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 CG9S2016FA0000409Pump · low pressureDURING A MAINTENANCE CHECK FLIGHT, THE AIRCRAFT LOST ENGINE POWER APPROXIMATELY 2-3 MILES FROM AIRPORT ON APPROACH. ACFT WAS ABLE TO LAND UNEVENTFULLY ON ANOTHER RUNWAY AT THE SAME AIRPORT. PILOT STATED HE WAS APPROACHING AIRPORT FROM WEST AND WAS DIRECTED TSDR ASMF201611005Pump · failedAIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB AT FL 170´, THE LEFT ENGINE EXPERIENCED THRUST DETERIORATION AT A SHOW RATE, THE LEFT ENGINE THRUST LEVER WAS ADVANCED TO THE FULL THRUST POSITION WITHIN INDICATION OF THRUST INCREASING AT ALL PARAMETERS. AIRCRAFSDR ASMF201610014Pump · failedAIRCRAFT RETURNED DURING CLIMB AT FL 170´, THE LEFT ENGINE EXPERIENCED THRUST DETERIORATION AT A SHOW RATE, THE LEFT ENGINE THRUST LEVER WAS ADVANCED TO THE FULL THRUST POSITION WITHIN INDICATION OF THRUST INCREASING AT ALL PARAMETERS. AIRCRAFT WAS SENT TO THSDR JJBA20160826018Pump · inoperativeNR 1 PROP TORQUE LAGS P/L INPUTS. FLUCTUATES 50% WITH NO P/L INPUTS. R & R THE NR 1 ENGINE FUEL PUMP AND NR 1 ENGINE MFC IAW PWMM 72-01-40 PERFORMED OPS CHECK IAW AMM 71-00-00, OPS AND LEAK CHECKED GOOD. NO OTHER DEFECTS NOTED AT THIS TIME.SDR 39LA20160825167Pump · leakingREPORTED A VERY INTENSE FUEL ODOR RETURNING DEPARTURE AT THE END OF AN 8 HOUR CONOP. DURING REFUELINGS THROUGHOUT THE DAY, OCCASIONAL DROPS OF FUEL WERE NOTICED AT THE NR 2 ENGINE GAIN DRAIN. THE NR 2 ENGINE DRAIN LINES FROM THE ENGINE PLATFORM TO THE ACFT FSDR ASAA2016081717743Pump · failedFUEL DRIPPING FROM THE BOTTOM COWL OF NR 1 ENGINE. ACFT GROUNDED. WHILE ACCOMPLISHING ENGINE DRAINS AND VENTS INSPECTION WITH ENGINE RUNNING FUEL STARTED TO LEAK OUT FROM THE HMU ATTACHMENT TO THE FUEL PUMP AT STEADY RATE AND ALSO FROM THE FUEL PUMP PAD DRASDR AALA201608089002Pump · failedFLIGHT CREW REPORTED RECIEVEING A NR 1 ENGINE FUEL CONTROL ECAM FAULT DURING TAKEOFF ROLL AND ABORTED THE TAKEOFF AT 60 KNOTS. AIRCRAFT GROUNDED. MAINTENANCE REPLACED THE NR 1 ENGINE FUEL PUMP AND FUEL METERING UNIT IAW AMM 73-12-41 & 73-22-52. A SATISFACTORSDR AALA20160802007Governor · faultyDURING TAKE OFF, NR 1 ENGINE LAGGED BEHIND NR 2 AND WAS SLOW TO ATTAIN TAKE OFF POWER. DURING CLIMB THE NR 1 ENGINE REQUIRED MANUAL THROTTLE MOVEMENT TO ATTAIN COMMANDED CLIMB EPR WITH A THROTTLE LEVER SPLIT THAT REACHED 5 INCHES. EMERGENCY DECLARED. LANDINSDR AALA20160731007Pump · faultedDURING TAKE OFF, NR 1 ENGINE LAGGED BEHIND NR 2 AND WAS SLOW TO ATTAIN TAKE OFF POWER. DURING CLIMB NR 1 ENGINE REQUIRED MANUAL THROTTLE MOVEMENT TO ATTAIN COMMANDED CLIMB EPR WITH A THROTTLE LEVER SPLIT THAT