Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR MEX2003400Eec · failedAIRCRAFT RETURN TO PLATFORM, DURING RT ENGINE START WITHOUT EPR AND EGT INDICATIONS ON PRIMARY DISPLAY AND EGT INDICATION ONLY ON SECONDARY DISPLAY WITH CIRCUIT BREAKER THROWN AWAY P6, M16,17,18,22,23 AND 24. DURING REVISION WERE DETECTED EICAS MESSAGES P ADCSDR MEX2003399Eec · failedAIRCRAFT RETURNED TO PLATFORM , DURING TAXI, RT ENGINE SHUT OFF SLOWLY. DURING REVISION WERE DETECTED EICAS MESSAGES R ENG FUEL SOL, R ENG OIL PRESS. R ENG PRI CONT AND R ENG SEC CONT. THE ENGINE WAS CHECK FOR CONDITION AND DETECTING FLAME EVIDENCE IN TURBISDR MEX2003386Engine · malfunctionedFLT 494 - MID-MEX - AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AFTER RIGHT ENGINE STARTED, IT SHUT DOWN. RIGHT ENGINE AND EICAS MESSAGES WERE CHECKED IAW 72-00-00 AND RIGHT ENGINE WAS RESTARTED, ALL CORRECT. DURING OVERNIGHT SERVICE, RIGHT ENGINE WAS SDR MEX2003280Module · malfunctionedAIRCRAFT RETURNED TO GATE, EICAS STATUS MESSAGE ELEV ASYM. FIM PROCEDURE WAS PERFORMED WITH NEGATIVE RESULTS IAW 27-09-00 FIG 106 PAGE 150. THE STAB/TRIM ALL LOCK AND ASYM MODULE WAS INTERCHANGED IAW FIM PROCEDURE 27-09-00, ALL TESTS CORRECT. (M)SDR MEX2003261Fmc · inoperativeDURING TRANSIT CHECK WAS DETECTED BOTH INTERNAL SYSTEM OUT SERVICE IN ANY SELECTION. THE BOTH FMC COMPUTER SYSTEM WERE DEFERRED IAW MEL. FMC COMPUTERS WERE REPROGRAMMED IAW MM 34-21-00, ALL TESTS CORRECT.SDR MEX2003222Shaft · brokenFLT 402 - MEX-JFK - AIRCRAFT RETURN TO PLATFORM, ENGINE NR 1 DID NOT START. DURING REVISION, THE STARTER SHAFT WAS BROKEN. THE STARTER WAS REPLACED IAW MM 80-11-01, ALL TESTS CORRECT. (M)SDR MEX2003193Recorder · failedDURING TRANSIT CHECK, FLT REC OFF LIGHT TURNED ON. ASSOCIATED BRAKES WERE RESET BUT FAIL CONTINUES. WIRING WAS CHECKED IAW WDM 31-31-03, ALL CORRECT. FLIGHT DATA RECORDER AND FDAU WERE REPLACED IAW MM 31-31-03, ALL TESTS CORRECT. (M)SDR MEX2003159Warning Light · illuminatedAIRCRAFT RETURNED TO PLATFORM DUE TO MACH SPEED TRIM MESSAGE ILLUMINATION. THE BITE TEST ON P61 ADC WAS ACCOMPLISHED AND LIGHT ILLUMINATION IN OVERHEAD P11. FLIGHT CONTROLS TEST WAS ACCOMPLISHED AND LT ELEV PCU MESSAGE ILLUMINATED. THE MESSAGE APPEARED ONLYSDR MEX2002309Engine · bird ingestionFLT 490 - MID-MEX - DURING TAKEOFF AFTER THE ROTATION MOVEMENT, LEFT ENGINE HAD A BIRD STRIKE, THE ENGINE MOMENTARILY STALLED BUT IT RECOVERED ALL PARAMETERS ITSELF. AT MEX, PERFORMED BORESCOPE INSPECTION TO SUCH ENGINE IAW MM 71-05-00 FIG 103. ENGINE WAS FOSDR MEX2002025Valve · failedFLT 913 - MTY-MEX - AIRCRAFT RETURNED TO PLATFORM, EICAS MESSAGE LEFT HYD RSVR PRESS WARNING. THREE QUARTERS OF HYDRAULIC FLUID WAS ADDED, RVSR WAS DISCONNECTED AND CLEANED, AFTER ENGINE WAS STARTED FAIL APPEARED AGAIN, AIRCRAFT TOOKOFF IN THAT CONDITION. HY
Other aircraft with N301AM · 2
The FAA can assign a mark to another aircraft once a registration is cancelled. N301AM is registered now to the first aircraft listed.