JASC 2820
Service difficulty reports · 3,630
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 ASAA2020121633719Indication Sys · false indicationFUEL IMBALANCE INDICATION CAME ON 1 HOUR FROM LANDING. THE FUEL IMBALANCE CHECKLIST WAS RUN. THERE WERE NO ABNORMAL ENGINE INDICATIONS, NO SUSPECTED FUEL LEAK AND NO FUEL LOSS. THE WINGS WERE LEVEL AND THE AIRPLANE WAS IN TRIM. GROUNDED-YES. PERFORMED FQISDR HALA2020121600222Actuator · defectiveATB-ECAM FUEL OUTER TANK TRANSFER RT OUTER FAILED TO OPEN. 6100 LBS TRAPPED. DIVERTED TO KLAX. REMOVED & REPLACED OUTER TANK FUEL INLET ACTUATOR, PER A330 AMM 28-25-57 OK FOR SERVICE. TAGGED PART PER TOPP 40-28-85 ODI REQUIREMENT ACTUATOR, SINGLE OFF 43-28SDR 9JLA2020120224738Valve · defectiveDURING PREFLIGHT CHECKS THE FLIGHT CREW DETERMINED THE FUEL CROSS FEED VALVE FAILED TO CLOSE. THE MAINTENANCE TEAM VERIFIED THE DISCREPANCY. THE MAINTENANCE TEAM REMOVED THE DEFECTIVE VALVE WITH AN OVERHAULED CROSS FEED VALVE. OPERATIONAL CHECKS WERE SATISFSDR FDEA202011152878Shutoff Valve · failedLEVEL 1 TANK 1 TIP TRAPPED. SYNOPTICS SHOWED 7000 LBS REMAINING IN TANK 1 AND 5100 LBS OF THAT WAS SHOWING IN THE TIP TANK. EMERGENCY DECLARED. R & R FUEL TRANSFER SHUTOFF VALVE, PER AMM 28-21-16-4 P/N OFF 19650-4 S/N OFF 0600, P/N ON 19650-4 S/N ON 0410.SDR BWVR135625Check Valve · stickingTHE CHECK VALVE IS TO PREVENT FUEL IMBALANCE WING TO WING. WHEN CHECK VALVE IS OPERATING CORRECTLY IT IS DIRECTING FUEL FROM ONE SIDE FUEL STORAGE/DISTRIBUTION DIRECTLY TO THE OPPOSITE ENGINE. A FUEL IMBALANCE CONDITION WAS NOTED WHILE THE AIRCRAFT WAS IN MASDR AALA202011139008Actuator · stuckAIRCRAFT WAS GROUNDED. LEFT OUTER FUEL TRANSFER VALVE STUCK IN THE OPEN POSITION. REMOVED AND REPLACED LEFT FUEL TRANSFER VALVE ACTUATOR, PER AMM 28-15-51.SDR UIEA2020110902366Pressure Switch · malfunctionedRIGHT AFT PRESSURE LIGHT IS OUT. TRANSFER TO MDDR 137297 MEL 28-22-01, DUE 16NOV20, CAT C. CONTINUITY CHECK OF GROUND WIRE, PIN 2 OF CONNECTOR D2822, CHECKS GOOD. JUMPERED PINS 2 & 3 ON CONNECTOR D2822, LIGHT IN F/D COMES ON. REQUIRES RT AFT BOOST PUMP PRESDR G1IA202010041003O-Ring · leakingFAR 135.415 REPORT. PILOT REPORTS "NORMAL DEPARTURE. CLIMBING OUT OF 10000 RIGHT ENGINE TORQUE REDUCED TO 1400 ON IT'S OWN. FUEL FLOW INCREASED TO 450. RETURNED TO PAFA WITH NORMAL LANDING". DURING INSPECTION, MAINTENANCE FOUND EVIDENCE OF RT ENGINE FUEL SDR ASAA2020101933392Actuator · failedNR 1 ENGINE FAILED TO START. EGT HUNG UP AT APPROXIMATELY 450C, THEN ROLLED BACK. GROUNDED-YES. VERIFIED FROM PILOTS PACKS WERE OFF DURING ENGINE START. PERFORMED B737-800 FIM 80-50 TASK 806 STEP FOUND 2 MESSAGE NUMBER 75-20411, 75-10411 THE HPTACC POSITIOSDR IPXA2020102161546Tank · inoperativeINSPECTION TYPE: N/A ATB NO