REACHED 5 INCHES. EMERGENCY DECLARED. LANDING USDR OG5R2016FA0000315Washer · brokenENGINE DRIVEN FUEL PUMP PLUNGER RETAINING METAL WASHER AND PLASTIC WASHER BROKE OFF AND WAS FOUND IN THE OIL SCREEN AND OIL SUMP. BOTH PIECES WERE FOUND CRACKED IN HALF.SDR OG5R2016FA0000314Washer · brokenENGINE DRIVEN FUEL PUMP PLUNGER RETAINING METAL WASHER AND PLASTIC WASHER BROKE OFF AND WAS FOUND IN THE OIL SCREEN AND OIL SUMP. BOTH PIECES WERE FOUND CRACKED IN HALF.SDR AALA201606239002Pump · defectiveDIVERTED, ACFT WAS GROUNDED. FLIGHT CREW REPORTED WHILE AT 38,000 THE RT ENGINE ROLLED BACK FOLLOWED BY AN ECAM MESSAGE INDICATING THE RT ENGINE STALLED. THE ACFT DESCENDED TO FL 290 AND THE RT ENGINE ROLLED BACK UP AND STARTED TO RUN NORMAL. THE ACFT DIVERSDR AALA201606169009Pump · defectiveRETURNED TO DEPARTURE, AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED A RT ENGINE LOW PRESSURE PUMP STATUS MESSAGE OCCURRED AT FL 24000, 1 CHANNEL AND RETURNED TO DEPARTURE. MAINTENANCE REPLACED THE NR 2 ENGINE LOW PRESSURE FUEL PUMP AND THE FUEL PRESSURE SWITCHSDR FDEA201605141586Pump · malfunctionedFLIGHT TEST FTAM 4-66, RT ENG SHUTDOWN & RE-LIGHT FL 220 AIRSPEED 300KTS. AFTER THE NORMAL SHUTDOWN OF THE RT ENG, RELIGHT WAS ATTEMPTED. WHEN THE RT FUEL CONTROL SWITCH WAS POSITIONED FROM CUT OFF TO RUN THE SPAR, VLV OPEN & THE ENG VLV ON THE RT ENG DID NOSDR IPXA2016041202051Pump · inoperativeAT +/- 1000 AGL AFTER T/O NR 2 ENGINE HAD LOUD BANG AND ROLLED BACK. PERFORMED SEVERE DAMAGE QRH. NO RESTART ATTEMPTED. N1 OIL QTY AND OIL PRESS INDICATED. WINDMILLED 1HR 15 MIN. REPLACED ENGINE NR 2 FUEL PUMP IAW MM 73-11-01. PN OFF-ON: 5006834M, SN OFSDR AALA20160408003Pump · malfunctionedAIRCRAFT WAS GNDED. DURING TAKEOFF, THE NR 2 ENG EXPERIENCED AN UNCOMMANDED POWER REDUCTION. TAKEOFF WAS ABORTED AT APPROX 110 KNOTS. R & R RT ENG DRIVEN FUEL PUMP & FUEL CONTROL IAW AMM 73-12-01 & MCM 73-91-99. ACCOMPLISHED LEAK CHECK & OPERATIONAL CHECKSSDR AALA201604119011Pump · defectiveAIRCRAFT WAS GNDED. NR 2 ENG SLOW TO ACCELERATE TO TAKEOFF LAGS NR 1 ENG BY 2 SECONDS & EXCEEDS THE 6.2 SECONDS TO REQUIREMENT TO GET TO TAKEOFF. REPLACED THE FOLLOWING COMPONENTS ON THE NR 2 ENG, FUEL PUMP, FUEL, METERING UNIT, RT 7TH STAGE BLEED VLV IAW 73SDR UIEA2016033100227Pump · malfunctionedUPON LEVEL OFF AT FL 360, RT ENG COMPRESSOR STALLED 4 TIMES. NO EXCEEDANCES WERE NOTED. ACCOMPLISHED NR 2 ENG BORESCOPE INSPECTION IAW ECM ITEM NR 2016-098 STEPS 4-9, WITH NO SIGNIFICANT DISCREPANCIES NOTED. REFERENCE WO 012864 FOR DETAILS. ACCOMPLISHED STESDR AALA201603289001Pump · defectiveAIRCRAFT WAS GNDED. NR 2 ENG STALLS, 5 HRS INTO FLT, HAD