JASC 2840
Service difficulty reports · 1,865
Reports filed under 2840 · Fuel Indicating 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 = '2840' 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 = '2840' 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 QXEA200700496Computer · failedDEN - RECEIVED A FUEL CHANNEL 1/2 FAIL CAUTION MESSAGE IN FLIGHT. RETURNED TO THE FIELD. MAINTENANCE REPLACED THE FUEL QUANTITY GAUGING COMPUTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR AMTA200700176Control Panel · malfunctionedRT AFT FUEL BOOST PUMP LOW PRESS LIGHT INOPERATIVE, RELAMP NO HELP. REMOVED AND REPLACED FUEL MANAGEMENT CONTROL PANEL IAW AMM 28-22-14-4, TEST OK. (K)SDR QXEA200700462Unknown · unknownDEN - ON TAXI OUT FOR FLIGHT 4327, RECEIVED A "XFLOW" CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENANCE CLEARED THE FAULTS IAW CRJ-700 SERVICE LETTER SL-28-007 REVISION C. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE, NO PARTS REPLACED.SDR P5CA0701515Unknown · unknownAT PUSHBACK OFF BLOCKS, RECEIVED STATUS MESSAGE FUEL OVRD 2 FWD. DEFER PER MEL 28-31-2.SDR 07FDEA00380Door · missingUPON LANDING INTO PWM DISCOVERED FUELING PANEL MISSING. FOUND PANEL ON RUNWAY. REPLACED R/COOLING AIR INLET FAIRING CTR SECTION ASSY IAW AMM 53-15-73-4.SDR QXEA200700122Bulb · burned outSEA FLIGHT NR 2224, "TANK 2 AUX PUMP" LIGHT BURNED OUT. MAINTENANCE RELAMPED TANK 2 AUX PUMP LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR CA070124001Computer · malfunctioned(CAN) JUST PRIOR TO TOP OF CLIMB, LEFT FUEL QUANTITY AND TOTAL FUEL QUANTITY STARTED TO REDUCE, FOLLOWED BY FUEL IMBALANCE MESSAGE. CREW ELECTED TO RETURN TO DEPARTURE AIRPORT. ON FINAL APPROACH FUEL INDICATIONS RETURNED TO NORMAL. FUEL SYSTEM INSPECTED, WITH SDR QXEA200700003Computer · malfunctionedELP - TAXI FOR FLIGHT 4017, RECEIVED A "X FLOW" PUMP CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENANCE REPLACED THE FUEL QUANTITY GAUGING COMPUTER AND THE PUMP CARTRIDGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR AMTA200600751Indication Sys · malfunctionedLT FUEL TANK AND TOTAL FUEL QTY IND INTERMITTENT EICAS MSG FUEL QTY IND DISPLAYED. DEFERRED IAW MEL 28-41-11, AUTH NR: D28DE29-1406. 07 JAN 07.SDR CA061220006Indicator · chafed(CAN) LT FUEL QUANTITY CAUTION LIGHT ILLUMINATES DURING DESCENT. FAULT CODE INDICATES PROBES NR 3 DEFECTIVE. PROBE NR 3 REPLACED AND FURTHER INVESTIGATION REVEALED THAT THE WIRING IN LT TANK FOUND CHAFING AT (2) PLACES (WS 116.0) ON TOP OF FUEL PILOT VALVE LISDR UPS06M48748Warning Light · illuminatedFUEL QTY/USED CHK ALERT ILLUMINATED ABOUT 1 HOUR INTO FLIGHT. RUN CHECKLIST AND ISOLATED PROBLEM FUEL LEAK IN TAIL 3500LB DISCREPANCY BETWEEN FUEL BURNED AND FUEL ONBOARD AT BEGINNING OF RUNNING CHECKLIST. REMOVED AND REPLACED TANK 2 RT SIDE COMPENSATOR IAW SDR COMA0670219Computer · malfunctionedFLIGHT 5440 - FUEL CHANNEL 1/2 CAUTION AND AUTO CROSSFLOW INHIBIT CAUTION MESSAGES. CENTER TANK AND TOTAL FUEL INDICATIONS