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 DXTR2021031101Canister · crackedDURING DESCENT, A FAINT SMELL OF FUEL WAS NOTICED IN CABIN FOR APPROXIMATELY 30 SECONDS. FOUND FUEL POOLING IN FLAP JACK SCREW TUBE(OUTBOARD TUBE) ON LH INBOARD FLAP WITH EVIDENCE OF JACK SCREW DAMAGE. ALSO NOTED JACK SCREW DAMAGE IN MID FLAP INBOARD JACK SCRSDR QMLA202102012003Fuel · odorSLIGHT SMELL OF FUEL ON TOUCH DOWN. PERFORMED FUEL SYSTEM DRAIN TEST ON #1 AND #2 ENGINES FUNCTIONAL CHECK, OK. WORK PERFORMED IAW ARRIUS 2B2 CH.73-00-00-760-801-A01SDR ASAA2021013033981Fuel Sys · out of balanceMAIN TANKS FUEL QUANTIY IMBALANCE LIMIT EXCEEDED @ FL 380 DURING FUEL BALANCE. GROUNDED - YES. PER ACARS REPORT, FUEL IMBALANCE EXCEEDED 1000LBS. NO TURBULENCE, SIGNIFICANT LOAD OR RAPID/LARGE CONTROL INPUT WAS REPORTED. CONDITIONAL INSP NOT REQUIRED PER B737-SDR A6WA202101257564Flange · gougedFUEL PRESSURE BOX AFT UPPER FLANGE, INBOARD AND OUTBOARD CORNERS GOUGED BLEND OUT DAMAGE ON FUEL PRESSURE BOX AFT UPPER RT FLANGE, 0.390 L X 0.120 W X 0.045 D, REF REO 601R-28-20-044, REV A DATE: 2021-01-21. BLENDED OUT DAMAGE ON FUEL PRESSURE BOX AFT UPPER LSDR ASAA2020113033615Pressure Switch · inoperativeLEFT CENTER TANK FUEL PUMP LOW PRESSURE LIGHT DOES NOT ILLUMINATE WITH CENTER TANK FUEL DEPLETED. GROUNDED-YES. PERFORMED B737-800 FIM 28-22 TASK 820, FOUND FUEL BOOST (CENTER LEFT TANK) INOPERABLE. R & R FUEL BOOST PUMP PRESSURE SWITCH, REF B737-800 MM 28-SDR ABXA20200803213Warning Message · false activationLT FUEL VALVE EICAS DURING START NO FUEL FLOW. AIRCRAFT BACK TO BLOCK AND GROUNDED. TROUBLESHOT BOTH LT ENGINE SPAR VALVE & ENGINE VALVE NO DEFECTS NOTED. PERFORMED GROUND IDLE ENGINE IDLE RUN, IAW B767 AMM 71-00-00, NO DEFECTS NOTED ENGINE. OPERATES NORMSDR UIEA2020091741998Light · no indicationNO ENGINE VALVE LIGHT MOVING THE FUEL CONTROL TO START. PERFORMED ENG FUEL SHUTOFF VALVE ACTUATOR TEST, OPS CHK OK IAW AMM 28-22-11.SDR 2020FA0000397Gascolator · leakingSUBMITTING REPORT ON BEHALF OF CERTIFICATE HOLDER: THE GASCOLATOR IS LOCATED ON LOWER SIDE OF COWLING AND STICKS OUT TO MAKE ACCESS EASY FOR PREFLIGHT FUEL SUMP TO BE PERFORMED. AT SOME POINT THE GASCOLATOR WAS HIT/JARRED WHICH ALLOWED IT TO MOVE SLIGHTLY ANDSDR 2021FA0000083Fuel Feed · pilot errorCREW WAS FLYING IN CRUISE AND CROSSFEEDING FUEL FROM THE RIGHT TO THE LEFT TO CORRECT A FUEL IMBALANCE (R WING HEAVY). CREW WAS THEN INSTRUCTED BY ATC TO CLIMB; AT THIS POINT TOTAL FUEL WAS APPROX 950 LB (555 LB IN THE