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1. 4 1 3 Aircraft Category AC Code Description Code Description Emergency Vehicle Ultra Light Paraglider 19 Glider 21 Aircraft D Exxx lt 15 500 Ibs Motor Glider D Kxxx 1A Balloon amp Airship 22 Aircraft gt 15 500 Ibs lt 75 000 Ibs Only one of the Codes mentioned in the table above must be used 4 1 4 _ Flight ID FID Per ICAO regulation Mode S data must contain a valid flight identification FID to ensure that the correlation between flight plan and radar data will work automatically FID setting is required to correspond to the aircraft identification that has been correctly specified at item 7 of the ICAO flight plan It contains seven characters at a maximum left aligned no additional zeros dashes or spaces blanks For an aircraft using a company call sign the Flight ID mostly consists of the ICAO three letter designator for the aircraft operator followed by an identification code e g KLM511 BAW213 JTR25 If no company call sign is used or no flight plan is filed the default FID to be set consists of the registration marking of the aircraft e g DEABC with no dashes spaces blanks or additional zeros even if they are included in the registration marking on the aircraft tail number While 28 Document No 03 2112 010 71e Revision 1 02 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics entering the FID into the transponder the last remaining di2. Operation and Installation avionics 3 4 Unpacking and Inspection of the Equipment Carefully unpack the equipment and inspect for transport damages If a damage claim has to be filed save the shipping container and all packing materials as evidence to your claim For storage or reshipment the original packaging should be used 3 5 Mounting e In cooperation with a maintenance shop location and kind of the installation are specified The maintenance shop can supply all cables Suitable sets of cables are available from Funkwerk Avionics GmbH e Select a position away from heat sources Care for adequate convection cooling e Leave sufficient space for the installation of cables and connectors e Avoid sharp bends and wiring close to control cables e Leave sufficient lead length for inspection or repair of the wiring of the connector containing the memory so that when the mounting hardware for the rear connectors Is removed the assembly may be pulled forward several inches e Bend the harness at the rear connectors to inhibit water droplets formed due to condensation from collecting in the connector e For mounting details drawing refer to chapter 3 12 2 Mounting Advices 16 Document No 03 2112 010 71e Revision 1 02 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics 3 6 Equipment Connections 3 6 1 Electrical Connections One 15 pin D SUB miniature connector includes al
3. remaining digits shall be filled with blanks Press to save and return to STBY 12 Document No 03 2112 010 71e Revision 1 02 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics Please refer to section 4 2 1 for configuration of the 24 bit Address AA and Aircraft Category AC 2 6 Transponder Mode selection Press E repeatedly to select from following Modes e STBY gt Standby Transponder only responds to directly addressed Mode S interrogations squitter remains active If a ground switch is connected actuation of this switch will cause the transponder switch to standby mode e ACS gt Mode A C S Standard condition transponder responds to mode A C and S interrogations e A S gt Mode A S no C Altitude is not transmitted neither on C nor on S requests All other Mode S data as well as Mode A replies are transmitted If no 24 bit address AA was defined or entered as 000000 the transponder works as Mode A C transponder in that case the following Modes are possible apart from Standby e AC gt Mode A C Transponder replies only on Mode A and Mode C interrogations e A gt Mode A Transponder replies only on Mode A interrogations 2 7 Squawk Setting The active Squawk is displayed in the upper line while the standby Squawk is presented at the lower line Setting the Standby Squawk e Press gt to set the cursor turn
4. TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics 13 Press with further Records can now be created and configured as described in the aforementioned steps at start up of the transponder one of the defined records with all associated configurations need to be selected 14 Press You have now left the configuration mode and are back in normal operation 15 Switch Off the transponder 16 Switch On the transponder Your ICAO 24 Bit Aircraft Address is now stored 34 Document No 03 2112 010 71e Revision 1 02 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics 4 2 2 Functions Overview In order to access the functions described in the following table press during Standby mode and release at the corresponding counter value Proceed analogue to the steps 1 to 4 described in the table in section 4 2 1 The lower line contains the ICAO 24 Bit Aircraft Address AA the Aircraft Category AC und die Flight ID FID AA and AG are marked by a line above the numbers Digits 1 6 ICAO 24 Bit Aircraft Address HEX Format Digits 7 8 Aircraft Category Digits 9 16 Flight ID FID Counter Function 5 1 4 Just display of ICAO 24 Bit Aircraft Address AA Aircraft ID AC Flight ID FID Display Mode automatically switches back to STBY Change only FID AA AC input locked e Set Cursor with amp e turn rotar
