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 CA131011005Shroud · corroded(CAN) THE FUEL SHROUD ASSY IN THE CARGO BAY UNDERFLOOR, LOCATED FS574.0, WAS FOUND CORRODED AND WAS LEAKING INTO THE BELLY INSULATION REF IPC 28-20-00, FIG 5, ITEM 105. THE CORROSION AT THE O-RING LOCATION WAS DETERIORATED TO THE POINT WHERE THE O-RING WOULD NSDR CALA2013100791790Valve · malfunctionedAFTER NR 1 ENGINE SHUTDOWN GOT FUEL SPAR VALVE STATUS MESSAGE WITH MESSAGE 2814001. REMOVED SPAR VALVE IAW MM 28-22-02. REPLACED ACTUATOR IAW EA 2820-1615 REV B & ECRA 2820-02085, ACCOMPLISHED EA 2820-1615 UP TO STEP 53. REQUIRE OP CHECK IAW MM 28-22-00 TASSDR CALA2013100891863Battery · faultyFUEL SHUTOFF VALVE BATTERY STATUS MSG. DEF IAW MEL. ACCOMPLISHED FIM 28-22 TASK 842, REPLACED ENG FUEL SPAR VALVE BATTERY IAW MM. OPERATIONS TESTED IAW MM, OPERATIONS NORMAL.SDR CALA2013100491738Proximity Switch · faultyCENTER FUEL PUMPS NOT TESTING CORRECTLY, NO CENTER LT OR RT FUEL PUMPS LIGHT ON TEST. ADJUSTED FUELING PNL PROX SW.SDR CALA2013100491732Valve · malfunctionedPRE-FLIGHT FUELING NR 3 TANK REFUEL VALVE FIRST CANNOT BE CLOSED CAUSED OVERFLOW FROM VENT PORT. FUEL DRAINING OUT RT VENT SCOOP FOLLOWING FUELING. PROBABLY AT SEVERAL GALLONS PER MIN. DRAIN OUT ALL RESIDUAL FUEL FROM RT SURGE TANK. ACCOMPLISHED RESET FUELSDR CALA2013100191625Valve · out of positionCREW REPORTED FUEL LEAKING FROM WATER DRAIN VALVE ON LT WING. UNABLE TO FUEL. REPOSITIONED VALVE NO LEAKS.SDR CA131001004Line · chafed(CAN) DURING ROUTINE MAINTENANCE A FUEL LEAK WAS NOTED AT THE NACELLE DRAIN LINE. INVESTIGATION FOUND THE FUEL LINE AND MOTIVE FLOW LINE CHAFFING AT THE SPLIT WASHERS WITHIN THE SHROUD IN THE DRY BAY. THE 2 FUEL LINES AND ASSOCIATED HARDWARE WERE REPLACED. FSDR CALA2013101692109Manifold · crackedFOUND FUEL MANIFOLD ASSEMBLY 344N2014-1 INSIDE 531BB WAS CRACKED. REMOVED FUEL MANIFOLD ASSEMBLY 344N2014-1. WELD REPAIRED FUEL MANIFOLD ASSEMBLY UNDER R & R 12429 IAW GPM 7-0-04-009. INSTALLED FUEL MANIFOLD ASSEMBLY IAW AMM 28-21-05. PRESSURE CHECKED GOODSDR CALA2013092791518Tube · rupturedUNWANTED FUEL TRANSFER INTO CENTER TANK WHILE FUELING WITH CENTER FUEL VALVE CLOSED. APPROXIMATELY 100 LBS OF FUEL RISE PER MIN WITH TRUCK SHOWING 40 PSI NOZZLE PRESSURE. PRESSURIZED FUELING MANIFOLD & FOUND TUBE ASSEMBLY 344N2014-1 RUPTURED INSIDE LT CENTERSDR DXTA2013092305513Actuator · inoperativeATTEMPTED FUEL TRANSFER TO BALANCE. POSITIONED SWITCHES TO STOP TRANSFER. FUEL