BEEN AT FL 400, REC MAX 409, FOR ABOUT 5 MIN WITH NO TURB & GOT NUMEROUS NR 2 ENG STALL ECAM WARNINGS. ENG WOULD GO TO IDLE, ECAM WARNING WOULD DISAPPEAR & ENG WOULD ACCELERATE TRIGGERING THE WARNING ASDR YAXA2016032502Fitting · misalignedTHIS ENG WAS RECEIVED IN OVERHAULED CONDITION IN PREPARATION FOR INSTALLATION ON THE ACFT. DURING INSPECTION OF THIS ENG PRIOR TO INSTALLATION ON ACFT, IT WAS FOUND THAT THE FUEL PUMP INLET FITTING AS ALIGNED FROM THE MANUFACTURER WILL NOT ALLOW THE 3/16" CLESDR YAXA2016032501Fitting · misalignedTHIS ENG WAS RECEIVED IN OVERHAULED CONDITION IN PREPARATION FOR INSTALLATION ON THE ACFT. DURING INSPECTION OF THIS ENG PRIOR TO INSTALLATION ON ACFT, IT WAS FOUND THAT THE FUEL PUMP INLET FITTING AS ALIGNED FROM THE MANUFACTURER WILL NOT ALLOW THE 3/16" CLESDR CA160216024Pump · leaking(CAN) DURING A ROUGH RUNNING ENGINE SNAG IT WAS FOUND THAT THE FUEL PUMP WAS LEAKING FROM THE LOWER FLANGE BELOW THE STOP FOR THE FUEL MIXTURE CONTROL. THE FUEL PUMP WAS REPLACED. THERE HAVE BEEN 3 SIMILAR INCIDENTS IN THE LAST 2 DAYS OF PUMPS LEAKING. IT MAY SDR CA160216020Pump · leaking(CAN) AIRCRAFT SNAGGED, DURING VISUAL INSPECTION OF ENGINE FOUND FUEL PUMP LEAKING AROUND MIXTURE LEVER PIVOT POINT. FUEL PUMP REPLACED.SDR ASAA2016020915433Pump · failedNR 1 ENGINE MAIN FUEL PUMP HAS HISTORY OF FUEL LEAKAGE FROM THE PAD CAVITY DRAIN DURING ENGINE START. INTERMITTENT INPUT SHAFT SEAL LIFT OFF IS SUSPECT. ACFT GROUNDED. REMOVED NR 1 ENGINE FUEL PUMP PACKAGE REF AMM 73-11-01-000-801-F00. INSTALLED FUEL PUMP PSDR CA160107007Pump · leaking(CAN) DURING INSPECTION MAINTENANCE FOUND THE ENGINE DRIVEN FUEL PUMP WAS LEAKING AT THE LOWER AREA OF THE PUMP WHERE THE MIXTURE CONTROL SHAFT AND STOP IS. PUMP WAS REPLACED.SDR 2016FA0000268Spline · shearedSHAFT SHEARED ON TAKEOFF. PUMP SEIZED. DRIVE SHAFT SPLINE SHEARED.SDR SIMA20160105004Pump · unknownTAKEOFF 1, AFTER THRUST WAS SET, RECEIVED AN E1 FUEL LOW PRESSURE EICAS MSG, WITH ASSOCIATED RELAYS CLICKING CYCLING THE FUEL PUMPS. NR 1 ENG WAS ON PUMP C. ABORT BELOW 80 KTS HIGH SPEED. E1 FUEL LOW PRESS WITH PUMP 1C SELECTED. 1C FUEL PUMP & LOW PRESS WASDR CA151229004Coupling · failed(CAN) DURING TAKEOFF THE ENGINE HAD A LOSS OF TORQUE FROM 1800FT.LBS TO 1000FT.LBS APPROXIMATELY. THEN THE PILOT CONTINUE WITH THE MANEUVERS AND LANDED WITHOUT INCIDENT. DURING REPLACEMENT OF THE FCU AND FUEL, THE MAINTENANCE CREW FOUND THAT THE COUPLING BETSDR K11A2015122172001O-Ring · leakingFUEL LEAKING FROM NR 3 ENGINE FUEL PUMP, INSPECTED AND FOUND O-RING WAS BAD, REPLACED O-RING WITH NEW, LEAK AND OP'S CHECK GOOD. NO OTHER DEFECTS NOTED.SDR