JASC 2840
Service difficulty reports · 1,864
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 UIEA2018081901743Warning System · false activationLT CTR FUEL PUMP MSG FLIGHT ON DESCENT. PERFORMED OPERATIONAL TEST OF THE ENGINE FUEL FEED SYSTEM IAW AMM 28-22-00. OPS CHECKS GOOD. NO DEFECTS NOTED AT THIS TIME.SDR ASAA201808205854Warning Message · false activationFUEL CLASS II MESSAGE. ACFT GROUNDED. RESET FQIC 1 & 2. OPS CHECKED GOOD IAW AMM 28-42-00-710-001.SDR UIEA2018081601706Warning System · activatedRIGHT AFT FUEL PUMP CAUTION MESSAGE ON GROUND. TRANSFERRED TO MEL 28-22-01 MDDR 98078 CAT "C".SDR 2020F00031Warning Message · activatedFUEL IMBALANCE MSG DISPLAY IN FLIGHT (MAX IMBALANCE L TANK 15.0/R TANK 5.1).SDR UIEA2018081301684Not Reported · malfunctionedMAIN TANK IN FLIGHT FUEL IMBALANCE OF 1200LBS (LEFT LOW/RIGHT HIGH). BITE TEST OF M-121 FUEL QTY PROCESSOR SHOWS NO FAULTS FUEL CONFIG LIGHT DID NOT ILLUMINATE AND NO ASSOCIATED EICAS MSG IN VIEW SUSPECT 1200LB APU FUEL BURN DUE TO 4 PLUS HOUR DELAY INBD. NOTESDR UIEA2018081301682Status Message · false activationFUEL QTY CHANNEL STATUS MESAGE AT FL 36.0 + 1559Z. PERFORMED FQIS BITE TEST IAW AMM 28-41-00. BOTH CHANNEL BITE CHECK GOOD, NO DEFECTS NOTED.SDR ASAA2018081425765Indicator · intermittentLEFT MAIN TANK REFUEL PANEL QUANTITY INDICATOR WAS INTERMITTENT. ACFT GROUNDED. REPLACED THE FUEL PANEL NR 1 INDICATOR IAW AMM 28-41-61.SDR AALA201808089017Pressure Switch · defectiveLEFT TANK PUMP 2 LOW PRESSURE, ECAM MESSAGE OCCURRED TWICE DURING FLIGHT. THE AIRCRAFT WAS GROUNDED. REPLACED LEFT FUEL PUMP NR 2 PRESSURE SWITCH (15QA). OPS GOOD.SDR ASAA2018080645659Indicator · unknownINDICATOR FOR FUEL CENTER TANK FLUCTUATES FROM 0.00 TO 0.09 WHEN EMPTY. ACFT GROUNDED. COMPLIED WITH FIM 28-41, TASK 814 AND 28-41, TASK 801. NO CURRENT FAULTS, NO FAULT HISTORY. PERFORMED FQIS GROUND TEST. TESTED PASSED. FUEL QUANTITY IS CORRECT IN FLIGHT DSDR BKEA201808060401Indicator · unknownAPPROXIMATELY 25 MINUTES INTO FLIGHT, AFTER LEAVING WITH 11,700 LBS OF FUEL, GAUGES READ 3280, 3360, AND 1220. ONE HOUR 45 MINUTES INTO FLIGHT, GAUGES READ, 2240, 2360, AND130 AMBER. NR 3 EVENTUALLY WENT TO ZERO. AFTER 10 MINUTES AT ZERO, NR 3 LOW PRESSURSDR UIEA2018072501549Unknown · malfunctionedLEFT ENG SPAR VALVE LIGHT DID NOT ILLUMINATE ON LEFT ENG START, BACK TO BLOCKS. TRANSFERRED TO MEL 28-40-02 CAT C , DUE DATE 04AUG18.SDR HALA2018072500403Warning System · false activationETOPS SIGNIFICANT SYSTEM, ECAM: FUEL APU AFT PUMP FAULT. T/S PER TSM 28-22-00. TEST OK. NO FUEL APU AFT PUMP FAULT
AT TIME.SDR UIEA2018071901518Light · inoperativeRIGHT SPAR VALVE LIGHT DID NOT CYCLE WHILE STARTING THE RIGHT ENGINE. REPLACED RT SPAR VALVE LIGHT ASSY AS PER SWPM 20-84-18, OPS CHECK GOOD AT THIS TIME.SDR FDEA201807141713None · noneTANK 3 TIP TRAPPED & TNK 3 FUEL QTY LO ALERT AT CRUISE FUEL QTY- 21.0K, QRH COMPLIED WITH. ELECTED TO PUT FUEL
