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 AALA201607229003Pressure Switch · faultedFUEL AUTO FEED FAULT AFTER GEAR RETRACTION ON TAKEOFF. REPLACED FUEL PRESSURE SWITCH 39QA AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 28-21-15-400-001-A.SDR UIEA2016072000604Relay · not seatedLEFT FWD FUEL PUMP EICAS MSG, LT FORWARD FUEL PUMP, ON LANDING, DEFERRED IAW MEL 28-22-01, MDDR 68556. CAT-C DUE. LP 787233, ITEM M3: REF MDDR 68554, RESEATED RELAY K 188 IN P33 PANEL, OPS CHECK C/W IAW MM 28-22-00, OPS NORMAL. THIS CLEARS MDDR 68554, PLACASDR ASAA2016071817419Actuator · failedFOLLOW-UP TO X-FEED VALVE ACTUATOR C/B OUT. ACFT GROUNDED. REMOVED & REPLACED CROSSFEED VALVE ACTUATOR IAW AMM 28-22-21. PERFORMED OPERATIONAL TEST IAW AMM 28-22-21-710-801, OPS CHECKED GOOD.SDR AALA20160718004Relay · faultyDURING CRUISE FUEL WOULD NOT FEED FROM THE NR 2 ACTUATOR CENTER FUEL TANK. EMERGENCY NOT DECLARED. LANDING UNEVENTFUL. ACCOMPLISHED ECO M0104AA, REMOVED AND REPLACED RELAYS E0217XXZ060A2 AND E0217XXW0600A2. OPS CHECKED NORMAL.SDR AALA20160715001Relay · faultyDURING CRUISE, FUEL WOULD NOT FEED FROM THE NR 2 ACTUATOR CENTER FUEL TANK. LANDING UNEVENTFUL. ACCOMPLISHED ECO M0104AA, REMOVED AND REPLACED RELAYS E0217XXZ060A2 AND E0217XXW0600A2. OPS CHECKED NORMAL.SDR 2016FA0000326Clamp · failedHOSE CLAMP ASSEMBLY FAILED ON THE FUEL INDUCTION SYSTEM CAUSING ENGINE TO FAIL.SDR AALA201607099005Pressure Switch · malfunctionedAIRCRAFT WAS NOT GROUNDED: FUEL-L- PUMP LOW PR 2 FAULT DURING DESCENT, 13000 FT. MAINTENANCE BLED FUEL SWITCH 75QA1 AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW TSM 28-21-00-810-852-A.SDR UIEA2016063000548Pressure Switch · defectiveLEFT AFT FUEL PUMP C/B POPPED ON GROUND WAS RESET AND REMAINED OK. PRESSURE SWITCH REPLACED IAW MM 28-42-01.SDR QXEA2016062700410Coupling · looseAT CRUISE FLIGHT OF 23,000, THE NR 1 ENGINE FUEL PRESSURE CAUTION FLASHED ON AND OFF ABOUT 12 TIMES. DID NOT SELECT THE NR 1 AUXILIARY PUMP ON, DUE TO THE CAUTION FLASHING ON FOR LESS THAN 1-2 SECONDS EACH TIME. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. SDR RAIA201606270002Switch · burnedSMOKE AND BURNING ODOR COMING FROM ABOVE CAPTAIN`S OVERHEAD PANEL. REMOVED FUEL CONTROL PANEL TO FURTHER INVESTIGATE SMOKE ODOR. R & R FUEL CONTROL PANEL DUE TO CROSSFEED SWITCH BURNED. R & R CIRCUIT BREAKER FOR FUEL CROSSFEED. OPS CHECK GOOD.SDR UIEA2016062700470Housing · dirtyLT WING JETTISON PUMP CTR AUXILIARY BONDING RESISTANCE BETWEEN PUMP TO WING HIGH RESISTANCE. PUMP HOUSING CLEANED AND