TDR 94
- 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
- Non-diversity model for non-TCAS applications
- 250-625 watts power output
- Version available with altitude input via the ARINC control bus, with 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 (see table below)
- 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 |
|
622-9352-001 |
original version |
|
622-9352-002 |
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 |
|
622-9352-003 |
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 |
|
622-9352-004 |
Supersedes -003; Auto Altitude Mode; Same as -003 but includes upgrades for Class 3A/ADSB Mode S Transponder status |
|
622-9352-005 |
Supersedes -004; Auto Altitude Mode; Same as -004 but with improved altitude resolution status for aircraft that have digital source of altitude information |
|
622-9352-006 |
Auto Altitude Mode; Same as -005 but with improved software for TCAS flag |
|
622-9352-007 |
Supersedes -004/005/006; Auto Altitude Mode; Enhanced Mode S; Can be installed in aircraft WITHOUT Pro Line 4 or 21 |
|
622-9352-008 |
Supersedes -007/8; Enhanced Mode S; With ADS-B capability; Can be installed in aircraft WITH Pro Line 4 or 21; Can also be installed in an aircraft WITHOUT Pro Line 4 or 21 if STRAP inputs are set properly |
|
622-9352-108 |
Supersedes -007/8; Enhanced Mode S; With ADS-B capability; Can be installed in aircraft WITH Pro Line 4 or 21; Can also be installed in an aircraft WITHOUT Pro Line 4 or 21 if STRAP inputs are set properly |
|
622-9352-207 |
Supersedes -007; Auto Altitude Mode; Enhanced Mode S; Can be installed in aircraft WITHOUT Pro Line 4 or 21 |
|
622-9352-308 |
Supersedes -008; Enhanced Mode S; Can be installed in aircraft WITH Pro Line 4 or 21 |
|
622-9352-309 |
Supersedes -004/005/006/007/008/207/308 |
|
622-9352-310 |
Supersedes -007/008/207/308/309 |
|
622-9352-408 |
Supersedes -108; Enhanced Mode S; Can be installed in aircraft WITH Pro Line 4 or 21 |
|
622-9352-409 |
Supersedes -004/005/006/007/108/207/408 |
|
622-9352-410 |
Supersedes -007/008/108/207/308/309/408/409; ADS-B Capable |
|
622-9352-501 |
Automatically generates flight ID if absent |
|
622-9352-502 |
Automatically generates flight ID if absent |
|
622-9352-551 |
ADS-B Capable (DO-260B) - rotorcraft application |