JASC 2800
Service difficulty reports · 741
Reports filed under 2800 · Aircraft Fuel 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 = '2800' 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 = '2800' 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 2006FA0000727Guard · out of rigPROTECTIVE GUARDS ARE CALLED OUT BY IPL ORIGINALLY, IPL REV 7 DOES, REV 8 DOES NOT. CURRENT REVISION 12, CALLS FOR THE GUARDS TO BE INSTALLED REV 13 IS IN TRANSIT BUT SHOULD INCLUDE THE CALL OUT. THIS AIRCRAFT HAS INDICATIONS THAT ELEVATOR CONTROL LINES HAVESDR 2006UALA01306Pressure Switch · leakingLEFT JETT NOZZLE LEAK. MANUALLY CYCLED LEFT JETT VALVE, OPEN SEVERAL TIMES AND LET IT DRIVE TO THE CLOSED POSITION. STARTED FUELING AGAIN AND NOZZLE STARTED LEAKING AGAIN. SUSPECT LEAKING NOZZLE TUBE. REF IPC 28-31-01-001 ITM 65 CONT OF AMIS ITEM 4202009 :RSDR CA060404002Disk · rupturedFUEL AUTO TRANSFER FAULT ECAM IN CLIMB. SELECTED MAN AS PER ECAM. REALIZED NR 1 TANK WAS FEEDING BOTH ENG AND UNBALANCE INCREASED. UNABLE TO GET FUEL FROM CENTER OR RIGHT TANK. RETURNED TO YYZ. RECTIFICATION: TSM TASK 28-12-00-810-801 CARRIED OUT. OVERPSDR 2006FA0000237Debris Monitor · debondedAFTER REMOVAL OF DEBRIS MONITOR FOR 50 HR, CLEAN AND INSP, THE SCAVENGE CUP/SCREEN TUBE ASSY (PN A8858 IS UNSCREWED FROM UNIT. THE O-RING FLANGE RING GLUED ONTO SCREEN TUBE SHEARS OFF OF SCREEN GLUE LINE, AND STAYS IN THE MAIN UNIT. FIX MAYBE TO APPLY GLUE TSDR UPS06146137Unknown · unknownFERRY FLT FROM TLS DIVERTED INTO YMX DUE TO FUEL MIGRATION/FUEL IMBALANCE. FOUND CTR TK CAL.SENSOR FAULTY CAUSING AUTOFUEL FEED TO BURN FR INNER TKS WHILE CTR TKS CONTAINED MORE THAN 3K OF FUEL DURING CRUISE. SUS- PECT FUEL MIGRATION CAUSED BY TRIM TK SYS FAUSDR KBM2006F00044Valve · leakingELECTRO VALVE LEAKING, REMOVED AND REPLACED. (K)SDR 2006UALA00095Fuel Sys · unknownFLIGHT DIVERTED DUE TO UNPLANNED/UNEXPLAINED FUEL BURN. NO FUEL LEAK INDICATIONS NOTED. TASKS ACCOMPLIHSED WERE: DRIP STICK READINGS TAKEN ON ALL AIRCRAFT FUEL TANKS AND RESULTED IN ALL WITHIN LIMITS. REVIEWED POST FLIGHT REPORT FOR SIGNS OF FAULTS AND RESSDR 2006FA0000123Mount · crackedDURING SCHEDULED INSPECTION FOUND THE FUEL FLOW TRANSDUCER MOUNT CRACKED COMPLETELY ACROSS ON ONE END. (K)SDR 2006FA0000142Vent Line · chafedDEFECT WAS NOTED DURING SEB04-4, WHICH REQUIRED INSP OF FUEL HOSES IN OLDER PRODUCTION AC. IN ORDER TO INSPECT ALL LINES, HEADLINER IS REQUIRED TO BE PULLED. LINES IN QUESTION ARE LOCATED ABOVE DOORS IB OF LT AND RT FUSELAGE RIB. PROBLEM WAS CHAFING OF FUELSDR MASA200501064Unknown · unknownFUEL IMBALANCE OF 900 LBS ON T/O ROLL. OPS CHECKED GOOD.SDR SDR2005085Unknown · unknownAFTER TAKEOFF, MASTER