5. er er er or er ee er er F A a i F Fi Fi Fi tof SF on in en in Men en Men Ahle den en Men Release You have now entered the configuration mode for the ICAO 24 bit address Initially the Cursor is located at the first digit in the lower line The first six digits define the ICAO 24 Bit Aircraft Address In order to enter your 24bit address select the respective letter or number by usage of the rotary knob gt moves the cursor rightwards O moves the cursor leftwards It is important to enter the ICAO 24 Bit Aircraft Address correctly With digits 7 and 8 the Aircraft Category is specified see page 28 section 4 1 3 32 Document No 03 2112 010 71e Revision 1 02 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics Display Example With digit 9 and the following the Flight ID is defined e g DEOLK Important Without blanks or any special characters and also without dashes The last digits of the line must be filled with blanks Press with the rotary knob you can now select yes if a Ground Switch is installed if not select no and proceed with step 11 Press at this stage the respective speed category shall be selected by using the rotary knob see section 4 1 6 Press at this stage a GPS receiver for ADS B Out can be selected Selectable by rotary knob Document No 03 2112 010 71e Revision 1 02 33
6. 010 71e Revision 1 02 11 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics 2 5 _ Flight ID FID The FID is an identifier required by Mode S Operation During future application of flight plans a FID could be assigned on a per flight basis If no FID is assigned today s normal case the registration marking of the aircraft should be used as FID The FID should not contain dashes or blanks The FID must not be confused with the 24 bit Aircraft Address 2 5 1 Display of Flight ID Press es repeatedly until STBY appears Press and hold D while a counter is shown beside the active squawk release at values between 1 and 4 Display The lower line contains the 24bit address AA and the aircraft category AC marked by a line above the numbers as well as the Flight ID FID without any line above the numbers cursor Digits 1 to 6 ICAO 24 bit Aircraft Address AA HEX format Digits 7 to 8 Aircraft Category AC Digits 9 to 16 Flight Identification FID This screen will appear for 5s and will be left automatically afterwards 2 5 2 Configure Flight ID Press ap repeatedly until STBY appears Press and hold while a counter is shown beside the active squawk release at values between 5 and 19 Enter Flight Id with cursor button and rotary knob Enter FID left aligned without any blanks or dashes e g 12345621DEFAV for the marking D EFAV The last
7. GND elder Er BM i me cee io I O CO shielded cable GND a a N L Q N m Q S brown brown LIGHT not connected CO Q teen __________ blue a red UB Ground Switch If a ground switch is connected in on ground FLY GND state pin 15 must be connected to GND otherwise leave Pin 15 open 20 Document No 03 2112 010 71e Revision 1 02 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics 3 8 Antenna 3 8 1 Antenna Selection e Recommended antennas see section 3 11 Accessories e Choose an antenna type compatible with the vehicle and the mounting location e Specified features depend on proper installation of the antenna e The radiation pattern needs to be verified considering aircraft type and mounting location e The electrical interference between the antenna and any other equipment must be taken into account in such a way that no reduction of the performance of any other system will occur e Install only certified antennas 3 8 2 Installation Recommendation e Take note of the antenna manufacturer s instructions e The usually deployed Dipole or Blade antennas necessarily require a high frequency capable solid metal ground plane at the antenna base e For installation in composite aircrafts ground planes are to be added The ground plane should be as large as possible but in any case not smaller than 10 cm x 10 cm If in doubt please con