CA151229018Pump · failed(CAN) PILOTS REPORTED LT ENGINE THRUST UNCOMMANDED, REDUCED TO ABOUT 86.5 PERCENT N1 THEN WENT BACK TO T/O THRUST BY ITSELF ON T/O ROLL. FF WENT TO OVER 3000 KG/MNTS. BASED ON PREVIOUS EXPERIENCE, MAINTENANCE SUSPECTED LT ENGINE FUEL PUMP AT FAULT. AFFECTEDSDR CA151229003Shaft · fractured(CAN) THE OPERATOR REPORTED TO MFG AN IFSD DUE TO A FUEL PUMP INPUT DRIVE SHAFT FRACTURE. THE FUEL PUMP IS REPORTEDLY ZERO TIME SINCE THE LAST SHOP REPAIR . THE PUMP IS STILL UNDER INVESTIGATION AND THE PARTS HAVE BEEN PUT INTO QUARANTINE UNTIL OUR DCAA HAVESDR SIMA20151212001Fmu · failedAT FL 350 NR 2 ENG SURGED BY INCREASING & DECREASING N1 & N2 RPM'S. NO ITT LIMITS WERE EXCEEDED. EICAS CHECK MSG ON BOTH MFD'S WHILE ENG WAS SURGING. THE ACFT YAWED & HAD TO BE TRIMMED AFTER APPROX 5 MINS. THE NR 2 ENG WAS NORMAL, WITH NO MSGS NOTED. ALL SDR CA151214017Pump · low pressure(CAN) ENGINE DRIVEN FUEL PUMP FAILURE IN FLIGHT. LOW PRESSURE WARNING LIGHT ACTIVATED. PILOT ACTIVATED MANUAL FUEL PUMP.SDR 2015FA0000638Pump · malfunctionedDURING A CIRRUS PROGRESSIVE INSPECTION PROGRAM PHASE 2 INSPECTION DISCOVERED ENGINE FUEL FLOW TO BE 15.7 GALLONS PER HOUR. THE PUMP WAS REPLACED.SDR SWAA2015113046483Pump · faultyINFLIGHT SHUTDOWN & DECLARED EMERGENCY. NR 1 ENG FAIL MESSAGE ON EGT INDICATION ON DESCENT. R & R FUEL PUMP IAW MT.SDR DXTA2015111306129Pump · failedDURING TAKEOFF THROUGH 3000 FEET WITH THROTTLE IN TAKE OFF, THE RT ENGINE N2 WENT TO 102 & INDICATED RED. THE FLYING PILOT FELT A POWER BUMP & THEN SLOWLY RETARDED THE RT ENG TO IDLE. THE ITT ON THE RT ENG SLOWLY SURGED BETWEEN AROUND 500 & 700 DEGREES A COUSDR AALA201511109028Pump · defectiveNUMBER 2 ENG FAILED & SHUTDOWN ON TAKEOFF ROLL. STATUS MSG, RT ENG LOW PRESS PUMP. REPLACED THE RT ENG FUEL FLOW GOVERNOR & HIGH PRESS FUEL PUMP. ACCOMPLISHED SATISFACTORY LEAK & OPERATIONAL CHECKS. SEE AALA201511109005 FOR ADDITIONAL PART INFORMATION.SDR CG9S2015FA0000550Pump · malfunctionedDURING A CIRRUS PROGRESSIVE INSPECTION PROGRAM, PHASE 2 INSPECTION DISCOVERED ENGINE FUEL FLOW TO BE 13.8 GALLONS PER HOUR. THIS ACFT HAD BEEN FLOWN AN UNDERMINED NUMBER OF FLIGHTS WITH THE FUEL FLOW LOW. THIS RESULTED IN STUCK EXHAUST VALVES IN CYLINDERS NRSDR 2015FA0000546Pump · low pressurePILOT REPORTED LOW FUEL FLOW ON CLIMB OUT IN THE RANGE OF 13.4 TO 13.6 GALLON 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. WHEN THE ALTITUDE SDR ASOA20151102064Pump · faultedTHE CREW REPORTED NR 2 ENGINE UNCOMMANDED SHUTDOWN. MAINTENANCE REPLACED THE NR 2 ENGINE FUEL PUMP AND METERING UNIT. OPS CHECKS WERE GOOD.SDR YAXA2015110202Pump · leakingWHILE REPLACING