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 2003FA0000899Elbow · brokenAT CRUISE, PILOT NOTICED A BLUE FUEL STAIN STREAMING BACK FROM THE LEFT ENGINE COOLING LOUVRES. FOUND BROKEN 90 DEGREE ELBOW FITTING ON FUEL MANIFOLD VALVE INLET WAS BROKEN DUE TO VIBRATION OF ENGINE.SDR HEEA088496Tube · chafedFUEL TUBE CHAFED. SCRAPPED.SDR BAQA085214Servo · malfunctionedPILOT VALVE IS JAMMING. JUST REPAIRED AND UNIT WAS JUST INSTALLED WHEN PROBLEM OCCURRED.SDR HEEA088028Pressure Switch · stuckFUEL PRESSURE SWITCH STICKS CLOSED. REPLACED SWITCH.SDR EIA2003091Check Valve · bentJETTISON PUMP CHECK VALVE FOUND BENT. INSTALLED NEW VALVE. PART NUMBER 60-703137.SDR USAASB03090Control Panel · faultyCLT - FLT 1125 - EN ROUTE PIT TO MSY, THE FUEL CROSSFEED VALVE WOULD NOT CLOSE AND THE LEFT CENTER BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED WITH 1,000 LBS OF FUEL IN THE TANK. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED ASDR HEEA087468Hose · kinkedFUEL HOSE KINKED. REPLACED HOSE.SDR HEEA087467Hose · kinkedINLET FUEL HOSE KINKED. REPLACED HOSE.SDR HEEA087465Hose · corrodedFUEL HOSE HAS CORROSION AT SLEEVE ON BOTH ENDS. REPLACED HOSE.SDR 2003F00392Transfer Valve · failedRT TANK O'FILL, VENTED FUEL OPERATED IAW CESNA LETTER QTY WAS LESS THAN 32000 LBS. A FUEL TRANSFER CHECK WAS PERFORMED BY MAINTENANCE PER CESSNA MM. NO DEFECTS FOUND, SYSTEM FUNCTIONED NORMALLY. (M)SDR DHL2003806009Seal · leakingFUEL LEAK UNDER WING BETWEEN NR 3 & 4 PYLON. TORQUED GAMMA SEAL JUST OUTBOARD NR 3 PYLON LEAK CHECKED GOOD IAW M/M 28-21-14.SDR DHL2003604583Access Panel · corrodedRT C/W AUX TANK, PERFORM ANTI-CORROSION TREATMENT TO RT UPPER ACCESS DOOR NR 5056. REMOVED CORROSION ON 5056 RT UPPER ACCESS DOOR IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 43. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DSDR CA030606004Line · severed(CAN) DURING THE LAST OPS 4 INSPECTION, SEB 95-6, RUBBER FUEL HOSE INSPECTION AND REPLACEMENT WAS ACCOMPLISHED. SUBSEQUENT INSPECTION REVEILED THAT THE FUEL PRIMER LINE FROM THE MANIFOLD TO THE PRIMER T FITTING ROUTED NEAR THE ALTERNATOR PULLEY FOUND BROKEN INSDR QXEA200300674Switch · leakingBOI- FUEL LEAKING FROM MAIN LANDING WHEEL BINS. FOUND RIGHT ENGINE INLET PRESSURE SENSOR LEAKING. REPLACED SENSOR. LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR HEEA086962Line · corrodedDISSIMILAR METAL CORROSION DUE TO STEEL SLEEVE ON ALUMINUM TUBE.SDR QXEA200300665Cartridge · failedPDX- ON FLIGHT 2493 AFTER TAKEOFF GOT A LEFT TRANSFER SHUT OFF VALVE AMBER MESSAGE. NO CENTER TANK FUEL ABNORMALITIES NOTICED. AUTO TRANSFER APPEARED EXCESSIVE BUT NO ABNORMAL IMBALANCE OR ANY FUEL LOSS NOTED. APPROXIMITLY 15 MINUTES AFTER DEPARTURE LEFT TRSDR BAQA086745Line · leakingPUMP LEAKED FUEL BADLY FROM BOTH ENDS WHEN INSTALLED. NEVER PUT INTO SERVICE. 