8. alternative ways of mounting e Mounting directly at the panel Use the standard mounting blocks of Mounting Block Set MB800AS included in delivery e AKT 76 mounting frame was removed Fasten the two R and L marked Mounting Blocks MB800A2 as shown mind markings R for right and L for left e AKT 6 mounting frame cannot be removed Use mounting block set MB800KT Document No 03 2112 010 71e Revision 1 02 25 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics Spacer Plate Distanzblech as lo KT76 frame remains in the panel i 3 KT76 Rahmen bleibt montiert Mounting Block Set MB800KT ad a V O KT76 frame removed 3 KT76 Rahmen entfernt Mounting Block Set MB800A2 v 148 mm lt l 158 mm direct panel mounting Befestigung direkt am Panel Mounting Block Set MB800AS 26 Document No 03 2112 010 71e Revision 1 02 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics 4 SETTINGS 4 1 Overview The TRT800A is capable of storing the following information e ICAO 24 Bit Aircraft Address AA see section 4 2 1 e Aircraft Category AC see section 4 1 3 e g o 19 for gliders o 21 for aircrafts with a MTOW below 15 500 Ibs motor glider o 1C for ultra light aircraft e Flight Identification FID e g DEOLKT see section 4 1 4 Important Enter FID without a
9. rotary knob to set numbers of the standby Squawk e Press O to activate the Standby Squawk this moves the current active Squawk into Standby Document No 03 2112 010 71e Revision 1 02 13 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics 2 8 VFR Squawk The transponder features a user defined squawk code for VFR flight factory setting 000 e Activate VFR Squawk Press VFR is indicated now the active Squawk is moved into Standby but not visible because the indication of the Standby Squawk is overlapped by VFR e Display Standby Squawk Wagen Press amp or O or use the rotary knob the VFR Squawk remains active Example e Now the Standby Squawk can be adjusted by using the rotary knob and activated with e In order to store the current active Squawk as new VFR Squawk replacing the factory setting 7000 Press and hold until an S is indicated approx 3 s after releasing the button VFR is shown 2 9 ID Special Position Identification SPI Squawk Ident Press ID to activate transmission of the special position identification pulse with every reply within 18 seconds IDT appears on the display By pressing a special position identification pulse SPI is transmitted with every reply within 18 seconds which causes an accented marking on the Controller s screen The Special Position Identification has to be ac
10. uesussessssssssnsnnsnnnnnnnnnnnnnn nennen nme nenne nenne nennen 6 1 4 Features r rn rr rserrernrrnrverrernernrrarnernennsnnenernennsnuenennennnnneneenee T OPERATIONS 8 21 OM ONS EE EEE 8 Pe OG EEE 10 23 Display Brightness ea een 10 2 4 Display Indications rrorrarrarnarnarnnnvannnnvnnnnannnnnannnnnannnnnennee 10 25 FOOD PD a E E EA 12 2 5 1 Display of Flight ID scccccccervedncessenatcaustnatucosmasseeeedcanccanese 12 2 5 2 Configure Flight ID rrnnrnannnnrnarorarnnrrvnnrnnennrrnannnenen 12 2 6 Transponder Mode SeIECTtION cccceceeceeeeeeeeeeeeeeeeseeeeeeess 13 2 7 SQUAWK SetiNG 2 0 cece cece cecceeeceeee seca eeseeeaeeseeseeeseeeeeeeeeeas 13 2 8 VER Squawk raronnrnnrnrrnernnrnnnnnrnennnrnennernennennnnnnnnennannennennennere 14 2 9 ID Special Position Identification SPI Squawk Ident 14 2 10 BOTN 14 INSTALLATION een ne a nee 15 Gel NOCO nen eine are ne ee 15 3 2 Telecommunication data 2202202202202n nennen nenne nnenne nen 15 3 3 Scope of Delivery uunuussessusesennennnnnnnenennnnnnnnnennennn nennen 15 3 4 Unpacking and Inspection of the Equipmernt 16 MON ee 16 3 6 Equipment Connections rrarrnrrnrnnrvnrrnrrnrvnrrnnnnnnnsvnnnnennennsene 17 3 6 1 Electrical Connections rarrarnarvarnarvnrnnrnnrvnnvnennnnnsnnn 17 3 6 2 Static Air Port rrrernnrnernnnnernnrnennnrnnrnnnnennennennennennenneene 18 IV N
11. 71e Revision 1 02 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics 5 APPENDIX 5 1 Technical Data Compliance CS ETSO 2C112a EASA 210 268 Applicable Documents CS ETSO 2C112a EUROCAE ED 73B Class 1 Level 2es EUROCAE ED 26 RTCA DO 160D RTCA DO 178B Software Level D Temperature Ranges Operation 20 C to 55 C for 30 min 0 C Storage 55 C to 85 C shock 6G Operation an 20 G crash safety Environmental Categories RTCA DO 160D Env Cat C1Z CAA SM XXXXXXZBAAA TTIM B3F3 XXA Power Supply 10 VDC 16 VDC 040A 13 8 VDC typ 0 0A 13 8 VDC max 10 W max External 2A slow blow fuse Panel cut out 160 x 42 mm Weight 0 8 kg 1 76 Ib Receiver Characteristics RF input power level resulting in a 90 Sensitivity reply rate A MTL for ATCRBS and ATCRBS Mode S All Call interrogations 74 dBm 3 dB B MTL for Mode S interrogations 4 dBm 3 dB Document No 03 2112 010 71e Revision 1 02 37 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics Reply transmission 1090 1 MHz frequency RF Peak Power Output gt 21 dBW 126 W at antenna base with maximum cable attenuation of 1 5 dB Squitter ADS B transmitted at random intervals uniformly distributed over the range from 0 8 to 1 2 seconds full self verification of data and occurrence Mode S Elementary Surveillance ICAO 24 bit Aircraft ai
