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 2001FA0000156Pump · leakingPILOT REPORTED FUEL SMELL IN CABIN, LATER NOTIFIED FUEL LEAKING FROM ENGINE COMPARTMENT. TECHNICIAN FOUND LOW PRESSURE FUEL PUMP LEAKING AT RELIEF AND SCREWS LOOSE. PUMP REMOVED AND REPLACED WITH NEW UNIT. (REFERENCE TEXTRON LYCOMING AD 98-18-12 AND TEXTRON LYSDR GLBA2001093Pump · failedABORTED T/O, RIGHT LOW FUEL PRESSURE LIGHT ILLUMINATED. REPLACED LP PUMP.SDR 2001UALA00640Pump · failedAIRCRAFT DIVERTED TO MSP DUE TO NUMBER THREE ENGINE SHUTDOWN. *S/D* THE ENGINE DRIVEN FUEL PUMP LOST FUEL FLOW CAUSING THE ENGINE TO FLAME OUT. REPLACED THE FUEL CONTROL UNIT AND THE FUEL PUMP.SDR 01FDEA00323Pump · failedON T/O NR 1 ENG SHUTDOWN. ENG MET ALL RESTART PREM. REMOVED AND REPLACED NR 1 ENG FUEL CONTROL UNIT AND FUEL PUMP PER JRH, LEAK CK GOOD. OK FOR SERVICE.SDR 20010511CW004Gasket · leakingDURING LANDING ROLLOUT, AN EXPLOSION AND FIRE OCCURRED IN LEFT ENGINE. EXAMINATION FOUND THE FUEL PUMP RELIEF VALVE COVER GASKET LEAKING FUEL. AD AND SB HAD BEEN ACCOMPLISHED SEVERAL HUNDRED HOURS AGO. THE DAMAGE WILL REQUIRE REPLACEMENT OF ALL ENGINE ASSESDR MWEA010667Pump · failedDURING CRUISE RIGHT ENGINE UNSPOOLED TO 75 PERCENT. REMOVED AND REPLACED RIGHT ENGINE FUEL PUMP.SDR LS1R071919Pump · noisyPART IS NOISY.SDR SW15200110851Pump · defectivePART INSTALLED NEW AT OVERHAUL. TEST CESS OPERATION WITHIN REQUIRED PRESSURE AND FLOW. AT INSTALLATION IN AIRCRAFT, PUMP WOULD NOT FUNCTION AND WOULD NOT ALLOW FUEL TO BE PUMPED THRU USING BOOST PUMP.SDR S01271013APump · malfunctionedREGISTRATION NUMBER - B18771 NR 2 ENGINE FLAME OUT AT FL330, TAT -4 DEGREES C, EGT 352 DEGREES C, EPR W.02 DROPPING, ENGINE SHUTDOWN, WINDMILLED APPROX 1 MIN AT OIL PRESS 22 PSI, ENG WAS RESTARTED AND OPERATED NORMALLY. IAW AMM 71-00-43, MAIN FUEL FILTER AND ESDR CA010409010Pump · failed(CAN) LT ENGINE WOULD NOT RUN WITHOUT AUXILIARY ELECTRIC FUEL PUMP ON HIGH. FUEL PUMP AT DRIVE REPLACED, GROUND CHECKED OK.SDR GLBA2001068Pump · failedRIGHT FUEL PRESSURE ANNUNCIATOR ILLUMINATED. REPLACED ENGINE DRIVEN FUEL PUMP, OPS CHECKED SYSTEM GOOD. RETURNED TO SERVICE.SDR 2001FA0000688Pump · failedON 16 MAR O1 BPA RETURNED TO SERVICE (PN IO360, SN 966336A) AFTER SATISFACTORY TEST AFTER OVERHAUL. THE ENGINE WAS SUBSEQUENTLY INSTALLED AT ANOTHER FACILITY. THE MECHANIC NOTIFIED US BY PHONE THAT FUEL WOULD NOT FLOW THRU THE FUEL PUMP EVEN WITH THE USE OF SDR CA010424002Shaft · failed(CAN) THE NR 2 ENGINE FLAMED OUT. AFTER THE PILOT LANDED THE AIRCRAFT SUCCESSFULLY, REMOVE THE AFCU, MFCU AND