JASC 2897
Service difficulty reports · 656
Reports filed under 2897 · Fuel System Wiring, 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 = '2897' 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 = '2897' 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 HEEA083739Connector · damaged"B" PIN LOOSE CAUSING FUEL FILTER LIGHT IN COCKPIT TO ILLUMINATE ON CAUTION PANEL.SDR AUS20030125Wire · worn(AUS) FUEL QUANTITY SYSTEM WIRE 284120002922-2 LOCATED UNDER WING ACCESS PANEL 624AT AT WING STN 225 FOUND TO BE CHAFED IN AREA WHERE WIRE ASSEMBLY EXITS ALLOY CONDUIT AND GOES TO FUEL QUANTITY PROBE.SDR AUS20030030Wire Harness · chafed(AUS) LT WING FUEL CAPACITANCE LOOM CHAFING ON THE UPPER SURFACE OFTHE LOWER WING SKIN AT THE INBOARD END.SDR O2G2003F00003Harness · intermittentRT WING HEAVY CONDITION CAUSED BY FUEL IMBALANCE. ON CLIMB OUT, FUEL MIGRATED TO WING TIPS MAKING IMBALANCE SEEM MORE THAN IT WAS. BOTH FUEL TANKS OPENED, INSPECTED ALL PROBES, CONNECTORS, AND WIRING. REPLACED ANY CONNECTORS THAT COULD HAVE HAD CORROSION STSDR SWIA200211534Wire Harness · chafedLT WING WIRE HARNESS CHAFED ON FUEL LINE THAT GOES TO VENT VALVE. FOUND DURING "C" CHECK INSPECTION. REMOVED AND REPLACED LT WING WIRE HARNESS WITH SERVICEABLE UNIT. OPS CHECK GOOD.SDR UPS02439771Wire Harness · burnedINSPECTION TYPE: C, FWD BOOST PUMP PRESS LIGHT ON , C/B CYCLES AND POPS PUMP C/B ON P14 PANEL; NR 1 & 3 BOOST PUMP PRESS LIGHT ON. FWD CGO CEILING AT STA 920 RBL 5 WIRING BUNDLES W220 & W842 ADJACENT T O NR 4 FWD BOOST PUMP FOUND BURNED WIRE AND POOR CONSDR MALA020594Wire Harness · peelingSEVERAL WIRES IN THE LEFT WING FUEL CELL HAVE THE OUTER LAYER PEELING AT STA WJ183.21, BETWEEN FUEL PANELS 523BT AND 523CT. MAINTENANCE REPLACED LEFT OUTBOARD FUEL PROBE HARNESS. LEFT FUEL INDICATING SYSTEM OPS TESTS AND CAPACITANCE TEST GOOD IAW SAAB 340 AMSDR A152Wire · corrodedDURING INSPECTION OF FUEL PANEL DIODES: FOUND FUEL PANEL DIODES AND WIRING CONNECTION CORRODED: CLEANED , TREATED AND REINSTALLED PANEL.SDR AUS20021015Harness · worn(AUS) NO2 FUEL TANK ELECTRICAL HARNESS CHAFING.SDR P2EA2002M048Wire Harness · defectiveDURING TROUBLESHOOTING THE RIGHT WING AFT FUEL BOOST PUMP WIRING HARNESS WAS FOUND DEFECTIVE. REMOVED AND REPLACED RIGHT WIND AFT BOOST PUMP WIRE HARNESS IAW MM 28-20-07.SDR 02FDEA00402Wire · brokenTWO WIRES FOUND BURNT & BROKEN ABOVE AVIONICS RACK IN CAC. REMOVED AND REPLACED WIRES PER C901-836-16C. OPS CHECK BOOST PUMP CARRIED OUT AS PER WC E1-2821-7-5000-03 PART 3 & 4.SDR HEEA080064Wire Harness · chafedCHAFING 20 INCHES FROM TOP FUEL PROBE CONNECTORS.SDR CA020611001Wire Harness · chafed(CAN) DURING INSPECTION AND COMPLYING WITH AD 2002-09-13 AND CESSNA SERVICE BULLITEN CQB02-1 REV. 1, FOUND THAT THE BLACK WIRE IN THE HARNESS WAS CHAFED THROUGH AND ARCING TO GROUND ON THE FUEL PUMP SHROUD. THE OTHER WIRES IN THE HARNESS WERE ALSO CHAFED, BUSDR AUS20020530Wire Harness · chafed(AUS) FUEL BOOST PUMP WIRING HARNESSES CHAFED. FOUND DURING INSPECTION IAW AD/CESSNA400/111 (SB CQB02-1R1).SDR HEEA079014Pressure Switch · corrodedFUEL BOOST PUMP PRESSURE SWITCH WIRES CORRODED AND BROKEN.SDR AUS20020464Harness · worn(AUS) LT FUEL BOOST PUMP WIRING HARNESS CHAFED. FOUND DURING INSPECTION IAW SB CQB02-1.SDR AUS20020408Harness · chafed(AUS) LT FUEL TANK HARNESS WIRE CHAFFED BUT WITHIN ACCEPTABLE LIMITS OF SB CQB02-1. HARNESS MODIFIED IAW SB AND REINSTALLED.SDR AUS20020409Harness · chafed(AUS) RT FUEL TANK HARNESS WIRE CHAFED BUT WITHIN