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 UALA2013021800979Gasket · defectiveNR 2 ENGINE LEAKING FUEL FROM ENGINE FUEL PUMP. REPLACED GASKET ON FM10 TUBE. RAN ENGINE-NO LEAKS NOTED. NR 2 ENGINE FUEL FLOW TRANSMITTER REPLACED. NEED TO ACCOMPLISH LEAK AND OP CHECK PER MM. ACP'D LEAK CHECK. NO LEAKS NOTED.SDR CA130225007Pump · leaking(CAN) CUSTOMER CALLED TO REPORT A STATIC FUEL LEAK FROM THE HIGH PRESSURE PUMP DRAIN. CUSTOMER IS LOOKING FOR TROUBLESHOOTING ASSISTANCE.SDR COEA2013020801779Pump · malfunctionedUNCOMMANDED ENGINE ACCELERATION PDX FLT 7671 ON SHORT FINAL FOR RUNWAY 3 IN PDX, THE AIRCRAFT EXPERIENCED AN UNCOMMANDED ENGINE ACCELERATION. THE ENGINE WAS SHUT DOWN IN FLIGHT AND THE AIRCRAFT LANDED SUCCESSFULLY. AN EMERGENCY WAS DECLARED WITH THE TOWER OSDR USAA2013020800036Pump · failedAFTER ENGINE START, ECAM SHOWED NUMBER 2 ENGINE FAIL, ENGINE THEN SHUT DOWN. REMOVED AND REPLACED NR 2 ENGINE FUEL PUMP/FILTER, BLEED VALVE PRESSURE REGULATOR AND HYDROMECHANICAL UNIT. ENGINE FUEL PUMP DETERMINED TO BE CAUSE OF FAILURE.SDR CA130212006Pump · leaking(CAN) A FUEL LEAK AT THE ECOLOGY TANK WAS NOTICED. A LEAK WAS ALSO OBSERVED COMING FROM THE INTERFACE BETWEEN THE FUEL PUMP AND FUEL CONTROL UNIT. THE LEAK RATE WAS INCREASED BY INCREASING THE POWER DURING GROUND RUN TESTS. THE CUSTOMER WILL REPLACE THE FUESDR SIMA20130124009Pump · malfunctionedON FLIGHT 9806 THE CREW REPORTED THE ENGINE NR 2 PULSING ON DESCENT THROUGH 11,000 RETURNED TO NORMAL ON LEVEL OFF OCCURED AGAIN ON APPROACH. THE CREW DECLARED AN EMERGECNY AND LANDED WITHOUT INCIDNET. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPSDR REXA2013012100168Packing · damagedON FLIGHT 3774 DTW TO LAN ENGINE FLAMEOUT ON LANDING ROLLOUT. WHILE TRYING TO DEPLOY RIGHT THRUST REVERSER THE THRUST REVERSER DID NOT DEPLOY AND AT THE TIME NOTICED THE ENGINE HAD A FLAMEOUT. SECONDS LATER RIGHT ENGINE OIL PRESSURE SHOWED UP ON CD NR 1. PESDR CA130124026Pump · failed(CAN) REPORTED THAT AN ACFT OPERATING AS DA351 ON A IFR FLIGHT DECLARED AN EMERGENCY AT 2330Z DUE LT ENGINE FAILURE APPROXIMATELY 20NM SOUTH INBOUND TO DESTINATION. EMERGENCY CONTINGENCIES WERE PUT INTO EFFECT BY CARS O/C. ACFT LANDED SAFELY WITHOUT INCIDENT ASDR CA130116014Pump · shorted(CAN) FUEL PUMP CIRCUIT BREAKER/SWITCH TRIPPED DURING FLIGHT. ATTEMPTS TO RESET RESULTED IN SMOKE AND FUMES IN THE COCKPIT FROM THE SWITCH. MAINTENANCE DISCOVERED A DEAD SHORT