PERFORMED RESISTANCE CHECK AND FOUND WITHIN LIMITS IAW SWPM 20-20-00.SDR UIEA2016062700519Connector · damagedAFT CARGO APU FUEL DUCT CLIP IS DAMAGED. AFT CARGO APU FUEL SHROUD REPLACED CONNECTOR.SDR IPXA2016070805539Tube · kinkedINSPECTION TYPE: 3C, RT WING FUEL TRANSFER PIPE HAS A LARGE DENT AT XOS 703.6. REPAIRED THE TRANSFER PIPE IAW EA 011-2820-A6336 REV. I/R AND EO MD11-2820-61199-A. (MINOR)SDR AALA201606229008Contact · defectiveAIRCRAFT WAS NOT GROUNDED. FUEL CENTER TANK PUMP 1 LOW PRESSURE FAULT. MAINTENANCE ACCOMPLISHED TSM 28-21-00-810-817-A AND FOUND CONTACT 69QA BAD. CONTACT 69QA WAS REPLACED AND A SATISFACTORY OPS CHECK WAS ACCOMPLISHED.SDR P5CA2016061900143Relay · failedLEFT FWD FUEL BOOTS PUMP AUTOMATIC FUNCTION INOPERATIVE. TRANSFER TO MEL 28-22-01-01. T/S SYSTEM USING WIRING DIAGRAM 28-25-11, 28-22-11, AND FIM TASK 28-25, FAULT TREE 808. REPLACED LT FWD PUMP PWR SENSE RELAY K513 IAW SWPM CH 20-81-19, SYSTEM CK'S GOOD IASDR AALA201606169001Fuel Line · low pressureAIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED FUEL, LEFT PUMP 2, LOW PRESSURE ON ECAM AT CRUISE ALTITUDE. FUEL SYS RETURNED TO NORMAL AND ECAM CAUTION WENT AWAY AFTER 15 MINUTES. MAINTENANCE ACCOMPLISHED A PURGE OF THE PRESSURE SWITCH FEED LINE OF THE MAISDR AALA201606089013Pressure Switch · defectiveAIRCRAFT WAS NOT GNDED. CTR TANK PUMP NR 2 LOW PRESS LIGHT CAME ON DURING START. REPLACED CTR TANK NR 2 BOOST PUMP LOW PRESS SWITCH AMM 28-21-15. A SATISFACTORY LEAK & OPERATIONAL CHECK WAS ACCOMPLISHED.SDR ASAA2016060716978Actuator · failedDURING THE FIRST START ATTEMPT, APU FAULT LIGHT ILLUMINATED. ACFT GROUNDED. PERFORMED APU BITE CK, REF FIM 49-60, TASK 801 FOUND FAULT 49-31214 APU FUEL VALVE SHOWS NOT OPEN. PERFORMED FIM TASK FOR FAULT FOUND APU FUEL SHUTOFF VALVE INOPERATIVE. R & R APU SHSDR AALA20160606004Coupling · disconnectedAIRCRAFT WAS GNDED. UNWANTED & UNCOMMANDED TRANSFER OF FUEL FROM RT WING TANK TO CTR TANK. FOUND RT WING INBD FUELING VLV LINE DISCONNECTED FROM FRONT SPAR. RECONNECTED CTR FUEL TANK FUEL & DEFUEL COUPLING.SDR AALA201606069001Pressure Switch · faultyRETURNED & ACFT WAS GNDED. FLIGHT CREW REPORTED AN EICAS FAULT MSG FOR THE RT FWD FUEL PUMP ALONG WITH A LOW PRESS LIGHT FOR THE SAME FUEL PUMP DURING CLIMB OUT. THE ACFT RETURNED WHERE MX REPLACED THE PRESS SWITCH AT THE RT FWD FUEL BOOST PUMP IAW AMM 28-42SDR EVCA201606061Filter · leakingDURING CRUISE FLIGHT, CREW NOTICED A STRONG FUEL ODOR IN THE CABIN. MECHANIC FOUND AN UNSERVICEABLE CHECK VALVE, PN: 869A-6TT AND FILTER