CONTINUED TO TRANSFER OUT OF LT TANK. RAN PROCEDURE B OF FUEL QUANTITY ASYMMETRY CHECKLIST. X-BP LIGHT WOULD NOT EXTINGUISH. FUEL CONTINUED TO DEPLETE FROM LEFT TANK. RAN PROCESDR CALA2013092391375Circuit Card · faultyNR 2 FUEL CUTOFF SWITCH LIGHT INTERMITTENT DURING FIRE TEST. TEST FAILS WITH OVHT. REPLACED AFOLTS CARD & CLEANED FLT DESK TEST SW. TESTED ABOVE 4 TIMES PASSED.SDR ASOA20130922110RFitting · brokenNR 1 ENGINE SHUTDOWN INFLIGHT AND DIVERTED. MX INSPECTED NR 1 ENGINE AND FOUND MAIN FUEL LINE ADAPTER FITTING BROKEN. MX R & R FUEL LINE FITTING, LEAK AND OPS CHECKED SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.SDR DXTA2013091705508Float Valve · failedUPON LEVELING OFF AT FL400 "WING TANK O'FULL R" CAS MESSAGE DISPLAYED. COMPLIED WITH QRH AND NOTICED A LARGE AMOUNT OF FUEL EXITING RIGHT WING TIP AREA. AIRPLANE LOST APPROXIMATELY 600 LB OF GAS IN 10-15 MINUTES. FUEL LEAK STOPPED DURING EMERGENCY DESCENT ASDR ASAA2013091795995Actuator · failedNR 2 ENG WOULD NOT START, SPAR VALVE NR 2 CIRCUIT BREAKER OUT. ACFT GROUNDED. R & R NR 2 ENG SPAR VALVE ACTUATOR, IAW AMM 28-22-11/401, NR 2 ENG SPAR VALVE OPS CHECK AND GROUND VERIFICATION GOOD.SDR CA130916006Line · chafed(CAN) DURING THE ACCOMPLISHMENT OF TASK RJ2-57-900-320, INTERNAL ZONAL INSPECTION OF THE CENTER WING SECTION, THE STANDBY FUEL FEED SYS TUBE ASSEMBLY THAT JOINS THE 2 BOOST PUMPS IN THE CENTER WING TANKS WAS FOUND CHAFING ON THE CENTER FRAME AT APPROXIMATELY FSDR WRNA201309130013Actuator · inoperativeDURING CRUISE FLIGHT, THE CREW COULD NOT SHUT OFF FUEL FLOW TO THE UPPER AUX TANK. CREW DIVERTED DUE TO THE MALFUNCTION. FUEL WAS ADDED AND THE MALFUNCTION WAS TRANSFERRED TO DMI. TRAVEL WAS RESUMED. ONCE IN DESTINATION, THE AUX FILL VALVE ACTUATOR WAS REPSDR CALA2013090991133Switch · brokenFUELER REPORTS UNDERWING FUELING PANEL RT MAIN TOGGLE SWITCH IS BROKEN. REPLACED FUELING PANEL IAW MM.SDR CALA2013090490987Pressure Switch · faultyRT AFT FUEL BOOST PUMP NO PRESSURE LT WITH SWITCH OFF NO EICAS OFF MESSAGE. REPLACED PRESSURE SWITCH & CLEANED CONNECTOR IAW AMM. PRESSURE LIGHT WORKS OKAY.SDR CALA2013082890818Unknown · malfunctionedLEFT FORWARD FUEL PUMP EICAS WITH SWITCH ON. OK TO CONTINUE IAW 28 22A. LT FORWARD FUEL PUMP INOPERATIVE. CIRCUIT BREAKER COLLARED & INDICATOR BLACKED OUT, NEEDS TS. FOUND NO POWER AT CONN D1762. REPLACED RELAY K188 LT FORWARD FUEL BOOST PUMP & THEN POWESDR SIMA20130826005Line · leakingFUEL ODOR IN FLIGHT DECK AFTER APU & NR 1 ENGINE START. RETURNED TO GATE, R & R APU "OUT" FUEL LINE AT FUEL CONTROL, REF AMM 49-32-01. OPS CHECKED GOOD, NO LEAKS NOTED OR FUEL ODOR IN COCKPIT. FOUND GROUND CONNECTION VALVE SPRING BROKEN REF AMM 21-22-04. SDR CALA2013082090591Line · looseNR 2 ENGINE PYLON MAIN FUEL LINE AT BULKHEAD IS LOOSE. REMOVED FUEL LINE & BULKHEAD FITTING. FOUND CRACK IN PYLON WHERE FITTING IS ATTACHED. ACCOMPLISHED REPAIR ON CRACKED NR 2 PYLON STRUCTURE.SDR CALA2013081990512Line · leakingEXTREME STRONG ODOR OF FUEL IN CABIN. APPEARS TO BE CENTERED AROUND THE OVERWING AREA. REPLACED ALL HST FUEL LINES.SDR CALA2013081990519Sump · leakingFUEL SUMP LEAK. RESEATED LT CENTER FUEL SUMP, LEAK STOPPED.SDR CALA2013081490444Pressure Switch · inoperativeFOUND BROKEN SCREW ON FUEL PUMP MAIN GEAR ASSY, NR 2 ENGINE RT SIDE. R & R FUEL PUMP FILTER DIFFERENTIAL PRESSURE SWITCH.SDR ASOA20130812094Flapper Valve · leakingFUEL LEAK FROM LT WING REPORTED. MX R & R THE LT WING FLAPPER VALVE WITH LEAK CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130805090Flapper Valve · leakingAFTER TAKEOFF, FUEL REPORTED TO BE VENTING FROM LT WING. CREW PEFORMED UNEVENTFUL AIR TURN BACK. R & R LT WING FLAPPER VALVE AND LEAK CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR 7GMB2013092600131Valve · failedDURING CLIMBOUT ATC REPORTED FUEL VENTING FROM LEFT WING, FOLLOWED BY FUEL IMBALANCE EICAS MESSAGE. CONDUCTED AN AIR TURNBACK. LANDED SAFELY AND RETURNED TO GATE. 700 LBS OF FUEL WAS VENTED OUT FROM THE LT WING TANK. FOUND FUEL WAS COMING FROM LT PRESSURE FUESDR CALA2013072990040Solenoid Valve · failedFUELER REPORTS RT REFUEL VALVE WILL NOT OPEN NORMALLY. TRANSFERRED FUEL IAW AMM. VALVE OPENED AND FUEL TRANSFERRED INTO RT WING. WHEN FUEL TRUCK BECAME AVAILABLE AND PRESSURE FUELING WAS PERFORMED, IT WAS NOTED THAT THE RT REFUEL VALVE WAS SURGING. PRESSISDR AALA20130722005Clamp · disconnectedBNA INFLIGHT DFW-PHL CREW REPORTED WING FUEL IMBALANCE. EMERGENCY DECLARED FLIGHT DIVERTED BNA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND A DISCONNECTED FUEL LINE CLAMP IN THE CENTER TANK. RECONNECTED CLAMP. SYSTEM GROUND CHECKED NORMALSDR UALA2013072305174Valve · inoperativeRIGHT DEFUEL VALVE INOPERATIVE. REPLACED VALVE, CHECKED GOOD.SDR UALA2013071204871Warning Light · inoperativeDURING TROUBLESHOOTING FOR POSSIBLE UNWANTED FUEL TRANSFER PROBLEM IAW AMM, FOUND FUEL TRANSFER LIGHTS FOR LT AND RT POSITION INOPERATIVE DURING TRANSFER VALVE MOVEMENT. VALVE