executing a test the operator has the possibility to select the following options e IOS displaying this allow to display the result on the IOS screen the operator can then decide to output them on the line printer or to save them into a file e Automatic execution The test is executed without any operator intervention as soon as it is selected e Print the result on the printer The test result is sent to the printer automatically at the end of the test execution and in the storage file e Check cockpit configuration The cockpit configuration will be checked against the configuration required by the test as regards to the main parameters e Check tolerance The tolerances are automatically checked at the end of the test execution A function that allows the operator to show the last result of a selected test on the IOS screen without running this test shall be available A documentation function shall be available in order to allow the operator to display the complete description of the test on the IOS screen initial conditions procedure tolerances and references Page 65 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 8 2 4 3 Software control change and configuration cont
110. ny changes in these requirements During the Installation the Seller shall co operate by THY when locating the Equipment such as Isolation Transformer Motion Cabinet Smoke Generator Wiring Routes Air Handler Unit Location etc and THY to advise the locations 16 3 HANDLING The Seller shall be responsible of the handling of all parts of the FS and the complete installation Page 93 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 17 TECHNICAL SUPPORT 17 1 TECHNICAL PUBLICATION All the documents shall be delivered as 2 sets of hardcopy and softcopy Associated editing tools for all kind of documents including drawings wiring manuals schematics etc shall also be provided 17 1 1 Publication Content At least the following documentation shall be provided a Documentation Inventory b Hardware Manuals 1 Operation Manuals for all simulator systems 2 Maintenance Manuals e Preventive and Corrective Maintenance Manual e Fault Isolation Manual 3 Test Equipment Documentation 4 PCB Documentation 5 Engineering Drawings such as wiring all schematics mechanical assemblies etc 6 c Software Manuals 1 Simulator Software Manuals e Software Maintenance Manuals Software Design Documents 2 All OEM Software Documentation User manuals CDs and licences of all operating and application programs 3 User Guides of all Software Utilities All OEM Documentatio
111. oftware P N The result of this identification shall be displayed for operator reference and may be printed on request to a printer or toa file Current date simulator identification as defined in 8 1 1 and loading result in clear language shall also be indicated Page 12 of 102 D Turkish Airlines A320 Full Flight Simulator Technical Specification Initial DMC upload with new software shall be entirely automated No operator action shall be required except software P N selection and upload activation Comprehensive error logging and reporting shall be provided No change on A C EIS2 software media content shall be performed A facility aimed to archive and manage at least the two last versions P N of A C EIS2 software media content shall be provided Cross loading of embedded software between LRUs shall then be enabled and proposed to the operator if software P N are not identical No operator action shall be required except source and destination LRU selection and cross loading activation Automated cross loading error reporting and logging shall provide the same facilities than A C embedded cross loading software as a minimum In any case no LRU dismounting or LRU swapping shall be required The complete loading 3DMCs and 6 DUs shall not take longer than the quickest process on aircraft 3 3 EGPWS SPECIFIC ENVIRONMENT 3 3 1 EGPWS Mode Terrain profiles in the vicinity of the airports have to be correlated to EGPWS terrain dat
112. partment 2 places near display units or projectors Computer room near visual cabinets Underneath the flight compartment 6 7 WALKWAY PLATFORM DRAWBRIDGE Seller shall install a safety gate equipped with suitable safety interlocks to access the Flight compartment from the drawbridge The safety gate extreme breadth shall allow for a passage as wide as the drawbridge Passage shall be at least 75 cm wide Seller design shall ensure the alignment and same extreme breadth of the entrance door the safety gate and the drawbridge Seller shall install a walkway platform allowing for an easy and safe access to the external side of interface cabinets and to the Visual system Projectors platform and mirror compartment In particular the Seller shall install all necessary handrail protection on the access ladder and the projector platform The projector platform access shall be coupled with the Motion System interlock that when area used for maintenance resetting required to verify the safety of the area When the FS motion system comes to its normal rest position the crew shall enter or exit via a drawbridge which shall automatically extend towards the entry platform Drawbridge slope shall not exceed 2 The guard rail of the drawbridge shall be articulated in order to take a minimum space when the drawbridge is raised Should the motion system comes to rest in an unusual position or in case of emergency situation the crew shall
