JASC 7310
Service difficulty reports · 1,981
Reports filed under 7310 · Engine Fuel Distribution, 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 = '7310' 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 = '7310' 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 2002FA0001084Manifold · malfunctionedTHE CREW REPORTED A MOMENTARY POWER ROUGHNESS. THE AIRCRAFT FUEL CONTROL SYSTEM AND IGNITION SYSTEM WERE INSPECTED. THE FUEL MANIFOLD WAS REPLACED ALONG WITH 2 INJECTOR NOZZLES. A GROUND OPERATIONAL CHECK WAS PERFORMED. FOLLOWING THAT A FUNCTIONAL CHECK FLIGHTSDR AMW2002F00003Pump · failedWHILE FLIGHT WAS ENROUTE, THE LT LOW FUEL PRESSURE ANNUNCIATOR ILLUMINATED IN FLIGHT. THE CREW THEREFORE RETURNED THE AIRCRAFT TO THE FIELD WITHOUT ANY FURTHER INCIDENT. THE CORRECTIVE ACTION WAS THAT REPLACED THE LT LOW PRESSURE ENGINE DRIVEN FUEL PUMP.SDR AUS20021067Tube · loose(AUS) RH ENGINE WASTE FUEL DRAIN TUBE DISCONNECTED FROM ENGINE FUEL NOZZLE MANIFOLD. INVESTIGATION FOUND THAT THE WASTE FUEL DRAINTUBE HAD BEEN DISCONNECTED THE PREVIOUS NIGHT AS PART OF THEPROCESS USED IN CARRYING OUT A COMPRESSOR WASH ON THE ENGINE. FOLLOWINSDR CA021031015O-Ring · leaking(CAN) FUEL DRAIN VALVE LEAKING AT O-RING. REPLACED VALVE.SDR DL764021047Fuel Line · leakingNR 2 ENG FUEL JUMPER LINE LEAKING REF IPC 73-11-06-11 ITEM 85. REMOVED AND REPLACED LEAKING FUEL HOSE ON RT ENG, PERFORMED LEAK TESTS NR 2 AND 3 PER PFHB 1-0-7-7 NO LEAKS NOTED.SDR I7W2002F00000Valve · stuckENGINE FUEL BY-PASS ACTUATED CAUSING POWER FLUCTUATION AND NTS ACTUATION. VALVE STUCK OPEN. FOUND FAULT IN AIRCRAFT WIRE BUNDLE NEXT TO CONNECTOR PLUG.SDR AUS20020977Manifold · cracked(AUS) LH ENGINE SECONDARY FUEL MANIFOLD CRACKED IN AREA OF UPPERNOZZLE END SWAGED FITTING. LEAKING FUEL CAUGHT FIRE CAUSING DAMAGE TO FIRE TUBING ON MANIFOLDS, SUPPLY LINE, ENGINE MOUNTSAND COWLS.SDR AUS20021305Solenoid · leaking(AUS) LT ENGINE PRIMARY-ONLY SOLENOID LEAKING FROM VALVE BODY.SDR WVE2002F00018Line · chafedDURING 1200 HOUR INSPECTION, THE ENGINE FUEL FEED LINE WAS FOUND CHAFING ON THE FORWARD FIREWALL AFT OF THE INLET ASSEMBLY. INSTALLED ADDITIONAL ADEL CLAMP. NO DAMAGE OCCURRED TO FUEL LINE. LINE IMPROPERLY SECURED. (2002B1363)SDR 2002F00812Fuel Filter · dirtyON DESCENT NR 3 ENGINE FUEL PRESSURE LIGHT ON, THROTTLES AT IDLE, ENGINE FLAMED-OUT. PERFORMED EMERGENCY RESTART, OK. REMOVED AND REPLACED NR 3 ENGINE LP FUEL FILTER IAW M/M 73-11-02, PERFORMED LP FUEL PUMP DRIVE TEST 19 OF M/M 71-00-00, OK.SDR BSY2002F00014O-Ring · failedAIRCRAFT ABORTED TAKE OFF BECAUSE LT ENGINE 200 RPM LOW. FOUND O-RINGS ON LEFT FUEL MANIFOLD IN WING ROOT SUCKING AIR, REMOVED AND REPLACED O-RINGS. OPS GOOD.SDR IXXA0200047OSeal · defectiveEN ROUTE FROM LRD TO TOL, THE NUMBER TWO ENGINE FLAMED OUT DURING CLIMBOUT FROM LRD. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE WHICH REVEALED THE FUEL FLOW TRANSMITTER LEAKINGSDR AUS20020821Filter · dirty(AUS) RH ENGINE FUEL FILTER LIGHTLY CONTAMINATED.SDR EVAB2002001Intake Pipe · crackedEXPERIENCED AN ENGINE FIRE ACCOMPANIED BY BOTH AUDIO AND VISUAL WARNING. FIRE WAS OBSERVED FROM THE COWLING. WHEN THE THROTTLE WAS PULLED BACK THE FIRE WENT OUT AND ALL WARNINGS STOPPED. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED. SUBSEQUENT INVESTISDR CA020702007Tube · contaminated(CAN) WHILE PERFORMING A REMOVAL / INSTALLATION OF THE FUEL NOZZLES,A SMALL PIECE OF METAL DEBRIS WAS FOUND WITHIN THE INTERNAL PASSAGE OF ONE OF THE FUEL MANIFOLD TRANSFER TUBES. THE DEBRIS WAS LODGED WITHIN THE TUBE AND HAD TO BE EXTRACTED BY PUSHING IT THRSDR CA020628001Tube · contaminated(CAN) WHILE PERFOMING A SCHEDULED REMOVAL / INSTALLATION OF THE FUEL NOZZLES, A SMALL PIECE OF METAL DEBRIS WAS FOUND WITHIN THE INTERNAL PASSAGE OF ONE OF THE FUEL MANIFOLD TRANSFER TUBES. THE DEBRIS WAS LODGED WITHIN THE TUBE AND HAD TO BE EXTRACTED BY PUSHISDR GLBA2002094Filter · restrictedLEFT FUEL FILTER ANNUNCIATOR ILLUMINATED AT 25 - 30 PERCENT TQ. REPLACED HIGH AND LOW PRESSURE FUEL FILTERS OPS CHECKED SATISFACTORYSDR AALA20020909Line · leakingMEM - FLT 2069 - EN ROUTE CVG-DFW, CREW NOTED 500 POUND FUEL IMBALANCE DURING CLIMB-OUT. ALSO NOTED DIFFERENCE IN FUEL FLOW IN LEFT ENGINE. IN-FLIGHT FUEL CHECKLIST COMPLETED. SHUT DOWN LEFT ENGINE, AND TOOK EMERGENCY DIVERSION TO MEM. LANDED MEM WITH FUELSDR UPS02838684Fitting · looseINSPECTION TYPE:N/A, AT 1 HOUR AND 35 MIN AFTER TAKEOFF, NR 3 ENGINE FLAMED OUT IN MODERATE TURBULENCE AND RAIN. FLAME-OUT OCCURRED AT 35,000 FEET AND MUCH .80. ATTEMPTED INFLIGHT ENGINE START AT 35,000, WAS UNSUCCESSFUL. PERFORMED FLAME-OUT INSP PER M/M 71SDR SWIA200210939Fuel Line · crackedAFTER TAKEOFF FUEL DISCOVERED LEAKING FROM RIGHT ENGINE. ENGINE SHUTDOWN AND AIRCRAFT RETURNED TO THE FIELD. FOUND CRACKED FUEL LINE AT HMU. REPLACED LINE. LEAK CHECK GOOD. REMOVED AND REPLACED HMU FUEL RETURN HOSE IAW EMB POWERPLANT BUILDUP 71-00-00. OPSDR HEEA079939Connector · corrodedFADEC FAULT AND FADEC DEGRADE LIGHT ILLUMINATED. ECU HAS CORROSION ON CONNECTOR AND HAD QUIET MODE SWITCH FAULT INDICATED. REPLACED WITH SERVICEABLE ECU.SDR HEEA079937Ecu · damagedECU HAS A BROKEN CONNECTOR PIN.SDR CA020605004Line · cracked(CAN) HEAVY FUEL LEAK OBSERVED ON LT ENGINE DURING GROUND RUN. AFTER INVESTIGATION, FOUND THAT THE PRESSURE LINE BETWEEN FCU AND FUEL FLOW DIVIDER WAS FOUND CRACKED AT THE B-NUT ON FCU SIDE. THE CRACK WAS PARALLEL TO THE WELDING OF THE B-NUT SEATING.SDR AUS20020818Line · loose(AUS) FUEL PRESSURE LINE ON FCU LOOSE. LOSS OF POWER.SDR HEEA078810Line · leakingFUEL LINE LEAKING. REPLACED WITH SERVICEABLE