ASSY PN: 206-364-603-101.SDR 2016FA0000267Fuel Sys · malfunctionedUPON INITIAL DESCENT, FROM A CRUISING ALTITUDE OF 45,000 FT, THE PILOT BEGAN REDUCING ENGINE POWER. THE NR 2 ENGINE ROLLED BACK TO IDLE, THEN SHUTDOWN UNCOMMANDED. THE PILOT ATTEMPTED TO RESTART THE NR 2 ENGINE, BUT WAS UNSUCCESSFUL. THE LANDING WAS UNEVENTFSDR AALA201605289003Pressure Switch · defectiveAIRCRAFT WAS NOT GNDED. CTR TANK PUMP 2 INOPERATIVE. REPLACED NR 2 CTR TANK PRESS SWITCH IAW AMM 28-21-15-0401.SDR ASAA2016052516849Warning Light · false activationFUEL IMBALANCE ON CLIMBOUT, GOT CENTER TANK RT PUMP LOW PRESSURE LIGHT. STARTED GETTING IMBALANCE BETWEEN MAIN TANK 1 & 2. OPENED CROSSFEED & NOTED NR 1 ENGINE BURNING OFF CENTER TANK & NR 2 STILL BURNING OFF NR 2 MAIN TANK FUEL WITH 2000 LB IN CENTER. ONCESDR SWAA2016052351982Valve · faultyAIR TURN BACK. NR 1 SPARE VLV CLOSED LT ILLUMINATED BRIGHT ON CLIMB OUT. R & R NR 1 ENG SPARE VLV IAW AMM.SDR ASAA2016052016805Actuator · failedFUEL IMBALANCE AT FL370, RAN QRH 12.2 CROSSFEED SELECTOR INOPERATIVE. FOUND C/B CROSSFEED VALVE POPPED. BOTH ENGINES SEEMED TO BE RUNNING ON LT TANK. FUEL IMBALANCE QUICKLY GREW TO 2000 POUNDS. DIVERTED, NORMAL LANDING. ACFT GROUNDED. DIVERSION - 16 MINUTSDR IPXA2016040601754Actuator · inoperativeDIVERSION - NR 1 FUEL TRANSFEED DISAGREE ALERT DURING FLT NR 1 TANK 2000, LBS IMBALANCE AFTER LANDING NR 1 FUEL TRANSFEED DISAGREE LIGHT DISAPPEARED. R & R NR 1 FUEL CROSS FEED VALVE ACTUATOR IN REF TO MM 28-22-31-4. OPS CHECK NORMAL IN REF TO MM 28-22-30. OSDR 2016FA0000156Strainer · misinstalledFUEL GASCOLATOR/STRAINER ON FIREWALL WAS FACTORY-INSTALLED BACKWARD. FUEL FROM TANKS ENTERED THE "OUT" PORT, FUEL GOING TO CARBURETOR WENT OUT THE "IN" PORT. PORTS ARE MARKED PLAINLY BUT NOT EASILY VISIBLE AFTER INSTALLATION. PROBLEM WAS FOUND AFTER NOTICING SDR HYIA20160323001B-Nut · loosePILOT REPORTED FUEL SMELL IN CABIN. TIGHTENED UNION JAM NUT & B NUT FOR LINE LEADING INTO RT FUEL TANK, IN RT BOOST PUMP PANEL IAW MM CH 28. LEAK CHECKED GOOD.SDR AALA201603209002Contactor · trippedAIRCRAFT WAS GNDED. CTR TANK 1 INOPERATIVE. FOUND THE GFI CONTACTOR 69QA POPPED. PERFORMED TSM 28-21-00-810-828 PUMP AN ACFT WIRING CHECK WITH NO FAULTS FOUND. REPLACED GFI CONTACTOR 69QA AS A PRECAUTIONARY MEASURE & ACCOMPLISHED A SATISFACTORY OPERATIONALSDR AALA20160306009Ufi · malfunctionedRIGHT CTR PUMP ONLY ALLOWED 1,500 PDS TO ENGS, THEN QUIT. EMER DECLARED & FLIGHT LANDED WITHOUT INCIDENT. FOUND NO POWER TO RT UFI. REPLACED RT UFI & RAM ASSEMBLY. PERFORMED ALL