ENGINE DRIVEN FUEL PUMP. I FOUND THE FUEL PUMP SPLINES WITH NO LUBRICATION AND WORN WELL BEYOND LIMITS. (NOTE: THE SPLINED ADAPTER WAS SPINNING FREELYSDR AU010228Cap · contaminated(AUS) ELECTRIC FUEL PUMP OUTLET T FITTING BLANKING CAP CONTAMINATED WITH SWARF. THE BLANKING CAPS ARE FITTED DURING MODIFICATION IAW EO E121-01 REV1.SDR 20010404CW006Pump · failedPILOT NOTICED EXCESSIVE CONSUMPTION OF FUEL COMPARED TO FLIGHT TIME AND LANDED. FOUND FUEL DRAINING FROM ENGINE COWLING AREA. PILOT PRESSURIZED FUEL SYSTEM, FOUND FUEL LEAKING FROM LOW PRESSURE FUEL PUMP GASKET BETWEEN PUMP REGULATOR AND PUMP BODY. THE INTESDR DL76L010382Pump · looseA/C DIV SNN DUE FUEL QTY DISCREPANCY BETWEEN FUEL TOTALIZER AND FMS FUEL REALITY. INCREASE THROUGH OUT FLT ACCOMPANIED BY INCREASING FUEL IMBALANCE WITH EXCESSIVE CONSUMPTION FROM RT WING. FOUND 2 EA FASTENER LOOSE AT FUEL PUMP FLANG FITTING AFT LINE TO FUEL SDR AU010193Pump · contaminated(AUS) RT ENGINE DRIVEN FUEL PUMP ADJUSTABLE ORIFICE CONTAMINATED WITH A SMALL PARTICLE.SDR DHL2001702003Pump · failedNR 2 ENGINE FAILURE ON TAKEOFF ROLL AT 90 KTS. REMOVED AND REPLACED FUEL PUMP. FUEL CONTROL UNIT CHECKS GOOD PER M/M 73-11-1 & 72-00.SDR DL72S010322O-Ring · leakingAT FL 310, NR 2 ENGINE OIL PRESSURE WAS BELOW GREEN BAND. OIL QTY WAS ZERO. ENGINE SHUT DOWN PER POM. FOUND O-RING LEAKING AT FUEL PUMP TO GEARBOX INTERFACE. REPLACED SAME.SDR 0100619933Pump · failedDURING FLIGHT AT FL350, THE RIGHT ENGINE CEASED OPERATING. THE FLIGHT CREW FOLLOWED COM PROCEDURES, DIVERTED TO CLE, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE DRIVEN FUEL PUMP LOCATED ON THE RIGHT ENGINE. OPERATIONAL CHECK NORMAL.SDR DL72L010239Shaft · shearedNR 3 ENG FAILED ON T/O ROLL. ABORTED AT 130 KIAS. REPLACED NR 3 ENG FUEL PUMP PER M/M. OPS CK AND LEAK CK ON IDLE RUN. ALSO TRIM ENG PER PFHB 4077 TEST Y. CK NML. RETORQUED FUEL PUMP QUAD RING PER M/M.SDR CA010320020Pump · failed(CAN) DURING TAKEOFF, NR 1 ENGINE FAILED. REJECTED TAKEOFF ACCOMPLISHED. A/CSECURED AND AIRCRAFT RETURNED TO GATE. H.P. PUMP AND FCU CHANGED I.A.W. 73-11-1, TRIM RUNS AND LEAK CHECK CARRIED OUT I.A.W. 71-09-00. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT.SDR 20010406CW009Pump · failedFUEL LEAK IN AREA OF FUEL PUMP ABOVE INJECTOR. CAUSED FIRE. HOSES WERE NOT REMOVED TO DETERMINE EXACT CAUSE.SDR CA010219019Diaphragm · cracked(CAN) DURING AN INSPECTION, A FUEL STAIN WAS NOTICED ON AN ADF ANTENNA. IT WAS TRACED TO THE HEATER FUEL PUMP. THE PUMP WAS DISASSEMBLED AND A CRACKED DIAPHRAGM WAS FOUND. WHEN THE HEATER WAS RUNNING, FUEL