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 ASAA2016112518816Compensator · failedNR 1 MAIN TANK FUEL QUANTITY FAILS SYSTEM TEST REF AMM TASK 28-41-00-730-801. GROUNDED - YES. PERFORMED TANK AND COMPENSATOR TEST REF AMM TASK 28-41-21-710-801. COMP BAD AT 60.62 PICOFARADS AND F1 TANK UNIT BAD AT 64.79 PICOFARADS. INITIATED MIG-2C S/N 40-0005SDR ASAA2016112418812Clamp · brokenNR 2 MAIN TANK REFUEL INDICATOR INOPERATIVE. ACFT GROUNDED. ACCOMPLISHED TEST IAW AMM SUBTASK 28-41-61-710-003. NO FAULTS NOTED. AS PRECAUTIONARY CLEANED INDICATOR CONNECTOR WITH CONTACT CLEANER. FOUND CLAMP THAT HOLDS INDICATOR BROKEN, WOULD NOT TIGHTEN. ISDR ASAA2016112319207Compensator · out of toleranceENGINEERING REQUEST CHECK NR 2 (RIGHT) FUEL TANK UNIT AND COMPENSATOR VALUES. GROUNDED - YES. REF T/C NG-28FCD-18090-1, REMOVED AND REPLACED TANK 2 F8, F9 AND F10 TANK PROBES, REF AMM 28-41-21-400-801. REMOVED AND REPLACED TANK NR 2 F1 AND F15, REF AMM 28-41-2SDR ASAA2016112218814Probe · failedNR 2 MAIN FUEL TANK FAILS SYSTEM TEST IAW FQIS SYSTEM TEST IAW AMM 28-41-00-730-801. ACFT GROUNDED. DRAINED NR 2 FUEL AND TAGGED EXTERNAL POWER. REMOVED AND REPLACED NR 2 COMP PROBE (F15), F1 TANK UNIT AND F8 TANK UNIT IAW AMM 28-41-21-400-801. REMOVED AND RSDR ASAA2016112218813Control Unit · failedNR 1 MAIN FUEL TANK FAILS FQIS SYSTEM TEST, IAW AMM 28-41-00-730-801. ACFT GROUNDED. ACCOMPLISHED NR 1 FUEL TANK FQIS TANK AND COMP UNIT TEST IAW AMM 28-41-21-710-801. FOUND TANKS UNITS F1, F2, F6 AND F10 TO BE OUT OF LIMITS. REMOVED NR 1 MAIN FUEL TANK WINSDR ASAA2016112118832Compensator · failedRT MAIN TANK FUEL QUANTITY JUMPED AROUND GOING DOWN AS MUCH AS 500LBS, AND STAYING THERE FOR SOMETIME. LATERAL IMBALANCE INDICATION GOT AS MUCH AS 1000LBS AT ONE TIME BUT STEADIED OUT AT 700LBS DIFF BETWEEN L/R MAIN TANKS. AIRCRAFT FUEL TOTALIZED AND FUEL USEDSDR ASAA2016112018765Compensator · out of limitsWHILE ACCOMPLISHING TSR818110, FOUND RT NR 2 FUEL TANK UNITS F1, F2, F3, F9, F10, AND COMPENSATOR PROBE F15 EMPTY CAPACITANCE TO BE OUT OF LIMITS, IAW AMM 24-41-21-710-801. ACFT GROUNDED. REPLACED THE COMPENSATOR PROBE F15, AND T/U F1, 9, AND 10, IAW AMM 28-SDR ASAA2016111918740Not Reported · failedTECH SERVICES REQUEST CHECK NR 1 FUEL TANK, TANK UNIT AND COMPENSATOR VALUES. GROUNDED, YES. ACCOMPLISHED TSR 818103 ALL STEPS AND T/C 78528000 FUEL ENTRY PERMIT. REMOVED AND REPLACED NR 1 FUEL TANK F15, F1, F2, AND F3 REF AMM 28-41-21. OPS TEST PASSED WITH NOSDR 6CBA2016111816156Pressure Switch · failedAFTER DEPARTING,IN CRUISE FLIGHT THE FLIGHT CREW REPORTED BOTH FUEL PUMPS CYCLING ON & OFF 5 SEC. INTERVALS. COMPLETED QRH PROCEDURE, CYCLING PERSISTED. THE AIRCRAFT MADE AN UNSCHEDULED