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 UIEA2016121901047Circuit Card · inoperativeLEFT SPAR VALVE FAILED ON ENGINE SHUT DOWN. TROUBLESHOT IAW FIM 28-22 14, R & R THE LT SPAR VALVE LIGHT DIODE, FUSE CARD IAW AMM 33-16-02. OPS CHECKED OK.SDR AALA20161215013Pressure Switch · faultyAIRCRAFT NOT GROUNDED. NR 1 TANK FORWARD FUEL BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED APPROXIMATELY 3 MINUTES AFTER TAKEOFF AND REMAINED ON FOR APPROXIMATELY 4 MINUTES. AFTER SHUTDOWN THE LIGHT CAME ON WITH THE SWITCH IN THE ON POSITION. REMOVED AND REPLASDR AALA201612159001Actuator · failedAIRCRAFT WAS GROUNDED. TRIM TANK INLET VALVE FAILED OPEN. MAINTENANCE REPLACED TRIM TANK INLET VALVE ACTUATOR PER AMM 28-27-42.SDR ASAA2016121219025Circuit Breaker · trippedDURING CRUISE AT FL380, RECEIVED A FUEL IMBALANCE. DECIDED NO FUEL LEAK AND PROCEEDED TO CROSSFEED AND CROSSFEED WOULD NOT OPEN. FUEL FLOW NORMAL. BOTH ENGINE TAKING FUEL FROM NR 1 TANK. ACFT GROUNDED. INSPECTED FUEL CROSSFEED VALVE & FOUND MANUAL INDICATIONSDR B4VR121216ATransducer · inaccurateINACCURATE READINGS FROM RIGHT ENGINE FUEL PRESSURE TRANSDUCER. TRANSDUCER HAS ONLY 307.9 HOURS SINCE NEW. NEW TRANSDUCER WAS INSTALLED AND INDICATION ISSUES WENT AWAY.SDR AALA201612139011Switch · faultedFUEL AUTO FEED FAULT. MAINTENANCE REPLACED PRESSURE BUTTON SWITCH ON CENTER PUMP 1 AND 2 PER ESPM 20-45-11 AND PRESSURE SWITCH (40QA) PER AMM 28-21-15. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.SDR AALA201612109008Pressure Switch · faultedFUEL AUTO FEED FAULT. MAINTENANCE REPLACED PRESSURE BUTTON SWITCH ON CENTER PUMP 1 AND 2 IAW ESPM 20-45-11 AND PRESSURE SWITCH (40QA) IAW AMM 28-21-15. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.SDR QMLA2016120916141Filter · leakingDURING TAKE OFF PHASE, THE PILOT NOTICED THE FUEL FILTER LIGHT ILLUMINATED. TOOK PRECAUTIONARY MEASURES AND LANDED THE HELICOPTER. THE MECHANIC CHANGED OUT THE FUEL FILTER. THE FILTER BOWL FITTER HAD A LITTLE SEDIMENT IN THE BOTTOM. THE BOWL WAS CLEANED, AND ASDR AALA20161213023Switch · defectiveAIRCRAFT WAS GROUNDED. RIGHT CENTER FUEL PUMP AUTO SHUTDOWN IS INOPERATIVE. REMOVED AND REPLACE SWITCH S346 IAW WDM 28-21-11 AND 28-21-14. SYSTEM CHECKS NORMAL.SDR FDEA201612014299Packing · leakingDURING PREFLIGHT, WHEN THE FUEL PUMPS WERE SELECTED ON, THE NR 2 ENGINE HAD A FUEL LEAK COMING FROM THE PYLON FUEL DRAIN LINE. THE FUEL LEAK WAS COMING FROM LINE DOWNSTREAM FIRE SOV. R & R THE PACKING ON THE NR 2 ENGINE FUEL FEED LINE AND CONDUIT BETWEEN LSDR AALA20161202012Valve · faultyDURING CLIMB THE CENTER FUEL PRESSURE LIGHT ILLUMINATED. DEACTIVATED MAIN PUMPS TO GET FUEL OUT OF CENTER TANK. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED CENTER BOOST PUMP UFI IAW AMM 28-20-28, EXTRACTION CHECK VALVE IAW AMM 28-20-26-401, AND FORWARD AND ASDR AALA20161202011Ufi · faultyDURING CLIMB THE CENTER FUEL PRESSURE LIGHT ILLUMINATED. DEACTIVATED MAIN PUMPS TO GET FUEL OUT OF CENTER TANK. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED CENTER BOOST PUMP UFI IAW AMM 28-20-28, EXTRACTION CHECK VALVE IAW AMM 28-20-26-401, AND FORWARD AND ASDR UIEA2016122801058Valve · malfunctionedRIGHT ENGINE DID NOT START, START VALVE LIGHT ILLUMINATED. REMOVED AND REPLACED RIGHT ENGINE FUEL SPAR VALVE AND OPS CHECKED GOOD IAW AMM 28-22-11.SDR UIEA2016113000916Line · damagedFUEL LINE DAMAGED. REPLACED THE FUEL LINE IAW MM 28-25-22/201.SDR AALA20161129012Pressure Switch · faultyAIRCRAFT NOT GROUNDED. RIGHT FORWARD FUEL BOOST PUMP FLICKERD LOW PRESSURE DURING CLIMB AND CRUISE. FUEL IMBALANCE DEVELOPED OVER TIME. LEFT TANK INDICATED GREATER BURN RATE. REMOVED AND REPLACED TANK 2 FORWARD FUEL BOOST PUMP PRESSURE SWITCH IAW AMM 28-42SDR 2016FA0000574Hose · damagedPILOT REPORTED FUEL ODOR IN CABIN. FOUND SEVERAL FUEL HOSES CRACKED AND SPLIT IN THE WING ROOT.SDR ASMF20161216010Valve · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING START ENGINES, THE LEFT ENGINE AUTO STAR SYSTEM FAILED. MAINTENANCE PERSONNEL PERFORMED REVISION TO AUTO STAR SYSTEM, DETECTING THE EICAS MESSAGE FAIL, MAINTENANCE CODE 28-19217 AND THE CIRCUIT BREAKER C2822803 POPPESDR SWAA2016111409681Pressure Switch · failedAIR TURNBACK, ON CLIMB THROUGH FL 280 NR 1 FUEL BOOST PUMP FORWARD LIGHT ILLUMINATED STEADY UNTIL OFF AT FL320. R&R NR 1 FORWARD FUEL BOOST PUMP PRESSURE SWITCH IAW AMM.SDR AALA201703089016Switch · faultyAIRCRAFT WAS NOT GROUNDED. WHEN NR 1 LEFT FUEL PUMP WAS TURNED ON, FAULT INDICATED. MAINTENANCE FOUND PUSH BUTTON SWITCH (PBSW) 13QA WAS BAD AND REPLACED PBSW (13QA) PER ESPM 20-45-11. (SEE ALSO AALA201611149017 FOR PUMP AND AALA201703089015 FOR RELAY).SDR AALA201703089015Relay · faultyAIRCRAFT WAS NOT GROUNDED. WHEN #1 LEFT FUEL PUMP WAS TURNED ON, FAULT INDICATED. MAINTENANCE FOUND RELAY WAS BAD AND REPLACED RELAY (53QA) PER ESPM 20-46-50. (SEE ALSO AALA201611149017 FOR PUMP AND AALA201703089016 FOR PBSW).SDR AALA20161114005Circuit Breaker · trippedAIRCRAFT WAS NOT GROUNDED. DURING CRUISE FLIGHT CREW RECEIVED A FUEL IMBALANCE EICAS MESSAGE AND ACCOMPLISHED THE FUEL IMBALANCE CHECKLIST. SUBSEQUENTLY EICAS MESSAGES LEFT FORWARD FUEL PUMP, LEFT AFT