113. peration as if malfunction was never selected unless additional action is defined in the malfunction description document The functionality of the 6 different types of RESETS is e Specific SYSTEM RESET the 8 different SYSTEM RESETS required are listed here above from a to h Each system reset activation shall make the system concerned return to standard nominal operation in accordance with cockpit controls status e MALFUNCTIONS RESET clear all active malfunctions and return to nominal operation for each system that has been affected unless additional action is required in the malfunction description consequences e STANDARD ATMOSPHERE shall return to the ISA atmosphere conditions conform to Airworthiness Authorities requirements e WINDSHEAR RESET shall remove all active windshear including predictive windshears and microburst e ENVIRONMENT RESET The state after function activation shall be No storms Std atmosphere No icing conditions No rail hail or snow No microburst No wind and no wind gradient No windshear Visual conditions CAVOK No thunderstorm No lightning No haze Horizon bright Runway dry and smooth No turbulence e MASTER RESET shall be defined at the Initial phase of the project e A C Computers RESET the instructor shall be able to reset each individual computer refer to paragraph 3 1 VVVVVVVVVVV VV V 7 2 6 3 Services Following SERVICE controls shall be available EXTERNAL POWER GR
114. priate effects on flight path and motion Special motion cues due to turbulence shall be simulated Wind insertion or modification shall not produce heavy changes but should gradually increase decrease on flight path and motion Compatibility of winds and turbulence shall comply with the following table SURFACE WIND WIND FIELDS MICROBURST TURBULENCE SURFACE WIND YES YES YES WIND FIELDS YES NO YES MICROBURST YES NO YES TURBULENCE YES YES YES The last wind type selected shall have priority and eliminate the non compatible wind types 4 1 2 Icing Conditions Icing conditions shall be selectable from the Instructor Operating Station Icing conditions shall produce realistic effects on airframe engines probes aircraft weight aerodynamics depending on operation of de ice systems 4 1 3 Temperature And Atmosphere Pressure Ground level outside air temperature shall be variable from the Instructor Operating Station Effects of temperature change on altitude readings shall be simulated Ground and sea level barometric pressure shall be variable from the Instructor Operating Station Note Simulator design shall ensure that computed atmospheric parameters remain at a realistic value within the whole A C operation domain i e in flight operation with low outer temperature on ground 4 2 RUNWAY 4 2 1 Runway Type Smooth and bumpy runway types shall be available from the Instructor Operating
115. re from condensation in the FS air conditioning system shall be trapped and contained Ventilation The heat dissipation ratio shall include the visual system equipment s in the flight compartment and the visual projector The ACU distribution shall include cold air for visual projector assembly 1 duct per projector assembly 6 5 INTERIOR NOISE LEVEL The acceptable acoustic noise level in the crew and instructor areas as measured near the head level of the occupants when seated at their positions shall not exceed 55dB NR according to standard ISO R1996 checked when sound is switched off FS entrance door is closed and FS room noise level does not exceed 55 dB NR With A C unit running When FS in vibration conditions rolling on runway buffet no noise shall be generated by the crew compartment structure doors sheet iron 6 6 TELEPHONE AND BOOM SET 6 6 1 Telephone A telephone system shall be provided in order to permit direct communication between the following locations Page 39 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification Computer room Motion cabinet Maintenance Crew Room Flight compartment IOS The manufacturer shall ensure that telephone set installed is fully compliant with vendor s company standard installation 6 6 2 Boom Set Maintenance BOOM SET type phone shall be provided on 5 locations Inside flight compartment near pilot seats On top of flight com
116. real time until the desired target value The malfunction shall be activated after an instructor validation of the malfunction The instructor shall be able to pre select a set of several malfunctions that will be activated simultaneously after having armed a condition Once a variable malfunction has been inserted it shall be possible to modify the vary value The concerned parameter shall still vary with environment or cockpit action in a realistic manner For each active malfunction current value of variable parameter shall always be indicated below the malfunction selection area on page Reset Reset of a malfunction shall be possible by Malfunction Reset or Master Reset or direct malfunction clearance refer to paragraph 7 2 6 2 All malfunction resets or Master Reset shall require confirmation by the Instractor Direct Malfunction clearance shall not require a confirmation of the Instructor Selecting again an active malfunction on page shall clear the malfunction It shall be possible also to display the malfunction definitions descriptions origins and consequences on instructor s demand 7 2 6 18 FS status An overall status of the simulator shall be displayed on each page in a dedicated area or a permanent window It shall content Page 54 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification a The list of active malfunctions with corresponding arming status for variable malfunctions
117. rent altitudes one above and the other one below the A C 7 Corrective Resolution RA CORRECTIVE Mode C Mode S Same level right Climb or descent Advisory CHANGE V S transponder SAME LEVEL RIGHT Enhanced Resolution RA ENHANCED Mode C Mode S Below left Climb or descent then Advisory BELOW LEFT transponder increase rate of climb or descent Reversal Resolution RA REVERSAL Mode C Mode S Forward below Climb or descent then Advisory V S REVERSED transponder reverse direction of climb FORWARD BELOW or descent Page 24 of 102 D Turkish Airlines A320 Full Flight Simulator Technical Specification TYPE IOS page title INTRUDER INITIAL ACTION REQUIRED BY TCAS TYPE INTRUDER THE CREW Sas Lesser Resolution RR CROSSING FLIGHT PATT CROSSING FLIGHT PATH Haeds Cogs 3 C Mode S oman below Climb or descent Lotte teg Advisory FORWARD BELOW transponder the flight path of the sem Siem Bearing Data ABOVE RIGHT transponder 12 Conflict No warning CONFLICT No transponder level left faa e a visual check NO WARNING fitted SAME LEVEL LEFT Page 25 of 102 3 Turkish Airlines A320 Full Flight Simulator Technical Specification 3 7 2 Link with IOS Specific IOS TCAS page shall enable scenario selection control and modification of TCAS airport traffic e 12 scenario buttons shall be displayed refer to paragraph 3 7 1 2 a scenario shall be immediately activated or deactivated after pressing the corresponding button The scenario
