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 AALA201509129014Pump · defectiveFLIGHT CREW REPORTED THAT DURING CRUISE UP THE NE COAST, THE RT ENG UNSPOOLED. THE CREW SEEMED TO THINK IT MAY HAVE BEEN A COMPRESSOR STALL. THE CREW ELECTED TO DIVERT & DECLARED AN EMER. IT WAS REPORTED INITIALLY THAT THERE MAY HAVE BEEN SOME FUMES IN THE SDR 2015FA0000562Pump · low pressurePILOTS REPORTED LOW FUEL FLOW ON CLIMBOUT AT 13 GALLONS PER HOUR. WE HAVE ESTABLISHED AN OPERATIONAL MINIMUM FUEL FLOW OF 16.0 GALLONS PER HOUR DUE TO OUR EXPERIENCE WITH THESE ENGINE DRIVEN FUEL PUMP ANEROID FAILURES. ATTEMPTED TO ADJUST PUMP IAW SID97-3 ANSDR 2015FA0000563Pump · low pressurePILOTS REPORTED HIGHER THAN NORMAL CHT ON CYLINDERS NR 1 AND NR 3 ALONG WITH LOW FUEL FLOW ON CLIMB, IN THE RANGE OF 12 TO 14 GALLONS PER HOUR. WE HAVE ESTABLISHED AN OPERATIONAL MINIMUM FUEL FLOW OF 16.0 GALLONS IAW HOUR DUE TO OUR EXPERIENCE WITH THESE ENGISDR CA150831012Gear · worn(CAN) LEFT ENGINE LOST POWER IN FLIGHT. APPROXIMATELY 25 MINUTES AFTER DEPARTING, WHILE IN CRUISE AT 8000 FT, THE LT ENGINE QUIT. FUEL PUMP REMOVED AND FOUND THE COUPLING SHAFT, PN: 631683 ROUNDED INTERNALLY AND DRIVE GEAR, PN: 631684 WORN. DRIVE GEAR AND CSDR CA150831011Drive Coupling · worn(CAN) LEFT ENGINE LOST POWER IN FLIGHT, APPROXIMATELY 25 MINUTES AFTER DEPARTING, WHILE IN CRUISE AT 8000`, THE LT ENGINE QUIT. FUEL PUMP REMOVED AND FOUND THE COUPLING SHAFT PN: 631683 ROUNDED INTERNALLY AND DRIVE GEAR, PN: 631684 WORN. DRIVE GEAR AND COUPLINSDR FQAR20150813086Pump · blockedDURING A PREFLIGHT ENGINE RUN, THE CREW SET BOTH ENGINES RPM TO 1500; THE RT ENGINE SUBSEQUENTLY FAILED. THE CREW NOTED THE RT SIDE FUEL PRESSURE WAS ZERO. THEY SELECTED FUEL CROSSFEED, WHICH RESTORED FUEL PRESSURE AND ALLOWED THE RT ENGINE TO BE STARTED. WSDR ASMF201510005Pump · leakingDURING TRANSIT CHECK, IT WAS DETECTED A FUEL LEAK IN THE LT ENG. PERFORMED LT ENG START IAW AMM 71-00-00, DETECTING FUEL LEAK IN THE FUEL PUMP COUPLING. ACFT WAS SENT TO THE HANGAR & REPLACED THE LT FUEL PUMP IAW AMM 73-11-01, TESTED CORRECT.SDR P5CA2015080100058Pump · failedNR 3 ENGINE ROLLED BACK AND FLAMEOUT, OIL PRESSURE STABILIZED AT 14 PSI DURING CRUISE. N1 & N2 ROTATION 17.8/ 17.7. FIRE SWITCH NOT PULLED. NR 3 ENGINE FUEL PUMP REPLACED IAW AMM 73-11-01. OPS AND LEAK CHECKED OK.SDR N3XR2015073000019Pump · leakingDURING PREFLIGHT, THE CREW NOTICED AVGAS LEAKING FROM HOSE CONNECTED TO DRY BAY OF ENGINE DRIVEN FUEL PUMP.SDR N3XR201507300018Pump · leakingDURING PREFLIGHT, THE CREW NOTICED AVGAS LEAKING FROM HOSE CONNECTED TO DRY BAY OF ENGINE DRIVEN FUEL PUMP.SDR N3XR201507300020Pump · leakingDURING PREFLIGHT, THE CREW NOTICED AVGAS LEAKING FROM HOSE CONNECTED TO DRY BAY OF ENGINE DRIVEN FUEL PUMP.SDR