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 AALA201705199007Warning Message · false activationFUEL AUTOFEED FAULT. FUELED AIRCRAFT IAW AMM12-11-28, ALL FAULTS CLEARED.SDR AALA201705199020Transmitter · faultyDIVERTED DUE TO A FUEL FLOW ANOMALY. NO EMERGENCY DECLARED AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE NR 1 ENGINE FUEL FLOW TRANSMITTER IAW AMM 73-31-17. AIRCRAFT WAS GROUNDED.SDR ASMF201705002Pump · failedCAPTAIN REPORTED THAT DURING CRUISE, THE FUEL QUANTITY INDICATION WAS WRONG, FUEL QUANTITY WAS VERIFIED USING FUEL DIPSTICK. OPS TESTED FOR THE SYSTEM FUEL QUANTITY INDICATOR PERFORMED IAW AMM 28-24-00, FUEL TRANSFER WHEN NOT COMMANDED WAS PERFORMED IAW FIM 2SDR ASAA2017051220727Circuit Breaker · trippedNR 2 SPAR VALVE REMAINED IN TRANSIT ON START ATTEMPT. ACFT GROUNDED. FOUND THREE CIRCUIT BREAKERS TRIPPED. NR 2 ENGINE SPAR VALVE, NR 2 ENG LT & RT IGNITION. PERFORMED CIRCUIT BREAKER RESET PROCEEDURES IAW 20-60-01, RAN NR 2 ENGINE, OPS CHECKED GOOD. GROUSDR AALA201705129004Control Valve · faultedDURING CLIMBOUT, RECEIVED A FUEL CTR RT TRANSFER FAULT ON ECAM. 10,500 LBS OF FUEL IN THE CENTER TANK. REMOVED AND REPLACED THE SINGLE MOTOR ACTUATOR VALVE.SDR UIEA2017051000768Relay · malfunctionedLEFT AFT FUEL PUMP EICAS MESSAGE DISPLAYED ON PUSHBACK. REMOVED AND REPLACED GFI RELAY K10705 IAW SWPM 20-81-22. OPS CHECKED GOOD.SDR CALA2017050501252Unknown · malfunctionedFUEL LEAK ON RIGHT SIDE AFTER CENTER PUMPS OFF MORE THAN 2000LB SPLIT IN 20 MINS. FUEL IMBALANCE REPORTED LT MAIN 13.7 RT MAIN 9.8 AND CONFIG LIGHT ON. STUCK BOTH TANKS CONFIRMED IMBALANCE, PERFORMED TEST OF THE ENGINE X-FEED VALVES IAW AMM 28-22-02-714-055 &SDR P5CA2017050300101Warning Message · intermittentNR 1 ENGINE SPAR VALVE INDICATION INTERMITTENT.SDR AALA201705029037Unknown · malfunctionedAIRCRAFT WAS GROUNDED. CAPTAIN REPORTED RIGHT MAIN TANK LOST 1500 LBS OF FUEL AND THE FUEL CONFIGURATION LIGHT ILLUMINATED. RIGHT PUMPS SHUT OFF TO EMPTY CENTER TANK. AFTER CENTER TANK WAS AT 0 IT ROSE AGAIN TO 400 LBS WHEN RIGHT TANK PUMPS WERE TURNED ON ASDR AALA201705029023Control Valve · stuckAT CRUISE RECIEVED A FUEL ACT TRANSFER FAULT ECAM, SELECTED FOWARD ON ACTUATOR PUMP IAW ECAM PROCEEDURES. FWD ACTUATOR RAN EMPTY, MESSAGE WENT AWAY FOR A FEW MINUETS, THEN RETURNED. FUEL IN AFT ACTUATOR INDICATES 4100 LBS. REPLACED INTERMITTENTLY STICKING ASDR AALA201705019049Gfi · trippedAIRCRAFT WAS GROUNDED. EMERGENCY WAS DECLARED FOR CENTER TANK FUEL BOOST PUMP INOPERABLE. FOUND GROUND FAULT INTERRUPTERS 69QA AND 70QA TRIPPED. RESET GFI IAW AMM 28-21-00 C/W. OPS TEST OF MAIN FUEL PUMP SYSTEM REF AMM 28-21-00-710-007. OPS CK GOOD. A/C OK FORSDR A6WA201744943Switch · not seatedAFTER ROTATION EXPERIENCED FAINT ELECTRICAL, BURNT / OVERHEATED BRAKE ODOR. WENT AWAY, RETURNED AFTER 5-6 MIN AND AGAIN 20 MIN INTO FLIGHT. EACH TIME A LITTLE STRONGER ODOR. NO INOP FANS, LIGHTS OR ASSOCIATED MESSAGES. ODOR MAINLY IN COCKPIT. 