JASC 7314
Service difficulty reports · 1,734
Reports filed under 7314 · Engine Fuel Pump, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '7314' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '7314' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA200903251036Pump · failedNR 3 ENG FLAME OUT DURING DESCENT, 280KTS/13000. PERFORMED LEVEL 3 ENG RPM LOW CHECKLIST, FOLLOWED BY ENG RESTART IN FLIGHT CHECKLIST, GOOD RESTART 10000/270 KTS. CKD ALL DEU AND FADEC NO FAULT SHOWN, INSP INLET & EXHUAST, CORE AREA NO DEFECT NOTED, R & R SDR DL76G090380Pump · malfunctionedAT FL340 DURING A CROSS FEED OPS TO CORRECT MINOR FUEL IMBALANCE THE LEFT ENG ROLLED BACK TO 52 PERCENT N1. LEFT MAIN BOOST PUMP WERE TURNED BACK ON AND X-FEED VLV CLOSED. ACFT RETRIMMED AND A/T ARM SW TURNED OFF. INITIALLY ENG WAS UNRESPONSIVE TO CHANGES ISDR G1IA2009622Pump · inoperativeDEPARTING BFI EXPERIENCE A UNCONTROLLED SHUT DOWN ON THE RIGHT ENGINE. THIS HAPPENED ON CLIMBOUT AT APPROXIMATELY 2000 FEET. THE FLIGHT CREW WITH MEDICS (NO PATIENT) RETURNED TO BFI WITHOUT FURTHER INCIDENT. GALVIN FLYING SERVICE WAS CONTACTED TO TROUBLESHOSDR ASAA0954598Pump · leakingDURING IDLE ENGINE RUN DISCOVERED NR 1 ENGINE LEAKING FUEL FROM FUEL PUMP PAD DRAIN AT A RATE OF 63 DROPS PER MINUTE. REPLACED THE NR 1 ENGINE FUEL PUMP PER MM 73 11 01. ALL LEAK AND OPS CHECKS ARE GOOD.SDR DL777090319Pump · intermittentON PUSH BACK CENTER FUEL PUMP L EICAS MSG CAME ON. MX MSG 28-11002.28-11030 T/S PER FIM 28-22-00-810-838 BOTH MSG INTERMITTENT FAULT.SDR CA090127003Pump · failedAME NOTICED FUEL IN THE DRAIN CAN ON A DAILY CHECK. DURING A SUBSEQUENT GROUND RUN HE FEELS THAT THE ENGINE PERFORMANCE FROM LOW TO HIGH IDLE IS NOT AS FAST AS IT SHOULD BE. THE AIRCRAFT IS GROUNDED AND A REPLACEMENT PUMP ASSY AND SUPPORT PARTS HAVE BEEN DISSDR HALA2009011900029Pump · malfunctionedETOPS SIGNIFICANT SYSTEM, BTB, LEFT ENG NO START ON IGNITION NR 1 OR NR 2 OR BOTH ENG VALVE-FUEL ANNUNCIATOR STAYED ON 15 SECONDS AND FUEL FLOW WAS LOWER THAN NORMAL. REPLACED LT ENGINE FUEL PUMP PER MM TASK 73-11-01 LEAK AND OP CK NML ON NR 1 ENGINE START.SDR CA090302002Pump · failed(CAN) INSTALLED OVERHAULED FUEL PUMP ON ACFT 30/01/08, PUMP FAILED 16/01/09.SDR COMA2009010750058Pump · failedON APPROACH, NR 2 ENGINE ROLLED BACK TO SHUTDOWN WHILE BEING VECTORED FOR THE APPROACH. EMERGENCY DECLARED, ACFT LANDED SAFELY. REMOVED AND REPLACED RT ENG FUEL