12. A 201 301 f unkwerk Operation and Installation avionics 1 3 Customer Support In order to facilitate a rapid handling of return shipments please follow the instructions of the input guide Reshipment RMA provided at the Service Area within the Funkwerk Avionics web portal www funkwerk avionics com Any suggestions for improvement of our manuals are welcome Contact service funkwerk avionics com Informations on software updates are available at Funkwerk Avionics 6 Document No 03 2112 010 71e Revision 1 02 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics 1 4 Features In order to operate the Mode S transponder it is necessary to request an ICAO 24 Bit Aircraft Address at the responsible national aviation authorities The received Code is assigned to the specific transponder aircraft and must be configured within the transponder The 24bit Address is stored in an external memory which allows the transponder being exchanged without requiring any further configuration for detailed information refer to sections 4 1 2 and 4 2 1 e Class 1 Level 2es Non Diversity Mode S Transponder for ground based interrogations at 1030 MHZ and response at 1090 MHz e Replies to Secondary Radar Interrogations o Mode A replies with a Squawk one of 4096 possible Codes e g flight plan number Squawk assigned by a Controller or the VFR Squawk 7000 o Mode C replies including en
13. Aircraft Address see 4 2 1 Setup Steps 22 Document No 03 2112 010 71e Revision 1 02 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics 3 11 Accessories External memory AC Address Adapter for RS232 including wiring 9 pol SUB D Jack and Connector Antenna cable 2 5 m 8 2 ft TNC gt BNC RG 142 1 075 dB Antenna cable 4 0 m 13 2 ft TNC gt BNC RG 142 1 72dB Antenna cable 6 5 m 21 3 ft TNC gt BNC RG 142 2 8 dB C1 105 Transponder DME Antenna TSO C66b C74c C1105 Comant Industries Inc Height 3 25 Weight 90 g 0 2 Ibs MB800AS Mounting Block Set for direct panel mounting 2x mounting block standard MB800KT Mounting Block Set for KT 76 frame mounting in a remaining KT76 frame 2x mounting block 2x spacer plate Document No 03 2112 010 71e Revision 1 02 23 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics 3 12 Drawings 3 12 1 Dimensions 161 mm 41 3 mm gt Connector plug has to be clamped with both spring locks a Document No 03 2112 010 7 fe Revision 1 02 Document No 03 2112 010 71e Revision 1 02 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics 3 12 2 Mounting Advices Panel cut out 160 x 42 mm horizontal aligned in viewable and reachable position to the pilot There are three
14. EN Ge ee ne ee 19 3 7 1 Conductor Cross Section rrarrarnnrrnnrrarrarnnrrnernernnnre 19 3 7 2 TRT8OOEM External Memory arrnrrnnrrnrnnnrnnrnennnnr 19 3 7 3 TRI800EMSS External Memory with RS232 20 38 SAHNE Anne erinnern anne 21 3 8 1 Antenna Selection 0220220020020 sen enn sen nennen nennen 21 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation 5 avionics 3 8 2 Installation Recommendation 22402200200 en 21 3 8 3 Antenna Wiring u2402002e0eennnennnnnn nn enne nennen 21 3 9 Post Installation Check cece secs eecceeeeeeceeeseeeeeeseeeseesaees 22 3 10 Starting Up 0 0 cece ccecc sees cece eeseeeeeeseeeseeeeeseeeeeeseeeseesaees 22 ll 0 EN 23 el DANE rn 24 TEN 24 3 12 2 Mounting Advices a r2u0un nennen 25 SETTINGS Are 27 4 1 Overview rrarnnrrnnrnannannnnrnarnannnnrnurnunnnnnnnrnusnunnnnnnnenunnnnnnennesnnsen 27 4 121 EO Oen 27 4 1 2 ICAO 24 Bit Aircraft Address AA J rrrrrnrrnarnnervanennr 27 4 1 3 Aircraft Category AG rrrarnnnrnarrnnrnnnnnannnernnnrnarnnnennnn 28 4 1 4 Flight ID KPD Lune 28 4 1 5 Option Ground Switch rrnrnnnnnnnnnnnnnnnnnnvnnnnarnnnnnnnennere 29 4 1 6 Reply Information Speed Category RI 29 4 1 7 Serial Interface RS232 rrorrnarnnnrnanrvannnrrvanrnarnanennre 29 4 2 CUNN 31 4 2 1 Setup Steps rrrrrnrnnrnnnvnnnnrnnnvnnvnnnnnrnvnnsnn
15. TRT800A OLED Mode S Transponder TRT800A P N 800ATC A 201 301 Operation and Installation Document No 03 2112 010 716e avionics TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics Change History Revision Date Description of Change 19 11 2008 First Release 1 01 24 04 2009 Added explanation of LOCK indicator in 2 3 In consequence of customer feedback added hint in section 4 2 1 Corrections after internal review 1 02 02 07 2010 Corrections after internal review GMT pedo ones List of Service Bulletins SB Service Bulletins have to be inserted into this manual and to be enlisted in the following table Rev Insertion No Issue Date Date SBTRTEODAHS 104 prozos pp BEE 1 1 1 1 1 1 pp 1 1 Survey of Variants Part Number Description P N 800ATC A 201 301 Version with OLED Display Manual adjustment of display brightness one VFR Code eight storable record sets for AA AC Code ICAO 24bit Address FID Ground Switch Rl Code GPS Interface Setting 2 Document No 03 2112 010 71e Revision 1 02 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics Table of Contents 1 Document No 03 2112 010 71e Revision 1 02 OENERA LE 5 el yD wasser de near nee mer 5 1 2 Abbreviations rrarnarnernnrnrvnrnernernennrnennennnnnnnernennsnuenennennenneneenee D 1 3 Customer Support
