TDR 94D
- Solid-state, airborne, ATC transponder providing Mode A,C, and S operation
- Can be controlled via CTL-92 control or ARINC 429 as from a compatible ARINC 429 control unit
- Diversity version capable of transmitting and receiving on either of two antennas mounted on top and bottom of aircraft
- Fully compatible with TCAS II system installations requiring antenna diversity
- CTL-92T Transponder/TCAS control can be used in conjunction with CTL-92 control to add TCAS control functions
- 250-625 watts power output
- Version available with altitude input via the ARINC control bus, with expanded installation configuration options and enhancements to diagnostic and maintenance performance, with Class 3A/ADSB Mode S Transponder status , with improved altitude resolution status, with improved software to prevent non Collins TCAS Systems displaying a TCAS flag, or intermttent TCAS flag, when TCAS is in standby mode, that is compliant with European requirements for Elementary and Enhanced Surveillance for SSR Mode S operation; included is the capability for the transponder to process aircraft Flight Identification inputs and to support expanded ground station Surveillance Identifier SI codes), with ADS-B (Automatic Dependant Surveillance) capability
- New variant (-502) includes the ability to automatically generate a fixed flight ID from the Mode S code for U.S. registered aircraft
DIMENSIONS |
3.33"H x 4.90"W x 12.50"L |
WEIGHT |
8.5 lbs |
POWER REQUIREMENTS |
27.5 more or less 2.5V at 28W nominal, 30W max |
POWER OUTPUT |
250W min, 625W max |
RECEVIER IF |
60 MHz |
RECEIVER SENSITIVITY |
-77 dBm more or less 3dBm |
SOFTWARE |
DO-178A, level 2 |
ICAO |
Annex 10 |
ENVIRONMENTAL |
DO-160B (FAA); ED-12A (EUROCAE) |
DO-181, DO-144 |
DO-181, DO-144 |
FAA TSO |
TSO-C112, class 2A |
PART NUMBER | DESCRIPTION |
622-9210-001 |
original version |
622-9210-002 |
Auto Altitude Mode; Same as -001 but with upgraded TCAS interface performance, and added altitude input improves the "Burst" control interface necessary for several system configurations |
622-9210-003 |
Auto Altitude Mode; Same as -002 but with updated improvements to Mode S transponder requirements per RTCA and installation configuration options are expanded and enhancements to its diagnostic and maintenance performance is implemented |
622-9210-004 |
Supersedes -003; Auto Altitude Mode; ADS-B Compatible |
622-9352-005 |
Supersedes -003; Auto Altitude Mode; ADS-B Compatible |
622-9210-006 |
Auto Altitude Mode; Same as -005 but with improved software for TCAS flag |
622-9210-007 |
Supersedes -004/005/006; Auto Altitude Mode; Enhanced Mode S; Can be installed in aircraft WITHOUT Pro Line 4 or 21 |
622-9210-008 |
Supersedes -007; Enhanced Mode S; Can be installed in aircraft WITH Pro Line 4 or 21; Can also be installed in aircraft WITHOUT Pro Line 4 or 21 if STRAP is set properly |
622-9210-108 |
Supersedes -007/008; ADS-B capability; Enhanced Mode S; Can be installed in aircraft WITH Pro Line 4 or 21; Can also be installed in aircraft WITHOUT Pro Line 4 or 21 if STRAP is set properly |
622-9210-207 |
Supersedes -007; Auto Altitude Mode; Enhanced Mode S; Can be installed in aircraft WITHOUT Pro Line 4 or 21 |
622-9210-308 |
Supersedes -008; Enhanced Mode S; Can be installed in aircraft WITH Pro Line 4 or 21 |
622-9210-309 |
Supersedes -004/005/006/007/008/207/308 |
622-9210-310 |
Supersedes -007/008/207/308/309 |
622-9210-408 |
Supersedes -108; Enhanced Mode S; Can be installed in aircraft WITH Pro Line 4 or 21 |
622-9210-409 |
Supersedes -004/005/006/007/108/207/408; ADS-B capable (DO-260A) |
622-9210-410 |
Supersedes -007/008/108/207/308/309/408/409; ADS-B Capable (DO-260A) - CSDB data source |
622-9210-500 |
ADS-B Capable (DO-260B) - fixed wing application |
622-9210-501 |
ADS-B Capable (DO-260B) - fixed wing application |
622-9210-502 |
Automatically generates flight ID if absent |
622-9210-550 |
ADS-B Capable (DO-260B) - rotorcraft application |
622-9210-551 |
ADS-B Capable (DO-260B) - rotorcraft wing application |