JASC 7314
Service difficulty reports · 1,735
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 AU001037O-Ring · damaged(AUS) ENGINE DRIVEN FUEL PUMP O-G SEAL DAMAGED. A PORTION OF THE SEAL BLOCKED THE METERING ORIFICE AT THE FCU ALLOWING THROUGH ONLY ENOUGH FUEL FOR IDLE POWER. SUSPECT SEAL DAMAGED DURING PUMP ASSEMBLY AT OVERHAUL. (X)SDR SWIA972047Pump · failedAFTER TAKEOFF, RIGHT ENGINE SURGING. TORQUE FLUCTUATION 10 - 15 PERCENT, NH FLUCTUATION. RETURNED TO SLC. REMOVED AND REPLACED THE HMU AND THE FUEL PUMP ON THE RIGHT ENGINE IAW EMB MM 73-21-00 AND RII 13-301. P/N ON: PUMP 3040627 HMU 786390-10, S/N ON: PUMSDR CA001110003Pump · failed(CAN) FUEL PUMP FAILED. (X)SDR 20001101SH022Pump · brokenLEFT ENGINE FLAMED OUT IN-FLIGHT, RESTART PROCEDURES TRIED, BUT ENGINE WOULD NOT START. EMERGENCY DECLARED, AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHOOTING FOUND DRIVESHAFT FOR HIGH PRESSURE FUEL PUMP BROKEN. ENGINE OIL FILTER CHECKED FOR METAL CONTAMINATSDR USAABB00104Pump · malfunctionedPIT - FLT 115 - ON APPROACH TO PIT, THE CREW RECEIVED THE EICAS MESSAGE RT ENG LP PUMP AND THE RIGHT ENGINE SHUT DOWN. CREW WAS ABLE TO RESTART THE ENGINE AND LANDED AT PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FUEL FLOW GOVERNOR AND THE FUEL PUMSDR CA001103015Shaft · sheared(CAN) NR 1 ENGINE QUIT AS POWER WAS APPLIED FOR THE TAKEOFF ROLL. FOUND THE FUEL PUMP SHAFT SHEARED. FUEL PUMP AND FUEL CONTROL UNIT WERE REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE.2000-11-07 TC:REFERENCE AIRWORTHINESS DIRECTIVE 2000-22-06,& ASB A6381.SDR CA001024031Filter · failed(CAN) CREW REPORTED A RT FUEL TO PRESSURE CAUTION MESSAGE IN DESCENT. MESSAGE WENT AWAY WHEN THE THRUST LEVERS WERE PUSHED FORWARD.MAINTENANCE REPLACEDTHE RT ENGINE FUEL FILTER ELEMENT AND RT ENGINE FUEL LO PRESS SWITCH. AIRCRAFT BACK IN SERVICE.SDR 20010305CW008Pump · leakingWITH HIGHWING TANK CONNECTED TO THE FUEL PUMP INLET PORT, THE NONE DRIVEN FUEL PUMP LEAKS REGARDLESS THE MIXTURE LEVER POSITION. WITH THE MIXTURE LEVER IN IDLE CUT OFF, THE FUEL FLOW IS THE SAME AS IN FULL RICH. 3 TO 4MM/0.012IN TO 0.016IN/ AWAY FROM THE IDLSDR AU001008Pump · contaminated(AUS) ENGINE DRIVEN FUEL PUMP VAPOR SEPARATOR CHAMBER CONTAINED A SMALL PIECE OF UNIDENTIFIABLE CONTAMINANT. REF: OPER CNTRL NR AU001005 FOR SUSPECTED ORIGIN OF CONTAMINATION. (X)SDR 0003652299Pump · failedDURING TAKEOFF JUST PRIOR TO V1 SPEED, THE NR 1 ENGINE CEASED OPERATING. THE ENGINE FAIL INDICAITON AND THE AUTO PACK TRIP INDICATION LIGHTS ILLUMINATED. TAKEOFF WAS ABORTED AT 130 KNOTS WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL PUMP AND FUEL CONTROL SDR 20001016SH003Pump · leakingAT 80 HRS TT, FWD SEAL VENT LINE STARTED DISCHARGING SMALL AMTS OF OIL IRREG. OIL ON OUTSIDE OF LT COWL SUSPECTED TO BE RESIDUAL OIL VENTING FROM HEAT. NO BLUE FUEL STAINS EVIDENT. THERE WAS A LOW PRESSURE WHEN PRIMING WITH BOOST PUMP, NOT OUT OF NORMAL RANSDR CA001020017Pump · failed(CAN) RECURRING PROBLEM. AIRCRAFT HAS FLOWN 48.7 HOURS SINCE LAST OCCURRENCE AND REPAIRS. THIS TIME FOLLOWS REPLACEMENT OF IN-LINE ELECTRIC FUEL BOOST PUMP 481-802, AFTER FAILURE. FUEL SERVO SCREEN CHECKED, NOZZLES REMOVED, FLUSHED LINES SERVO TO NOZZLES. SDR 20001031SH016Pump · failedINTERNAL FAILURE, PUMP STOPPED BEFORE TAKEOFF. (X)SDR RAIA0009046Pump · failed6881-DCA- LEFT ENGINE FAILED AT APPROXIMATELY 1000 FEET AFTER TAKEOFF. RETURNED TO DCA. MAINTENANCE INSPECTED AND REPLACED LEFT ENGINE FUEL PUMP.SDR CA000925021Pump · leaking(CAN) DURING LEAK CHECK AFTER INSTALLATION, A LEAK WAS DISCOVERED AT THE FUEL PUMP TO MFC MATING SURFACE. THE MS9967-016 O-RINGS WERE REPLACED, BUT THE LEAK PERSISTED. CLOSER INVESTIGATION OF THE PUMP MATING SURFACE REVEALED THAT THE O-RING CUTOUTS AT THE OUTLSDR 20001019SH001Pump · defectiveUNABLE TO ADJUST FUEL FLOW TOP END AND IDLE MIXTURE. (X)SDR AU000903Drive Shaft · sheared(AUS) ENGINE DRIVEN FUEL PUMP INPUT DRIVE SHAFT SHEARED. (X)SDR EIA2000044Pump · inoperativeKSEA - FLT U823 - WITH RIGHT ENGINE THRUST LEVER AT FORWARD MECHANICAL STOP, EPR=1.80+- .04. RT N1 RPM INITIALLY AT 100 PERCENT, THEN DROPPED TO 94 PERCENT WHILE THRUST LEVER STILL AT STOP. POWER REDUCED FOR REJECTED TAKEOFF. REPLACED FUEL PUMP PER 73-11-1.SDR 20000913SH026Pump · mismanufacturedACFT WAS UNDERGOING WING REPAIRS FOLLOWING FUEL TANK CONTAMINATION. POST-FUEL SYSTEM CHECKS CARRIED OUT AND 3 FUEL PUMP CANNISTERS WERE FOUND TO HAVE BLOWN SEALING SLEEVE COVER SEALS. THE CANNISTERS WERE REMOVED AND SENT FOR REPAIR INSPECTION. ON RETURN, CASDR 20000913SH025Pump · mismanufacturedACFT WAS UNDERGOING WING REPAIRS FOLLOWING FUEL TANK CONTAMINATION. POST-FUEL SYSTEM CHECKS CARRIED OUT AND 3 FUEL PUMP CANNISTERS WERE FOUND TO HAVE BLOWN SEALING SLEEVE COVER SEALS. THE CANNISTERS WERE REMOVED AND SENT FOR REPAIR INSPECTION. ON RETURN, CASDR 20000913SH024Pump · mismanufacturedACFT WAS UNDERGOING WING REPAIRS FOLLOWING FUEL TANK CONTAMINATION. POST-FUEL SYSTEM CHECKS CARRIED OUT AND 3 FUEL PUMP CANNISTERS WERE FOUND TO HAVE BLOWN SEALING SLEEVE COVER SEALS. THE CANNISTERS WERE REMOVED AND SENT FOR REPAIR INSPECTION. ON RETURN, CASDR 20000913SH023Pump · mismanufacturedACFT WAS UNDERGOING WING REPAIRS FOLLOWING FUEL TANK CONTAMINATION. POST-FUEL SYSTEM CHECKS CARRIED OUT AND 3 FUEL PUMP CANNISTERS WERE FOUND TO HAVE BLOWN SEALING SLEEVE COVER SEALS. THE CANNISTERS WERE REMOVED AND SENT FOR REPAIR INSPECTION. ON RETURN, CASDR 20000912SH025Pump · failedWITH TOP END FUEL PRESSURE SET IAW SPEC, AT IDLE, THE PUMP PRESSURE DROPS TO LOW. LESS THAN 25 PSI TO OPERATE FUEL SERVO AT IDLE. (X)SDR 2000UALA00500Pump · malfunctionedWITH 1.1 FUEL IN CENTER TANK, WING GAUGES DISAGREE BY 2000 LBS. AFTER CENTER TANK EMPTY, 2000 LBS IMBALANCE REMAINED. FUEL USED SHOWED .3 DIFF, A-C REMAINED IN TRIM. X-FEED FUEL LEFT TO RIGHT WITH A-P DISCONNECTED A-C ROLLED TO RIGHT. *S/D* IMBALANCE WAS SDR 20010305CW010Pump · leakingFUEL PUMP