IN THE FUEL PUMP. THE CIRCUIT BREAKER/SWITCH WAS DAMAGED FROM THE REPEATED RESET SDR CA130207001Drive Shaft · worn(CAN) ENGINE REMOVED FOR O/H AT OWNER`S REQUEST. ENGINE IN SERVICABLE CONDITION AT TIME OF REMOVAL. ENGINE DRIVEN FUEL PUMP REMOVED AND DRIVE SHAFT SPLINES FOUND TO BE SEVERLY WORN. DRIVE PROBABLY WOULD HAVE FAILED WITHIN NEXT 50 TO 100 HRS OF OPERATION.SDR USAA2012123100014Pump · faultyAT THE TOP OF DESCENT, CREW REPORTED NR 1 ENGINE HAD A STRONG VIBRATION FOLLOWED BY A COMPRESSOR VANE FAULT AND ENGINE FAIL MESSAGE. CREW SHUT DOWN THE ENGINE AND DECLARED AN EMERGENCY, LANDING IN SFO WITHOUT INCIDENT. SINGLE ENGINE TIME WAS APPROXIMATELY 20SDR CA121219009Drain Line · missing(CAN) DURING INSPECTION, THE LT ENGINE WAS FOUND TO BE MISSING DRAIN LINES FROM THE FUEL PUMP AND THE HYDRAULIC PUMP. NEW DRAIN LINES INSTALLED, DEFECT RECTIFIED.SDR USAA2012111600012Pump · failedTHE RIGHT ENGINE FLAMED OUT ON DESCENT INTO CLT. R ENG SPEED CARD (EICAS). AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. REPLACED THE RT ENGINE MAIN ENGINE CONTROL, FUEL PUMP, CIT SENSOR, T2 SENSOR, AND N1 SENSOR. MAIN ENGINE CONSDR QMLA2012111312179Pump · crackedON POST FLIGHT, NOTICE FUEL ODOR, OPEN ENIGNE COWLING NOTICED FUEL LEAKING FROM HMU ASSY. THERE ARE TWO CRACKS ON FUEL PUMP HOUSING. LOCATED THE 5:00 IS 1.5 " IN LENGTH ON THE IN SERVICE PORT LOCATED AT THE 6:00 RT ABOVE THE DRAIN PORT LENGTH IS 1.0".SDR ASAA2012110893282Pump · leakingDURING NR 1 ENGINE TEST 3A IDLE LEAK CHECK FOUND FUEL PUMP PAD DRAIN LEAKING AT RATE OF 25 DROPS PER MIN. R & R NR 1 ENGINE FUEL PUMP REF MM 73-11-01-400-801-F00, STEPS 3.G. THRU 3.I.(3). COMPLETED LEAK/ OPS GROUND VERIFICATION CHECKS. NO LEAKS NOTED. REF MMSDR CA121115011Pump · leaking(CAN) DURING ACFT 100 HOUR INSPECTION, OIL WAS FOUND TO BE LEAKING FROM THE FUEL PUMP DUE TO DETERIORATION OF THE DIAPHRAM. FUEL PUMP RELACED.SDR CA121106006Pump · leaking(CAN) ENGINE DRIVEN FUEL PUMP FOUND LEAKING DURING ACFT MAINTENANCE. FUEL PUMP REPLACED.SDR IPXA12676105Pump · crackedON T/O LEFT ENGINE STARTED SURGING. NO EICAS INDICATIONS. STATUS MESSAGE LT ENGINE ANALOG N2 EICAS DISAGREE LT ENG CONTROL HIGH OIL TEMP INDICATIONS AND LOW OIL PRESSURE. AIR TURN BACK INFLIGHT SHUTDOWN OF LEFT ENGINE. OPEN.SDR CA121031004Pump · leaking(CAN) NAVY BLUE DYE FLUID FOUND ON AFTERNOON WALK AROUND. BLUE FLUID COULD BE SEEN ON LT SIDE OF FCU. STARTER GENERATOR HAS A LINE