RIGHT WING, 395 LB IN THE LEFT WING). CRSDR ASAA2020073102958Solenoid Valve · damaged#2 ENG EDP DEPRESSURIZATION SOLENOID VALVE DAMAGED. GROUNDED - YES. REMOVED AND REPLACED #2 ENG EDP DEPRESSURIZATION SOLENOID VALVE REF B737-900 AMM 29-11-11-400-805-001 AND 29-11-11-00-805-001 OPS AND LEAK CHECK GOOD.SDR UIEA2020070741487Unknown · unknownWITH ZERO LBS ON CENTER TANK, LT CENTER PUMP REMAINED ON. NO EICAS MESSAGE OR PRESSURE LIGHT. TRANSFERRED 3.5K LBS OF FUEL FROM CTR TO RT TANK. PRESS LIGHT AND EICAS MESSAGE APPEAR IAW AMM 28-26-00 & 28-42-00.SDR YV3R2020060100276Sensor · intermittentCUSTOMER REPORTED FUEL FLOW SENSOR P/N: G768-3 WAS INTERMITTENTLY FAILING.SDR SWAA2020042944945None · noneSUPPLEMENTAL INFORMATION: LEFT MAIN TANK FUEL INDICATION SHOW INBALANCE INDICATION AT 200 LBS. FUEL INDICATION DROPPED TO 1200 LBS IMBALANCE BEFORE INC. AGAIN TO SHOW BALANCED FUEL. / REF DMA # 0287864 TRANSFERRED TO NRC #D417636. SEE NRC AND ATTACHED SAM 326 SDR ASAA2020012743965Fuel Sys · malfunctionedDURING CLIMB OUT, NOTICED MASTER CAUTION FUEL. THERE WAS AN IMBALANCE OF 1200 LBS DIFFERENCE FROM LEFT MAIN TANK, RAN QRH MAIN TANK LEFT WAS SLOW TO BURN NORMALLY THEN BURNED NORMAL FOR REMAINDER OF THE FLIGHT. GROUNDED - YES. PILOT STATED THAT THE NR 1 TANSDR ASAA2020012743964Fuel Sys · malfunctionedBEFORE DEPARTURE, HAD BOTH MAIN TANKS SHOWING FULL WITH CTR FUEL BEING USED FOR T/O AND CLIMB. AT TOP OF CLIMB, ENTRY CRUISE, NOTED THE RT MAIN TANK SHOWING 7.96 WITH LT MAIN STILL SHOWING 8.58. AFTER 30 MINUTES THE DIFFERENCE REMAINED THE SAME, BALANCEDSDR CALA2019111101966Unknown · odorRIGHT MAIN WHEEL WELL HAD HEAVY FUEL SMELL DURING WALKAROUND THEN NOTICED RIGHT SIDE OF VAPOR BARRIER HAS 3 CRACKS ANDONE LOOKS LIKE IT IS MORE THAN 17 INCHES. CHECKED BOTH LEFT AND RIGHT MAIN W/W AREAS FOR FUEL LEAK OR FUEL SMELL, NONE FOUND. 30-10 REQUIRES OSDR IXXA20191109021Unknown · faultedIN CRUISE VIA AIRLINK, CREW REPORTS POSSIBLE FUEL LEAK FROM LEFT MAIN TANK, UNABLE TO COMPENSATE, FUEL LEAK IS NOT INTERNAL, 2900LBS FUEL IN-BALANCE, UNABLE TO CONTROL WITH CROSSFEED. AS A PRECAUTIONARY MEASURE, AIR TURN BACK TO KPHX WITH AN EMERGENCY DECLARATSDR QMLA2019101719080Unknown · odorMED CREW REPORTED SMELLING FUEL IN CABIN DURING THE SECOND LEG OF A PATIENT TRANSPORT FLIGHT. THE AIRCRAFT WAS LANDED, AND MECHANIC WAS CALLED TO INSPECT THE AIRCRAFT. THE BAGGAGE COMPARTMENT MEDICAL SERVICES PANEL WAS REMOVED TO EXPOSE A FUEL VALVE THAT WAS TSDR CALA2019082601431Cap · missingPDA 2- FUEL