JASC 2820
Service difficulty reports · 3,631
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 2004FA0000943Transducer · inoperativeFUEL FLOW TRANSDUCER INOPERATIVE-NOT PROVIDING SIGNAL TO IDU.SDR 20040820Check Valve · crackedFUEL SYSTEM CHECK VALVE PN 6-2255-44, HOUSING WAS FOUND CRACKED.SDR QXEA200400546Valve · leakingDURING POST FLIGHT FOUND FLUID ON OUTSIDE OF NR 1 ENGINE NACELLE. REMOVED AND REPLACED REFUEL/DEFUEL TRANSFER SHUT OFF VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR ASMF200407022Valve · failedDURING FUELING IN TRANSIT CHECK, FILLED FUEL CENTRAL VALVE FAILED. VALVE, TOTALIZER AND FUEL QUANTITY INDICATOR WERE CHECKED IAW MM 28-40-02, ALL CORRECT. DURING TRANSIT CHECK AT MEX VALVE FAILED AGAIN AND IT WAS REPLACED IAW MM 28-20-02, TEST CORRECT.SDR QXEA200400527Actuator · failedFLIGHT 2391-THE CREW WAS UNABLE TO TRANSFER FUEL IN FLIGHT, IN EITHER DIRECTION. THE NR 2 FUEL VALVE REMAINED CLOSED. MAINTENANCE INSPECTED THE AIRCRAFT SYSTEM AND REPLACED THE FUEL TRANSFER SHUT-OFF VALVE ACTUATOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFSDR JGV2004F00005Valve · crackedFUEL DRAIN SUMP UPRIGHT BAR IS CRACKED THRU LOWER SPOT WELD. FOUND DEFECT AFTER REMOVING SUMP DEBRI SCREEN. HIGH TEMPERATURE AT WELDING TIME. RECOMMEND NO SCREENS.SDR QXEA200400505Valve · leakingPDX - MAINTENANCE DISCOVERED A FUEL LEAK ON THE NR 2 NACELLE. THE LEAK WAS NOTED TO BE COMING FROM THE REFUEL - DEFUEL VALVE. THE VALVE WAS REPLACED. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR 2004FA0000773Line · chafedIN COMPLIANCE WITH MFG SL NR 419. FOUND FUEL LINE CHAFED OVER .5000 WAY THROUGH TUBE WALL. CAUSED BY FLAP ACTUATOR. CHAFE WAS NOT VISIBLE. FOUND BY FEELING. RECOMMEND MFG RUN LINE STRAIGHT THROUGH FUSELAGE WALL THEN ROUTE AFT. ALSO RECOMMEND MAKING INTO SDR WLDA200428Valve · failedAIRCRAFT N272WA FLT. NR WOA584 ON TAKEOFF ROLL, (TANK WING OVERFILL)LEVEL TWO ALERT, CREW ABORTED TAKEOFF TAXIED BACK TO THE GATE. MECHANIC FOUND NR 1 FILL VALVE FAILD, REPLACED THE VALVE SYSTEM CHECK NORMAL.SDR DL757040534Connector · failedWORKING MCO RT AFT MAIN FUEL PUMP INOPERATIVE. FOUND RT AFT SPAR MOUNTED CONNECTOR D40930P BURNED AND ARCING. REPLACED CONNECTOR D40930P, OPS CHECK OK.SDR CA040610010Line · corroded(CAN) FUEL LINE ASSEMBLY LOCATION/LOCATED UNDER FLOOR AND UNDER CENTER CONSOLE. THIS LINE IS DIRECTLY FORWARD OF THE BELLY DRAIN. IT IS UP STREAM FROM THE GASCOLATOR AND DOWN STREAM OF THE FUEL SHUT-OFF. FUEL SMELL WAS DETECTED. FUEL STAINING WAS PRESENT. THSDR CHQA000502Valve · leakingDURING CLIMBOUT OF MCO, LIQUID WAS SEEN LEAKING FROM THE TRAILING EDGE OF THE RIGHT WING. RETURNED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RT TANK VENT VALVE. FURTHER INVESTIGATION REVEALED THAT THE FLAPPER VALVE TO RIGHT DRSDR ASMF200405021Valve · leakingDURING REFUELING A FUEL LEAK WAS DETECTED IN LT MAIN GEAR DOOR. LT CENTRAL TANK VALVE WAS DETECTED WITH LEAK AND FUEL VALVE