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 CA120321010Nut · loose(CAN) DIAPHRAM LEAKING AT PLUNGER NUT. NUT FOUND LOOSE.SDR ASMF20120307002Pump · leakingDURING TRANSIT CHECK, A FUEL LEAK DETECTED IN THE RT ENGINE. MX PERSONNEL DETECTED THE LEAK BETWEEN FUEL PUMP AND GEAR BOX, FOUND OUT OF ITS OPERATIONAL LIMITS IAW MM 73-11-00; FUEL PUMP WAS REPLACED IAW MM 73-11-01, TESTED CORRECT.SDR ESMR2012022801Pump · leakingACFT WAS INBOUND WHEN THE ENGINE BEGAN TO LOOSE POWER. THE PILOT USED THE FUEL BOOST PUMP TO KEEP THE ENGINE RUNNING AND LANDED WITHOUT INCIDENT. THE ENGINE RAN FINE AT IDLE ON THE GROUND. WITH THE ENGINE OFF AND THE FUEL SELECTOR TURNED ON, FUEL WAS RUNNINGSDR CA120213002Pump · malfunctioned(CAN) PILOTS REPORTED THAT THEY HAD THE LT & RT CHECK EDS, CAS MESSAGE COME ON DURING TAXI. MAINTENANCE DOWNLOADED BOTH ENGINE COMPUTERS AND FOUND THAT BOTH ENGINES LOGGED AN UNCOMMANDED SHUTDOWN AT DIFFERENT TIMES DURING THE TAXI. THE CREW DID NOT NOTICE ANSDR CA120408002Pump · failed(CAN) AUXILIARY FUEL PUMP WARNING LIGHT CAME ON IN FLIGHT. AUXILIARY FUEL PUMP REPLACED.SDR O2MA20120207001Pump · faultyDURING THE APPROACH THE LT ENGINE FLAMED OUT WHEN THE THROTTLE LEVER WAS RETARDED TOWARDS FLIGHT IDLE. THE PIC DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED WITH NO INCIDENT. THE LT ENGINE WAS NEVER ATTEMPTED TO BE RESTARTED DURING THE APPROACH. ATTEMPTS WESDR UALA2012020600724Pump · unknownNR 2 ENG FUEL PUMP REPLACEMENT.SDR UALA2012013000582Pump · faultyENG PARAMETERS FLUCTUATING IN CRUISE. DISCUSSED WITH ENG CONTROLLER REPLACE FCU AND FUEL PUMP. REMOVED FUEL CONTROL. STARTED TO REMOVE FUEL PUMP PER MM. FUEL PUMP JUST NEEDS ATTACH BOLTS LOOSENED TO BE REMOVED. REPLACED NR 1 ENGINE FUEL PUMP PER MM. CHANSDR USAA2012011700023Pump · failedENGINE NR 2 MOMENTARILY FAILED DURING IDLE DESCENT AT FL200, 280 KNOTS. CREW FELT AIRCRAFT YAW AND REPORTED N2 AT APPROXIMATELY 30 PERCENT. UPON IGNITION ACTIVATION, ENGINE RELIT ITSELF AND CONTINUED TO OPERATE NORMALLY. MAINTENANCE REMOVED AND REPLACED THESDR 2012FA0000024Housing · galledENGINE DIED ON INITIAL RUN-UP DUE TO FUEL STARVATION. FOUND GALLING BETWEEN FUEL PUMP DRIVE GEAR AND HOUSING. CAUSE UNDETERMINED. SENT BOTH PARTS OUT FOR O/H.SDR USAA2011122700034Pump · failedAFTER ENGINE START, AND POSSIBLY DURING POWER CHANGE OVER, NR 2 ENGINE FAILURE ECAM MESSAGE WITH AUTO SHUTDOWN OF NR 2 ENGINE. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE HYDRO-MECHANICAL UNIT AND FUEL PUMP/FILTER ASSEMBLY IAW AIRBUS MAINTENANCE MANUAL 73-11SDR SWAA20111212468Pump · faultyDIVERSION -- AT CRUISE N1 82 PERCENT - 84 PERCENT ENGINE NR 2 FLUCTUATES 0.3 PERCENT ALL OTHER PARAMETERS FOLLOW. REMOVED AND REPLACED FUEL PUMP AND MEC PER MT.SDR UALA2011121206826Pump · leakingNR 1 ENGINE HAS FUEL POURING FROM FUEL PUMP, ACFT RTB. REMOVED & REPLACED FUEL CONTROL & FUEL PUMP.SDR ASAA11510743Pump · leakingAFTER PUSHBACK AND ENGINE START ANOTHER AIRCRAFT REPORTED SUBSTANTIAL AMOUNT OF FUEL STREAMING FROM NR 1 ENGINE. SHORTLY THEREAFTER A STRONG ODOR OF RAW FUEL WAS PRESENT IN THE CABIN AND FLIGHT DECK. FUEL AT IDLE INDICATED .84 ON NR 1 ENGINE AND .80 ON NR 2 SDR CA111117010Pump · unserviceable(CAN) LT ENGINE NOT GOING PAST 30 PERCENT NG ON START. THIS WAS AN INTERMITTENT SNAG ON FIRST START OF DAY WOULD BE DIFFICULT TO START THEN WOULD HAVE NO ISSUES. AFTER SOME TROUBLESHOOTING THAT DID NOT FIX THE ISSUE, THE LT ENGINE HIGH PRESSURE FUEL PUMP WAS SDR K11A2011111572601Pump · shearedENGINE NR 1 FLAME OUT DURING TAKEOFF AT 80 KNOTS, ALL PARAMETERS WERE NORMAL UNTIL FLAME OUT OCCURED. CREW ADVICED TOWER CLEARED RUNWAY AND RETURNED BACK TO BLOCKS. REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP AND DISCOVERED THE SHAFT SHEARED OFF. PERFORMED LSDR CA111115009Pump · leaking(CAN) DURING PRE-FLIGHT INSPECTION AN OIL LEAK WAS OBSERVED ON THE RT SIDE BY THE PILOT. AFTER INVESTIGATION THE MECHANICAL GAS PUMP WAS REPLACED. RUN UP WAS PERFORMED, NO LEAKAGE.SDR CA111115008Pump · leaking(CAN) RT ENG POWER LOSS. FOUND OIL LEAK FROM THE DRAIN ON CROSS FEED LT PUMP. PUMP HAS BEEN REPLACED. 2 ENGS RUNNING & RETURNED TO SERVICE. NO PROBLEMS TO REPORT.SDR CA111128004Pump · inoperative(CAN) AUXILIARY FUEL PUMP NOT WORKING. REPLACE AUXILIARY FUEL PUMP.SDR CA111128003Pump · leaking(CAN) OIL LEAKING FROM ENGINE DRIVEN FUEL PUMP. FUEL PUMP REPLACED.SDR CA111207004Pump · noisy(CAN) AUXILIARY FUEL PUMP NOISY DURING PRIME. FUEL PUMP REPLACED.SDR ASMF201110004Pump · leakingDURING TRANSIT CHECK, A FUEL LEAK IN THE RT ENGINE WITH 60 DROPS PER MINUTE. MX PERSONNEL PERFORMED REVISION DETECTING THE RT FUEL PUMP WITH LEAK WITHIN OPERATION LIMITS IAW MM 71-71-00 DISPATCHING THE ACFT IN SUCH CONDITION. MX PERSONNEL REPLACED THE RT FUELSDR GLBA20111017GPump · leaking"SUP" -MX REPORTED THAT THE LT HP FUEL PUMP WAS LEAKING. MX REPLACED THE FCU, OPS CK GOOD.SDR CA111004007Pressure Switch · failed(CAN) CREW REPORTED THEY HAD NR 1 ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED. ENGINE OPERATION WAS NORMAL AND THE ACFT DIVERTED TO LANDING UNEVENTFULLY. IN MX DRAINED FUEL FROM THE PUMP HOUSING DRAIN PLUG, FOUND FREE OF VISIBLE, GROSS CONTAMINATION. THE FUESDR CA110928014Pump · noise(CAN) AUXILIARY FUEL PUMP MAKING GROWLING NOISE DURING GROUND RUN FOLLOWING 50 HR INSPECTION AUXILIARY FUEL PUMP REPLACED.SDR ASAA11510323Pump · leakingNR 2 ENGINE HAS HISTORY OF FUEL PUDDLING ON GROUND DURING ENGINE START. BAGGED FUEL & VENT DRAIN LINES ON NR 2 ENGINE & RAN AFTER 3 HR WAIT AFTER START HAD CONTINUOUS FUEL FLOW FROM PUMP PAD DRAIN UNTIL SHUTDOWN REF MM 71 71 00. REPLACED FUEL PUMP PACKAGE ASSDR CA110922012Pump · failed(CAN) AUXILIARY FUEL PUMP WARNING