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 IMJ2004F00003Pump · failedNR 2 ENGINE FUEL LIGHT ILLUMINATED IN FLIGHT. FUEL PUMP FAILEDSDR AUS20040462Pump · leaking(AUS) RT ENGINE DRIVEN FUEL PUMP LEAKING EXCESSIVELY FROM PUMP BODY. A LARGE AMOUNT OF FUEL WAS SPRAYING ONTO THE TURBOCHARGER WITH A HIGH RISK OF ENGINE FIRE. THE PUMP WAS A NEW ITEM WITH NO SIGN OF DAMAGE TO THE PUMP AND ALL THE MFGS TAMPER WIRES ARE IN PLACSDR DHL2004805005Pump · malfunctioned25 MIN AFTER SETTING CRUISE THRUST, FL 360, ENGINE NR 1 FLAMED OUT. ENGINE INSTRUMENTS NORMAL, DESCENDED TO FL 240 AND INITIATED IN-FLIGHT ENGINE START PROCEDURE, ENGINE START NORMAL, CLIMBED BACK TO FL 360. ALL ENGINE INDICATIONS NORMAL. COMPLETED ALL EMERGENSDR CA040525003Diaphragm · crackedPILOT REPORTED FUEL PRESSURE INDICATOR DROPPED INTERMITTENTLY DURING ALL PHASES OF OPERATION. AIRCRAFT WAS RETURNED TO MAINTENANCE BASE. FUEL FOUND TO BE LEAKING FROM WOBBLE PUMP. WOBBLE PUMP DIAPHRAGM FOUND TO BE CRACKED. DIAPHRAGM REPLACED, ENGINE GROUNSDR 2004FA0000432Pump · inoperativeENGINE DRIVEN FUEL PUMP NO METERED OR UN METERED FUEL PRESSURE WHILE ENGINE RUNNING. FUEL PUMP RECENTLY INSTALLED HAD 2.7 HOURS ON IT, AFTER OVERHAUL. INSTALLED NEWLY OVERHAULD PUMP. OPS CHECK GOOD. PROBABLE CAUSE OF PUMP FAILURE, UNKNOWN.SDR CA040528008Pump · leakingDURING AIRCRAFT 100 HOURS INSPECTION, THE TECHNICIAN DISCOVERED A BLUE COLORED TRACE OF FUEL ORIGINATING FROM THE FUEL PUMP LOW-METERED ADJUSTMENT SCREW. PRESSURIZED THE FUEL SYSTEM AND NOTICED MORE FUEL LEAKING FROM THE ADJUSTMENT SCREW OF THE FUEL PUMP. THSDR AALA20040551Pump · inoperativeDURING CLIMB RT ENGINE REDUCED TO 30 PERCENT WITH ACCOMPANING YAW. SHUT DOWN ENGINE AND RETURNED TO ELP. LANDED OVERWEIGHT WITHOUT INCIDENT. PERFORMED OVERWEIGHT LANDING INSPECTION. REPLACED RT ENGINE DRIVEN FUEL PUMP IAW MM 73-12-01 AND RT ENGINE FUEL CONTRSDR BAQA093854Shaft Seal · leakingSHAFT SEAL IS LEAKING. REPLACED WITH SERVICABLE UNIT FROM ITS, 05/19/2004SDR 31177050304Pump · failedDURING DESCENT FROM CRUISE, RIGHT ENGINE FLAMED OUT. ENGINE WAS SUCCESSFULLY RESTARTED. DIVERTED TO KBDL. REPLACED RIGHT ENGINE FUEL PUMP DUE TO LOW PRESSURE. REPLACED RIGHT ENGINE FUEL CONTROL DUE TO METAL CONTAMINATION IN STRAINER BETWEEN FUEL PUMP AND FSDR KBM2004F00062Pump · inoperativeFUEL PUMP, UNIT INOPERATIVE. REMOVED AND REPLACED.SDR HUN2004F00001Pump · failedON THREE OCCASIONS THIS AC HAD FUEL SYSTEM PROBLEMS. IN FEB THE ENGINE DIED AT IDLE/LOW POWER OPERATIONS. THE FUEL PUMP WAS REPLACED AND PROBLEM WENT AWAY (OUR OTHER DA20C1, N6634DC, HAD THE SAME PROBLEM AND REMEDY). AT THE END OF APRIL 556DC LOST POWER ANDSDR AUS20040319Pump · leaking(AUS) AIRCRAFT MOUNTED ENGINE FUEL PUMP LEAKING.SDR 2005FA0000946Pump · failedENGINE FAILED ON FINAL APPROACH. WAS ABLE TO RESTART AFTER LANDING BUT HAD TO PULL THE MIXTURE CONTROL LEAN ABOUT 1INCH TO KEEP IT RUNNING. AFTER COOLDOWN, MIXTURE WAS OK AGAIN. THIS IS THE FIRST OF 3 FUEL PUMP FAILURES ON THIS AIRCRAFT/ENGINE IN APPROX 90 SDR 2004FA0000790Pump · failedFUEL LEAKING INTO MANIFOLD REFERENCE LINE. PILOT EXPERIENCED INFLIGHT ROUGH ENGINE WHEN AUXILIARY FUEL PUMP TURNED ON. FUEL CONTINUED TO RUN ON GROUND AFTER ENGINE SHUTDOWN. PROBABLE CAUSE: MFG DEFECT: LEAKING DIAPHRAGM.SDR 2004FA0000789Pump · failedFUEL LEAKING INTO MANIFOLD REFERENCE LINE. PILOT EXPERIENCED INFLIGHT ROUGH ENGINE WHEN AUXILIARY FUEL PUMP WAS TURNED ON. FUEL CONTINUED TO RUN ONTO THE GROUND AFTER ENGINE SHUTDOWN.SDR FFK2004F00004Pump · failedAFTER INSTALLING AN ENGINE WITHIN 3 FLIGHT HOURS THE ENGINE DRIVEN FUEL PUMP SHAFT FAILED. PUMP FAILED ON TAKEOFF AND QUIT RUNNING.SDR CA040430002Pump · failed(CAN) RT ENGINE FUEL FILTER BY-PASS LIGHT FLICKERING AT TAKE-OFF CLIMB POWER SETTINGS. AIRCRAFT RETURN TO MAINTENANCE BASE, MAINTENANCE TECHNICIAN FOUND FUEL FILTER CONTAMINATED BY A LOTS OF FINE GREY SEDIMENT. IT WAS DETERMINED THAT THE ENGINE DRIVEN MOTIVE FSDR BAQA094234Pump · leakingFUEL PUMP LEAKING. REPLACED WITH SERVICABLE UNIT. 04/22/2004SDR CA040426004Pump · inoperative(CAN) PUMP WAS RECENTLY MODIFIED/OVERHAULED. IT WAS DISCOVERED THAT ENGINE DRIVEN FUEL PUMP OUTPUT PRESSURE DROPPED RIGHT OFF AT IDLE POWER BUT WAS FINE AT HIGH POWER SETTINGS. ENGINE DID NOT GIVE ANY INDICATION OF PUMP PRESSURE DIFFICULTIES, ROUGH RUNNING, QSDR DAT2004F00000Line · crackedLEAVING 4400 FEET, THE RT ENGINE TORQUE FELL FROM 3200 LBS TO 2000 LBS THEN TO 1500 LBS THEN STABILIZED AT 2000 LBS FOR A WHILE THEN WENT BACK TO 3000 LBS. THE FLIGHT CREW TURNED BACK AND CALLED DEC TO TELL THEM OF THE SITUATION. THE FLIGHT CREW ADVISED THE SDR BAQA094061Pump · failedFUEL PUMP FAILED OUT OF BOX (TSI 4.3 HOURS), RUNS FOR APPROX. 30 SECONDS THEN POPS CIRCUIT BREAKER. A REPLACMENT FOR THIS PUMP WAS ORDERED. REPLACED WITH SERVICABLE UNIT.SDR BAQA094292Pump · inoperativeFUEL PUMP INOPERATIVE. REPLACED WITH SERVICABLE UNIT. 04/29/2004SDR BAQA094196Pump · intermittentFUEL PUMP HAS INTERMITTENT OPERATION, POPPING CIRCUIT BREAKER. REPLACED WITH SERVICEABLE UNIT FROM AEC, 04/19/2004SDR CA040406003Seal · leaking(CAN) DURING A ROUTINE ENGINE INSPECTION THE NR 1 ENGINE COWL WAS REMOVED TO FACILITATE THE INSPECTION ON THE ENGINE. WHEN THE COWL WAS REMOVED IT WAS NOTED THERE WAS A LARGE BLUE STAIN ON THE BOTTOM OF THE COWL, JUST BELOW THE ENGINE DRIVEN FUEL PUMP. THIS SDR 2004FA0000303Pump · leakingDURING ENGINE 100 HOUR INSPECTION AND SERVICE FOUND THAT THE ENGINE DRIVEN FUEL PUMP LEAKING FUEL FROM THE REGULATOR HOUSING. (SO05200407947)SDR