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 SWAA053456Pump · leakingNR 1 ENGINE FUEL PUMP LEAKING. REMOVED AND REPLACED FUEL PUMP PER MM.SDR CA060228020Pump · failedDURING START UP PILOT COULD NOT PRIME AIRCRAFT. FURTHER INVESTIGATION FOUND PUMP HAD FAILED. PUMP REPLACED AND NO FURTHER DEFECTS WERE NOTED.SDR COE2006F00001Coupling · looseWHEN INSPECTING FUEL PUMP IAW CAB 05-18 AND PWC1645 FOR REDDISH-BROWN STAIN ON COUPLING SHAFT AREA. FOUND NO VISIBLE SIGN. COUPLING WAS LOOSE ON SHAFT WHEN COUPLING WAS REMOVED. FOUND SPLINES WORN ON FUEL PUMP AND COUPLING. THE SB MUST SUPPLY A MEANS TO RESDR ACE101005Pump · leakingNR 2 ENGINE LEAKING FUEL FROM NACELLE. MAINTENANCE REPLACED LOW PSI FUEL PUMP DUE EXTRUDED VALVE BODY GASKET. FUEL WAS NOT DUMPED OVERBOARD AS THE VALVE BODY WAS LEAKING EXTERNALLY.SDR CA051011011Shaft · shearedAIRCRAFT SUFFERED A NR 2 EDP FAILURE DURING APPROACH. ON INVESTIGATION, THE QUILL DRIVE WAS FOUND SHEARED AND THE CASE DRAIN DPI HAD ACTIVATED, THE FILTER WAS FULL OF BRASS. NR 2 EDP REPLACED.SDR CA051104001Spline · damaged(CAN) DURING CRUISE THE ENGINE WAS REPORTED TO HAVE LOST POWER AND THE CREW SHUTDOWN THE ENGINE IN FLIGHT. SUBSEQUENT INSPECTION REVEALED A DAMAGED FUEL PUMP DRIVE SPLINE.SDR CA051011006Drive Assy · shearedIN CRUISE FLT AT 7000 FEET, NR 1 ENGINE LOST POWER. FLT CREW SECURED NR 1 ENGINE IAW APPLICABLE FLT MANUAL PROCEDURES AND LANDED A/C AT NEAREST AIRPORT. UPON INVESTIGATION, MX FOUND THAT CAUSE OF ENG FAILURE WAS DUE TO ENG DRIVEN FUEL PUMP. WHEN FUEL PUMP WSDR CA051004003Pump · leaking(CAN) ENGINE DRIVEN FUEL PUMP REPLACED BECAUSE OF OIL LEAK. SB548A HAD BEEN COMPLIED WITH.SDR QXEA200501264Pump · malfunctionedSEA FLIGHT NR 2176 - AFTER PUSHBACK, POWER LEVERS MOVED TO FLIGHT IDLE, PROP LEVERS MOVED TO MAX TORQUE ON NR 2 ENGINE INDICATED 62 PERCENT AND WARNING HORN SOUNDED. THE TORQUE INDICAITON OCCURED AS THE PROPS WERE COMING OUT OF FEATHER. SECONDS LATER, TORQUESDR SWAA052838Seal · tornAIR TURNBACK, INFLIGHT SHUTDOWN, DECLARED EMERGENCY. NR 2 ENGINE FLAMED OUT. FOUND TORN FUEL PUMP SEAL CAUSING FUEL LEAK. REMOVED AND REPLACED SEAL PER MM.SDR 0501385506Pump · failedDURING CRUISE FLIGHT ENGINE NR 1 FLAMED OUT. FLIGHT CREW DIVERTED TO OMA PERFORMING AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED ENGINE NR 1 FUEL CONTROL AND FUEL PUMP.SDR QXEA200501215Pump · malfunctionedSEA FLIGHT 2078 ON CLIMBOUT NR 1 ENGINE FUEL PRESSURE CAUTION LIGHT ACCOMPANIED BY FALLING TORQUE AND FLUCTUATING AND FALLING FUEL FLOW. ACCOMPLISHED NR 1 ENGINE FUEL PRESSURE CAUTION CHECKLIST. UPON SELECTING NR 1 AUX PUMP ON, NOTED A MOMENTARY JUMP IN TORQSDR DL76S050470Pump · leakingFUEL IMBALANCE OF 3500LBS, DIVERTED TO OMA, FOUND BOLT AT LT ENGINE FUEL PUMP