LANDING WHERE IT LANDED SAFELY. THE MAINTENANCE CREW ON SITE INSPECTED THESDR ASAA2016111518741Not Reported · failedTECH SERVICES REQUEST CHECK NR 1 FUEL TANK UNIT AND COMPENSATOR VALUES. GROUNDED, YES. ACCOMPLISHED TSR818109 ALL STEPS. FOUND NR 1 FUEL TANK F15=75.01, F1=67.42, F2=43.09, F3=42.93 ARE OUT OF LIMITS REF AMM 28-41-21-710-801. REMOVED AND REPLACED F15 AND F1, ASDR ASAA2016111518701Compensator · failedNR 2 MAIN TANK SHUT OFF AT 8400 LBS, THEN JUMPED TO 8900 LBS. ACFT GROUNDED. COMPLIED WITH FQIS BITE TEST, IAW FIM 28-41 TASK 801. FOUND FAULTS TANK 1, 28-41108 COMPENSATOR DATA BAD AND TANK 2, 28-41208 COMPENSATOR DATA BAD. COMPLIED WITH FIM 28-41 TASK 807SDR ASAA2016111218626Circuit Breaker · trippedFLIGHT CREW FOUND FUEL QTY 2 CIRCUIT BREAKER OPEN. ACFT GROUNDED. ACCOMPLISHED GV OF FUEL QTY 2 CIRCUIT BREAKER, NO DEFECTS NOTED, CLOSED THE CIRCUIT BREAKER IAW AMM 20-60-01, ACCOMPLISHED FQIS BITE CHECK IAW FIM 28-41 TASK 801, NO FAULTS NOTED, NO HISTORY,SDR ASAA2016102818503Compensator · failedCHECKED DRY CAPACITANCE OF NR 2 TANK. ACFT GROUNDED. ACCOMPLISHED FQIS SYSTEM TEST, DRY CAL AND FOUND NR 2 TANK CAPACITANCE HIGH AT 407.5 AND COMP PROBE CAP HIGH AT 59.4 IAW AMM 28-41-00-730-801. ACCOMPLISHED TANK AND COMP UNITS TEST AND FOUND COMP PROBE F15SDR HALA2016102600377Warning System · activated
OPEN - ATO - TANK L AFT PUMP LO LIGHT ILLUMINATED ON THROTTLE ADV FOR T/O, MAIN TANK FUEL AC BOOST PUMPS. DEFERRED USING MEL 28-22-01.SDR 2017FA0000431Transmitter · malfunctionedREMOVED AND REPLACED THE LEFT FUEL SENDER, DUE TO ERRATIC INDICATIONS OF FUEL AND QUIT WORKING COMPLETELY INTERMITTENTLY.SDR A6WA201644450Indication Sys · malfunctionedFUEL CH 1 & 2 CAUTION MESSAGE IN FLIGHT. ALL FUEL QUANTITIES SHOWED DASHES. DIVERTED TO SWF. MESSAGES WENT AWAY MINUTES LATER AND FUEL QUANTITIES RETURNED.SDR 2017FA0000430Transmitter · malfunctionedREMOVED AND REPLACED THE RT FUEL SENDER, DUE TO ERRATIC INDICATIONS OF FUEL AND QUIT WORKING COMPLETELY INTERMITTENTLY.SDR AALA20161011003Processor · faultyAIRCRAFT WAS GROUNDED. AIR INTERRUPT LAX-SYD. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT OVERWEIGHT. CREW REPORTED FUEL DISAGREE WITH EXCESSIVE DIFFERENCE BETWEEN CALCULATED AND FUEL QUANTITY. ACCOMPLISHED FIM 28-41-00-810-825 AND RECEIVED MAINTENASDR ASAA2016100818248Compensator · out of limitsMAIN TANKS AUTO SHUTOFF AT 8360 IN NR 1 TANK AND 8230 IN NR 2 TANK - BOTH LESS THAN FULL. ACFT GROUNDED. PERFORMED SYSTEM TEST OF FQIS AND FOUND #2 FUEL TANK UNIT CAPACITANCE OUT OF TOLERANCE, REF B737-800 AMM 28-41-00-730-801. TANK AND COMPENSATOR UNIT TEST SDR ASAA2016100318203Compensator · failedDURING 800-28EA-16443, FOUND THE NR 1 FUEL QUANTITY