LEAKS THROUGH OUTLET PORT, WITH FUEL SELECTOR VALVE IN ON POSITION, WITH HIGHWING TANK CONNECTED TO FUEL PUMP INLET PORT, THE NONE DRIVEN FUEL PUMP LEAKS REGARDLESS THE MIXTURE LEVER POSITION. WITH MIXTURE LEVER IN IDLE CUT OFF, THE FUEL FLOW IS THESDR DLM11001558Connector · damagedAIRCRAFT ARRIVED WITH MCO NR 007341002 TAIL LEFT PUMP OFF LIGHT ILLUMINATED IN FLIGHT (TRANSFER PUMP. FOUND RECEPTACLE IN PUMP HOUSING WITH BURNED PINS AND WIRING. THE RECEPTACLE SMELLED OF FUEL BUT NO EVIDENCE OF A FUEL LEAK WAS NOTED. REPLACED HOUSING P/NSDR CA000905014Pump · failed(CAN) WHILE IN 4 FT HOVER, AN ENGINE FLAMEOUT OCCURRED. UPON INVESTIGATION IT WAS DISCOVER THE THE ENGINE DRIVEN FUEL PUMP TO BE IN BY PASS. FUEL CONTROL AND FUEL PUMP REPLACED.SDR 2000UALA00468Pump · malfunctionedENGINE INDICATION PROBLEM. *S/D* REPLACED FUEL PUMP AND MAIN ENGINE CONTROL (MEC), PERFORMED ACCELERATION CHECK WITH ALL PARAMETERS NORMAL.SDR RIVA0000022Shaft · shearedTHE NR 3 ENGINE FAILED APPROXIMATELY 400 FEET ABOVE GROUND LEVEL. ON RETURN TO PIT, THE NR 1 TIRE BLEW. METAL WAS FOUND IN THE FUEL PUMP FILTER. THE FUEL PUMP AND FUEL CONTROL UNIT WERE REMOVED AND REPLACED. THE NR 1 AND NR 2 TIRES WERE REMOVED AND REPLACESDR 20000919SH021Pump · inoperativeIDLE PRESSURE WAS LOW AND UNABLE TO ADJUST HIGHER. (X)SDR 20000919SH020Pump · inoperativeIDLE PRESSURE WAS LOW AND UNABLE TO ADJUST HIGHER. (X)SDR 0002719998Shaft · shearedDURING DESCENT INTO MSP, THE RIGHT ENGINE EXPERIENCED A FLAME-OUT PRECEEDED BY AN OIL LOW PRESSURE LIGHT INIDICATION AND A RIGHT ENGINE GENERATOR OFF LIGHT INDICATION. THE FLIGHT CREW FOLLOWED THE EMERGENCY CARD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLASDR QXEA0002060Regulator · inoperativeSEA - ON CLIMBOUT OF SEA, CREW SELECTED CLIMB POWER FOR NR 2 ENGINE. NR 2 ENGINE WOULD NOT RETARD FROM TAKEOFF POWER SETTING. CREW SHUTDOWN NR 2 ENGINE AND RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE FUEL FLOW REGULATOR. PERFORMED ENGINSDR 20000919SH022Pump · inoperativeIDLE PRESSURE WAS LOW AND UNABLE TO ADJUST HIGHER. (X)SDR 20000912SH026Pump · failedIDLE PRESSURE WAS LOW AND UNABLE TO ADJUST HIGHER. PRESSURE WAS ALSO ERRATIC. (X)SDR CA000731013Pump · leaking(CAN) WHEN LEFT INNER FUEL PUMP WAS TURNED ON FOR APU TIME, NR 2 ENGINE BEGAN LEAKING FUEL. THE NR 2 PUMP WAS THEN TURNED OFF UNTIL REQUIRED FOR ENGINE START. NR 2 ENGINE FCU RIGGING CHECKED, NR 2 BOOST PUMP RUN FOR 15 MINS. NO FUEL LEAKAGE NOTED. FUNCTION CHSDR 20000804SH004Pump · brokenNR 2 ENGINE SHUT DOWN IN-FLIGHT. PILOT MADE NORMAL LANDING. INVESTIGATED PROBLEM. PULL FUEL PUMP OFF. FOUND INTERNAL SPLINES OF PUMP GROUND OFF. SPLINES MISSING DUE TO ABNORMAL WEAR ON SPLINES. INSTALLED NEW PUMP. GROUND RAN ENGINE. ENGINE FUNCTIONED PSDR 20000811SH012Pump · damagedPILOT REPORTED WHEN ELECTRIC FUEL WAS TURNED ON, THE ELECTRIC FUEL PUMP AND ALTERNATOR FIELD CIRCUIT BREAKERS TRIPPED. INSPECTED FUEL PUMP AND FOUND LEAD-IN WIRE TO ELECTRIC PUMP HAD