Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2002F00284Line · leakingDURING TAKEOFF, ON CLIMB-OUT HAD EXCESSIVE FUEL FLOW ON NR 1 ENGINE. TOWER CALLED AND SAID VAPORS TRAILS WERE NOTED FROM NR 1. SCANNED NR 1 AND SAW FLUID. LEVELED OFF AND PULLED POWER BACK. FUEL LEAK STOPPED. DUMPED FUEL PRIOR TO LANDING. REMOVED AND REPSDR 20010207SG004Light · inoperativeDURING PREFLIGHT, FOUND EGRESS LIGHT OUT IN ONE ''C'' AND GALLEY. REPLACED WIRE STRIP, OPS CHECKED OK. (M)SDR 20010207SG011Relay · inoperativeAT CRUISE ALTITUDE OF 39,000 FEET, THE PILOT NOTICED THE DC STANDBY BUS FAIL LIGHT ON AND ESSENTIAL STANDBY POWER LIGHT ON THE PILOT''S CAUTION WARNING PANEL. WHILE WORKING THE PROBLEM THE CREW NOTICED THAT ALL POWER WAS LOST TO THE CABIN PRESSURIZATION CONTRSDR 20010207SG010Oxygen Mask · failedAT CRUISE ALTITUDE OF 39,000 FEET, THE CABIN ALTITUDE HAD STARTED TO RISE AT ABOUT 200-500 FOOT PER MINUTE. MOST OF CABIN MASKS DEPLOYED, BUT OTHERS DID NOT. THE FOLLOWING OXYGEN PANELS DID NOT OPEN NOR THE MASKS DROPPED, ROW 4 CENTER LEFT; 2 CENTER LEFT; 16SDR 20010207SG017Compressor · vibratesON DESCENT, NR 2 ENGINE VIBS WENT ABOVE 2.5 WITH WARNING LIGHT ON IN ''''B'''' CHANNEL. ''''A'''' CHANNEL WAS DEFERRED SO UNABLE TO CROSSCHECK. VIBRATIONS FELT IN THROTTLE AND AIRFRAME. SHUT NR 2 ENGINE DOWN IN FLIGHT IAW EMERGENCY PROCEDURES. PERFORMED TESDR 20010104AP011Compressor · vibrationON DESCENT, NR 2 ENGINE VIBS WENT ABOVE 2.5 WITH WARNING LIGHT ON IN B CHANNEL. A CHANNEL WAS DEFERRED SO UNABLE TO CROSS CHECK. VIBRATIONS FELT IN THROTTLE AND AIRFRAME. SHUT NR 2 ENGINE DOWN IN FLIGHT IAW EMERGENCY PROCEDURES. PERFORMED TEST NR 16 LP COM
Other aircraft with N160AT · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N160AT now.