BLANK. DECLARED EMERGENCY, RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. RESET NR 1 AND NR 2 FUEL COMPUTER.SDR 2006UALA02267Probe · unknownDIVERTED TO ANC DUE TO FUEL INBALANCE. FUEL IMBALANCE RIGHT 64 LEFT 60 AND LEFT TANK DECREASING AT HIGH RATE. LEFT TANK DOWN TO 11.8 RIGHT 54.3. ON DESCENT LEFT TANK STARTED GAINING FUEL AT HIGH RATE. ON MAINT PAGE 1, PROBE 1 SHOWING 2.0 ON LEFT TANK. RIGSDR MASA200602627Warning System · malfunctionedASH 2799 LAS. ABORTED TAKEOFF DUE TO X-FLOW CAUTION MSG ON GROUND AT TAKEOFF ROLL. SYSTEM WAS RESET AND FAULT WAS CLEARED, NO FURTHER ACTION WAS REQUIRED.SDR EIA2006376Indicator · fluctuatesINFLIGHT AFTER TAKEOFF, CREW CALLED AND REPORTED NR 2 MAIN FUEL QTY INDICATION FLUCTUATION, AIRCRAFT RETURN JFK. RESET CB REPLACED NR 2 FUEL GAUGE AND NR 2 DTCU, VERIFIED WITH STICKS.SDR COMA0660619Computer · malfunctionedFLIGHT 5455 - EN ROUTE CHS-CVG RECEIVED A FUEL IMBALANCE CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO CHS. NO FAULTS LOGGED IN REFUEL/DEFUEL COMPUTER, RESET REFUEL/DEFUEL COMPUTER, FUEL QTY INDICATION NORMAL.SDR COMA0670194Computer · malfunctionedFLIGHT 5146- FUEL CHANNEL 1 FAIL STATUS MESSAGE. LANDED WITHOUT INCIDENT AT IND IAW QRH PROCEDURE. RESET FUEL COMPUTER. NO FURTHER DEFECTS.SDR QXEA200602091Warning System · malfunctionedOKC - ON TAXI FOR FLIGHT 4188, RECEIVED A X-FLOW PUMP AMBER CAUTION MESSAGE FOLLOWED BY A AUTO XFLOW INHIBIT MESSAGE. RETURNED TO THE GATE. MAINTENANCE CLEARED THE STATUS MESSAGE IAW FIM TASK 28-13-00-810-A01. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SDR ASMF200608011Probe · failedACFT RETURNED, NON COMMANDED LEFT TURN -20 DEG COMPENSATION WING DOWN AILERON, DIFFERENCE OF 4000 LBS OF FUEL BETWEEN MAIN TANKS. MX FUEL READING: FUEL 21900 LBS W/ 9300 LBS LT TANK, 9300 LBS RT TANK & 3400 LBS CENTRAL TANK. ACFT TOWED, NEW READING: 8400 LBS SDR QXEA200602031Switch · unknownPDX FLIGHT 2125 FUELING ON LIGHT ILLUMINATED ON PUSHBACK. MAINTENANCE RESET SWITCH ON FUEL PANEL. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200621901Computer · failedIN FLIGHT, CREW GOT FUEL CHANNEL 1 FAIL AND RETURNED TO BNA. RAI FUEL SYSTEM COMPUTER, IAW AMM 28-41-21-400-801-A01, OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M)SDR PG9A110603Pressure Switch · no testPRESSURE SWITCH PRODUCED NO INDICATION DURING TESTING./ REPLACED WITH SERVICEABLE PART.SDR AMTA200600486Unknown · unknownNR 2 FUEL QTY INDICATOR FLUCTUATED +/- 300 LBS IN FLIGHT. SUMPED NR 2 FUEL TANK IAW MM. PERFORMED FIM. FQIS BITE CHECK. NO FAULTS NOTED. GROUND TEST PASSED. (K)SDR 2006FA0000868Switch · mismanufacturedAFTER ARRIVAL, FOUND FUEL LEAK NEAR IB END OF RT WING. INVESTIGATION SHOWED THE LOW LEVEL FUEL LIMIT SWITCH WAS NOT ASSEMBLED. THE FLOAT, PN L15F2, WAS NOT ATTACHED TO THE MOUNT ASSY PN 62266503. THIS ALLOWED FUEL TO LEAK FROM THE WING. SWITCH WAS ASSEMBLESDR DXTA200601454Warning Light · erraticAIRCRAFT ON ACTIVE, PUSHED FOR TAKEOFF POWER, GOT FUEL GAUGE ANNUN LIGHT. TAXIED OFF