WITH BLUE ON IT. LOWER COWLING HAS BLUE FLUID ON IT. ON MORNING WALK AROUND ALL ENGINE COWLINGS & ENGINE COMPONENTS WHERE CLEASDR JJBA20121022005Pump · malfunctionedDURING CLIMB CREW REPORTED THE NR 2 ENGINE WAS SURGING CAUSING THE ACFT TO YAW DURING THE SURGING. DECLARED AN EMERGENCY AND RETURNED THE FIELD. GROUND MX WAS ABLE TO REPRODUCE THE ISSUE ON THE GROUND. R & R THE MFC AND THE HP FUEL PUMP. AN OPS CHECK PRODUSDR 2012FA0000716Pump · leakingPILOT WROTE-UP "FUEL FLOW METER INOP" DURING INITIAL START-UP. FOUND NO OR VERY LOW FUEL FLOW INDICATION AT IDLE BUT ENGINE RAN NORMAL, FOUND NORMAL FUEL FLOW INDICATION AT MID TO HIGH POWER SETTINGS WITH ENGINE RUNNING NORMALLY. FOUND GAUGE TO BEOPERATING PROSDR UALA2012101005759Pump · leakingNR 1 ENG FUEL LEAKING BETWEEN FUEL PUMP AND FMU AT SIX O'CLOCK POSITION. WHILE PERFORMING ENG RUNS OFF OF A-13 CHECK FOUND FUEL LEAK NUMBER 1 ENGINE BETWEEN FUEL CONTROL AND PUMP. R & R NR 1 ENG FUEL PUMP PER MM. REPLACED NR 1 ENG FUEL PUMP PER MM UP STEP G2SDR 2012FA0000709Pump · out of toleranceENGINE DRIVEN MECHANICAL FUEL PUMP WOULD NOT DELIVER ADEQUATE FUEL FLOW AFTER ADJUSTMENT.SDR CA120924006Pump · failed(CAN) RIGHT ENGINE FLAMED OUT APPROXIMATLEY 40 MILES FROM RUNWAY. LANDING WAS CARRIED OUT WITHOUT INCIDENT. TROUBLESHOOTING REVEALED FAILURE OF ENGINE INTERNAL DRIVE FOR FUEL PUMP. ON APPROACH TO AIRPORT THE RT ENGINE FAILED. WE ELECTED TO SHUT THE ENGINE SDR CA120924012Pump · unserviceable(CAN) WHILE ACFT WAS CARRYING OUT A LOCAL TRAINING FLIGHT, THE LT ENGINE EXPERIENCED A TOTAL SHUTDOWN WITH PROPELLER FEATHERING. THE FOLLOWING SYSTEMS ALSO FAILED, LOSS OF INDICATIONS FOR BOTH ENGINES, BOTH ATTITUDE INDICATORS, BOTH HS AND BOTH INVERTERS, THESDR CA120829008Warning Light · illuminated(CAN) ELECTRIC FUEL PUMP RUN LIGHT REMAINS ON AFTER ENGINE START. LIGHT EXTINGUISHES WHEN PROP COMES OUT OF FEATHER.SDR 9PVA2012F00176Pump · defectiveAFTER LEVEL OFF AT FL380 AND APPROX 18 MINUTES INTO THE FLIGHT THE "ENG 1 FUEL" CAUTION LIGHT ON THE OVERHEAD PANEL ILLUMINATED, INDICATING "EITHER FUEL FILTER BLOCKED OR FUEL OVERHEAT" IAW THE AIRPLANE FLIGHT MANUAL THE NR 1 ENGINE THRUST LEVER WAS REDUCED TOSDR JIKA2012082701Pump · failedWHEN SWITCHING OFF EMERGENCY BOOST PUMP DURING CLIMB, LEFT ENGINE FUEL PRESSURE DROPPED TO 10, AND ENGINE SPUTTERED. PILOT TURNED BOOST PUMP BACK ON AND ENGINE RECOVERED. PILOT RETURNED TO MX BASE. MAINTENANCE TROUBLESHOT