16. c Discharge ESD Document No 03 2112 010 71e Revision 1 02 39 Funkwerk Avionics GmbH Gewerbestra e 2 D 86875 Waal Germany phone 49 8246 9699 0 fax 49 8246 1049 E mail service funkwerk avionics com www funkwerk avionics com funkwerki avionics
17. coded flight level o Mode S replies including aircraft address and flight level o Extended Squitter containing additional information on position and velocity e IDENT capability for activating the Special Position Identification Pulse SPI for 18 seconds which is requested by the Controller Squawk Ident e Maximum flight level 35 000 ft maximum airspeed 250 kt e Display information contains Squawk code mode of operation and pressure altitude e Temperature compensated high precision piezo resistive pressure sensor e RS 232 I O data port enabling connection with certain GPS Receivers in order to support ADS B Out e 8 storable entries for AA AC Code FID Ground Switch Rl Code and GPS Interface setting stored in external memory TRI 800EM Document No 03 2112 010 71e Revision 1 02 7 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics 2 OPERATION 2 1 Controls Activate i VFR Operation Mode deactivate Mode Change i Active Standby Active aak Squawk ON OFF Squawk Ident filser MOD FID Rotary Knob Standby l for adjusting values Squawk Flight ID at the cursor FID position Select Operation Cursor Mode adjustment DIM Regulation Document No 03 2112 010 71e Revision 1 02 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics ON OFF Switch ON press button for approx 0 5 s Switch OFF press button fo
18. ennennsnnsnnsnnene 31 4 2 2 Functions Overview rrrrrarnnrrnrrnarnarnnnrnernarnnennnnnernnenen 35 rd oa BD Plea een eee ee eee eee ee eee 37 9 1 Technical Data 0220220ssusnesnennennnnnennnnnennnnnennennennn nenn 37 5 2 Environmental Conditions 2zu22002202200200nne nn nnn nennen 38 Document No 03 2112 010 71e Revision 1 02 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics 1 GENERAL This manual contains information about the physical mechanical and electrical characteristics and about installation and operation of the Mode S Transponder TRT800A 1 1 Symbols Advices whose non observance can cause radiation damage to the human body or ignition of combustible materials Advices whose non observance can cause damage to the device or other parts of the equipment Supplementary information 1 2 Abbreviations pb Meaning Explanation FID Flight ID Flight plan number or if not assigned registration number of aircraft Special Position Activation on request by controllers Identification Squawk Ident transmits SPI Pulse for 18 seconds which highlights the respective traffic item on the controllers radar screen AA Aircraft Address assigned ICAO 24 bit Address AC Aircraft Category Defines aircraft type into specific categories Reply Information Document No 03 2112 010 71e Revision 1 02 5 TRT800A P N 800ATC
19. er to support the ADS B Out functionality Broadcasting of own position which could be Document No 03 2112 010 71e Revision 1 02 29 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics received by other appropriately equipped aircrafts and processed for collision avoidance Selectable Options How to proceed see 4 2 Configuration e GPS Receiver for ADS B out o FREEFLIGHT GPS WAAS Sensor 1201 19200 Bd setting of the GPS receiver not required o NexNav NNL 3101 setting of the GPS receiver not required o KLN94 Bendix King KLN 89B KLN 94 KMD 150 9600 Bd setting of KLN89B KLN94 Standard RS232 Sentence setting of KMD 150 Type 1 Sentence o NMEA Format 4800 Bd setting data format RMC is expected to minimize the amount of data other sub formats are to be avoided e Comm A B support 38400 Bd Data format for special purpose An additional data link processor allows COMM A B operation and processing of the position information of a flight management system simultaneously Setting for all described GPS systems 1 2 messages per 2 sec Information regarding Comm A B support as to usability of other GPS equipment are available from Funkwerk Avionics GmbH 30 Document No 03 2112 010 71e Revision 1 02 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics 4 2 Configuration Programming of the ICAOA 24 bit Aircra