MISSING AND LEAKING. REPLACED GASKET AND 4 BOLTS.SDR 2005FA0001195Pump · wornTHE ENGINE FUEL PUMP DRIVE WAS FOUND WORN TO THE POINT WHERE IT WOULD NO LONGER DRIVE THE PUMP, CAUSING AND ENGINE FAILURE. THE PUMP HAD 148 HOURS ON IT SINCE OVERHAUL. IT HAS NOT BEEN DETERMINED IF THE LOCATOR PIN WAS INSTALLED IN THE DRIVE.SDR KESE0508001Pump · seizedELECTRIC FUEL PUMP FAILED UPON THROTTLE RETARDATION WHILE TURNING BASE LEG TO FINAL FOR LANDING. ENGINE SHUT OFF AND SUCCESSFUL DEAD STICK APPROACH AND LANDING EXECUTED. NO DAMAGE OR INJURIES. PUMP PISTON FOUND TO BE SIEZED AND WAS BROKEN FREE WITH FORCE. SDR B65A105845Pump · unserviceablePART FAILED IN FLIGHT, REPLACED PART.SDR CA060322005Spline · wornTHE ENGINE LOST POWER BECAUSE THE ENGINE DRIVEN FUEL PUMP FAILED. THE CAUSE OF THE PUMP FAILURE WAS DISENGAGEMENT OF THE DRIVE SHAFT SPLINES FROM THE DRIVER GEAR SPLINES DUE TO EXCESSIVE WEAR.SDR COMA0560436Pump · failedFLIGHT 4998 - NR 2 HYDRAULIC SYSTEM HIGH TEMP AND LOW PRESSURE WARNING. REPLACED THE RT ENGINE HYDRAULIC PUMP.SDR CA050808002Pump · failed(CAN) AIRCRAFT WAS HAVING PROBLEM WITH INITIAL START. FUEL CHECK VALVE AND FCU HAD BEEN CHANGED FOR TROUBLESHOOTING. REPLACED ENGINE DRIVEN FUEL PUMP, AIRCRAFT RETURNED TO SERVICE.SDR CA050727006Shaft · shearedDEPARTING DEWAR LAKE(300NM NORTH OF YFB) FOR YFB, THE NR 2 ENGINE SPOOLED DOWN ON TAKEOFF. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED SAFELY. MAINTENANCE DETERMINED THE NR 2 ENGINE DRIVEN FUEL PUMP INPUT SHAFT HAD SHEARED. THE PUMP WAS REPLACED ASDR CA050729003Pump · failedDURING INSPECTION RUN-UP, THE FUEL PRESSURE DROPPED TO 3 PSI AT IDLE (NORMAL PRESSURE IS 12 PSI). THE ENGINE HAD DIFFICULTY RUNNING. THE PART WAS REMOVED AND RETURNED TO THE OVERHAUL FACILITY FOR WARRANTY WORK.SDR 2005000011Pump · failedREJECTED TAKE OFF AT 80 KNOTS NR 2 ENGINE WILL NOT MAKE POWER ONLY WENT TO 110 PERCENT N1 LOWER THAN 1&3. CORRECTIVE ACTION REMOVED AND REPLACED THE FUEL PUMP AND M.E.C. STILL IN WORK.SDR CA050712012Shaft · sheared(CAN) LEFT HAND ENGINE DRIVEN FUEL PUMP FAILED IN FLIGHT. CREW SELECTED BOOST PUMP TO RESTORE FUEL PRESSURE. 2 MINUTES LATER FUEL BOOST PUMP (P/N 215-61620-3, S/N 113, TSO 113.8 HOURS) FAILED. CREW FEATHERED ENGINE AND LANDED THE AIRCRAFT WITH NO FURTHER INSDR YAX2005F00001Pump · fluctuatesFUEL FLOW FLUCUATION AND SURGING. SOME CASES ENGINE QUITING. (K)SDR 2005000009Pump · defectiveNR 1 ENGINE WOULD NOT MAKE TAKEOFF POWER. REMOVED AND REPLACED MAIN ENGINE FUEL PUMP NR 1 ENG IAW 73-12. REMOVED AND REPLACED MAIN FUEL FILTER IAW 73-11. REMOVED AND REPLACED MEC IAW 73-20 RAN ENGINE PER OMNI JET RUN HANDBOOK, OPS CHECKS GOOD AT THIS TIME.SDR AALA20050437Pump · malfunctionedABOUT 2000 FT ABOVE GROUND LEVEL ON FINAL