FUEL PUMP AND FUEL CROSSFEED WERE RECEIVED AND FUEL CONTINUSDR QMLA2016103016119B-Nut · leakingTHE PILOT AND MEDICAL CREW SMELLED A STRONG FUEL ODOR WITHIN THE CABIN OF THE AIRCRAFT. THE MECHANIC WAS CALLED OUT TO INSPECT THE AIRCRAFT AND FOUND A FUEL LINE FROM THE PUMP ON THE ENGINE SIDE UNDER TORQUED. TORQUED THE B-NUT, AND ACCOMPLISHED A GROUND RUNSDR ASAA2016102618487Check Valve · missingCENTER FUEL TANK AND CENTER PUMPS ON. RT FUEL QUANTITY DECREASED BY APPROXIMATELY 200 PPH. AFTER CENTER TANK DEPLETED, WING TANKS REMAINED SLIGHTLY IMBALANCED UNTIL CORRECTED. ACFT GROUNDED. ACCOMPLISHED BOTH ENGINE IDLE RUN, WITH ALL SIX BOOST PUMPS ON, FUELSDR AALA201610249001Actuator · faultyAIRCRAFT WAS GROUNDED. IN FLIGHT NR 2 FUEL VALVE SHOWED IN TRANSIT ON FUEL PAGE, REMAINED SAME UNTIL ENGINE SHUTDOWN. ALL OTHER INDICATIONS NORMAL. MAINTENANCE REPLACED THE NR 2 ENGINE LOW PRESSURE FUEL VALVE ACTUATOR PER AMM 28-24-51-000-001-A AND 28-24-51SDR ASAA2016102218444Battery · failedENGINE FUEL SPAR VALVE ELECTRICAL CONTROL AND IND TEST FAILS STEP 4. (2)(I) , SHOWS 31VDC - OUT OF TOLERANCE. ACFT GROUNDED. ATTACHED CONNECTOR TO NEW EMERGENCY FUEL SHUTOFF BATTERY IAW AMM 28-22-14. FAILED TEST STEP NOW PASSES OPS TEST. REMOVED EMERGENCY FUSDR 2016FA0000504Line · chafedDURING INVESTIGATION FOLLOWING AN INSTRUMENT PANEL FIRE ON LANDING ROLLOUT, THE INCOMING PRIMER LINE UNDER THE INSTRUMENT PANEL HAD BEEN CHAFFED THROUGH BY A LANDING LIGHT WIRE. THE CHAFFING HAD CREATED A PIN HOLE IN THE PRIMER LINE AND THE RESULTING FIRE APPSDR 2016FA0000503Regulator Valve · leakingHEATER FUEL REGULATOR SHUTOFF VALVE PN 23D04 HAD BEEN VISUALLY INSPECTED FOR LEAKS OR FUEL STAINS IAW AD2004-25-16R1, 06/20/05, AND A-107A. THE FUEL REGULATOR SHUTOFF VALVE PASSED ITS INSPECTION UNDER STATIC OR NO PRESSURE CONDITIONS. NOT UNTIL LATER WHEN WESDR P5CA2016101400280Fuel Sys · malfunctionedCOULD NOT GET FUEL OUT OF CENTER TANK. RT CENTER WING JETTISON & OVERRIDE PUMP OPS NORMAL IAW AMM 28-31-00.SDR 2016FA0000571Insulator · failedFUEL MIGRATION FROM THE RT TANK TO CENTER TANK. UPON INVESTIGATION IT WAS FOUND THAT A CLAMP INSULATOR HAD FAILED AND STARTED TO CHAFE A SMALL DIAMETER FUEL LINE. THE FUEL LINE EVENTUALLY WAS PUNCTURED AND ALLOWED FUEL TO MIGRATE FROM THE RT TANK TO CENTER TANSDR ASAA2016092918161Impeller · vibrationLEFT CENTER TANK BOOST PUMP CREATES VIBRATION ON RUDDER PEDALS WHEN SELECTED ON. ACFT GROUNDED. REMOVED AND REPLACED LEFT CENTER TANK BOOST PUMP IAW AMM 28-22-41. DISCONNECTED POGO STICK. BUT DID NOT ADJUST AND REINSTALLED POGO STICK IAW AMM 