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 98ZZZX715Line · leakingFUEL LINE, .3750 INCH, SERVING RIGHT WING TANK TO FUEL SELECTOR HAD DEVELOPED PIN HOLE LEAKS DUE TO PITTING CORROSION. LINE LIES UNDER COCKPIT FLOOR, BUT IN CLOSE PROXIMITY TO UNDERSIDE OF FLOOR. BELIEVE CORROSION DUE TO YEARS OF MOISTURE DRAINING AT THE REARSDR AU980653Pipe · loose(AUS) RT FUEL SELECTOR PIPE TO TANK LOOSE.SDR 98FDEA00040Coupling · leakingFUEL LEAKING OUT OF AFT PYLON J-BOX. RAN ENG AND INSPECT FUEL SYS AND FUEL NOZZLES, NO LEAKS NOTED. REMOVED PYLON CAPS AND SIDE PANEL TO INSPECT FUEL LINE. CAP LOOSE, NO LEAKS NOTED. FOUND DAMAGED FWD GAMMA COUPLING OF NR 3 ENGINE. REMOVED AND REPLACED BOSDR P2EA98003Valve · failedPIT - FLT 435 - EMERGENCY DECLARED, LANDING AT DESTINATION AIRPORT UNEVENTFUL, WITH CROSSFEED OPEN AND LEFT BOOST PUMPS OFF, FUEL CONTINUED TO BURN OUT OF THE LEFT WING TANK. REPLACED FUEL CROSSFEED VALVE PER MM 28-22-21. LEAK AND OPS CHECK OK. RAN ENGINES SDR 98ZZZX1832Seal · leakSEALS USED TO REPAIR FUEL LEAK - 2 SCRAPPED ON SITE. REMOVED AND REPLACED 2 EACH.SDR 98ZZZX1831Seal · leakSEALS USED TO REPAIR FUEL LEAK - 2 SCRAPPED ON SITE. REMOVED AND REPLACED 2 EACH.SDR 98ZZZX1830Seal · leakSEALS USED TO REPAIR FUEL LEAK - 2 SCRAPPED ON SITE. REMOVED AND REPLACED 2 EACH.SDR 98ZZZX1829Seal · leakSEALS USED TO REPAIR FUEL LEAK - 7 SCRAPPED ON SITE.SDR 98ZZZX1828Seal · leakSEAL USED TO REPAIR FUEL LEAK - SCRAPPED ON SITE. REMOVED AND REPLACED.SDR 98ZZZX1827Seal · leakSEALS USED TO REPAIR FUEL LEAK - SCRAPPED ON SITE. REMOVED AND REPLACED 2 EA.SDR 98ZZZX1826Seal · leakSEAL USED TO REPAIR FUEL LEAK - SCRAPPED ON SITE. REMOVED AND REPLACED.SDR 98ZZZX1825Seal · leakSEAL USED TO REPAIR FUEL LEAK - SCRAPPED ON SITE. REMOVED AND REPLACED.SDR 98ZZZX1824Seal · leakSEALS USED TO REPAIR FUEL LEAK - SCRAPPED ON SITE. REMOVED AND REPLACED 4 EACH.SDR 98ZZZX1823Seal · leakSEALS USED TO REPAIR FUEL LEAK - SCRAPPED 4 ON SITE. REMOVED AND REPLACED 4 EACH.SDR HALA9800005O-Ring · failedSTRONG FUEL SMELL IN CABIN DURING GROUND OPERATION. REPLACED O-RING ON FUEL SHROUD DRAIN. (M)SDR HEEA0012516Check Valve · leaksCHECK VALVE LEAKS THROUGH WIRES.SDR HEEA0012495Cartridge · inoperativeFUEL SYS CARTRIDGE INOPERATIVE.SDR 98ZZZX293Cartridge · failedFUEL PUMP DOES NOT PUMP FUEL DUE TO FAILED CARTRIDGE.SDR AALA980010Fuel Tansfer Sys · malfunctionedDTW - FLT 0583 - DURING CRUISE FROM BDL/ORD, LATERAL FUEL IMBALANCE NOTED. NR 3 FUEL TANK WOULD NOT DECREASE. AIRCRAFT AIR INTERRRUPTED AND LANDED DTW WITHOUT INCIDENT. INSPECTED FUEL PANEL AND TRANSFERRED FUEL FROM TANK NR 3 TO TANKS 1 AND 2. UNABLE TO DUSDR QXEA9800002Filter · dirtyAFTER TAKEOFF DURING CLIMBOUT, THE NR 1 ENGINE LOW FUEL PRESSURE LIGHT ILLUMINATD AFTER THE BOOST PUMP WAS SWITCHED OFF. WHEN TURNING THE PUMP BACK ON THE LOW FUEL PRESSURE LIGHT GOES OUT. RETURNED TO THE FIELD AND ACCOMPLISHED AN UNEVENTFUL LANDING AT SEA. SDR COMA9860006Conduit · chafedDURING COMPLIANCE OF SB601R-28-008, THE CONDUIT FOR WIRING TO RIGHT FUEL CROSSFLOW SOV WAS FOUND CHAFED THROUGH THE WALL THICKNESS. THE CHAFING TOOK PLACE BETWEEN THE CONDUIT AND THE FUEL LINE SUPPORT BRACKET AT STATION 485 