DAC Technologies GEN-X electronic flight bag P/N 1069-4000-01 User's Manual
Contents
1. 23 INTERCONNECT FOR AIRCRAFT WITHOUT EMERGENCY BUSS 24 OUTLINE DRAWING cabo ob ket ssion sosed ke 25 1069 2510 01 D doc 1069 2510 01 Page 6 of 27 Rev D Equipment Installation Manual GEN X Electronic Flight Bag 5 dy DAC INTERNATIONAL INTRODUCTION This manual contains installation data specifications and Instructions for Continued Airworthiness for the DAC International GEN X Electronic Flight Bag EFB consisting of Part Number 1069 4000 01 Remote Processor Unit RPU and 1069 48XX XX Display Unit DU DESCRIPTION The DAC International GEN X is designed to be a robust electronic flight bag The GEN X system may be used with any software which can run under Windows XP Professional It may include DAC International Software called GENESYS PART NUMBERS GEN X RPU 1069 4000 01 Electronic Flight Bag Remote Processor Unit 1069 2510 01 D doc 1069 2510 01 Page 7 of 27 Rev D INTERNATIONAL Equipment Installation Manual GEN X Electronic Flight Bag DAC PART NUMBERS Gen X RPU Mount 1069 6001 01 Electronic Flight Bag Remote Processor Unit Mount Gen X DU 1069 48XX XX Electronic Flight Bag Display Unit ___ First digit is the color code of the display 01 Grey 02 Black 03 Brown V Second digit is the resolution capability of the display 0 800 X2. gt gt 1069 2510 01 D doc 1069 2510 01 Page 22 of 27 Rev D INTERNATIONAL Equipment Installation Manual GEN X Electronic Flight Bag b DAC TYPICAL ETHERNET INTERCONNECTIONS CAT5E ETHERNET CABLE PIC WIRE amp CABLE PN E10424 OR EQUIV R R T T R R T T EFB 1 HUB OR SWITCH R R T T EFB 2 T T R R R R T T EFB 1 EFB 2 TYPICAL CROSS OVER INTERCONNECT 1069 2510 01 D doc 1069 2510 01 Page 23 of 27 Rev D Equipment Installation Manual GEN X Electronic Flight Bag uS dy DAC INTERNATIONAL INTERCONNECT FOR AIRCRAFT WITHOUT EMERGENCY BUSS 28VDC a MAIN BUSS 28VDC RELAY AVIONICS BUSS 28VDC 5A REMOTE PROCESSOR UNIT RPU AVIONICS BUSS 1N4007 DIODES 2 ESSENTIAL PWR V EMERGENCY PWR CHASSIS GND CHASSIS GND 1069 4000 01 1069 2510 01 D doc 1069 2510 01 Page 24 of 27 Rev D Equipment Installation Manual GEN X Electronic Flight Bag DAC INTERNATIONAL OUTLINE DRAWING I 8 Inch Display Unit 588 400 6 900 1470 400 2 756 em 2 756 re 8 N 5 Ai T E aa 1 1 705 8 2 627 3 450 L 625 485 799 4 272 467 1
3. GEN X Electronic Flight Bag 5 dy DAC INTERNATIONAL DU Replacement 1 Attach mount stud body with four screws making sure to select the appropriate set of mounting holes on the display unit that will be nearest to the aircraft window 2 Align red dots on DU connector and cable connector Push together and verify positive lock 3 Perform operational test of the GEN X as prescribed in the aircraft maintenance manual Battery Replacement 1 Remove RPU according to section RPU Removal 2 Locate and remove the RPU battery cover by removing the two screws holding it to the RPU housing 3 Remove battery by pulling on cloth tab 4 Install new battery observing correct orientation 5 Reinstall battery cover 6 Reinstall RPU according to section RPU 7 Close GEN X system circuit breakers 8 Verify battery condition light is off 1069 2510 01 D doc 1069 2510 01 Page 14 of 27 Rev D Equipment Installation Manual GEN X Electronic Flight Bag 5 dy DAC INTERNATIONAL Battery Checkout The lithium ion battery installed in the Gen X RPU is incased in a smart electronic package which eliminates the risk of overcharging during temperature extremes as well as monitoring the age and condition of the battery itself When a condition exists that causes the battery to be incapable of performing its intended function the battery monitor light on the RPU is lit yellow If during normal inspection inte