AUS20040238Pump · contaminated(AUS) INSPECTION OF ENGINE DRIVEN FUEL PUMP FOLLOWING STRIP FOR OVERHAUL. THE PUMP WAS FOUND TO CONTAMINATED WITH WHAT APPEARS TO BE CARBON POWDER. PUMP SHAFT BUSHING CONTAMINATED, CAUSING PUMP ROTATION TO BE RESTRICTED.SDR AUS20040227Bearing · failed(AUS) ENGINE DRIVEN FUEL PUMP FAULTY. PUMP CONTAMINATED WITH A BLACK CARBON POWDER TYPE SUBSTANCE. POOR PUMP LUBRICATION CAUSED EXCESSIVE BEARING WEAR.SDR CA040325003Adapter · broken(CAN) OIL LOSS WAS NOTED BY PILOTS AS THE OIL PRESSURE DROPPED. INFLIGHT SHUTDOWN WAS INITIATED. ON LANDING, MAINTENANCE DISCOVERED THAT THE ENGINE DRIVEN FUEL PUMP DRIVE ADAPTER HAD BROKEN AND CAUSED THE LOSS OF OIL FROM THE ACCESSORY CASE. ALSO NOTED WAS THASDR BAQA093729Filter · failedUNIT FAILED FILTER BY-PASS CHECK. THIS UNIT WAS ORIGINALLY ON THE ENGINE WHEN INSTALLED ON A/C S/N 5498. REPLACED WITH SERVICABLE UNIT. 03/11/2004SDR AALA20040259Pump · failedATL INFLIGHT T593/21 ON ROTATION LEFT HAND ENGINE UNCOMMANDED SHUTDOWN. RETURNED TO ATL AND LANDED WITHOUT INCIDENT. REPLACED NUMBER 1 ENGINE FUEL CONTROL (76960612-HAMILTON SUNDSTRAND) AND FUEL PUMP. TRIMMED ENGINE TO PROPER PARAMETERS PER 71-00-00 PAGE 50SDR AALA20040164Pressure Switch · inoperativeSJU INFLIGHT T1522/02, RIGHT INNER NR 2 PUMP FAILURE AND NR 1 PUMP WAS ON MEL. RETURNED TO SJU. LANDED WITHOUT INCIDENT. SUMPED RIGHT INNER NR 2 TANK AND ACCOMPLISHED RIGHT INNER NR 2 PUMP OPERATION. REPLACED THE FUEL PRESSURE SWITCH FOR NR 1 PUMP. SYSTEMSDR 2004F00157Pump · failed'FUEL BOOST ON' AMBER CAS MESSAGE CAME ON IMMEDIATELY AFTER LANDING. LEFT ENGINE FUEL BOOST PUMP FAILURE. REMOVED FAULTY PUMP AND INSTALLED NEW SERVICEABLE UNIT. PERFORMED RUN-UP LEAK CHECK PER CESSNA MM. AIRCRAFT RETURNED TO SERVICE. (M)SDR 58184Pump · leakingAFTER ARRIVAL, CREW FOUND FUEL LEAK IN THE LT NACELLE AREA. REMOVED AND REPLACED LOW PRESSURE FUEL PUMP (PUMP, FUEL BOOST-LOW PRESS ENGINE D) P/N 143890425, S/N B-314.SDR 0400076632Pump · malfunctionedAT FL380, THE CREW OBSERVED DECREASING PARAMETERS ON THE NR 4 ENGINE. THE COM PROCEDURES WERE FOLLOWED BUT THE ENGINE REMAINED AT IDLE. ALL INDICATIONS REMAINED IN THE NORMAL RANGE, SO THE ENGINE WAS LEFT AT IDLE POWER. WHEN DESCENDING THROUGH 8000 FEET ON SDR 2004FA0000020Pump · leakingINSTALLED OVERHAULED FUEL PUMP FROM MFG ON 4NOV03. DURING AIRCRAFT INSPECTION 22DEC04 HAD FUEL SEEP FROM WIRES ON PUMP.SDR ANCF200300030Pressure Switch · activeEICAS MSG R ENG FUEL FILTER DISPLAYED. C/A: WAS REPLACED FUEL FILTER ELEMENT IN RT ENGINE IAW A-M-M 73-11-02. FUEL PUMP FILTER DIFFERENTIAL PRESSURE SWITCH WAS REMOVED AND REPLACED IAW AMM 73-34-01 PAGE 401. P/N ON AND OFF 42D395//42D362, S/N ON 0111, SSDR CA040127013Pump · failed(CAN) ENGINE DRIVEN