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 20010612CW011Fuel Line · leakingRT ENGINE CLIMBING OUT, AROUND 3000 FEET , NOTICED F/F DOWN TO 12 GPM FOUND FUEL LEAK BETWEEN FUEL LINE AND FUEL MANIFOLD. REPAIRED FUEL LEAK, OPS CHECKED GOOD.SDR AU010292Pipe · fractured(AUS) ENGINE FUEL PIPE FRACTURED. FUEL LEAKING.SDR RAIA00104001Fuel Filter · clogged7320-STL-DURING TAKEOFF RIGHT HAND ENGINE FUEL CLOG LIGHT CAME ON. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND ENGINE FUEL FILTER IAW ATR72 MAINTENANCE MANUAL.SDR SIMA200108001Fuel Line · chafedORD - FLT 4100 - OIL SMELL IN CABIN. FOUND CHAFED FUEL LINE FROM FUEL PUMP METERING UNIT TO FUEL COOLED OIL COOLER ON NR 2 ENGINE. REMOVED AND REPLACED LINE IAW AMM. OPS CHECK GOOD. (M)SDR DL757010461O-Ring · leakingRT ENGINE FUEL PUMP FILTER CASE LEAKING. REPLACED DAMAGED O-RING. LEAK CK OK.SDR DL757010411Engine · malfunctionedON TAKEOFF ROLL LEFT ENGINE DID NOT REACH TAKEOFF POWER LEFT ENGINE INDICATED 1.09 EPR RIGHT ENGINE 1.26 EPR TRIED TO RUN UP LEFT ENGINE FARTHER LEFT OIL PRESSURE RED WARNING INDICATED HIGH OIL PRESSURE STOPPED TAKEOFF ROLL AT VERY LOW SPEED LESS THAN 40 KNOTSDR KBMA88679Pressure Switch · malfunctionedFUEL PRESSURE SWITCHES NOT OPERATING PROPERLY. CAUTION LITE REMAINS ON WITH CIRCUIT BREAKER IN.SDR 20010411CW014Tube · disconnectedDURING TAXI FOR TAKEOFF, THE RIGHT ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN. AIRCRAFT WAS TAXIED BACK AND TURNED OVER TO MAINTENANCE. INSPECTION REVEALED THE P3 LINE DISCONNECTED AT THE FUEL CONTROL. THE LINE WAS RECONNECTED AND THE ENGINE GROUND RUN NORMSDR AU010155Switch · leaking(AUS) FUEL FILTER BYPASS SWITCH LEAKING FROM SWITCH BODY IN THE AREA WHERE THE ELECTRICAL CONNECTOR IS SOLDERED TO THE SWITCH. FUEL WAS SEEN RUNNING INTO THE ENGINE INTAKE PLENUM. A REPLACEMENT SWITCH HAD POOR SOLDERING OF THE CONNECTOR IN THE SAME AREA ASTHESDR AUS20011125Line · misrepaired(AUS) ENGINE FUEL PRIMER LINE CHAFED THROUGH AND THEN INCORRECTLY REPAIRED. ELECTRICAL TAPE HAD BEEN WRAPPED AROUND THE LINE TO STOP FUEL LEAKS.SDR GAIA01045BOPShutoff Valve · shortedFLT 2724 - ROC-BOS - NR 2 ENGINE FAILED ON CLIMB-OUT. ATTEMPTED RESTART FAILED. DID HAVE OIL PRESSURE AND ROTATION. AIRCAFT MADE AN UNEVENTFUL RETURN TO ROC. FOUND NR 2 FUEL SHUTOFF VALVE WIRES SHORTED IN AIRCONDITIONING BAY, CAUSING NR 2 FUEL SHUTOFF VALVESDR AUS20010813Filter · leaking(AUS) FUEL FILTER BOWL LEAKING.SDR A6WA200100014Flow Divider · leakingDURING START OF NR 2 ENGINE, A FLIGHT ATTENDANT AND SEVERAL PASSENGERS VERBALLY REPORTED FIRE. NO INDICATION IN COCKPIT. THE NR 2 ENGINE WAS SHUTDOWN AND