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 CA020215014Pump · leaking(CAN) OIL WAS FOUND LEAKING FROM RIGHT ENGINE DRAIN LINES. PUMP WAS REPLACED WITH NEW.SDR CA020213008Pump · making metal(CAN) NR 1 ENGINE FUEL BOOST PUMP WAS MAKING TOO MUCH NOISE AND VIBRATING AS COMPARED TO NR 2 FUEL BOOST PUMP. INSPECTED THE NR 1 ENGINE DRIVEN FUEL PUMP FILTER AND FOUND NON-FERROUS METAL IN THE FILTER. INSPECTED THE FUEL CONTROL FILTER FOR CONTAMINATION ANSDR CA020226005Pump · leaking(CAN) DURING SCHEDULED MAINTENANCE, NOTICED A DRIP OF FUEL COMING OFF OF THE ENGINE DRIVEN FUEL PUMP TO ENGINE FLANGE. WITH A CLOSER LOOK FOUND A BROWN STAIN AS WELL. REMOVED ENGINE DRIVEN FUEL PUMP ASSEMBLY AND INSPECTED. FOUND SPLINE DRIVE COUPLING WHICH ENTSDR RAIA00202048Pump · failed5538-STL- LEFT ENGINE FAILED DURING CLIMB. MAINTENANCE REMOVED AND REPLACED THE #1 ENGINE FUEL PUMP, ENGINE AND PUMP OPS AND LK CK OK.SDR 2002FA0000176Pump · failedHAD AN ENGINE FAILURE WHICH RESULTED IN THE AIRCRAFT LANDING SHORT OF THE AIRPORT. NO ONE WAS INJURED AND THE AIRCRAFT WAS NOT DAMAGED. ENGINE QUIT DUE TO ENGINE DRIVEN FUEL PUMP FAILURE. FUEL PUMP WAS REMOVED, A NEW PUMP INSTALLED, AND THE AIRCRAFT RETURNESDR CA020201013Pump · leaking(CAN) AFTER COMPLETION OF UNLOADING FREIGHT, OUR AIRCRAFT WAS REPOSITIONING TO THE MAINTENANCE FACILITY AT FBO. DURING ENGINE SHUTDOWN, AN ENGINEER FROM OUR CONTRACTED AMO NOTICED FUEL LEAKING FROM THE RIGHT ENGINE LOWER COWLING. IN ORDER TO STOP THE FUEL FROMSDR GLBA2002010Pump · failedRIGHT LOW PRESSURE FUEL LIGHT ILLUMINATED. REPLACED FUEL PUMP, OPS CHECKED SYSTEM SATISFACTORY.SDR CA020125008Seal · failed(CAN) NR 2 ENGINE LOW OIL PRESS AND QUANTITY IN CRUISE YHM-YWG.ENGINE SHUT DOWN AND AIRCRAFT RETURNED TO YHM.ENGINE INSPECTED I.A.W. PW M.M. 72-00 PAGE 664 AND FUEL PUMP MAIN CARBON SEAL REPLACED.SDR DLM88020046Pump · failedRT ENGINE SHUT DOWN TWO MINUTES INTO CLIMB, EGT WENT TO ZERO, HAD F/F AND N1AND N2. SHUT ENGINE DOWN, WINDMILLED FOR 15 MIN WITH POSITIVE OIL PRESS. REPLACED FUEL PUMP.SDR GLBA2002001Pump · failedLEFT LOW FUEL PRESSURE LIGHT ILLUMINATED. REPLACED FUEL PUMP, OPS CHECKED SYSTEM SATISFACTORY.SDR GLBA2001247Pump · failedRIGHT LOW PRESSURE FUEL LIGHT. REPLACED LOW PRESSURE FUEL PUMP, OPS CHECKED SYSTEM SATISFACTORY.SDR CA011227005Filter · failed(CAN) AFTER DEPARTURE , NR 2 FUEL PRESSURE CAUTION LIGHT ILLUMINATED, CREW UNABLE TO EXTINGUISH, AIRCRAFT RETURN TO DEPARTURE AIRPORT FOR NORMAL LANDING. NR 2 ENGINE HP FUEL FILTER REPLACED.SDR CA011219011Pump · failed(CAN) NR 3 ENGINE SPOOLED DOWN DURING T/O ROLL. T/O ABORTED AT 60 KNTS. NR 3 ENGINE FUEL PUMP RELACED. SN 4617 REMOVED.SDR