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 CA041217006Line · wrong part(CAN) DURING ENGINE VISUAL INSPECTION AT PWC, WE HAVE IDENTIFIED THAT 2 ITEMS FROM THE FUEL PRESSURE TUBING WERE NOT GENUINE AND WERE MANUFACTURED BY AN UNKNOWN SOURCE. THOSE 2 ITEMS HAVE NO IDENTIFICATION NUMBERS BUT WERE INSTALLED IN REPLACEMENT OF: FUEL CONSDR CA041215007Engine · failed(CAN) DURING CLIMB (6000 FT) THE ENGINE EXPERIENCED AN UNCOMMANDED POWER ROLL-BACK ACCOMPANIED BY ITT INCREASE, A LOUD BANG AND FLAMES EVIDENT FROM THE EXHAUST. THE PILOT SHUT THE ENGINE DOWN IN FLT, DECLARED AN EMERGENCY AND SUBSEQUENTLY LANDED ON A ROAD. PWSDR 04FDEA03389Filter · cloggedAFTER T/O DURING LANDING GEAR RETRACTION, OBSERVED BOTH NR 1 AND 3 ENG FUEL FILTER PRESSURE DROP LIGHTS WERE ILLUMINATED. AFTER SELECTING CLIMB POWER. THE NR 3 LIGHT EXTINGUISHED AND NR 1 REMAINED ILLUMINATED. LEVELED OFF AT 5000 FT AND WHEN THE POWER WAS SDR DXTA200400461Fuel Filter · warning lightDURING TAKEOFF ROLL FUEL FILTER L-ANNUNCIATOR ILLUMINATED. TAKEOFF ABORTED, ANNUNCIATOR EXTINGUISHED DURING ABORT. REPLACED LEFT AND RIGHT ENGINE FUEL FILTER AND ASSOCIATED PACKING. PERFORMED SATISFACTORY ENGINE RUNS AND LEAK CHECKS. REFERENCE P + W 545 AMSDR DXTA200400460Filter · warning lightDURING TAKEOFF ROLL MASTER CAUTION ILLUMINATED TRIGGERED BY RIGHT ENGINE FUEL FILTER BY-PASS ANNUNCIATOR. REMOVED AND REPLACED RT FUEL FILTER IAW P&W 545 MM CHAPTER 73-10-07. LEAK CHECK GOOD, FILTER INSTALLED IS NEW. OPERATIONAL CHECK SATISFACTORY.SDR CA041129018Manifold · malfunctioned(CAN) AFTER REPLACING A SET OF FUEL MANIFOLD ADAPTERS ON A PT6A-27 ENG, A GROUND RUN WAS CARRIED OUT. THE RESULTING GROUND RUN SHOWED SIGNS OF FUEL LEAKAGE FROM THE TRANSFER TUBES P/N 3011155.ENGINE PERFORMANCE DATA SHOWED THAT THE T5 TEMPERATURE AND FUEL FLOWSDR CA041126004Line · cracked(CAN) UPON DECENT INTO AIRPORT POWER LEVER STAGGER WAS ENCOUNTERED BY FLIGHT CREW. UPON LANDING AND TAXING THE OIL PRESSURE COULD NOT BE MAINTAINED AND THE FLIGHT CREW SHUT DOWN THE ENGINE. UPON INVESTIGATION THE FUEL FLOW TRANSMITTER LINE WAS FOUND CRACKED SDR CA041209008Line · cracked(CAN) WHILE ON A SLING OPERATION, PILOT NOTICED A FLUID LEAKING FROM THE BELLY IN THE CARGO MIRROR. THE AIRCRAFT WAS LANDED IMMEDIATELY AND IT WAS DISCOVERED THAT FUEL WAS LEAKING FROM A FUEL LINE FITTING. THE ENGINE WAS SHUT DOWN AND THE LINE WAS CHECKED FOR SDR CA041119008Fuel Line · damaged(CAN) DURING A SCHEDULED OIL PUMP REPLACEMENT SEVERE WEAR WAS FOUND ON THE PRIMARY FUEL MANIFOLD FEED LINE NEAR THE FUEL FLOW TRANSMITTER. THE DAMAGE WAS CAUSED BY CONTACT BETWEEN THE FUEL FLOW TRANSMITTER INLET LINE B-NUT AND THE FEED LINE DUE TO LACK OF CLESDR DXTA200400433Pressure Switch · defectiveAT POWERING UP FOR TAKEOFF THE AMBER FUEL FILTER BYPASS R CAS MESSAGE CAME ON, ABORTED TAKEOFF. TROUBLESHOT AND FOUND FUEL FILTER DPI SWITCH DEFECTIVE. REMOVED WITH NEW SWITCH. OPS CHECK AND LEAK CHECKED GOOD. WORK DONE IAW ROLLS ROYCE AE3007C MM