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 FWTA20110830001Tube · chafedDURING ACFT REFUELING, APPEARANCE OF FUEL LEAK FROM NR 3 L/E SLAT OTBD CANISTER DRAIN. LOCATED LEAK; SLAT TRACK HOUSING DRAIN TUBE CHAFED THROUGH AND LEAKING.SDR CA110902006Shutoff Valve · intermittent(CAN) LT ENGINE NO START ON FIRST ATTEMPT. SHUTOFF VALVE CYCLED AND FOUND OPERATIVE. VALVE CHANGED AS PRECAUTION AND SENT FOR INSPECTION. O/H OF UNIT PERFORMED. INSPECT VALVES ON ACFT FLEET FOR ROUGH OR SLOW OPERATING VALVES. REPLACE NEXT HIGHEST TIME VALVSDR CA110831003Flex Hose · deteriorated(CAN) DURING REPAIR, FUEL WAS NOTED DRIPPING FROM THE BELLY OF THE ACFT. INSPECTION REVEALED THE FUSELAGE FUEL TANK GRAVITY TRANSFER FLEX HOSE ASSEMBLIES WERE SATURATED WITH FUEL, DRIPPING AT A SLOW BUT STEADY RATE. THIS WOULD HAVE BEEN MISSED ON A NORMAL DSDR UALA2011082404546Shutoff Valve · leakingFUEL LEAKING FROM OUTBD LT FUEL SHUTOFF ACTUATOR. FUEL LEAK ONLY PRESENT DURING FUELING PROCESS. REPLACED LT OTBD FUELING SHUTOFF VALVE PER MM. OPS CHECKS GOOD, NO LEAKS NOTED.SDR UALA2011081904410Actuator · faultyLEFT ENGINE START. LT SPAR LIGHT ON PED AND LT ENGINE VALVE LIGHT ON EICAS. P6 PANEL F1 CIRCUIT BREAKER POPPED. REPLACED THE SPAR VALVE ACTUATOR AND ELECTRICAL CONNECTOR DUE TO THE BACK SHELL BEING LOOSE. OPS CHECKED NORMAL. ALSO ACCOMPLISHED ELECTRICAL CONNESDR UALA2011081604343Tube · rupturedUNWANTED FUEL IN CENTER TANK DURING FUELING. WKRG SMC007, LOCATED & REMOVED RUPTURED SECTION OF FUELING MANIFOLD IN CENTER TANK. PART ON OSTF F2171 COMING FROM AA ORD ETA 1300 VIA STERLING. CENTER FUEL TANK CONTINUES TO TAKE FUEL WITH BOTH CENTER TANK FUEL SDR UALA2011081604344Valve · leakingFUEL TRANSFERRING FROM CENTER TO RIGHT TANK AT RATE OF 20LB EVERY 3 MIN. OPENED & VENTED RIGHT TANK, FOUND RIGHT TANK SUCTION VALVE LEAKING WITH CENTER PUMPS ON. REPLACED RT SUCTION VALVE.SDR UALA2011081504307Unknown · malfunctionedFUEL SYSTEM PROBLEM, FLIGHT DIVERTED. CENTER TANK PUMP 1 DID NOT COME ON 15 MINUTES INTO FLIGHT UNTIL AFTER THE AUTO FEED FAULT PROMPTED FLT CREW TO DESELECT AUTO FEED, PUTTING FEED SYS IN MANUAL. AUTO FEED FAULT ON ECAM AND PFR. DF STICKER APPLIED. ACCOMPSDR CA110817001Line · contaminated(CAN) NEW MAIN FUEL LINE DELIVERERD FROM HSI FOUND TO HAVE METAL CONTAMINATION INSIDE OF THE HOSE. COMPANY SQID11-07823 RASIED HSI INFORMED.SDR 2011FA0000521Restrictor · failedACFT WAS SQUAWKED FOR INSUFFICIENT FUEL TRANSFER OPERATION ON THE LT SIDE. BECAUSE THE PUMP WAS MAKING NOISE BUT THERE WAS MINIMAL FLOW, THE PUMP WAS REPLACED WITH AN O/H UNIT. THE O/H PUMP MADE THE