LINE.SDR HEEA078809Hose · kinkedFIRE SHIELD TO FUEL NOZZLE HOSE KINKED. REPLACED WITH SERVICEABLE HOSE.SDR CA020510011Line · bent(CAN) DURING COMPLIANCE WITH AD 93-02-05 (FUEL INJECTION)TUBE WAS FOUND BENT, AFTER REMOAL, TUBE WAS FOUND WORN TOO. IT WAS NOT CHAFING ON OTHER COMPONENT.SDR RAIA00204138Fuel Filter · clogged5299-STL- LEFT ENGINE FUEL IMPENDING BYPASS MESSAGE. MAINTENANCE REMOVED AND REPLACED FUEL FILTER.SDR CA020430001Fuel Filter · leaking(CAN) WHILE DE-INHIBITING ENGINE FCU, FUEL FOUND LEAKING FROM FIREWALL MOUNTED FUEL FILTER AT BASE OF CANISTER O-RING. FILTER CANISTER REMOVED, NEW FILTER ELEMENT AND O-RING WERE INSTALLED, FILTER ASSY TORQUED IAW AT-802 MM AND PRESSURE TESTED SERVICEABLE. SDR CA020501015Line · damaged(CAN) WHILE THE AIRCRAFT WAS IN FOR AN ENGINE CHANGE , FOUND ON NR 1 ENGINE , THAT THE FUEL TUBE ASSY LINE DISCONNECT TO HP PUMP WAS DENTED. ONCE REMOVED, FOR REPLACEMENT , NOTICED THAT THE FERRULE, THE FERRULE SEAL CARRIERS WERE WORN AND PITTED AND ALSO THE CSDR ALG2002F00058Shroud · defectiveDURING TESTING OF NOZZLE, WHEN NOZZLE WAS TORN DOWN FOR REPAIR, FOUND UNSERVICEABLE. NEW SHROUD FROM STOCK WAS DEFECTIVE FROM FACTORY. TRIED TO REASSEMBLED SHROUD AND PARTS WOULD NOT PROPERLY FIT.SDR CA020521004Fitting · worn(CAN) ENROUTE TO VICTORIA AIRPORT STRONG SMELL OF JET FUEL NOTICED. THEY WERE JUST IN ZONE WITH TOWER. PILOT DECLARED EMERGENCY WITH AIRPORT. A/C LANDED WITH NO INCIDENT AND AIR TAXI BACK TO HANGAR. INVESTIGATION OF ODOUR FUEL CONTROL TO START FUEL LINE FITTSDR ALG2002F00056Nozzle · bentDURING TESTING OF NOZZLE. FOUND ORIFACE BENT CAUSING STREAKS IN SPRAY.SDR CA020411002Line · cracked(CAN) DURING CLIMB, CREW RECEIVED LT ENGINE FIRE WARNING. WARNING WENT OUT AFTER ENGINE THROTTLED BACK, BUT THEN ITT BEGAN CLIMBING. CREW SHUTDOWN ENGINE AND PERFORMED SINGLE ENGINE LANDING. SUBSEQUENT INSPECTION REVEALED THAT FUEL LINE BETWEEN FLOW DIVIDERSDR AUS20020361Sleeve · worn(AUS) THE FIRE SLEEVE OF FUEL HOSE (PN 10544E) WAS FOUND CHAFFED APPROX 0.005 IN (0.127MM) IN DEPTH THROUGH WALL OF FUEL HEATER.SDR AUS20020295Diaphragm · damaged(AUS) LH ENGINE MANIFOLD VALVE DIAPHRAGM TORN. LENGTH OF TEAR APPROXIMATELY 12.7MM (0.5IN).SDR 2002FA0000329Line · leakingLT ENGINE HAD A FUEL LEAK. FOUND FUEL BYPASS TUBE LEAKING. LEAK AT SOLDIER JOINT, CRACK OR OTHER DEFECT. INSTALLED NEW TUBE.SDR VNAA0202017Filter · cloggedEN ROUTE FROM SAT TO OKC, THE CREW RECEIVED A LEFT HAND HIGH PRESSURE FILTER BYPASS CAS MESSAGE AND RETURNED TO SAT. FAIRCHILD MAINTENANCE INSPECTED AND REPLACED THE HIGH PRESSURE FILTER AND THE HIGH PRESSURE BYPASS TEMPERATURE SENSOR IN ACCORDANCE WITH DORNISDR EWK2002F00001Line · corrodedDEEP CORROSION ON FUEL PRESSURE LINE AT CONJUNCTION OF FUEL LINE AND DEFROSTER HEAT DUCT. INSULATE FUEL LINE FROM