118. rnal busses based on international norms 8 1 1 Computers Type This paragraph is about all computers used in the FS architecture hosts interface Instructor station specific FS systems Seller shall define the computer configuration with the aim of minimising the different type of computing elements Detailed and explained functional architecture of the computers shall be supplied The computer hardware resources consumed by the software shall be identified and functions associated justified The load of all these computer functional elements shall be measured For same type of computer the same level of hardware firmware and operating system shall be used up to the end of the project If one item must be upgraded all the items of the same family shall be upgraded at the same level All these individual computers e Shall have the capability to be totally replaced at the rack or board level in no more than 10 minutes without specific tools and with one person only e Shall have all cables power supply cords signal cables arriving at the rear side of the computer and terminated with robust and reliable plugs Shall be provided with a hot redundant power supply Shall run a power on self test diagnostic Shall be provided with a high level language compiler Shall be interconnected by an Ethernet Local Area Network LAN This shall be supported by the industry standard networking software protocols TCP IP Network File s
119. rol The development and maintenance of all software shall be performed using a change and configuration control tool This tool shall e Manage all simulation software components from program modules to final simulation configuration file e Allow modifications of these components in a dedicated environment and keep access to the reference ones editing compiling e Manage all changes history with production and archiving of a detailed evolution document Manage and control multi users s access Optimise storage space Generate status reports for administrators and programmers Provide automatic tracking of source file update and the capability to correlate object files with their associated source files Interface with editors compilers provided with the operating system Provide facilities to list all source files and revision information Assist in the development debug and validation of the FS programs Ensure the consistency of generated files by controlling dependencies between software components and checking coherence of shared data This tool shall be used to define the composition of the FS load It will enable on line determination of the versions and descriptions of the software modules comprising of the current load Previous versions of the load shall be preserved on disc and the selection to use one of these will be possible 8 2 4 4 Software supply and documentation All the software produced by Seller an
120. rt their operational status to the on line diagnostic The On Line Diagnostic shall allow a global supervision of the FS e Voltage and Current values of all power supplies shall be monitored by online diagnostic system e Failing channel of systems shall be monitored and trouble shooting guidelines shall supervise the maintenance personnel e All Circuit breakers shall be monitored by On Line Diagnostic system e Online diagnostic shall display the value of any selected label ARINC and I O controlled by the interface computer e Diagnostics tools shall be easy modifiable by maintenance personnel to reflect the changes when any H W and S W modification required e Diagnostic Tools shall be accessible from both flight compartment and computer room Page 76 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 12 2 2 On Line Diagnostic Main Features It shall run on a separate and dedicate processor without interference with real time simulator programs It shall be capable of simulator functions general survey All interface boards and controllers Each power supplies including computer visual batteries Each circuit breakers Motion and control loading system voltages pressures temperatures warning abort conditions safety features Air conditioning and ventilation airflow air conditioning unit A C computer rack blowers and exhaust system Fire detection identifying different zone T
121. s the Visual System Field of View and cut off angles All control levers in the flight compartment shall be provided and shall move through the same range of motion as is available in the aircraft requiring the same force to move them as required in the aircraft Similarly all instruments indicators push buttons and switches in the compartment shall be operable The flight compartment shall be airtight enough to comply with the fire suppression system requirements 6 2 FLIGHT COMPARTMENT GENERAL ARRANGEMENT The Flight compartment shall include e The crew compartment with Scratch Resistant cockpit windows e Instructor operating station e Three movable and adjustable SEATS one for the instructor and two for the observers e A movable rear panel with the folding seat e A location for emergency equipment shall be mutually agreed between THY and the seller e The rear panel shall generate no vibration or noise and it shall be equipped with mechanical interlocks and sensors to forbid motion when it s not in opened or closed position 6 3 LIGHTING Beside cockpit aircraft lighting enough lighting shall be provided to lighten the cockpit In case of main power failure an emergency lighting shall be provided for at least 15 minutes The light control shall be located both at the entrance door and at the IOS Technical premises shall be lit for maintenance purpose Maintenance lighting shall be provided underneath the flight co