BOTH FIRE BOTTLES WERE RELEASED. ACFT WAS EVACUATED VIA RT SIDE EVACUATION SLIDES. MAINTENANCE REMOVEDSDR AU010029Flow Divider · corroded(AUS) ENGINE FUEL FLOW DIVIDED CORRODED. PARTICLES OF CORROSION BLOCKING FUEL INJECTORS. AIRCRAFT HAD BEEN CONTAMINATED WITH EDAAND DECONTAMINATED IAW AD/GEN/80 AND MANUFACTURERS INSTRUCTIONS.SDR AU010041Pipe · worn(AUS) NR 3 ENGINE LT PRIMARY FUEL PIPE CHAFING ON COMBUSTOR CASE IN AREA OF THE FORWARD FLANGE OF THE CUSTOMER BLEED FLANGE.SDR CA010206008Manifold · cracked(CAN) DURING CLIMB A NR 2 ENGINE FIRE WAS EXPERIENCED AND THE ENGINE WAS SHUT DOWN. INSPECTION REVEALED SIGNS OF A FIRE IN ZONE 2. ITS LEFT FUEL MANIFOLD WAS CRACKED. THIS CRACK WAS IN SUCH A POSITION THAT THE TASK GENERATED BY AD 97-11-05 WOULD NOT LIKELY HAVSDR CA010301002Line · misrepaired(CAN) DURING RECEIPT OF A LOANER ENGINE, IT WAS NOTED THAT ONE OF THE INSTALLED LINES FROM THE FLOW DIVIDER TO THE FUEL MANIFOLD HAD AN UNAPPROVED WELD REPAIR ACCOMPLISHED ON IT. THE LINE WAS REPLACED.SDR AU010001Pipe · chafed(AUS) ENGINE FUEL PIPE FROM FLOW DIVIDED TO FUEL MANIFOLD CHAFED ON COMBUSTOR HOUSING.SDR AU001213Line · failed(AUS) NR 3 ENGINE FUEL LINE LOCATED BETWEEN THE FLOW DIVIDER AND FUELMANIFOLD FRACTURED AND LEAKING FUEL. FUEL IGNITED CAUSING DAMAGETO THE WIRING HARNESS AND TGT HARNESS.SDR 20001228SH002Hose · leakingDURING ANNUAL INSPECTION, THE FLEXIBLE FUEL HOSE WAS FOUND WET WITH FUEL NEAR ONE OF THE FITTINGS. THE HOSE WAS NOT THAT OLD AND WAS MADE IN THE FIELD. (X)SDR R7MR32952Tube · leakingLEAKING BEYOND SERVICEABLE LIIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR CA001201018Line · loose(CAN) ENGINE DECELERATED ON TAKEOFF FOR TEST FLIGHT AFTER ENGINE CHANGE. CAUSE WAS DETERMINED TO BE LOOSE B-NUT ON GOVERNOR TO FUEL CONTROL UNIT AIR LINE.SDR 20001204SH010Line · brokenTHE NR 1 ENGINE QUIT EN ROUTE. THE PILOT ATTEMPTED TO RESTART THE DEAD ENGINE WITH NO SUCCESS. A FORCED LANDING WAS SUCCESSFULLY MADE. THE LEFT ENGINE WAS LATER REMOVED FROM THE AIRCRAFT AND INSTALLED ON A TEST STAND. THE NR 6 CYLINDER MANIFOLD TO NOZZLE, SDR EISA20000199Fuel Line · leakingDURING CLIMBOUT, LOST THRUST ON NR 1 ENGINE. AIR TURNBACK TO (IND). FOUND FUEL LINE LEAKING. REMOVED AND REPLACED FUEL LINE, OPS CHECK GOOD IAW M/M 73-00.SDR 20001215SH016Line · wornP2 HOSE WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR 20001215SH015Coupling · wornP2 UNION WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR CA001103011Line · damaged(CAN) AD 93-02-05 AND LYC SB 342C ADDR BENDING LIMITS FOR FUEL LINE ALONG WITH MEANS OF MINIMIZING HAZARDS OF FUEL LINE DAMAGE. 