OG5S2015FA0000356Pump · leakingON POST FLIGHT, PILOT REPORTED FUEL DRIPPING FROM BOTTOM OF COWL. UPON FURTHER INSPECTION BY MAINTENANCE, IT WAS DETERMINED THAT THE ENGINE DRIVEN FUEL PUMP WAS THE SOURCE OF THE LEAK. PUMP WAS REPLACED, OPS AND LEAK CHECK WAS GOOD.SDR 2015FA0000352Pump · leakingON PRE-FLIGHT INSPECTION, PILOT NOTED FUEL DRIPPING FROM FUEL PUMP DRAIN. UPON FURTHER INSPECTION FROM MAINTENANCE IT WAS DETERMINED THAT THE ENGINE DRIVEN FUEL PUMP CASE DRAIN WAS THE SOURCE OF THE LEAK. PUMP WAS REPLACED SYS WAS RUN UP AND LEAK CHECKED GOODSDR 2015FA0000350Pump · leakingON PRE-FLIGHT, PILOT NOTICES FUEL LEAKING FROM 1 OF THE ENGINE DRAINS. UPON FURTHER INSPECTION BY MAINTENANCE, IT WAS DETERMINED TO BE COMING FROM THE CASE DRAIN OF THE ENGINE DRIVEN FUEL PUMP. PUMP WAS REPLACED LEAK CHECKED GOOD.SDR BGJA20150721002Pump · failedDURING TAKEOFF ROLL THE RIGHT ENGINE WOULD NOT MAKE FULL POWER. THE PILOT CANCELLED THE TAKEOFF AND RETURNED TO THE SHOP. THE AIRCRAFT NEVER LEFT THE GROUND. MAINTENANCE WAS NOTIFIED AND TROUBLESHOOT THE ISSUE. MAINTENANCE FOUND THE RIGHT ENGINE WASTE GATE WASSDR CA150716009Pump · failed(CAN) DURING A ROUTINE LANDING, AFTER TOUCHDOWN, AS THE AIRCRAFT WAS SLOWING THE ENGINE STOPPED. THE PILOT RESTARTED THE ENGINE AND TAXIED OFF THE RUNWAY TO HIS HOME BASE WITHOUT FURTHER INCIDENT AND REPORTED TO MAINTENANCE. AFTER INSPECTING THE AIRCRAFT AND FSDR CA150619010Pump · failed(CAN) VIA ACARS FLIGHT NOTIFIED DISPATCH, THEY HAD A REJECTED TAKEOFF BETWEEN 70 - 80KTS DUE ENG N1 FLUCTUATIONS. THEY RETURNED TO GATE UNDER NORMAL POWER. RESOLUTION 2 ENG FUEL PUMP REPLACED IAW AMM 73-21-11 PB 401. NR 2 ENG HMU REPLACED IAW AMM 73-21-10 PSDR CA150612007Pump · leaking(CAN) THIS FUEL PUMP WAS FOUND TO BE LEAKING AFTER 1.9 HOURS’ TIME SINCE NEW. THIS FUEL PUMP HAD BEEN INSTALLED TO REPLACE A PREVIOUSLY LEAKING FUEL PUMP OF THE SAME PART NUMBER, WHICH HAD THE SAME FAILURE AFTER ONLY 2.1 HOURS’ TIME SINCE NEW. THE ORIGINAL FSDR CA150612006Pump · leaking(CAN) THE FUEL PUMP WAS NOTED TO BE LEAKING FUEL BY GROUND CREWS AFTER 2.1 HOURS’ TIME SINCE NEW. THE FUEL PUMP HAD BEEN INSTALLED NEW ON THE ENGINE. AS PART OF A NEW EXCHANGE ENGINE PURCHASED & INSTALLED DURING AN OVERHAUL. THE FUEL PUMP WAS LEAKING FROM TSDR 2015FA0000301Pump · low pressureTHE ENGINE DRIVEN PUMP PRODUCED LOW FUEL FLOW DURING TAKING OFF.SDR 2015FA0000289Pump · leakingFUEL PUMP FAILED AND THE ENGINE STOPPED DURING TAXI.SDR 2015FA0000300Pump · low pressureTHE ENGINE DRIVEN FUEL PUMP PRODUCED LOW FUEL FLOW DURING TAKING OFF.SDR 2015FA0000298Pump · low pressureTHE ENGINE DRIVEN FUEL PUMP HAS LOW FUEL FLOW.SDR ASAA2015051611750Pump · malfunctionedNR 2 ENGINE HAS HISTORY OF FUEL LEAKS. ACFT GROUNDED. REMOVED NR 2 ENGINE FUEL PUMP