122. s as per shown in figure 8 AOC REPLY IMPENDING MESSAGES DOWNLINE F PLAN INIT REQUEST A FPLAN LFBO pat F PLAN LFBD AOC MENU AOC LOG Figure 8 AOC REPLY page The REPLY button from the AOC LOG page shall select this page The selection of any of those messages shall permit the IMPENDING MESSAGES Window to come up for managing the appropriate answer The Downlink message description shall be displayed entirely Page 20 of 102 K Turkish Airlines A320 Full Flight Simulator Technical Specification 3 5 4 Messages Modification A software utility shall be provided to create modify AOC message The message shall be extracted from the software diskette referenced in EALEQGEN Refer to SUMMARY 3 6 WEATHER RADAR The weather radar system shall be fully simulated and fully correlated with other systems such as visual sound motion and air data effects 3 6 1 Ground Mapping Function The ground mapping function shall be available for airports selected with full EGPWS correlation refer to paragraph 3 3 1 3 6 2 Cloud Model Definition 10 cloud models including a vertical profile to simulate antenna tilt effect shall be provided Refer to following array Some of these cloud models shall be made of multiple cells NB Cloud Models Thickness Width TBC Type of cloud TBC 1 STORM 1 18 000 ft 150 X 150 NM Rain an
123. screte value insertion e A slew slide graphical tool that will allow the instructor to adjust a value by continuous touch slide until reaching the desired value The following requirements are the minimum for IOS pages and the final IOS page layout shall be determined by the IOS freeze date 7 2 6 1 Freeze Controls Following FREEZE controls shall be provided e ALTITUDE FREEZE e FUEL FREEZE e POSITION FREEZE e FLIGHT FREEZE RELEASE The FLIGHT FREEZE function shall be a combination of the other freeze facilities ALTITUDE plus POSITION plus FUEL Pressing again FLIGHT FREEZE control key with the simulator already in frozen state shall RELEASE the aircraft Trim wheel shall remain frozen further to a FLIGHT FREEZE activation Once the FUEL FREEZE function has been activated through dedicated control key the only way to remove it is to press again the same key whatever the selections are made on other FREEZE and RELEASE controls 7 2 6 2 Reset Following RESET controls shall be available on this panel FIRE AGENT IDG RECONNECT BRAKES OVERHEAT ELEC RAT OXYGEN BATTERIES AICRAFT DE ICING MALFUNCTION RESET MASTER RESET ENVIRONMENT RESET STANDARD ATMOSPHERE WINDSHEAR RESET Page 46 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification Additionally When the malfunction is cancelled the corresponding cause is cleared and each system that has been affected returns instantaneously to nominal o
124. shall provide the List of LRUs used on the FS 13 3 2 LRU Markings Marking of the equipment shall be permanent and legible It shall be readable without LRU dismount Simulated Instruments shall be labelled clearly showing that it is simulator use only The LRU identification shall include the following e Name of item Manufacturer s Part Number Manufacturer s Serial Number Manufacturer s name Modification state 13 3 3 Localisation Markings Adequate coding shall be used to identify all cabinets chassis modules and or units Where access can be made to both the front and rear of a cabinet chassis or module similar identification will be shown All assembly subassembly localisation shall be clearly labelled All Components shall be identified by a reference designation Corresponding reference designations shall be shown on system diagram engineering drawing and maintenance manuals for easy identification of all components Repetitive items like lighted announciators fuses plugs and fans must be clearly numbered 13 3 4 Cable Connection Cable and cable connection points shall be identified by means of a reference designation system that establishes the point of connection for each cable Origin and destination location and cable reference shall identify all cables ends 13 3 5 Wires All wires between components whose connection to a terminal shall be accomplished by a machine screw or binding post arr
125. splayed on the IOS page Init TAXI repositions the aircraft at the exact position reached after pushback completion either straight pushback if available or the pushback in accordance with the runway in use For specific airports whose terrain altitude in greater or equal to 10 000 FT ASL the 10 000 FT repositioning shall be grayed out For repositioning on flight initial soeed at repositioning completion shall always be inside the flight envelope During repositioning there shall be an automatic stabilisation of following parameters e pitch trim e rudder trim e attitude e power setting including parameters display e And no crash shall occur If the instructor changes a parameter affecting the balance of the A C a new action on the same repositioning control shall take into account the revised parameter set and stabilise the FS accordingly The simulator shall be in FLIGHT FREEZE status after each repositioning completion 7 2 6 17 Malfunctions The instructor shall be enabled to control and monitor the simulated malfunctions There are two types of malfunctions discrete or variable An information page shall be associated to any malfunction The malfunction list shall be conform to Al specification and shall be divided by aircraft systems ATA numbers Before being in fail conditions it shall be necessary to first select the malfunction then activate it Each malfunction regardless of the type could be condi