FAILS SYSTEM TEST IAW AMM TASK 28-41-00-730-801. ACFT GROUNDED. REPLACED THE TANK UNIT NR 1 AND COMPENSATOR PROBE. FQIS READS NORMAL IAW AMM 28-41-21, AND 28-41-00.SDR ASAA2016100318202Compensator · failedDURING 800-28EA-16443, FOUND THE NR 2 FUEL QUANTITY FAILS SYSTEM TEST IAW AMM 28-41-730-801. ACFT GROUNDED. ACCOMPLISHED TANK AND COMPENSATOR TEST IAW AMM 28-41-21. FOUND F15R COMPENSATOR AND F1R, F8R, F9R, AND F10R BAD. REMOVED AND REPLACED TANK AND COMPENSDR ASAA2016100218186Warning Light · illuminatedFUEL IN CENTER TANK INDICATED .30 ON THE GROUND PRIOR TO FLIGHT BUT SHOWED 1.38 @ TOP OF CLIMB. CENTER PUMPS WERE TURNED ON AND TANK WAS BURNED DOWN TO 0.00 WHEN LOW PRESS LIGHTS ILLUMINATED. GROUNDED - YES. PERFORMED FQIS BITE PROCEDURE, REF B737-900 FIM 28-4SDR FDEA201609273373Indication Sys · faultyFUEL SYSTEM HAS MEL 28-42-02-02-A. AFTER T/O TRIM FUEL DASHES CAME AND WENT CAUSING FMMS ISSUES. FUEL LOW LEVEL LIGHTS THEN CAME ON AND OFF. REF MEL 28-42-02-02-A, STEP 5 DELETES FUEL QTY. INPUTS TO FMS, REF AMM 28-42-41-04, RT FUEL LOW LEVEL LIGHTS CHECK SDR P5CA2016092500272Warning System · false activationLEFT FORWARD FUEL PUMP EICAS MESSAGE, STARTED TO RUN QRH PROCEDURE AND EICAS MESSAGE WENT OUT, CANNOT DUPLICATE MESSAGE. OPS CHECK OF ENGINE FUEL FEED SYSTEM GOOD IAW AMM 28-22-011.SDR ASAA2016091618048Warning System · false activationWHEN STARTING NR 1 ENGINE SPAR VALVE CLOSED, LIGHT ILLUMINATED BRIGHT AND REMAINED ILLUMINATED. ACFT GROUNDED. FOUND FUEL SPAR VALVE NR 1 ENGINE, P6-3, B4 OPEN. PERFORMED CB RESET PROCEDURE, REF AMM 20-60-01. NO DEFECTS NOTED. VALVE CONNECTOR GVI, NO DEFESDR ASAA2016091217992Indication Sys · malfunctionedFUEL QTY NR 1 TANK WENT BLANK FOR A FEW SECONDS THEN CAME BACK WITH A DIFFERENT QTY. STARTED WITH 8.57 THEN WENT TO 8.13. ACFT GROUNDED. NO CURRENT FAULTS, FQIS BITE IAW FIM 28-41 TASK 801. NR 1 FUEL TANK INDICATOR WITHIN TOLERANCE, CHECKED WITH DRIP STICKS SDR AALA20160919009Transmitter · leakingDURING CLIMB FUEL DISAGREE MESSAGE LIGHT ILLUMINATED. DOWN 7000 LBS ALMOST 2 HRS INTO THE FLIGHT. RETURNED TO FIELD. THE AIRCRAFT WAS GROUNDED. OBVIOUS FUEL LEAK IN SYSTEM. LEFT AND RIGHT CENTER AUXILIARY TANK UNITS NR 1 RIGHT AND NR 1 LEFT REPLACED. OPERATIOSDR AALA20160911003Transmitter · faultyDURING CLIMB, FUEL DISAGREE MESSAGE LIGHT ILLUMINATED. DOWN 7000 LBS ALMOST 2 HRS INTO THE FLIGHT. OBVIOUS FUEL LEAK IN SYSTEM. LEFT AND RIGHT CENTER AUXILIARY TANK UNITS NR 1 RIGHT AND NR 1 LEFT REPLACED. OPS AND LEAK CHECKED NORMAL. THE AIRCRAFT WAS GROUNDESDR HALA2016090800345Indication Sys · malfunctionedDURING CRUISE FLIGHT, WITH THROTTLES DISPLACED TO MATCH N1, FUEL FLOW WAS +100 LBS AN HOUR ON THE NR 1 ENG. HOWEVER