WAS REPLACED IAW MM 28-10-00, TEST CORRECT.SDR 2004FA0000428Line · inadequateUPON INSPECTION OF VALVE LINE SEVERAL LOCATIONS WERE FOUND WHERE THE INNER KEVLAR LINE HAS BUNCHED UP AND BECAME EXPOSED THROUGH THE OUTER PROTECTIVE NYLON COVER. THIS WAS FOUND IN VARIOUS PLACES ALONG LENGTH OF LINE. EACH OF THE PEA SIZED EXPOSED AREAS HAVESDR NZZ2004F00000Hose · looseEXPERIENCED AN ENGINE FIRE DUE TO LOOSE FIREWALL TO FUEL PUMP INLET HOSE. HOSE LEAKED WHEN PRESSURIZED BY FUEL BOOST PUMP. ON TAXI OUR, ENGINE RAN ROUGH (AIR LEAKING). PILOT HIT BOOST PUMP, MOMENTAIRLY ENGINE SMOOTHED OUT AND CAUGHT FIRE. DAMAGE MOSTLY TO SDR CA040420007O-Ring · leaking(CAN) DURING ROUTINE WALK AROUND , MAINTENANCE DISCOVERED FUEL LEAK AROUND RT WING DRYBAY DRAIN. DRY BAY PANELS WERE REMOVED AND DRY BAY FOUND TO HAVE SMALL AMOUNT OF FUEL PRESENT. THE COUPLING THAT ATTACHES THE AIR SCOOP TO THE FUEL TANK VENTLINES ON THE RTSDR AUS20040286Gascolator · contaminated(AUS) ENGINE FAILED. INVESTIGATION FOUND WATER AND RUST IN THE AIRCRAFT FUEL FILTER GASCOLATOR AND CARBURETOR.SDR AALA20040428Pump · inoperativeDFW - INFLIGHT T1118 FUEL WOULD NOT FLOW FROM CENTER TANK AND ALL THREE AFT CENTER PUMP CIRCUIT BREAKERS WERE POPPED. LANDED WITHOUT INCIDENT AT DFW. RESET CIRCUIT BREAKERS, RAN PUMP AND TRANSFERRED FUEL. COULD NOT DUPLICATE. SYSTEM GROUND CHECKED NORMAL SDR RYNA2075O-Ring · faultyDURING CRUISE FLIGHT (FUEL CONFIG) LIGHT ILLUMINATED AND THE EICAS ADVISORY MESSAGE (FUEL CONFIG) WAS DISPLAYED. ACCOMPLISHED THE FUEL CONFIGURATION CPM PROCEDURES AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED MANIFOLD (O-RING) IN PYLON AT STATION 287.9.SDR AUS20040235Seal · faulty(AUS) REFUEL/DEFUEL VALVES NOT CLOSING CORRECTLY ALLOWING AIR TO BE DRAWN INTO ENGINE FUEL SYSTEM. INVESTIGATION FOUND THE SEALINGWASHERS INSIDE THE VALVE ASSEMBLIES TO BE DEFECTIVE.SDR 0401595656Fuel Line · chafedTHE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EA 56-197969. OPERATIONAL CHSDR 2004FA0000395Servo · inoperativeFUEL MIXTURE CONTROL ARM WILL NOT ROTATE TO (IDLE CUT-OFF) POSITION.SDR QXEA200400221Fuel Sys · unknownDEN - FLIGHT 4183 - ON TAKEOFF CLIMBOUT, FUEL MIGRATED TO THE CENTER TANK IN EXCESS OF 500 POUNDS. FUEL LEVEL RETURNED TO ZERO IN THE CENTER TANK WITHIN 5 MINUTES. MAINTENANCE INSPECTED THE SYSTEM AND FOUND NO FUEL LEAKS OR MIGRATION TO THE CENTER TANK. OPESDR CA040319005Line · chafed(CAN) DURING THE INSP PROCESS OF SB550-28-14, WING FUEL BOOST PUMP WIRING INSPECTION, IT WAS NOTED THAT BOOST PUMP WIRING WAS RUBBING ON MAIN EJECTOR TO CHECK VALVE ALUMINUM FUEL LINE P/N 6526355-37, CAUSING CHAFFING WEAR THROUGH FUEL LINE. THE WEAR WAS APPROXSDR AUS20040176Check Valve · faulty(AUS) FUEL SYSTEM CHECK VALVE SUSPECT FAULTY.SDR QXEA200400193Ejector · leakingPDX - FLIGHT 2555 - CREW NOTED THE CENTER TANK FILLING WITH FUEL. MAINTENANCE INSPECTED THE AIRCRAFT SYSTEM AND FOUND THE LEFT PRIMARY EJECTOR BAD. THE LEFT