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TT31 Transponder Installation Manual
00455-00
5.4.4 Molex Crimp Terminals
18 June 2014
Issue AP
The Molex connector contacts should be wired with wire of 18-24 AWG. The contacts are compatible with a wide range of crimp tools. Ensure that the contact has been crimped using both the conductor crimp and the insulator crimp.
Once crimped, the contacts should be slotted into the rear of the connector shell. Push the contact in until the retaining tab clicks into place. Tug gently to confirm the contact is locked in place.
The contacts can be easily removed using the Molex removal tool, or equivalent. This is pushed gently into the connector shell from the side opposite from the wire entry, and lifts the retaining tab from the stop, allowing the contact to be eased out by pulling on the wire.
5.5 Antenna Installation
The antenna should be installed according to the manufacturer’s instructions.
The following considerations should be taken into account when siting the Antenna.
The antenna should be well removed from any projections, the engine(s) and propeller(s). It should also be well removed from landing gear doors, access doors or others openings which will break the ground plane for the antenna.
The antenna should be mounted on the bottom surface of the aircraft and in a vertical position when the aircraft is in level flight.
Avoid mounting the antenna within 3 feet of the ADF sense antenna or any COMM antenna and 6 feet from the transponder to the DME antenna.
Where practical, plan the antenna location to keep the cable lengths as short as possible and avoid sharp bends in the cable to minimise the VSWR.
To prevent RF interference, the antenna must be physically mounted a minimum distance of 3 feet from the TT31 Mode S transponder.
Electrical connection to the antenna should be protected to avoid loss of efficiency as a result of the presence of liquids or moisture. All antenna feeders shall be installed in such a way that a minimum of
RF energy is radiated inside the aircraft.
5.5.1 Antenna Cable
The TT31 is designed to meet Class 1 requirements with an allowance of 2 dB for loss in the connectors and cable used to connect it to the antenna. Excessive loss will degrade both transmitter output power and receiver sensitivity.
Allowing 0.25dB loss for the connector at each end of the antenna cable assembly leaves an allowance of 1.5dB maximum loss for the cable itself.
An acceptable cable:
Trig Avionics Limited
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Table of contents
- 7 PREFACE
- 8 INTRODUCTION
- 10 TECHNICAL SPECIFICATIONS
- 10 Approved Deviations
- 11 Mode S Transponder Installation Approval
- 11 ADS-B Installation Approval
- 12 UNIT AND ACCESSORIES SUPPLIED
- 14 INSTALLATION
- 15 Primary Interface – Pinout
- 16 Secondary Interface - Pinout
- 16 Orientation Diagram
- 17 Molex Crimp Terminals
- 17 Antenna Cable
- 18 BNC Connector
- 21 Power Input
- 21 Lighting Bus Input
- 21 Mutual Suppression
- 21 Serial Port Options
- 21 Altitude Inputs and Output
- 22 Squat Switch Input
- 22 Ident Switch Input
- 22 External Standby Input
- 22 Audio Output
- 22 Altitude Alerter Output
- 23 GPS Position Input
- 23 TIS Traffic Output
- 24 INSTALLATION SETUP AND TEST
- 24 Aircraft Registration (VFR Flight ID)
- 24 Aircraft Address Programming
- 25 VFR Squawk Code
- 25 Airspeed Category
- 25 Aircraft Category
- 25 Squat Switch Source
- 25 ARINC TIS Output
- 25 RS232 Input/Output
- 26 ADS-B Configuration
- 27 Audio Volume
- 27 LCD Dim Point
- 27 LCD Brightness Curve
- 27 Interface Check
- 27 Altitude Check
- 27 Lighting Bus
- 28 Temperature
- 28 RS232 Input Check
- 28 Transponder Cycles
- 29 POST INSTALLATION CHECKS
- 30 NORMAL OPERATION
- 33 CONTINUED AIRWORTHINESS
- 33 GPS Receiver Maintenance
- 33 GPS Receiver Design Changes
- 34 LIMITED WARRANTY
- 35 ENVIRONMENTAL QUALIFICATION FORM
- 37 ADS-B COMPLIANCE