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 QXEA200500115Actuator · failedFLT RETURNED TO FIELD WHEN THE CREW WAS UNABLE TO TRANSFER FUEL FROM THE RIGHT TANK. MAINTENANCE INSPECTED THE SYSTEM AND THEN REPLACED THE REFUEL/DEFUEL SHUT-OFF VALVE ACTUATOR ASSEMBLY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR QXEA200500119Valve · leakingPDX - DURING A MAINTENANCE WALKAROUND FUEL WAS FOUND LEAKING FROM THE SINGLE POINT REFUELING VALVE DRAIN HOLE. THE AREA WAS INSPECTED AND THE REFUEL / DEFUEL ADAPTER WAS REPLACED. OPERATIONAL AND LEAK CHECKS WERE PERFORMED AND ALL WERE GOOD. THE AIRCRAFT WASDR ASMF200501006Valve · leakingDURING FUEL SERVICE WAS DETECTED HIGH SUPPLY PRESSURE ON FUEL DISPENSER (80 PSI), PROMOTING FUEL LEAK ON RT CENTRAL TANK VALVE. AIRCRAFT WAS FUELED THROUGH LT VALVE AND RT VALVE WAS DEFERRED IAW MEL 28-21-1. DURING OVERNIGHT SERVICE RT FUEL VALVE WAS REPLACED SDR CA050112004Tube · chafed(CAN) UPON INSPECTION OF THE FUEL TRANSFER PRESSURE SWITCH, IT WAS NOTICED THAT ONE OF THE ENGINE CONTROLS WAS RUBBING AGAINST THE MAIN FEED LINE TO THE RT NAC TANK. REPLACED TUBE ASSY AND TIED BACK TELEFLEX CABLES TO PREVENT FURTHER RUBBING.SDR P5CA0401292Valve · dirtyENGINE NR 2 FUEL VALVE MSG FUEL SPAR VLV 2 STATUS MSG. REMOVED NR 2 FUEL SPAR VALVE. CLEANED SHAFT AND REINSTALLED SPAR VALVE. OPERATION CHECKS OK PER MM 28-22-01.SDR CA041224009Fuel Sys · malfunctioned(CAN) AFTER DEPARTURE DURING CRUISE, A FUEL UNBALANCE WAS NOTICED AND LEAK SUSPECTED FROM NR 1 ENGINE. ENGINE NR 1 WAS SECURED AND AIRCRAFT LANDED BACK TO DEPARTURE AIRPORT. BOTH ENGINES WERE RAN AND NO LEAK WAS FOUND. THE AUTO FEED SYSTEM WAS PUT INOPERATISDR CA041224002Ejector · cracked(CAN) OVERNIGHT, APPROX 1200 LBS OF FUEL TRANSFERED INTO THE CENTER TANK. THE FLT HAD REPORTED AN INCREASE OF 120 LBS IN 10 MINUTES, HOWEVER IT WAS NOT DETERMINED IF THE FUEL TRANSFER WAS NOTED ON GROUND OR IN FLT BY THE CREW. MAINTENANCE FOUND THE LT MAINSDR QXEA200400018Line · chafedLT HAND WING FUEL BAY AT 522CT, HAS TWO FUEL LINES RUBBING IN TANK YW1545. REPAIRED IAW AMM 28-21-06 AND HORIZON AIR EA 6-28-20.SDR MASA200400707Warning Light · illuminatedASH 2827 FROM ROC TO CLT ABORTED TAKEOFF DUE TO A FUEL IMBALANCE CAUTION MESSAGE. CONTRACT MAINTENANCE TRANSFERRED FUEL AND OPS CHECKED THE FUEL TRANSFER SYSTEM OPS GOOD. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT.SDR 2005FA0000085Fuel Line · splitAIRCRAFT DEPARTED BGR, TEMPERATURE THE PREVIOUS RIGHT AND DAY WERE CLOSE TO FREEZING. AIRCRAFT RETURNED WITH FUEL SMELL IN COCKPIT. INVESTIGATION FOUND LT FUEL CROSSFEED LINE HAD SPLIT. UPON REMOVAL OF LINE, PRESENCE OF WATER WAS FOUND. PROBABLE CAUSE WAS SDR QXEA200400882Fuel Line · chafedPDX - FUEL FEED LINE INSIDE LEFT WING PANEL 523AT IS CHAFED BY EJECTOR MOTIVE FLOW LINE. REPAIRED IAW HORIZON AIR EA 6-28-14.SDR CWQR200400006Tube · crackedAIRCRAFT WAS LEAKING FUEL. TECHNICIAN FOUND A 1.3 INCH CRACK IN -Y- TUBE IN PRESSURE REFUELING SYSTEM. NO EVIDENCE OF DAMAGE TO TUBE ASSY. REPLACED TUBE ASSY, AND LEAK CHECKED GOOD.SDR CA041129012Hose · cracked(CAN) AIRCRAFT ON TRAINING FLIGHT. PILOT REPORTS STRONG FUEL ODOR IN COCKPIT. INVESTIGATION REVEALED LT FUEL PRESSURE FLEXIBLE HOSE TO GAUGE LEAKING FROM UNDER HOSE FITTING SOCKET WHEN FUEL BOOST PUMP TURNED ON. THIS FUEL LEAK WAS A FINE MIST SPRAY. HOSES WESDR UPS04M43464Isolation Valve · inoperativeAT APPROX 4 HRS AFTER DEPARTURE, THE FUEL QTY/USED CHECK LEVEL 2 ALERT DISPLAYED. OBSERVED THAT FUEL TANK QUANTITY WAS APPROX 5000 LBS LESS THAN FUEL BURN AMOUNT FROM FUEL TOTALIZER. ISOLATED ALL TANKS AND OBSERVED THAT TAIL TANK QUANTITY CONTINUED TO DECREASDR AALA20041092Pressure Switch · inoperativeFUEL ANOMALY WITH CROSSFEED VALVE OPEN AND ONE LEFT FUEL PUMP OFF. FUEL IS BURNED FROM RIGHT TANK ONLY. ATTEMPTS TO TURN OFF BOTH LEFT PUMPS RESULTS IN LEFT LOW PRESSURE LIGHT ILLUMINATED. LANDED RDU WITHOUT INCIDENT. CHECKED FUEL CROSSFEED FROM LEFT TO RISDR P5CA0401270Fuel Sys · leakingA/C RETURN TO BLOCK DUE TO FUEL GOING OVERBOARD FROM RIGHT WING VENT BOX. DRAINED SURGE TANK, CHECKED FUELING SYSTEM PER AMM 28-21-00, CHECKS NORMAL WITH ALL PUMPS RUNNING & FUELING DUCTS PRESSURIZED.SDR COMA0460593Pump · malfunctionedFLIGHT 4973 FUEL INBALANCE CAUTION MESSAGE. REPLACED THE CROSS FLOW PUMP.SDR GUU2004F00039Line · leakingDURING FLIGHT, STRONG EXHAUST ODOR PRESENT IN AIRCRAFT WITH BLEED OPEN. REMOVED AND REPLACED FUEL LINE AT LT ENGINE COMPRESSOR INLET. OPERATIONAL CHECKS NORMAL. NO SMELL NOTED.SDR P5CA0401263Fuel Cell · overservicedFUEL SPILL RIGHT WING. FOUND NR 4 MAIN OVER FILLED. DRAINED RIGHT SURGE TANK IAW 28/21/00, RESET SYSTEM & CONTINUED FUELING. CHECK OF VOLUMETRIC SYSTEM IAW 28-21-00 SATISFACTORY.SDR GTIA040819Line · chafedSTRONG FUEL SMELL IN CABIN WITH APU RUNNING. ITEM TRANSFERRED TO DMI 02911151 IAW MEL 49-1-0. CAT (C). PLACARD INSTALLED. FOUND FUEL LINE ON FUEL HEATER (APU) CHAFED THROUGH, REMOVED LINE AND ROUTED LINE SO IT DOES NOT CHAFE, LEAK CHECK GOOD.SDR DXTA200400417Warning Light · illuminated"WING O FILL R" AMBER LIGHT CAME ON IN FLIGHT, LOST ABOUT 400 LBS OF FUEL. INSPECTED RIGHT WING OUTBOARD TRANSFER VALVE. NO DEFECTS NOTED. PERFORMED FUEL TRANSFER SYSTEM SHUTOFF TEST. FOUND ALL OPERATION NORMAL. NO FURTHER ACTION TAKEN. WORK PERFORMED IASDR 04FDEA02846Line · crackedCENTER CARGO COMPARTMENT, LEFT SIDEWALL AREA AT APPROXIMATELY AT STA Y= 1801, A CRACKED OF 1 1/4 INCH FOUND AT THE FUEL SHROUD LINE. CENTER CARGO COMPARTMENT, LEFT SIDEWALL AREA AT APPROXIMATELY AT STA Y= 1801, 1 1/4 INCH CRACKED AT THE FUEL SHROUD LINE REPAISDR 04FDEA02845Line · crackedCENTER CARGO COMPARTMENT, LT SIDEWALL AREA AT APPROXIMATELY AT STA Y= 1781, A CRACKED OF 1.1/8 INCH FOUND AT THE FUEL SHROUD LINE. CENTER CARGO COMPARTMENT, LEFT SIDEWALL AREA AT APPROXIMATELY AT STA Y= 1781, 1 1/8 INCH CRACKED AT THE FUEL SHROUD LINE. REPAISDR 04FDEA02818Tube · crackedLEFT WING LEADING EDGE UPPER PYLON FUEL SAXAPHONE LINE IS CRACKED AT MOUNTING POINT. REMOVED, REPAIRED, REINSTALLED FUEL LINE IAW FEDEX EA 8-2822-77635.SDR 0401735801Line · chafedTHE FUEL SUPPLY TUBE IN THE RT 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 IAW EO 2822-01068-01. OPERATIONAL CHESDR 0401765814Fuel 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 EO 2822-01068-01. OPERATIONASDR 0401745813Line · chafedTHE FUEL SUPPLY TUBE IN THE RT 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 IAW EO 2822-01068-01. OPERATIONAL CHESDR 0401755810Fuel 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 EO 2822-01068-01. OPERATIONASDR 0401715655Line · chafedTHE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 12N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-01068-01. OPERATIONALSDR 0401705803Line · 