PULLED OUT OF HOUSING AND WAS SHORTING TO GROUND. (X)SDR CA000801027Pump · shorted(CAN) THE ELECTRICAL WIRE WHERE IT ENTERS THE PUMP HAS SHORTED. THIS WIRE IS COVERED BY A BRAIDED WIRE. NO DISASSEMBLY HAS BEEN CARRIED OUT, HOWEVER, 24V WAS APPLIED TO PUMP TO CONFIRM SHORT. SUBMITTER STATED THIS IS THE SECOND PUMP REPLACEMENT ON THIS AIRCSDR 20000914SH010Pump · failed53 MINTUES AFTER TAKEOFF, AT A FLIGHT ALTITUDE 1,500 MSL, 5 MILES WEST OF EVERETT, WA, LEFT ENGINE QUIT. RESTARTED WITH AUXILIARY FUEL PUMP AND LANDED. REPLACED ENGINE DRIVEN PUMP WITH OVERHAULED PUMP FROM LYC. PUMP HAD BEEN NEWLY OVERHAULED. REPAIR STATIOSDR RAIA0007009Pump · failed7002-SGF- RIGHT ENGINE WOULD NOT ACHEIVE TARGET TORQUE. MAINTENANCE INSPECTED AND REPLACED RIGHT ENGINE FUEL PUMP.SDR CA000801010Pump · leaking(CAN) ON LANDING WHITEHORSE, YUKON. FLAME WAS SEEN COMING FROM RT ENGINE. DURING TAXI WITH HIGHER RPM NO FLAME WAS SEEN. THE TOWER AT WHITEHORSE FIRST NOTED THE FLAME AND ADVISED THE PILOT OF IT GOING OUT WHILE TAXIING. CAUSE OF FIRE WAS FUEL VENTING FROM FUESDR 20010305CW009Pump · leakingTESTED FUEL PUMP, MOTOR DRIVEN FUEL PUMP REACHED SPECIFIED CALIBRATING VALUES. WITH HIGHWING TANK CONNECTED TO THE FUEL PUMP INLET PORT, THE NONE DRIVEN FUEL PUMP LEAKS REGARDLESS THE MIXTURE LEVER POSITION THROUGH THE OUTLET PORT. WITH MIXTRUE LEVER IN IDLSDR CA000801028Pump · inoperative(CAN) BURNING ODOR WAS NOTICED FROM LT WING TIP AND LT LANDING LIGHT. CIRCUIT BREAKER TRIPPED. (TIP TRANSFER PUMP RECEIVES POWER FROM THIS BREAKER AND PUMP IS RUNNING WHENEVER MASTER SWITCH IS ON). PUMP WAS REMOVED AND APPROXIMATELY 1/2 OF THE PUMP BODY WASSDR CA000724009Pump · failed(CAN) DURING CLIMB OUT OF YYZ, NR 1 ENGINE EXPERIENCE A MOMENTARY LOST OF THRUST. ALL ENGINE PARAMETERS DROPPED AND THEN COME BACK. FUEL AMPLIFIER N1 AND N2 DATUM ADJUSTED, WIRING CHECKED FROM AMPLIFIER TO FUEL PUMP, FUEL PUMP REPLACED. AIRCRAFT RELEASE FOR FLSDR 20000801SH041Cartridge · inoperativeFUEL PUMP CARTRIDGE INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR C8GA200000004Pump · inoperativeFLT 216 KDAY-KHSV WITH ENG POWER SET AT REDUCED TAKEOFF POWER SETTING OF 2.0 EPR AND 95 PERCENT N1 NR 1 ENG WENT TO 2.4 EPR, RETARDED THROTTLE AND EPR QUICKLY DROPPED TO 1.8. TRIED TO RESET POWER AND NO EPR RESPONSE TO THROTTLE MOVEMENT OCCURRED. ABORTED TAKSDR 0002092708Pump · inoperativeDURING NORMAL CRUISE FLIGHT, THE NR 3 ENGINE EXPERIENCED A FLAME-OUT. THE FLIGHT CREW ATTEMPTED TO RESTART THE NR 3 ENGINE. BUT ENGINE WOULD NOT RESTART. ALL COM PROCEDURES WERE FOLLOWED. THE FLIGHT DIVERTED TO DEN AND LANDED WITHOUT INCIDENT. MAINTENANCESDR L1GA200000130Pump · failedACFT ABORTED TO NR 1 ENGINE POWER REDUCED TO 80 PERCENT N2 W/O THROTTLE INPUT. NR 1 ENGINE FUEL PUMP REPLACED.SDR CA000530018Pump · failed(CAN) LOW FUEL FLOW PRESSURE WARNING LIGHT AND INDICATION. FUEL PUMP REPLACED DUE TO DE-COUPLED SPLINE DRIVESHAFT.
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