lled, each system is separate of the other except that both TDR-94D transponders are controlled by the single CTL-92E Transponder Control Unit. The CTL-92E provides a means for entering the flight identification code into the TDR-94D transponder(s). The flight identification code is one of the additiona

er No. I DC Primary bus through a 3 amp circuit breaker labeled NO. I XPDR. This circuit breaker also supplies power to the 28VDC IN NO I pin of the CTL-92E control unit. The number two transponder unit if installed is supplied electrical power from the 28VDC Essential bus through another existing 3 amp

nsponder(s) arc located on the forward pilot side lower avionics shelf in the nose of the aircraft. The transponder(s) arc controlled with a single CTL-92E control unit located in the cockpit on the 3 0070120A SDNY_GM_02757727 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00244