8130 AND HISTORICAL RECORD CARD ENCLOSED. REMOVED FROM ENGINE LE47204. REPLACED WITH SERVICEABLE UNIT.SDR AUS20031168Hose · deteriorated(AUS) FUEL HOSE LOCATED BETWEEN FUEL SELECTOR AND FUEL BOWL PERISHED.SDR AUS20030533Line · damaged(AUS) LOW PRESSURE FUEL SUPPLY LINE LEAKING FROM AREA APPROXIMATELY MIDWAY BETWEEN TWO END FITTINGS. LINE IS IN CONTACT WITH TWO FLEXIBLE TOILET SERVICING LINES IN THIS AREA. SUSPECT TUBE CORRODED THROUGH. INVESTIGATION BY MANUFACTURER FOUND THE DAMAGE TO BESDR HEEA086556Valve · inoperativeENGINE FAILS TO START AFTER SITTING IDLE FOR A WHILE. REPLACED WITH SERVICEABLE VALVE.SDR HEEA086555Valve · leakingFUEL VALVE LEAKING. REPLACED WITH SERVICEABLE VALVE.SDR AUS20030530Line · cracked(AUS) STAINLESS STEEL FUEL PIPE LOCATED BETWEEN FUEL FILTER BOWL AND BOWL DRAIN VALVE CRACKED BENEATH (B) NUT FERRULE AT DRAIN VALVE END.SDR 197051603Check Valve · failedFUEL TRANSFERS FROM RT TO LT WING WHILE AIRCRAFT IS NOT IN USE.SDR 051603Diaphragm · rupturedLOW PSI FUEL PUMP FOUND LEAKING ON RAMP - RUPTURED DIAPHRAGMSDR CA030515004Tube · grooved(CAN) THIS AC HAS CLEVELAND BRAKE STC INSTALLED. DURING MAIN GEAR RETRACTION AND EXTENSION LT MAIN GEAR FORWARD HYD BRAKE UNIT CONTACTED MAIN FUEL SUPPLY TUBE AND DAMAGED TUBE BY ERODING A TWO-INCH LONG BY ONE-QUARTER INCH WIDE GROOVE IN TUBE WALL. THIS FUEL TSDR 2004FA0000175Coupler · seizedP2 HEATER HOSE SEIZED ONTO THE FITTING AT THE ENGINE.SDR FFS2003F00019Line · leakingPILOT REPORTED LT FUEL BOOST PUMP CIRCUIT BREAKER POPPED IN FLIGHT. UPON INSPECTION OF FUEL PUMP IN LT WING ROOT, IT WAS APPARENT THERE HAD BEEN A BRIEF FIRE IN THE AREA. PLASTIC SPIRAL WRAP AROUND FUEL LINE HAD SHRUNK AND MELTED. PNEUMATIC LINE TH LT WING SDR CA030627015Line · chafed(CAN) ABOVE FUEL LINE WAS FOUND CHAFED DURING 200 HR INSPECTION. IT WAS DETERMINED THIS WAS CAUSED FROM RUBBING ON STEERING ROD MOUNT. THIS WOULD BE VERY DIFFICULT TO SEE BUT CLOSE INSPECTION SHOULD BE CARRIED OUT.SDR CA030411002Switch · cracked(CAN) FUEL BYPASS SWITCH REMOVED FOR TESTING AND FOUND TO BE UNSERVICEABLE DUE TO ELECTRICAL MALFUNCTION. UPON FURTHER INSPECTION IN COMPONENET SHOP THE END FITTING BASE WAS FOUND TO BE CRACKEDSDR MYN2003F00000Diode · failedDIODE CR 406 SHORTED, ALLOWING POWER FROM LT FUEL TRANSFER CIRCUIT TO FEED BACK TO THE RT FUEL TRANSFER CIRCUIT. WHEN LT TP FUEL SHUT OFF VALVE WAS COMMANDED ON AND RT TIP FUEL SHUTOFF VALVE COMMANDED OFF. THE RT TP FUEL SHUT OFF VALVE HAD POWER ON PINS A ANSDR AUS20030617Line · chafed(AUS) FUEL LINE CHAFED BY AILERON CABLE.SDR QXEA0300408Controller · malfunctionedPDX- ON FLIGHT 2438, AT 39,000 FT, SAT -65 DEGREES CELCIUS, LEFT AUTO CROSSFLOW ON FUEL PUMPS STARTED CYCLING EVERY FEW SECONDS AND FUEL WAS NOT TRANSFERING FROM RIGHT TO LEFT TANK UNTIL DESCENDED TO LOWER AND WARMER ALTITUDE. TESTED FUEL TRANSFER SYSTEM WITHSDR CA030323001Flapper Valve · broken(CAN) BOTH CHECK VALVES WERE REMOVED FROM AIRCRAFT AND DISASSEMBLED.THE CHECK VALVE THAT WAS LOCATED AT THE HAND WOBBLE PUMP IN THE AIRCRAFT WAS FOUND TO HAVE A BROKEN SPRING ON THE INTERNAL FLAPPER VALVE. WHEN EXTERIOR WAS CLEANED, CRACKS WERE FOUND IN THE MASDR CA030319004Flapper Valve · deteriorated(CAN) ON