CHIME TRIM TANK AFT TRANSFER INOPERABLE WHEN TRANSFER STARTED GREEN CHEVRONS CAME ON SYNOPTIC PAGE, BUT NO FUEL MOVED TO TRIM THEN FAULT. R & R 72QU TRIM TANK REFUEL/AFT TRANSFER RELAY, IAW ESPM 20-46-50-0101. R & R TRIM TANK REFSDR IPXA2020102161545Tank · inoperativeINSPECTION TYPE: N/A, ATB TRIM TK AFT TRANSFER INOPERABLE ON ECAM. BITE CHECKED FQIS, IAW 28-42-00-0501 AND CGCC, IAW 31-46-00-0501. NO FAULTS NOTED, OPERATIONS CHECKED GOOD, IAW 28-26-00-0501.SDR UIEA2020101602264Pressure Switch · failedON TAKEOFF ROLL WITH 7000 LBS IN CENTER TANK, CENTER RT FUEL PUMP EICAS MESSAGE. ITEM TRANSFERED TO MDDR 136106, PER MEL 28-22-02A CAT C DUE DATE 25-OCT-20. MX ACTION C/W CB COLLARED. TIME INITIALS GTCAT 0338. CVG MX, 17OCT. REMOVED AND REPLACED RIGHT CENSDR 2020FA0000489Control Valve · failedDEPARTED KFCM, REFUELED AT KLNK. DURING FLIGHT, PILOTS BANKED HARD LEFT, EMERGENCY DESCENT TO LAND IN SALINA, KS. CHIEF PILOT STATED "FUEL CONTROL VALVE FAILED AND WERE 'DANGEROUSLY LOW ON FUEL'". HE FURTHER STATED, "OUR 55'S ARE OLD AND SOMETHING'S ALWAYS SDR AALA202010129029Check Valve · inoperativeAIRCRAFT WAS GROUNDED. FUEL SMELL NOTED IN AFT CARGO BIN AND IN CABIN ON ARRIVAL. REMOVED AND REPLACED 177QM2 (AALA202010119011) CHECK VALVE, PER AMM 28-28-37 AND 178QM2 (AALA202010129029) IAW AMM 28-28-38. PERFORMED FUNCTIONAL TEST OF ACT TANK CHECK VALVESSDR AALA202010119011Check Valve · inoperativeAIRCRAFT WAS GROUNDED. FUEL SMELL NOTED IN AFT CARGO BIN AND IN CABIN ON ARRIVAL. REMOVED AND REPLACED 177QM2 (AALA202010119011) CHECK VALVE, PER AMM 28-28-37 AND 178QM2 (AALA202010129029) IAW AMM 28-28-38. PERFORMED FUNCTIONAL TEST OF ACT TANK CHECK VALVESSDR 2020FA0000445Control Box · defectiveON 10/8/2020, N824MG DEPARTED KLNK WITH PASSENGERS FLYING TO KELP. AFTER TAKEOFF THE CREW ATTEMPTED TO START THE FUEL TRANSFER AND NOTICED THE TRANSFER/CROSS FLOW VALVES TRANSITION LIGHTS WERE NOT ILLUMINATING WITH ANY OF THE TRANSFER OPTIONS. THE CAPTAIN NOSDR UIEA2020100862174Pressure Switch · malfunctionedLEFT AFT FUEL PUMP EICAS ILLUMINATED WITH LEFT AFT FUEL PRESS FLICKERS. PERFORMED FIM 28-22-43819. UNABLE TO DUPLICATE EICAS MESSAGE. LEFT AFT FUEL PRESS LIGHT FLICKERS. INSTALLED DMI 135536, IAW MEL 28-42-01-01. M/P C/W. MCC EC 1012 DISP JD 1012. RIV MSDR QMLA2020093020050Fuel Filter · leakingFUEL FILTER ASSY DEVELOPED A LEAK. WAS CHANGED OUT THEN THE SERVICEABLE ONE INSTALLED. OPS CHECK GOOD FOR MAINTENANCE, BUT THE NEXT DAY ON PREFLIGHT INSPECTION BY THE PILOT THE FILTER "BYPASS" WARNING LIGHT BUTTON ON THE ASSY WOULD NOT OPERATE CORRECTLY. PASDR 2020F00410Booster · intermittentCENTER FUEL LOW ANNUNCIATION CENTER FAILS TO FEED IN FLIGHT. FOLLOWED QRH PROCEDURE, RETURN TO SKBQ, AS WE RETURNED CENTER FUEL PRESS LOW