JASC 2820
Service difficulty reports · 3,631
Reports filed under 2820 · Aircraft Fuel Distribution System, 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 = '2820' 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 = '2820' 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 2004FA0000319Fuel Line · corrodedFRONT FUEL LINE FROM LT WING TANK WAS IN CONTACT WITH FRESH AIR DUCT IN THE WING, AERO DUCT PN CEET 1.5 INCH. THIS CAUSED CORROSION ON THE ALUMINUM FUEL LINE. PROBLEM WAS FOUND WHEN FUEL STARTED LEAKING OUT OF THE WING. REPLACED FUEL LINE AND FRESH AIR DUCTSDR AALA20040071Valve · inoperativeDURING CRUISE DECREASED FUEL NOTED LT MAIN TANK, QTY LT TANK STABILIZED 63,300 LBS. RT MAIN TANK INCREASED 64,500 LBS TO 66,900 LBS WHILE CONTINUING TO USE CENTER TANK FUEL PROBES 18, 19, 20 LT MAIN TANK INDICATED LOWER HEIGHT PROBES 18, 19, 20 RT MAIN TANK. SDR AALA20031384Fuel Tank · malfunctionedEN ROUTE SJC-NRT AN UNWANTED FUEL TRANSFER AS A GRADUAL DECREASE IN FUEL NOTED IN LEFT TANK AND STABILIZED AT 63300 POUNDS WHILE INCREASING IN RIGHT TANK FROM 64500 TO 66900 WHILE USING CENTER TANK. LANDED LAX WITHOUT INCIDENT. A/C FERRY TO DFW FOR FURTHER EVASDR ABO2003F00000Sensor · leakingINVESTIGATED FUEL LEAK, FOUND BOTH FUEL SENDING UNITS LEAKING INTO AVIONICS BAY WITH STANDING FUEL, THIS BAY IS LOCATED BETWEEN THE WINGS, THIS IS A FIRE HAZARD.SDR 2003FA0001205Vent · corrodedFOUND FUEL LEAK RT DOOR FRAME, CAUSED BY CORROSION AND CHAFING OF FUEL VENT PIPE IN WING ROOT. INSPECTED L/S AND FOUND BEGINNINGS OF LEAK ON THAT SIDE ALSO.SDR AUS20031226Check Valve · cracked(AUS) CENTER FUEL TANK RT BOOST PUMP DISCHARGE CHECK VALVE BODY CRACKED. CRACK LENGTH APPROXIMATELY 31.75MM (1.25IN).SDR AUS20031296Hose · deteriorated(AUS) REAR ENGINE FUEL PRESSURE HOSE LOCATED BETWEEN FIREWALL AND FUEL MANIFOLD DETERIORATED AND LEAKING ONTO LT EXHAUST STACK.SDR 2004FA0000268O-Ring · wornTHE CHECK VALVE BETWEEN THE AUXILIARY FUEL TANK AND THE RT MAIN TANK FAILED, ALLOWING FUEL FROM THE RT MAIN TO DRAIN INTO THE AUX TANK AND OVERFLOW FROM THE FILLER NECK. THE PUMP AND VALVE ASSEMBLY IS INTENDED TO MOVE FUEL FROM THE AUX TANK TO THE RT MAIN TANSDR CA031127009Line · corroded(CAN) DURING A FUEL SELECTOR CHANGE INTERGRANULAR CORROSION WAS NOTED ON THE FUEL LINE ELBOW. CORRODED PART REPLACED WITH NEW UNIT.SDR 39906Line · leakingFUEL ODOR IN CABIN CAUSED US TO REMOVE SIDEWALLS TO TRACE LINES. FOUND BOTH CROSSOVER LINES AND SCUPPERS WET WITH FUEL. COULD NOT GET LINES TO STOP LEAKING BY TORQUING. DEFUELED AND DISASSEMBLED ALL FITTINGS ASSOCIATED. CLEANED AND INSPECTED AND FOUND ALL SDR BAQA091136Fuel Tank · leakingFUEL TANK LEAKING. REPLACED WITH SERVICEABLE UNIT. 11/25/03SDR BAQA091135Fuel Tank · leakingFUEL TANK LEAKING. REPLACED WITH SERVICEABLE UNIT. 11/25/03SDR 2003FA0001262Vent · obstructedON RUNUP, ENGINE WOULD QUIT. ALLOWED TO SIT APPROX 3 MINUTES, IT WOULD START AND RUN, THEN QUIT. WHEN FUEL CAP WAS REMOVED A WHOOSH OF INCOMING AIR WAS HEARD. ENGINE RAN WITH THE CAP OFF. SUSPECT ICE BLOCKING FUEL VENT LINES INSIDE WING. AFTER OVERNIGHTSDR HNAA0300072Line · detectedINTERMITTENT NR 1 FUEL PRESSURE CAUTION LIGHT DURING CLIMB OUT. (OCCURRED AFTER TURNING OFF AUX FUEL PUMP) INSTALLED NEW MOTIVE FLOW LINES FROM COLLECTOR BAY TO ENGINE FIREWALL.SDR AMCR200300008Control Valve · leakingUPON RETURN FROM FLIGHT, MINOR FUEL LEAKAGE WAS OBSERVED ON AFT FUSELAGE. DURING FUELING, FOUND THE FUELING PRESSURE CONTROL VALVE LEAKING. INVESTIGATION REVEALED THAT EXCESSIVE FUELING PRESSURE MAY HAVE BEEN EXCEEDED WHEN AWAY FROM BASE. SUGGEST OPERATORS MOSDR CA031126001Line · leaking(CAN) REFERENCE AIRCRAFT SB 351 054 AIRFRAME FUEL FILTER SUBSTITUTION. FUEL LINE PN 351-054-1 LEAKS THROUGH THE STAINLESS STEEL BRAIDED CASING OF THE LINE. MAINTENANCE SUSPECTS THE LINE HAS DETERIORATED WITH AGE. THE LINE WAS MANUFACTURED IN 1994 AND HAS ACCUSDR 2003FA0001210Line · swollenFUEL LINES IN LT AND RT DOOR POSTS FOUND SWOLLEN AND POROUS. RADIUS BEND AREA NEAR LOWER PORTION OF DOOR POST IS THE AREA AFFECTED.SDR CA031114001Ejector · cracked(CAN) FUEL WAS TRANSFERRING FROM THE RT TANK TO THE CENTER TANK. THE TRANSFER WAS NOTICED WHILE THE A/C WAS ON GROUND. INVESTIGATION REVEALED THAT THE RT PRIMARY EJECTOR WAS CRACKED AND THE FUEL WAS LEAKING FROM THE EJECTOR TO THE CENTER TANK. THE EJECTOR WSDR 03FDEA01869Line · crackedDURING THE PRESSURE TEST OF TAIL TANK FUEL SHROUD DRAIN SYSTEM FOUND TAIL TANK TRANSFER FUEL SHROUD TUBING LOCATED AT STA. Y 1791 LT SIDEWALL OF CENTER CARGO WITH A CRACK LINE MEASURED APPROX. 1 INCH IN LENGTH. COMPLIED WITH EA 1-2822-71762 FUEL SYSTEM -SDR RU3A03017Float · damagedFUEL LEAK IN FLT AND ON GROUND AFTER LANDING, RT WING, LOWER SURFACE, 500 LBS FUEL LOST. REPLACED FAULTY FUEL VENT FLOAT ASSEMBLY. (M)SDR AUS20031166Hose · deteriorated(AUS) FUEL SUPPLY HOSE FROM TANK OUTER SECTION PERISHED.SDR AUS20031165Hose · deteriorated(AUS) FUEL SUPPLY HOSE FROM TANK OUTER SECTION PERISHED.SDR CA031029006Line · worn(CAN) DURING ROUTINE INSP, TECH WAS FOCUSED ON STEERING ARM INSTALLATION AND NOTICED THAT RT STEERING ARM WAS CHAFING ON FUEL LINE. SECTION OF FUEL LINE AFFECTED RUNS FROM UNION FITTING NEAR FUEL SELECTOR TO FUEL STRAINER BOWL LOCATED AT FIREWALL. REASON FOR SDR CA031017009Check Valve · failed(CAN) AFTER PILOTS HAD DEPLANED PASSENGERS AND BAGGAGE AT A SCHEDULED STOP THEY NOTICED FUEL COMING OUT OF THE FUEL VENT. MAINTENANCE TOWED THE A/C TO THE HANGER AND