AIRCRAFT SYSTEM, REPLACED LEFT ENGISDR 2012FA0000707Pump · out of toleranceENGINE DRIVEN MECHANICAL FUEL PUMP WILL NOT OUTPUT HIGHER THAN 13 GPH AFTER ADJUSTMENT. OUTPUT SHOULD BE IN THE 17 - 18 GPH RANGE.SDR 2012FA0000706Pump · out of toleranceENGINE DRIVEN MECHANICAL FUEL PUMP WILL NOT OUTPUT HIGHER THAN 14.3 GPH AT WIDE OPEN THROTTLE AFTER ADJUSTMENT. SHOULD BE IN THE 17 - 18 GPH RANGE.SDR CA120912010Shaft · sheared(CAN) REPORTED THAT THEY HAVE RECEIVED A FUEL PUMP WITH A SHEARED DRIVE SHAFT SPLINES. THIS PUMP WAS INTRODUCED BY CEB 73-3117 AND WAS MEANT TO ELIMINATE THE REQUIREMENT FOR THE RECURRING INSPECTION.SDR 2012FA0000708Pump · out of toleranceENGINE DRIVEN MECHANICAL FUEL PUMP WILL ONLY OUTPUT 10.5 GPH AT WIDE OPEN THROTTLE AFTER ADJUSTMENT. OUTPUT SHOULD BE IN THE 17-18 GPH RANGE.SDR UALA2012062903435Helicoil · failedWHEN REMOVING IDG OIL-FUEL HEAT EXCHANGER TUBE SEAL FOR INSPECTION THE ATTACHMENT BOLT HELICOIL CAME OFF FROM THE MAIN FUEL PUMP. REPLACED LEFT FUEL PUMP AS PER A MM 73-11-01. ACCOMPLISHED ENG WET MOTOR AND IDLE LEAK TEST PER AMM 71-00-00, NO FAULT FOUND.SDR 2012FA0000705Pump · out of toleranceENGINE DRIVEN MECHANICAL FUEL PUMP WILL ONLY DELIVER 13 GPH AT WIDE OPEN THROTTLE AFTER ADJUSTMENT. CORRECT OUTPUT SHOULD BE IN THE RANGE OF 17 - 18 GPH.SDR SIMA20120610007Pump · shutdownFLIGHT 4050 - ON ARRIVAL AT GATE WITH NR 2 ENGINE RUNNING, PARKING BRAKE ON, NO APU OR GPU, HAD NR 2 ENGINE FLAMEOUT, SHUTDOWN UNCOMMANDED WITH ECAS MESSAGE. AIRCRAFT REMOVED FROM SERVICE. PERFORMED CMC AND FDR DOWNLOAD, FOUND THAT NR 2 ENGINE FUEL PUMPSDR UALA2012060803129Pump · faultyRIGHT ENGINE FLAMEOUT DESCENDING THROUGH 180. RESTARTED ON ITS OWN PASSING 150. AFTER FDR INFO HAS BEEN EVALUATED, ACCOMPLISH ENGINE FLAMEOUT FIM 73-21-00. DUE TO RIGHT ENGINE FLAME OUT & R ENG FUEL VALVE LIGHT ON ACCOMPLISH FIM. ACCMP'D FIM-76-11-00 FIG 1SDR CA120604008Pump · leaking(CAN) LOW PRESSURE ENGINE DRIVEN FUEL PUMP FOUND LEAKING FROM TELL TALE DRAIN. FUEL RESIDUE FOUND ON LOWER FIREWALL AND LT BATTERY BOX.SDR CA120601005Pump · failed(CAN) FUEL PUMP WAS FAILED OUT OF THE BOX. THE PUMP CREATED ZERO FUEL PRESSURE.SDR REXA2012051600742Pump · leakingFUEL DRIPPING OUT OF LEFT ENGINE EXESSIVELY, LARGE PUDDLE ON THE GROUND. REMOVED AND REPLACED LEFT ENGINE FUEL PUMP IAW AMM 73-11-01. OPS CHECK AND LEAK CHECK GOOD. OK FOR SERVICE.SDR CA120515005Pump · leaking(CAN) DURING INSPECTION FOUND FUEL