THE LEFT TANK WAS 3,500 LBS LESS THAN THE RIGHT. FUEL CROSSFEED OPERATES NORMALLY. PERFORMED FUEL QAUNTITY BITE TEST IAW TASK 28-41 TASK 85SDR CALA2016090600625Indication Sys · malfunctionedRECEIVED FUEL IMBALANCE WARNING DURING CRUISE. FUEL QUANTITY CONTINUED TO INDICATE AN INCREASED LOSS APPROX 200 LBS IN 10 MINUTES, SHUT DOWN NR 1 ENG IAW CHECKLIST, PERFORMED FIM TASK 05-51-48. FUEL IMBALANCE EXCEEDANCE CONDITIONAL INSPECTION. OPS OK. PERFSDR SWAA2016090855584Probe · leakingNR 2 MAIN TANK HAD POSSIBLE FUEL LEAK, LEFT MAIN AT 8500 RIGHT MAIN AT 8480. AT 1505Z LEFT MAIN AT 8100 RIGHT MAIN AT 7720 - 380LB IMBALANCE IN 14 MINUTES. COMPLIED WITH QRH AND SHUT DOWN NR 2. FUEL FLOW AT FL 370 WAS DEAD EVEN. CENTER TANKS WERE BEING USE PRSDR ASAA2016082617821Circuit Breaker · trippedNR 2 FUEL QTY CIRCUIT BREAKER (P6-3 A5) FOUND OUT DURING MAINTENANCE. ACFT GROUNDED. INSPECTED THE CIRCUIT BREAKER AND PANEL P6-3 IAW AMM 20-60-00. NO FAULTS NOTED. RESET THE CIRCUIT BREAKER, NORMAL INDICATION VERIFIED.SDR 2017FA0000432Transmitter · erraticREMOVED LT FUEL SENDER DUE TO ERRATIC INDICATIONS.SDR AALA20160822004Probe · malfunctionedFUEL LT WING TK HI TEMP WARNING DURING CLIMB. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO FIELD DFW. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED THE LEFT WING TEMPERATURE PROBE (54QTI) IAW AMM 28-42-15-0401.SDR HALA2016080800322Indicator · malfunctionedPOWER INTERRUPTION, DOUBLE AMBER BARS THRU FUEL USED COUNTERS REPORTED BY FLT CREW. RESET BFCMC. PERFORMED BITE TEST IAW AMM 28-51-00-740-801A OK. NO FAULTS NOTED. OK FOR SERVICE.SDR P5CA2016080800184Warning System · false activationLT FORWARD FUEL PUMP EICAS MESSAGE. LEFT FORWARD FUEL PUMP PRESSURE LIGHT DISPLAYED. LEFT FORWARD FUEL BOOST PUMP TESTED IAW AMM 28-22-00. NO FAULTS FOUND, CHECK SERVICEABLE.SDR P5CA2016080100177Warning System · false activationEICAS MESSAGE CENTER LT FUEL PUMP AND ENGINE FUEL FEED SYS. OPS TEST IAW AMM 28-22-00/501, NO FAULT FOUND.SDR UIEA2016072700641Warning Message · false activationAFTER LANDING STATUS MESSAGE FUEL QTY CHANNEL. FQIS PROCESSOR BITE TEST CARRIED OUT IAW AMM 28-41-00, ALL TESTS PASSED, MESSAGE ERASED.SDR UIEA2016072000600Warning System · activatedCREW PERFORMED LOW SPEED REJECTED T/O WHEN EICAS MSG FOR OVERRIDE JETT PUMP NR 3 FWD APPEARED. PLACED ON DMI.SDR AALA20160713021Warning Message · false activationDURING CLIMB THE FUEL IMBALANCE LIGHT ILLUMINATED WITH ALL BOOST PUMPS ON. LEFT TANK INDICATING LOWER THAN RIGHT. LANDING UNEVENTFUL. MAINTENANCE ACCOMPLISHED AN OPS CHECK OF FUEL PUMP AND FUEL TRANSFER IAW AMM 28-41-00 AND BITE PROCEDURE "FUEL QUANTITY SYSTEMSDR UIEA2016070200558Switch · defectiveDURING