VJ32002F00003Pump · leakingLEAKING FUEL FROM CASE DRAIN.SDR CA020108003Pump · stripped(CAN) ENGINE SHUT DOWN IN CRUISE FLIGHT. AIRCRAFT MADE AN UNSCHEDULED LANDING TROUBLESHOOTING REVEALED NO FUEL FLOW TO DIVIDER. HIGH PRESSURE FUEL PUMP REMOVED. FUEL PUMP SPLINES FUND TO BE STRIPPED. PUMP REPLACED.SDR CA020131008Fuel Control · failed(CAN) ON TAKEOFF ROLL NR 2 ENGINE CAUTION LIGHT FLICKERED. WERE NO ABNORMAL IND.S. AFTER TAKEOFF AT 600 FT MSL NR 2 ENGINE MANUAL CAUTION LIGHT ILLUMINATED FOLLOWED BY COMPLETE FAILURE OF NR 2 ENGINE. ENGINE AUTO-FEATHERED, ALL ENGINE PARAMETERS INDICATED ZERSDR MVI2001F00000Shaft · shearedAFTER NORMAL APPROACH WITH A GO AROUND FROM 501 AGL, FULL ENGINE POWER WAS ATTAINED ON ALL ENGINES. AT 700 FT, FE NOTED EPR ROLLBACK ON NR 3 ENGINE. ENGINE SUBSEQUENTLY WOULD NOT RESPOND TO POWER SETTINGS AND WAS SHUTDOWN. INSPECTION FOUND FUEL PUMP DRIVE SSDR KBMA112017Switch · failedFUEL PUMP FAIL LIGHT DOES NOT LIGHT UP WHEN CIRCUIT BREAKER IS PULLED. REMOVED AND REPLACED WITH NEW SWITCH.SDR CA011116014Pump · failed(CAN) DURING CLIMB AFTER TAKEOFF FROM RUNWAY 16 AT YYC WHEN THE PILOT ADJUSTED THROTTLE AND MIXTURE THE ENGINE STOPPED PRODUCING POWER. AN EMERGENCY LANDING WAS CARRIED OUT ON THE END OF RUNWAY 16.SDR WVB2001F00001Pump · leakingDURING INSPECTION IT WAS NOTICED THAT THE RIGHT FUEL PUMP WAS LEAKING AT THE BODY GASKET THE PUMP WAS REMOVED FROM SERVICE. THIS IS A M STYLE PUMP.(K)SDR 2001FA0000511Pump · leakingLEAKING FUEL FROM CASE DRAIN.SDR VJ32001F00001Pump · leakingLEAKING FUEL FROM CASE DRAIN.SDR 2001UALA02123Pump · faultyUNABLE TO DEVELOP TAKEOFF POWER ON NUMBER 2 ENGINE. REPLACED ENGINE. ENGINE WAS PLACED IN TEST CELL. FUEL PUMP OUTPUT PRESSURE WAS FOUND TO BE LOW, AT HIGH POWER SETTINGS. PUMP WAS REPLACED AND THE ENGINE DEVELOPED TAKEOFF POWER.SDR HEEA076614Pump · failedENGINE OSCILLATIONS AND SEAL LEAKING. REPLACED WITH SERVICEABLE FUEL PUMP.SDR SWIA200110237Pump · defectiveDURING CLIMB TO 16000 FT NR 2 ENGINE TORQUE FLUCTUATED THEN RAPIDLY DROPPED TO 11 PERCENT TQ. OTHER ENGINE INDICATIONS WERE NORMAL. PERFORMED PRECAUTIONARY ENGINE SHUT DOWN. REMOVED AND REPLACED RIGHT ENGINE HMU AND FUEL PUMP IAW MM 73-21-00. OPS AND LEAK CSDR AALA20011811Pump · leakingDFW - FLT 2499 - EN ROUTE SAT-DFW - UPON DESCENT, NR 1 ENGINE SHUTDOWN. LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED LOW PRESSURE FUEL PUMP. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR FPI2001F00001Pump · faultyENGINE HAD LOW POWER PROBLEM. ENGINE MAX FUEL PRESSURE WAS 26 PSI AT 2700 RPM. SPECS 28 TO 31 PSI. THE HIGH PRESSURE ADJUSTMENT WAS BOTTOMED OUT. THE FUEL PUMP WAS REMOVED AND REPLACED.SDR CA010831018Cover · loose(CAN) COVER SCREWS WERE FOUND WITH INSUFICIENT TORQUE AS PER FOCA AD HB 2001-500. COVER SCREWS WERE TORQUED TO SPECIFICATIONS AND SAFTIED AS PERSB28-009NO SIGNS OF FUEL LEAKAGE OR EXTRUDED GASKET MATERIAL WAS FOUND.SDR CA010831019Pump · leaking(CAN) INSPECTION OF THE ENGINE DRIVEN FUEL PUMP AS PER PILATUS AWD HB2001-500 AND SB 28-009 REVEALED THAT FUEL PUMP WAS LEAKING AND EXTRUDED GASKET MATERIAL WAS FOUND. THE TORQUE OF THE SCREWS WAS CHECKED. 1/8TH TO 1/4 TURNS WERE NEEDED TO TORQUE THE SCREWS TSDR WVBA2001045Pump · leakingDURING INSPECTION IT WAS NOTICED THAT THE FUEL PUMP WAS LEAKING FROM THE PARTING SURFACE AND THE PUMP BODY. THIS IS THE SIDE WITH THE LADDER SEAL TO THE PUMP BODY. THE PUMP WAS REMOVED FROM SERVICE. THIS IS A (M) STYLE PUMP.SDR DLM88011368Pump · defectiveON T/O FROM PWM DURING CLIMBOUT NR 2 ENG ROLLED BACK TO IDLE MOMENTARILY THEN WENT BACK TO CLIMB POWER THEN SHUTDOWN AT APPROX 10,000 FT. DIVERTED TO BGR. REPLACED FUEL PUMP AND CONTROL.SDR SABA010043Fuel Control · inoperativeAircraft 963 on lfight 5136 from LYH to CLT. During takeoff roll the right engine fuel pressure warning light came on. The takeoff was aboorted. No emergency was declared and no emergency proecdures were used. Aircraft returned to the gate with no other pSDR C2XA01IA312Pump · faultyIAH - FLIGHT 3050, THE CREW REPORTED THAT THE NUMBER TWO ENGINE EXPERIENCED A SUDDEN POWER LOSS DURING CLIMBOUT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE DRIVEN FUEL PUMP, AND THE ASDR WVBA2001044Pump · inoperativeDURING INSPECTION, FUEL STAIN WAS OBSERVED FROM THE DISCHARGE FITTING ON THE PUMP BODY FUEL STAIN WAS ALSO NOTED ON THE PUMP BODY HOUSING PARTING FLANGE. PUMP WAS REMOVED FROM SERVICE. NOTE: THIS IS A (M) STYLE PUMP THAT IS RE-DESIGNED TO RELIEVE LEAKS ON THSDR WVBA2001043Pump · leakingDURING INSPECTION, FUEL WAS OBSERVED LEAKING FROM THE SET SCREW THAT HOLDS THE DRIVE SHAFT LOCK NOT IN CHECK IN THE PUMP BODY. THE PUMP WAS REMOVED AND REPLACED. THE LOCK NUT WAS REMOVED FOR INSPECTION AND IT WAS NOTED THAT A BACK UP PACKING BEHIND THE ORINGSDR AUS20010919Pump · unserviceable(AUS) ENGINE FUEL PUMP HOUSING CRACKED IN AREA OF CONCENTRIC SHAFTSUPPORT.SDR WVBA2001040Pump · stuckDURING PREINSPECTION RUN, IT WAS NOTED THAT THE ENGINE DRIVEN FUEL PUMP PRESSURE WAS LOW AFTER ADJUSTMENTS WERE MADE THE DESIRED PRESSURE SETTING WAS NOT OBTAINABLE. TROUBLESHOOTING, IT APPEARS THE RELIEF VALVE IS HUNG UP PUMP WAS REMOVED FROM SERVICE AND SENSDR WVBA2001041Pump · leakingDURING INSPECTION IT WAS FOUND THAT FUEL WAS LEAKING FROM THE SET SCREW FOR THE DRIVE COUPLING LOCK NUT REFERENCE THE