126. such as INIT A amp B F PLN RAD NAV PROG PERF SEC F PLN etc The complete copy load process shall not take more than 30 seconds The load function facility shall be extended to FMPrep files stored on host media disks network 3 4 2 2 Link with IOS The following page shall be accessible through Master Index page The permanent FMPrep shall be sorted in predefined order to comply with the syllabus Windows permanent and import shall have the capability to display up to 10 FMPrep Beyond this number the window display shall be controlled through scroll bars However for import window the most recent FMPrep must always be displayed at the bottom of window The permanent and import FMPrep shall be identified by their FMPrep name with minimum 12 characters field The LOAD button shall be active if a unique FMPrep has been selected in one of the 5 windows By default the last temporary FMPrep stored shall be selected The LOAD button shall be greyed if no FMPrep is selected The COPY TEMPORARY button shall allow to store a temporary FMPrep which will be manually entered during the current session A default name Departure airport Destination airport shall be automatically given and shall be displayed at the bottom of the temporary FMPrep list This list shall be limited to min 5 last FMPrep stored All the temporary FMPrep shall be deleted after a simulation version change Page 15 of 102 D
127. t EEN 73 10 6 3 Alignment moecedure CEEEEEEEEEEEEKEEEEEEEEEEEREEEREEEEEEEREEEEEEEKEEEEEEEEEEEEEENEEE 73 11 VISUAL SYSTEM sanaaa eaaa aa EEan aea Eaa aA AE Eaa ESS 74 dk E GENERAL EE 74 Ae OP NC orci ead eae es 74 11 3 CUSTOMISED AIRPORT MODEL AUIOGNMENT 74 11 4 PARAMETERS SEV TIN Git sicssese casscneidanedsatsiuscadsdactecercnessesinneviterieatcancaeedes 74 12 OPERATION AND MAINTENANCE cccccceeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeees 75 E a Re TION assis Gears costed ities 75 12 1 1 Start Up and Shut Down Procedures cceeeeeeeeeeeeeeeeeeeeeeeeeeeees 75 121 2 Ee 75 12 1 3 Air GOMMIMOMNING E 76 EN E e un E DETSCHON D 76 12 2 ON LINE DIAGNOSTICS ere aa eatin 76 Ne 2 ET 76 12 2 2 On Line Diagnostic Main Features 2 22 eececeeeeeeeeeeeeeeeeeeenees 77 12 3 OFF LINE DIAGN OS TGS eege eet eendeiteg 78 E Du lg WAG e 78 12 3 2 Motion and E e 78 12 3 3 Instructor Station ia ccncncsstesnseneneacdreeasnsdsaasnacsoendeacdsaasnaddeansssdaassnandeacsonccas 78 12 3 4 Computer COMPICN geet 79 Ve E 79 12 3 6 Smok Generatol nesena e deed e 79 124 MAIN TENANCE FEA TURES cies yisesvean vices reac dees EEN 79 1241 EE 79 ee E 79 ke PMS PAIN e 79 AZ AA VISUAL SySteMi sssp edad esesnsesre see ate ee ec 79 Page 6 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 12 4 5 Computerised Documentation E 80 12 4 6 Motion And Control Loading System
128. t Simulator Technical Specification e Fail safe thermal protection for the motor amplifier and power supply will be incorporated Significant thermal events will be detected and will shutdown the control loading system if sufficiently serious e Mechanical components of different channels within the control loading frame will be colour coded as an aid to identification Page 81 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification 13 QUALITY OF CONSTRUCTION AND SAFETY REQUIREMENTS The manufacturing phase of the simulator materials safety precautions EMC etc should meet the standards of ISO 9001 and EU norms The manufacturer shall be ISO 9001 certified or shall prove that a quality plan based on ISO 9001 has been followed 13 1 MATERIAL PARTS PROCESSES AND FINISHES All equipment must operate safely in a local ambient temperature of 35 C should the air conditioning fail 13 1 1 Standard Parts The construction materials and workmanship shall be free from any defect or characteristic which may render the equipment unsuitable for its intended purpose All work shall be carried out to the relevant codes of practice All materials fittings and accessories supplied by the Seller shall be of a high quality and wherever possible standard parts will be used When standard parts cannot be used suitable alternatives within the limits of the specification will be agreed 13 1 2 Metallic Parts Meta
129. t of failure during the emergency sequence it shall be possible to bypass motion servo jacks to bring motion in rest position and manually push the drawbridge to fully extended position Page 72 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification There shall be Motion amp C L Emergency Stop button shutting off both the motion system and the C L system by de energising the electro mechanical actuators When it has been pressed the motion system shall smoothly decelerate to down rest position and C L system power shall be disconnected without shock or damage to equipment or personnel And the flight compartment shall be available for evacuation within 30 second This button shall be located in cockpit 2 places computer room power control cabinet motion control cabinet motion base The motion shall be inhibited when e Motion inhibits switches located on motion base visual platform and visual mirror area are activated e Main or emergency cabin doors are opened e Drawbridge gate open e Visual platform and mirror areas are opened Drawbridge shall be individually operable from the flight compartment when motion at rest 10 6 TESTING AND ALIGNMENT 10 6 1 QTG The motion system shall be designed and fully equipped in such a manner that the evaluation of all the subjective and objective tests as listed in the authorities official documents referenced in the chapter 1 can be successfully conducted