2 LIMITS LISTED ARE NO BENDS WITHIN 0.69 INCH FROM END AND MIN RADIUS OF 0.62 INCH (.6250 INCH) TO CENTER OF FUEL LINE. WHEN LINESDR CA001030010Line · leaking(CAN) UPON STARTING THE LT ENGINE, THE ENGINEER NOTICED SMOKE COMING FROM INSIDE THE COWLING. HE SIGNALED THE PILOT TO ABORT THE START. WHEN THE COWLS WERE OPENED FUEL WAS NOTICED LEAKING OUT THE LINE CONNECTING THE FUEL PRESSURE TRANSMITTER AND THE HIGH PRSDR 20001113SH007B-Nut · looseAIRCRAFT WAS LEVEL FLIGHT WHEN ENGINE DECELERATED AND QUIT. PRELIMINARY INSPECTION FOUND PC LINE B-NUT AT FUEL CONTROL LOOSE. LINE WAS REMOVED, INSPECTED, AND RE-INSTALLED. ENGINE GROUND RUN. (X)SDR AU001007Pipe · disconnected(AUS) LEFT ENGINE DECK PRESSURE LINE DISCONNECTED. (X)SDR DL73K002017Actuator · intermittentAFTER STARTING NR 1ENG (NORMAL START) DURING TAXI OUT NR 1 ENG FLAMED OUT. ON RESTART ATTEMPT AT GATE, NO FUEL FLOW INDICATION AFTER START LEVER RAISED TO IDLE. REPLACED BAD FUEL SOV ACTUATOR AND GATE ASSY PER MM. RAN NR 1 ENG, ALL PARAMETERS GOOD.SDR 20010409CW015Manifold · fracturedRIGHT SECONDARY FUEL MANIFOLD WAS FOUND FRACTURED. REMOVED AND REPLACED ALL FUEL MANIFOLDS. A PRESSURE AND LEAK CHECK WAS CONDUCTED, RESULTED IN NO LEAK FOUND.SDR AU001059Line · broken(AUS) NR 2 AND NR 4 CYLINDER FUEL INJECTOR LINES PN LW-12098-0-170 AND PN LW-12098-0-240 BROKEN AT OR NEAR NIPPLE ON NOZZLE END OF LINE. (X)SDR AU000845Valve · failed(AUS) NR 1 ENGINE FUEL VALVE FAILED TO OPEN DURING ENGINE START.SDR CA000927009Line · chafed(CAN) DURING GROUND HANDLING FUEL LEAK ON LT ENGINE WAS OBSERVED. FURTHER INVESTIGATION REVEALED THAT FUEL LINE BETWEEN FCU AND FUEL LIMITER WAS CHAFED THROUGH. TEMPORARY REPAIR TO FLY AIRCRAFT BACK TO HOME BASE. AT HOME BASE FUEL LINE REPLACED BY NEW AND AIRCSDR 20000831SH001Fuel Line · deterioratedIN CRUISE FLIGHT ENGINE RAN ROUGH, HAD LOW EGT 900DG ON NR 2 CYLINDER. AFTER LANDING AND TROUBLESHOOTING FOUND DEBRIS IN FUEL LINE FROM SERVO TO FLOW DIVIDER. REPLACED RUBBER FUEL LINE WITH TEFLON LINE P/N LW12784-4-172 IAW LYCOMING SI1274B. SUBMITTER SUGGSDR CA000906004Valve · worn(CAN) THE HELICOPTER EXHIBITED OCCASIONAL OSCILLATIONSIN TORQUE, N1 & TOT. AFTER EXTENSIVE TROUBLESHOOTING AN OVERHAULED DOUBLE CHECK VALVE WAS INSTALLED AND PROBLEM WAS RECTIFIED.VALVE ASSEMBLY SENT TO STANDARD AERO LTD IN WINNIPEG AS CORE EXCHANGE FOR OVERHASDR CA000901005Filter · obstructed(CAN) A/C 741, AUGUST 14/2000, FLT 906, YYC, LOG SEQUENCE 0281117. ENGINES WERE ACCELERATED FOR TAKEOFF AND NR 2 ENGINE COMPRESSOR STALL OCCURRED. TAKEOFF WAS ABANDONED AT 15 KNOTS. AIRCRAFT RETURNED TO RAMP. MAINTENANCE REQUESTED ENGINE TO BE RUN. ENGINE