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.

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 CONDec 17, 2004SDR 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. PWDec 14, 2004 · Pilats PC12SDR 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 Dec 7, 2004 · N306FE · Doug DC1030FSDR 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 AMNov 30, 2004 · N670QS · Cessna 560XLSDR 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.Nov 29, 2004 · N621QS · Cessna 560XLSDR 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 FLOWNov 26, 2004SDR 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 Nov 25, 2004 · Swrngn SA227ACSDR 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 Nov 19, 2004 · Bell 206BSDR 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 CLENov 18, 2004SDR 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 7Oct 28, 2004 · N949QS · Cessna 750SDR 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 4066928Oct 26, 2004 · N860DA · Boeing 777232SDR 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 FAOct 25, 2004 · N410FE · Airbus A310SDR 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.Oct 22, 2004 · N3547C · Piper PA31350SDR PG9R97678Fuel Nozzle · crackedCRACKED SHROUD/ REPLACED. (K)Oct 13, 2004 · N1076T · Bell 206L1SDR PG9R97676Fuel Nozzle · crackedNOZZLE CRACKED/ REPLACED. (K)Oct 13, 2004 · N22425 · Cessna STC206CSDR CA040924004Line · leaking(CAN) FUEL LEAK DISCOVERED IN THE AREA COVERED BY AD (CAMPAIGN) NR 9-0065.Sep 19, 2004 · Airbus A330*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 LAAug 23, 2004 · N1673U · Cessna 207SDR 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, DECIAug 20, 2004SDR 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.Aug 6, 2004 · Beech 1900CSDR CA040812008Manifold · chafed(CAN) DURING RECEIVING INSPECTION A 0.010 (DAMAGE TO FUEL MANIFOLD),Aug 5, 2004 · Urocop EC120BSDR 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 DELIVERJul 29, 2004 · Fokker F28MK0100SDR 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.Jul 23, 2004 · Cessna 550SDR 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 ADDIJul 21, 2004 · Snias AS350BASDR 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 AJul 21, 2004 · N3014X · Piper PA32300SDR 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 FORJul 9, 2004 · N452PA · Boeing 74746NFSDR 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 ENGINJul 9, 2004 · N198MSDR 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.Jul 6, 2004 · Beech B100SDR 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.Jul 2, 2004 · N121LH · Piper PA42720SDR 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 FOUNJun 30, 2004 · Cvac 440SDR 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 WERJun 23, 2004 · N367PH · Dhav DHC8202SDR 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.Jun 20, 2004 · N505MC · Boeing 7472D3BSDR 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.Jun 15, 2004 · N421GF · Cessna 421CSDR 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.Jun 10, 2004 · N974SP · Cessna 172SSDR 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 FCUJun 2, 2004 · N159MC · Swrngn SA227ACSDR 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 Jun 2, 2004 · N419JK · Lancar LC40550FGSDR 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 POWMay 19, 2004 · N14639 · Boeing 737524SDR DXTA200400312Warning Light · illuminatedON TAKE-OFF AT 60 KNTS, (FUEL FILTER BYPASS L) CAS MESSAGE CAME ON, ABORTED TAKE-OFF. ITEM IS UNDER INVESTIGATION.May 14, 2004 · N986QS · Cessna 750SDR 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 BEMay 7, 2004 · Boeing 737217SDR 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 FMay 6, 2004 · Diamon DA20C1SDR 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.May 1, 2004 · Cessna 210MSDR 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.Apr 28, 2004 · Snias AS350BASDR CA040727012Pressure Valve · unserviceable(CAN) FUEL ENTERING WHEEL EARLY, VALVE CHANGED. LIGHT OFF OCCURING NOW AT 17 PERCENT NG (NORMAL).Apr 23, 2004 · Snias AS350B2SDR 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 OApr 9, 2004 · Cessna 208BSDR 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, NOTApr 4, 2004 · Piper PA28140SDR BAQA094034Manifold · cloggedUNIT REMOVED DUE TO SUSPECT CLOGGING, RETURNED TO TEC BY TONY N, WITHOUT NOTIFICATION. HARCARD WAS ENCLOSED. REPLACED WITH SERVICABLE UNIT. 04/01/2004Mar 24, 2004 · N135MF · Urocop EC135T1SDR BAQA094033Manifold · cloggedUNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004Mar 24, 2004 · N135MF · Urocop EC135T1SDR BAQA094032Injector · cloggedUNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004Mar 24, 2004 · N135MF · Urocop EC135T1SDR BAQA094031Manifold · cloggedUNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004Mar 24, 2004 · N135MF · Urocop EC135T1SDR BAQA094030Manifold · cloggedUNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004Mar 24, 2004 · N135MF · Urocop EC135T1SDR BAQA093896Line · damagedEXCHANGE. ENG S/N LE45573. MANIFOLD HAS TUBE DAMAGE. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/23/2004Mar 19, 2004 · N213AE · Bolkms BK117B1
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