FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N742AL and the event date: up to this one’s cancellation.
Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR TSAA0752062Control Rod · out of adjustNON-ETOPS FLIGHT 376 OAK-RNO - DURING CLIMB, THE AIRCRAFT FAILED TO PRESSURIZE. THE CREW RETURNED TO OAK WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE FORWARD ENTRY DOOR HORIZONTAL CONTROL ROD PER AMM 52-11-00-5 AND PRESSURIZED THE AIRCRAFT ON THE GROUNSDR TSAA0549043Fuel Control · failedETOPS FLT 944 HNL-SNA - APU AUTO SHUT DOWN WITH OVER SPEED INDICATION. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND FCU CANNON PLUG PIN 1 TO 10 RESISTANCE MORE THAN 100K OHMS AND PIN 10 TO 12 UNDER 30 OHMS. REPLACED APU FUEL CONTROL UNITSDR TSAA0549042Apu · shutdownFLT 484 OGG-SNA - APU AUTO SHUT DOWN WITH OVER SPEED INDICATION. CREW DIVERTED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED APU INSPECTION AND AUTO SHUTDOWN INSPECTION PER AIRCRAFT FIM 49-30-00-810-802 AND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVSDR TSAA0534030Pitot Head · obstructedETOPS FLT 441 (LAS) CAPTAIN AND FIRST OFFICER’S AIRSPEED DISAGREE; ABORTED TAKEOFF. FOUND DEBRIS IN CAPTAIN SIDE PITOT TUBE. CLEANED DEBRIS FROM PITOT; OPERATIONS CHECKED PITOT TUBES AND RETURN TO SERVICE.SDR TSAA0572023Hmu · defectiveETOPS, MAINTENANCE RUN: NR 2 ENGINE FLAMED OUT DURING ENGINE RUN. THE ENGINE RUN WAS PERFORMED AFTER A HEAVY PHASE CHECK. REMOVED AND REPLACED NR 2 ENGINE FUEL PUMP AND HMU PER MM 73-21-10-4 AND 73-11-01-4. LEAK AND OPS CHECK GOOD PER MM 71-00-00. NO FAULSDR TSAA0436053Precooler · failedCLIMBING THROUGH 15,000 FT THE BLEED TRIP OFF LIGHT FOR THE NR 2 ENGINE ILLUMINATED. PERFORMED QRH CHECKLIST, RETURNED TO KWA. OVER-WEIGHT LANDING AT 131.2 K, LOW TO MEDIUM SINK RATE. VERIFIED NR 2 ENGINE BLEED TRIP ON THE GROUND. REMOVED AND REPLACED PRE-COOSDR TSAA0436052Precooler · failedETOPS FLIGHT 352, CLIMBING THROUGH 15,000 FT THE BLEED TRIP OFF LIGHT FOR THE NR 2 ENGINE ILLUMINATED. PERFORMED QRH CHECKLIST, RETURNED. OVER-WEIGHT LANDING AT 131.2 K, LOW TO MEDIUM SINK RATE. VERIFIED NR 2 ENGINE BLEED TRIP ON THE GROUND. REMOVED AND REPLASDR TSAA0436048Sensor · failedTHE NR 2 ENGINE BLEED TRIPPED IN FLIGHT, DIVERTED TO HNL. PERFORMED ENGINE GROUND RUN-UP TO VERIFY BLEED TRIP AND OPS CHECK, RUN-UP OK. REMOVED AND REPLACED THE NR 2 ENGINE BLEED AIR REGULATOR FOR TROUBLESHOOTING IAW AMM 36-11-03-4, LEAK AND OPS CHECK OK. RSDR TSAA0436050Bleed Valve · failedTHE NUMBER TWO ENGINE BLEED TRIPPED IN FLIGHT, DIVERTED TO HNL. PERFORMED ENGINE GROUND RUN-UP TO VERIFY BLEED TRIP AND OPS CHECK, RUN-UP OK. REMOVED AND REPLACED THE NR 2 ENGINE BLEED AIR REGULATOR FOR TROUBLESHOOTING IAW AMM 36-11-03-4, LEAK AND OPS CHECK SDR TSAA0321195Sensor · dirtyDURING CRUISE, EQUIPMENT FAIL LIGHT ILLUMINATED, EQUIPMENT COOLING EXHAUST FAN INOPERATIVE IN NORMAL AND ALTERNATE POSITION. RETURNED TO SNA. DEFERRED EQUIPMENT COOLING FAN IAW MEL 21-27-3, AIRCRAFT RETURNED TO SERVICE. CLEANED EQUIPMENT COOLING EXHAUST FAN