RESET LIGHTS AND TOOK ACTIVE AGAIN WITHOUT PROBLEMS.SDR QXEA200601293Computer · unknownPDX - ON FLIGHT 2503, RETURNED TO GATE. CROSSFLOW PUMP CAUTION MESSAGE ILLUMINATES WHEN MANUAL OVERRIDE IS SELECTED JUST PRIOR TO TAKEOFF. MAINTENANCE COULD NOT DUPLICATE PROBLEM. REMOVED AND REPLACED FUEL QUANTITY GAUGING COMPUTER FOR PRECAUTIONARY REASON.SDR DXTA200601369Warning Light · unknownAUX TRANSFER LIGHT ILLUMINATED, TAKE OFF ABORTED. ITEM IS UNDER INVESTIGATION.SDR AMTA200600285Warning Light · illuminatedNR 2 TANK FUEL QUANTITY INDICATION LIGHT COMPARTMENT IS TOO HIGH. VERIFIED FUEL LOAD BY USING FUEL QT INDICATION USING FUEL STICKS NO FAULT NOTED FUEL LOAD MATCH. (K)SDR TRAX200600129Warning Light · illuminatedAFTER 1 HR IN FLIGHT, AUTO XFLOW INHIBIT STATUS MSG CAME ON. ALSO, LOST RIGHT FUEL QUANTITY, INDICATION AND TOTAL FUEL QUANTITY (AN EMERGENCY WAS DECLARED).SDR AMTA200600280Indication Sys · fluctuatesNR 2 FUEL QTY FLUCTUATING BY AS MUCH AS 400 LBS DURING FLIGHT. PERFORMED FIM 28-41-810-814, PERFORMED FQIS BITE TEST, NR1 AND NR2 TANK READ 3800 AT THIS TIME AND BITE TEST SHOWS NO FAULT FOR NR2 TANK. SUMPED TANKS REF: 12-1-1-OO-3. NR 2 TANK QTY OK FOR SERVSDR QXEA200601007Warning Message · false activationSEA - ON FLIGHT 2453, RETURNED TO GATE, XFLOW PUMP CAUTION MESSAGE CAME ON AFTER AUTO OVERRIDE WAS SELECTED TO MANUAL. MAINTENANCE PULLED AND RESET FUEL SYSTEM CIRCUIT BREAKERS CB-1-M11 AND CB-2-U11. NO FURTHER CAUTION MESSAGES NOTED. OPERATIONAL CHECK NORMSDR AMTA200600279Fuel Tank · reads highRT MAIN FUEL TANK READ 400 LBS HIGH. FQIS TEST SHOWS NO FAULT FOR RT MAIN TANK. CHECK GOOD, C/W FIM 28-41-00-810. (K)SDR 2006FA0000460Gauge · fluctuatesPART HAS A DEAD SPOT IN ITS TRAVEL CAUSING FUEL GAUGE TO FLUCTUATE RAPIDLY BETWEEN FULL AND EMPTY ALSO CAUSES LOW FUEL WARNING LIGHT TO FLASH CONTINUOUSLY. (K)SDR 2006UALA00583Warning Light · illuminatedSTAB FUEL TRANSFER EICAS MSG. AIRCRAFT 8177 HAS NO HISTORY OF "FUEL STAB XFR" EICAS MESSAGE IN THE LAST 12 MONTHS. LAXMM RELEASED THE AIRCRAFT FOR SERVICE AS THEY FOUND NO MESSAGE DISPLAYED IN THE LOWER EICAS. REMOTE ELECTRONIC UNIT (REU) WAS ALSO REMOVED /SDR 06FDEA1140Computer · malfunctioned1.5 HR INTO FLT, FL320 RT CTR PUMP FAULT, QRH 0.5 HR LATER CTR TK QTY FAILED AT 2.3 W/SOME FEEDING FROM OUTERS. RT CENTER BOOST PUMP IN W/W GOOD POWER AT PUMP. NEED BOOST PUMP. REMOVED AND REPLACED CTR2 BOOST PUMP MFG 2052C23 S/N 6715. SUSPECT CTR TANK LOSDR 2006UALA00568Warning Light · illuminatedSTOPPED AT OMA DUE TO RT CENTER TANK LOW PRESSURE LIGHT ILLUMINATED. TRANSFERRED FUEL INTO CENTER FUEL TANK. RIGHT CENTER TANK FUEL BOOST PUMP LIGHT WORKED OK.SDR COMA0570132Warning System · false activationFLIGHT 5276 - RT ENGINE LOW FUEL PRESSURE CAUTION. RESET SYSTEM, OPERATIONAL CHECK SATISFACTORY.SDR QXEA200600130Probe · malfunctionedPDX - DURING CLIMB-OUT LEFT TANK GRADUALLY INDICATED LOWER FUEL LOW FUEL WARNING AND FUEL IMBALANCE FOLLOWED. CENTER TANK NOTED AT 140 LBS AND THEN 200 LBS LEFT TANK