WARNING CAUTION AND FUEL ON CAP PANEL INTERMITTENTLY ON. AIRCRAFT RETURNED TO AIRPORT. INSPECTED FUEL TANK AND FOUND NO EVIDENCE OF DEBRIES. CLEANED FUEL FEEDER TANK. (K)SDR AU510001605Fuel Sys · faultyFUEL SYSTEM SUSPECT FAULTY. LIMITED INFORMATION PROVIDED.SDR CALA0500303Control Panel · inoperativeA SMOKY ODOR NOTICED IN COCKPIT WHEN CREW TURNED ON ENGINE ANTI-ICE & IGNITION DUE TO WEATHER WHILE EN ROUTE. CENTER AUTOPILOT TRIPPED OFF & F/O'S AIRSPEED INDICATOR FAILED. ODOR BEGAN TO DISSIPATE. WHEN WEATHER CONDITIONS ABATED IGNITION & ENGINE ANTI-ICE SDR 2005UALA00908Engine · flamed outENGINE FLAMEOUT DURING NR 2 ENGINE START.SDR 2005UALA00783Totalizer · malfunctionedCREW REPORTED FUEL IMBALANCE, INCORRECT TOTALIZER & FMC CALCULATED TO CONTINUE TO LHR. KICKED OFF A-P & ACFT LT WING HEAVY. MX REPLACED FUEL QTY PROCESSING UNIT. FAULT REPEATED INBOUND. FUEL TANK PROBES R13 & R14 REPLACED. NO FURTHER FUEL IMBALANCE OR INDISDR 2005FA0001044Gascolator · leakingDURING TROUBLESHOOTING, IT WAS DISCOVERED THAT THE GASCOLATOR WAS ALLOWING AIR TO BE INTRODUED INTO THE SHIPS FUEL SYSTEM PRIOR TO THE FUEL REACHING THE ENGINE DRIVEN FUEL PUMP. INSTALLING A NEW GASCOLATOR RESOLVED THE PROBLEM. (K)SDR S2YA05034Control Panel · malfunctionedDURING FLIGHT, CREW REPORTED AN AMBER CAS MESSAGE FOR BOTH LT AND RT FUEL QUANTITY INDICATORS. THE CREW CONSULTED WITH MECHANIC AND MADE AN AIR-TURN-BACK. MECHANIC REPLACED THE FUEL CONTROL PANEL AND ALL OPERATIONAL CHECKS WHERE GOOD. (K)SDR 2005FA0000184Adapter · leakingDOUBLER INSTALLEN IN FUEL TANK HAS NO ACCESS AND MFG CAN NOT TELL US HOW TO STOP FUEL LEAK.SDR 2005F00074Guard · stickingFLT 725 - MIA-MEX - CREW REPORTED NR 2 CROSSFEED VALVE WOULD NOT OPEN IN FLIGHT. AIRCRAFT RETURNED TO MIA, AIRCRAFT LANDED AT MIA WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR 2 FUELING VALVE SWITCH IN THE ON POSITION AT THE WING FUELING STATION. MAINTENANSDR 05FDEA00112Warning Light · illuminatedAT FL310 WITH FUEL SYSTEM AUTO LVL 2 ALERT "TNK WING OVERFILL". COMPLIED WITH QRH PROCEDURES. WITH FUEL SYSTEM IN MANUAL & CROSS FEED MANIFOLD PRESSURIZED) RECEIVED SAME LVL 2 ALERT "TANK WING OVERFILL". SWITCHED TO AUTO (OPPOSITE CONTROLLER) ALERT WENT OSDR CA050105014Adapter · incorrect(CAN) THE INNER RING ON THE FUEL CAP HOUSING IS HELD IN PLACE BY LOCKING TABS. THE FUEL CAP LOCKS ONTO THIS RING. THE LOCKING TABS THAT HOLD THE RING IN PLACE SLOWLY, OVER TIME OF CONSTANT USE RELEASED THE RING TO LET THE CAP COME OUT OF THE HOUSING. CHECKINGSDR HEEA088623Line · leakingLEAKING AT FLEX LINE. REPLACED WITH SERVICEABLE ASSY.SDR DXTA200300065Vent Line · out of positionWING TANK "FULL R AMBER CAS" MESSAGE ILLUMINATED IN CRUISE