ANNUNCIATION BECAME INTERMITTENT.SDR HYIA20200921001Packing · leakingTHE PILOT REPORTED A FUEL SMELL IN COCKPIT. MAINTENANCE INSPECTED AND FOUND THE CABIN HEATER FUEL FILTER BOWL LEAKING. REMOVED AND REPLACED THE BOWL SEAL WITH NO FURTHER DEFECTS NOTED.SDR ASAA2020091423177Actuator · inoperativeDURING NR 2 ENGINE START, SPAR VALVE DID NOT OPEN, START ABORTED. GROUNDED - YES. CONFIRMED WITH NR 2 FUEL LEVER IN IDLE, SPAR VALVE CLOSED LIGHT STAYS IN-TRANSIT. REMOVED AND REPLACED SPAR VALVE ACTUATOR, REF B737-900 AMM 28-22-11-000-804/AMM 28-22-11-400-SDR HYIA20200916001Manifold · crackedTHE PILOT REPORTED DURING TAXI IN FUEL SMELL IN COCKPIT AND ON NACELLE. MAINTENANCE INSPECTED AND FOUND A CRACK IN THE FUEL DISTRIBUTION MANIFOLD PLUG RECEPTACLE. REMOVED AND REPLACED THE RIGHT FUEL MANIFOLD ASSEMBLY, WITH NO FURTHER DEFECTS NOTED.SDR AALA202009109005Shutoff Valve · defectiveAIRCRAFT WAS GROUNDED: AFTER RETURN TO GATE FOR PAX DISTURBANCE, FUEL WAS STREAMING OUT OF RIGHT WING TANK SURGE VALVE, RIGHT CENTER BOOST PUMP WAS ON AND AFTER TURNING OFF RIGHT CENTER PUMP LEAK STOPPED. REPLACED NR 2 FUELING SHUTOFF VALVE, PER AMM 28-21-51SDR 2020FA0000399Rod End · wornTHERE HAVE BEEN TWO INSTANCES WITH CBP AIRCRAFT IN WHICH THE ENGINE CONTROL ROD-END (FUEL FLOW L’HOTELLIER END FITTING AND BALL JOINT) DISENGAGED AT THE HMU LEVER DURING ENGINE OPERATIONS. THIS INCIDENT OCCURRED WITH N842BP.SDR FDEA202008252031Seal · leakingDURING REFUELING FOUND RUNNING FUEL LEAKAGE FROM CENTER TANK (RIGHT WING TO AIR CONDITIONING FAIRING), IAW ENGINEERING (EMAIL) GVI DONE AROUND THE LEAK AREA, NO STRUCTURAL DAMAGE FOUND. ALSO PERFORM CHECK TO FASTENERS FROM OUTSIDE OF THE CENTER TANK AROUND SDR UIEA2020082601874Bolt · looseR FUEL SPAR VALVE ACTUATOR MOUNT BOLT (4EA) ARE LOOSE AND NEEDS SAFETY WIRE. INSTALLED AND SECURED AND INSTALLED SAFETY WIRE PER AMM 28-22-01 OPS NORMALSDR HALA2020081800174Actuator · faultedETOPS SIGNIFICANT SYSTEM. AFT FUEL TXFR ECAM ON TAXI. SYSTEM TESTS OF FCMC 1 FAULTED INNER TANK INLET 603QL1 REMOVED AND REPLACED 603QL1 FUEL INLET ACTUATOR PER AMM 28-26-53-400-801-A. OPERATIONS TEST OK, OK FOR SERVICE.SDR UIEA2020081971790Actuator · malfunctionedWHILE IN FLIGHT R FUEL SPAR VAL CAUTION MESSAGE LIGHT ILLUMINATED REMOVED AND REPLACED R/H FUEL SHUTOFF VALVE ACTUATOR IAW AMM 28-22-11, OPS CHECK GOODSDR P5CA2020081870284Lamp · inoperativeRIGHT ENGINE SPAR VALVE LIGHT INOPERABLE. RELAMPED RT SPAR VALVE LIGHT IAW B767 AMM 33-13-00. OPS CHECK GOOD.SDR AALA2020082099023Check Valve · unserviceableAIRCRAFT NOT GROUNDED - RIGHT WING OUTER TANK LEAKING FUEL INTO INNER TANK. MEL 28-02C RH INTRCELL XFR VLV, AUTHORIZED 04AUG2020T1513Z. CREW REPORTED TRANSFER VALVES CLOSED ON ECAM FUEL PAGE. PERFORMED AMM TASK 