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 CA020405003Line · chafed(CAN) THE L/H FUEL CROSS TRANSFER TUBE WAS FOUND CHAFED THROUGH AND SEEPING FUEL. THE WEAR MARK ON THE TUBE MEASURED APPROXIMATELY 5/16 INCH IN LENGTH X 1/8 INCH IN WIDTH. REF: IPC 28-20-00. WEAR OCCURRED FROM THE WIRE BUNDLE COVERING OF THE GEAR UPLOCK MICROSSDR HEEA078364Hose · kinkedFUEL HOSE KINKED.SDR HEEA078363Hose · kinkedFUEL HOSE KINKED.SDR HEEA078362Hose · kinkedFUEL HOSE KINKED.SDR HEEA078361Fitting · corrodedHOSE IS CORRODED AT FITTING.SDR HEEA078359Hose · corrodedFUEL HOSE END FITTING ON HOSE CORRODED.SDR HEEA078347Tube · crackedFUEL TUBE SLEEVE CRACKED.SDR HEEA078346Tube · kinkedFUEL TUBE KINKED.SDR HEEA078288Line · corrodedFUEL LINE CORRODED.SDR HEEA078287Line · corrodedFUEL LINE CORRODED.SDR HEEA078286Line · corrodedFUEL LINE CORRODED.SDR QXEA0202006Pressure Switch · failedMFR- LEFT HAND AND RIGHT HAND BOOST PUMP ON INTERMITTENTLY DURING FLIGHT. REMOVED AND REPLACED LEFT HAND AND RIGHT HAND PRIMARY EJECTOR PRESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR HEEA078183Line · corrodedFUEL SYSTEM LINE HAS CORROSION.SDR QXEA0200453Switch · faultyPDX- ON CLIMBOUT HAD 230 POUNDS OF FUEL IN CENTER TANK WITH TRANSFER SYSTEM ACTIVE. FUEL LEVEL IN CENTER TANK DECREASED TO 90 POUNDS. LEFT HAND WING FUEL QUANTITY APPEARED TO INCREASE. BOOST PUMPS CYCLED ON AT FLIGHT LEVEL 410 AND REMAINED ON FOR SEVERAL MISDR QXEA0202005Pressure Switch · failedPDX- BOOST PUMPS CYCLED CONTINUOUSLY. CENTER TANK EJECTOR PUMPS REMAINED ON CONTINUOUSLY WITH A STEADY 100-110 POUND QUANTITY IN CENTER TANK. REMOVED AND REPLACED LEFT HAND AND RIGHT HAND PRIMARY EJECTOR PRESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RSDR WVBA2002005Valve · leakingDURING SOME LINE MAINTENANCE, THE TECHNICIAN NOTICED FUEL STAIN FROM THE HEATER DRAIN. THE SOURCE WAS FOUND TO BE THE FUEL PRESSURE REGULATOR WHICH WAS LEAKING FROM THE LOWER PARTING SURFACE. THE UNIT WAS REMOVED AND REPLACED.SDR HEEA078092Valve · leakingFUEL SYSTEM IS SEEPING FROM VALVE ASSY.SDR 2002FA0000214Line · corrodedLINE DEVELOPED PINHOLE LEAK DUE TO CORROSION WHERE CABIN VENT SCEET HOSE RESTED ON TOP OF IT.SDR CA020215011Fuel Line · broken(CAN) WHILE IN CRUISE THE #1 ENGINE SHUTDOWN BY ITSELF. COULD NOT RE-START THE ENGINE. CAPTAIN DECIDED TO LAND IN HOUSTON, TEXAS. MAINTENANCE FOUND A BROKEN FUEL LINE ON THE MEC GOING TO VARIABLE STATOR ACTUATOR.SDR AUS20020090Pipe · corroded(AUS) RH INBOARD FUEL TRANSFER PIPE CORRODED AND LEAKING.SDR QXEA0200093Coupling · failedEUG - CREW RECEIVED FUEL EJECTOR CAUTION LIGHT AND FUEL IMBALANCE, RIGHT TANK LOW CAUTION MESSAGE AND