RBL 24 WL 57. REPLACED DAMAGED WIRISDR 98ZZZX831Hose · deterioratedDURING A FATAL AIRCRAFT ACCIDENT INVESTIGATION, INTERNAL DETERIORATION OF MIL-6000 HOSE WAS FOUND PLUGGING A VENT LINE. THE HOSE WAS DATED DURING 1977 AND 1986. THE AIRCRAFT WAS OPERATING ON AUTO GAS (STC'D). THIS CONDITION HAS BEEN SEEN AND REPORTED BEFORESDR TWAA9715203Valve · not securedIND - FLT 468 - DURING CRUISE, FUEL TRANSFERRED TO THE RT HAND FUEL TANK. CLOSED THE DE-FUEL VALVE AND SECURED THE ACCESS DOOR. (X)SDR AU971555Valve · faulty(AUS) FUEL CROSSFEED VALVE FAULTY.SDR AU971554Valve · failed(AUS) FUEL CROSSFEED VALVE FAULTY.SDR 97UAL900850Tube Assy · damagedCENTER TANK WENT FROM 300 INDICATED TO 1200 IN IST 1.5 HOURS OF FLIGHT. WHEN MAINS BELOW HALF, SCAVENGED BACK TO ZERO. *S/D* THIS PROBLEM WAS CAUSED BY TWO MINOR LEAKS TO THE CENTER FUEL TANKS. ONE WAS A LEAKY COUPLING ON THE FUEL SCAVENGE PLUMBING IN THESDR 98ZZZX156Line · chafedFORWARD FUEL LINE COMING FROM THE WING AS IT ENTERS RESERVOIR TANK COMPARTMENT. THERE ARE THREE AN3 BOLTS RETAINING A SEAL IN THE SIDE WALL OF COMPARTMENT. FORWARD BOLT CHAFING LINE, BOLT TURNED OUT TO BE AN3-4A, PARTS MANUAL CALLS FOR AN3-3A. BOTH SIDES OFSDR 98ZZZX152Line · chafedDURING ANNUAL INSPECTION, FUEL LINE WAS FOUND CHAFED NEARLY THROUGH AT HALF-WAY POINT. CHAFING CAUSED BY CARBURETOR HEAT CONTROL CABLE WHICH PASSES CLOSE TO THIS LINE WHERE IT GOES THROUGH THE FIREWALL. AREA IS VERY DIFFICULT TO INSPECT REQUIRING A MIRROR ANSDR 97UAL900849Valve · malfunctionedUNWANTED FUEL TRANSFER FROM NR 2 TANK TO NR 3 TANK. *S/D* REPLACED THE NR 3 TANK FUEL MANIFOLD VALVE.SDR HEEA0012096Cartridge · defectiveFUEL PRESSURE READS LOW WHEN GENERATOR IS OFF LINE.SDR HEEA0012060Valve · defectiveNR1 ENGINE STALLING.SDR 99ZZZX113Line · chafedPILOT REPORTED ERRATIC FUEL FLOW INDICATION. DURING GROUND ENG RUN-UP FOR T/S, A LOUD POP WAS HEARD, LARGE SPARK SHOT FROM BEHIND COPILOT'S INSTRUMENT PANEL, AND THE 3-AMP STEREO CB OPENED. INVEST REVEALED THE 28-VOLT POWER LEAD FOR THE STEREO (INSTALLED SEVSDR 9721239760Fuel · leakingDURING TAXI OPERATIONS, DISCOVERED FUEL VENTING FROM THE RIGHT WING. EMERGENCY EQUIPMENT WAS CALLED AS A PRECAUTION AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE TRANSFERRED EXCESS FUEL AND PERFORMED BACKFLUSH PROCEDURES PER MM, OPERATISDR 9721216641Fuel · leakingDURING TAKEOFF, FUEL STARTED VENTING FROM THE LEFT WING. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. DRAINED SURGE TANKS. EXACT PART CAUSING PROBLEM TO BE DETERMINED.SDR HEEA0011770Valve · defective6 TO 10 SEC DELAY INTERMITTENTLY WHEN SWITCH IS ACTIVATED. SENT TO BELL HELICOPTER TEXTRON FOR INSPECTION AND REPAIR.SDR 98ZZZX1423Fuel Line · leakingPILOT REPORTED ODOR OF FUEL IN THE COCKPIT. INSPECTION REVEALED FUEL SEEPAGE WHERE THE TUBE ASSEMBLY CONNECTS TO THE TEE AT THE HEADER TANK INLET (THIS IS THE TUBE ASSY FROM THE LEFT WING TANK). THE FLARE WAS FOUND TO HAVE AN OUTSIDE DIAMETER LARGER THAN THESDR 98ZZZX1315Fuel Line · leakingPILOT REPORTED ODOR OF FUEL IN THE COCKPIT. INSPECTION REVEALED FUEL SEEPAGE WHERE THE TUBE ASSEMBLY CONNECTS TO THE TEE AT THE HEADER TANK INLET (THIS IS THE TUBE ASSY FROM THE LEFT