PUMP.SDR FFKA20081217001Pump · inoperativeABOUT 40 OR SO MILES FROM AIRPORT, THE ENGINE DRIVEN FUEL PUMP DIED. WHEN THE FUEL PRESSURE STARTED DROPPING THE PILOT WENT THROUGH THE "HAIL MARY" MANEUVER (SWITCH TANKS, MIXTURE RICH, CHECK THE MAGNETOS, ELECTRICAL FUEL PUMP ON). AS SOON AS HE HIT THE ELECSDR 2008FA0000893Pump · leakingLT ENG FUEL PUMP DEVELOPED LEAK THROUGH THE BLEED HOLE IN A PLUG INSTALLED ON THE PRESSURE ADJUSTMENT PORTION OF THE PUMP. SYS WAS PRESSURIZED BY THE ELECTRIC FUEL PRESSURE BOOST PUMP AND A LEAK WAS DETERMINED TO BE APPROX (1) DROP PER SECOND AT A PRESSURE OFSDR 2008FA0000894Pump · shearedON SECOND TEST FLIGHT AFTER FACTORY REBUILT ENG INSTALLATION, ENG QUIT DURING TAKEOFF, JUST AFTER LIFTOFF, ALTITUDE LESS THAN 5 FT AGL. PILOT LANDED ACFT AND ROLLED OUT WITHOUT FURTHER INCIDENT. DURING THIS EVENT, PILOT REPORTED THAT AT TAKEOFF INITIATION, POWSDR UALA2008120306741Pump · leakingNR 1 ENG FUEL PUMP LEAKING AT INLET TUBE FLANGE. ACCOMPLISHED NR 1 ENG FUEL PUMP REPLACEMENT. NOW HAVE A FUEL LEAK FROM THE DRIVE FLANGE WILL NEED TO PULL PUMP AND RESEAL. REPLACED O-RING SEAL. RUN CHECKS OKAY.SDR DL764081684Pump · failedRTB - TAXI OUT LT FWD FUEL PUMP FAILED. RETURNED FOR ADDITIONAL FUEL.SDR CA090225014Shaft · shearedPILOT REPORT ENGINE FUEL PUMP ON APPROACH AND VACUUM PUMP FAILURE. FUEL PUMP AND VACUUM PUMP FOUND BOTH WITH SHAFT BROKEN. BOTH REPLACED, ENGINE DIDN`T START. ENGINE REMOVED AND SENT FOR REPAIR. REPORT FROM REPAIR SHOP RECEIVED WITH INDICATION OF METAL CONSDR Q2SA753004Pump · defectiveON CLIMB-OUT FROM EBLG (LIEGE, BELGIUM), NR 2 ENGINE FILTER BYPASS LIGHT ILLUMINATED, THEN WENT OUT. APPROXIMATELY 3 MINUTES LATER, NR 2 ENGINE FLAME OUT OCCURRED. IN FLIGHT ENGINE START COMPLETED. 3 HOURS, 20 MINUTES LATER AT FL350, FILTER BYPASS LIGHT ILLSDR PNSA110804Pump · failedAFTER TAKEOFF PILOT SHUT THE FUEL BOOST PUMP (ELECTRIC) AND NOTICED AN IMMEDIATE FUEL FLOW REDUCTION, AND ENGINE BEGAN TO SHUT DOWN. PILOT TURNED BOOST PUMP BACK ON AND POWER WAS RESTORED FULLY. PILOT MADE A UNEVENTFUL LANDING AT THE DEPARTURE AIRPORT. MAINSDR 2008FA0000746Pump · malfunctionedCRUISE NR 1 ENG STARTED TO SPOOL DOWN OTHER PARAMETERS ARE NORMAL, PERFORMED IN-FLIGHT START CHECKLIST SEVERAL TIMES INCLUDING RESETTING SWITCHES, NO LIGHT OFF. ACFT DIVERTED AND THE CREW PERFORMED ENG INSPECTION AND START ON NR 1 ENG HIGH IGNITION SYS, ENGINESDR 2008FA0000688Pump · crackedPUMP