130. the Authorities and THY s facilities within the time schedule mentioned in JAA requirements refer to paragraph 1 This final QTG documentation will provide all QTG tests required for a level D Approval including e All Motion Visual latencies and Sound Tests 14 2 IN PLANT THY S FOLLOW UP Throughout the project period THY shall be allowed to consult the Seller s working documents and have access to the Simulator A Log Book for FFS shall be made available by the Seller for THY s access after the on site acceptance These Log Books shall contain detailed comments on any software and hardware modification and shall constitute a good tool for configuration management The Seller shall forward and update the log book after the on site installation of FFS During the H W S W integration period THY engineers may participate the period A satisfactorily furnished independent office chairs cupboards desks internet connection telephones connected to the external network etc shall be made available to THY engineers 14 3 PROGRESS MEETINGS Progress reports shall be sent to THY monthly The items in this Technical Specification which should be agreed during the project shall be discussed by these meetings THY and the Seller shall mutually freeze the details Throughout the project period conference call meetings shall be carried out when required One week before the meeting the Seller and THY shall set up an agenda an
131. the flight The En Route means that the A C is located above 10000 ft or at a distance of more than 50 N M from any of the defined airport Refer to paragraph 7 2 6 14 1 These environment conditions shall be defined by the following a Wind b Temperature Delta ISA c Visual conditions The transitions between the Airports and En Route environments shall be performed smoothly following a realistic atmosphere transition model and conform to the general atmosphere requirements refer to paragraph 4 1 7 2 6 15 Hard copy Hard copy of the current page shall be permanently possible A commercial off the shelf colour printer with standard communication protocol shall be installed at the back of the AFT cabin area 7 2 6 16 Position initialisation Following initialisations shall be available REPOSITION CASE GATE PARKING TAXI HOLDING POSITION TAKE OFF OPPOSITE TAKE OFF LEFT BASE LEG RIGHT BASE LEG LEFT DOWNWIND VMC SEELEN Page 52 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification REPOSITION CASE 9 RIGHT DOWNWIND VMC 10 LEFT DOWNWIND IMC 11 RIGHT DOWNWIND IMC 12 APPROACH 1 13 APPROACH 2 14 APPROACH 3 15 FINAL 16 10 000 FT ASL 17 35 000 FT ASL For the repositioning cases above the TRACK X TRACK HEADING ALTITUDE and A C STATUS configurations shall be determined by THY at the initial phase of the project For init Gate Parking the gate number shall be di
132. ting the debriefing tool application using a simulator session recorded file shall be password protected 19 1 4 DATA STORAGE The simulator recording media shall have the capacity to store at least 3 simulator Page 101 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification training sessions of 4 hours each The data transfer from the simulator to the debriefing station shall be made by means such as network laptop removable disk etc The simulator session recorded shall not be specific to a dedicated debriefing station but should be able to be replayed in any similar debriefing station facility installed in or out of the training centre where the session has been recorded 19 2 SPARE COMPUTERS Spare computers with the same software and hardware configuration of the HOST rehosted retargeted simulation computer s Airbus EFCS and FWC simulation package computer s and IOS computers shall be provided as options 19 3 SPARE SOFTWARE DEVELOPMENT FACILITY If requested by the THY an extra Software Development Facility computer for development shall be proposed This computer will enable change configuration control software development and maintenance activities to be centralized e g for several FFS of a same family The Seller shall propose a structure able to Run under the same operating system as the FFS Support the entire project with more than 50 spare space disk max storage capac
133. tion of electrical outlets one outlet dedicated to the Pilot the other to the First officer in cabin shall be submitted to following considerations e Power supply shall be let to the end user choice and shall offer typical safety features limitation of the available power to the lowest value filter incorporated at level of outlet electro magnetic compliance with the on board equipment e The plugs shall be permanently supplied after the simulator initialisation 3 8 4 Oxygen System crew and passengers The seller shall simulate the crew amp passengers Oxygen System THY shall provide breathable air supply source Page 26 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification The controls shall have action on crew airflow and indicator in accordance with normal and emergency usage ECAM shall reflect the IOS settings Passenger oxygen system shall be simulated to extend of appropriate cockpit indications and controls in accordance with aircraft data 3 8 5 Communication Systems 3 8 5 1 General communication Two way communications between instructor and each crewmember shall be possible by means of the A C and IOS ACPs refer to paragraph 7 2 4 2 and Communication Panel refer to paragraph 7 2 6 8 Typical background radio noise control shall be provided at the Instructor Operating Station This background noise shall be able to be muted or the user shall be able to tune its level CIDS shall be
134. tionality of IOS e Refer to following array for microburst information of 6 pre selected Microburst based on Royal Aircraft Establishment models Page 29 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification Microburst 1 2 3 4 5 6 R Radius m 1200 1100 1200 1200 1100 1100 H Height m 350 550 300 550 300 550 Max velocity 45 60 70 90 60 75 knots X Lateral distance 0 0 579 322 0 0 to threshold m Y Longitudinal 1852 3334 3334 1852 5556 1852 distance to threshold m When selecting a microburst the following variables shall be set to determined values Centre of microburst distance to runway threshold on runway axis Centre of microburst distance to runway threshold on runway across axis Radius of microburst Height of microburst centre above ground level Vortex factor multiplier Surface wind speed Surface wind direction All these variables shall be easily and directly modifiable by action through the IOS in Maintenance mode and shall be displayed on IOS screen when a windshear or microburst is selected As recommended by authorities Its centre will be indicated on IOS map by a dedicated symbol 4 1 1 2 Wind vector Wind selection from the Instructor Operating Station shall be available Wind speed and direction shall be variable A realistic boundary layer effect due to the ground on surface wind shall be simulated Wind vector sha