28-15-00-740-002-A FUNCTIONAL TEST OF THE INTESDR AALA2020082099022Check Valve · unserviceableAIRCRAFT NOT GROUNDED - RIGHT WING OUTER TANK LEAKING FUEL INTO INNER TANK. MEL 28-02C RH INTRCELL XFR VLV, AUTHORIZED 04AUG2020T1513Z. CREW REPORTED TRANSFER VALVES CLOSED ON ECAM FUEL PAGE. PERFORMED AMM TASK 28-15-00-740-002-A FUNCTIONAL TEST OF THE INTESDR AALA202008059017Valve · failedAIRCRAFT NOT GROUNDED - RIGHT WING OUTER TANK LEAKING FUEL INTO INNER TANK. CREW REPORTED TRANSFER VALVES CLOSED ON ECAM FUEL PAGE. PERFORMED AMM TASK 28-15-00-740-002-A FUNCTIONAL TEST OF THE INTERCELL TRANSFER VALVES, OPS CHECKED GOOD. REMOVED & REPLACEDSDR ASAA2020080322976Actuator · faultedDURING ENGINE START, NUMBER 1 ENGINE WOULD NOT START. TWO FAILED ATTEMPTS, ONCE ON IGN L & ONCE IGN R. ENGINE SPINS UP NORMALLY TO 25% N2, ONCE START LEVER IS ADVANCED MINIMAL EGT INCREASE TO ABOUT 200 DEGREES THEN ENGINE N2 & N1 DECELERATES. ABORTED ENGINE STSDR QMLA2020080320039Fuel Filter · faultedDURING PATIENT TRANSPORT THE "FUEL FILTER" CAUTION LIGHT ILLUMINATED INSIDE CLASS D. THE PILOT ANNOUNCED TO THE MED CREW THAT HE HAD A POTENTIALLY CRITICAL SITUATION AND WAS IMMEDIATELY EXECUTING A PRECAUTIONARY LANDING. DECLARED AN EMERGENCY WITH TOWER. FLEWSDR JJBA2020080372005Flapper Valve · damagedATC REPORTED FUEL OR SMOKE COMING FROM RH WING 1/4 - 1/3 FROM WING TIP ON TAKEOFF JUST AFTER ROTATION. FOUND FLAPPER VALVE AT RIB 19 TORN/DAMAGE. R&R FLAPPER VALVE. PERFORMED FLAP VALVE OPERATION CHECK. OPS CHECK SAT. REINSTALLED FUEL TANK ACCESS PANEL. LEAK CSDR HALA2020072400154Actuator · malfunctionedETOPS SIGNIFICANT SYSTEM - ENG 2 FUEL LP SHUT OFF VALVE MOTOR INOP. // VERIFIED ENG 2 LP FUEL VALVE MOTOR 1 INOP PER AMM 28-24-00-710-803-A 07/22/20 2020495. REPLACED THE NR 2 ENG LP FUEL VALVE ACTUATOR IAW AMM 28-24-51. OPS CHECKED OK.SDR UIEA2020072001586Fuel Sys · unknownRT ENGINE STARTED ON SECOND ATTEMPT, ENGINE RAN NORMALLY FOR 3 MINUTES. THEN FUEL FLOW WENT TO ZERO AND ENGINE SHUTDOWN. RETURNED TO BLOCKS. PERFORMED AN OPS CHECK IAW 28-22-11. RAN ENGINE THREE TIMES WITH NO FAULTS IAW AMM 70-00-00. CYCLED SPAR VALVE CIRCUITSDR AALA202007139010Actuator · unserviceableAIRCRAFT NOT GROUNDED, IN-FLIGHT ECAM FAULT: CTR TK L XFER. COMPLIED WITH ECAM PROCEDURES AND PUMP RETURNED TO NORMAL OPS SHORTLY THEREAFTER. REMOVED AND REPLACED FUEL CONTROL VALVE ACTUATOR 11QL PER AMM 28-26-51, OPERATIONAL CHECK GOOD, CLEARED MEL.SDR ABXA20200713125Actuator · failedR ENG FUEL VAL EICAS MSG. AIRCRAFT WAS GROUNDED.SDR UIEA2020070901503Switch · unsecureLT FWD FUEL PUMP EICAS BLED PRESSURE SWITCH SENSE LINE FOR LT BOOST PUMP, RE-SECURED SWITCH AND LINE. LT FWD BOOST PUMP AND PRESS LIGHTS OPS CK NORMAL IAW AMM 28-42-01.SDR 2020FA0000325Fitting · looseHELICOPTER LANDED AFTER A TRIP AND THE PILOT PROCEEDED WITH THE ENGINE SHUT DOWN PROCEDURE. AS PER THE ENGINE SHUTDOWN CHECK LIST, THE ENGINE SWITCH WAS IN THE IDLE POSITION. THE PILOT MOVED THE NR 1 AND 2 FUEL PUMP SWITCHES TO THE OFF POSITION. PILOT WAS WASDR FDEA202007031439Valve · failedTNK 3 TIP TRAPPED ALERT DURING CRUISE. 