HOUSING CRACKED ALONG SEAM. POSSIBLE WEAK SPOT UPON MANUFACTURING. (K)SDR CA080829004Pump · leaking(CAN) THE FUEL WAS FOUND DURING REGULAR INSP LEAKING, FUEL PUMP WAS REPLACED WITH SIMILAR ONE. THE PROBLEM DIDN’T AFFECT THE ENG PERFORMANCE. FUEL TRACE WAS LOCATED BETWEEN BODY STAGE OF THE PUMP. THIS IS THE FIRST PROBLEM OF LEAK WITH THIS TYPE.SDR 2008FA0000663Pump · wornAFTER TAKEOFF THE PILOT COULD NOT ADJUST THE LT ENGINE POWER OUTPUT. ENGINE REMAINED AT TAKEOFF POWER WHILE POWER LEVER WAS RETARDED TO IDLE. PILOT RETURNED TO AIRPORT AND SUCCESSFULLY SHUTDOWN THE LT ENGINE BY PLACING POWER LEVER TO CUT-OFF POSITION AND MADESDR EXD2008F00000Pump · failedTHE FLIGHT CREW REPORTED APPROXIMATELY (1) HOUR INTO THE FLIGHT, THE LT ENGINE SHUT DOWN WITH NO WARNING OR PRIOR INDICATION OF A PROBLEM. THE TREND MONITORING WAS COMPLETED PRIOR TO THE ENGINE PARAMETERS WERE NORMAL. THE FLIGHT CREW PROMPTLY NOTIFIED ATC AND SDR CA080910006Pump · malfunctioned(CAN) FUEL PUMP ELECTRICALLY MALFUNCTIONING, REPLACED FUEL PUMP.SDR 08FDEA03522Pump · malfunctionedAT FL 350 IN STEADY CRUISE FLT, FELT SLIGHT VIBRATION FOLLOWED BY NR 1 EPR ROLL BACK, NR 1 N1,N2 EGT ROLLBACK. N1 STABILIZED AT 26 PERCENT, EGT 180 DEG NR 1 GEN BREAKER LIGHT ON AND NR 1 LOW OIL PRESSURE LIGHT ON. THRUST LEVEL BOUGHT TO IDLE AND DESCENT STARSDR CA080815005Spline · worn(CAN) DURING SKYDIVING OPS, SHORTLY AFTER TAKE-OFF ACFT CRASHED UNDER UNKNOWN CIRCUMSTANCES. IT WAS REPORTED THAT PILOT WAS ATTEMPTING TO RETURN TO THE POINT OF DEPARTURE WHEN THE ACCIDENT OCCURRED. PRELIMINARY ASSESSMENT OF ENGINES REVEALED LT ENGINE WITH SEVSDR RAIA00808001Pump · malfunctionedFLT 5570-CLT - CREW REPORTED AN ENG NR 2 LOSS OF POWER IN FLIGHT ON INITIAL CLIMBOUT AND RECEIVED AN E2 NO DISPATCH MESSAGE ON LANDING. MAINTENANCE REMOVED AND REPLACED THE NR 2 FPMU AND PERFORMED AN OPERATIONAL CHECK OF THE ENG WITH NO OTHER DEFECTS NOTED. SDR 2008FA0000531Seal · leakingFUEL PUMP DRIVE SHAFT SEAL FAILED RESULTING IN LARGE FUEL LEAK AT DRAIN. (K)SDR CA080722004Seal · leaking(CAN) ON DAILY INSP, FUEL WAS DISCOVERED IN THE OIL SEAL DRAIN COLLECTOR CAN. FURTHER INVESTIGATION FOUND FUEL LEAKING FROM THE SEAL ON THE FUEL HIGH PRESSURE PUMP. THERE WAS NO INDICATION OF GREASE WASH OUT OF THE FCU BRG. THE FUEL PUMP WAS REPLACED WITH A SESDR JLT2008F00000Pump · failedON THE EVENING OF FRIDAY, JULY 18TH, ON CLIMB, EN ROUTE, THE CREW OBSERVED THE