DEFUELED THE A/C. THEY FOUND THAT THE ONEWAY VALVE GOING TO THE AUX TANK, SOMETHING HOLDING SDR CNMA200300004Relief Valve · leakingFUEL REPORTED LEAKING INFLIGHT FROM RIGHT AILERON AREA- FUEL QUANTITY LOSS CONFIRMED. AIR TURNBACK TO FRA.SDR 2003UALA00772Valve · defectiveFUEL IMBALANCE BETWEEN LT AND RT TANKS. THE CAUSE OF THE FUEL IMBALANCE CONDITION WAS DUE TO A DEFECTIVE CROSS-FEED VALVE BODY ASSY. SHOP FINDINGS REVEALED THAT THE SPLINE AND SEAL ON THE VALVE DISK WERE WORN OUT. THIS WAS THE FIRST TIME THE VALVE WAS REMOVED SDR 55032Line · looseODOR OF FUMES FROM COCKPIT. TIGHTENED RT ENG P3 SUPPLY LINE B NUT. OPS CK NORMAL. NO FUMES NOTEDSDR UIEA200300059Actuator · failedDIVERSION TO ANC, ENROUTE CREW REPORTED EICAS MESSAGE FUEL IMBALANCE 1-4. CHECKLIST COMPLETED. NR 4 CONTINUED TO DECREASE, NR 3 REMAINED CONSTANT QUANTITY. SYSTEM CONTROL ADVISED AND AIRCRAFT DIVERTED TO ANC DUE TO FUEL LEAK FROM NR 4 MAIN TANK. MAINTENANCSDR CA031021007Lever · broken(CAN) LT ENGINE DID NOT START. NO FUEL FLOW. MAINTENANCE FOUND FUEL VALVE CONTROL CABLE BROKEN AT LT AFT FUSELAGE SECTION. A FLEET CAMPAIGN WILL BE PERFORMED. AWAITING RESULT.SDR HALA0300875Actuator · failedFUEL CROSS FEED VALVE REMAINED ILLUMINATED WHEN OPEN OR CLOSED. FUEL CROSS FEED EICAS LIGHT ILLUMINATED. REMOVED AND REPLACED FUEL CROSS FEED ACTUATOR IAW AM. REPLACED CONNECTOR D1544. OPS CHECK OK IAW AMM, MPN, SN ON 439391; SN OFF 3696(K)SDR CA030930013Tube · burned(CAN) DURING AMJOR INSPECTION (C-CHECK AND 96 MTH INSP.) A FUEL TUBE ASSEMBLY IN CENTER TANK WAS DISCOVERED WITH EVIDENCE OF ARCING. FURTHER INSPECTION REVEALED ADJACENT PART (STIFFENER PN 60010011193) HAD ALSO SIMILAR EVIDENCE OF ARCING. TUBE ASSEMBLY WAS RESDR AUS20030989Line · leaking(AUS) NR 1 ENGINE FUEL FEED LINE FROM FRONT SPAR TO PYLON LEAKING. LINE WAS WORN IN AREA OF O RING SEAL.SDR ACE0918021Diaphragm · perforatedON PREFLIGHT INSPECTION, PILOT NOTICED FUEL LEAKING FROM THE ENGINE GANG DRAIN. MAINTENANCE REPLACED THE LOW PSI FUEL PUMP DUE TO FUEL DRAINING FROM THE DRY SIDE OF THE PRESSURE RELIEF VALVE ASSEMBLY. DISASSEMBLY OF THE PUMP REVEALED MULTIPLE HOLES IN THE DISDR C2XA03IA094Fitting · crackedDURING POST FLIGHT THE CREW NOTED EVIDENCE OF A FUEL LEAK ON NR 1 ENGINE. MAINTENANCE FOUND A CRACKED FITTING ON THE NR 1 ENGINE FPMU. THE FITTING WAS REMOVED AND REPLACED, AND A LEAK CHECK WAS PERFORMED, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETUSDR 2003FA0000937Vent Line · chafedTHIS AIRCRAFT IS EQUIPPED WITH OPTIONAL INBOARD FUEL FILLER CAPS. THE FUEL FILLER CAP ADAPTER ASSY. (P/N C156005-0105) HAS A SPRING LOADED FLAPPER WHICH IS DEPRESSED BY THE FUEL DISPENSING NOZZLE WHILE FILLING THE TANK. THE FLAPPER HAS BEEN HITTING ON THE (PSDR