5800 LBS TRAPPED IN #3 TANK. EMERGENCY DECLARED WITH ATC. IN REF TO FFC ERO 5200247 REMOVED REPLACED AND OPS CHECKED #3 MOTIVE SHUTOFF VALVE IRW FE MD10- 30 AMM 28-21-13-2 AND FE MD10-30 FIM 28-14-00-810-803. OPS CHSDR UIEA2020070101458Pin · backed outINFLIGHT ONLY, WITH FUEL IN THE CENTER TANK INDICATING EMPTY, CTR L FUEL PUMP EICAS AND CTR L PRESS LIGHT WILL NOT DISPLAY. TROUBLE SHOT L CTR FUEL PUMP PRESS SWITCH, FOUND A PUSHED BACK PIN. REPOSITIONED PIN, OPS CHECK GOOD IAW AMM 28-42-00 / 28-42-01. THISDR AALA2020062979008Relay · faultyAIRCRAFT NOT GROUNDED: AFTER TAKE OFF IN CLIMB, MESSAGE FOR CTR TK R XFR FAULT LIGHT ILLUMINATED AMBER AND FUEL ABOVE 11.6 IN CENTER TANK. REPLACED AUTO CONTROLL RELAY 8QL IAW ESPN 20-46-50.SDR HALA2020062600134Switch · malfunctionedETOPS SIGNIFICANT SYSTEM FUEL APU VALVE FAULT ON ECAM. FOUND APU ISOL VALVE (5QF) ON GRD RPT. REPLACED ACTUATOR. NO HELP. REINSTALLED ORG ACTUATOR. OPS CHK OF THE APU FUEL ISOL. VLV AND APU LP S/O VLV ACTUATOR FOUND STUCK OPEN. FOUND APU FUEL VENT P/BSWSDR HALA2020062300130Actuator · malfunctionedETOPS SIGNIFICANT SYSTEM - "FUEL AFT XFER" INOP STATUS MESSAGE ON STATUS PAGE. // PER TSM TASK 28-27-00-810-829-A FOUND FUEL TRIM TANK ISOLATION VALVE
FAULTING (FIN 702QN). REMOVED AND REPLACED FUEL TRIM TANK ISOLATION VALVE ACTUATOR (FIN 702QN) PER AMM 28SDR 2020FA0000317Fuel Line · corrodedATTEMPTED TO START AIRCRAFT TO TAXI TO HANGAR. LT ENGINE STARTED NORMALLY. RT ENGINE WAS VERY DIFFICULT TO START AND WOULD QUIT AS SOON AS BOOST PUMP WAS TURNED OFF. OWNER VERIFIED THAT HE HAD BEEN HAVING SERIOUS DIFFICULTY STARTING AND MAINTAINING ENGINE OPSDR AALA202006049005Ufi · malfunctionedAIRCRAFT WAS NOT GROUNDED. IMMEDIATELY AFTER TAKEOFF, LEFT CENTER FUEL PUMP LOW PRESSURE LITE CAME ON. CREW FOLLOWED QRH PROCEDURE. MAINTENANCE ACCOMPLISHED FIM TASK 28-22-00-810-822, UFI REPORTS STATUS CODE 10. RESET UFI AND FAULT CLEARED. A SATISFACTORSDR UIEA2020060401205Control Panel · faultyCTR L FUEL PUMP FLOW BAR NOT ILLUMINATED. REMOVED AND REPLACED FUEL MGMT PANEL IAW AMM 28-22-17.SDR ASAA2020051332723Unknown · leaking#1 ENGINE HAS FUEL LEAKING FROM LOWER COWL DRAIN. GROUNDED - YES. RAN #1 ENGINE AT IDLE ACCOMPLISHED INSPECTION OF ENGINE VENTS AND DRAINS REF B737-900 AMM 71-71-00-200-801-F00 NO LEAKAGE NOTED DURING ENGINE RUN OR AFTER ENGINE SHUTDOWN. SUSPECT #1 ENG SPAR VA
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