SAME NOISE AND BEHAVED THE SAME. FURTHER TROUBLESHOOTING (ANSDR QMLA2011081111084Line · disconnectedPILOT REPORTED AFTER TAKEOFF THEY SMELLED FUEL ODOR IN CABIN. INSPECTED ENGINES AND AIRFRAME FUEL EXPANSION BOX FOR EVIDENCE OF FUEL AND LEAKS. NO LEAKS OR FUEL WERE FOUND. DURING INSP OF THE EXPANSION BOX THE OUTER DUCT AROUND THE LOWER FUEL VENT LINE WAS SDR C2XA11RI133Switch · out of positionFLIGHT 3129 - DTW - FLIGHT CREW REPORTED FUEL 1-2 LOW LEVEL, FUEL QTY 1-2 INDICATION DASHED. MX REPOSITIONED REFUEL TOGGLE SWITCH TO CLOSED POSITION AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR UALA2011080804145Float Valve · unsecureFUEL IMBALANCE. FUEL SYSTEM IS CONTINUALLY BEING WRITTEN UP FOR FUEL IMBALANCE. THE SCAVENGE SYSTEM HAS BEEN CHECKED ON CH1904 WITH NO FAULTS FOUND, PLEASE ACCOMPLISH A REFUEL-JETTISON & FUEL FEED MANIFOLD LEAK TEST WITH REFERENCE TO MM. IF REQUIRED MM FOR CSDR C2XA11RI141Fitting · looseFLIGHT 2887 - IAD - FLIGHT CREW REPORTED FUEL ODOR IN CABIN AND COCKPIT DURING TAXI AND PUSHBACK. IAD MX FOUND FITTING LOOSE ON LOW PRESSURE SWITCH. MX TIGHTENED FITTING AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR GLBA20110804GB-Nut · loosePILOT REPORTED THAT DURING INSP THE LT ENGINE WAS LEAKING FUEL. MX TIGHTENED A B-NUT AT THE ENG FMU FUEL OUTLET TUBE IAW EMM 73-21-00, LEAK CHECK GOOD.SDR GLBA20110804FTank · leakingPILOT REPORTED THAT DURING THE WALK-AROUND THERE WAS A FUEL LEAK ON THE LT ENGINE. MX CLEANED OUT THE EPA TANK, NO OTHER LEAKS FOUND, IAW EMM 71-70-01, OK FOR SERVICE.SDR CA110809005Fuel Cell · leakingFUEL LEAK FROM RT WING AFTER FUELING COMPLETE WHILE STILL ON THE GATE. BOARDING HALTED. MX INVESTIGATING. FUEL LEAKING OUT OF RT WING (OVERFLOWING FROM VENT) TRANSFERRED FUEL OUT OF L & R TANK TO CENTER. FUEL BALANCED. CAM FAULT "RIGHT WING TANK OVERFLOW", CSDR YENA20110726310Unknown · malfunctionedFLT 415 BOS-SAN, HAD AN AIR RETURN TO BOSTON DUE TO CENTER TANK PUMP 1 FAILED AFTER SLAT RETRACTED. PERFORMED OPS CHECK OF NR 1 CENTER TANK PUMP PER AMM 28-21-51. OPS CHECK NORMAL. SUSPECT IMPROPER CONFIGURATION OF AIRCRAFT DUE TO MEL 28-21-02 CONDITION 1 BSDR UALA2011072503773Actuator · malfunctionedLEFT ENGINE FLAMED OUT AFTER IT HAD BEEN STABILIZED AT IDLE. DURING NEXT START ATTEMPT, ENGINE REACHED 30 PERCENT N2 THEN FLAMED OUT WITH LT ENG FUEL VALVE EICAS MESSAGE. REPLACED LT SPAR VALVE ACTUATOR.SDR AALA20110725TUL09Circuit Breaker · failedDEN - INFLIGHT PDX-DFW. CREW REPORTED AFT CENTER BOOST PUMP, FORWARD LEFT WING FUEL BOOST PUMPS AND FUEL QUANTITY INDICATION FAILED. FLIGHT DIVERTED DEN LANDED WITHOUT