135. tioned on following criteria e Altitude e Airspeed e time delay e slats flaps lever position Page 53 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification e gear lever position For all those criteria except Go around the instructor has to enter the desired value at which he wants the malfunction to be triggered Once a malfunction has been armed the condition description shall be displayed on corresponding page below the malfunction selection area in order to indicate to the instructor that a malfunction is impending The altitude used for armed malfunction shall be e Altitude above airfield below 2000 FT e Baro Altitude above 2000 FT It shall be possible to program a specific malfunction page by entering several codes of desired malfunctions The code number shall be of the type XX YY where XX being the ATA number and YY being the malfunction number within the ATA number The malfunctions built in this page shall be controllable as per other malfunctions in normal system page For variable parameter malfunction value change shall be obtained by selecting a target value controlled as follows e Either directly by entering the target value of the parameter via a scroll bar or an alphanumeric keypad the Inc Dec rate of change being predefined depending on malfunction definition e Or via a potentiometer tool allowing the instructor to control continuously the rate of increase or decrease in
136. tning Variable turbulence Icing Low visibility Rain shafts Hail Shall be provided in that sequence The value and the selection of these items shall be correlated for having a realistic meteorological situation They shall produce accurate effects on A C path 4 1 1 Winds And Turbulence 4 1 1 1 Windshear and microburst Representative modelling of three dimensional Windshear dynamics based on aircraft related data to comply with the authorities official documents referenced in the chapter 1 and the Pilot Windshear guide ACO054 shall be provided Among the available windshear scenarios which can be detected by Predictive Windshear System will be marked as suitable for Predictive Windshear Training At least three separate windshear scenario shall be provided for predictive windshear system training at Prior V1 After Take Off e Approach The following windshears shall be simulated correlated with Weather Radar simulation and selectable from the IOS e FAA wind fields 4 6 7 8 9 and 10 as defined in FAA AC 120 41 e Seven microburst of which six microburst shall be based on Royal Aircraft Establishment models and shall be selected from the IOS 3 in take off position and 3 in approach position for each selectable Airport The seventh Microburst shall be selectable by Instructor on IOS to fill in required values and the Instructor shall be capable to be positioning the Microburst by Drag and Drop func
137. tomatically and flash in FFS Status dedicated area refer to paragraph 7 2 4 18 3 5 3 1 Impending Messages Window A unique Impending Window shall be provided and displayed either on the AOC MENU page or on the AOC REPLY page The Impending window shall provide the user the possibilities to manage the messages This impending window shall include the following functions The Impending window shall store the pre selected AOC Uplink or Reply messages for processing The maximum number of messages stored in the list shall be 10 The last pre selected message shall be displayed at the bottom of the list The user shall have the possibility to select a message The selected message shall be displayed in reverse video Without selection the first message of the list shall be selected by default The seller shall provide a way to change message parameters type and or values SEND or REMOVE buttons shall permit to send remove the selected message These buttons shall be activated only if the selected message is visible on the screen AOC LOG page shall be automatically displayed after a SEND action 3 5 3 2 AOC Menu Page The AOC MENU page shall contain functions as per shown in figure 6 Page 18 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification This page shall list the AOC uplink messages The Impending messages window shall come up after selection of any messages r AOC MENT IMPEMD WO
138. underside of the simulator and motion cabinet In the event of a failure detected by the system or a switch off the control loading system shall de energise C L electro mechanical actuators and inhibit the motion operation in normal mode Page 69 of 102 3 Turkish Airlines A320 Full Flight Simulator Technical Specification 9 2 6 Recording Devices Seller shall provide all the sensors position and force needed to run the QTG tests in accordance with the authorities official documents referenced in the paragraph 1 General Requirements During the simulator acceptance the Seller shall provide special test fixtures to measure the characteristics of the control load systems These results included in the Master QTG shall be in accordance with A C references and with the results of the alternate approach used for the recurrent checks Page 70 of 102 3 Turkish Airlines A320 Full Flight Simulator Technical Specification 10 MOTION SYSTEM 10 1 GENERAL DESCRIPTION Seller shall provide a fully digital six degrees of freedom Electric Motion System to simulate all degrees of freedom of the aircraft It shall be equipped with safety devices providing full protection for flight compartment and its occupants The motion system shall guarantee level D performances whatever the selected visual system The motion system shall fulfil all requirements as defined by level D in the authorities official documents referenced in the chapter
