Transponder. At the publication date of this manual the software version identifier for the TT21 and TT22 is 2.12 and the FPGA version identifier is 1.2. The TC20 controller software version identifier is 1.14. The software and FPGA versions are subject to change without notice.
The TT22 has a nominal power output of 250 watts, and meets the power output requirements for Class 1. The ADS-B function meets DO-260B class B0 for the TT21 and class B1S for the TT22. The TT21/TT22 is certified to ETSO 2C112b and ETSO C166a, and to FAA TSO C112c and C166b.
00560-00 Power Input The TT21/TT22 operates on 11 to 33 Volts DC. Front Panel Datalink A two wire data link is used to connect the TT21/TT22 and the controller. Front Panel Power The controller is powered from the transponder. Remote On/Off The on-off switching is on the controller, and switches this input.
22 August 2017 00560-00 3.4 Installation Approval The conditions and tests required for the TSO approval of the TT21/TT22 Mode S Transponder are minimum performance standards. It is the responsibility of those desiring to install this transponder on or within a specific type or class of aircraft to determine that the aircraft operating conditions are within the TSO standards.
TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 Issue AP 4. Unit and Accessories supplied 4.1 TT21 Mode S Transponder Items The TT21 Mode S transponder includes the following items: Unit Description Part Number TT21 Mode S Transponder 00675-00-01 TT21/TT22 Mounting Tray 00667-00 4.2 TT22 Mode S Transponder Items...
00736-00 Short mounting screws, 4-40 thread 00737-00 4.5 Required Items Additional items you will require, but which are not in the TT21/TT22 package, include: Antenna and fixing hardware. The TT21/TT22 is compatible with any transponder antenna approved to ETSO C74 or 2C112 or...
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TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 Issue AP equivalent. Cables. You need to supply and fabricate all required cables. Guidance on cable types is given in section 5 below. Fixings. To secure the transponder tray to the airframe you will need at least 3 flat head screws and three self-locking nuts.
The rubber band can be snipped off and discarded when the installation is complete. If you are using the Trig compact cut-out, you do not need the mounting adapters. The controller should be mounted using the four SHORT screws provided.
4-40. 5.3 Transponder Main Unit Mounting The TT21/TT22 Mode S transponder is designed to be mounted in any convenient location in the cockpit, the cabin, or an avionics bay. The following installation procedure should be followed, remembering to allow adequate space for installation of cables and connectors.
5.5 TT21/TT22 Transponder Electrical Connections The TT21/TT22 has a single 25 way female socket which provides the data and power inputs to the transponder. A single TNC coaxial connector attaches to the antenna.
The power supply can be 11-33 Volts DC; no voltage adjustment is required. Use a 3 Amp circuit breaker for power supply protection to the TT21/TT22. It is always good practice to use more than one ground wire in an installation.
TMAP interface comprises a balanced pair of signals, called A and B, both of which must be connected for communication to work. There are two sets of TMAP pins on the TT21/TT22, TMAP1 A and B, and TMAP2 A and B. This is to support future installation wiring options. The two sets are identical, and either pair (TMAP1 or TMAP2) may be used to connect to the control head.
Issue AP signal when it is transmitting, and can be suppressed by other equipment that asserts the signal. The TT21/TT22 will drive approximately 24 Volts on the output (independently of supply voltage), and will treat the input as active whenever the bus has greater than 10 Volts.
5.6.10 TIS Traffic Output The TIS traffic is an RS232 output and supports the display of uplinked Traffic Information Service messages. The TT21/TT22 TIS output can drive the Trig proprietary traffic protocol, and can also support the format used by certain Garmin handheld displays, including the 495, 496, 695 and 696.
5.8 TC20 Controller Interface Details 5.8.1 TMAP Bus TMAP is a Trig proprietary bus based on RS485 signalling. It provides a bi- directional interface between the transponder and the control head. Each TMAP interface comprises a balanced pair of signals, called A and B, both of which must be connected for communication to work.
00560-00 TMAP A and B lines on the controller should be connected to the corresponding A and B lines of either TMAP1 or TMAP2 on the TT21/TT22. 5.8.2 Altitude Out The TC20 incorporates an altitude encoder. Certain GPS receivers can benefit from having altitude information supplied to them.
5.10 Wiring Considerations The connection from the TT21/TT22 transponder to the TC20 uses a minimum of six (6) signal lines; the TMAP pair, the Power and Ground pair, and the Remote On discrete line plus associated ground line. In a certified installation the normal wire choice would be Tefzel hook-up wire.
TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 The distance between the TT21/TT22 transponder and the TC20 controller is limited by the impedance of the wire between them. The TC20 is powered from the TT21/TT22, not from aircraft power, and therefore the acceptable voltage drop in the power line is what limits the distance.
TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 Issue AP 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.
00560-00 5.11.2 Antenna Cable The TT21 is designed to meet Class 2 requirements with an allowance of 2 dB for loss in the connectors and cable used to connect it to the antenna. The TT22 is designed to meet Class 1 requirements with the same 2 dB allowance.
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TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 Issue AP Insertion MIL-C-17 Electronic Length Length Loss Cables Cable Electronic in Feet dB/metre at Specialists Metres 1090MHz Type 8’ 4” 2.54 0.59 M17/128 (RG400) 10’ 4” 3.16 0.47 3C142B 12’ 6”...
TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 Avoid routing the cable round tight bends. Avoid kinking the cable even temporarily during installation. Secure the cable so that it cannot interfere with other systems. 5.11.3 TNC Connector This section describes the technique for attaching the antenna cable to the supplied TNC connector.
TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 Issue AP 0.28 0.19 Crimp the centre contact to the cable. Insert the cable into the connector – the centre contact should click into place in the body, the inner shield should be inside the body of the connector and the outer shield should be outside the body.
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TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 The following diagram shows the general arrangement, although other combinations may be used: For aircraft with ¼ inch static lines, two adapters are provided which can convert from ¼ inch inside diameter hoses to the 5 mm hose in the install kit.
Issue AP 6. Installation Setup and Test The TT21/TT22 uses a simple setup system to program important system parameters, including the Mode S address. In the original factory configuration, the setup screen is the first thing that runs when you switch on the transponder.
These addresses are usually written as a 6 digit hexadecimal number, although you may also encounter one written as an 8 digit octal number. The TT21/TT22 only understands the hexadecimal format, so you must first convert an octal number to hexadecimal.
TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 Issue AP the aircraft. 6.1.5 Aircraft Category To assist ATC tracking of aircraft, an aircraft category can be transmitted by Mode S transponders. Using the rotary knob, select the aircraft category that most closely matches the aircraft the transponder is installed in.
9600 bps. Panel mount GPS units with Aviation format outputs generally also run at 9600 bps. NMEA GPS units generally run at 4800 bps. Trig TN70, Freeflight 1201 and NexNav 3101 GPS receivers run at 19200 bps. The Trig TN72 runs at 9600 bps.
00560-00 Issue AP used by ATC to identify taxiing routes and potential conflicts. When configured for ADS-B, the TT21/TT22 will ask for the aircraft length and width (wingspan), in metres, and will calculate the appropriate size code for transmission. 6.1.13 GPS Antenna Offset The GPS antenna offset is used together with the aircraft length and width to manage taxiway conflicts.
The purpose of these exercises is to present a changing load on the power lines from the TT21/TT22. If you suspect a potential problem with the wiring to the controller, it is worth monitoring the displayed voltage for several seconds to find the worst-case reading.
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Note: DO NOT EXCEED THE ALTITUDE OR RATE OF CLIMB LIMITS OF THE PITOT-STATIC INSTRUMENTS OF THE AIRCRAFT. The Trig altitude encoder is a solid state device and will not be affected by excess altitude or rate of climb and descent, but the mechanical instruments in the aircraft can easily be damaged by being driven beyond their intended range.
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TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 Skip over the configuration modes until reaching the encoder calibration section. Accept the Yes/No question; the LOW ALTITUDE set point will now be active, and an altitude will be displayed. On the static test set, drive the altitude to 0 feet.
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TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 Issue AP 18. Read the primary altimeter value, and turn the right knob on the TC20 until the altitude displayed on the TC20 matches the altitude on the primary altimeter. 19. Press ENT on the TC20; the display moves to the test screen.
TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 7. Post Installation Checks Post installation checks should be carried out in accordance with your certification requirements. These checks should include: Mode S interrogations to verify correct address programming. Verification of the reported altitude using a static tester.
TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 Issue AP 8. Normal Operation 8.1 Overview On the front panel is a monochrome LCD display flanked by a rotary mode selector knob (OFF, SBY, GND, ON, and ALT) and a continuously rotating knob used for code and data entry.
TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 8.3 Mode Selector Knob The left hand knob controls the power to the transponder and the operating mode. Power is removed from the transponder. The transponder is on, but will not reply to any interrogations.