CHAPTER 7SDR DL777040991Line · chafedFUEL LEAK FROM ENG AFTER START, FOUND FUEL LEAKING FROM LINE BETWEEN FMU AND DRAIN CANISTER. REMOVED AND CLEANED FMU DUMP FILTER REF 73-21-13-100-801. REMOVED DRAIN LINE DUE DAMAGE AT CLAMP AREA INSTALLED NEW LI PURCHASED FROM AA P/N FK21039, AA P/N 4066928SDR 04FDEA02993Warning Light · illuminatedFUEL FILTER CLOG LIGHT ON T/O AT 60KTS. REJECTED T/O. ALL INDICATIONS NORMAL ON 60 PERCENT RUNUP FOR ENG ANTI-ICE. ECAM WARNING STOPPED STOPPED AS SOON AS POWER WAS REDUCED. I THINK IT WAS NR 1 ENG, BUT AM NO T POSITIVE. ENT BY: 001941 RPT BY: 119121 FASDR 4025Line · failedON TAKEOFF OUT OF TAMPA, ENGINE STARTED SURGING, RETURNED TO TPA. MAINTENANCE FOUND RUBBER PIECES IN FUEL INJECTION UPPER DECK LINE, CLEANED UPPER DECK AND CHANGED RUBBER HOSES, OPS CHECKS GOOD.SDR PG9R97678Fuel Nozzle · crackedCRACKED SHROUD/ REPLACED. (K)SDR PG9R97676Fuel Nozzle · crackedNOZZLE CRACKED/ REPLACED. (K)SDR CA040924004Line · leaking(CAN) FUEL LEAK DISCOVERED IN THE AREA COVERED BY AD (CAMPAIGN) NR 9-0065.SDR B7T2004F00000Hose · leakingAIRCRAFT ON CLIMB-OUT, AT 200 FT AGL ENGINE SURGED AS IF IT WAS NOT RECEIVING ENOUGH FUEL. PILOT SWITCHED FUEL TANKS (FROM RT TANK TO LT TANK) AND FUEL BOOST PUMP WAS TURNED ON AND ENGINE SMOOTH OUT FUEL BOOST WAS TURNED OFF AND IN APPROXIMATELY 10 SECONDS LASDR C7GR861JManifold · misinstalledLTS101-750B-1 ENGINE, SN: LE-48166BEF WAS RECEIVED BY THIS REPAIR STATION (CRS NR C7GR861J) FOR ROUTINE MAINTENANCE. SINCE WE HAD RECEIVED SOME NEW MANIFOLD ASSEMBLIES WITH IMPROPERLY TORQUED BOLTS (16 EA) THAT SECURE EIGHT COVERS ON THE INJECTOR BLOCKS, DECISDR CA040810004Line · worn(CAN) WHEN INSTALLING INSPECTION PANEL ON LT OB NACELLE FOUND FUEL LINE FROM FUEL BOWL FORWARD TO ENGINE WAS CHAFING ON BULKHEAD IN SIDE OF NACELLE. THE LINE WAS WORN ABOUT A QUARTER OF ITS WALL THICKNESS.SDR CA040812008Manifold · chafed(CAN) DURING RECEIVING INSPECTION A 0.010 (DAMAGE TO FUEL MANIFOLD),SDR CA040803009Vent Line · disconnected(CAN) DEFECT WAS RECORDED, RT FUEL LEAK REPORTED FROM RT NACA FUEL VENT . THIS WAS SECOND OCCURRENCE. AFTER INSPECTION, MAINT DISCOVERED THAT FUEL VENT LINE WAS DISCONNECTED (SEPARATED) AND NOT LINED UP, (TO SHORT). PROBLEM WAS RELATED TO THE MFG NOT DELIVERSDR CA040929005Manifold · leaking(CAN) INVESTIGATION OF AN UNCOMMANDED ENGINE IFSD REVEALED FUEL LEAKAGE AT THE ENGINE FUEL MANIFOLD. THE MANIFOLD IS UNDER INVESTIGATION AT MFG. THIS REPORT WILL BE SUPPLEMENTED TO PROVIDE ROOT CAUSE, ONCE ESTABLISHED.SDR CA040811004Line · cracked(CAN) FUEL LEAK DISCOVERED AT LT INJECTOR ON START UP. START ABORTED. UPON INSPECTION, FUEL SUPPLY LINE WAS FOUND CRACKED AT FLARE. LINE REPLACED, A/C RETURNED TO SERVICE. A NUMBER OF THIS PARTICULAR P/N LINES HAVE FAILED IN THE PAST. RECOMMEND USING ADDISDR VJ02004F00000Hose · failedDURING OWNER REQUESTED OIL CHANGE FOUND LW-13175-4-340 HOSE GUSHING FUEL ON TO ENGINE. HOSE FAILED OVER 10 INCH SECTION. INSTALLED NEW TSO-C53A TYPE D