CAP MISSING ON ARRIVAL. INSPECTION AT DEPARTURE STATION- NO REPORT OF MISSING CAPS. INSPECTED FUEL COUPLING FOR LEAKS AND DAMAGE- NONE NOTED. APPLIED CDL 28A.SDR 2A6R2019050351901Unknown · defectiveFOLLOWING THE SEVERAL LEAK ISSUES WE HAD WHILE PERFORMING THE POST INSTALLATION CHECKS ON CRFS INSTALLATION KIT, AS350 PN- HM019-600-11 SN- 0025 WE WERE INSTRUCTED TO REPLACE THE TANK ASSY WITH ONE FROM KIT SN- 0023. AFTER INSTALLATION OF THE NEW TANK ASSY WE SDR AALA2019041649004Unknown · unknownAIRCRAFT NOT GROUNDED: PILOT REPORTS WITH CENTER FUEL TANK EMPTY RIGHT TANK SHOWED INCREASE BURN THAN THE LEFT. THE DIFFERENCE WAS 100 LBS EVERY 10 MIN. FUEL FLOWS WERE THE SAME. AFTER LANDING A 220 LB DIFFERENCE CORRECTED IT SELF TO A 10 LB DIFFERENCE BY TSDR AALA201904129002Fuel Sys · malfunctionedAIRCRAFT WAS NOT GROUNDED: PILOT REPORTS FUEL STARTED OUT BALANCED. BY 1.5 HRS. INTO THE FLIGHT, CENTER TANK EMPTY, LEFT ENGINE HAD 500 MORE LBS. THANKS THE RT. FUEL FLOW WAS HIGHER ON THE LEFT 2.62 VS 2.58. BALANCED THE FUEL, AT THE TOP OF DESCENT 2 HRS IN FSDR AALA201904129003Fuel Sys · malfunctionedAIRCRAFT WAS NOT GROUNDED: PILOT REPORTS APPROX. ONE MINUTE AFTER T.O. RIGHT MAIN TANK IMBALANCE ALERT DISPLAYED. FUEL FLOWS WERE EVEN. FUEL FOR BOTH ENGINES WERE BEING FED FROM RIGHT MAIN. RAN IMBAL QRH. NO FUEL LEAK SUSPECTED SO BALANCED MAIN TANKS, CROSSFEESDR ASAA2019040878928Warning Message · illuminatedCLASS 2 MAINTENANCE FUEL MESSAGE GROUNDED - YES. DEFERREDSDR CA190329027Panel · damaged(CAN) DURING REFUEL THE FUELER REPORTED THAT THE #1 FUEL VALVE WAS INTERMITTENT. MAINTENANCE INVESTIGATED AND OBSERVED SMOKE FROM THE REFUEL/DEFUEL PANEL. THE PANEL WAS REMOVED FROM THE AIRCRAFT AND FURTHER TROUBLESHOOTING REVEALED THAT THE L/H FUEL OPEN LIGHTSDR CA190620013Line · corroded(CAN) BOMBARDIER HAS OPENED A NEW CAW PROJECT RJ-CA-28-0022 TO FURTHER INVESTIGATE IF THESE FINDINGS HAVE CAUSED AN UNACCEPTABLE DEGRADATION OF LIGHTNING STRIKE PROTECTION IN THE WING TANKS. FOLLOWING THE DASH 8 FINDING OF CORRODED OR BLACKENED FUEL COUPLINGSSDR AALA201903139001Warning Message · false activationTHE PILOT REPORTED THAT DURING DECENT, THE FUEL SCAVENGE SYSTEM WAS INOPERATIVE WITH 800 LBS REMAINING IN THE CENTER TANK. MAINTENANCE ACCOMPLISHED FIM 28-22-00-810-901 WITH NO FAULTS FOUND.SDR UIEA2019021903255Pressure Switch · inoperativeLEFT AFT FUEL PUMP PRESSURE LIGHT DOES NOT ILLUMINATE. PERFORMED FIM 28-22 FT 828, BLOCK 23. FOUND THE LEFT AFT PRESSURE SWITCH INOPERATIVE. REMOVED AND REPLACED L AFT AFT FUEL PUMP PRESSURE SWITCH IAW AMM 28-42-01, OPS CHECKED GOOD, NO FUTHER DEFECTS NOTESDR FDEA201812053441Fuel Sys · unknownSUSPECTED FUEL LEAK ENROUTE 2 HOURS INTO FLIGHT FUEL WAS 4000 LBS LOWER THAN EXPECTED. 