4. 600 1 1024 768 Third and fourth digits represent display size 08 8 10 10 12 12 Gen X Display Cable 1069 4700 XX Electronic Flight Bag Display Cable V Last 2 digits specify straight or right angle RPU mating connector 01 Straight 02 Right Angle REGULATORY COMPLIANCE Software The software was developed in accordance with RTCA DO 178B to criticality level E in accordance with FAA Advisory Circular AC 120 76A for Type B software Hardware The GEN X hardware was developed as a Class 3 EFB in accordance with FAA Advisory Circular AC 120 76 1069 2510 01 D doc 1069 2510 01 Page 8 of 27 Rev D Equipment Installation Manual GEN X Electronic Flight Bag DAC INTERNATIONAL INSTALLATION KIT Installation kits are available under kit part number 1069 4200 01 Individual pieces are available under the part numbers shown Contact DAC International sales to place orders Part Number Description Qty 1069 4200 01 Installation Kit GEN X P10440 Connector J2 Mate Cable End Straight Includes Backshell 1 1069 2510 01 Equipment Installation Manual for GEN X 1 A right angle connector which mates with J2 is also available for purchase separately Part Number Description P10512 Connector J2 Mate Cable End Right Angle 1 Includes Backshell An Optional 16 foot non terminated Gen X Display Cable is also available for purchase for installations
5. connectors by twisting counterclockwise one quarter turn then pulling the connector free Remove safety pin clip from front of mount by pulling sharply 5 Twist the thumb screws on the RPU counterclockwise one quarter turn and pull up then forward to remove rear guide pins from mount bracket RPU Installment 1 Open the two circuit breakers powering GEN X 2 Insert the RPU guide pins into the holes in the rear of the mount bracket Seat RPU mounting hole located on flange near handle over mount guide pin Once units have been fully mated twist thumbscrews 2 clockwise until positive lock is achieved Insert safety pin clip through mount guide pin to secure 4 Close the two circuit breakers 5 Perform operational test of the GEN X as prescribed in the aircraft maintenance manual DU Removal 1 Power down the GEN X by opening its two RPU circuit breakers and wait approximately one minute for the system to power down 2 Verify that the three RPU annunciators located on the connector side of the RPU are extinguished 3 Remove the safety pin on rear of mount 4 Twist off retaining nut being careful to capture the washer and spring on rear of mount 5 Pull DU straight off mount and disconnect the connector by pulling the locking ring away from the connector body 6 Remove and retain four screws and mount stud assembly from DU body 1069 2510 01 D doc 1069 2510 01 Page 13 of 27 Rev D Equipment Installation Manual
6. that may require a shorter cable run Part Number Description Qty 1069 4701 01 16 Gen X Display Cable non terminated RPU end 1 NON SUPPLIED EQUIPMENT Single Wire MIL W 22759 16 or equiv Shielded Wire MIL C 27500 or equiv Ethernet Wire PIC Wire amp Cable PN E10424 or equiv 1069 2510 01 D doc 1069 2510 01 Page 9 of 27 Rev D Equipment Installation Manual GEN X Electronic Flight Bag DAC INTERNATIONAL SPECIFICATIONS Physical The GEN X RPU attaches to its mount through two 25 guide pins and a two lock turn wing nuts The mount is attached to the airframe via four mounting holes See the paragraph titled Outline Drawing for further details RPU oae GO 2 655 Includes mounting flange nid 8 561 Includes mounting flange NC P DEP ER 12 810 Includes mounting flange 7 8 Ib Includes mounting flange DU 8 nears A ete A 9 90 Width nce 6 90 Depth oet socius 1 705 Weight E Rx ei 3 4 Ib DU 10 Height anne Ree 11 60 8 13 roei 1 705 sete elie eee sto es 4 6 Ib DU 12 Height edet endis 13 00 mere Deere et eter tea 9 20 DIC PU 1 76 W ght