RG9080 SERIES COMPONENT MM FOR PARTS BREAKDOWN. PUMP WAS REMOVED FROM SERVICE.SDR EISA20010106Pump · failedNR 2 ENGINE QUIT RUNNING AT FL190. OIL PRESSURE WENT TO 20 PSI. SHUT ENGINE DOWN AT 2250Z, DECLARED EMERGENCY. MADE UNEVENTFUL LANDING. (WINDMILLING PRESSURE). REMOVED AND REPLACED NR 2 ENGINE HP FUEL PUMP.SDR Z4MR601462Relief Valve · leakingA RANDOM INSPECTION OF THE FUEL PUMP REVEALED FUEL LEAKING FROM THE ENGINE DRIVEN LOW PRESSURE FUEL PUMP RELIEF VALVE GASKET.SDR GNB2001F00001Pump · erraticENGINE DRIVEN FUEL PUMP - FUEL PUMP ERRATIC ON UNMETERED FUEL PRESSURES.SDR UG82001F00000Pump · malfunctionedRIGHT ENGINE FUEL (PRESSURE) ANNUNICIATOR ILLUMINATED. ENGINE DRIVEN FUEL PUMP PERFORMANCE DEGRADING. REPLACED ENGINE DRIVEN FUEL PUMP WITH AN OVERHAULED UNIT.SDR DL78K011027Pump · faultyNR 2 ENGINE SHUTS DOWN AFTER REACHING IDLE. T/S PER FIM 73-06-00-810-807 FOUND FUEL PUMP PRESSURE LOW PER AMM 73-11-01-200-802. REPLACED FUEL PUMP PER AMM 73-11-01-4. LEAK CHECK AND OPS CHECK OK.SDR 2001F00243Diaphragm · rupturedPOST RAYTHEON AIRCRAFT SERVICE BULLETIN 71-3307, ENGINE DRIVEN LOW PRESSURE FUEL PUMP DRAIN MOD. EXPERIENCED A FAILURE OF THE LOW PSI ENGINE DRIVEN FUEL PUMP ON THE NR 1 ENGINE. THE RESULT OF THE DIAPHRAGM RUPTURE WAS TO HAVE FUEL VENTED OUT OF THE NACELLE TSDR CA010622033Pump · leaking(CAN) THE PILOT NOTED FUEL DRIPPING FROM THE OVERBOARD DRAIN TUBE. MAINTENANCE DISCOVERED FUEL COMING FROM THE FUEL PUMP SEAL DRAIN. THERE IS A CRITICAL SERVICE BULLETIN C53 01-01. ALTHOUGH THE PART NUMBER DID NOT MATCH THE BASIC FUEL PUMP WAS IDENTIFIED BY THSDR SW032001B3673Pump · failedFUEL PUMP FAILED DURING FLIGHT. NO FLIGHT ABORT.SDR CA020405009Pump · inoperative(CAN) AFT BOOST PUMP NOT FUNCTIONAL.SDR 20010613CW014Pump · leakingON LANDING, A SMELL OF FUEL WAS DETECTED IN THE CABIN OF THE AIRCRAFT. MAINTENANCE WAS CALLED TO CHECK THE AIRCRAFT FOR A FUEL LEAK, UPON INSPECTION IT WAS FOUND TO BE LEAKING FUEL FROM THE CASE DRAIN IN THE ENGINE DRIVEN PUMP. PUMP WAS REMOVED AND TRIMMED ISDR WVBA2001033Pump · leakingDURING INSPECTION IT WAS NOTICED THAT FUEL STAIN WAS ON THE BODY OF THE FUEL PUMP NEAR THE DRAIN COMING FROM THE PARTING SURFACE (LOWER) NOTE THIS IS A NEW STYLE PUMP DESIGNED TO RELIEVE THE LEAKING PROBLEM THE OLDER PUMPS HAD IN THIS AREA. THE PUMP WAS REPLSDR 20010605CW014Shaft · brokenUPON DISASSEMBLY I FOUND THE SHAFT IN TWO PIECES. THE STANDARD 64-0197 SHAFT IS A SOLID ONE PIECE SHAFT. THE SHAFT THAT WAS REMOVED FROM THIS UNIT WAS MACHINED INTO TWO DIFFERENT PIECES, AND WAS HELD TOGETHER BY TWO PINS. THIS IS NOT A STANDARD REPAIR. ONE
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