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flight identification code is one of the additional requirements for ADS-B functionality. Software in the Rockwell Collins CTL-92E is controlled by Rockwell Collins assigning a specific part number to the CTL-92E. ffegie 88.66° ON ALT OFF ATC 0 Om % Rockwell Collins CTL-92E transponder control head ADS-

E Transponder Control Unit The transponders) TDR-94D(s) are controlled by a single Rockwell Collins CTL-92E Transponder Control Unit. When a single TDR-94D is installed, the number I transponder must be selected on the CTL-92E. When dual transponder systems arc installed, each system is separate of the

AMC 5. 2014 2.5.2 Aircraft equipment requirements The aircraft must be equipped with at least the following: I. A single or dual Rockwell Collins TDR-94D transponderts) part numbers 622- 9210-550 installed in accordance with drawing list PHI-576-DL-0015. Revision IR. 2. A single CTL-92E Rockwell Coll

tallations for general condition and security. 300 Hours of Operation Remove the right side nose avionics bay access panel and visually inspect the TDR-94D transponder(s) and mounting racks for general condition, security of attachment, and deformation. If dual TDR-94D transponders are installed, pay p

ine Control (FADEC) and associated systems. ST10959SC: Installation of Rockwell Collins Pro Line 21 Electronic Flight Instrument System (EFIS) with Rockwell Collins FMS-6100, Localizer Performance with Vertical Guidance (LPV) approach capability and Universal Avionics System Company (UASC) Terrain Awareness Wa

X 0 or 1 CI 429.200 GPS Antenna CI 429-200 0 or 1 GPS-40005 GPS Receiver 822-2189- 004/005/006/007/010/011/100 0, 1 or 2 *Either TDR-94 or TDR-94D will be Installed. The above equipment is installed in accordance with FM Supplemental Type Certificate No. ST11216DS . See the List of Applicabl

teroperenea (Department of Transportation Teeferaffiviation Administration Suppkmentaf Type Cert cate Wum6ersRo9e4iRc This certfficate issueito: Rockwell Collins. Inc. 400 Collins Road NE, MS 164-100 Cedar Rapids, IA 52498 certifies that the change in the type disOnfor the following product with the limitat

al wiring and component provisions, per the Installation Instructions (-02 Installation), PHI document PHI-S7641.0003, revision 2. • Installed the TDR-94D (part number 622-9210-551. 2 each). per the PHI mechanical drawing PHI-S76-60936. revision IR. Installed the ADS-B 1/FAIL Annunciator (part number 9

ine Control (FADEC) and associated systems. ST10959SC: Installation of Rockwell Collins Pro Line 21 Electronic Flight Instrument System (EFIS) with Rockwell Collins FMS-6100, Localizer Performance with Vertical Guidance (LPV) approach capability and Universal Avionics System Company (UASC) Terrain Awareness Wa

X 0 or 1 CI 429-200 GPS Antenna CI 429-200 0 or 1 GPS-40005 GPS Receiver 822-2189- 004/005/006/007/010/011/100 0, 1 or 2 *Either TOR-94 or TDR-94D will be installed. The above equipment is installed in accordance with FM Supplemental Type Certificate No. ST11216DS . See the List of Applicabl