7. 131 Note Dimensions are in inches 1069 2510 01 D doc 1069 2510 01 Page 25 of 27 Rev D Equipment Installation Manual GEN X Electronic Flight Bag DAC INTERNATIONAL II 10 Inch Display Unit 8 130 1 170 400 2 756 1 818 2 756 8 S N zs ES 2 L N J L 1 403 1 705 z 3 252 ot 7 4065 4 877 UE 1 071 1 735 Note Dimensions are in inches 1069 2510 01 D d 96 1069 2510 01 Page 26 of 27 Rev D Equipment Installation Manual GEN X Electronic Flight Bag bt DAC INTERNATIONAL Ul Remote Processor Unit in Mount 11 900 6 900 Ea L 12 810 Lt Ye 12 500 8 634 I 2 655 TE 7 875 ed Note Dimensions are in inches 1069 2510 01 D doc 1069 2510 01 Page 27 of 27 Rev D
8. EN X Electronic Flight Bag DAC Vy INTERNATIONAL Table Of Contents RECORD OF REVISIONS ee etu o ecco vo ceno cc een ato o see ao one co oo Q ado oo see ae oet c oo aeo xo oen Q no sea q o eta Loon 3 INTRODUCTION e ae Ro a bl o eaa ga a 7 DESCRIPTIQN 3 eon Ga ee eG sn pae ee oa 7 PARI NUMBERS X etos reee o eee eue esu eae aoo 46 0 ae 660006660 6646060 0 00 606 0 660 7 25598 o eaae dun ea a Dua ea sepa Casa 8 doc Rosin nudo 8 TVAR DI WARE ca Chace LE 8 INSTALLATION KIT eo ee ree e ee a eo eo eed c ao eo ee oar co Ceo eoe a oes oo ee redeo o vende e aeu ai ea 9 NON SUPPLIED EQUIPMENT 25 06220 s Eee posce peedorucse e Poo co e 9 TEE 10 la ALIE 10 PIDE 10 EDBECTRICAL 50 teet ua Suwa se Tu qusa i aS a 10 PATA NSBDIDS EE 11 A 1 OPERATIONZ ccscscsiscsssccssescctedacsscsessescsssssscscssssoscssedsosecsessoscsssss0seesess0000esessbecssecs0secsesceveisvassesedsosecdessodes
9. Equipment Installation Manual GEN X Electronic Flight Bag DAC INTERNATIONAL EQUIPMENT INSTALLATION MANUAL For the GEN X Electronic Flight Bag P N 1069 4000 01 RPU P N 1069 48XX XX DU RELEASED Rev D DAC International 6702 McNeil Drive Austin TX 78729 Copyright 2005 DAC International All rights reserved 1069 2510 01 D doc 1069 2510 01 Page 1 of 27 Rev D Equipment Installation Manual GEN X Electronic Flight Bag P DAC INTERNATIONAL This page intentionally left blank 1069 2510 01 D doc 1069 2510 01 Page 2 of 27 Rev D Equipment Installation Manual GEN X Electronic Flight Bag b DAC RECORD OF REVISIONS DESCRIPTION DATE Initial Release E633 11 21 06 Added Typical Ethernet Interconnections Battery 4 30 06 Checkout amp Maintenance E709 Clarified Ground Names and Connections E713 Updated as per ECO E726 06 Add Optional Non terminated Display Cable E748 APPROVED R zz 5 3 07 5 23 07 07 25 07 456 B D Ease _ p gg 5 21 _ BEEN p NEN 1069 2510 01 D doc 1069 2510 01 Page 3 of 27 Rev D Equipment Installation Manual GEN X Electronic Flight Bag P DAC INTERNATIONAL This page intentionally left blank 1069 2510 01 D doc 1069 2510 01 Page 4 of 27 Rev D Equipment Installation Manual G