20. ft Address and of the Aircraft Category shall be executed by qualified personnel only A wrong Aircraft Address or Flight ID may cause serious problems ATC or with ACAS TCAS systems Pilot and owner are responsible for correctly set transponder data 4 2 1 Setup Steps Initially after installation The entered ICAO 24 bit address is stored in one out of eight possible records Record Presetting Beside the 24bit address and the FID one record stores also the settings made for the serial interface GPS COMM A B and also for the optionally installed Ground Switch A stringently required input is the speed category RI of the respective aircraft see section 4 1 6 Reply Information Speed Category RI Any menu item can be passed by If no changes are made the original settings will remain stored Modification of one menu item does not impact the others No entries will be deleted All those data are stored in one record If more than one record exists a record can be selected out of a list during start up of the transponder Display Example Start up Transponder 2 Ensure the transponder mode is SIBY If necessary change the mode by pressing Document No 03 2112 010 71e Revision 1 02 31 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics Press A counter is shown at the upper right corner Hold the counter has reached 47 r ig
21. gits must be filled with blanks The ICAO Flight Plan only specifies 7 characters for FID Funkwerk Avionics reserves 8 characters as stated in ED 73B for further expansion of the flight plan The user shall only program 7 characters for FID 4 1 5 Option Ground Switch If a ground switch is connected and declared in the configuration the transponder is able to acknowledge on ground and in flight state In on ground state stand by mode is activated With a connected ground switch see section 3 6 1 2 the transponder automatically changes into Standby mode once the gear touched the ground For this the Setup must be configured accordingly For a detailed description of the Setup progress please refer to 4 2 1 Setup Steps 4 1 6 Reply Information Speed Category RI Besides AA AC and FID another important part of the Mode S data is the Speed Category of the respective aircraft This speed category shall be configured in the setup see 4 2 1 and must contain one of the following codes Description No maximum airspeed data available Maximum airspeed lt 75 kt 75 kt gt maximum airspeed lt 150 kt 150 kt gt maximum airspeed lt 300 kt 300 kt gt maximum airspeed lt 600 kt 13 600 kt gt maximum airspeed lt 1200 kt Maximum airspeed gt 1200 kt Not assigned 4 1 7 Serial Interface RS232 With the additionally available address adaptor TRI800EMSS the RS232 interface can be connected to a GPS receiv
22. l electrical connections except for the antenna Use only an External Memory TRT800EM or TRT800EMSS as they are part of the certification and include a memory with the stored ICAO 24bit Aircraft Address The UB wire has to protected by circuit breaker 2 Amp 3 6 1 1 Mutual Suppression Other equipment on board e g DME may transmit in the same frequency band as the transponder If such a device is installed a suppression wiring shall be installed in order to protect the receiving parts of the different devices from in band transmissions Mutual suppression is a synchronous pulse that is sent to the other equipment to suppress transmission of a competing transmitter for the duration of the pulse train transmission The transponder transmission may be suppressed by an external source and vice versa To activate mutual suppression connect the SUPP_I O signal to the according signals of the other equipment Document No 03 2112 010 71e Revision 1 02 17 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics 3 6 1 2 Ground Switch If a Ground Switch is connected and activated in the Setup the transponder is enabled to distinguish between On Ground and In Flight Condition In On Ground Condition the transponder automatically enters the Standby mode In order to activate this function the input FLY GND must be connected to a switch which connects the input with GND in case the gea
23. ny blanks and dashes e Ground Switch Yes No see section 4 1 5 e Speed Category RI see section 4 1 6 e RS232 Interface Configuration e g for connecting a GPS Receiver to support ADS B Out All ofthese data are configurable in the Setup refer to section 4 2 1 and are stored in the external memory module integrated within the housing of the D Sub connector included in the delivery The cable with this connector shall remain in the aircraft even if the unit is removed to ensure that the ICAO 24bit aircraft address is fixed to the aircraft 4 1 1 Error Logging If errors occur those will be internally stored in the order of appearance The error list can be displayed as described in chapter 4 2 2 4 1 2 ICAO 24 Bit Aircraft Address AA Ask your national aviation authority e g in Germany LBA Referat B5 Department Verkehrszulassung how to obtain the AA In the case of aerial sports equipment the contact point would be the respective associations Only the assigned AA has to be used and must not be modified at any time because a duplicate address would jeopardize the data surveillance and integrity figures of Mode S Document No 03 2112 010 71e Revision 1 02 27 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics If no AA is stored after power on the display shows CRADLE OFF and the transponder operates in Mode A C Configuration of the AA see section 4 2 1