28-22-41-400-801SDR COEA2016092602976Fuel Line · leakingFLIGHT 8675, ENROUTE, AIR TURNBACK DUE TO A STRONG FUEL ODOR IN COCKPIT AT TAKEOFF AND CLIMBOUT. PILOT RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. AFTER EXTENSIVE INSPECTION, MAINTENANCE REPLACED RUBBER VENT HOSES IN RT AND LSDR COEA2016092603976Line · looseFLIGHT 7675, FUEL ODOR IN COCKPIT ON CLIMB OUT. ACCESSED FUEL RESERVOIR AND PERFORMED EXTENSIVE TROUBLESHOOTING, FOUND LOOSE CONNECTION ON FUEL MAINFOLD AND TIGHTENED AND LEAK CHECKED. NO LEAKS PRESENT AT THIS TIME.SDR ASAA2016092218114Shutoff Valve · failedFUELER REPORTED NR 2 FUELING VALVE DOES NOT OPEN ELECTRICALLY. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 FUEL TANK FUELING SHUTOFF VALVE. LEAK AND OPS CHECKED GOOD, IAW AMM 28-21-51-000-801 AND 28-21-51-400-801.SDR 1MYR2017081100433Transmitter · malfunctionedREMOVED RT FUEL SENDER PN S38522 SN 4688 AND INSTALLED RT FUEL SENDER PN S38522 SN 4963. WE HAVE BEEN HAVING A TERRIBLE TIME WITH FUEL SENDERS FROM CESSNA. WE KEEP GETTING ERRATIC INDICATIONS OF FUEL AND THEY QUIT WORKING COMPLETELY INTERMITTENTLY. CESSNA HSDR AALA201609199036Line · damagedLEFT WING FUEL IMBALANCE WHEN CENTER FUEL USED. IMBALANCE SEEMED TO TERMINATE WHEN CENTER FUEL AT 11,000 LBS. OPERATES NORMAL WITH CENTER FUEL AT 0 AND BALANCED. NO FUEL LEAK PERCIEVED. AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE AFT CROSSFEED VALVE, FORSDR AALA201609129005Pressure Switch · wornFUEL CENTER TANK LOW PRESSURE ECAM OCCURED SEVERAL TIMES, NR 2 CENTER TANK PUMP. MAINTENANCE REPLACED PRESSURE SWITCH 40QA AND OPERATIONAL CHECKED SATISFACTORY PER AMM 28-21-15.SDR HALA2016090800347Valve · damagedAFTER TAKEOFF, FUEL IMBALANCE ADVISORY ECAM MESSAGE. RIGHT WING TANKS 7000 LBS HEAVIER THAN LEFT TANKS. TRIM TANK WAS TRANSFERRING FORWARD AND APPEARED TO BE GOING INTO THE RIGHT TANK ONLY. IMBALANCE CONTINUED UNTIL TRIM TANK EMPTY MAX IMBALANCE WAS 12500 LSDR AALA201609079001Switch · defectiveAIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED WHEN LEAVING 15,000 THEY RECEIVED AN ECAM MESSAGE FOR FUEL LT TANK PUMP 1 LOW POWER INTERMITTENT AND FOLLOWED ECAM PROCEDURE BY TURNING THE PUMP OFF. MAINTENANCE REPLACED THE PUSH BUTTON SWITCH FOR THE LT FUEL TSDR 2017FA0000434Transmitter · malfunctionedREMOVED RT FUEL SENDER, INSTALLED LT FUEL SENDER AND INSTALLED RT FUEL SENDER. .SDR AALA201609069021Pressure Switch · faultyAIRCRAFT WAS NOT GROUNDED, ECAM FUEL CENTER TANK PUMP 2 LOW PRESSURE. REPLACED PRESSURE SWITCH 40QA AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 28-21-15.SDR SWAA2016082955251Check