PACKAGE IAW AMM 73-11-01-000. COMPLETED FUEL PUMP PACKAGE INSTALLATION REF BOEING AMM 73-11-01-400-801-F00. GROUND VERIFICATION ACCOMPLISHED.SDR ASAA2015050911659Pump · leakingNR 2 ENGINE HAS HISTORY OF FUEL LEAKS. MAIN FUEL THE PUMP IS SUSPECT. ACFT GROUNDED. REMOVED FUEL PUMP PACKAGE ON NR 2 ENGINE REF MM 73-11-01-000-801-F01. REMOVED HMU IAW TC N8473000. BEGAN INSTALLATION OF NR 2 ENGINE FUEL PUMP PACKAGE WITH NEW FUEL PUMP. RSDR CA150519016Pump · malfunctioned(CAN) CRUISING AT FL 230, WITH NO SYMPTOMS OR FAULT INDICATIONS THE CREW REPORTED AS A LOSS OF POWER. DECREASING SIGNIFICANTLY WITHIN 1 SEC AND IFSD. AN ATTEMPT TO START THE ENGINE IN FLIGHT WAS NOT SUCCESSFUL. SINGLE ENGINE LANDING PERFORMED WITH NO TROUBLSDR ASAA2015043011713Pump · unknownPOWERPLANT ENGINEERING REQUESTS NR 1 ENGINE VENTS AND DRAINS INSPECTION TO DETERMINE SOURCE OF FUEL LEAK. ACFT GROUNDED. IAW POWERPLANT ENGINEERING REQUEST R & R NR 1 ENG MAIN FUEL PUMP IAW AMM TASK 73-11-01 AND MAINTENANCE N8473000 AND N8473001. ALL LEAK CSDR YAXA2015091402Pump · leakingWHILE PARKED ON THE RAMP, THE AIRPLANE WAS FOUND TO HAVE FUEL LEAKING FROM THE ACCESSORY CASE SEAL DRAIN LINE ON THE LT ENG. THE ENG DRIVEN FUEL PUMP WAS FOUND TO HAVE A SHAFT SEAL LEAK THAT SEALED ITSELF WHEN PRESS WAS APPLIED WITH THE BOOST PUMP OR BY RUNNISDR 2015FA0000171Pump · leakingTHIRD FUEL PUMP IN A ROW TO LEAK FUEL FROM THE VENT LINE.SDR 2015FA0000145Pump · faultyREMOVED DEFECTIVE ENGINE DRIVEN FUEL PUMP RG9080J9A/M, SN E3394 AND INSTALLED "DEFECTIVE" NEWLY O/H FUEL PUMP, PN RG9080J8A/M, SN E-1186 THE FUEL PUMP WOULD NOT MAINTAIN PROPER FUEL PUMP AT IDLE RPM. WE OBTAINED ANOTHER NEWLY O/H FUEL PUMP RG9080J8A/M, SN D-1SDR 2015FA0000568Pump · low pressureDURING A ACFT PROGRESSIVE INSPECTION, PROGRAM 50 HR INSPECTION DISCOVERED ENGINE FUEL FLOW TO BE LOW OUT OF LIMITS. IN THIS CASE WE WERE ABLE TO ADJUST THE FUEL FLOW TO WITHIN LIMITS IAW CMI SID97-3F. DURING FLIGHT CHECK IAW SID97-3, FUEL FLOW WAS LOW OUT OFSDR AALA201504149034Pump · failedFLIGHT 784, DURING APPROACH AT 3000 FEET, THE ACFT ENCOUNTERED A FUEL CONTROL FAILURE ON NR 2 ENGINE. A GO AROUND WAS INITIATED TO COMPLY WITH THE EMER CHECKLIST. THE NR 2 ENGINE NR 1 FIRE BOTTLE WAS FIRED AS A PRECAUTION. THE FLIGHT LANDED WITHOUT FURTHER SDR 2015FA0000136Pump · leaking(B-9571) LOW FUEL FLOW WAS INDICATED DURING TAKEOFF.SDR 2015FA0000139Pump · leaking(B-9736) FIELD MECHANIC FOUND FUEL LEAKAGE.SDR 2015FA0000138Pump · leaking(B-9578) LOW FUEL FLOW WAS INDICATED DURING TAKING OFF.SDR 2015FA0000135Pump · leaking(B-9733) LOW FUEL FLOW WAS INDICATED DURING TAKING OFF.SDR ASAA2015032511094Pump · leakingON ENGINE CHECK, OBSERVED FUEL UNDER NR 1 ENGINE. ACFT GROUNDED. RAN NR 1 ENGINE FOR APPROXIMATLELY 10 MINUETS