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GTXTM 327 TRANSPONDER INSTALLATION MANUAL

Garmin International, Revision JMay 2003 GTXTM 327 TRANSPONDERINSTALLATIONMANUALPage AGTX 327 INSTALLATION ManualRev J190-00187-02 Copyright 1999-2003 Garmin Ltd. or its subsidiariesAll Rights ReservedExcept as expressly provided herein, no part of this MANUAL may be reproduced, copied, transmitted, disseminated,downloaded or stored in any storage medium, for any purpose without the express prior written consent of hereby grants permission to download a single copy of this MANUAL and of any revision to this MANUAL onto ahard drive or other electronic storage medium to be viewed and to print one copy of this MANUAL or of any revisionhereto, provided that such electronic or printed copy of this MANUAL or revision must contain the complete text ofthis copyright notice and provided further that any unauthorized commercial distribution of this MANUAL or anyrevision hereto is strictly International, E.

Garmin International, Inc. 190-00187-02 Revision J May 2003 GTXTM 327 TRANSPONDER INSTALLATION MANUAL

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Transcription of GTXTM 327 TRANSPONDER INSTALLATION MANUAL

1 Garmin International, Revision JMay 2003 GTXTM 327 TRANSPONDERINSTALLATIONMANUALPage AGTX 327 INSTALLATION ManualRev J190-00187-02 Copyright 1999-2003 Garmin Ltd. or its subsidiariesAll Rights ReservedExcept as expressly provided herein, no part of this MANUAL may be reproduced, copied, transmitted, disseminated,downloaded or stored in any storage medium, for any purpose without the express prior written consent of hereby grants permission to download a single copy of this MANUAL and of any revision to this MANUAL onto ahard drive or other electronic storage medium to be viewed and to print one copy of this MANUAL or of any revisionhereto, provided that such electronic or printed copy of this MANUAL or revision must contain the complete text ofthis copyright notice and provided further that any unauthorized commercial distribution of this MANUAL or anyrevision hereto is strictly International, E.

2 151st StreetOlathe, KS 66062 USAT elephone: 913-397-8200 Aviation Panel-Mount Technical Support Line (Toll Free): (Europe) 5, The Quadrangle, Abbey Park Industrial EstateRomsey, SO51 9DL, : 44 OF REVISIONSR evisionRevisionDateDescriptionECO #A01/19/00 Initial Release12550B02/28/00 Update Configuration Procedure12785C06/01/00 Update Configuration Procedure. Add JTSO references and STC Interconnect Diagram, New RF ConnectorSpacer P/N, Plus Misc P/N s @ Section and Clarifications16867G05/01/02 Updated unit and accessory part numbers18295H11/01/02 Revised to reflect new software19608J5/22/03 Revised to reflect software OF EFFECTIVE PAGESPage ..Ji ..Jii ..Jv ..Jvi ..JPage ..J2 ..J3 ..J4 ..J5 ..J6 ..J7 ..J8 ..JPage ..J10 ..J11 ..J12 ..J13 ..J14 ..J15 ..J16 ..JPage ..J18 ..J19 ..J20 ..J21.

3 J22 ..J23 ..J24 ..JPage JPage JPage BlankPage JGTX 327 INSTALLATION ManualPage i190-00187-02 Rev JINFORMATION SUBJECT TO EXPORT CONTROL LAWSThis document may contain information which is subject to the Export Administration Regulations ("EAR") issued by theUnited States Department of Commerce (15 CFR, Chapter VII, Subchapter C) and which may not be exported, released,or disclosed to foreign nationals inside or outside of the United States without first obtaining an export license. Aviolation of the EAR may be subject to a penalty of up to 10 years imprisonment and a fine of up to US $1,000,000 underSection 2410 of the Export Administration Act of 1979. Include this notice with any reproduced portion of this product, its packaging, and its components contain chemicals known to the State of California to cause cancer, birthdefects, or reproductive harm.

4 This Notice is being provided in accordance with California's Proposition 65. If you haveany questions or would like additional information, please refer to our web site at iiGTX 327 INSTALLATION ManualRev J190-00187-02 This page intentionally left blankGTX 327 INSTALLATION ManualPage iii190-00187-02 Rev JTABLE OF DESCRIPTION .. EQUIPMENT DESCRIPTION .. MUTUAL SUPPRESSION PULSES .. INTERFACE SUMMARY .. GTX 327 TRANSPONDER SPECIFICATIONS .. TRANSPONDER Physical Characteristics of the GTX 327 .. EQUIPMENT AVAILABLE .. Configurations Available .. INSTALLATION Accessories .. ADDITIONAL EQUIPMENT REQUIRED .. INSTALLATION APPROVAL .. ATC TRANSPONDER TESTS AND INSPECTIONS .. LIMITED WARRANTY .. UNPACKING AND INSPECTING ANTENNA Location Considerations .. Antenna INSTALLATION .