LT ENGINE, SN 91535, FUEL LIGHT ILLUMINATED. THE CREW REDUCED POWER. ENGINE THEN EXPERIENCED AN UNCOMMANDED INFLIGHT SHUTDOWN. CREW SECURED THE ENGINE AND ATTEMPTED A RESTART. RESSDR CA080718005Pump · leaking(CAN) AFTER REPLACING THE ENGINE, A LEAK CHECK WAS COMPLETED AND IT WAS FOUND THAT THE LP FUEL PUMP WAS LOOSING FUEL OUT THE VENT LINE. THE PUMP WAS REPLACED WITH NO FURTHER PROBLEMS.SDR MT92008F00002Pump · failedDURING AN OPERATIONAL INSPECTION, THE FUEL PUMP WAS REJECTED IAW SB1645. A REPLACEMENT PUMP WAS INSTALLED (TSO 0.0) AND ON THE OPERATIONAL RUN CHECKS THE FUEL PRESSURE LOW LIGHT AND THE FUEL PUMP ON LIGHT ON THE ANNUNCIATOR PANEL STARTED CYCLING WHEN THE TORQSDR CA080708006Pump · leaking(CAN) DURING A GROUND RUN OF THE ACFT THE ENGINE FUEL PUMP WAS LEAKING.SDR CA080626001Pump · leaking(CAN) OIL LEAK NOTICED PRIOR TO ANNUAL INSP. OIL WAS LEAKING OUT THE VENT LINE FROM THE FUEL PUMP. REMOVED PUMP, REMOVED FUEL VENT FITTING, FOUND VENT CHAMBER FULL OF ENGINE OIL. REPLACED WITH NEW PUMP.SDR A8O2008F00000Pump · failedEMERGENCY ACTION TAKEN DURING FLIGHT DUE TO A COMPONENT OR SYSTEM MALFUNCTION. AFTER DUAL ENGINE REPLACEMENT DUE TO MPI, ON TEST FLIGHT, CREW DISCOVERED DUAL FUEL OVERTEMP ANNUNCIATOR LIGHTS CAME ON. CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WHERE SDR CA080618008Pump · inoperative(CAN) WHEN POWER WAS APPLIED THE PUMP WOULD OPERATE UNLESS IT WAS TAPPED WITH A HAMMER. PUMP WAS REPLACED AND NO FURTHER ISSUES WERE NOTED. WILL SUPPLY HOURS ON THE PUMP IN THE NEXT FEW DAYS.SDR UPS08852422Pump · malfunctionedINSPECTION TYPE:N/A AT FLT F/L 36.0 WITH BOOST OFF NR 2 ENGINE FLAMED OUT WHEN THROTTLE WAS MOVED TO IDLE. THIS WAS DURING A CONDITION FLT WITH A NEW PROCEDURE THAT THE FLT CREWS ARE FOLLOWING. A/C WAS NOT IN NORMAL FLT CONDITION WHEN THE FLAME OUT OCCURRED.SDR CA080603005Pump · malfunctioned(CAN) REINFORCED PAPER WIPERS LEFT IN THE FUEL TANK AFTER WORK CARRIED OUT. DURING A 300 HOUR INSP, THERE WAS SIGNIFICANT FUZZ LIKE DEBRIS FOUND IN THE ENGINE DRIVEN FUEL PUMP FILTER THAT WAS A BLUISH COLOR. WHEN PICKING UP THE HELICOPTER AT THE SERVICE CTRSDR UPS08M52170Pump · failedINSPECTION TYPE:N/A THE NR 1 ENGINE FLAMED OUT ON DESCENT. ATTEMPTED TO RESTART ENGINE TWICE, UNSUCCESSFUL. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED FUEL PUMP ON NR 1 ENG. PERFORMED LEAK CHECK AND ENG TEST PER AMM 73-12-SDR CA080702009Drive Shaft · distressed(CAN) ACCORDING TO REPORTS, CREW DECLARED AN EMERGENCY DUE TO ENGINE DISTRESS. DURING SUBSEQUENT LANDING, A/C EXITED THE RUNWAY BEFORE HITTING A DITCH. THE LANDING GEAR COLLAPSED AND THE NOSE OF THE A/C WAS SEVERELY DAMAGED. THE RUNWAY EXCURSION WAS CAUSED BY SDR USAABB08070Pump · malfunctionedHNL FLT 47 EN ROUTE LIH TO PHX. AIRCRAFT DISPLAYED EICAS MESSAGE "L ENG LP PUMP". THE CREW DECIDED TO DIVERT BACK TO HNL. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE LP PUMP.SDR BB08070Warning System · activatedHNL FLT 47 - EN ROUTE LIH TO PHX. AIRCRAFT DISPLAYED EICAS MESSAGE "L ENG LP PUMP". THE CREW DECIDED TO DIVERT BACK TO HNL. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. (OPEN)SDR CA080410004Pump · leaking(CAN) DURING A DAILY INSP OIL WAS FOUND LEAKING FROM THE ENGINE DRIVEN FUEL PUMP, PART WAS REMOVED AND REPLACED (TC NR 20080410004)SDR CA080331004Pump · noisy(CAN) AUX FUEL PUMP HAD EXCESSIVE NOISE THE PUMP WAS REPLACED. (TC NR 20080331004)SDR BB08036Pump · failedHNL FLT 26 - EN-ROUTE OGG TO PHX, ON CLIMB-OUT FROM OGG, RECEIVED EICAS MESSAGE "R ENG LP PUMP". FLIGHT DIVERTED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE CHECKED WIRING FROM D321 E, J3 AND D319 E, J3 TO SWITCH S10134. NO FAULTS WERE FOUND. CHECKED ESDR CA080221012Pump · leaking(CAN) DURING THE PREFLIGHT CHECK THE ENGINE DRIVEN FUEL PUMP FOUND LEAKING OIL. (TC NR 20080221012)SDR CA080215008Pump · erratic(CAN) RT ENGINE DRIVEN FUEL PUMP REPLACED DUE TO ERATIC PRESSURE INDICATIONS. (TC NR 20080215008)SDR SWAA080469Pump · failedNR 1 ENGINE FAILED DURING TAXI. REMOVED AND REPLACED FUEL PUMP AND HMU PER MM.SDR 183801212008Solenoid · leakingAT APPROX 01:30 MDT, MEDFLIGHT 2 WAS ATTEMPTING TO DEPART SCENE WITH PATIENT. PILOT DETECTED ODOR OF SMOKE IN THE COCKPIT AND ABORTED TAKEOFF. PILOT SECURED ENGINE AND ADVISED GROUND PERSONS THAT HE WAS UNABLE TO TRANSPORT PATIENT VIA HELICOPTER. PATIENT WASSDR CALS097002Pump · contaminatedRTO AT SGN DUE TO ENG-3 CONT MSG COME ON DURING T/O ROLL, THE DETAILED DESCRIPTION AS FOLLOWS: 1) DUE TO ENG-3 SVA ACTUATOR FAILURE TO CAUSE N2 OVERSPEED AND ENG-3 CONT MSG DURING A/C TAKE OFF ROLLING. 2) EEC FAULT MSG: ENG-3 SVA FAIL, ENG-3 OVERSPEED GOVERNORSDR CA080119001Pump · leaking(CAN) FUEL PUMP LEAKING OIL FROM DRAIN LINE. PUMP REMOVED AND NEW PUMP INSTALLED. DEFECT RECTIFIED. (TC NR 20080119001)
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