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 UIEA2017070201090Switch · inoperativeRT ENGINE FUEL VALVE LIGHT INOPERATIVE. REPLACED THE FUEL VALVE SWITCH IAW AMM 33-13-00, OPS NORMAL.SDR CALA2017062601990Shutoff Valve · faultyUNWANTED FUEL TRANSFER FROM THE CENTER TANK TO THE LEFT, LEFT TANK INCREASES WITH THE CTR PUMPS ON. WHEN CENTER PUMPS OFF THE LEFT TANK QTY DECREASES AND THE CENTER TANK INCREASES. IAW FIM28-220-00-810-849: REPLACED LT TANK OUTLET FLOAT OPERATED SOV IAW AMM28-SDR UIEA2017061201000Warning Light · false activationAFTER 30 MINUTES OF FLIGHT, THE RT FWD FUEL PRESSURE MESSAGE ILLUMINATED AND THE PRESSURE LIGHT IN BOTTON. TEST FLIGHT. PERFORMED TROUBLESHOOTING IAW FIM 28-22, FT819 FOUND K107 , AND THE RT FWD RELAY OPEN AND PERFORMED A RESET. PERFORMED FIM FIG 119 FT 83SDR 2017FA0000322Filter · leakingDURING THE ENGINE PERIODIC INSPECTION THE FUEL FILTER PN 3033355 WAS INSPECTED AND REINSTALLED USING A NEW O-RING PN M25988/1-928 IAW MAINTENANCE MANUAL 731002, -TECH PUMP WHICH STATES TORQUE TO BE 30 TO 50 INCH POUNDS TORQUE TO THE FILTER BOWL. THE LEAK CHECSDR HALA2017060500136Gasket · tornETOPS SIGNIFICANT SYSTEM - FUEL DISAGREE - PROG2 DISPLAYED ON CDU SCRATCHPAD WITH TOTALIZATOR FUEL DIFFERENTIAL - 4.2 BELOW CALCULATED. AFTER LANDING FA'S REPORTED STRONG FUEL ODOR IN REAR CABIN.// REMOVED BYPASS & INLET MANIFOLD FROM #2 ENG FUEL PUMP & MEC. FSDR FDEA201703291000Fuel Sys · leakingLEFT WING INBOARD DRY BAY CENTER FORWARD DRAIN HAS A RUNNING FUEL LEAK.SDR CALA2017031700600Warning Message · false activationWITH RIGHT CENTER BOOST PUMP ON, RECEIVED A FUEL IMBALANCE ON NR 1 INDICATOR. CROSSFEED WAS CLOSED. EMERGENCY DECLARED. ACCOMPLISHED FIM TASK 28-21-00-810-815. NO FUEL TRANSFER NOTED, CROSSFEED VALVE AND BOOST PUMPS OP CHECKED GOOD.SDR AALA20161213021Pump · faultyDURING FIRST HOUR OF FLIGHT WITH CENTER PUMPS ON, CREW OBSERVED 700 POUNDS FUEL BURN FROM RIGHT MAIN TANK. REMOVED AND REPLACED CENTER FUEL TANK RIGHT FUEL BOOST PUMP IAW AMM 28-22-41. LEAK AND OPERATIONAL CHECK GOOD.SDR R61A201611130652Warning Light · false activationDURING FLIGHT, CREW RECEIVED AN SPDA FAIL AND A FUEL FEED 1 FAULT ADVISORY MESSAGE. CREW RAN QRH AND NOTED THAT THE PACKS WERE OFF THE BLEED VALVE CLOSED. CABIN PRESSURE CONTINUED TO RISE, CREW DONNED OXYGEN MASKS AND PERFORMED EMERGENCY DESCENT. DIVERTED AND SDR QMLA2016100716116Warning Light · illuminatedPILOT REPORTED THAT THE FUEL LOW PRESSURE LIGHT ILLUMINATED IN FLIGHTSDR VNAA2016100300005Computer · faultyINFLIGHT AUTO CROSSFLOW INHIBIT STATUS MESSAGE APPEARED FOLLOWED BY FUEL CHANNEL 1 FAIL, LEFT FUEL QUANTITY GAUGE FAILED, THEN TOTAL FUEL QUANTITY FAIL. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESSDR ASMF201610007Actuator · leakingDURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED IN THE RIGHT ENGINE. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING FUEL LEAK IN THE TRANSIENT BLEED VALVE DRAIN PORT. THE RIGHT ENGINE WAS MOTORING, AFTER IT WAS STARTED AND ENGINE OPERATIONAL TEST WAS PERFOSDR HALA2016080900323Fuel Sys · malfunctionedFUEL IMBALANCE ABOUT 1000 LBS AN HOUR. NO STATIC TRANSFER BETWEEN LEFT & RIGHT MAIN TANKS. WITH LEFT & RIGHT FUEL PUMPS ON NO FUEL TRANSFER BETWEEN TANKS. PRESSURIZED ENGINE PRESSURE FEED MANIFOLD WITH LEFT PUMPS AND OPENED RIGHT DEFUEL VALVE. NO FUEL TRANSSDR ASAA2016071617390Fuel Sys · fluctuatesFUEL FLUCTUATIONS UP TO 800 LBS BETWEEN MAIN TANK 1 & 2 WERE OBSERVED AFTER THE CENTER TANK FUEL WAS EXHAUSTED. TOTALIZER ALSO FLUCTUATED IN CONJUNCTION WITH THE MAIN TANK FLUCTUATIONS. YOKE DID NOT DEFLECT, INDICATING NO IMBALANCE. FLUCTUATIONS WERE QUICK CYSDR ASOA20160715035Unknown · leakingPAX REPORTED A FOOT WIDE STREAM OF FUEL COMING FROM RT WING FROM THE TAKEOFF TO 3-5 MINUTES AFTER DEPARTURE. MX PERFORMED GVI OF RT WING NO SIGNS OF FUEL LEAK. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR RJEF201605300001Warning Message · false activationDURING TAKEOFF OF THE ACFT, THE EICAS MSG, FUEL LOW PRESS, WAS DISPLAYED. THEREFORE, A REJECT TAKEOFF PROCEDURE WAS PERFORMED. ONCE THE ACFT WAS AT THE GATE, THE DEFUEL SOV, PREVIOUSLY DEFERRED, WAS INSPECTED TO ASSURE ITS CLOSED POSITION. THE ACFT WAS RETUSDR ASAA2016041116347Fuel Tank · contaminatedAT FL360 WITH LESS THAN 22000 POUNDS FUEL ONBOARD, THE NR 2 MAIN TANK FUEL DECREASE FROM 8.55 TO 7.33. THE IMBALANCE LIGHT ILLUMINATED WITH CENTER TANK PUMPS STILL IN USE THE NR 2 MAIN TANK FUEL GAUGE FLUCTUATED BETWEEN 8.3 & 7.3, MOSTLY STAYED AT 7.3 AFTER CESDR DALA2016032402278Probe · wornWEAR ON FUEL ACCESS PROBES 1460C, 1466C, 1373C. PROBES WERE REPLACED IAW AMM 28-40-02 AND EA 09-2122-14, REV B.SDR QMLA201602216009Drain Valve · failedAFTER TAKEOFF, NURSE IN THE BACK THOUGHT SHE SMELLED FUEL FUMES. LANDED AT NEAREST AVAILABLE SITE, AIRPORT, WITHOUT FURTHER INCIDENT..SDR ASAA2016021115425Unknown · unknown600 LBS OVERBURN, LT FUEL REMAIN A.09 RT, 3.38. FUEL USED 4.7, 