CENTER TANK BEGAN TO TAKE ON FUEL. THE CENTER TANK HAD OVER 4500 LBS OF FUEL UPON LANDING. MAINTENANCE REPLACED THE FAILED RIGHT WIGGINS CLAMP AND RIGHT PRISDR HEEA077815Tube · brokenFUEL TUBE IS BROKEN.SDR 2002FA0000201Hose · splitUPON INSTALLATION OF A FUEL SELECTOR NOTICED THE OUTER COVER OF THE HOSE SPLIT AS IT WAS INSTALLED ON AN NIPPLE FITTING. AFTER CLOSE EXAMINATION, THE NEW HOSE SHOWS A MARK / CUT GOING THE LENGTH OF THE HOSE. IN SOME AREAS IT IS A MARK AND OTHER AREAS IT IS SDR AUS20020067Coupling · misrigged(AUS) FUEL TRANSFER SYSTEM COUPLING INCORRECTLY ASSEMBLED.SDR LS1R088277Pump · roughFUEL PUMP ROUGH.SDR DL76S020060Switch · malfunctionedDURING THE BOARDING OF FLIGHT 706 FROM SEA/ATL CREW REPORTED SMOKE IN THE COCKPIT. CAUSE OF SMOKE WAS FOUND TO BE THE RT AFT FUEL PUMP SWITCH IN P5 PANEL. REPLACED SWITCH ASSY, PART WAS REPLACED.SDR QXEA0201976Pressure Switch · leakingBOI - DURING PREFLIGHT, CREW FOUND FUEL LEAK FROM CENTER FUSELAGE AREA NEAR WING LEADING EDGE. MAINTENANCE REPLACED THE EJECTOR PUMP PRESSURE SWITCH. OPERATIONAL AND LEAK CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR 2002UALA00053Fuel Line · chafedUNWANTED FUEL TRANSFER FROM RIGHT FUEL TANK TO CENTER TANK. FOUND CHAFED WATER SCAVENGE FUEL LINE. DAMAGE CAUSED FROM COUPLING CONTACT ON ADJACENT FUEL LINE DUE TO INCORRECT CLAMPING. REPLACED WATER SCAVENGE FUEL LINE.SDR 2003FA0000351Line · brokenTHE TUBE FAILED ADJACENT TO FERRULE ON THE ENGINE DRIVEN FUEL PUMP FITTING. FAILURE WAS FOUND UPON REMOVAL OF THE PART FROM THE AIRCRAFT TO PERFORM OTHER MAINTENANCE. RECOMMEND CHANGING THIS RIDGED LINE TO A FLEXIBLE LINE;SDR 2003FA0000350Line · brokenTHE TUBE FAILED INSIDE THE FERRULE ON THE ENGINE DRIVEN FUEL PUMP FITTING DUE TO RUBBING AND VIBRATION. FAILURE WAS FOUND AFTER PILOT COMPLAINED OF LOW M.A.P., ABOUT 2 IN HG, AT MAXIMUM OPERATING PERIMETERS, AND FUEL CONSUMPTION LOW.SDR HEEA077660Fuel Filter · malfunctionedFUEL FILTER LIGHT WILL NOT COME ON WHEN BUTTON IS PUSHED.SDR DLM11020007Controller · failedTANK 1 FUEL QTY WENT AMBER WITH FSC IN AUTO. REPLACED FSC.SDR CA021208001Control Panel · shorted(CAN) BURNING ODOR FROM COCKPIT REFUEL/DEFUEL PANEL. REFUEL/DEFUEL CONTROL PANEL REPLACED.SDR 2002F00301Bypass Valve · inoperativeBYPASS VALVE INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M)SDR AUS20011338Line · corroded(AUS) FUEL LINE EXCESSIVELY COORODED DUE TO WATER CONTAMINATION.SDR AUS20011337Valve · corroded(AUS) FUEL SYSTEM CHECK VALVE EXCESSIVELY CORRODED AND CONTAMINATED DUE TO WATER IN FUEL CROSSFEED LINE.SDR 2001FA0000608Support · brokenEYE SCREW, IS A SUPPORT STRUT WHICH ATTACHES TO THE EXHUST