LIGHTS TEST OK BUT DO NOT WORK WITH OVERRIDE LEVER OPENING AND CLOSING.SDR UALA2013071104848Pressure Switch · malfunctionedLEFT FUEL PUMP LOW PRESSURE LIGHT DOES NOT COME ON. CLEANED AND INSPECTED LT CENTER FUEL PUMP PRESSURE SWITCH. ACCOMPLISHED FUEL PRESSURE INDICATING OPS CHECK.SDR UALA2013070504703Shutoff Valve · failedFUELER ADVISES CENTER FUELING VALVE NOT CLOSED. R & R LT AUX TANK FUEL SHUTOFF VALVE. ALL OPS NORMAL AT THIS TIME. NO LEAKS NOTED.SDR ASOA20130628335Pressure Switch · defectiveACFT WAS ON THE GROUND WHEN CREW SAW VISABLE SMOKE ON THE F/O SIDE OF ACFT. MX R & R THE NR 2 ENGINE FUEL LOW PRESSURE SWITCH IAW AMM 28-45-01, OPS CHECK GOOD IPC REFERENCE EMB 145 28-21-00, FIG 01 ITEM 110A. ACFT RELEASED TO SERVICE.SDR ASOA20130626065RPressure Switch · inoperativePILOT REPORTED VISIBLE SMOKE IN COCKPIT ON THE F/O'S SIDE WITH THE FUEL PUMPS ON. MX PERFORMED A DETAILED VISUAL INSPECTION IN THE COCKPIT AND NO SMOKE NOTED. R & R THE NR 2 ENGINE LOW PRESSURE SWITCH WITH OPS CHECK SUCCESSFUL.SDR HNAA2013062600359Solenoid Valve · leakingCREW NOTICED FUEL LEAKING OUT OF LT WING NACA SCOOPS. SHUTDOWN ENGINE. REMOVED FUEL LID PANELS 524AT AND 524CT. INSPECTED AUX PUMP CHECK VALVE. NO PROBLEM. R & R SOLENOID ARMING VALVE IAW MM 28-25-21. OPS CHECKED FUEL TRANSFER SYS. OPS AND LEAKED CHECKEDSDR EOPA201306260001Fuel Filter · leakingFUEL FILTER ASSY, PN 1743640-01, LEAKING FROM PRESS TO TEST BUTTON.SDR CA130626009Pressure Switch · stuck(CAN) THE MICROSWITCH SIDE OF THE FUEL FILTER/FUEL PRESSURE WARNING SYS ASSEMBLY IS STUCK IN THE CLOSED POSITION, CAUSING A FALSE FUEL PRESSURE WARNING INDICATION.SDR CA130627008Shroud · corroded(CAN) THE FUEL SHROUDS AND FUEL LINES WERE REMOVED FORM THIS ACFT THAT IS CURRENTLY DOWN FOR HEAVY MAINTENANCE. THERE IS NO MFG REQUIREMENT TO DISASSEMBLE THIS SYS FOR INSPECTION. ONCE AGAIN THE INSIDES OF THESE COMPONENTS WERE COVERED WITH A BLACK SUBSTANCE,SDR UALA2013062504388O-Ring · leakingNR 2 PYLON LEAKING FUEL FROM DRAIN AFT OF ENG TAILPIPE. FOUND FUEL RECIRCULATION CHECK VALVE LEAKING. REPLACED MATING SURFACE O-RING, NO LEAKS NOTED.SDR CA130715006Hose · leaking(CAN) UPON PARKING THE A/C AFTER A SCHEDULED COMMUTER FLIGHT, FUEL WAS SEEN DRIPPING FROM THE ENGINE COWL. NO ABNORMAL INDICATIONS OR PERFORMANCE ISSUES WERE NOTED DURING THE FLIGHT. SUBSEQUENT GROUND RUN REVEALED FUEL LEAKING FROM THE TUBE BETWEEN THE FUEL SDR CA130619006Line · chafed(CAN) THE AFFECTED FUEL LINE IS A .5 ALUMINUM