4.7, FUEL FLOW WITHIN 20LBS/HR. ACFT GROUNDED. USING ALTERNATE FUELING MANUAL CONFIRMED THAT GAUGES AND FUEL STICKS ARE IN SYNC WITH ONE ANOTHER. FUEL QTY IN TANK AT 5950 LBS, FUEL STICK NR 4 RESDR QXEA2016012800070Unknown · leakingBEFORE START, DURING WALKAROUND ON RAMP, NOTICED FUEL DRIPPING FROM APU DRAIN. PERFORMED OPS TEST IAW AMM 49-00-00-710-801. NO DEFECTS OR LEAKS. RETURNED TO SERVICE.SDR ASAA2015112813970Fuel Sys · unknownWHILE BURNING OUT OF CENTER TANK, STARTED NOTICING SLOW DECREASE IN NR 2 MAIN TANK QTY FUEL MONITORING INDICATED LOSS OF 1300 LBS BETWEEN 2 WAYPOINTS 1.5 THIS CORRESPONDS WITH WHAT WE SAW ON THE NR 2 FUEL GAUGE DECISION WAS MADE TO RETURN TO DEPARTURE, BY THE SDR COZA20151119065Panel · stuckWHILE PERFORMING CENTER FUEL TANK AUTO SHUTOFF TEST, FOUND RT CENTER FUEL TANK TEST SWITCH STICKING. REPLACED FUEL TEST PANEL P61-8 AND OPS TEST NORMAL.SDR CA151013004Fuel Sys · contaminated(CAN) ON ARRIVAL AT THE PLATFORM, WHILE DESCENDING FROM THE HOVER ONTO THE DECK, THE NR 2 FUEL BYPASS CAUTION CAME ON. ONCE ON THE DECK, APPROXIMATELY 7 SECONDS LATER, NR 1 FUEL BYPASS CAUTION ALSO CAME ON. FOLLOWING SHUTDOWN AND DISCUSSION WITH MAINTENANCE SDR A6WA201543065Unknown · malfunctionedAPPEARS FUEL IS LEAKING FROM RT TANK TO CTR TANK. GAINED 250 LBS OF FUEL IN CTR TANK IN CRUISE FLIGHT. NOTED FUEL QUANTITIES & DEPOWERED ACFT FOR 35 MINUTES. ON REPOWER, NOTED FUEL QUANTITIES, NO SIGNIFICANT CHANGE. VERIFIED NO STATIC LEAKS BETWEEN TANKS. SDR R61A201508050515Warning Message · false activationTHE CREW REPORTED THAT THEY RECEIVED A FUEL FEED 1 FAULT ADVISORY MESSAGE DURING CRUISE FLIGHT. THE CREW FOLLOWED THE QRH AND RECEIVED AN ENGINE FUEL LOW PRESSURE CAUTION MESSAGE ON THE EICAS ON DESCENT. THE CREW DECLARED AN EMERGENCY. THE ACFT LANDED AT ITSSDR CA150612005Drain · wrong part(CAN) OWNER ASK TO HAVE A FUEL LEAK REPAIRED AND COMPLAINED THAT FUEL DRAINING WAS VERY SLOW. AFTER DRAINING TANKS IT WAS NOTED THAT AN UNAPPROVED REPAIR HAD BEEN UNDERTAKEN AND THE SEALANT APPLIED COVERED THE DRAIN CHANNEL TO THE QUICK DRAIN. IN ORDER FOR FUESDR ASAA2015061012057Fuel Sys · malfunctionedINITIALLY SHOWED A NR 800 LB DIFFERENCE IN FUEL QUANTITY BETWEEN THE FUEL TOTALIZER AND THE FMC FUEL QUANTITY. THE LT, RT, AND CENTER QUANTITY ADDED UP TO EQUAL THE FUEL TOTALIZER QUANTITY OF 18.4. HOWEVER THE FMC ACTUAL FUEL SHOWED 17.6. ACFT GROUNDED. CYCSDR HALA2015052400093Fuel Sys · malfunctionedFUEL IMBALANCE IN FLIGHT, FUEL