REQUIRED TESTS, ALL CHECKED NORMAL. RT CTR PUMP OPERATES NORMAL IAW MM 28-22-SDR SWAA2016030749715Coupling · disconnectedAIR TURN BACK, DURING CLIMB & THEN DESCENT, VISIBLE FUEL STREAM EMANATING FROM WINGS, NOTICEABLE EXCESSIVE FUEL BURN. CONNECTED COUPLINGS IAW AMM.SDR AALA201602179001Check Valve · defectiveAIRCRAFT WAS GNDED. FLEW 2, 4 HOUR FLIGHT, ON ARRIVAL LT FUEL WING 4800 & RT WING 3200. FUEL BURN 7700 ON LT ENG & 7600 ON RT. FOUND LT WING CHECK VLV 37QM & AIR RELEASE VLV 86QM FAULTING. R & R CHECK VLV & AIR RELEASE VLV IAW AMM 28-21-43-0401 & 28-21-41-SDR AALA201602169007Check Valve · defectiveAIRCRAFT WAS GNDED. FLEW 24 HOUR FLIGHT, ON ARRIVAL LT FUEL WING 4800 & RT WING 3200. FUEL BURN 7700 ON LT ENG & 7600 ON RT. FOUND LT WING CHECK VLV 37QM & AIR RELEASE VLV 86QM FAULTING. R & R CHECK VLV & AIR RELEASE VLV IAW AMM 28-21-43-0401 & 28-21-41-04SDR AALA201602169006Control Unit · defectiveAIRCRAFT WAS NOT GNDED. ECAM, FUEL AUTO FEED FAULT, MOMENTARILY CAME ON. RETURNED TO NORMAL OPERATION. FOUND THE NR 2 CTR TANK PUMP DID NOT AUTOMATICALLY TRANSFER FUEL. REPLACED THE FUEL LEVEL SENSING CONTROL UNIT 9QJ. ACCOMPLISHED A SATISFACTORY OPERATIOSDR 2016FA0000049Fuel Divider · defectiveIMMEDIATELY AFTER TAKEOFF FLIGHT CREW NOTED FLUID WHICH SMELLED LIKE FUEL COMING OUT FROM THE ENGINE COWLING AREA AND WAS ON WINDSCREEN. FLIGHT CREW IMMEDIATELY DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ENGINE COMPARTMENT AND DISDR 2016FA0000028Line · leakingDURING ANNUAL INSPECTION, A FUEL ODOR WAS NOTED IN THE COCKPIT. INVESTIGATION FOUND THE ALUMINUM FUEL PRESSURE LINE HAS CORRODED THROUGH AT THE POINT WHERE A WIRE BUNDLE WAS ZIP TIED AGAINST THE FUEL PRESSURE LINE.SDR AALA201601139006Actuator · defectiveAIRCRAFT WAS NOT GNDED. FUEL TRIM LINE FAULT ECAM ON DESCENT. REPLACED TRIM TANK ISOLATION VLV ACTUATOR. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 28-27-52-000-802-A & 28-27-54-400-802-A.SDR CA160111012Seal · defective(CAN) FUEL MOTIVE LINE STRAINER, CHECK VALVE FOUND TO HAVE A SWOLLEN RUBBER SEAL WHICH PREVENTED THE FLAPPER FROM SEALING. SPRING UNABLE TO RETURN VALVE TO CLOSED POSITION.SDR UIEA2016011000007Pressure Switch · faultyLEFT AFT FUEL PUMP SWITCH DOES NOT ILLUMINATE WHEN SELECTED OFF. NO ASSOCIATED EICAS MSG. R & R FUEL PRESS SWITCH AT LT AFT BOOST PUMP IAW AMM 28-22-01. LEAK & OPERATIONS CHECKED OK.SDR ASAA2016010814690Actuator · failedDURING ENGINE NR 1 START THE SPAR VALVE CLOSED LIGHT REMAINED BRIGHT WHILE START LEVER WAS IN IDLE DETENT. AFTER STARTER CUTOUT ENGINE