SYSTEM MANUAL AND TRANSFER FUEL FROM TANK NR 2. ALERT WENT AWAY. FUEL SYSTEM BACK TO AUTO. ALERTS RETURN
DURING ARRIVAL AND APPROACH. FUEL QTY 16K.SDR SIMA201807132003Unknown · malfunctionedFUEL QUANTITY INDICATION ON BOTH ENGINES AND TOTAL FUEL INDICATED INCREASED AND DECREASED UP TO 900 POUNDS. THE FUEL IMBALANCE MESSAGE APPEARED AND DISAPPEARED MULTIPLE TIMES DURING FLIGHT. PERFORMED FUEL BALANCE (WING TRANSFER) IAW AMM 28-10-00. NO FURTHER IMSDR UIEA2018071201443Warning System · false activationRT FWD FUEL PUMP EICAS MESSAGE DISPLAYED FOR APPROX 60 SECONDS DURING INITIAL CLIMB. OPS CK FUEL SYSTEM IAW AMM 28-21-00. OPS GOOD.SDR UIEA2018070901386Warning System · false activationCTR RT FUEL PUMP EICAS MESSAGE ON TAKE OFF ROLL. REJECTED T/O. TRANSFERRED FUEL TO WINGS IAW AMM 28-26-00 ACCOMPLISHED. OPS CHECK ON CENTER PUMP IAW AMM 28-22-00 OPS CHECK GOOD AT THIS TIME.SDR UIEA2018070901391Warning System · false activationRT FWD FUEL PUMP EICAS FOR SEVERAL MINUTES AFTER TAKE OFF. PERFORMED OPS CHECK ON RIGHT FWD FUEL BOOST PUMP IAW FIM 28-22 FT 820, NO FAULT FOUND AT THIS TIME.SDR UIEA2018070601361Warning System · false activationRT FWD FUEL PUMP EICAS MSG FOR SEVERAL MINUTES AFTER TAKE OFF. PERFORMED OPS CHECK ON RIGHT FWD FUEL BOOST PUMP PER FIM 28-22, FAULT TREE 820. NO FAULTS FOUND AT THIS TIME.SDR UIEA2018070601351Warning System · false activationRIGHT FUEL SPAR VALVE EICAS MESSAGE IN FLIGHT. ACCOMPLISHED BY RIGHT SPAR VALVE LIGHT. PERFORMED OPS CHECK IAW AMM 28-22-11 PARA I, RUN ENGINE IAW 71-00-00. OPS CHECK NORMAL AT THIS TIME.SDR UIEA2018070301323Warning System · activatedON START OF RIGHT ENG- NO SPAR VALVE "LIGHT". DISPATCH NOTIFIED.SDR ASAA2018062625206Tank Unit · failedACCOMPLISHED T/C NG-28FCD-18090-1 FOR NR 2 TANK AND FOUND TANK UNIT 1, 2, AND 3 OUT OF LIMITS PER AMM 28-41-21-710-801. GROUNDED - YES. REF T/C NG-28FCD-18090-1. REMOVED AND REPLACED TANK UNIT NR 1, TANK UNIT NR 2 AND TANK UNIT NR 3 REF AMM 28-41-21-400-801. ASDR ASAA2018061875074Indicator · failedCENTER TANK GAUGE ON REFUEL PANEL DOES NOT INDICATE CORRECTLY. ACFT GROUNDED. REMOVED AND REPLACED THE CENTER REFUEL QUANTITY INDICATOR, OPS CHECKED GOOD IAW AMM 28-41-61.SDR ASAA2018060874963Probe · no testNR 1 MAIN TANK FQIS FAILED A SYSTEM TEST IAW AMM 28-41-00-730-801, & NG-28FCD-18088-1. ACFT GROUNDED. THE NR 2 TANK UNIT AND NR 9 TANK UNIT WERE OUT OF LIMITS. REPLACED IAW AMM 28-41-21/401. TANK AND COMPENSATOR UNITS TESTED FOR THE NR 1 TANK PASSED IAW AMM SDR ASAA2018060864962Probe · no testNR 2 MAIN TANK FUEL QUANTITY INDICATING SYSTEM FAILED A SYSTEM TEST IAW AMM 28-41-00-730-801. ACFT GROUNDED. REMOVED AND REPLACED THE FUEL QUANTITY PROBES NR F8 & F9 IAW AMM 28-41-21-400-801. ACCOMPLISHED FQIS SYSTEM TEST IAW AMM 28-41-00-730-801. OPS CHECKSDR AALA201806073005Probe · inaccurateDIVERTED DUE TO A FUEL IMBALANCE OF 3500 POUNDS. AN EMERGENCY DECLARED. THE AIRCRAFT LANDED WITHOUT INCIDENT AND REMOVED FROM SERVICE. DETERMINED