THEN WENT DASHES. AUTO PILOT WAS DISCONNECTED AND NO IMBALANCE WAS NOTED. RETURNED TO THE FSDR KBM2006F00003Switch · inoperativeFUEL PRESSURE INDICATOR LIGHT, ILLUMINATED. DURING FLIGHT, REMOVED AND REPLACED. (K)SDR KBM2006F00020Gauge · sticksFUEL GAUGE STICKS AND READS INCORRECT, REMOVED AND REPLACED. (K)SDR 2006FA0000020Conduit · leakingLT NACELLE TANK SENDER WAS LEAKING OUT OF TOP OF NACELLE. SENDER SCREWS HAD BEEN TIGHTENED AND GASKETS REPLACED BUT STILL LEAKED. TECH FOUND ALUMINUM CONDUIT THAT SENDER WIRING IS ROUTED THROUGH IN TANK TO HAVE APPROX 10-15 PINHOLES IN IT FROM CORRODING FROM TSDR DHL2005362010Amplifier · malfunctionedFUEL ON GAGES AND TOTALIZER APPEARED TO BE GOING AT AN EXTREME RATE. EMERGENCY DECLARED AND LANDING MADE AT PHL. FUEL QTY WENT DOWN 9000 LBA IN ABOUT 30 MIN. REPLACED F/Q AMP OPS CHECK OK PER MM 28-42-00. RAN ENGS 1/2 PER JRH 16.5. NO DEFECTS NOTED. ADDISDR AU510001925Indication Sys · faulty(AUS) NO1 ENGINE SHUT DOWN DUE TO FUEL STARVATION. INVESTIGATION FOUND THE FUEL GAUGE INDICATION WAS 400LBS FUEL QUANTITY LHS AND 250LBS FUEL QUANTITY RHS. THE MAGNETIC STICKS SHOWED NIL LHS AND NIL RHS. ACTUAL FUEL EMPTIED FROM TANKS INTO CONTAINERS AT WAS 2 SDR SIM2006F00004Computer · failedNOTIFIED BY DISPATCH, AIRCRAFT DIVERSION, DUE TO FUEL CHANNEL 1 FAIL EICAS MESSAGE. CREW FOLLOWED AOM PROCEDURES AND LANDED. RAI FQGC OPS CHECK GOOD. (K)SDR CHQA200500199Fuel Heater · inoperativeFLIGHT 3002 - PIT-BWI - WHILE IN CRUISE FLIGHT AT FL230, THE FUEL IMBALANCE LIGHT APPEARED AND THE LEFT FUEL TANK INDICATED 0 POUNDS. COMPLETED QRH CHECKLIST FOR FUEL IMBALANCE, DECLARED AN EMERGENCY WITH ATC. LANDED IN BWI WITHOUT INCIDENT. REMOVED AND REPSDR HNAA050099Indicator · malfunctionedNR 2 FUEL GAUGE INDICATES DOUBLE THE FUEL BURN NR 2 FUEL GAUGE, OPS NORMAL DURING FERRY FLT. REFUELED IN LGA. MAGNA STICKED NR 2 TANK AND NR 2 FUEL GAUGE MATCHES MAGNA STICK READING. GAUGE OPS NORMAL AT THIS TIME.SDR S2YA05067Pressure Switch · inoperativeDURING FLIGHT, THE CREW REPORTED THE RT AUX PUMP AUTO FUNCTION DID NOT STOP THE PUMP, RT NO AUX TRANSFER ILLUMINATED WHEN PUMP WAS IN AUTO FUNCTION. BETWEEN MX AND OPS, IT WAS DECIDED AN AIR-TURN-BACK WAS THE BEST OPTION. MX INSPECTED THE SYSTEM BUT COULD NOSDR QXEA200501354Bulb · burned outNR 2 TANK AUX PUMP LIGHT BURNED OUT. SPOILER OUTBD CAUTION LIGHT COMES ON AT 185-190 KTS. MAINTENANCE REMOVED AND REPLACED FCECU AND PERFORMED APPLICABLE OPS TESTS AND FUNCTIONAL TESTS. NO DEFECTS NOTED. REMOVED AND REPLACED NR 2 SPOILER UNLOAD VALVE. PERSDR AU510002127Totalizer · faultyFUEL INDICATING SYSTEM COMBINED PROCESSOR TOTALIZER UNIT (CPT) FAULTY.SDR 2005UALA01125Computer · malfunctionedRETURN TO FIELD DUE TO A FUEL QUANTITY ISSUE. OPERATED BOTH ENGINES TO OBSERVE ENGINE FUEL BURN AND THE POSSIBILITY OF FUEL LEAKS. VISUALLY CHECKED MFLI (MAGNETIC FUEL LEVEL INDICATORS) FOR VERIFICATION OF FUEL QUANTITY INDICATIONS. ALSO, FQIC (FUEL QUANTIT
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