TUBE THAT RUNS FORWARD FROM THE SELECTOR VALVE, UNDER THE RUDDER BARS, AND TO THE FIREWALL FITTING, ALL ON THE COPILOT`S SIDE. THE RT NOSEGEAR STEERING BUNGEE IS ACTIVATED BY A BELLCRANK ON THE RT RUDDER BAR, AND SDR UIEA2013061500328Shutoff Valve · malfunctionedDEPARTED WITH FUEL IN ALL THREE TANKS AND ALL PUMPS ON. AT TOP OF CLIMB NOTED THAT FUEL WAS BEING USED FROM LT MAIN TANK AS WELL AS CENTER TANK. THIS LED TO A FUEL CONFIG EICAS MESSAGE. COMPLIED WITH QRH PROCEDURE, FUEL TRANSFER FEED ON, LEFT PUMP OFF WHICHSDR CA130610015Line · leaking(CAN) THE PILOTS NOTICED A FUEL ODOR IN THE CABIN THAN NOTIFIED MAINTENANCE. THE CABIN ODOR WAS THE RESULT OF A LEAKING FUEL LINE LOCATED IN THE FUEL GALLEY AREA. THE PROBLEM WAS LOCATED IN FUEL BAY 5 FWD PUMP, WHICH WAS A RESULT FROM ARCING AT BOTH THE FUELSDR CALA2013082790787Control Unit · malfunctionedLEFT MAIN FUEL TANK REFUEL VALVES DID NOT SHUTOFF. LEFT TANKS HAD SHUT DOWN WITH STOP ON GAUGE & ALL VALVES CLOSED. AFTER TRANSFERRING FUEL FROM LT TO CTR & BACK AGAIN VERIFIED THAT WHEN CLOSING VALVES INBD TAKES A LONG TIME TO CLOSE & WHEN TRANSFERRING WITSDR 2013FA0000316Gascolator · looseDURING ANNUAL CONDITION INSPECTION, GASCOLATOR FILTER WAS NOT REMOVABLE, CUP COULD NOT BE SEPARATED FROM BODY. ENTIRE ASSY WAS REMOVED INCLUDING A MOUNTING BRACKET AND COOLING SHROUD. WHEN REMOVED, INLET TO GASCOLATOR HELD BY FOUR HEX-HEAD COUNTERSUNK SCRSDR E81R2013052970025Tube · disconnectedINVESTIGATED SOURCE OF FUEL STAINS NOTED ON RT WING INBD L/E INBD RT NACELLE AREA. FOUND RT ENGINE FUEL RETURN LINE TUBE ASSY. DISCONNECTED FROM FUEL RETURN LINE NACELLE FIREWALL BULKHEAD FITTING ON AFT (NACELLE) SIDE.SDR ALGA0528201330224Transfer Pump · inoperativeDURING CRUISE FLIGHT, FUEL CAUTION ILLUMINATED WITH BOTH TRANSFER PUMPS ON. LIGHT FLICKERED INTERMITTENTLY DURING FLIGHT.SDR USAA2013052800003Control Panel · intermittentENROUTE, LEFT FWD FUEL PUMP OFF EICAS MESSAGE AND PUMP LIGHT FAILED TO COME ON . FUEL INBALANCE OCCURED, LEFT SIDE USES MUCH MORE THAN RIGHT. FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. FOUND LEFT FWD FUEL PUMP PB INTERMITTENTLY DID NOT TURN PUMP OFSDR EOPA130529265Fuel Filter · leakingAIRFRAME FUEL FILTER, SEEMED FUNCTIONAL, NO NOTICABLE DEFECT. UPON POST FLIGHT INSPECTION, ENGAGED BOOST PUMPS, FUEL LEAKED PAST THE BYPASS PRESS-TO-TEST BUTTON. REPLACED THE AIRFRAME FUEL FILTER ASSY WITH SERVICEABLE ASSY.
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