APPROACH, GOT LT FUEL INLET LOW LIGHT. SHORTLY AFTER THAT NR 1 ENGINE FAILED. REPLACED LT WING TANK PROBES NUMBER 5 THROUGH 12, LT WING TANK COMPENSATOR, RT WING TANK PROBES NUMBERS 6, 5, 9, 10, AND 11 AND RT WING TASDR XNA01244Tube · crackedENGINE FIRE WARNING NR 2 ENGINE PERFORMED ALL REQUESTED CHECKLIST RETURN TO AIRPORT AS REQUEST. REMOVED AND REPLACED FUEL DE-ICING CRACKED TUBE ASSY IAW MM 73-14-00. OPS CK OK IAW MM 73-10-00. (ORIG/CLOSED)SDR KBM2005F00123Pump · leakingFUEL PUMP, UNIT LEAKING AT VENT SEAL. REMOVED AND REPLACED. (K)SDR DXTA200500750Pump · inoperativeNR 2 ENGINE FUEL ANNUNCIATOR ILLUMINATED AT 40 KNOTS ON T/O STATIC POWER, ARMED APR AT BRAKE RELEASED, T/O ABORTED. REMOVED INOP FUEL PUMP & INSTALLED AN OVERHAULED UNIT AS REQUIRED, OPS & LEAK CHECK GOOD. ALL WORK PERFORMED IAW HONEYWELL TFE-731-5BR MM CHAPTESDR CA050512009Coupling · wornAIRCRAFT IN CRUISE, ENGINE SPUTTERED AND DIED. BOOST PUMP ACTIVATED AND ENGINE RESTARTED. PART IS AN ON-CONDITION ITEM. THE SQUARE DRIVE ROUNDED OFF UNTIL IT WOULD NO LONGER ENGAGE THE DRIVE GEAR P/N 631684. THIS CAUSED THE FUEL PUMP TO STOP ROTATING RESULSDR CA050527018Pump · unserviceableTHE ENGINE EXPERIENCED AN UNCOMMANDED IN-FLIGHT SHUT-DOWN SHORTLY AFTER TAKEOFF. THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. THE ENGINE FUEL CONTROL UNIT ANDFUEL PUMP WERE SUBSEQUENTLY REPLACED.SDR 2005FA0000626Capacitor · failedTHE MAGNETO WAS OVERHAULED 70 HOURS AGO, THE CAPACITORS WERE SUPPLIED BY OVERHAULER. THE OVERHAUL WAS DONE AND CAPACITORS ARE FAA PMA`D.SDR CA060228022Pump · seizedDURING AN ATTEMPTED START, THE AUX FUEL PUMP LIGHT ILLUMINATED. SYSTEM WOULD NOT FUNCTION. FURTHER INVESTIGATION FOUND PUMP SEIZED. PUMP REPLACED AND NO FURTHER DEFECTS WERE NOTED.SDR CA050527006Coupling · fracturedDURING CRUISE, THE ENGINE EXPERIENCED AN UNCOMMANDED TORQUE AND TEMPERATURE INCREASE. THE ENGINE WAS SHUT DOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED A FRACTURED FUEL PUMP COUPLING SHAFT.SDR CA050512006Pump · failedFUEL PUMP ERRATIC, LOSING PRESSURE.SDR WCL2005F00000Pump · intermittentLT FUEL PUMP PRESSURE LIGHT INTERMITTENT. TOOK PRECAUTIONARY ACTIONS AND STARTED TO FEED FUEL AND TURNED. THE INTERMITTENT FUEL PUMP OFF. (EA11200503945) (K)SDR CA050506009Relief Valve · leaking(CAN) DURING GROUND RUN WITH THE LOWER ENGINE COWLING REMOVED, THE ABOVE MENTIONED RELIEF VALVE WAS FOUND LEAKING FUEL. THIS WAS NOT NOTICEABLE WHEN THE COWLING WAS INSTALLED. THIS RELIEF VALVE HAD BEEN INSPECTED FOR S/B 73-5125 AT 1084.7 HOURS WHICH SPECIFIEDSDR 2005FA0000603Pump · malfunctionedPILOT REPORTED THAT IDLE RPM WAS TOO HIGH, 850 RPM. WHILE TECH WAS TRYING TO ADJUST IDLE, FOUND THAT THE FUEL PRESSURE WAS LOW - 16 PSI AND UNABLE TO ADJUST. REPLACEMENT