PUMP DRIVE SEAL LEAKING. THE DRIVE CAVITY DRAIN LINE IS ROUTED ABOVE THE HEIGHT OF FUEL PUMP CAVITY DRAIN OUTLET PREVENTING LEAKING FUEL FROM DRAINING FROM THE CAVITY AND CAUSING FLOODING OF THE PUMP MOTOR.SDR 2012FA0000290Seal · leakingFUEL LEAKING PAST MIXTURE CONTROL SHAFT SEALS. ACFT AND ENGINE HAS A TURBO NORMALIZING SYS INSTALLED. WHEN ELECTRIC FUEL PUMP OPERATED ON BOOST (LOW), ENGINE DRIVEN FUEL PUMP HAD A LEAKAGE RATE OF FUEL OF ABOUT 1 DRIP EVERY 1.5 TO 2 SECONDS.SDR CA120510007Pump · leaking(CAN) DURING 50 HR INSPECTION, THE ENGINE DRIVEN FUEL PUMP WAS FOUND TO BE LEAKING. FUEL PUMP REPLACED.SDR 2012FA0000318Pump · leakingDURING AN ANNUAL INSPECTION, THE ENGINE DRIVEN FUEL PUMP WAS FOUND TO BE LEAKING FUEL FROM THE RELIEF VALVE GASKET. FUEL WAS ALSO FOUND IN THE UPPER DECK PRESSURE LINES AT THE PUMP. SB REFERENCES THE EXACT SAME PROBLEM AND INCLUDES THE MODEL NR OF THIS PUMPSDR 2012FA0000242Housing · wrong partFUEL PUMP WAS RECEIVED FOR A FUNCTIONAL TEST DUE TO POOR OPERATION BELOW 1400 RPM WITH THE BOOST PUMP TURNED ON. WHEN TESTED, THE FUEL PRESSURE WAS SET 10 PSI LOW AND TEST FLUID WAS NOTICED LEAKING FROM THE UPPER DECK REF PORT OF THE PUMP RELIEF VALVE COVER. SDR CALA2012040900246Packing · leakingFOUND FUEL LEAKING FROM LT ENGINE FUEL PUMP STRAINER. REMOVED AND REPLACED THE FUEL PUMP STRAINER PACKING IAW AMM 73- 11-04. ENG RUN ACCOMPLISHED PER AMM 71-00-00, NO LEAKING NOTED.SDR UALA2012040902156Pump · out of toleranceFUEL PUMP NR 2 MALFUNCTIONED. REPLACED MAIN FUEL PUMP PER MM. OPS & LEAK CHECKED OK.SDR CA120410007O-Ring · leaking(CAN) FOUND FUEL LEAKING FROM THE ENGINE FUEL PUMP DISCHARGE FILTER COVER, IT WAS A RESULT OF THE PACKING, PN: M25988-1-928, "BLOWN " OUT OF ITS SEALING AREA. THE FUEL PUMP, DISCHARGE FILTER COVER WAS INSTALLED AND TORQUED IAW MM, PN 3021242, DATED APRIL 03,SDR UALA2012040502122Pump · lack of lubeFUEL PUMP HAS LACK OF LUBRICATION. PUMP REMOVED AND INSTALLED NEW PUMP. LEAK CHECKED AND RUNS GOOD.SDR CA120423023Pump · inoperative(CAN) AUX FUEL PUMP INOPERATIVE. AUXILIARY FUEL PUMP REPLACED.SDR LD2R20120403001Adapter · backed outWHILE PERFORMING A SERVICE BULLITIN TO REPLACE THE FUEL PUMP SPLINE ADAPTER, WE FOUND THE ENGINE DRIVEN FUEL PUMP DRIVE SHAFT TO BE MIGRATING OUT OF THE FUEL PUMP AND INTO THE ACCESSORY GEAR CASE. UPON INSPECTION OF THE GEAR CASE WE FOUND A RETAINING PLUG IN
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