24. r approx 3 s activate deactivate VFR Squawk ress shorti VER p y store active Squawk as VFR VFRW Squawk press button 3 s see section 2 8 1 change between active and standby Squawk 2 works as cursor back button opposite CHANGE function of the cursor button during entering values and also for navigating backwards through the configuration menu see 4 2 1 Squawk Ident sends Ident marking SPI for 18 s in normal mode see section 2 9 Select transponder mode ACS A S or Standby see section 2 6 Set position of Cursor Activation for DIM Regulation see section 2 3 Flight ID configuration of Flight ID FID J in standby mode press button for 5 s Adjust Enter values at current cursor position select options set standby Squawk see section 2 1 Document No 03 2112 010 71e Revision 1 02 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics 2 2 ON OFF Switch ON press button for 0 5 s Switch OFF press button for 3 s After turning on the display appears as follows Device Name Software Version FPGA Vers 48 Firmware Version Example If more than one aircraft address FID exists select the correct entry with the rotary knob and confirm with de If there is no external memory TRT800EM connected or no 24bit address defined 000000 the message CRADLE OFF appears and the transponder is not working as Mode S device but as Mode A C tran
25. r is weighted or remains open in the other case This option must additionally be activated in the Setup For details on configuration please refer to section 4 2 1 3 6 2 Static Air Port Install a silicon soft tube fitting the 5 mm static air port at the backside of the transponder and secure plumbing with appropriate clamps 18 Document No 03 2112 010 71e Revision 1 02 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics 3 7 Wiring 3 1 Conductor Cross Section Power Supply Power GND AWG20 0 62 mm Signals AWG22 0 38 mm The conductors must be approved for aircraft use 3 7 2 TRI800EM External Memory blue GND not assigned internal use connected to EEPROM internal use connected to EEPROM RS232 Output COMM A TX RS232 not assigned not assigned red UB internal use connected to EEPROM internal use connected to EEPROM RS232 Input COMM B RX RS232 Suppression I O not assigned brown Ground Switch FLY GND P 003 17 c TNC Connector XPDR Antenna Ground If a ground switch is connected in on ground Switch state pin 15 must be connected to GND FLY GND otherwise leave Pin 15 open Document No 03 2112 010 71e Revision 1 02 19 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation eiaries 3 7 3 TRT800EMSS External Memory with RS232 unite TXD N ses a gf T ellow FLY
26. rcraft address as assigned by national Address Hex Code aviation authority FID Flight ID Flight Plan call sign or aircraft registration marking Capability Report Reports the available data and means by which the transponder can report Pressure Altitude Up to 35 000 ft in 25 ft increments Flight Status in flight on ground Mode S Enhanced Surveillance Level 2es Comm A Comm B 56 112 Bit Messages SI capability 5 2 Environmental Conditions Temperature Altitude EEE Low ground survival 451 55 C temperature Low operating temperature Temperature High Short time Operating 452 70 C Temperature High Operating Temperature In Flight Loss of Cooling No auxiliary cooling required 38 Document No 03 2112 010 71e Revision 1 02 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics Altitude 35 000 ft Temperature Variation EN range Penn per minute 6 0 A 6 G operational shocks 20 G Crash Safety Test Type R in all 6 directions Vibration 180 8 Vierationcumem Explosion Proomess 9 0 x Notestrequired Water Proofness 10 0 X No test required Powerinput DC feo Be ooo Voltage Spike Conducted 70 A SSS Induced Signal Susceptibility Radio Frequency Susceptibility Emission of RF Energy Lightning Induced Transient a 22 0 Susceptibility 1 0 3 Lightning Direct Effects No test required Icing No test required 4 0 Electrostati