STALSDR CA000829009Fuel Line · leaking(CAN) FSR WAS CALLED INTO ASSIST. BW1A MAINTENANCE CONTROL ON AOG WITH AIRCRAFT 9Y-WIN, WITH A LEAKING FUEL LINE ON THE NR2 ENGINE. THE AIRCRAFT WAS IN BARBADOS WITH NO PARTS. PRELIMINARY REPORTS WAS THE LINE FROM THE FUEL COOLED OIL COOLER HAS PIN HOLE, LEAKISDR AALA20001201Valve · malfunctionedMCI - FLT 851 - APPROX 35 MIN AFTER TAKEOFF, WHILE AT CRUISE AT FL260 DISCOVERED AT 900 LB FUEL IMBALANCE BETWEEN RIGHT MAIN AND LEFT MAIN FUEL TANKS. CENTER TANK HAD 10,000 LBS OF FUEL STILL REMAINING, LEFT TANK WAS STILL FULL 9100 LBS AND RIGHT TANK 8200 LBSDR CA000719002Line · leaking(CAN) THE LINE GOING TO THE LEFT HAND START INJECTOR FOUND LEAKING DURING A GROUND RUN, AFTER REMOVAL FOUND THE FLARE WAS CRACKED 60 PERCENT AROUND THE CIRCUMFERENCE.SDR CA000718016Check Valve · failed(CAN) NR 2 ENGINE LEAKING FUEL FROM ECOLOGY DRAIN WHEN LT INNER PUMP SELECTED ON. ECOLOGY DRAIN CHECK VALVE REPLACED AND AIRCRAFT RETURNED TO SERVICE.SDR 20000720SH040Manifold · malfunctionedFUEL MANIFOLD ASSY CAUSES ENGINE TO RUN HOT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR 20000721SH004Manifold · malfunctionedFUEL MANIFOLD ASSY CAUSES ENGINE TO RUN HOT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR SIMA0931Fuel Line · chafedORD - FLT 4256 - NR 2 ENGINE FLAMED OUT AT CRUISE IN MODERATE TURBULENCE. AIRCRAFT RETURNED TO ORD, NORMAL LANDING. FOUND FUEL FEED LINE CHAFED AND LOOSE IN INBOARD WING AT RIB 7 AT JOINT LINE. REMOVED AND REPLACED FUEL AT RIB 7 IAW ATR 42 AMM. OPS CEHCK FSDR 20000721SH023Manifold · leakingFUEL MANIFOLD STARTED TO LEAK AT THE SILVER SOLDER JOINT BY THE LARGE B-NUT. FUEL CAUGHT FIRE AND BURNED ENGINE COWL ON TAKEOFF. (X)SDR CA000606005Gascolator · failed(CAN) AIRCRAFT REFUELED AND TAXIED ONTO RUNWAY FOR DEPARTURE. AIRCRAFT BOOST PUMPS WERE NOT TURNED ON AT THIS POINT AS THE PILOTS WERE INSURING ENGINES WOULD RUN WITHOUT BOOST PUMPS AS STATED IN THE OPS MANUAL. WHILE TAXIING ON THE RUNWAY, NR 1 ENGINE FLAMEDSDR 20000721SH040Hose · leakingHNL - FLT 8666 - ON CLIMB-OUT, PILOT REPORTED ''FUEL FUMES IN COCKPIT''. AIR TURNBACK TO HNL. FUEL ACCUMULATION IN ENGINE COWL DUE TO LOOSE FUEL LINE CONNECTION AT FIREWALL FUEL FILTER. TIGHTENED THE NOSE FITTING, FLUSHED COWLING WITH SOAP AND WATER. PERFOSDR 20000721SH005Manifold · malfunctionedFUEL MANIFOLD ASSEMBLY CAUSES ENGINE TO RUN HOT. (X)SDR AU000409Pipe · cracked(AUS) NO1 ENGINE FUEL CONTROL UNIT TO OVERSPEED GOVERNOR AND DRAINVALVE RIGID PIPE CRACKED AROUND THE FLARED END AT THE FCU ATTACHMENT. FUEL LEAKING FROM PIPE.
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