VALVE CLOSED LIGHT WENT BRIGHT THEN DIM. THE ENGINE SHUTDOWN AT THAT TIME. SPAR VALVE LIGHT REMAINS BRIGHT WITH THE START SDR UIEA2016010800006Indication Sys · malfunctionedDURING FUEL CROSS FEED, LT AFT FUEL PUMP PRESS LIGHT FAILED TO ILLUMINATE WITH PUMP SWITCH OFF. COULD NOT DUPLICATE ON GND. OPERATIONS CHECK FUEL BOOST LT AFT GOOD IAW AMM 28-22-03.SDR ASAA2016010714711Relay · failedWHILE ACCOMPLISHING T/C 78128006, THE LT CENTER TANK AUTO SHUTOFF FUNCTIONAL TEST FAILED. ACFT GROUNDED. R & R THE LT AUTO SHUTOFF RELAY, R936, REF WDM 28-23-11. OPS CK GOOD REF T/C 78128006.SDR 2016FA0000032Servo · malfunctionedTHIS ACFT ENTERED A PRACTICE AUTOROTATION OVER A RUNWAY. UPON ROLLING THE THROTTLE DOWN, THE ENGINE DIED. ACFT MADE AN OTHERWISE UNEVENTFUL FULL-DOWN AUTOROTATION. CLUTCH ACTUATOR WAS DISENGAGED AND ENGINE RESTARTED NORMALLY. PILOT WAS UNABLE TO GET ENGINESDR VNAA2016010300003Fuel Cap · detachedCREW REPORTED RT FUEL CAP DOOR OPENED IN FLIGHT AND FUEL CAP CAME OFF AFTER BANGING UP UNDERNEATH WING WHILE ATTACHED TO CHAIN. FUEL CAP SEPARATED FROM ACFT IN FLIGHT. MAINTENANCE INSPECTED, REPLACED FUEL/DEFUEL CAP AND PERFORMED CHECKS IAW AMM. ACFT RELEASEDSDR ASAA2015122614457Actuator · stiffON CLIMBOUT AT 10,000 FT, CROSSFEED IN TRANSIT LIGHT STARTED COMING ON AND OFF INTERMITTENTLY. CONTINUED TO DO SO IN CLIMB. RECYCLED CROSSFEED VALVE AS CENTER FUEL ALMOST GONE. LIGHT STOPPED FLASHING. ACFT GROUNDED. CURRENTLY SYSTEM WORKS BUT DURING COURSE SDR CA151229014Tube · chafed(CAN) MAINTENANCE WAS TROUBLESHOOTING A REPORTED FUEL SEEP FROM THE FUEL SHROUD DRAIN FOLLOWING AIRCRAFT REFUELING. WELDED REFUEL/DEFUEL TUBE ASSEMBLY P/N 72810012-001 WAS FOUND WITH A PIN HOLE CAUSED BY CHAFING OF THE WELDED REFUEL/DEFUEL TUBE ASSEMBLY WITH SDR AALA20151224006Module · faultyAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB CTR FUEL PRESS LOW LIGHT ILLUMINATED. CTR TANK PUMPS NOT FEEDING. R & R FWD & AFT CTR PUMP UFI & RAM MODULES IAW AMM 28-20-28. SEE ALSO AALA2015122000SDR AALA20151224005Module · faultyAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB CTR FUEL PRESS LOW LIGHT ILLUMINATED. CTR TANK PUMPS NOT FEEDING. R & R FWD & AFT CTR PUMP UFI & RAM MODULES IAW AMM 28-20-28. SEE ALSO AALA2015122000SDR AALA20151224004Ufi · faultyAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB CTR FUEL PRESS LOW LIGHT ILLUMINATED. CTR TANK PUMPS NOT FEEDING. R & R FWD & AFT CTR PUMP UFI & RAM MODULES IAW AMM 28-20-28. SEE ALSO AALA2015122000
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