LIGHT ACTIVATED. MAINTENANCE CONFIRMED AUXILIARY FUEL PUMP UNSERVICEABLE. AUXILIARY FUEL PUMP REPLACED.SDR AALA20110825TUL07Pump · brokenBAQ - INFLIGHT VVI-MIA. CREW REPORTED LEFT ENGINE LOW PRESSURE PUMP MESSAGE WITH A LOSS OF ENGINE POWER. LEFT ENGINE WAS SHUTDOWN (SINGLE ENGINE TIME 20 MINS). EMERGENCY DECLARED FLIGHT DIVERTED BAQ LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. SDR GLBA20110822JPump · leakingPILOT REPORTED THAT THERE IS A FUEL LEAK FROM THE HIGH PRESSURE FUEL PUMP DRAIN ON THE LEFT ENGINE. MX REPLACED THE LEFT HIGH PRESSURE FUEL PUMP IAW 73-10-02 AND THE FCU IAW TC. 1900-7320.00, OK FOR SERVICE.SDR TXHA20110818001Shaft · shearedON TAKEOFF ROLL THE LT ENGINE FLAMED OUT, PILOT ABORTED TAKEOFF NO FURTHER INCIDENT, RETURNED TO BLOCK. INVESTIGATION BY MX FOUND THE LT FUEL PUMP SHAFT SHEARED.SDR CA110829010Pump · leaking(CAN) ENGINE DRIVEN FUEL PUMP FOUND LEAKING OIL DURING 50 HR INSPECTION. FUEL PUMP REPLACED.SDR SF3R20110819001Metering Unit · failedSERVO VALVE (PN 22282790-104) NONCONFORMITY IS THE LASER WELD JOINING THE FEEDBACK WIRE (FBW) TO THE FEEDBACK SPRING IS MISALIGNED WITH THE WELD JOINT. THE FAILURE MODE IS THAT THE FEEDBACK WIRE WELD JOINT CAN BREAK. THE FAILURE EFFECT AT SERVO LEVEL IS LOSSSDR CA110812005Pump · failedFUEL PUMP WAS INSTALLED TO REPLACE ANOTHER PUMP WITH LOW IDLE PRESSURE. ON STARTUP FOR GROUND TEST, IT WAS NOTICED THAT THE PUMP HAD ZERO OUTPUT. ON REMOVAL FOR REPLACEMENT, IT WAS NOTED THAT THE DRIVE SHAFT WAS SHEARED. IT WAS THEN NOTICED THAT THE FITTING SDR CA110811007Pump · malfunctionedFUEL PUMP WAS INSTALLED TO REPLACE ANOTHER PUMP WITH LOW IDLE PRESSURE. ON STARTUP FOR GROUND TEST, IT WAS NOTICED THAT THE PUMP HAD ZERO OUTPUT. ON REMOVAL FOR REPLACEMENT, IT WAS NOTED THAT THE DRIVE SHAFT WAS SHEARED. IT WAS THEN NOTICED THAT THE FITTING SDR CA111019019Pump · unsecure(CAN) THE PILOT WAS PERFORMING AN AEROBATIC ROUTINE DURING AN AIRSHOW. WHILE PULLING THE POWER OFF TO PERFORM A TAIL SLIDE THE ENGINE QUIT. THE PILOT DECLARED A MAYDAY TO THE AIR BOSS AND MANAGED TO RESTART THE ENGINE. HE THEN CANCELLED THE REST OF HIS PERFSDR 9JLA20110801001Pump · defectiveTHE CREW REPORTED DURING CLIMBOUT THAT THE ENG 2 FUEL ANNUNCIATOR ILLUMINATED. THE FUEL FILTER HAD BEEN REPLACED 2 DAYS PRIOR WITH SATISFACTORY OPERATIONAL CHECKS. TROUBLSHOOTING FOUND THAT THE ENGINE DRIVEN FUEL PUMP WAS DEFECTIVE. P/N 3070850-57 S/N 396995SDR SWAA115523APump · faultyDECLARED EMERGENCY - ON DESCENT FROM FL 350, WITH THROTTLES AT IDLE AND N1 APPROX 60 PERCENT, NOTICED A LOUD POP AND VIBRATION COMING FROM NR 2 ENGINE, ON LEVEL OFF BOTH THROTTLES SLOWLY ADVANCED AND OPERATED NORMAL, AGAIN ON DESCENT RETARDED APPROX 60 PERCENTSDR CA110803021Pump · faultyAUX FUEL PUMP WARNING LIGHT CAME ON IN FLIGHT. AUX FUEL PUMP REPLACED.SDR 2011FA0000475Pump · failedFUEL PUMP