10. GA Green D Blue Common VGA Blue Common E Green Common VGA Green Common F Blue VGA Blue H IDO IDO J Video Ground Video Ground K H Sync Horizontal Sync L ID1 ID1 or DDC Data M ID2 ID2 N V Sync Vertical Sync P Sync Rtn Sync Return R ID3 ID3 or DDC Clock 1069 2510 01 D doc 1069 2510 01 Rev D Page 21 of 27 Equipment Installation Manual GEN X Electronic Flight Bag INTERNATIONAL DAC N TYPICAL INTERCONNECT REMOTE PROCESSOR UNIT RPU GND GND CLK CLK RXD RS232 COM2 TXD RS232 COM2 DA2 DA2 1 1 DAO DAO USBD0 USBD0 SYSTEM PWR V GND IN SYSTEM PWR V GND LED3 IN USB1 PWR ETHERNET SHIELD ESSENTIAL PWR V CHASSIS GND EMERGENCY PWR V COM X GND COM X TX COM X RX ET6 ET3 RX TX 2 TX USBD1 USBD1 USB1 GND ARINC RX A ARINC SHIELD ARINC RX B CHASSIS GND RGN RE GREE BGN GGN VIDEO GN H SYNC ID1 OR DDC DATA 1 2 V SYNC SYNC RTN 103 OR DDC CLOCK 1069 4000 01 DISPLAY UNIT DU GRAY GND WHITE GND WHITE CLK PURPLE CLK ORANGE RS232 WHITE DA2 GREEN DA2 WHITE DA1 BLUE 1 WHITE 0 YELLOW DAO BLACK USBD0 BROWN USBD0 RED IN SYSTEM PWR V BROWN GND RED IN SYSTEM PWR V BLACK GND BLACK LED3 IN 1069 48XX XX 28 ESS BUS 28 EMER BUS RX ETHERNET TX ARINC TX A FMS ARINC 429 ARINC TX B lt
11. Page 16 of 27 Rev D Equipment Installation Manual GEN X Electronic Flight Bag P DAAC INTERNATIONAL 7 Electrical loads for this appliance are as specified in the DAC International Installation Manual 1069 2510 01 this manual 8 There no airworthiness limitations associated with the installation of this appliance 1069 2510 01 D doc 1069 2510 01 Page 17 of 27 Rev D Equipment Installation Manual GEN X Electronic Flight Bag b DAC ENVIRONMENTAL The GEN X meets the environmental test categories detailed below in accordance with RTCA DO 160E Environmental Conditions and Test Procedures for Airborne Equipment and 14 CFR 25 869 Code of Federal Regulations Title 14 Aeronautics and Space Subpart D Design and Construction Subsection 25 869 a 4 Fire Protection Systems NOMENCLATURE GEN X Electronic Flight Bag PART NO 1069 4000 01 1069 4808 XX and 1069 4700 XX MANUFACTURER DAC International ADDRESS 6702 McNeil Drive Austin TX 78729 Standard Section Category DO 160E 4 0 Temperature and Altitude A4 Temperature Category A4 Operating Low temp 15 C and Operating High temp 55 C Short time Operating Low temp 30 C and Short time Operating High temp 55 C Ground Survival Low temp 55 C and Ground Survival High Temp 85 C Altitude Category Al Altitude at 50 000 feet for 2 hours Decompression from 8 000 feet to 50 000 feet within 15 Overpr
12. ane Illustrated Parts Catalog IPC 3 Wiring diagram information contained in the installation data package should be placed in the aircraft operator s appropriate airplane Wiring Diagram Manual 4 Scheduled Maintenance Program tasks are as follows a Recommended Periodic Scheduled Servicing Battery Replacement b Recommended Periodic Scheduled Preventive Murntenance Tests Car With normal power applied to the Essential and Emergency busses check the three indicator lamps on the RPU The Essential buss light and Emergency buss light are lit green and the Battery light is off If the Battery light is lit yellow the battery must be replaced The battery is good for three years and is on condition Recommended Periodic Inspections 2 8 Battery status indicator lamp inspection recommended every 300 hours Or operators performing scheduled maintenance under a CAMP Continuous Airworthiness Maintenance Program shall determine a suitable interval for internal battery checks and replacement d Recommended Periodic Overhaul None Required e Special Inspection Requirements None Required 5 Application of Protective Treatments None Required Special os E M Se None Required 1069 2510 01 D doc 1069 2510 01