2 TIMES ON APU BLSDR ASAA2017042020506Valve · malfunctionedSPAR VALVE ENG 2 CIRCUIT BREAKER POPPED. GROUNDED - YES. CONDUCTED GVI OF P6-3 AND P6-2 PANELS TO ENSURE C/B B3 CONDITION IS NORMAL, AND IT PASSED, PER B737-900 AMM 20-60-01. RESET C/B , B3 PERFORMED VERIFICATION OF NORMAL SPAR VALVE OPERATION PER B737-900 FIMSDR AALA201704219006Actuator · stickingAIRCRAFT WAS GROUNDED. ACT 1 WILL NOT ACCEPT FUEL. MAINTENANCE FOUND ACT 1 INLET VALVE ACTUATOR STICKING. REPLACED ACT 1 INLET VALVE ACTUATOR (5QH) PER M/M 28-28-34. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.SDR DALA2017041703220Structure · corrodedCORROSION, STA 912, RBL 56 CENTER WING TANK. REPAIRED IAW ERA 555238-14.SDR HALA2017041500101Actuator · defectiveFUELERS REPORT HAVING TROUBLE FUELING. LT FUEL OUTER TANK, INLET VALVE ACTUATOR FAULT. RESET FCMC 1 & 2, NO HELP, DOWN POWER A/C, RESET POWER, FCMC 1 & 2 SYS TEST OK. NO FURTHER DEFECTS NOTED DURING CONTINUED FUELING. OK FOR SERVICE. REMOVED & REPLACED LT FUELSDR VQI2017F00001Sump · leakingON ARRIVAL AT ACFT FOR FIRST FLIGHT, CREW DETECTED A STRONG FUEL ODOR IN THE COCKPIT AND THROUGHOUT CABIN. ODOR DISSIPATED WITH APU BLEED ON. DURING INSPECTION, IAW TSM 055000810831A, FOUND RT CENTER TANK FUEL SUMP LEAKING. RESEATED SUMP DRAIN AND CLEANED ASDR V6NA20170406001Fuel Line · crackedDEGRADED ABILITY TO TRANSFER FUEL WHICH COULD HAVE LED TO AN UNSAFE FUEL CONDITION. PRECAUTIONARY DIVERSION. LANDED WITHOUT INCIDENT. DETERMINED TO BE RESULT OF CRACKED FUEL TUBE FLARE. REPLACED FLARED END OF TUBING. AIRCRAFT RETURNED TO SERVICE.SDR AALA201704079005Warning Light · false activationFUEL AUTOFEED FAULT IN CLIMB AND CRUISE WHILE IN AUTO MODE. ACCOMPLISHED ECAM NOW NORMAL ACTIONS AND REQUIRED FOLLOW UP. NO SIGNIFICANT OF FUEL IMBALANCE. MAINTENANCE COULD NOT DUPLICATE, NO FAULTS FOUND, ACCOMPLISHED TS IAW TSM 28-21-00-810-816-A AND TSM 28-SDR VE7A2017040300001Drain Valve · leakingDURING FLT, THE AIRCRAFT YAWED SLIGHTLY TO THE RIGHT & THEN BACK LEFT. IMMEDIATELY FOLLOWING THE OCCURRENCE OF THE YAW, THE FIRST LIMITATION INDICATOR (FLI) FLUCTUATED SLIGHTLY, AND THE FEEL OF THE COLLECTIVE SETTING CHANGED AS THE POWER REQUIRED TO HOLD THE SDR AALA201703299008Concentrator · faultyFUEL CENTER TANK NR 1 PUMP LOW IAW ECAM. NO FAULT FOUND IAW TSM 28-21-00-810-813-A. OPS NORMAL IN MANUAL AND AUTO MODES. DUE TO SIMULTANEOUS AIRMAN HITS OF LEFT WING PUMPS 1 & 2 AND CENTER TANK PUMP NR . REPLACED SYSTEM DATA ACQUISITION CONCENTRATOR NR 1 IAWSDR HALA2017032700086Valve · faultedECAM FOR TRIM TANK TRANSFER FAULT. REMOVED AND REPLACED THE LEFT OUTER TANK INLET VALVE IAW AMM 28-25-57. OPS NORMAL.SDR CALA2017032100662Ufi · faultyLOW PRESSURE LIGHT FOR THE FUEL PUMP LIGHT ON CENTER TANK, RIGHT PUMP REPLACED RT CENTER UFI AND RAM REF AMM28-22-19. RAN PUMP, CHECKED OK.SDR AALA201703249002Relay · faultyLEFT CENTER TANK FUEL PUMP EICAS MESSAGE AND OVERHEAD SWITCH. REMOVED AND REPLACED UNIVERSAL FAULT INDICATOR AND RELAY ADAPTER MODULE IAW TDG SUPPLEMENT 28-22-00. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.SDR AALA201703239023Indicator · faultyLEFT CENTER TANK FUEL PUMP EICAS MESSAGE AND OVERHEAD SWITCH. REMOVED AND REPLACED UNIVERSAL FAULT INDICATOR AND RELAY ADAPTER MODULE IAW TDG SUPPLEMENT 28-22-00. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.SDR AALA201703149002Ufi · malfunctionedAIRCRAFT WAS NOT GROUNDED. CENTER TANK LEFT FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED WITH FUEL IN CENTER TANK. ACCOMPLISHED FIM 28-22-00-810-801. RESET LEFT UNIVERSAL FAULT INTERRUPTER IAW FIM 28-22-00-810-822. OPERATIONAL CHECK GOOD.SDR HALA2017031200061Actuator · failedDURING LINE SERVICE, UNABLE TO FUEL RIGHT OUTER, REMOVED AND REPLACED RIGHT OUTER INLET FUEL VALVE ACTUATOR. PER AMM 28-25-57-000-801-A. OPS CHECK OK . OK FOR SVCSDR AALA201703139024Not Reported · unknownAIRCRAFT WAS GROUNDED. AT CRUISE ALTITUDE FL 280 WE NOTICED THE PLANE WAS FLYING WITH RIGHT WING DOWN. THOUGHT IT MIGHT BE CONTROL PROBLEM, TURNED OUT TO BE FUEL IMBALANCE. RAN QUICK REFERENCE HANDBOOK, DECLARED EMERGENCY, DIVERTED TO JFK. LANDED WITH 5000 LBSSDR HALA2017030600050Transfer Sys · malfunctionedSTATUS MESSAGE FOR FUEL AFT TRANSFER ILLUMINATED. FUEL WILL NOT TRANSFER AFT DURING CLIMB. FCMC 1 AND 2 RESET. FUEL VALVE TESTED IAW AMM 28-25-00. FUEL TRANSFER IN BOTH DIRECTIONS NORMAL.SDR HALA2017030400045Actuator · failedAIRCRAFT NOT TAKING FUEL, FOUND LEFT OUTER TANK INLET VALVE ACTUATOR FAILED. REMOVED AND REPLACED THE LEFT INLET VALVE ACTUATOR IAW AMM 28-25-57. OPS CHECKED GOOD, OK FOR SERVICE.SDR AALA201702199009Actuator · failedTRIPPED FUEL TRIM TANK INLET VALVE M61 CIRCUIT BREAKER. MAINTENANCE REPLACED TRIM TANK FUEL INLET VALVE ACTUATOR IAW AMM 28-27-52.SDR AALA201702139014Actuator · failedRIGHT CENTER FUEL PUMP INOPERATIVE ON ECAM DISPLAY. REMOVED AND REPLACED FUEL CONTROL VALVE ACTUATOR.SDR UIEA2017021300178Valve · malfunctionedEVIDENCE OF FUEL MIGRATION FROM RT MAIN TANK TO LT MAIN TANK. REMOVED AND REPLACED THE FUEL CROSSFEED VALVE BODY IAW AMM 28-22-02, OPS CHECKED IAW AMM 28-22-00. NO DEFECTS NOTED </P>)SDR AALA20170210014Fuel Sys · low pressureDURING TAKE OFF ROLL WITH THE RIGHT FOWARD BOOST PUMP ON MEL THE RIGHT AFT MAIN TANK LOW PRESSURE LIGHT ILLUMINATED. TAKE OFF ABORTED AT APPROXIMATELY 70 KNOTS. MAINTENANCE SUMPED FUEL TANKS IAW AMM 12-11-00 WITH NO WATER FOUND. ACCOMPLISHED OPERATIONAL TEST ISDR AALA201702099007Relay · faulty(ECAM) FUEL ACT TRANSFER FAULT. COMPLIED WITH QRH/ECAM PROCEDURES. FLT DIVERTED. REPLACED RELAYS 13QH, 14QH AND 22QH.SDR AALA201702099006Relay · faulty(ECAM) FUEL ACT TRANSFER FAULT. COMPLIED WITH QRH/ECAM PROCEDURES, FLT DIVERTED. REPLACED RELAYS 13QH, 14QH AND 22QH.SDR AALA201702099005Relay · faultyAIRCRAFT NOT GROUNDED. (ECAM) FUEL ACT XFR FAULT. COMPLIED WITH QRH/ECAM PROCEDURES. PER MAINTENANCE CONTROL AND DISPATCH, FLT DIVERTED TO LAS. REPLACED RELAYS 13QH, 14QH AND 22QH. (SEE AALA201702099006 & AALA201702099007)SDR ASAA2017020419667Module · failedON FINAL, SELECTING TAXI LIGHT TO ON FUEL VALVE OPEN LIGHT ILLUMINATED THEN EXTINGUISHED. SELECTING FIXED LANDING LIGHT FROM PULSE, VALVE OPEN LIGHT ILLUMINATED. ON SHUT DOWN AT GATE, SELECTING FUEL PUMP OFF VALVE LIGHT ILLUMINATED AGAIN. ACFT GROUNDED. INSPESDR UIEA2017012700114Valve · no testON STARTING THE RT ENGINE SPAR VALVE FAILED OPS CHECK IAW AMM 28-21-02.SDR AALA20170113015Actuator · faultyLEFT FUEL SPAR VALVE STUCK IN TRANSIT. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED LEFT FUEL SPAR VALVE ACTUATOR IAW AMM 28-22-11. OPERATIONAL CHECK GOOD.SDR CALA2017010900033Skin · corrodedCENTER WING TANK UPPER SKIN AT FWD OF FR43 RT O/B OF 1292 SEAT TRACKS C1 HAS CORROSION. INTERIM REPAIR ACCOMPLISHED PER ECRA5710-02585 PART 1. ACCOMPLISHED HFEC SURFACE SCAN IAW NTM 51-10-16. ACCOMPLISH INITIAL INSPECTIONS OF THE AFFECTED AREA PER PART 2 OF ECSDR HALA2017010700011Filter · leakingFUEL LEAKING FROM RIGHT ENGINE AFTER LANDING. FUNCTIONAL TEST OF THE EMERGENCY SHUTDOWN SYSTEM OK IAW AMM 76-20-00-720-801. REMOVED AND REPLACED LP FUEL FILTER HOUSING IAW AMM 73-11-01. OPS OK. LEAK CHECKED OK.SDR ASAA2017010119206Drain Mast · crackedAPU DRAIN MAST HAS EXTENSIVE CRACKING AROUND ROOT FILLET AND DELAMINATION OF THE LEADING EDGE. GROUNDED - YES. REMOVED AND REPLACED DAMAGED APU DRAIN MAST PER REF AMM 28-25-07-020-801 AND 28-25-07-420-801.SDR DXTA2016122806348Fuel Sys · unknownFUEL WILL NOT TRANSFER FROM CENTER TO RIGHT WING. FUEL MIGRATES BACK TO CENTER TANK FROM LEFT WING. PERFORMED OPS CHECK OF CENTER TANK TRANSFER SYSTEM. FUEL TRANSFERS FROM CENTER TO RIGHT TANK NORMALLY. WITH 80 LBS IN CENTER TANK AND 3000 LBS FUEL IN WING TANSDR ASAA2016122419141Actuator · failedDURING LANDING ROLLOUT, THE SPAR VALVE CLOSED LIGHT ILLUMINATED FOR APPROX 5 SECONDS. NO ABNORMAL ENGINE PARAMETERS NOTED. ACFT GROUNDED. REMOVED THE NR 1 SPAR VALVE ACTUATOR IAW AMM 28-22-11-000-804. INSTALLED THE NR 1 SPAR VALVE ACTUATOR IAW AMM 28-22-11-SDR AALA20161227008Float Valve · faultyDURING CRUISE, UNWANTED TRANSFER OF FUEL FROM THE CENTER TANK TO THE NR 1 LEFT MAIN TANK. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED LEFT MAIN FUEL SCAVENGE FLOAT OPERATED SHUT OFF VALVE IAW AMM 28-22-16. OPERATIONAL AND LEAK CHECK GOOD.SDR AALA201612239016Relay · malfunctionedLEFT FUEL TANK PUMP NR 1 LOW PRESSURE ECAM MESSAGE. MAINTENANCE REPLACED THE NR 1 TANK PRESSURE SWITCH AND MICROSWITCH (17QA) AMM 28-21-15.SDR AALA201612239015Pressure Switch · malfunctionedLEFT FUEL TANK PUMP NR 1 LOW PRESSURE ECAM MESSAGE. REPLACED THE NR 1 TANK PRESSURE SWITCH AND MICROSWITCH (17QA) AMM 28-21-15.SDR IPXA2016122312037Fuel Sys · malfunctionedAT TOP OF CLIMB, ATTEMPTING TO TRANSFER UPPER AUX FUEL INTO THE MAIN TANKS. HAD 5000 LBS IN UPPER AUX. WHEN UPPER AUX GOT TO 2500 LBS THE PUMPS TURNED AMBER AND TRANSFER STOPPED. NO SUCCESS ON REPEATED ATTEMPTS FUEL FOUND TO BE IN LOWER AUX TANK WHICH IS DEACTSDR VNAA2016121600034Valve · leakingFUEL LEAKING FROM NR 2 ENGINE DRAIN. REMOVED AND REPLACED THE RELIEF VALVE.
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