HOSE. FAILED HOSE WAS ORIGINAL INSTALLED AT MFG OF AIRCRAFT. HOSE MFG 2Q78, OLD BLACK RUBBER STYLE. IF ASDR P5CA0401115Drain Mast · leakingAFTER ENGINE START, NR 3 ENGINE LEAKING FUEL, RETURNED TO THE GATE. FOUND FUEL LEAKING FROM DRAIN MAST, AFTER ENGINE START. SUSPECTED LEAK FROM STRUT DRAIN, DISCONNECTED DRAIN PIPE, WET SPAN ENGINE AT IDLE, STILL NO LEAKS EVIDENT, ENGINE COWL SECURED, OK FORSDR 198M2004Filter · contaminatedAIRCRAFT EXPERINCED A SERIES OF FUEL BY-PASS INDICATIONS. DURING THE TROUBLESHOOTING WE DISCOVERED THE FILTERS TO HAVE BEEN CONTAMINATED WITH DIEGME AS A RESULT OF USING AN ANTI-ICE ADDITIVE. I FOLLOWED THE OEM M/M AND REMOVED ALL FUEL PARTS ON ALL THREE ENGINSDR CA040707003Manifold · crackedSLIGHT FUEL ODOR IN CABIN WHEN AIRCRAFT SLOWED FOR LANDING. THE CREW NOTICED FUEL DRIPPING FROM THE RT ENGINE AFTER SHUTDOWN. MAINTENANCE FOUND A CRACKED FUEL MANIFOLD INLET ELBOW. THE MANIFOLD WAS REPLACED.SDR GW12004F00003Line · fracturedPILOT REPORTED FUEL DRIPPING OUT OF COWLING ON SHUT DOWN. REMOVAL OF COWLING AND GROUND RUN OF ENGINE REVEALED FRACTURE OF HIGH PRESSURE FCU TO FUEL NOZZLE DELIVERY TUBE. TUBE WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE.SDR CA040702003Bar · broken(CAN) DURING CRUISE THE FLIGHT CREW NOTICED SEVERE SURGING ON THE NR 1 ENGINE. THE FUEL FLOW WAS ALSO DROPPING AND SURGING. THE ENGINE WAS SHUT DOWN AND THE PROPELLER WAS FEATHERED. THE AIRCRAFT RETURNED TO DEPARTURE. DURING INVESTIGATION MAINTENANCE CREW FOUNSDR QXEA200400474Valve · leakingSEA - FLIGHT 2065 - FUEL WAS NOTED DRIPPING FROM THE FORWARD FUEL DOOR AT A RATE OF 11 DRIPS PER MINUTE. MAINTENANCE INSPECTED THE AREA AND FOUND THE REFUEL / DEFUEL VALVE LEAKING. THE VALVE WAS REPLACED AND OPERATIONAL CHECKS WERE PERFORMED. THE CHECKS WERSDR P5CA0401105Manifold · leakingFUEL DRAINING FROM DRAIN MAST NR 3 ENGINE PORT ON ENGINE START. REPLACED NR 3 ENGINE VBR FUEL MANIFOLD ASSY AS PER MM 75-32-00. OPS & LEAK CHECK OK AS PER MM 71-00-00 TEST NR 3.SDR 2004FA0000632Line · crackedPILOT EXPERIENCED EGT FLUXUATIONS, MADE PRECAUTIONARY LANDING. INSPECTION REVEALED CYLINDER NR 4 INJECTOR LINE WAS CRACKED AND LEAKING FUEL AT THE BASE OF THE BRAZED ON SLEEVE BETWEEN THE SLEEVE AND THE BALL END.SDR 2004FA0000571Servo · inoperativeAIRCRAFT WAS REPORTED, ENGINE DIES ON IDLE SPEED, EXCESSIVE RICH MIXTURE, BLACK SMOKE EMITTED FROM EXHAUST. IDLE SPEED AND MIXTURE COULD NOT BE ADJUSTED IAW AD 2001-06-17 INSTRUCTIONS REF D, L, I, THRU 2, 1.SDR 2005FA0000053Line · leakingMRR-M04-11, ENGINE RPM ONLY WENT TO 97 PERCENT DURING TAKEOFF ROLL AND TORQUE WAS ALSO LOW, ALSO, THERE WAS LITTLE RESPONSE TO POWER LEVER MOVEMENT. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. INITIALLY SUSPECTED FCU FAILURE, BUT UPON INSPECTION FOUND FCUSDR 2004FA0000573Clamp · crackedAD WAS COMPLIED WITH AT 250 HOURS BY INSP AND INSTALLATION OF MFG SERVICE KIT (PN CK-002) (WORM TYPE CLAMP) INSTALLED ON THE FUEL PRESSURE TRANSDUCER. THE CLAMP WAS TORQUED TO THE EXACT TORQUE AS CALLED. 