FAILED TO HOLD ANY PRESSURE SETTINGS. SENT IN FOR WARRANTY.SDR GLBA20110719FPump · leakingPILOT REPORTED THAT FUEL WAS LEAKING FROM THE NR2 ENGINE GANG DRAIN. MX REPLACED THE NR2 ENGINE DRIVEN FUEL PUMP IAW BMM 73-10-00.SDR CA110718010Pump · failedENGINE NR 1 FUEL CAUTION ILLUMINATION DURING TAKEOFF POWER ONLY. PRIMARY EJECTOR PUMP FOUND TO AT FAULT, REPLACED.SDR ASMF201107009Pump · damagedACFT REJECTED TAKEOFF AT LESS THAN 70 KNOTS WITH GROSS WEIGHT OF 58764 KG DUE TO LEFT ENGINE NOT REACHING THRUST, 101PERCENT REQUIRED, ONLY IT REACHED 90 PERCENT THRUST WITH ATS SET AND OFF. MX PERFORMED BITE IN EEC IAW MM 73-21-00 AND BITE TO THE ATS WAS PERFSDR 2011FA0000453Pump · failedPILOT REPORTED LOW FUEL PRESSURE AT 700 RPM, 10-12 PSI. INSTALLED ANOTHER PUMP RAN ACFT OPS CHECKED OK. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME.SDR CA110621009Pump · leakingUPON STARTING THE NR 3 ENGINE, THE T5 WAS OBSERVED TO BE RISING WHILE THE NG WAS SLOW TO RISE. THE START WAS ABORTED WHEN THE T5 HIT 900 DEGREES. MX INVESTIGATED AND FOUND THAT THE FUEL PUMP WAS LEAKING AND THE FUEL WAS GOING THROUGH THE GARLOCK SEAL AND INTSDR AALA20110528DFW01Pump · failedDFW - CREW REPORTED ON APPROACH AIRCRAFT YAWED TO THE RIGHT, BOTH PACKS SHUTDOWN AND THE RIGHT ENGINE APPEARED TO QUIT PRODUCING THRUST FOR A VERY SHORT PERIOD OF TIME. FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINESDR CA110606001Drive Shaft · wornACCIDENT WAS REPORTED THAT THE CREW OF 2 HAD TO EJECT DURING A TRAINING MISSION. ACFT EXPERIENCED A SUSPECTED ENGINE FAILURE AND CRASHED APPROX 1.5 KM IN FRONT OF THE RUNWAY. AS A PRECAUTION, ALL RAAF PC-9 FLYING OPS HAVE BEEN TEMPORARILY SUSPENDED. DIRECTORSDR AALA20110502TUL09Pump · inoperativeTUL (REPEAT ITEM) CREW REPORTED DURING FUNCTIONAL CHECK FLIGHT RIGHT ENGINE FAILED TO RESTART (SINGLE ENGINE TIME 23 MIN). NO FUEL WAS DISPLAYED WITH FUEL CONTROL SWITCH IN RUN POSITION. EICAS DISPLAYED RIGHT ENGINE FUEL VALVE. EMERGENCY DECLARED FLIGHT RETUSDR IPXA11M66134Pump · inoperativeON DESCENT, GOT LEVEL 0 ENGINE RPM LO, ATTEMPTED RESTART IN FLIGHT, UNSUCCESSFUL. EMERGENCY DECLARED. R & R ENGINE DRIVEN NR 2 ENGINE FUEL PUMP IAW MM 73-12-12-01-4. ENGINE STATS & RUNS NORMAL IAW MM 71-02-03. 5 MINUTE MINIMUM IDLE POWER.SDR UALA2011041801886Pump · defectiveNR 1 ENG FUEL PUMP NEEDS TO BE OP AND LEAK CHECKED. FUEL PUMP CHANGED BY AMT. PERFORM IDLE RUN TO OPS CHK FUEL FILTER CONNECTOR NR 1 ENGINE. ACP'D FIVE MINUTE IDLE NR 1 ENGINE, OPS CHK OKAY. NO MESSAGES.SDR SWAA112754Pump · faultyINFLIGHT SHUTDOWN / DIVERSION / DECLARED EMERGENCY. WHILE CRUISING AT FL 350, THE NR 1 ENGINE FLAMED OUT. ALL ENGINE FULE PUMPS WERE ON AT THE TIME AND THE CROSSFEED VALVED WAS CLOSED. DESCENDED TO FL 230 WHERE WINDMILL AIRSTART WAS SUCCESSFUL. REMOVED AND
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