15 MINUTES LATER RECEIVED FUEL QTY CHK ALERT. RAN QRH CHECKLIST & DETERMINED LEAK WAS IN UPPER AUX ESTIMATE 10000 LBS OF FUEL LEAKED.PULLED AND RESET FUEL QTY NORMAL POWER ASDR ASAA2018112186900Status Message · false activationWHITE MAINT FUEL ON STATUS PAGE GROUNDED - YES. PERFORMED FLSS BITE TEST PER A321 AMM 28-46-00, NO FAULTS NOTED, FUEL MSG CLEARED.SDR UIEA2018103102458Switch · bindingRIGHT FUEL PUMP SWITCH STUCK IN THE OVERHEAD PANEL. R & R THE FUEL PUMP SWITCH. OPS CHECKED NORMAL IAW AMM 28-22-00.SDR UIEA2018103102456Switch · malfunctionedRESET SWITCH BROKEN ON THE REFUELING PANEL. R & R OVER FILL RESET SWITCH. OPS CHECKED NORMAL IAW AMM 28-21-13.SDR AALA2018090659001Warning Message · illuminatedDURING CRUISE, AN ECAM MESSAGE FOR LEFT TANK 2 LOW PRESSURE CAME ON TWICE, BUT RETURNED TO NORMAL BOTH TIMES.SDR BQVD2018081300001Flex Hose · disintegratedON RAMP, AFTER FLIGHT, PILOT NOTICED A PUDDLE OF FUEL UNDER THE ENGINE COWL. FOUND THE ENGINE DRIVEN FUEL PUMP SEAL WAS LEAKING. THE LEAKING FUEL PUMP PROBLEM WAS COMPOUNDING WITH ANOTHER SERIOUS PROBLEM. MAINTENANCE DISCOVERED THE DRAIN HOSE MATERIAL IS NOT SDR DALA2018051003281Access Panel · corrodedCORROSION ON THE COUNTERSINK HOLES OF THE FUEL ACCESS PANEL 141AL, AT THE CENTER TANK. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION II.SDR AALA201803099025None · noneAIRCRAFT WAS GROUNDED. RIGHT WING OVERFLOW. FUELER OVER-FUELED AIRCRAFT. AIRCRAFT DIVERTED TO ORD. EMERGENCDELCARED, AIRCRAFT LANDED OVERWEIGHT AND WITHOUT INCIDENT. MAINTENANCE PERFORMED REQUIRED OVERWEIGHT INSPECTION. MEL AUTHORIZED AIRCRAFT AUTO TRANSFER SYSDR UIEA2018021300211Switch · failedRT SPAR VALVE SWITCH ILLUMINATED. REMOVED AND REPLACED THE SWITCH, OPS CHECK GOOD IAW AMM 33-16-02. REPAIRED A BROKEN WIRE W456-0222-18 AT PIN 6 ON RIGHT SPAR VALVE IAW SWPM 20-10-15. OPS CHECKED GOOD IAW AMM 28-22-00.SDR 2018FA0000100Rotor · wornWORN ROTOR ULTIMATELY FAILED DURING FLIGHT, RESULTING IN A FATAL ACCIDENT. THE PILOT LIKELY HAD TO APPLY EXCESSIVE FORCE TO SWITCH FUEL TANKS WITH THE WORN ROTOR.SDR HALA20171800293Transfer Sys · malfunctionedDURING FINAL APPROACH, FUEL TANK TRANSFER FAULT. CHECKED CMC & CORRELATE FAULT MESSAGE FOUND. TROUBLESHOT IAW TSM 28-27-00. PERFORMED FCMC BITE TEST & TEST OK. OK FOR SERVICE.SDR HALA2017121800300Transfer Sys · malfunctionedFUEL T TANK XFER FAULT ECAM FOR 2 MIN FUEL 15880 0 FUEL IN T TANK. ACCOMPLISHED TSM 28-27-00-810-829-A.FCMS FUEL VALVES TEST OK IAW AMM 28-51-00-710-801.FCMS BITE TEST OK, IAW AMM 28-51-00-740-801. ACFT OK FOR SERVICE.SDR HALA20171800294Transfer Sys · malfunctionedFUEL T TANK TRANSFER FAULT ECAM FOR 2 MIN FUEL 15880 0 FUEL IN T TANK. ACCOMPLISHED TSM 28-27-00-810-829-A.FCMS FUEL VALVES TEST OK IAW AMM 28-51-00-710-801.FCMS BITE TEST OK, IAW AMM 28-51-00-740-801. ACFT OK FOR SERVICE.SDR UIEA2017120502361Switch · malfunctionedWHEN APU DC PUMP RUNNING, EICAS MSG 'DC FUEL PUMP ON' DOES NOT SHOW. APU DC FUEL PUMP PRESSURE SWITCH REMOVED, REPLACED AND TESTED IAW AMM 28-25-03 REV 122, FOUND SATISFACTORY.SDR UIEA2017112802328Panel · inoperativeREFUELING PANEL WILL NOT POWER ON AUTOMATICALLY. ACCOMPLISHED REFUELING IAW DDG PROCEDURES. R & R MAGNETIC ASSY IAW AMM 28-21-09, OPS CHECKED NORMAL.SDR VQI2018F00001Valve · leakingA DIESEL ODOR WAS IN THE CABIN SHORTLY AFTER TAKEOFF AND THE ACFT RETURNED TO FIELD. MX PERFORMED TSM 05-50-00-810-831-A AND FOUND FUEL LEAKING FROM THE RT CENTER FUEL TANK DRAIN VALVE. CLEANED RESIDUAL FUEL FROM FUSELAGE AREA AND APU INTAKE AREA. RAN APU ASDR AALA201711219018Computer · malfunctionedDURING DESCENT, FUEL LEFT OUTER TRANSFER OPEN, RIGHT OUTER TRANSFER OPEN. RESET FUEL QUANTITY INDICATION COMPUTER IAW AMM 28-15-00-740-002. OPS CHECKED GOOD.SDR SWAA2017110617601Control Panel · faultyNR 2 AFT FUEL BOOST PUMP LIGHT CAME ON IN CLIMB. RETURNED TO BASE. R & R THE NR 1 AFT BOOST PUMP CONTROL PANEL IAW AMM.SDR UIEA2017100601935Switch · failedON SHUT DOWN, THE RT SPAR VALVE DID NOT CLOSE, RT ENGINE SPAR VALVE INOPERATIVE. REMOVED AND REPLACED THE SPAR VALVE LIGHT SWITCH IAW WDM 28-22-21 OPS CHECKED OK.SDR AALA201709299002Meter · malfunctionedAFTER TAKEOFF, RECEIVED A NR 1 ENGINE CONTROL 1 SYS FAULT. RETURNED TO FIELD. REPLACED FUEL METER. AIRCRAFT WAS GROUNDED.SDR DALA2017080806153Unknown · leakingFUEL LEAKING FROM THE NR 2 ENGINE PYLON, AFT OF ENGINE EXHAUST. DETERMINED SOURCE OF THE LEAK AND REPAIRED IAW AMM 28 -11.SDR ASMF201707003Unknown · leakingAIRCRAFT RETURNED TO PLATFORM DUE TO DURING LEFT ENGINE START, A FUEL LEAK WAS DETECTED. DETECTED FUEL LEAK IN THE TBV DRAIN. THE LEFT ENGINE WAS MOTORING, AFTER IT WAS STARTED AND ENGINE OPERATIONAL TEST WAS PERFORMED IAW AMM 71-71-00, NO CONFIRMING FUEL L
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