Valve · obstructedDIVERSION, IN-FLIGHT SHUTDOWN 15 MINUTES INTO FLIGHT WITH 3000 LBS REMAINING IN CENTER TANK, HAD AN 830 LBS IMBALANCE BETWEEN MAIN TANKS. NR 1 TANK STILL FULL NR 2 TANK 830 LBS LOWER. PROGRESS PAGE ARRIVAL FUEL CONTINUED TO DECREASE. R & R RT CENTER TANK BOSDR AALA201608269001Switch · defectiveAIRCRAFT WAS NOT GROUNDED: LEFT FUEL PUMP 2 LOW PRESSURE. REPLACED LT FUEL PUMP L2 PUSH BUTTON SWITCH, 64QA1 IAW SPM 20-45-10 AND ACCOMPLISHED A SATISFACTORY OPS CHECK.SDR SWAA2016082455080Shutoff Valve · leakingPOSSIBLE FUEL LEAKED DURING CLIMB OUT. R & R THE NR 2 FUELING SHUTOFF VALVE IAW AMM.SDR FDEA201608242968Controller · malfunctionedRECEIVED A LAT FUEL IMBAL WARING AFTER 35 MIN OF FLIGHT. FUEL SYSTEM IN MANUAL AND PROPERLY CONFIGURED. RIGHT 17.8, CENTER 14.8, LEFT 20.2. QRH COMPLIED WITH TO CORRECT IMBALANCE. CREW VERBAL AFTER FUEL WAS BALANCED AND MESSAGE CLEARED. RECEIVED LAT FUEL SDR AALA201611049006Relay · blownAIRCRAFT WAS NOT GROUNDED. FUEL ACT TRANSFER FAULT - ACT 2 INDICATES EMPTY (600 POUNDS IN TANK) & ACT 1 REFLECTS 5100 POUNDS (ACTUAL 4960 POUNDS). MAINTENANCE REPLACED 5QH1 ACT INLET VALVE ACTUATOR AND 14QH RELAY AND 18QH RELAY PER AMM 28-28-54. (SEE ALSO ASDR AALA201611049005Relay · blownAIRCRAFT WAS NOT GROUNDED. FUEL ACT TRANSFER FAULT - ACT 2 INDICATES EMPTY (600 POUNDS IN TANK) & ACT 1 REFLECTS 5100 POUNDS (ACTUAL 4960 POUNDS). MAINTENANCE REPLACED 5QH1 ACT INLET VALVE ACTUATOR AND 14QH RELAY AND 18QH RELAY PER AMM 28-28-54. (SEE ALSO SDR AALA201608199001Valve · blownFUEL TRANSFER FAULT FOR NR 2 ACTUATOR INDICATES EMPTY & NR 1 ACTUATOR REFLECTS 5100 POUINDS. MAINTENANCE REPLACED 5QH1 ACT INLET VALVE ACTUATOR AND 14QH RELAY AND 18QH RELAY PER AMM 28-28-54. (SEE ALSO AALA201611049005 AND AALA201611049006).SDR 2016FA0000363B-Nut · brokenFUEL LINE FROM PRIMER SOLENOID TO THROTTLE BODY,BROKE IN HALF UNDER B-NUT, CAUSING THE ENGINE TO LOSE FUEL SUPPLY TO THROTTLE BODY.SDR 2016FA0000386Adapter · crackedTHE AIRCRAFT ARRIVED FOR UNRELATED MAINTENANCE WHEN IT WAS NOTED THAT A LARGE AMOUNT OF FUEL WAS EMANATING FROM THE BELLY AREA BETWEEN THE WHEEL WELLS. ACCESS WAS GAINED TO THE AREA BETWEEN THE WHEEL WELLS CONTAINING THE MAIN FUEL SHUTOFF VALVES. WITH BOOSTSDR 2016FA0000341Fitting · crackedNOTICED SLIGHT FLUCTUATING FUEL FLOW FROM FLIGHT. LANDED NORMALLY AND TAXI INTO TIE DOWN AREA. SHUTDOWN ENGINE AND EXITED THE ACFT AND REMOVED BAGGAGE. THE OTHER PILOT WITH ME WAS GOING TO TAKE AIRCRAFT BACK TO BASE. HE STARTED THE ENGINE AND I NOTICED FUE
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