S03428074Valve · failedB18271 20 MINS AFTER REFUELING COMPLETED AND WITH CORRECT LEVEL IN EACH TANK FUEL SPILL FROM LT SURGE TANK. REPLACED NR 1 MAIN TANK REFUELING VLV IN LAX. PARTS FROM UA. REPLACED NR 1 CROSSFEED VALVE AND BOOSTER PUMP BYPASS CHECK VALVE WHILE A/C ARRIVED TPE.SDR A6WA200340135Solenoid Valve · leakingSUSPECT FUEL LEAK AT APU BAY. INSPECTED AND FOUND NO FUEL LEAKS SUSPECT APU FUEL SOLENOID VALVE NOT FULLY CLOSING. REMOVED AND REPLACED FUEL SOLENOID VALVE. OPS AND LEAK CHECK GOOD. (M)SDR QXEA200301116O-Ring · leakingFUEL LEAKING FROM UNDERWING CENTER AREA DURING REFUELING. REMOVED AND REPLACED BOTH O-RINGS AT COUPLING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR 2003FA0001054Valve · failedDURING ROUTINE PHASE INSPECTION, THE MANIFOLD VALVE WAS FOUND TO BE LEAKING FUEL THROUGH THE AIR VENT. PROBABLE CAUSE IS INTERNAL FAILURE OF THE DIAPHRAGM. NO RECOMMENDATION AT THIS TIME.SDR AMTA200301064Pressure Switch · faultyEICAS MESSAGE 'CTR L FUEL PUMP'. TROUBLESHOT PER FIM 28-22-00 FIG 105. REMOVED AND REPLACED LEFT OVERRIDE PUMP PSI SWITCH. OPS AND LEAK CHECK GOOD PER MM 28-42-01-4. (M)SDR 2003FA0000849Fuel Line · wrong partDURING AN ANNUAL INSPECTION THE FUEL HOSES THAT ARE ROUTED FROM THE RT SIDE OF FIREWALL TO FUEL PUMP HAD BEEN SEVERLY EXPOSED TO HEAT FROM RT EXHAUST STACK CAUSING ONE HOSE TO BUBBLE UP. THESE HOSES DID NOT HAVE FIRE SLEEVE ON THEM. THIS IS AN INFLIGHT FIRE SDR HEEA088624Tube · twistedTUBE TWISTED AND WILL NOT SEAL IN CELL. REPLACED WITH SERVICEABLE ASSY.SDR QXEA200300953O-Ring · leakingPSC- ON FLIGHT 2092 FUEL LEAK ON NR 2 ENGINE AHEAD OF FUEL DOOR. REMOVED AND REPLACED O-RINGS ON MASTER REFUEL/DEFUEL VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR HEEA088450Check Valve · failedFUEL SYSTEM CHECK VALVE FAILURE.SDR DL76G030708Actuator · inoperativeFUEL CROSSFEED VALVE WOULD NOT OPEN IN FLIGHT. VALVE ACTUATOR REPLACEDSDR 2003FA0000854Fuel Sys · contaminatedAIRCRAFT HAS CONTAMINANT IN FUEL SYSTEM, A WHITE GEL/PASTE SUBSTANCE THAT IS CAPABLE OF PASSING THROUGH SCREENS AND CAN CLOG SMALL ORIFICES SUCH AS FLOW DIVIDER BORES. RT ENGINE FAILED ON GROUND AS A RESULT OF FLOW DIVIDER BLOCKAGE, CONTAMINANT IS IN ENTIRE FSDR HEEA088492Tube · chafedFUEL SYSTEM TUBE CHAFED. REPAIRED.SDR HEEA088079Check Valve · inoperativeCAUSING TRANSFER LIGHT TO STAY ON.SDR QXEA200300842Pressure Switch · leakingSEA- ON FLIGHT 2471 FUEL LEAKING FROM CENTER TANK AREA. REMOVED AND REPLACED LEFT BOOSTER PUMP PRESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR RAIA00307188Flow Valve · malfunctioned5452-STL- RT FUEL PRESSURE FELL TO ZERO. MAINTENANCE REMOVED AND REPLACED MOTIVE FLOW VALVE ACTUATOR.
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