MIGRATING. REPAIR IN WORK.SDR CWQR2015F00067Pump · chafedUPON OPENING SEVERAL WING TANK PANELS, MECHANIC NOTICED CHAFING DAMAGE TO EJECTOR PUMP. UPON FURTHER INVESTIGATION, FOUND NUMEROUS LINES AND FITTING ASSOCIATED WITH THE FUEL EJECTOR PUMP TO ALSO BE CHAFING. REPLACED.SDR UHLA2015041300248Warning Light · false activationE1 FUEL LOW PRESSURE AND E1 FUEL FEED FAULT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED ENGINE FEED EJECTOR PUMP OPS CHECK IAW FIM, OPS CHECK GOOD.SDR SWAA2015022536912Actuator · faultedFUEL CROSSFEED CIRCUIT BREAKER TRIPPED IN FLIGHT. R & R ACTUATOR IAW MM.SDR ASAA2014120809898Unknown · unknownFUEL TANKS DEVELOPED 600 LB IMBALANCE AFTER BEING BALANCED. ENGINE USE WAS NEAR EQUAL BOTH SIDES AT 6.28 & 6.30, RESPECTIVELY. ACFT GROUNDED. VERIFIED ON ACFT ARRIVAL TANKS READ -NR 1, 4.40 & NR 2, 3.83. PERFORMED PORTION OF FIM 28-41, TASK 820 FQIS BITE PROSDR UIEA2014121800651Warning Message · false activationDURING CRUISE, FUEL CONFIGURATION, EICAS MESSAGE CAME ON TWICE DUE TO FUEL IMBALANCE. CORRECTED BUT RETURNED. LT TANK WOULD GO LOW & RT TANK HIGH. WHEN CTR TANK EMPTY FUEL IMBALANCE DISCONTINUED. APPEARS CENTER TANK PUMP DOES NOT OVERRIDE FWD & AFT LT PUMPSDR SWAA2014071830094Module · faultyODOR IN COCKPIT ON DECENT. R & R P5 2 FUEL OVERHEAD MODULE IAW MM.SDR ASAA2014071708595Unknown · unknownAS CENTER TANK FUEL APPROACH 100 LBS, FELT & HEARD VIBRATION ON FLIGHT DECK AS IF A PUMP CAVITATING. LT CENTER TANK FUEL LOW LIGHT CAME ON. TURNED LT CENTER FUEL PUMP OFF, VIBRATION CEASED. RIGHT CENTER PUMP NORMAL OPERATION NO VIBRATION. LT & RT FUEL FLOWSSDR V0XD2014062192729Tank · crackedFUEL PROBE HAS CRACKED HOUSING. R & R TANK UNITSSDR DXTA2014050205751Valve · failedEN ROUTE AT FL250, RECEIVED A RT WING TANK OVER FILL EICAS MESSAGE. VISUALLY CONFIRMED VENTING FUEL. ACCOMPLISHED CHECKLIST & VENTING STOPPED. REMOVED FUEL BAY ACCESS PANELS TO O/B VENT FLOAT VALVE AND CLIMB VENT PLUMBING. FOUND O/B VENT FLOAT VALVE DAMAGEDSDR PRIA2014F00072Unknown · unknownAIRCRAFT DEPARTED, ENROUTE, AT 25 MINUTES INTO FLIGHT AND AT FL450 PIC NOTICED A 1500LB FUEL IMBALANCE WITH THE LT SIDE READING LOW. FUEL QUANTITY ON LT SIDE CONTINUED TO DECREASE ON BOTH THE PRIMARY AND STANDBY INDICATIONS. IT WAS AT THIS TIME THE PIC SUSPESDR QMLA2014012014008Unknown · leakingTHE PILOT HAD JUST LIFTED OFF FROM BASE WITH A MEDICAL CREW ONBOARD FOR A SCENE CALL. A FEW MINUTES INTO FLIGHT THE MEDICAL CREW NOTED A STRONG FUEL ODOR CONSUMING THE CABIN. THE PILOT IMMEDIATELY ABORTED THE MISSION & RETURNED TO BASE. TROUBLE SHOT FUEL LESDR CALA2013122693912Unknown · malfunctionedIN UNDER 2 HR FUEL IN LT TANK UP BY 1500 LBS. IAW FUEL IMBALANCE, FUEL EVEN USING CTR PUMPS. 