PRIMARY EJECTOR WAS REPLACED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CA040319003Valve · malfunctioned(CAN) CREW REPORTED SEVERAL INCIDENTS OF UNEXPLAINED FUEL LOSS FROM RT FUEL SYS RESULTING IN INCONSISTENT FUEL IMBALANCES ON VARIOUS OCCASIONS. NO VISIBLE SIGNS OF FUEL SYS LEAKAGES WITHIN ACRFT NOR ON GROUND. FUEL QTYS CLOSELY MONITORED BY CREW WHILE TROUBLESDR DL757040214Valve · malfunctionedFUEL LEAKING AT GOOD RATE OUT OF RIGHT WING TIP. SECURED ALL FUEL PUMPS. NOTICED FUEL HAD TRANSFERRED FROM LEFT MAIN TO RIGHT MAIN TANK. FOUND RT ENGINE SPAR VALVE BODY CRACKED. REPLACED VALVE, CHECKS OK.SDR KBM2004F00172Pressure Switch · inoperativeFUEL PUMP LIGHT WILL NOT EXTINGUISH. REMOVED AND REPLACED FUEL PRESSURE SWITCH.SDR GLBA20030569Line · leakingFUEL LINE PN 118920000330 CHAFED ON ACM DUCT ASSY COUPLING CREATING A FUEL LEAK, CHANGED FUEL LINE AND REPOSITIONED DUCT COUPLING AND SPIRAL WRAPPED FUEL LINESDR QXEA200400167O-Ring · leakingPDX - A FUEL LEAK WAS NOTED ON THE NR 2 NACELLE AND APPEARS TO BE NEAR THE FUEL DOOR. MAINTENANCE REPLACED THE O-RINGS AT THE MASTER REFUEL/DEFUEL SHUTOFF VALVE AND ABOVE THE FILLER PORT. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SSDR QXEA200400169Pin · backed outPDX - FLIGHT 2543 - WHEN SELECTING RIGHT BOOST PUMP ON, NEITHER THE RIGHT OR LEFT BOOST PUMPS TURN ON. WHEN SELECTING LEFT BOOST PUMP ON, SYSTEM OPERATES NORMALLY. MAINTENANCE INSPECTED THE FUEL SYSTEM AND FOUND AN OPEN WIRE FROM THE FUEL CONTROL PANEL TO K5SDR CA040220006Line · chafed(CAN) FUEL LINE WAS FOUND CHAFED DURING 200 HR INSPECTION.SDR BAQA092790Manifold · inoperativeNR 1 ENGINE NOT LIGHTING OFF ON ALL START ATTEMPTS. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/19/2004SDR BAQA092789Manifold · inoperativeNR 1 ENGINE WILL NOT LIGHT OFF ON ALL START ATTEMPTS. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/19/2004SDR BAQA092788Manifold · failedNR 1 ENGINE NOT LIGHTING OFF ON ALL START ATTEMPTS. REPLACED WITH SERVICABLE UNIT. 02/19/2004SDR 2004FA0000187Tube · chafedCOMPLETING CESSNA SB, WE FOUND BOOST PUMP WIRING CHAFING INTO FUEL TUBE. THE TUBE WAS CHAFED BEYOND LIMITS IAW SB. THERE IS POTENTIAL OF SPARKING IN THE FUEL BAY AREA IF THE BOOST PUMP WIRES SHORTED TO THE TUBE CAUSING A FIRE. THE BOOST PUMP WIRING HAD SOME SDR CA040127018Line · leaking(CAN) DURING START UP, PILOT NOTICED FUEL ODOR IN CABIN SHORTLY AFTER ENGINE START UP. MAINTENANCE WAS NOTIFIED AND AFTER INSPECTION IT WAS NOTED A FINE MIST FROM RT FLEXIBLE FUEL PRESSURE LINE. HOSE WAS REPLACED WITH NO FURTHER PROBLEMS.SDR MALA040166Pressure Switch · leakingFLIGHT ATTENDANT COMPLAINED OF JET FUEL SMELL IN GALLEY AND ROW 1 AREA, THROUGHOUT FLIGHT FROM DSM TO MSP. MAINTENANCE UNABLE TO DUPLICATE SQK. NO ABNORMAL SMELL OR ODOR NOTED IN CABIN OR COCKPIT WITH BLEED SYSTEM ON. INSPECTED WING AREA AND ENG COMPARTMENTSDR 2004UALA00417Warning System · activatedFUEL CONFIGURATION LIGHT ON 