27. sponder The transponder starts in standby mode see section 2 6 2 3 Display Brightness In active mode not standby press button for 2 s Adjust brightness DIM with rotary knob Return to normal operation press or wait 5 s 2 4 Display Indications 10 Document No 03 2112 010 71e Revision 1 02 TRT800A P N 800ATC A 201 301 Operation and Installation funkwerk Value Meaning Remarks Transponder is transmitting Replies on Interrogations Appears per reply diamond Extended Squitter ADS B out Transponder is locked by a Lock Information indicated ground station and will be as vertical dash below the directly addressed diamond PLL PLL Error Internal Error TRX Transmit Failure DC Low internal voltage Internal error FPG T T FPGA Failure Internal error Battery Power too low maybe battery generator fault transmits Ident Marking SPI ID Squawk Ident has been pressed active for 18 s Flight Level Flight Level in 100 ft steps BA ID FLO10 FLerr Invalid altitude measuring Beyond 1000 35 000 ft C Mode gets inactive ACS Operational Mode Modes see section 2 6 STBY A S ACS AC A 0000 Standby Squawk Could be changed with active Squawk by pressing in flight Ground Switch Info on ground if installed available Cradle no AA 24bit Address Transponder works in A C Off configured Mode no Mode S F G Document No 03 2112
28. tact the aircraft manufacturer e Keep away three feet from any other antenna e Pursue mounting in vertical position under the belly in flight direction 3 8 3 Antenna Wiring e Suitable antenna cables see section 3 11 Accessories e Keep wiring as short as possible e The smallest cable bend radius is 10cm Avoid sharp bends e Keep away from an ADF antenna cable at least 12 inches e Electrical connections to the antenna shall be protected against moisture to avoid loss of efficiency Document No 03 2112 010 71e Revision 1 02 21 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics Attenuation from antenna to transponder at 1090 MHz must not exceed 1 5 dB 3 9 Post Installation Check A certified maintenance shop must verify proper operation of the transponder by testing in accordance with Appendix F of 14 CFR Part 43 ATC Transponder Tests and Inspections All steering and control functions of the aircraft are to be examined in order to exclude disturbances by the wiring The most important factor in the transponder configuration is the setting of the ICAO address see section 4 2 1 3 10 Starting Up Turn the transponder on with After start up the following screens appear The TRI800A starts in Standby Mode indicated with STBY In order to change into operational mode indicated with ACS press de Very important is the correct configuration of the 24bit
29. tivated after the Squawk Ident request of the Controller 2 10 Error Codes Please refer to 2 4 Display Indications for possible displayed errors 14 Document No 03 2112 010 71e Revision 1 02 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics 3 INSTALLATION 3 1 Notes The following suggestions should be considered before installing The assigned installation company will supply wiring For diagrams refer to 3 7 Wiring Transponder External Memory all cables and antennas shall be installed according to FAA AC 143 13 2A Acceptable Methods Techniques and Practices Aircraft Alterations and the appropriate manufacturer s instructions 3 2 Telecommunication data Depending on your national telecommunications legislation the following data may be required when applying for the aircraft radio station license Type Designation TRT800A EASA Number EASA 210 268 Transmitter Power Output 126 W Emission Designator 12MOM1D 3 3 Scope of Delivery TRI800A Transponder TRT800A TRT800EM External Memory AC Address Adaptor with wiring MB800A2 Mounting block set mounting when KT 76 frame is removed 4x screw M4x20 zinc coated 1x mounting block KT76 left 1x mounting block KT 76 right 565101A4 TNC antenna connector 03 2112 010 71e Manual Operation and Installation Document No 03 2112 010 71e Revision 1 02 15 TRT800A P N 800ATC A 201 301 funkwerk
30. y knob to select characters e press es to save and to return to STBY 20 Test Mode eee eee 40 display error logging m Document No 03 2112 010 71e Revision 1 02 35 TRT800A P N 800ATC A 201 301 funkwerk Operation and Installation avionics Counter Function S 47 enter ICAO 24bit Aircraft Address Aircraft Category AG Flight ID FID the button shifts the Cursor one digit to the right the O button shifts it one digit to the left turn rotary knob to select characters press es to enter the next menu item changes are kept in memory but are not yet active press O to return to the previous menu item Ground Switch Info turn rotary knob to select option Yes No press amp to enter the next menu item changes are kept in memory but are not yet active press to return to the previous menu item Speed Category with respect to the maximum airspeed of the aircraft enter the corresponding value see 4 1 6 with the rotary knob press amp to enter the next menu item changes are kept in memory but are not yet active press to return to the previous menu item configure RS232 interface refer to section 4 1 7 turn rotary knob to select option press es to save and to return to STBY Transmission of position data is indicated by p type of squitter in the upper line in the test mode Turn power off and on with again to activate new settings Document No 03 2112 010
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