13. essure at 15 000 feet for 10 minutes 50 Temperature Variation 6 0 Humidity X 7 0 Operational Shock and Crash Safety Saw tooth 6g 11msec 3 shocks per direction Saw tooth 20g 11msec 3 shocks per direction 13 0 Fungus Resistance 14 0 Salt Spray 15 0 Magnetic Effect 12 0 Sand and Dust 16 0 Power Input N B 17 0 Voltage Spike 1069 2510 01 D doc 1069 2510 01 Page 18 of 27 Rev D INTERNATIONAL Equipment Installation Manual GEN X Electronic Flight Bag b DAC Standard Section Category DO 160E cont d 18 0 AF Conducted Susceptibility Power X Not tested Inputs 19 0 Induced Signal Susceptibility 20 0 Radio Frequency Susceptibility Not tested Radiated and Conducted 21 0 Emission of Radio Frequency Energy Cockpit Equipment Notes 1 Compliance to be shown by analysis only where applicable to critical aircraft equipment Not tested ce pem Susceptibility 1069 2510 01 D doc 1069 2510 01 Page 19 of 27 Rev D Equipment Installation Manual GEN X Electronic Flight Bag DAC INTERNATIONAL CONNECTOR PIN OUT The GEN X RPU contains three male connectors J1 Note The mate for this connector is normally part of pre made interface cable P N 1069 4700 XX J2 Standard Inputs Pin Signal Function A Power Common Power Common B Aircraft Common Chassis Ground DA 0 LVDS Da
14. kasa onu 5 6 Ib Electrical Emergency Buss Monitored only Input Voltage 28 VDC Nominal 10Vdc 32Vdc operational Input Current 0 001 Amp at 28 VDC Essential Buss Input Voltage 28 VDC Nominal 10Vdc 32Vdc operational Input Current 3 1 Amp at 28 VDC 1069 2510 01 D doc 1069 2510 01 Page 10 of 27 Rev D Equipment Installation Manual GEN X Electronic Flight Bag SS AC DAN INTERNATIONA L Data Input ARINC 429 Rte ieiti Supported ARINC Data Labels ARINC 429 Latitude Longitude Altitude Ground Speed Heading Track Angle Time to go Distance to Go Time to Destination Destination Waypoint decode last wpt only Destination Waypoint indica Reliability Auto Sensing 150 110 111 370 112 314 320 103 252 351 352 074 075 743 BNR 429 BNR BCD 260 125 310 010 311 011 076 203 204 312 012 014 044 313 013 056 113 300 307 061 062 063 tes GAMA label Greater than 10 000 hours 1069 2510 01 D doc 1069 2510 01 Rev D Page 11 of 27 Equipment Installation Manual GEN X Electronic Flight Bag D DAC INTERNATIONAL OPERATION The GEN X System is a Windows based PC system which consists of a Remote Processor Unit and a Display Unit which are connected thr
15. rvals this yellow light is observed the battery should be replaced according to the section Battery Replacement Equipment Checkout The GEN X Electronic Flight Bag is used to display user selected software that may perform a variety of tasks in the cockpit Refer to the pilots guide or Aircraft maintenance manual for actual tests 1 Apply power to both the battery buss circuit breaker and the essential buss breaker System will initiate 2 Insure operation of dimming and screen on off control 3 Insure operation of EFB touch screen 4 Perform the functional test of the GEN X Electronic Flight Bag Note FMS operation is not a functional requirement for operation 1069 2510 01 D doc 1069 2510 01 Page 15 of 27 Rev D Equipment Installation Manual GEN X Electronic Flight Bag DAC INTERNATIONAL CONTINUED AIRWORTHINESS This section provides data intended to assist the installer with establishing Instructions for Continued Airworthiness as required by FARs 23 1529 25 1529 27 1529 and 29 1529 1 Maintenance Manual information for the GEN X includes a system description removal instructions installation instructions and functional testing which are all contained in the DAC International Installation Manual 1069 2510 01 this document 2 Line replaceable unit LRU part numbers and other parts contained in the installation data package should be placed in the aircraft operator s appropriate airpl