6/2/04-DURING AN OIL CHANGE THE CLAMP SUPPLIED IN KIT SDR CALA0400493Shutoff Valve · shortedTHE AUTOTHROTTLE DISCONNECTED AND THE NR 1 ENGINE AUTO SHUTDOWN ON FINAL APPROACH TO IAH. NO RESTART WAS ATTEMPTED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND CANNON PLUG D05162P SHORTED WHICH CAUSED THE NR 1 ENGINE FUEL S/O VALVE TO POWSDR DXTA200400312Warning Light · illuminatedON TAKE-OFF AT 60 KNTS, (FUEL FILTER BYPASS L) CAS MESSAGE CAME ON, ABORTED TAKE-OFF. ITEM IS UNDER INVESTIGATION.SDR CA040510004Ring · damagedHAVE HAD SEVERAL OCCURRENCES OF FUEL LEAKS FROM THE JT8D FUEL FLOW TRANSMITTERS. THE LEAKS ARE EVIDENT AT VERY HIGH POWER SETTINGS. A FLEET CAMPAIGN HAS BEEN COMPLETED WHICH CHECKED ALL ENGINES FOR LEAKS AND RECTIFIED DEFECTS. AN EXTENSIVE INVESTIGATION IS BESDR 2004FA0000373Manifold · malfunctionedENGINE DIED ON DOWNWIND. PILOT LANDED SAFELY. ENGINE STARTED ON GROUND, BUT WAS IDLING AT 750 HAS BEEN SET AT 900. ALSO, HAD NO MIXTURE RISE. DURING SETUP FOR FUEL PRESSURE TESTS THE LINE FROM THE THROTTLE BODY TO THE FUEL MANIFOLD HAD RESIDUAL PRESSURE. THE FSDR AUS20040361Hose · loose(AUS) ENGINE FUEL HOSE LEAKING AT CONNECTION TO CHECK VALVE. FUEL LEAKING INTO ENGINE BAY. HOSE HAD NOT BEEN TIGHTENED DURING MAINTENANCE. PERSONNEL/MAINTENANCE ERROR.SDR CA040727010Pressure Valve · unserviceable(CAN) FUEL LEAKING INTO FUEL WHEEL LINE WITH BOOST PUMP PRESSURE. ENGINE LIGHTING OFF FUEL WHEEL. VALVE REPLACED , NOW LIGHTS OFF AT NEAR 17 PERCENT NG.SDR CA040727012Pressure Valve · unserviceable(CAN) FUEL ENTERING WHEEL EARLY, VALVE CHANGED. LIGHT OFF OCCURING NOW AT 17 PERCENT NG (NORMAL).SDR CA040413011Pump · failed(CAN) DURING ROUTINE INSPECTION ALUMINUM PARTICLES WERE FOUND IN THE AIRFRAME FUEL FILTER DOWNSTREAM OF THE FUEL BOOST PUMP. RUNNING THE BOOST PUMP SHOWED THAT WHILE IT MAINTAINED OPERATING PRESSURE AN INTERMITTENT GRINDING NOISE COULD BE HEARD. DISSASEMBLY OSDR CA050406006Fitting · leaking(CAN) ENGINE LOST POWER, SUBSEQUENT INSPECTION REVEALED A LOOSE FITTING ON THE INLET SIDE OF THE MECHANICAL FUEL PUMP CAUSING PUMP TO DRAW AIR THUS DEPLETING THE FUEL TO THE CARBURETOR. THE FITTING WAS TIGHTENED AND LOCK FLUID WAS USED ON THE JAM NUT ONLY, NOTSDR BAQA094034Manifold · cloggedUNIT REMOVED DUE TO SUSPECT CLOGGING, RETURNED TO TEC BY TONY N, WITHOUT NOTIFICATION. HARCARD WAS ENCLOSED. REPLACED WITH SERVICABLE UNIT. 04/01/2004SDR BAQA094033Manifold · cloggedUNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004SDR BAQA094032Injector · cloggedUNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004SDR BAQA094031Manifold · cloggedUNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004SDR BAQA094030Manifold · cloggedUNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004SDR BAQA093896Line · damagedEXCHANGE. ENG S/N LE45573. MANIFOLD HAS TUBE DAMAGE. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/23/2004
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