FLIGHT 10 MINS AFTER LEVELING AT FL 290. FUEL GAUGES SHOWED 2460LB BOTH SIDES. VISUAL INSPECTION IN AIR SHOWED FUEL VENTING OUT OF RIGHT WING. INSPECTED INBOARD AND OUTBOARD TRANSFER FLOAT VALVES, SDR HEEA087882Valve · inoperativeFUEL VALVE INOPERATIVE. REPLACED WITH SERVICEABLE PART.SDR VNAA0302011Transfer Pump · failedENROUTE, THE CREW NOTICED A FUEL IMBALANCE AND HAD A LEFT HAND FEEDER TANK LOW CAS MESSAGE AND FUEL ASSYMETRY CAS MESSAGE THEN DIVERTED TO BDL. ON FINAL THE MESSAGES CLEARED. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE INSPECTED AND REPLACED THE LEFT HSDR GLBA2003016Fuel CapLH FUEL CAP LEAKING FUEL, R&R FUEL CAPSDR HNAA0200088Packing · leaking9 DEC. 2002FUEL DRIPPING OUT OF GEAR WELL ABOVE CONTACTOR BOX #2 NACELLE. WIGGINS FITTING FWD OF NACELLE FIRE SEAL WAS FOUND LEAKING. REPLACED O-RINGS PN AS3209-218 LEAK CHECK GOOD.10 DEC. 2002FUEL COMING OUT OF DRAIN ON INBD SIDE OF #2 NACELLE. FOUND LEAK SDR CALA0200526ValveFUEL TRANSFER AND LOSS FOM AFT AUX AND CENTER FUEL TANK TO LEFT WING TANK. REPLACED FUEL TANK SCAVENGE SHUTOFF VALVE IAW AMM 28-15-21.SDR VNAA0210006Fuel FilterENROUTE, THE CREW RECEIVED A RIGHT HAND ENGINE HIGH PRESSURE BYPASS CAS MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND CONTACTED MAINTENANCE CONTROL. THE CREW WAS THEN INSTRUCTED TO RETURN TO DAY. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HASDR 2002FA0001067Line · chafedFUEL RUNNING OUT OF LEFT VENT WHEN TOPPED OFF. INSPECTION REVEALED LEFT VENT TUBE HAD A HOLE CHAFED IN IT BY FUEL FILLER PORT SCREEN. THIS AIRCRAFT HAD RAM WINGLETS INSTALLED SEVERAL HOURS BEFORE THIS OCCURED. LINE MAY HAVE BEEN BENT DURING THIS INSTALLATION, SDR HEEA080615Drain Valve · leakingFUEL DRAIN VALVE LEAKS. REPLACED WITH SERVICEABLE PART.SDR 0207008Reservoir · rupturedUPON ROUTINE INSPECTION, IT WAS NOTED THAT A FUEL STAIN WAS EVIDENT ON THE UNDERBELLY OF THE AIRCRAFT IN THE FACINITY OF THE FUEL SELEVTOR VALVE. CABIN FLOORING AND UPHOLSTERY WAS REMOVED AND THE FUEL SELECTOR AND FUEL RESEVOIR PN 0516009-18 WAS REMOVED & INSPSDR CA020731004Control Panel · failed(CAN) DURING TRANSIT REFUELLING, SMOKE NOTICED FROM FLIGHT DECK REFUEL/DEFUEL PANEL. MAINTENANCE PERSONNEL WERE SENT AND THE PANEL WAS REPLACED.SDR CA020715004Control Panel · failed(CAN) WHILE REFUELING USING THE COCKPIT REFUEL / DEFUEL PANEL, THE PANEL FAILED AND WAS FOLLOWED BY A STRONG ELECTRICAL SMELL. AIRPLANE DEPOWERED.COCKPIT REFUEL/DEFUEL PANEL REPLACED. AIRCRAFT RETURNED IN SERVICE.SDR HEEA079349Valve · shortedVALVE POPS CIRCUIT BREAKER.SDR VNAA0204024Flow Divider · failedSHORTLY AFTER TAKE OFF, THE CREW HAD A POWER SPLIT AND THE LEFT HAND ENGINE FUEL SHOWED 500 POUNDS PER HOUR