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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

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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

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- Standby Altimeter. S/N: 291256 Date: 2 JAN 201Q Next Due: JAN 2012 Next Due: JAN 2012. Next Due: JAN 2012. 17. Transponder Test, FAR 91.413: (TDR-94D) - NI S/N: a Date: 2 JAN 2010 Next Due: JAN 2012. - N2 S/N: 30MLF Date: 2 JAN 2010 Next Due: JAN 2012. IS. Compass System Type: Liter AHRS I.C