5 INSTALLATION Approval Considerations for Pressurized Aircraft .. Antenna Cable Antenna Cable Connectors .. GTX 327 COOLING AIR .. ELECTRICAL CONNECTIONS .. Power and Lighting Function .. Altitude RS-232 Serial Data Electrical INSTALLATION CONFIGURATION & CHECKOUT PROCEDURE .. AIRCRAFT STATION LICENSING REQUIREMENTS .. OPERATION .. Function Selection Switches .. Function Code Selection ..23 Page ivGTX 327 INSTALLATION ManualRev CONFIGURATION PAGES .. DISPLAY MODE Page .. DISPLAY BACKLIGHT Page .. KEY LIGHTING Page .. CONTRAST CONFIGURATION Page .. RS-232 INPUT/OUTPUT Page .. OPERATION CONFIGURATION Pages .. AIRCRAFT TYPE Page .. RS-232 INPUT VIEW Page .. GRAY CODE INPUT Page .. EXTERNAL SWITCH Page .. ANALOG INPUT Page ..32 APPENDIX A. CERTIFICATION CONTINUED AIRWORTHINESS.

6 ENVIRONMENTAL QUALIFICATION FORM ..36 APPENDIX B. ASSEMBLY AND INSTALLATION DRAWINGS ..39 APPENDIX C. STC 327 INSTALLATION ManualPage v190-00187-02 Rev JLIST OF ILLUSTRATIONSFIGUREPAGE2-1 RF Connector Assembly ..102-2 Dual GTX 327, Single Encoder, Serial Input GTX 327 Front Panel ..19B1 GTX 327 Outline GTX 327 Connector/Rack Kit Assembly GTX 327 Recommended Panel Cutout Dimensions ..45B4 GTX 327 Interconnect Wiring Dual TRANSPONDER Interconnect Wiring Diagram, Encoding Altitude Connections ..49 LIST OF TABLESTABLEPAGE2-1 Recommended Antenna Cable Type ..92-2 Pin Contact Part Numbers ..122-3 Recommended Crimp P3271 Pin Aircraft Power Pin Assignments ..142-6 Aircraft Lighting Pin Encoded Altitude Pin Assignments ..152-8 Discrete Inputs Pin RS 232 Input/Output Pin Assignments.

7 16 Page viGTX 327 INSTALLATION ManualRev J190-00187-02 GTX 327 HARDWARE MOD LEVEL HISTORYThe following table identifies hardware modification (Mod) Levels for the GTX 327 TRANSPONDER . ModLevels are listed with the associated service bulletin number, service bulletin date, and the purpose of themodification. The table is current at the time of publication of this MANUAL (see date on front cover) and issubject to change without notice. Authorized GARMIN Sales and Service Centers are encouraged to accessthe most up-to-date bulletin and advisory information on the GARMIN Dealer Resource web site using their GARMIN-provided user name and OF MODIFICATIONAt the time of this revision, the current software version for the GTX 327 is Thesoftware version and information in this document are subject to change without notice.

8 Visitthe Garmin web site ( ) for current MANUAL updates and supplementalinformation concerning the operation of this and other Garmin 327 INSTALLATION ManualPage 1190-00187-02 Rev MANUAL describes the physical, mechanical and electrical characteristics, plus the installationrequirements and operating instructions for the Garmin GTX 327 Digital Display TRANSPONDER pertaining to the maintenance, alignment and procurement of replacement parts is found inthe GTX 327 Maintenance MANUAL , Garmin P/N 190-00187-05. After INSTALLATION of the GTX 327, FAAForm 337 must be completed by an appropriately certificated agency and ATC TRANSPONDER tests requiredby 14 CFR, Part must be completed to return the aircraft to DESCRIPTIONThe Garmin GTX 327 is a panel-mounted TRANSPONDER with the addition of altitude reporting and timingfunctions.

9 The TRANSPONDER is a radio transmitter and receiver that operates on radar frequencies,receiving ground radar or TCAS interrogations at 1030 MHz and transmitting a coded response of pulsesto ground-based radar on a frequency of 1090 with other Mode A/Mode C transponders, the GTX 327 replies with any one of 4,096 codes, whichdiffer in the position and number of pulses transmitted. By replying to ground transmissions or TCAS interrogations, the GTX 327 enables ATC to display aircraft identification, altitude and groundspeed onATC radar screens or TCAS traffic indicators. The GTX 327 is equipped with IDENT capability thatactivates the Special Position Identification (SPI) pulse for 18 GTX 327 is configured with all key controls. The layout of the front panel keys and displayssegregates the TRANSPONDER s primary functions from the secondary timing functions.

10 The unit can beconfigured so the aircraft avionics master bus can turn the unit SUPPRESSION PULSESO ther equipment on board the aircraft may transmit in the same frequency band as the TRANSPONDER , suchas DME or another TRANSPONDER . Mutual suppression is a synchronous pulse that is sent to the otherequipment to suppress transmission of a competing transmitter for the duration of the pulse traintransmission. The TRANSPONDER transmission may be suppressed by an external source and otherequipment on board may be suppressed by the TRANSPONDER . This feature is designed to limit SUMMARYThe GTX 327 provides the following interface connections via the rear connector: Ten (10) encoding altimeter inputs. External IDENT input. External STBY input. External suppression pulse input. Switched power output of up to amps (for digital altitude encoder power).


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