POURED OUT AT THE FUEL PUMP HOUSING. THE DIAPHRAGM LOOSDR 20010406CW001Pump · leakingMETAL FOUND IN FUEL PUMP FILTER. UPON DISASSEMBLY OF FUEL CONTROL / FUEL PUMP FOR REPLACEMENT OF FUEL PUMP FOUND BLUE DYE BETWEEN FUEL PUMP AND FUEL CONTROL INDICATING FUEL CONTROL BEARING WASHOUT DUE TO FUEL PUMP SHAFT SEAL LEAKAGE. THIS REQUIRED SENDING FUESDR 20010227SG005Pump · failedENGINE OIL PUMP PN: 3104268-1 SN; A1178 WITH 1848.2 HOURS SINCE INSTALLATION FAILED. THE PUMP SEIZED AND CAUSED SHAFT TO SHEAR. PUMP WAS REPALCED WITH OVERHAULED UNIT.SDR 20010227SG002Pump · leakingENGINE DRIVEN FUEL PUMP BEGAN LEAKING FROM SHAFT SEAL.SDR WVBA2001004Pump · malfunctionedON PRE INSPECTION RUN UP, IT WAS NOTICED THAT THE FUEL PRESSURE WAS LOW ON THE LEFT ENGINE. THE FUEL PRESSURE WAS ADJUSTED IN ACCORDANCE WITH INSTRUCTIONS IN THE SERVICE MANUAL FOR THE AIRCRAFT WHICH RESULTED IN NO CHANGE IN THE FUEL PRESSURE ON THE GROUND RUSDR 20010227SG004Pump · leakingFUEL LEAK FROM PUMP DRAINSDR AU010047Seal · failed(AUS) LT ENGINE DRIVEN FUEL PUMP SEAL FAILED. FUEL LEAKING FROM VENT.SDR AALA20010021Pump · leakingMIA - FLT 9212 - EN ROUTE MIA-ABQ - DETECTED NR 1 ENGINE SHUT DOWN. RETURNED MIA AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 1 SIDE FUEL PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR P2EA00466Pump · failedFLT 355 - MDW - WHILE ADVANCING THROTTLES FOR TAKEOFF AND WITH BOTH ENGINES STABILIZED AT 1.4 EPR THE NR 1 ENGINE FAILED. ENGINE WAS SHUTDOWN AND TAKEOFF ABORTED. AIRCRAFT RETURNED TO GATE WITH NO INCIDENT. REMOVED AND REPLACED FUEL PUMP PER MM 73-11-1. OPSDR 20010209CW002Pump · leakingENGINE DRIVEN FUEL PUMP LEAKING OIL FROM DRAIN.SDR CA010129005Drive Shaft · failed(CAN) UPON DISASSEMBLY OF THE FCU AND FUEL PUMP, IT WAS FOUND THAT THE DRIVESHAFT FOR THESE UNITS ROTATED FREELY HAVING BECOME DISENGAGED IN THE GEARBOX. THE ENGINE IS BEING SHIPPED TO NATIONAL FLIGHT FOR ASSESSMENT AND REPAIR. A REPORT ON FAILED PARTS WILL FSDR 20010213CW006Pump · leakingENGINE DRIVEN FUEL PUMP LEAKING OIL FROM DRAIN.SDR 20010209CW004Pump · leakingENGINE DRIVEN FUEL PUMP LEAKING OIL FROM DRAIN.SDR 20010209CW003Pump · leakingENGINE DRIVEN FUEL PUMP LEAKING OIL FROM DRAIN.SDR 20010110CW001Pump · malfunctionedON APPROACH, 15MI OUT OF LAX, RT ENGINE SHUTDOWN WHEN THROTTLES PULLED BACK. RT ENG LLP PUMP, WAS OBSERVED. /REMOVED AND REPLACED RT ENGINE LOW PRESSURE FUEL PUMP.SYSTEM & LEAK CHECKED GOOD.SDR 20010227SG003Pump · leakingFUEL LEAK FROM BETWEEN PUMP AND MOUNTSDR 20010222CW004Pump · leakingSHORTLY AFTER TAKEOFF, PILOT SMELLED