MORE THAN THE RIGHT HAND. THE CREW NOTICED A FLUID OFF THE LEFT HAND ENGINE, DECLARED AN EMERGENCY, AND RETURNED TO PWM WITH NO FURTHER INCIDENTS. PISDR GLBA2002055Flow Divider · leakingFUEL ODOR IN COCKPIT ON TAXI, INSPECTED FOUND RIGHT FUEL FLOW DIVIDER LEAKING, REPLACED OPS CHECKED SYSTEM SATISFACTORYSDR 2002FA0000278Servo · malfunctionedREPORTED ENGINE LOST POWER TWICE (ENG RUNNING 1 HOUR).SDR HEEA077801Line · brokenFUEL LINE BROKEN.SDR HEEA077028Release System · failedFAILED INSPECTION.SDR GLBA2001191Filter · dirtyRIGHT FUEL FILTER ANNUCIATOR ILLUMINATED, REPLACED FUEL FILTER OPS CHECKED SYSTEM SATISFACTORYSDR 2001FA0000151Fitting · cloggedWHILE DEFUELING THE AIRCRAFT PREPATORY TO PAINTING, IT WAS DISCOVERED THAT NO FLOW COULD BE ACHIEVED THROUGH THE RIGHT DEFUEL FITTING. THE DEFUEL WAS ACCOMPLISHED BY TRANSFERRING ALL OF THE FUEL TO THE LEFT TANK AND REMOVING IT THROUGH THAT VALVE. WHEN WE OPSDR GLBA2001170Switch · inoperativeFUEL TRANSFERING WITH SWITCH IN THE OFF POSITION, REPLACED TRANSFER SWITCH OPS CHECKED SYSTEM SATISFACTORYSDR CA010813013Harness · chafed(CAN) DURING INVESTIGATION OF INTERMITTENT BOOST PUMP FOUND CHAFED SPOT ON WIRE HARNESS INSIDE FUEL TANK. MAGNIFIED VIEW SHOWED EVIDENCE OF ELECTRICAL CONTACT BETWEEN WIRE AND STRUCTURE OF FUEL TANK.SDR VNAA0107009Valve · failedFLIGHT 4082 WAS ENROUTE TO YOW AND THE CREW RECEIVED A CROSS BLEED FAIL CAS MESSAGE. FLIGHT 4082 THEN RETURNED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED THE FUEL CROSS BLEED SHUT OFF VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 28-00-00. OPERATISDR DL757010947Switch · defectiveSMOKE BEHIND OVERHEAD FUEL BOOST PUMP PANEL IN COCKPIT. FOUND RT FWD BOOST PUMP SWITCH AT FAULT. REPLACE SAME.SDR AALA20011195Pump · inoperativeMCI - FLT 2237 - EN ROUTE ORD-DFW - SHORTLY AFTER DEPARTURE ONE CENTER FUEL BOOST PUMP INOPERATIVE. THE SECOND CENTER FUEL BOOST PUMP ON PLACARD. DIVERTED MCI AND LANDED WITHOUT FURTHER INCIDENT. REPLACED CENTER FUEL BOOST PUMP. LEAK CHECKS GOOD. SYSTEM GSDR RU3A0103Tube · chafedDURING C-CHECK INSPECTION, THE RIGHT MOTIVE FLOW LINE WAS FOUND CHAFFING THE FORWARD ENGINE BLEED AIR LINE IN THE PYLON AREA. THE TWO LINES WERE RUBBING METAL TO METAL. THIS FUEL LINE RUNS ABOUT 300 PSI AND THE BLEED LINE IS ABOUT 500 DEGREES. IPC REFERENCESDR HEEA071985Transmitter · malfunctionedFUEL LOW LIGHT COMES ON AFTER REFUELING. REPLACED WITH SERVICEABLE UNIT.SDR 20010425AP009Switch · failedAFTER ENGINE START, RIGHT ENGINE AUTO SHUTDOWN WITH EICAS MESSAGE RT ENG SPAR VALVE AND SPAR VALVE LIGHT. REMOVED AND REPLACED RIGHT ENGINE SHUTOFF SWITCH IN FIRE CONTROL PANEL. (M)
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