A FAULTY MAGNETO, THE ENG DRIVEN FUEL PUMP WAS OBSERVED TO BE LEAKING FUEL FROM THE SEAL CAVITY, WHEN TURNING THE FUEL BOOST PUMP ON OR OFF, BUT NOT DURING RUNNING. THIS IS THE 3RD OCCURRENCE WE HAVE HAD OF SIMILAR LEAKAGE IN 3300 ENG HOURS. SDR 2015FA0000547Pump · low pressurePILOTS REPORTED LOW FUEL FLOW ON CLIMBOUT IN THE RANGE OF 14 GALLONS IAW HOUR. ESTABLISHED AN OPERATIONAL MINIMUM FUEL FLOW OF 16.0 GALLONS PER HOUR DUE TO OUR EXPERIENCE WITH THESE ENGINE DRIVEN FUEL PUMP ANEROID FAILURES. WHEN THE ALTITUDE COMPENSATING ANESDR JIKA201602230001Pump · malfunctionedTHE ENG OVERHAUL SHOP PERFORMED A COMPLETE TEAR DOWN & EVALUATION OF THE ENG DUE TO METAL IN THE OIL FILTER. TEAR DOWN REPORT SHOWED NO VISIBLE CAUSE FOR THE METAL IN THE FILTER. ALL INTERNAL COMPONENTS WERE SATISFACTORY. REASSEMBLED ENG. DURING TEST CELL SDR TIMA20151015006Gear Set · strippedDURING CRUISE CLIMB AT APPROX 9000 FT, THE LT ENG SUDDENLY LOST ALL POWER. ACFT RETURNED TO DEPARTURE LOCATION & LANDED WITHOUT INCIDENT. INSPECTION REVEALED THE LT ENG HIGH PRESS FUEL PUMP GEAR SET SPLINE WAS STRIPPED RESULTING IN FUEL PUMP FAILURE.SDR DSCR20151005001Relief Valve · fracturedDURING CRUISE PHASE OF FLIGHT, THE RT ENG EXPERIENCED LOSS OF FUEL PRESS. PILOT SHUT THE RT ENG DOWN, CONTACTED ATC & WAS DIVERTED. TECHNICIANS INSPECTED THE ENG & FOUND THE CAP HAD SEPARATED FROM THE HIGH PRESS RELIEF VLV, WHICH RESULTED IN THE LOSS OF FUELSDR 2015FA0000549Pump · malfunctionedDURING A MFG PROGRESSIVE INSPECTION PROGRAM 50 HOUR INSPECTION, DISCOVERED ENGINE FUEL FLOW TO BE 13.9 GALLONS PER HOUR. IN THIS CASE WE WERE NOT ABLE TO ADJUST THE FUEL FLOW TO WITHIN LIMITS IAW CMI SID97-3F. PUMP WAS REPLACED. WE HAVE ESTABLISHED AN OPERATISDR 2015FA0000548Pump · malfunctionedDURING A PROGRESSIVE INSPECTION PROGRAM, 50 HOUR INSPECTION, DISCOVERED ENGINE FUEL FLOW TO BE 14.4 GALLONS IAW 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 ANEROISDR CA150915004Pump · failed(CAN) WITH THE BOOSTER PUMP ON, THE ENGINE DRIVEN FUEL PUMP WAS FOUND INTERNALY LEAKING THROUGH THE PRESSURE REGULATOR DIAPHRAGM CHAMBER IN TO THE PUMP VENT LINE TO END UP IN THE INDUCTION SYSTEM. A NEW FUEL PUMP INSTALLED AND FOUND SERVICEABLE.SDR AALA201509159015Pump · defectiveDURING TAKEOFF NR 2 ENG DID NOT GEN PROPER THRUST. 1.53 EPR ON NR 1, 1.29 EPR ON NR 2 REJECT AT 55 KTS. NR 2 ENG LP & HP FUEL PUMP REPLACED IAW 73-12-41. FMU REPLACED IAW 73-22-52. FCOC REPLACED IAW 79-21-43. FUEL DIVERTER VLV REPLACED IAW 73-13-42. ALL SDR AALA201509149010Pump · 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
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