WING TANK). THE FLARE WAS FOUND TO HAVE AN OUTSIDE DIAMETER LARGER THAN THESDR 9720766633Check Valves · failedDURING CRUISE, FUEL STARTED VENTING FROM THE RIGHT WING TIP. AIRCRAFT RETURNED TO NRT AND LANDED WITHOUT INCIDENT. CORRECTED SURGE TANK VENT LINE LEAK AT OUTBOARD NACELLE RIB COUPLING AND REPLACED THE NBR 3 FORWARD AND AFT MAIN BOOST PUMP DISCHARGE CHECK VALVESDR CA971106004Fuel Hose · bent(CAN) BRACKET AT ENGINE DRIVEN PUMP OF FUEL SUPPLY LINE FOUND BENT AND WILL NOT FIT THE AIRCRAFT. SUBMITTER SCRAPPED HOSES.SDR MWEA97815Check Valve · leakingINFLIGHT NOTICED LARGE FUEL LEAK FROM LEFT WING AROUND AILERON PANEL. MTC FOUND RT FWD BOOST PUMP VOLUTE CHECK VALVE CAUSING LEAK AND DISASSEMBLED AND REASSEMBLED.SDR CA971106003Fuel Line · swollen(CAN) EIGHT INCH HOSE RECEIVED FROM MANUFACTURER NEW. FLOW TEST FOUND TO HAVE RESTRICTIONS CAUSING A FAN PATTERN IN THE FLOW.SDR AALA972047Actuator · defectiveLGA - FLT 253 - AFTER TAKEOFF LGA DURING CLIMB-OUT, FUEL CROSSFEED C/B POPPED. FUEL QUANTITY DECREASED MORE RAPIDLY IN RT WING TANK THAN LEFT WING TANK AND FUEL CROSSFEED FLOW BAR WOULD NOT ILLUMINATE. AIRCRAFT RETURNED TO LGA AND LANDED WITHOUT INCIDENT. RSDR CA971031009Fuel Line · deteriorated(CAN) AIRCRAFT OPERATING WITH AUTOMOTIVE FUEL (MOGAS). THE FUEL LINE WAS FOUND TO BE SWOLLEN INTERNALLY THEREBY RESTRICTING FLOW.SDR CA971031008Fuel Line · deteriorated(CAN) THE PILOT HAD A FUEL FLOW WARNING LIGHT ILLUMINATE. AFTER A SUCCESSFUL LANDING, INVESTIGATION FOUND THE FUEL LINE ON THE SWAGE OF THE FUEL PUMP TO BE SWOLLEN AND THE FUEL FLOW RESTRICTED.SDR HEEA0011697Cartridge · inoperativeEJECTOR INOPERATIVE.SDR 97ZZZX4618Hose Fitting · pluggedTHIS AIRCRAFT WAS INVOLVED IN AN ACCIDENT. ON CLIMB-OUT, AIRCRAFT LOST POWER. LANDED ON LAST 100 FEET OF RUNWAY. AIRCRAFT NOSE-OVER, AND CAME TO A STOP INVERTED. AFTER REPAIR, NEW OWNER WAS INSPECTING FUEL SYSTEM AND FOUND RT FUEL TANK AFT OUTLET FITTING CSDR CA971021010Fuel Line · deteriorated(CAN) IT WAS NOTED THAT FUEL FLOW THROUGH THE LINE WAS IRREGULAR. THE LINE HAD BEEN DISCONNECTED FROM THE FUEL PUMP. CUTTING THE LINE FOR FURTHER INVESTIGATION SHOWED IT TO HAVE SWOLLEN INSIDE AND THEREBY RESTRICTING FUEL FLOW. SUBMITTER STATES THAT THE AIRCRASDR 9719066633Drain Fitting · looseDURING CLIMB, FUEL STARTED VENTING FROM THE RIGHT WING TIP. CLOSED CROSSFEED VALVES AND THE VENTING STOPPED. AIRCRAFT DIVERTED TO SEA AND LANDED WITHOUT INCIDENT. SECURED SURGE TANK DRAIN LINE FITTING AT NR 4 PYLON RIB AND REPLACED NR 3 FUEL BOOST PUMP DUE SDR 97ZZZX4503O-Ring · deterioratedA FUEL ODOR BECAME NOTICEABLE THEN STRONG IN THE CABIN OVER A SHORT PERIOD OF TIME. THE WHOLE FUEL SYSTEM WAS CHECKED AND NO LEAKS WERE VISIBLE. ONLY AFTER A FUEL STAIN (RED MOTOR GAS) WAS SEEN ON THE BELLY WAS THE SEEP TRACED TO THE FUEL (STRAINER SUMP) WHESDR USAAF97079Door · out of adjustFLT 1455 - PHL-MSP - EN ROUTE TO MSP, FUEL WOULD NOT TRANSFER FROM THE CENTER TANK TO THE WING TANKS. FLIGHT DIVERTED TO PIT FOR MAINTENANCE AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE FUELING PANEL POWER SWITCH TO OFF AND ADJUSTED THE MECHANISM ON TH
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