STACK AT ONE END AND THE FUEL SERVO TO ENGINE SUMP ATTACHMENT STUDS AT THE OTHER END. THE STRUT FELL BETWEEN THE THROTTLE ARM AND SUMP. THIS PREVENTED THE ENGINE FROM BEING ABLE TO REDUCE POWER BELOW 1SDR 2001FA0000622Line · leakingMOONEY 201 M20J: OWNER REPORTED LOW FUEL PRESSURE. FOUND AEROQUIP LINE LEAKING THROUGH BODY OF INNER TUBE STOCK. THIS LINE HAS A STAINLESS STEEL BRAID COVERING FULL LENGTH. HOSE HAD A CURE DATE 3RD QUARTER 1995 WITH MANUFACTURED DATE JAN 1998. HOSE IS CONNECSDR 2002F00284Line · leakingDURING TAKEOFF, ON CLIMB-OUT HAD EXCESSIVE FUEL FLOW ON NR 1 ENGINE. TOWER CALLED AND SAID VAPORS TRAILS WERE NOTED FROM NR 1. SCANNED NR 1 AND SAW FLUID. LEVELED OFF AND PULLED POWER BACK. FUEL LEAK STOPPED. DUMPED FUEL PRIOR TO LANDING. REMOVED AND REPSDR AUS20011449Control Unit · faulty(AUS) AUTO FUEL FEED MALFUNCTION. LIMITED INFORMATION PROVIDED.SDR AUS20011435Control Unit · faulty(AUS) AUTO FUEL FEED FAILS DURING DESCENT.SDR AUS20011282Valve · fod(AUS) FUEL SYSTEM NON-RETURN VALVE JAMMED OPEN BY FOD CAUSING A FUELIMBALANCE BETWEEN NO1 AND NO2 TANKS. INVESTIGATION FOUND APLASTIC BLANK WAS JAMMING THE VALVE OPEN. SUSPECT FOD WAS A BLANKING CAP FROM BOOST PUMP PRESSURE LINE. BOOST PUMP HAD BEEN REPLACED PSDR HEEA077262Hose · chafedINSULATION CHAFED THROUGH.SDR HEEA077255Hose · kinkedHOSE ASSY KINKED.SDR AUS20011264Line · chafed(AUS) CROSSFEED FUEL LINE LOCATED IN LT WHEEL WELL CHAFING ON UNDERCARRIAGE ACTUATOR CONTROL ROD. THE FUEL LINE HAD BEEN COVERED WITH A PLASTIC SLEEVE AFTER THE DAMAGE HAD OCCURRED. SUSPECT CAUSED BY INADEQUATE SECURING OF FUEL LINE. PERSONNEL/MAINTENANCE ERRSDR AUS20011263Line · chafed(AUS) FUEL CROSSFEED LINE LOCATED IN RT WHEEL BAY CHAFING ON UNDERCARRIAGE DOWNLOCK BACKUP CABLE. SUSPECT LINE INADEQUATELY SECURED. PERSONNEL/MAINTENANCE ERROR.SDR HEEA077008Valve · stuckINOPERATIVE - STUCK IN THE MID TRAVEL POSITION. TO BE SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED.SDR 2001FA0000514Fuel Line · corrodedAIRCRAFT EXPERIENCED A MASSIVE FUEL LEAK INSIDE OF CABIN AREA CAUSING AN INFLIGHT EMERGENCY. DETERMINED FUEL LEAK CAUSED BY CORROSION OF FUEL LINE FROM FIRE WALL TO FUEL PRESSURE INDICATOR. CORROSION CAUSED BY DISSIMILAR METAL OXIDATION WHERE FUEL LINE WAS RSDR HEEA076971Vent · leakingHAD STRONG FUEL ODOR IN COCKPIT. FOUND A SMALL AMOUNT OF FUEL HAD SEEPED THROUGH THE RT EXTERNAL TANK VENT DUE TO HIGH FUEL LEVEL AND THE ATTITUDE OF THE AIRCRAFT.SDR AUS20011144Tube · corroded(AUS) FUEL CROSSFEED PIPE LOCATED BELOW CABIN FLOOR CORRODED INTERNALLY PRODUCING A SMALL PIN HOLE LEAK. LEAKING FUEL CONTAMINATED THESURROUNDING INSULATION.
Back to JASC 2820