16. sess 12 REMOVAL AND REPLACEMENI 13 HDD VE 13 RPULINSTAEEMENT teret eee te peret eet iei thee eset esed vet etes dele reve ge SG y 13 s man uy am EE 13 DU REPLAGEMENT 14 BATTERY REPICA CEMENT N S 14 BATIERY CHECKOUT Ianya s ia tus aun 15 EQUIPMENT CHECK OUD 5 AE A lu S etie e e u um A cete dne Ee EE 15 CONTINUED AIRWORTHINESS 16 ENVIRONMENTAL 556 18 CONNECTOR PIN ivciccccsscscccscccscccscsccsicscsscsccscesonscsccsecscccecusscssssessescs tesctecsecscsvscetscecssescscedorsescctescsee 20 TYPICAL INTE RCONNE CD ecuocuucccco uu oo iuo oo oo eo oc o o e uu ou o o oo oo ut eu oo eoo eo e ee eo ee eoe ee ee eese noinen 22 1069 2510 01 D doc 1069 2510 01 Page 5 of 27 Rev D Equipment Installation Manual GEN X Electronic Flight Bag dy DAC INTERNATIONAL TYPICAL ETHERNET INTERCONNECTION S
17. ta 0 D DA 0 LVDS Data 0 E DA 1 LVDS Data 1 F DA 1 LVDS Data 1 G DA2 LVDS Data 2 H 2 LVDS Data 2 J CLK LVDS CLK K CLK LVDS CLK L LED 3 Emergency Operation warning light M USB DO USB Data 0 N USB DO 4 USB Data 0 P COM 2 TX RS232 COM 2 TX Touch Screen R COM 2 RX RS232 COM 2 RX Touch Screen 5 10 in system Pwr T VMC 10 V VMC10 in system Pwr U Power Ground Power Ground V Power Ground Power Ground Pin Signal Function A USB A USB 1 Power B Ethernet Ground Ethernet Shield C A Ess 28 VDC Power from Essential Buss D A Emer Power Common Emer E A Emer 28 VDC Emergency Buss Monitor F Com 2 Common RS 232 Bus Common G Com 1 TX RS 232 TX H Com RX RS 232 RX J ET 6 Ethernet wire 6 Rx K ET3 Ethernet wire 3 Rx L Ethernet wire 1 Tx 1069 2510 01 D doc 1069 2510 01 Rev D Page 20 of 27 Equipment Installation Manual GEN X Electronic Flight Bag amp DAC INTERNATIONAL Power Common M USB DI USB Data 1 N USB D1 USB Data 1 P USB Common USB Common R ARINC RX A 429 RX A 5 ARINC Shield ARINC Shield T ARINC RX B 429 RX B U ET2 Ethernet wire 2 Tx V Power Common J3 VGA Connector A Red Common VGA Red Common B Red VGA Red C Green V
18. u an LVDS cable Inputs to the RPU include FMS data and Ethernet connectivity to a switch which will in turn allow communications to the second EFB cameras and aircraft LAN or server systems On Off function is controlled through the power input logic described below shutdown down using System remains powered on Essential Buss OFF Emergency Essential Buss Buss System powers up using On On This is normal turn on sequence Essential Buss and charges internal battery System goes to internal OFF This assumes power loss emergency Battery Battery power 45 mins minimum at max battery life System performs normal OFF OFF This is the normal shutdown sequence internal battery ON This is an unexpected logic and unit remains on through essential buss power GEN X Display Unit LVDS Display Cable GEN X Remote Processor Unit FMS 28 VDC Emrg Buss Power 28 VDC Essential Buss Power FMS ARINC 429 Labels Switch Ethernet 1069 2510 01 D doc 1069 2510 01 Page 12 of 27 Rev D Equipment Installation Manual GEN X Electronic Flight Bag DAC N g INTERNATIONAL REMOVAL AND REPLACEMENT RPU Removal 1 Power down the GEN X by opening its two RPU circuit breakers and wait approximately one minute for the system to power down Verify that the three RPU annunciators located on the connector side of the RPU are extinguished 3 Remove the two
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