FUEL PUMP P/N 653351-2 FAILED DUE TO THE SEAL BETWEEN THE FUEL PUMP AND THE FUEL PUMP DRIVE. ALLOWING THE FUEL PRESSURE TO DROP AND ENGINE SHUT DOWN FOR LACK OF FUEL. THE FUEL PASSED THROUGH THE FUEL PUMP DRIVE DRAIN & OVER BOARD THE AIRCRASDR 2004FA0000169Pump · inoperativeAIRCRAFT EXPERIENCED ENGINE FAILURE DUE TO LOSS OF FUEL PRESSURE DURING TRAINING FLIGHT. STUDENT FAILED TO TURN ON ALTERNATOR SWITCH AND BATTERY POWER WAS INSUFFICIENT TO OPERATE ELECTRIC FUEL PUMP. FAILURE OCCURRED IN VICINITY OF AIRPORT AND SAFE LANDING WASDR 2004F00384Pump · failedDURING INITIAL CLIMB ENGINE NR 1 FAILED, FLAMED OUT, DUMPED FUEL AND RETURNED TO KMIA WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP PER MM 73-11-01. OPS CHECK GOOD, A/C RETURNED TO SERVICE NO FURTHER INCIDENTS. (M)SDR CA031205014Pump · leaking(CAN) CREW NOTED THAT FUEL WAS LEAKING FROM THE RT ENGINE COWL. MAINTENANCE FOUND THAT THE LOW PRESSURE FUEL PUMP HAD BLOWN OUT THE GASKET BETWEEN THE MAIN BODY AND THE REGULATOR ASSEMBLY ALLOWING FUEL UNDER PRESSURE TO ESCAPE. THE PUMP WAS REPLACED AND THE ASDR P5CA0300992Pump · leakingON ARRIVAL NR 1 ENG HAS HEAVY FUEL LEAK OUT OF DRAIN. REPLACED NR 1 ENGINE FUEL PUMP RUN UP & LEAK OK PER MM 73-11-01 AND 71-00-00.SDR 2003FA0001135Pump · leakingFUEL LEAKING AT REGULATOR HOUSING, THIS IS THE NEW STYLE PUMP, AND IS NOT YET AFFECTED BY AD 2003-14-03. WE ARE NOTING SIMILAR LEAKS WITH SEVERAL OF THESE PUMPS.SDR 2003FA0001134Pump · leakingFUEL LEAKING AT REGULATOR HOUSING.SDR BAQA090337Pump · malfunctionedENGINE WOULD NOT START. REPLACED FUEL PUMP.SDR BAQA090338Pump · malfunctionedNR 1 ENGINE SLOW TO START. REPLACED PUMP.SDR CA031020006Pump · leaking(CAN) CREW ARRIVED AT TERMINAL AND UPON SHUTDOWN WERE ALERTED TO FUEL COMING FROM RIGHT COWL. MAINTENANCE FOUND LOW PRESSURE FUEL PUMP HAD BLOWN OUT GASKET BETWEEN MAIN BODY AND THE REGULATOR ASSEMBLY. PUMP WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR DLM88030917Pump · malfunctionedAT LEVEL OFF (FL230) RT ENG FLAMED OUT, LT ENGINE BECAME UNSTABLE, BUT RECOVERED. RIGHT ENG FAILED COMPLETELY. NO VIBES NOTED. REPLACED FUEL PUMP AND CONTROL.SDR BAQA091386Pump · inoperativeFUEL PUMP PRODUCING LOW OIL PRESSURE. REPLACED WITH SERVICEABLE UNIT. 02/03/2004SDR IPM2003F00000Relief Valve · failedENGINE WOULD LOOSE POWER INTERMITTENTLY AND DURING CLIMB AFTER TAKEOFF. DETERMINED TO BE DEFECTIVE RELIEF VALVE AND SEAT IN ENGINE FUEL PUMP. (WP11200400873)SDR CA031004001Pump · failed(CAN) ENGINE DRIVEN FUEL PUMP IN SERVICE 100.1 HRS SINCE NEW. ON ENGINE RUN UP WOULD NOT SUPPLY RATED FUEL PRESSURE. ON IDLE PRESSURE 29 PSI. THERE IS ANOTHER PROBLEM WITH THOSE PUMPS RG9080J7A-OUTLET AND INLET FITTING OFTHE PUMP ARE HIGH PROFILE AND DIMENS
Back to JASC 7314