139. ured near the head level of the occupants when seated at their positions shall not exceed 55dB NR according to standard ISO R1996 checked when sound is switched off FFS entrance door is closed and FFS room noise level does not exceed 55 dB NR Even in FFS vibration conditions rolling on runway buffet no noise shall be generated by the crew compartment structure doors sheet iron motion jacks 4 4 5 Aircraft And Environmental Sounds Particular attention shall be put on the following noises e Ground power connected and electronic equipment cooling on e Engine Start There shall be a realistic noise level when all cabin and cockpit doors are closed e Power plant engine whine air noise and thrust reverse operation Aerodynamic noise and airframe sound including wind noises gear and door operation Landing gear actuation noises Runway effects including individual gear touch down and bounce Air conditioning airflow Cockpit equipment background noise Precipitation noise Thunder noise Shall be realistic according to the aircraft configuration Eg At a speed of 80 Mach the sound cannot be same as on ground Wipers noise e Crash noise 4 4 6 Warning Sounds And Voices Similarly audible cockpit warnings such as horns bells etc shall be simulated using actual aircraft components or equivalent to assure faithful reproduction of the individual sound of these devices 4 5 NAVIGATION AND COMMUNICATION ENVIRONMENT
140. utive programs The Installation of the Operating System and computer software utilities shall be at two separated levels with a detailed explained installation procedure and associated Media to be supplied Page 60 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification e Installation of the standard Operating System and computer software utilities as issued directly from the computer vendor vendor media tape CD and vendor procedure e From a separated Media Installation of the customised Operating system files Operating system generation and installation The purpose of the customisation will be justified The implementation will be detailed The complete vendor documentation administration installation maintenance programmer guide user guide reference manuals license etc shall be supplied ref 12 4 5 8 1 4 Network The FS network shall be adapted to the end user network site environment The computers network features shall enable the free exchange of data and programs e High speed communications File Transfer Virtual Terminal Service Network File System Remote control For Ethernet network interconnection the manufacturer shall deliver e An Ethernet HUB enabling Ethernet signal distribution inside each simulator complex Ethernet traffic from the main training centre Ethernet network e A programmable bridge filter used to isolate simulator complex network traffic from the
141. wind shall have an effect only on cloud model geographical position and shall not effect wind profile e Cloud model effects It will be possible to suppress weather system effects on motion and sound system e Microburst windshear selection A predictive windshear icon will be added on IOS weather radar page which enables to access IOS microburst and windshear pages Predictive windshear has been mentioned under section 4 Page 22 of 102 K Turkish Airlines A320 Full Flight Simulator Technical Specification 3 7 TCAS The TCAS simulation shall provide a full correlation with visual sound IOS and environment systems TCAS II Change 7 simulation shall have the following features All advisories shall be fully implemented with intruder carrying mode A mode C mode S transponder Instructor shall be able to select each possible corrective RA Preventative RA Proximate Traffic and TA Scenarios individually According to the selected scenario Intruder shall manoeuvre to keep its position against the own aircraft to complete selected mission RA and TA scenario selected the intruder shall track own aircraft When proximate traffic selected the intruder shall not track the own aircraft There shall be sufficient number of scenarios to cover all the TCAS aural messages There shall be multiple aircraft threats TCAS simulation shall be integrated with visual traffic Threat s shall also be visible on the IOS map screen 3 7
142. ystem NFS Special care shall be taken to avoid any spurious effects on simulation in case of communication through the local network area with the workstations All data exchange between computers used for real time simulation must be performed out of the local network area Each computer shall be identified by a name Computer tests shall permit to rapidly detect each faulty computer element The test customisation shall be possible in an easy way Results of the test shall appear on the screen but must also be captured in a file 8 1 2 Peripherals e Disk Page 59 of 102 Turkish Airlines A320 Full Flight Simulator Technical Specification Hot spare hard disks shall be provided for all hard disks used in the computers of simulator complex The hot spare disks shall have the capability to be Inserted removed while the computer is running Consulted modified while the simulation training disk is in use Disk to disk backup facility shall exist A write disk protection shall exist A modifiable label on each disk and disk enclosure shall identify the pair disk disk enclosure computer name training or hot spare All the simulation software shall be maintained in source and generated objects from the disk For any given program it shall be possible to maintain at least 3 versions of the file on disk In all cases the total storage capacities shall be well in excess of the simulation requirement Any other data storage m

TURKISH AIRLINES A320 Full Flight Simulator Technical Specification

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