THAT THE RIGHT FUEL QUANTITY WAS INCORRECT. PERFORMED FIM 28-41-00-810-814, NO FAULTS NOTED. TEST PASSED. FQIS SDR CA180616005Probe · false indication(CAN) FALSE INDICATION OF AMOUNT OF FUEL ATA 28-00. (TC# 20180616005)SDR HALA2018053000265Warning System · false activationETOPS SIGNIFICANT SYSTEM - FUEL L+R CTR PUMPS LO PR ECAM MESSAGE APPEARED FOR 30 SECONDS DURING FLIGHT. PERFORMED FCMC1 AND 2 BITE, NO FAULT NOTED AND PRESSURE SWITCHES FUNCTION GOOD PER TSM 28-21-00. NO 30 DAYS HISTORY, OK FOR SVC.SDR AALA201805296005Module · malfunctionedEMERGENCY DECLARED, DUE TO FUEL IMBALANCE. AIRCRAFT WAS GROUNDED, ACCOMPLISHED FUEL IMBALANCE MCM CARD 28-96-01. REPLACED SEM UNIT IAW MM 28-40-05, OPERATIONS CHECKED NORMAL.SDR ASAA2018052184712Indicator · malfunctionedHORIZONTAL AMBER LINES SHOWING ACROSS FUEL USED INDICATION NUMBERS. ACFT GROUNDED. PERFORMED AN ENGINE RUN ON ENGINES 1 & 2 IAW TSM 28-42-00-810-883-A. FAULTS CLEARED, NO FURTHER DEFECTS NOTED AT THIS TIME. ACFT OK FOR SERVICE.SDR FXTA201804100154Pressure Switch · failedLOW FUEL PRESSURE LIGHT CAME ON DURING START-UP. SENSOR ON ENGINE HAD FAILED.SDR ASAA2018040324123Compensator · no testDURING ACCOMPLISHMENT OF TSR701503, NR 1 MAIN TANK FQIS FAILS SYSTEM TEST IAW TASK 28-41-00-730-801. ACFT GROUNDED. USING FMC CDU DETERMINED THE NR 1 FQIS FAILS SYSTEM TEST IAW AMM TASK 28-41-00-730-801. READINGS SHOW THAT THE COMPENSATOR PROBE IS DEAD CENTSDR ASAA2018032624049Indicator · false indicationAT REFUEL PANEL CENTER TANK READ ALL 8. ACFT GROUNDED. PERFORMED FIM 28-41 TASK 814. CHECKED GOOD. NO FAULTS NOTED. NO HISTORY IN 30 DAYS. OPS NORMAL. OK FOR SERVICE.SDR HALA2018032000116Warning System · false activationETOPS SIGNIFICANT SYSTEM, DURING CRUISE FLIGHT ECAM: FUEL RIGHT PUMP 2 LOW PR CAME ON TWICE AND THEN EXTINGUISHED BOTH TIMES. ACCOMPLISHED FCMC 1/2 RESET AND BITE TEST FCMC 1/2, ALL TEST PASS. NO DEFECTS NOTED ON GROUND.SDR ASAA2018030423753Control Unit · faultedFUEL STATUS MAINTENANCE MESSAGE. ACFT GROUNDED. FLSCU-1(7QJ) REMOVED AND REPLACED, SYSTEM TESTED OK IAW AMM 28-46-34.SDR ASAA2018030323743Processor · failedRIGHT MAIN FUEL QTY BLANKED BRIEFLY AT GATE, ACFT GROUNDED. REMOVED AND REPLACED THE FUEL QUANTITY PROCESSOR UNIT IAW AMM 28-41-81, GROUND VERIFICATION TEST PASSED. ACCOMPLISHED BITE CHECK, LIGHTS STAY ON, NO FAULT NOTED. ACFT OK FOR SERVICE IAW FIM 28-41SDR SIMA20180225001Signal Cond Unit · failedAFTER TAKEOFF, FUEL QUANTITY INDICATIONS WENT TO AMBER DASHES AND EICAS MESSAGE E1/2 LOW FUEL MESSAGE PRESENTED. RMOVED AND REPLACED THE WING FUEL CONDITIONING UNIT IAW AMM 28-40-01, OPS CHECKED GOOD IAW AMM 28-40-00.SDR FDEA201802070313Float Valve · failed2.44 HRS INTO FLIGHT, RECEIVED A TANK 3 TIP TRAPPED LVL 1 ALERT. REMOVED & REPLACED INBD. TRANSFER FLOAT VALVE, NR 3 TANK IAW MM 28-21-10-2, & OPS. CHECKED NORMAL.SDR FDEA2018062900281Processor · malfunctionedDURING CRUISE AT FL 360, ALL TANK PUMPS OPERATING