ENGINE START RT ENGINE VALVE LIGHT FAILED TO CYCLE LAMP TEST CONFIRMED THAT THE LIGHT WAS FUNCTIONING PROPERLY. PLACED ON DEFERRAL. REPLACED SW LIGHT IAW 33-13-00. OPS CK OK IAW 28-22-01. THIS CLEARS MEL.SDR SWAA2016070553438Indicator · faultyBOTH CENTER FUEL PUMP LOW PRESSURE LIGHTS ILLUMINATED, NO DRAW FROM CENTER TANK. PRIMED CENTER TANK BOOST PUMPS PER AMM. RESET CENTER TANK BOOST PUMP UFI'S PER AMM.SDR ASAA2016070117222Totalizer · malfunctionedAFTER T/O FUEL TOTALIZER READ 1000 HIGH, STARTED WITH 25.85 LBS, RAMP FUEL AT 10K QTY INDICATED 24.8 LBS, WITH 1.9 USED = 26.7 LBS, AT TOP OF CLIMB QTY INDICATED 21.6 WITH 4.45 LBS USED = 26.0 LBS. ALSO TOTALIZER FUEL READ 500 TO 600 GREATER THAN FMC FUEL USUASDR ASAA2016063017221Compensator · failedNR 2 MAIN FUEL TANK AUTO SHUT OFF AT 8,260 LBS. ACFT GROUNDED. REMOVED NR 2 MAIN TANK ACCESS PANEL 632AB IAW AMM 28-11-11. REMOVED AND REPLACED NR 2 MAIN TANK COMPENSATOR PROBE IAW AMM 28-41-21. INSPECTED AREA, OK TO CLOSE ACCESS PANEL 632AB. INSTALLED ANDSDR UIEA2016061900432Warning System · activatedFUEL CONFIGURATION LIGHT ILLUMINATED QRN 12.1. ACCOMPLISHED BALANCE RESTORED. FQIS TEST PASS IAW AMM 28-41-00/501, OK FOR SERVICE IAW SL 767-SL-28-035-A, FUEL BALANCE MANAGEABLE THROUGH NORMAL PROCEDURE.SDR IPXA2016062004809Warning System · activatedEMERGENCY DECLARED AT 32000 FT, CENTER TANK PUMP FAULT. UPON FUEL SYS REVIEW ON OUTER TANKS WERE FEEDING BUT UNABLE TO FEED FUEL FROM INNER TANKS. DEFERRED AUTO FUEL FEED SYS IAW 28-21-09-1. R&R 91QA AND 154QA. OPS CK GOOD MM 28-21-00-0501.SDR AALA20160616002Indication Sys · malfunctionedAIRCRAFT WAS NOT GROUNDED. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT NOT OVERWEIGHT. DURING CLIMB THE RIGHT FUEL QUANTITY SHOWED 1000 LBS LOWER THAN THE LEFT WITH AMBER, "IMBALANCE" ILLUMINATED. THE DIFFERENTIAL INDICATION THROUGHOUT FLIGHT. MAINTSDR FDEA201606131980Computer · faultyAPPROX 60 NM FROM DESTINATION, GOT FUEL ADV ON ECAM. LT OUTER 6K, LT INNER 11.0, CTR WAS 0, TRIM TANK WAS 0, RT INNER STARTED AT 11, THEN 10, THEN 9, THEN 8, ALL THE WAY TO ZERO. RIGHT WAS 4.0 AND DECREASING. DIVERTED. WITH T/O OF 57, FUEL USED COUNTER WASSDR SIMA20160606002Indication Sys · faultyDVT INDICATION DUE ERRONEOUS FUEL INDICATIONS ON RT FUEL TANK, DECLARED EMER. FLIGHT CREW PLACARDED RT FUEL QTY INDICATIONS INOPERATIVE MEL 28-09. REMOVED AND REPLACED TU R-4 IAW EMB 145 AMM 28-41-02. REFERENCE NRWC 699-CMH-02573. MEL RESTOREDSDR UIEA2016060200393Sensor · delaminatedFUEL LEVEL SENSOR IS DELAMINATING IN RT WING SURGE TANK. R & R RT WING FUEL LEVEL SENSOR UNIT IAW MM 28-21-03-004-008 PGS 1 - 3 & MM 28-21-03-404-004 PGS 1 - 3.
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