8.7 General Low Temperature Operation The TT21/TT22 is certified to operate correctly down to -20°C, but at low temperatures the display may be impaired. On a cold day you may need to wait for the cockpit to warm up to ensure normal operation.
TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 8.8 ADS-B Monitor The ADS-B Monitor is only available on installations that include an ADS-B position source. The ADS-B Monitor provides a display of the position information that is being transmitted in ADS-B position reports. This can provide confirmation that the correct information is being transmitted, particularly where the GPS source is remote from the transponder.
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TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 Issue AP on the screen and pass that information to your avionics maintenance organisation. ______________________ Trig Avionics Limited...
9. Continued Airworthiness Other than for periodic functional checks required by the regulations, the TT21/TT22 Mode S transponder has been designed and manufactured to allow “on condition maintenance”. This means that there are no periodic service requirements necessary to maintain continued airworthiness, and no maintenance is required until the equipment does not properly perform its intended function.
Heriot Watt Research Park Riccarton, Currie, EH14 4AP Trig Avionics will not accept or pay for any charges for warranty work performed outside our factory without prior written consent. This warranty applies only to products in normal use. It does not apply to units...
TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 11. Environmental Qualification Forms Nomenclature: TT21 Mode S Transponder Part No: 00675-00-01 ETSO: 2C112b, C166a Manufacturer: Trig Avionics Limited Address: Heriot Watt Research Park, Riccarton, Currie, Scotland, EH14 4AP Conditions DO-160F Description of Conducted Tests...
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TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 Issue AP Vibration Aircraft zone 2; type 3, 4, 5 to category S level M, type 1 (Helicopters) to category U level G Equipment identified as Category X – no test Explosion required Equipment identified as Category X –...
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TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 Nomenclature: TT22 Mode S Transponder Part No: 00745-00-01 ETSO: 2C112b, C166a Manufacturer: Trig Avionics Limited Address: Heriot Watt Research Park, Riccarton, Currie, Scotland, EH14 4AP Conditions DO-160F Description of Conducted Tests Section...
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TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 Issue AP Equipment identified as Category X – no test Explosion required Equipment identified as Category X – no test Waterproofness 10.0 required Equipment identified as Category X – no test Fluids Susceptibility 11.0...
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TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 Nomenclature TC20 Mode S Controller Part Number: 00649-00 ETSO: 2C112b, C88a Manufacturer Trig Avionics Limited Address Heriot Watt Research Park, Riccarton, Currie, Scotland, EH14 4AP Conditions DO-160F Description of Conducted Tests Section...
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TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 Issue AP Equipment identified as Category X – no test Explosion required Waterproofness 10.0 Equipment tested to Category W (front face only) Equipment identified as Category X – no test Fluids Susceptibility 11.0...
00560-00 12. ADS-B Compliance TT21/TT22 transponders include support for Extended Squitter ADS-B out. The TT21/TT22 with software version 2.1 or higher is a DO-260B compliant broadcast participant. 12.1 ADS-B Parameters Supported The following table summarises the ADS-B parameters that are transmitted by the TT21/TT22 transponder when connected to an appropriate GPS receiver.
AC 20-165B when directly connected to the GPS units listed below, and will form the basis of a 14 CFR § 91.227 compliant ADS-B installation. The following combinations are available under Trig STC program for certified aircraft. GPS Unit...
Trig Avionics Limited. 12.3 CS-ACNS Compliance The TT21 or TT22 transponder can be connected to the following GPS units to form the basis of a CS-ACNS compliant ADS-B installation: GPS Unit GPS Output Setting...
14 CFR § 91.227. 12.5 Automatic Air/Ground Determination The TT21/22 can report ADS-B surface and airborne messages. The squat switch input is designed to be used with an automatic air/ground switching device as defined in section 5.6.7. If no squat switch input is available, the transponder can automatically determine the air/ground status from the GPS input.
TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 Issue AP 13.2 Front Panel Controller Dimensions Controller shown without the mounting adapters (00678-00) used for 57mm (2¼ inch) instrument mounting. All dimensions in millimetres. ______________________ Trig Avionics Limited...
TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 13.3 Front Panel Cut-out Options The front panel controller can be fitted to either the compact mounting hole or a conventional 57mm (2¼ inch) instrument cut-out. The compact mounting is a truncated 58 mm opening; please note that the mounting screws are NOT in the same location for the two options.
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TT21/TT22 Transponder Installation Manual 22 August 2017 00560-00 Issue AP Note: The following diagram is intended to be to scale, however variations in the printing process mean that you MUST check all dimensions before using it as a template. All dimensions in millimetres.
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