INCIDENT. REPLACED AC BUS CONTROLLER AND RT BUS "B" PHASE CIRCUIT BREAKER. SYSTEM GROUNDSDR UALA2011072503786Valve · faultyUNABLE TO OPEN LT SIDE FUELING VALVES FOR FUELING. TROUBLESHOOTING FOUND LEFT WING BOTH REFUEL VALVE INOPERATIVE. MANUAL OPEN NO HELP. SWAPPED CENTER RIGHT REFUEL CONTROL VALVE WITH LT WING OUTBOARD. REFUEL CARRIED OUT CHECK LT WING OUTBOARD VALVE OK. REPSDR ASMF20110712Manifold · leakingDURING FUELING SERVICE, DETECTED A FUEL LEAK THROUGH THE ACFT FUEL MANIFOLD, MX TIGHTEN THE SCREWS IAW AMM 28-21-11 CORRECTING THE LEAK.SDR ASAA11510161Actuator · malfunctionedAFTER TOUCH DOWN DURING LANDING ROLL LT SPAR VALVE CLOSED LIGHT ILLUMINATED AND REMAINED ON. EXTINGUISHED SOME TIME AFTER SPEED BRAKE STOWED. REPLACED LT SPAR VALVE ACTUATOR REF MM 28 22 11 000 804 28 22 11 400 804 28 22 00 710 801. SYSTEM OPS CHECK GOOD. SDR CA110721010Hose · mismanufacturedNEW FUEL HOSES WITH INTERNAL METAL CONTAMINATION. LOT NUMBERS WERE 500517 AND 35178. THESE ARE THE LARGE DIAMETER MAIN FUEL FEED LINES FROM THE FUEL TANKS DIRECTLY TO THE ENGINE`S LT AND RT SIDES. THIS IS THE 2ND TIME WE HAVE RECEIVED FUEL LINES WITH METAL SDR ASAA11510152Actuator · faultyRIGHT SPAR VALVE CLOSED LIGHT ILLUMINATED DIM ENGINE INDICATIONS ALL NORMAL. CHECKED NR 2 ENG SPAR VALVE CB NORMAL PERFORMED ENG NR 2 SPAR VALVE FAULT ISOLATION REF 28 22 00 GROUND VERIFICATION NORMAL. FOLLOWUP TSR ISSUED. REPLACED NR 2 ENG SPAR VLV ACTUATOSDR A6WA201140611Transfer Valve · malfunctionedIN FLT, RECEIVED FUEL IMBALANCE CAS MESSAGE. FUEL WAS IMBALANCED UP TO 1100 LBS. ESTIMATED T/O FUEL WAS 4500 LBS EACH WING AND 2500 LBS IN CENTER TANK. DURING QRH, IMBALANCE WAS 3570 LBS LT WING, 1370 LBS CENTER TANK, AND 4390 RT WING. IMBALANCED INCREASEDSDR CA110719010Servo · leakingFUEL SERVO FOUND TO BE LEAKING DURING 100 HR INSP. FUEL SERVO REPLACED.SDR CA110729005Fuel Line · chafedRIGID ALUMINIUM FUEL LINE, FOUND CHAFED THRU APPROX HALF OF WALL THICKNESS. LOCATION - RT AFT DOOR FRAME LOWER CORNER AT BEND WHERE LINE IS ROUTED THRU FLOOR BULKHEAD AND CONTINUES THRU INSIDE OF LOWER DOOR FRAME.SDR UALA2011070703357Actuator · faultyFUEL SPAR VALVE L LEFT ENGINE FUEL SPAR VALVE IS NOT IN COMMANDED POSITION. (STATUS) - REPLACED LT FUEL SPAR VALVE ACTUATOR, OPS CHECK OK PER MM AND TEST PER 28-22 TASK.SDR UALA2011070103248Switch · faultyRIGHT CENTER TANK FUEL PUMP INOPERATIVE AND DEACTIVATED. REPLACED RIGHT CENTER TANK SWITCH, OPERATIONAL CHECK OF PUMP NORMALSDR FDEA201107012521Shroud · crackedAFT CARGO COMPARTMENT - TAIL TANK TRANSFER FUEL LINE SHROUD FOUND CRACKED AT STATION Y=2005 DURING CHECK. REPAIRED LINE, LEAK CHECK CARRIED OUT AS PER AMM 28-25-00-5 REV 70.0, NO LEAK FOUND. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 112.SDR ASAA1159964Actuator · failedNR 1 ENGINE WOULD NOT START, NO F/F. NR 1 FUEL SPAR VALVE LIGHT REMAINS CONSTANTLY ON SPAR VALVE NOT OPENING. REPLACED NR 1 SPAR VALVE ACTUATOR IAW AMM 28 22 11 000 804 AND 28 22 11 400 804 OPS CHECK GOOD IAW AMM 28 22 00 710 801.SDR AALA20110628TUL06Cover Plate · leakingTUL - INFLIGHT DFW-LGA. CREW REPORTED LEFT WING FUEL LEAK. EMERGENCY DECLARED FLIGHT DIVERTED TUL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND FUEL BOOST PUMP COVER PLATE SEAL LEAKING. REPLACED SEALS. SYSTEM GROUND CHECK NORMAL OPERATIONSDR AALA20110628TUL01Tube · brokenSDF - INFLIGHT EWR-DWF. CREW REPORTED THAT FUEL WAS NOT BEING SUPPLIED FROM THE CENTER TANKS WITH FUEL BOOST PUMPS SELECTED ON. EMERGENCY DECLARED FLIGHT DIVERTED SDF LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BROKEN FUEL TUBE ON BOOSSDR AALA20110624TUL06Plate · corrodedLEFT DEFUEL VALVE ACTUATOR ADAPTER PLATE FAILED RESISTANCE CHECK PER CARD F1553AD. INSTALLED LEFT DEFUEL VALVE PER M/M 28-22-01. INSTALLED DEFUEL VALVE ACTUATOR PER ECO F1553AD.SDR SWAA114527Valve · leakingABORTED TAKEOFF/DECLARED EMERGENCY. TOWER REPORTED FUEL STREAMING FROM RIGHT WING, FLIGHT ATTENDANTS CONFIRMED LEAK. COMPLIED WITH LEAK CHECKLIST, BY TURNING OFF CENTER FUEL PUMPS AND LEAK STOPPED. REMOVED AND REPLACED LT WING FUEL SHUTOFF VALVE AND CENTER SDR CA110621003Fuel Feed · malfunctionedWHILE TAXIING TO DEPART FROM STATION THE CREW REPORTED AN AUTO FUEL FEED FAULT AND RETURNED TO THE GATE. AS THE ACFT WAS RETURNING TO THE GATE GROUND PERSONNEL REPORTED FUEL LEAKING FROM THE RT WING TANK. NO EMERGENCY WAS DECLARED. AFTER ENGINE START AND TASDR CALA2011061600440Unknown · malfunctionedSTATUS MSG FUEL SPAR VALVE L SAME TIME AS NEXT WRITE-UP. FUEL SCHEMATIC SHOWED L FUEL SPAR VALVE CLOSED, BUT ENGINE RAN NORMALLY, NORMAL SHUTDOWN AT GATE. PER FIM TASK 28-22-00-810-840, MX MSG NOT ACTIVE, A/C OK TO CONTINUE.SDR UALA2011061302893Valve · failedCENTER TANK SCAVENGE SYSTEM TRANSFERED FUEL BEFORE MAINS REACHED 50000LB SAMC TEXT: FUEL SHEET NOTED WITH \NR 2 TANK VTO EARLY'. FUEL SCAVENGE SYS FUNCTIONALTEST IAW MM. FOUND BOTH OUTLET FLOAT VALVES FAILED OPEN. FUEL KEEPS SCAVENGING FROM CTR TANK TO BOTSDR SIMA201116002Unknown · malfunctionedON FLIGHT 2840 ON THE FINAL APPROACH THE CREW REPORTED A FUEL ODOR IN THE COCKPIT. THE FUEL TANK 2 QUANTITY ON EICAS AND THE MULTI FUNCTION DISPLAY SHOWED AMBER DASHES UNTIL GATE ARRIVAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SSDR ASAA1159736Unknown · malfunctionedFUEL IMBALANCE OCCURED DURING CRUISE (APPROX 1100LBS) WITH ALL MAIN FUEL TANKS PUMPS ON AND CROSSFEED CLOSED. COMPLETED QRH NO FUEL LEAK DETECTED. LEFT TANK WAS LOW FUEL SIDE DURING IMBALANCE. ACCOMPLISHED FUEL CROSSFEED VALVE FUNCTIONAL TEST REF MM TASK 28 SDR UALA2011052302522Valve · leakingPRIOR TO ENG START, RT WING STARTED LEAKING FUEL OUT OF VENT. MAINT TEXT: WITH RIGHT WING TANK FULL AND BOOST PUMPS RUNNING, FOUND FUEL LEAKING INTO VENT TANK THROUGH UPPER VENT HOLE IN VENT TANK. REPLACED RT WING SUCTION VALVE REF AMM, CHECKS GOOD.SDR GLBA20110516FCheck Valve · failedSIG EVENT - THE PILOT REPORTED THAT 600 LBS OF FUEL DRAINED FROM THE MAIN TANK TO THE AUX TANK (LT). MX REPAIRED BY REPLACING THE LT AUX FUEL LINE CHECK VALVE.SDR Q2SA2011F00081Valve · malfunctionedWITH NR 4 CROSS FEED VALVE INDICATING "OPEN", NR 4 TANK (QTY) WENT DOWN AS IF CROSSFEED VALVE WAS CLOSED. NR 4 TANK BOOST PUMP LOW PRESSURE LIGHTS DID NOT FLASH, ENGINE NR 4 FLAMED-OUT. DESCENDED TO FL 300 AND RECYCLED NR 4 CROSSFEED VALVE, ALL ENGINE INDICASDR 2011FA0000297Fuel Sys · contaminatedFLIGHT CREW REPORTED RT FUEL INDICATOR BOUNCES 700-800 LBS IN FLIGHT. NORMAL TROUBLESHOOTING SHOWED SYS NORMAL. REMOVED CONNECTOR PLUGS TO FUEL CONTROL RELAY PANEL, UNDER CTR FLOOR, AND FOUND WATER IN ALL PLUGS. NO INDICATION OF WATER POOLING IN FLOOR AND ALL SDR CA110509004Line · twisted(CAN) UPON PERFORMING LC-2 INSPECTION, MAINTENANCE FOUND FUEL LINE TWISTED ON LT ENGINE LOWER NACELLE.SDR CA110509008Valve · malfunctioned(CAN) DURING CRUISE OF FLT 2580, THE FUEL CROSSFEED VALVE CIRCUIT BREAKER POPPED. ACFT WAS DIVERTED INTO DUE TO THE AVAILABILITY OF MANPOWER AND PARTS. BONDING RESISTANCE CHECK WAS PERFORMED, CIRCUIT BREAKER WAS RESET AND SYS TESTED SERVICEABLE. THERE HAS BESDR UALA2011050202132Tube · leakingFUEL TRANSFERING FROM RT TANK TO CENTER APPROX 400LBS-HR. FOUND CRACKED FUEL FEED 'WYE' AT OUTPUT OF RIGHT OVERRIDE PUMP IN CENTER TANK. TUBE WAS TEMP REPAIRED. PUMP OPS CHECKED AND LEAK CHECKED GOOD. Y SUPPLY PIPE OFF RT CENTER TANK BOOST PUMP HOUSING REMOSDR DJFA2011018Fuel Sys · leakingCREW REPORTED STRONG FUEL SMELL IN THE AFT CABIN AREA. CREW FOUND FUEL DRIPPING FROM SEVERAL AREAS IN THE TAIL AND A STRONG FUEL SMELL IN THE AFT EQUIPMENT BAY. MAINTENANCE FOUND THE SEALS ON THE PRESSURE REDUCING VALVE FOR THE SINGLE-POINT REFULING (SPR) SYSDR MASA2011050202547Packing · damagedFUEL LEAKING FROM RT WING ROOT. R2 PACKINGS BEHIND ADAPTER HOSE.
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