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 EO 2822-01068-01. OPERATIONASDR 0401695808Line · 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 EO 2822-01068-01. OPERATIONASDR 0401685802Line · 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 EO 2822-01068-01. OPERATIONASDR 0401675815Line · 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 WAS WITHIN ALLOWABLE LIMITS. REPAIRED PER EO 2822-01068-01. OPERATIONAL CHECK GOOD.SDR 0401655809Line · chafedTHE 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 EO 2822-01068-01. OPERATIONAL CHESDR 0401665802Line · 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 EO 2822-01068-01. OPERATIONASDR 0401645811Line · 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 EO 2822-01068-01. OPERATIONASDR CA050221002Seal · cracked(CAN) DURING FLIGHT FUEL FUMES ENTERED IN THE AIRCRAFT CABIN. AFTER LANDING 3 PAX WERE TAKEN TO THE HOSPITAL DUE TO FEELING SICK FROM THE FUMES. FUEL CAP WAS SUSPECTED TO BE LEAKING WHICH CAUSED THE FUEL TO ENTER THE CABIN THRU THE PAX DOOR SEAL. FUEL CAP WSDR 0401635806Fuel 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 58-199805. OPERATIONAL CHSDR 0401605657Fuel 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 56-199804. OPERATIONAL CHSDR 0401625804Fuel 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 58-200233. OPERATIONAL CHSDR 0401615807Fuel 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 58-200472. OPERATIONAL CHESDR 0401565816Fuel 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 58-200234. OPERATIONAL CHSDR 2004FA0000818Hose · looseLOST POWER ON TAKE OFF, APPROXIMATELY 100 FT IN THE AIR AT 100 MPH, HALFWAY DOWN RUNWAY. LANDED AT 10 FEET AT END OF RUNWAY. AIRCRAFT TAKEN BACK TO HANGER, REMOVED ENGINE COWL (TOP). NOTE: ENGINE PRIMER LINE TO LEFT AFT CYLINDER BROKEN. HOSE ASSEMBLY (CARSDR DHL2004801537Control Box · crackedITEM REF. NR. 1349: RT WING NR 4 ALT TANK FUEL LEVEL CONTROL BOX CRACKED. REMOVED AND REPLACED FUEL LEVEL CONTROL BOX ASSY ON RT WING NR 4 ALT TANK IAW MM 28-21-15 PG. 201-203.SDR DXTA200400395Check Valve · leakingA STRONG FUEL SMELL WAS NOTED IN THE CABIN WHILE AT CRUISE. FOUND PRE-CHECK VALVE LEAKING, INSTALLED NEW VALVE WITH NEW PACKINGS IAW MM CHAPTER 28-22-00. OPS CHECKS AND LEAK CHECKS GOOD.SDR 2004UALA00836Valve · inoperativeNR 2 CROSS FEED VALVE CLOSED AND UNABLE TO USE FUEL IN NR 2 RSV TANK. VALVE BODY COULD NOT BE DRIVEN OPEN BY THE ELECTRICAL ACTUATOR. VALVE BODIES ARE FLOWN TO FAILURE. THERE HAVE BEEN TWO OF THESE VALVE BODIES REPLACED IN THE LAST 12 MONTHS WITH AN MTBUR OSDR GTIA040745Line · leakingLGA - DRAINED FORWARD AUX TANK DUE TO FINDING FUEL IN SHROUD DRAIN. LOCATED LEAK AT INLET MANIFOLD LINE, REMOVED AND REPLACED O-RINGS. GTIA (M)SDR 2004FA0000759Line · leakingIT APPEARS THAT THE FUEL LINE WAS LEAKING FUEL AT THE ATTACH POINT OF THE STEEL BRAIDED LINE TO THE FITTING. THE FUEL LINE IS ATTACHED AT THE FIRE WALL AND GOES TO THE INLET SIDE OF THE ENGINE DRIVEN FUEL PUMP. (CE07200416055)SDR SWIA200413718Pump · obstructedSITTING ON GROUND, FUEL TRANSFERS FROM MAIN TANKS TO CENTER TANK. REMOVED OBSTRUCTION IN RIGHT TRANSFER EJECTOR PUMP. OPERATIONAL CHECK GOOD IAW 28-13-01.SDR CA040809001Line · cracked(CAN) APPROXIMATELY 1-5 INCH CRACK ALONG FLANGE. FUEL STAINING NOTED IN AREA. ROUGH RUNNING ENGINE. PIPE ASSEMBLY REPLACED.
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