ANNUAL INPSECTION, THIS FUEL CHECK VALVE WAS REMOVED FROM AIRCRAFT FOR INSPECTION. WE HAD TROUBLE DISMANTLING THE VALVE AS CORROSION HAD STARTED TO FUSE THE PARTS TOGETHER. ONCE DISMANTLED THE RUBBER SEAL ON THE INTERNAL FLAPPER VALVE WAS FOUND TO BESDR 2003FA0000284Elbow · crackedDURING POST FLIGHT INSPECTION RESIDUAL FUEL WAS NOTICED IN THE LEFT MAIN WHEEL WELL. WHEN SELECTING MAIN BOOST PUMP ON WITH APU MASTER SWITCH ON, FUEL WAS NOTICED RUNNING OUT OF THE FLEX HOSE ATTACHED TO THE APU FUEL SHUT OFF VALVE. MECHANIC FOUND THE ALUMINUMSDR 2004FA0000583Check Valve · misalignedHINGE PIN DISPLACED, FLAPPER DOOR MISALIGNED, ALLOWING REVERSE FUEL FLOW. PART MARKED 99240/2S6952.SDR 2004FA0000593Check Valve · stuckCHECK VALVE ASSY. GRAVITY/SUPPLY LINE FOUND STUCK OPEN ALLOWING FUEL DISPLACEMENT FROM HEADER TANK.SDR 2004FA0000592Check Valve · stuckCHECK VALVE ASSY. GRAVITY/SUPPLY LINE FOUND STUCK OPEN ALLOWING FUEL DISPLACEMENT FROM HEADER TANK.SDR 2004FA0000582Check Valve · stuckCHECK VALVE, GRAVITY/SUPPLY LINE FOUND STUCK OPEN ALLOWING FUEL DISPLACEMENT FROM HEADER TANK. AIRCRAFT INVOLVED IN FATAL ACCIDENT 03/07/03SDR 2003FA0000429Hose · failedPILOT REPORTED FUEL LEAK AT WING ROOT AREA, RIGHT SIDE OF AIRCRAFT. INSPECTING MECHANIC FOUND THAT WING ROOT FUEL HOSES WERE DETERIORATED CAUSING FUEL LEAKAGE. HOSES LOOKED TO BE ORIGINAL INSTALLATION BUT WERE VACUUM TYPE HOSE.SDR GTIA030114Fitting · leakingRIGHT WHEEL WELL AFT FUEL MANIFOLD INBOARD SIDE DRIPPING FUEL. RESECURED LOOSE FITTING AT APU FUEL LINE SHROUD CONNECTION. LEAK CHECK GOOD.SDR 2003F00139Tube · corrodedFUEL DISTRIBUTION TUBE HAS CORROSION PITTING. SCRAPPED.SDR HEEA085037Tube · corrodedFUEL DISTRIBUTION TUBE HAS CORROSION PITTING. SCRAPPED.SDR HEEA085036Tube · corrodedFUEL DISTRIBUTION TUBE HAS CORROSION PITTING. SCRAPPED.SDR DHL2003801003Seal1) SUBSTANTIAL FUEL LEAK FROM ACCESS PANEL INBOARD OF #1 PYLON.2) FOUND GAMMA SEAL TORN AT #1 MAIN FUEL MANIFOLD INBOARD OF #1 PYLON. REPLACED SEALS AND LEAK CHECKED OK PER M/M 28-20-0.SDR AC2A084862Tube · chafedFUEL TUBE HAS A GROOVE ON THE EXTERNAL SIDE OF THE FLARE. REPLACED WITH NEW TUBE ASSEMBLY.SDR QXEA200300290Switch · malfunctionedPDX-BOOST PUMPS CYCLING INFLIGHT. MAINTENANCE INSPECTED AND REPLACED THE ENGINE INLET PRESSURE SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR VNAA0302012Connector · failedEN ROUTE, THE CREW RECEIVED A FUEL ASYMMETRY CAS MESSAGE AND DIVERTED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE COAX CONNECTOR ON THE REFUEL PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 28-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFTSDR AUS20030134Pump · fod(AUS) FUEL SYSTEM EJECTOR PUMP FOD.SDR QXEA0300239Warning Light · illuminatedSEA-ON FLIGHT NUMBER 2504, LT TRANSFER SHUT OFF VALVE CAUTION MESSAGE IN FLIGHT. USED ABNORMAL CHECKLIST. AFTER 5-10 MINUTES, CAUTION MESSAGE DISAPPEARED. MDC, LT TRANSFER VALVE COMMAND DISAGREE. COMPLIED WITH FIM TASK. NO DEFECTS NOTED. COMPLIED WITH LR
Back to JASC 2820