HEAT DUCT. DANGER: POTENTIAL FOR FIRE.SDR EWK2002F00000Line · corrodedDEEP CORROSION ON FUEL PRESSURE LINE AT CONJUNCTION OF FUEL LINE AND DEFROSTER HEAT DUCT. INSULATE FUEL LINE FROM HEAT DUCT. DANGER/POTENTIAL FOR FIRE.SDR CA020213010B-Nut · leaking(CAN) SMALL AMOUNT OF FUEL OBSERVED LEAKING FROM RT FLOOR CAVITY DRAIN. CAVITY WAS OPENED, FUEL TRANSFER LINE INSPECTED. LEAK ORIGINATED FROM AFT 'B' NUT FITTING. TORQUE WAS CHECKED ON 'B' NUT, WITHIN SPECS. AIRCRAFT DRAINED OF FUEL, LINE REMOVED AND INSPECTSDR DXT2002F00000Tube · chafedDURING ROUTINE INSPECTION RIGHT FUEL SUPPLY TUBE ASSEMBLY WAS FOUND TO BE NEARLY 100 PERCENT CHAFFED THROUGH BY THE RIGHT ELEVATOR CABLE JUST FORWARD OF THE RIGHT BATTERY. MAINTENANCE REMOVED AND REPLACED THE FUEL SUPPLY TUBE ASSEMBLY WITH A NEW ASSEMBLY. MSDR S02271044Fuel Line · contaminatedNR 2 ENG UNSCHEDULED THRUST LOSS IN FL 350 AFT IGN SW ON APPROX 1 MIN. ENG OPER RESUME NML. SINCE IN-FLT RESTART SUCCESSFULLY, SUSPECT ENG FUEL SUPPLY SYS INTERRUPTED DUE TO WATER CONTAMINATION IN FUEL SYS. 2.IAW AMM FUEL PUMP FILTER INSP FOUND DIRTY AND RPLSDR ANCF200200002Switch · malfunctionedDURING TAKE OFF LEFT ENGINE N3 WENT TO OVER SPEED AND SHOWED DIFFERENCE BETWEEN ENGINE PARAMETERS, LH ENGINE HIGHER THAN THE RT, THE ENGINE DIDN’T SHUT DOWN, THE CREW PROCEEDED TO RETURN TO EDR. CORRECTIVE ACTION: PERFORMED BITE TO BVCU, FOUND ALTITUDE SWITSDR DL76S020048Gasket · leakingLEFT ENGINE FAILED IN FLT ON DESCENT INTO MCO. POM PROCEDURES FOLLOWED, ONLY ABNORMAL INDICATION WAS HIGH FUEL FLOW, COMPARED TO THE RIGHT ENGINE. ON ARRIVAL FOUND LEFT ENGINE IDG FUEL/OIL COOLER GASKET CUT AND LEAKING. REPLACED SAME. FULL POWER RUN UP PERSDR AUS20020019Line · ruptured(AUS) ENGINE HEAT EXCHANGER FUEL TUBE LEAKING. FUEL SPRAYING INSIDE COWLS AND ENTERING ENGINE THROUGH INTAKE.SDR AUS20020024Balance Tube · fractured(AUS) ENGINE BALANCE TUBE FRACTURED AT WELD JOINT. NR 3 CYLINDER INOPERATIVE AND PROPELLER BLADE LOOSE.SDR DL76S020013Manifold · defectiveENGINE FLAME-OUT ON CLIMBOUT AT 34000. RETURNED FOR LANDING AT MCO. ENGINE FAILED NO MORE THAN 27 MINUTES FROM LANDING. REPLACED FUEL MANIFOLDS AT 11 O'CLOCK AND 6 O'CLOCK POSITIONS RAN NR 2 ENG PER PFHB TEST 4 T/O POWER AND LEAK CK ALL PARAMETERS OK OK FORSDR 2002FA0000444Flow Divider · leakingRECEIVED NEW FLOW DIVIDER TO REPLACE FLOW DIVIDER WITH SUSPECTED LEAKING DUMP VALVE. AT MFG REQUEST, A LEAK CHECK WAS PERFORMED ON THE NEW FLOW DIVIDER. IT WAS FOUND THAT THE NEW FLOW DIVIDER LEAKED AT THE DUMP VALVE AND IS NOT SERVICEABLE. THIS IS SECOND FSDR NSV2002F00000Line · chafedMECHANIC FOUND EVIDENCE OF FUEL DRIPPING FROM LEFT ENGINE NACELLE. REMOVED AND REPLACED FUEL LINE, RAN UP, LEAK CHECKED GOOD. (CONTROL NR NSVA 02-03)
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