FOUND LEAK TO BE AT 14 DROPS A MINUTE. RUNNING AT IDLE. FOUND FUEL COMING FROM FUEL PUMP DRAIN. FOUND TO BE WITHIN LIMITS BUT WILL REQUIRE CHANGE SDR CA150611002Pump · failed(CAN) TPE331-12JR POWERED ACFT EXPERIENCED A LOSS OF TORQUE, RESULTING IN A FORCED LANDING AFTER ONLY NINE HOURS’ TIME SINCE NEW. TEAR DOWN EXAMINATION IDENTIFIED METALLIC DEBRIS WITHIN THE ENG FUEL SYS. THERE WAS METALLIC DEBRIS IN THE SCREEN BETWEEN THE FUSDR 2015FA0000134Pump · leaking(B-9571) FIELD MECHANIC FOUND FUEL LEAKAGE ON 19TH MARCH.SDR AALA20150715010Pump · faultyAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS NOT OVERWEIGHT. RETURNED DUE TO LT ENG COMPRESSOR STALL AT 10,000 FEET. NO ENG SHUTDOWN REPORTED. REPLACED LT ENG FUEL PUMP IAW 73-94-04.SDR ASMF201503016Pump · leakingAIRCRAFT RETURNED TO PLATFORM DUE TO DURING RT ENG START, A FUEL LEAK WAS DETECTED. THE PLATFORM WAS CLEANED BY FIREMEN & MX PERFORMED REVISION, DETECTING FUEL LEAK IN THE MAIN FUEL PUMP DRAIN PORT. THE RT ENG WAS MOTORING, AFTER IT WAS STARTED & ENG OPERATISDR CA150213017Pump · failed(CAN) DURING TAKEOFF GROUND ROLL PILOTS NOTED THAT THE RIGHT HAND ENGINE POWER ROLLED BACK, THE TAKEOFF WAS ABORTED. MAINTENANCE TROUBLESHOOTING FOUND ENGINE DRIVEN FUEL PUMP TO BE AT FAULT FOR THE POWER ROLL BACK DUE TO PUMP OUTPUT PRESSURE LOW. FUEL PUMP P/NSDR 2015FA0000133Pump · leaking(B-9739) LOW FUEL FLOW ABOUT 13.3 G/H WAS INDICATED DURING FULL THROTTLE.SDR CA150205011Pump · failed(CAN) AUXILIARY FUEL PUMP LOW PRESSURE WARNING ILLUMINATED DURING FLIGHT. PUMP REPLACED AFTER LANDING. DEFECT RECTIFIED.SDR HUNA20150129001Pump · malfunctionedON A FLIGHT, SUFFERED AN INFLIGHT UNCOMMANDED ENG SHUTDOWN OF THE LT ENG. CREW HAD BEEN CLEARED FROM FL 370 TO FL 240 FOR THE DECENT. THE SHUTDOWN OCCURRED AT OR NEAR TOP OF DECENT. THEY DECLARED AN EMER WITH CTR. THE CREW COMPLETED THE APPROPRIATE ACFT CHSDR USAA2015012000021Pump · failedEMERGENCY DECLARED FOR NR 2 ENG FAILURE DESCENDING OUT OF APPROX 2500. MULTIPLE FAILURES & MULTIPLE INDICATIONS. ENG STALL & FUEL HIGH PRESS FAILURE. RETURNED TO NORMAL AFTER 5TH OR 6TH RESTART. REPLACED THE NR 2 ENG FUEL PUMP IAW AMM 73-11-10. CROSS REFESDR USAA2015012000020Pump · inoperativeREJECTED TAKEOFF AT 50 KNOTS, NR 2 ENGINE WOULD NOT SPOOL. ACFT RETURNED TO GATE. REPLACED NR 2 ENGINE FUEL PUMP IAW AMM 73-11-10.SDR 2015FA0000132Pump · leaking(B-9733) LOW FUEL FLOW, ABOUT 15.3 G/H, WAS INDICATED DURING FULL THROTTLE.SDR CA150112009Pump · leaking(CAN) FUEL PUMP LEAKING FUEL INTERNALLY. NOTED FUEL IN FUEL PUMP DRIVE DRAIN. AIRCRAFT GROUNDED UNTIL ARGOTECH PUMP AND REPLACEMENT FCU ARRIVE.SDR 2015FA0000131Pump · leaking(B-9731) LOW FUEL FLOW WAS INDICATED DURING FULL THROTTLE.
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