SMOKE IN COCKPIT AND RETURNED TO AIRPORT. UPON INSPECTION, FOUND ENGINE DRIVEN FUEL PUMP TO BE LEAKING BETWEEN CASE HALVES. NO HEAT RELATED DAMAGE TO ENGINE AREA WAS NOTED.SDR 20010129CW019Washer · disintegratedINTERNAL TO THE LW15473 FUEL PUMP, ON THE UPPER END OF THE PULL ROD, SHOWS A WASHER PN6413701 AND PN6413703. WASHER 64113701 WAS MISSING FROM THE PULL ROD AND BELIEVED TO BE FOUND IN THE SUMP ANDSUMP SCREEN IN PIECES.SDR AALA20002093Pump · defectiveMIA - FLT 912 - EN ROUTE MIA-LAX, DETECTED AIRCRAFT INTERMITTENTLY OSCILLATING SIDE TO SIDE. OSCILLATION INCREASED DURNIG CLIMB. RETURNED MIA AND LANDED WITHOUT FURTHER INCIDENT. REPLACED RIGHT SIDE HIGH PRESSURE FUEL PUMP. ACCOMPLISHED LEAK AND POWER ASSUSDR 20010305CW007Pump · leakingWITH A 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/0.012 TO 0.016IN/ AWAY FROM THE IDLSDR TI1R001372Pump · failedFUEL PUMP CARTRIDGE, MOTOR WINDINGS OPEN. REMOVED AND REPLACED.SDR 20001129SH014Pump · damagedALT BRACKET CONTACTING FUEL INLET FITTING DUE TO FITTING ''CLOCKING'' AND BRACKET LOCATION. FACTORY ZERO TIMED ENGINE. BOTH COMPONENTS FACTORY INSTALLED CAUSED LOSS OF FUEL IN-FLIGHT. ENGINE PUMP REPLACED WITH CONTINENTAL SUPPLIED O/H UNIT AND FOUND NEW PUMSDR CA010625049Pump · broken(CAN) THIS ENGINE DRIVE FUEL FAILED DURING AN ATTEMPTED START ON THE GROUND. FAILURE DUE TO INTERNAL DRIVE - PUMP NOT DISASSEMBLED. CAN BE HEAD FOR PICK UP OR RETURNED TO MANUFACTURER. PLEASE REFER TO ALERTCEB A73-3091. PLEASE REFER TO ADDITIONAL ENCLOSED INFOSDR CA001218003Pump · failed(CAN) THIS ENGINE DRIVEN FUEL PUMP FAILED DURING AN ATTEMPTED START ON THE GROUND.FAILURE DUE TO INTERNAL DRIVE FAILURE - PUMP NOT DISASSEMBLED. CAN BE HELD FOR PICK UP OR RETURNED TO MANUFACTURER T.C. CASE PLEASE REFER TO ALERT CEB A73-3091.PLEASE REFER TO ADSDR 20010305CW006Pump · leakingWITH A 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 4 MM/0.012IN TO 0.016IN/ AWAY FROM THE SDR 20010305CW005Pump · failedHIGHWING TANK CONNECTED TO THE FUEL PUMP INLET PORT. THE NONE DRIVE FUEL PUMP LEAKS REGARDLESS THE MIXTURE LEVER POSITION. WITH MIXTURE LEVER IN IDLE CUTOFF, FUEL FLOW IS SAME AS IN FULL RICH. 3 TO 4 MM/0.012IN TO 0.016IN AWAY FROM THE IDLE CUT OFF STOP, THSDR CA001108009Pump · worn(CAN) NR 2 ENGINE DECELLED IN-FLIGHT. INLET FUEL LINE TO FUEL PUMP (P/N 76307-02003-083) HAD WORN A GROOVE ON FUEL PUMP UNION (P/N AN919-19D). THIS ALLOWED AIR INTO THE FUEL SUPPLY SYSTEM. FUEL PUMP P/N 6896810 REPLACED. AN919-10D UNION REPLACED. ENGINE G
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