Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 39LA20160914169Engine · flamed outUPON TAKEOFF, THE CREW REPORTED THAT THE NR 2 ENGINE SHUTDOWN. UPON LANDING, THE AIRCRAFT WAS SHUTDOWN WHILE THE PASSENGERS WERE EVACUATED. MAINTENANCE PERFORMED AN INSPECTION OF ALL FEED LINES IN THE AFT AND CENTER FUEL TANKS AND INSPECTED THE NR 2 AIRFRAMESDR 39LA20160906168Engine · flamed outWHILE 4.3 HOURS INTO A CONOP, THE CREW HAD JUST TAKEN OFF ENROUTE. WHILE TRANSITIONING TO FORWARD FLIGHT AT APPROXIMATELY 75 FT, THE CREW FELT THE ACFT YAW LT, HEARD A DECREASE IN ENGINE NOISE AND EXPERIENCED A LOSS OF AVAILABLE POWER. THE ACFT WAS STILL POSSDR 39LA20160825167Pump · leakingREPORTED A VERY INTENSE FUEL ODOR RETURNING DEPARTURE AT THE END OF AN 8 HOUR CONOP. DURING REFUELINGS THROUGHOUT THE DAY, OCCASIONAL DROPS OF FUEL WERE NOTICED AT THE NR 2 ENGINE GAIN DRAIN. THE NR 2 ENGINE DRAIN LINES FROM THE ENGINE PLATFORM TO THE ACFT FSDR 39LA20160817166Drain · pluggedDURING THE FIRST 3.6 HRS OF FLIGHT, 7 LEGS REPORTED, THE CREW DETECTED AN OVERWHELMING ODOR OF JET FUEL IN THE COCKPIT AND CABIN DURING CLIMBS AND DESCENTS. THE PILOT IN COMMAND EXPERIENCED A STRONG HEADACHE AND ONCOMING NAUSEA. THE SECOND IN COMMAND ALSO COSDR 39LA2014021257Generator · failedAFTER DEPARTURE FROM OASH THE DC GEN LIGHT ILLUMINATED. ACCOMPLISHED THE EMERGENCY PROCEDURES, GEN WOULD NOT RESET. R & R DC GEN PN 30E20-97A IAW S61 MM 4045-80, REV 47, 24-20-01.SDR 39LA2013012500003Access Panel · looseDURING CLIMB OUT, CREW CHIEF HEARD A CLAPPING NOISE FROM OUTSIDE THE ACFT. SUSPECTED THAT A PANEL WAS LOOSE AND SLAPPING AGAINST THE ACFT. SLOWED THE ACFT DOWN TILL THE NOISE STOPPED AND CONTINUED LANDING AT OUR NEXT STOP. AFTER LANDING CREW CHIEF DID A VISSDR P4YA0707201200001Engine · failedON APPROACH NR 2 ENGINE COMPRESSOR STALLED AND T SPIKED TO 950°C. REMOVED AND REPLACED ENGINE, ALL SYSTEMS CHECKED SATISFACTORY.SDR 3PRA2011110700001Landing Gear · lockedACFT FUNCTIONAL CHECK FLIGHT WAS BEING CONDUCTED, FLIGHT QUALITIES WERE ALL NORMAL UP UNTIL SUCH TIME AS THE ACFT LANDING WAS ATTEMPTED. WHEN ACFT TOUCHED DOWN AND POWER WAS BEING REDUCED, THE ACFT ENCOUNTERED SEVERE SHUDDER ON THE VERGE OF GROUND RESONANCE. SDR P4YA2010071500001Mount · crackedLT FWD TRANSMISSION MOUNT FITTING WAS FOUND TO BE CRACKED 2" AT STA 243. AREA WAS PREVIOUSLY REPAIRED AND DOUBLERS WERE REMOVED FOR INSPECTION. REPAIR IS IN PROGRESS AT THIS TIME.