OF ENGINE DRIVEN FUEL PUMP WAS REQUIRED. RECOM TO ADD A METHOD PLUS DATA FOR MAKING ADJSDR CA050418003Gasket · leaking(CAN) FUEL PUMP LEAKING FROM REAR GASKET. NOTICED ON 50 HOUR INSPECTION.SDR CA050427007Fitting · loose(CAN) ENGINE LOST POWER, SUBSEQUENT INSPECTION REVEALED A LOOSE FITTING ON THE INLET SIDE OF MECHANICAL FUEL PUMP CAUSING THE PUMP TO SUCK AIR, THUS DEPLETING THE FUEL TO THE CARBURETOR. THE FITTING WAS RETIGHTENED AND 'LOCK TIGHT' WAS USED ON THE JAM NUT, NOTSDR DUKESPUMPMPGPump · leakingPUMP IS LEAKING AT THE SEAL AT THE BASE OF THE PUMP, NEAR DRAIN PIPE.SDR DUKESPUMPPKMPPump · leakingPUMP IS LEAKING AT THE SEAL AT THE BASE OF THE PUMP-NEAR/AT DRAIN PIPE.SDR CA050419003Drive Assy · inoperative(CAN) DURING TAKEOFF ROLL THE ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN. TROUBLESHOOTING REVEALED A WORN FUEL PUMP DRIVE. THE FUEL PUMP WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR 101Pump · inoperativePILOT SQUAWKED THAT THE FUEL FLOW FOR THE RIGHT ENGINE WAS LOW AND ERRATIC IN-FLIGHT. MAINTENANCE INSPECTED AND TRIED TO ADJUST THE FUEL SYSTEM, REPLACED FUEL PUMP. NO FURTHER ACTION NEEDED.SDR 100Pump · inoperativeINSTALLED A FACTORY REMANUFACTURED ENGINE FROM CONTINENTAL THAT CAME WITH A NEW FUEL PUMP. UPON DOING THE ENGINE GROUND RUNS AND INITIAL ENGINE SET UP THE FUEL PUMP WOULD NOT SHUT OFF THE FUEL AFTER THE MIXTURE HAD BEEN PULLED BACK. INSPECTED SYSTEM FOUND TOSDR CA050609002Pump · leaking(CAN) DURING GROUND RUNUP, FUEL WAS LEAKING FROM FUEL PUMP, WHERE THE FUEL PUMP ATTACHES TO THE GEARBOX. FUEL PUMP RECEIVED AFTER INTERNAL SPLINE AD INSPECTION WHICH REQUIRES REMOVAL OF FRONT SEAL HOUSING TO ENABLE REMOVAL OF SHAFT. THIS SEEMS TO BE THE AREA SDR CA050329007Drive Assy · malfunctioned(CAN) FRENCH AUTHORITIES HAVE REPORTED AN INFLT SHUTDOWN WITH INDICATIONS OF A FUEL PUMP DRIVE MALFUNCTION.SDR AU510002016Pump · failedNR 3 ENGINE FUEL PUMP LOW PRESSURE IMPELLER SHEARED. INVESTIGATION FOUND THE FAILURE OF THE PUMP WAS CAUSED BY VIBRATIONS THAT WERE INTRODUCED BY THE INTERACTION OF THE IMPELLER SYMMETRICAL SUPPORT PINS WITH THE SPACER TUBE. THESE VIBRATIONS CAUSED A LOSS OFSDR CA050309007Pump · failed(CAN) THE NR 1 ENGINE FUEL PUMP FAILED ON TAKEOFF POWER APPLICATION. THE AIRCRAFT RETURNED TO THE COMPANY RAMP WHERE IT WAS DETERMINED THE FUEL PUMP HAD FAILED. THE PUMP WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE AFTER GROUND TESTING SERVICEABLE.SDR EM05004Pump · unserviceableENGINE NR 1 NO DISPATCH FAULT MESSAGE. MAINTENANCE, TROUBLESHOT SYSTEM IAW GE EM 72-00-00 FAULT CODES. REMOVED AND REPLACED FADEC, FAULT REMAINED. REMOVED AND REPLACED FUEL METERING UNIT, FAULT REMAINED. REMOVED AND REPLACED FUEL PUMP, FAULT CLEARED. SYST
Back to JASC 7314