1:50 AFTER TANK TO ENG LT TANK 1500 LBS ABOVE RT. LT ENG BURN 100 PPH MORE THAN RT ENG IAW SEQ 4502010, 4502009, 4502007 & 4502002. COMPLETED FUEL TRANSFERS WAS UNASDR CA131202019Relay · failed(CAN) DURING FLIGHT, CREW EXPERIENCED TRIPPING OF SEVERAL FUEL BOOST PUMP CIRCUIT BREAKERS. CREW DIVERTED TO THE NEAREST SUITABLE AIRPORT WHERE MAINTENANCE REPLACED THE GFI RELAYS FOR THE BOOST PUMPS THAT HAD THEIR C/B`S TRIP, ALL ELECTRICAL CONNECTOR`S TO TSDR R61A201310261113Tube · crackedDURING HEAVY CHECK, FOUND NACA VENT TUBE CRACKED UNDER ACCESS PANEL 524FT ON FWD INBD WELD LINE. MX REMOVED AND WELDED IAW ER DHC-8-400-57-L02378, PN 85711207-001.SDR DALA1615980177Actuator · not reportedACTUATOR INSPECTED AND REPLACED 2820-01243.SDR CA130916001Nut · missing(CAN) ENGINE MFG HAS COME ACROSS 1 UNAPPROVED PART OF MS9198-06 WHICH WAS INSTALLED ON A HIGHER LEVEL ASSY, PN 3073363-01, FUEL PRESSURE TUBE WHERE THE MS PART IS MISSING THE HOLE REQUIRED FOR THE SAFETY WIRE. ENGINE MFG IS CURRENTLY INSPECTING THE REST OF TSDR CALA2013091891272Unknown · malfunctionedCENTER PUMP SHOWS RUNNING WITH THE FUEL PANEL CLOSED.SDR SAJF201311102028Float Valve · obstructedAIRCRAFT GND TURN BACK DUE TO FUEL LEAK FROM RT WING SURGE TANK VENT PORT. THE FLOATING VLV IN MAIN TANK FAILED TO CLOSE, RESULTING FUEL OVERFLOW TO SURGE TANK THROUGH VENTING SYS & SPILL OUT FROM SURGE TANK VENT PORT. APPLIED MEL 28-15-02-02C TO DEACTIVATE SDR CALA2013082390696Switch · inoperativeFUEL MAIN TANK 1 AFT SWITCH LIGHT IN COCKPIT OVERHEAD WILL NOT ILLUMINATE. REPLACED NR 1 AFT MAIN TANK PRESSURE SWITCH IAW AMM. LEAK AND OPS CK OK.SDR CALA2013082290655Unknown · malfunctionedCENTER FUEL SLOWLY GAINS FUEL TO 300 LBS WITH PUMPS OFF. ACP FUEL SCAVENGE SYSTEM FUNCTION TEST PER AMM. NEED 24K ON EACH MAIN TANK & 1K-13200 ON CENTER TANK TO COMPLETE TEST. DURING TEST ITEM 'E' PG 525, ITEM E(3B), LEFT MAIN TANK HAD NO INCREASE OF FUEL WHISDR UALA2013070204613Relay · failedACFT WILL NOT TAKE FUEL. REPLACED RELAYS 181, 180, 186, 186, 46, 45, 184, 183. OPENED FUELING VALVES BY HAND TO PUT FUEL ON. NOW THE 6 FUELING VALVES WILL NOT OPEN. REPLACED RELAY K180. OPS CHECKED NORMAL.
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