1 HOUR INTO FLIGHT. FUEL IMBALANCE.SDR JIKA200400002Check Valve · stuckRT ENG WOULD NOT SHUT-OFF WITH CONDITION LEVER IN CUT-OFF POSITION. ATTEMPTS WERE MADE TO SHUT ENG DOWN WITH CONDITION LEVER; ENG WOULD NOT SHUT-OFF. PILOT CLOSED FUEL SHUT-OFF VALVE, ENG WOULD NOT SHUT DOWN. SHUT ENG DOWN BY MANUALLY MOVING FUEL CUT-OFF VASDR CA040108007Valve · inoperative(CAN) DURING REFUELING, FBO LINE CREW FAILED TO CARRY OUT SINGLE POINT REFUELING PRE-CHECK. DURING FUELLING, ONLY LT TANK WAS FILLED (RT REFUELING VALVE APPARENTLY FAILED IN THE CLOSED POSITION). BY THE TIME THE FLIGHT CREW NOTICED THE DIFFICULTY A SIGNIFICANTSDR 7011203Connector · looseAIRCRAFT WAS IN FOR AN ANNUAL INSPECTION. A FUEL LEAK WAS NOTED AS A DISCREPANCY. FURTHER INVESTIGATION REVEALED THAT THE ORIGIN OF THE LEAK WAS COMING FROM A HOSE/BULKHEAD FITTING CONNECTION ON THE FIREWALL. THE HOSE B-NUT WAS FOUND TO BE FINGER TIGHT. THE FISDR A8O2004F00000Line · leakingFUEL SYSTEM/FUEL DUMP SYSTEM AFFECTS FUEL FLOW OR LEAKAGE DURING FLIGHT. EMERGENCY ACTION TAKEN DURING FLIGHT DUE TO A COMPONENT OR SYSTEM MALFUNCTION. UPON ROTATION, THE LEFT FUEL FILTER LIGHT CAME ON. THE CREW ACTED FOLLOWING THE EMERGENCY PROCEDURE, DECLSDR MEX2003549Adapter · leakingTHE DISPENSER FUEL NOZZLE WAS REMOVED INADEQUATELY AFTER THE FUEL REFILLING SERVICE, THE ADAPTER CHECK VALVE SEAL WAS REMOVED AND A LITTLE FUEL LEAKAGE APPEARED. SUCH SEAL WAS REINSTALLED AND NO LEAKAGES APPEARED AGAIN. THE FUEL FILL ADAPTER WAS REPLACED ANDSDR DHL2003805013Warning Light · illuminatedIN FLIGHT WHEN ATTEMPTING TO TRANSFER FUEL TO NR 3 TANK, NR 3 MAIN SHUTOFF LIGHT INITIALLY AND RE-ILLUMINATED IN FIVE SECONDS WITH FILL VALVE IN OPEN POSITION AS A RESULT FUEL CANNOT BE TRANSFERRED TO NR 3 TANK. ABNORMAL PROCEDURE COMPLETED DID NOT CORRECT PRSDR 2004F00040Line · chafedFUEL FOUND LEAKING FROM LT ENGINE AFTER SHUTDOWN. VISUAL INSPECTION, FOUND CHAFED LINE. FUEL LINE REPLACED ON NR 1 ENGINE IAW J-31 AMM 20-10-00. VISUAL LEAK CHECK CARRIED OUT IAW J-31 AMM 51-11-00. FOUND SERVICEABLE P/N 3108051-1, ALSO FUEL FLEX LINE ON NRSDR CA031211001Line · corroded(CAN) FUEL LINE HAD A ROUGH LOOK TO THE SURFACE. THE FUEL LINE WAS ACCESSED BY REMOVING CENTER CONSOLE COVER AND PEELING BACK CARPET. CLOSER EXAMINATION OF LINE REVEALED CORROSION PITS AND RESIDUE THAT WAS DETERMINED TO BE CAUSED BY THE FUEL LINE CONTACT WITHSDR AWXA200301525Line · chafedLAS - FUEL LEAK - DURING B-3 CHECK FUEL WAS FOUND DRIPPING FROM RT ENGINE PYLON AFT DRAIN LINE, UPON FURTHER INVESTIGATION A FUEL LEAK WAS FOUND ON RT ENGINE FUEL FEED LINE AT 90 DEGREE ELBOW APPROXIMATELY 2 INCHES FROM ADEL CLAMP UNDER THE HOT AIR BLEED DUCT SDR CA040817001Line · cracked(CAN) FOUND A CRACK ON FLARE OF FCU SUPPLY LINE FROM FUEL PUMP. REPLACED LINE ON SITE WITH REMOVED SERVICEABLE UNIT FROM ANOTHER AIRCRAFT. LEAK CHECK C/O AND AIRCRAFT RETURNED TO SERVICE.
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