NORMALLY, NOTICED THE RT INNER PUMP QUANTITY WAS MORE THAN 2000 LBS LESS THAN RIGHT INNER AND CONTINUING TO DECREASE. TROUBLESHOT BY TURNING OFF BOTH RT PUMPS. TURNED ON RT INNER NR 1, QUANTITY DECREASED FURTHESDR ASAA2018013023330Indicator · failedCENTER FUEL QTY GAUGE AT WING REFUEL PANEL INOPERATIVE. ACFT GROUNDED. REMOVED & REPLACED CENTER FUEL QTY IND GAUGE REF B737-800 AMM 28-41-61. OPS CHECK GOOD. CTR FUEL TANK QTY IN FUEL RECEPTACLE PANEL MATCHES FLT DECK INDICATION.SDR ASAA2018012923445Control Panel · failedFUELERS UNABLE TO FUEL A/C USING AUTO FUEL PRE SELECT SWITCH MANUAL FUELING IS OK GROUNDED - YES. R&R PRESELECTOR FUEL QUANTITY PANEL IAW AMM 28-42-21. OPS CHECK GOOD. MEL LIST UPDATED. PLACARD REMOVED. MCC NOTIFIED.SDR ASAA2018012523308Probe · failedTWO HRS INTO FLIGHT, THE LEFT MAIN FUEL INDICATED 1500 LBS LESS THAN RIGHT. RAN QRH AND DETERMINED THERE WAS NO FUEL LEAK, RAN QRH TO BALANCE FUEL. RECEIVED FUEL WITHIN 300 LBS. AND LANDED. ON LANDING, THE LEFT INDICATOR WAS 1000 LBS MORE THAN RIGHT. ACFSDR ASAA2018011823235Processing Unit · faultyFUEL QUANTITY INDICATOR RIGHT MAIN TANK BLANKED TWICE FOR MAYBE TWO SECONDS BEFORE RECOVERING TO DISPLAY CORRECT VALVE. BLANK MEANS NO VALUE DISPLAYED AT ALL, COMPLETELY BLANK. GROUNDED - YES. REVIEWED IN FLIGHT FAULTS OF FQIS. LAST LEG AND SEVERAL OTHER LEGS SDR ASAA2018011423195Compensator · failedRT FUEL QTY ON THE UPPER DISPLAY UNIT INTERMITTENTLY GOES BLANK ALONG WITH THE TOTALIZER. WHEN SHOWING THE INDICATIONS APPEAR NORMAL. FMC "ACT PERF INIT" PAGE FUEL QTY INDICATION APPEARS UNAFFECTED. GROUNDED - YES. RELEASED PER MEL 28-6B, RT FUEL QTY INDICATIOSDR UIEA2018011300062Valve · malfunctionedRIGHT ENGINE SPAR VALVE OPS CHECK FAILED. OPS CHECKED IAW AMM 28-22-01, NO DEFECTS NOTED.SDR JJBA20180112008Tank Unit · inoperativeFUEL TANK UNIT NR 6 INOPERATIVE. FUEL TANK UNIT WAS REPLACED IAW AMM 28-41-02. OPS CHECKED GOOD.SDR ASAA2018011023135Probe · failedACFT GROUNDED. ACCOMPLISHED STEP 1 OF THIS TSR - TANK AND COMP UNITS TEST ON THE #2 TANK PER B737-800 AMM 28-41-21-710-801. FOUND THE COMPENSATOR PROBE, AND TANK UNITS 4, 6, 7, AND 11 OUT OF LIMITS. REPLACED THE TANK UNITS 4, 6, 7, 11, AND COMPENSATOR PROBE. SDR ASAA2017121322885Indicator · failed#1 MAIN TANK REFUEL INDICATOR INOP. GROUNDED - YES. REPLACED #1 REFUEL INDICATOR PER B737-900 AMM 28- 41-61. OPS CHECK NORMAL.SDR ASAA2017112722702Indicator · failedNR 2 TANK REFUEL PANEL INDICATION INOP. GROUNDED - YES. REMOVED AND REPLACED REFUEL PANEL #2 TANK INDICATOR PER B 737-800 AMM 28-412-61-400-801. GROUND BITE TEST OK.SDR ASAA2017112622703Warning Light · false activationCENTER TANK FUEL QUANTITY INDICATOR WAS INDICATING INTERMITTENT READINGS AT CRUISE. TOTALIZER IS BLANK. ACFT GROUNDED. REMOVED THE HARNESS 28400003-1 AND REINSTALLED CONNECTOR D11316, AND BUSSING PLUG. PERFORMED FIM 28-41 TASK 814, FQIS BITE TEST NOW PASS
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