ACCEPTABLE LIMITS OF SB CQB02-1. HARNESS MODIFIED IAW SB AND REINSTALLED.SDR EHA2002F00000Wire · defectiveFLOW SWITCH HAD A BROKEN WIRE FROM STOCK. CAUSED AIRCRAFT TO HAVE LATE DEPARTURESDR AUS20020388Wire · loose(AUS) FUEL CROSSFEED SELECTOR LIGHT ILLUMINATED WITH SELECTOR CLOSED. PROBLEM TRACED TO AN INTERMITTENT FAULT IN WIRING BEHIND THE PLUG.SDR 441M032002Wire · chafedWIRING FOR FUEL BOOST PUMPS IN EACH WING WERE CHAFED THROUGH TO CONDUCTOR. WIRING HARNESS HAS TWO CONNECTOR PLUGS, ONE TO EACH BOOST PUMP. CONNECTOR PLUGS ARE WIRED TO A THIRD, LARGER PLUG THAT CONNECTS TO BULKHEAD PLUG THAT FEEDS THROUGH INBOARD MOST RIB IN SDR DEBA2624DWire Harness · chafedFUEL BOOST PUMP WIRING IN THE WET WING AREA OF EACH WING, WAS CHAFED THROUGH THE INSULATION TO THE CENTER CONDUCTOR. THE WIRING, WHERE IT EXITS THE FEED THROUGH CONNETOR PLUG, INTO THE WET WING, AT THE INBOARD MOST RIB, IS CHAFING ON THE BOX THAT SURROUNDS THESDR ASAA0240027Module · burnedSEA - AFTER TAKEOFF AT SEVERAL HUNDRED FEET, NR 1 FUEL TANK FORWARD PUMP LIGHT ILLUMINATED IN CONJUNCTION WITH A 'POP' FOLLOWED BY SMOKE IN THE COCKPIT AND AN ELECTRICAL SMELL. RETURNED TO FIELD AND LANDED UNEVENTFULLY. FOUND SHORT CIRCUIT BETWEEN OPEN AND SDR 2002FA0000398Wire · chafedFOUND RT WING AUXILLARY BOOST PUMP WIRING, CHAFING ON BOOST PUMP HOUSING CAUSING AN ELECTRICAL ARCING INSIDE OF FUEL BAY.SDR COMA0260087Fuel Tank · damagedWHEN L/H BOOST PUMP CANISTER WAS REMOVED FOR REPAIR, FOUND THE WIRING INSULATION PULLED BACK AND WIRE CONDUCTORS EXPOSED.REPLACED CANISTER.SDR CA020123001Wire Harness · chafed(CAN) WHILE IN FLIGHT, CREW REPORTED THAT THE LEFT FUEL QTY INDICATION AND TOTAL FUEL QTY INDICATION WENT TO DASHES. FUEL QTY INDICATION WAS DEFERRED PER MEL AND MLIS WRE USED TO CHECK FUEL QUANTITY BEFORE EACH FLIGHT. UPON FURTHER INVESTIGATION, MAINTENSDR COMA0260077Wire Harness · chafedWHILE WORKING DEFERRED MAINTENANCE ON LT FUEL QUANTITY SYSTEM, FOUND THE FUEL LEVEL PROBE WIRE HARNESS, BETWEEN NR 3 PROBE AND CONNECTOR J3QB/P3QB CHAFING ON FUEL BAFFLE P/N 601R62359-1. REPLACED THE WIRE HARNESS.SDR COMA0260076Wire Harness · chafedWHILE WORKING DEFERRED MAINTENANCE ON LT FUEL QUANTITY SYSTEM, FOUND THE FUEL LEVEL PROBE WIRE HARNESS, BETWEEN NR 3 PROBE AND CONNECTOR J3QB/P3QB, CHAFING ON FUEL BAFFLE P/N 601R62359-1. REPLACED WIRE HARNESS.SDR CA011025003Connector · shorted(CAN) DURING GROUND HANDLING THE LT FUEL BOOST PUMP LOW PRESSURE LIGHT WAS OBSERVED TO BE ILLUMINATED WITH THE A/C NOT POWERED. INVESTIGATION REVEALED THE PROBLEM WAS LOCATED IN THE PL3 WING ROOT CONNECTOR. AN INTERNAL SHORT WAS ALLOWING THE LOW PRESSURE LIGHTSDR SWIA200110323Wire · damagedVENT VALVE WIRING LINE INSIDE FUEL TANK NEAR LEFT WING TIP HAS DAMAGE. REPLACED LEFT VENT VALVE WIRING LINE ASSY.SDR CA011002005Wire · burned(CAN) DURING TAKE OFF THE CREW OBSERVED A LOW FUEL PRESSUE LIGHT INDICATION ACCOMPANIED BY THE TRIP OFF OF THE CIRCUIT BREAKER SWITCH FOR THE LT SECONDARY PUMP.SMOKE WAS EMINATING FROM BEHIND THE LOWER LEFT PANEL AT THE SAME TIME. THE TAKE OFF WAS ABORTED AND SDR CA011011022Wire · pinched(CAN) ON REMOVAL OF THE BOOSTER PUMP, IT WAS FOUND THAT THE WIRE HARNESS, WHICH IS PART OF THE PUMP HAD APPEARED TO HAVE BEEN TRAPPED BETWEEN THE BOOSTER PUMP MOUNTING PLATE & THE AIRFRAME. THIS HAS CAUSED ONE WIRE OF THE HARNESS TO BE CRIMPED FLAT & THE INTERSDR C1HA200184009Wire · brokenDURING FLAP ASSYM PROCEDURE, FUEL WAS PUMPED LEFT PUMP NOZZLE FAILED TO CLOSE. FOUND BROKEN WIRE REPAIRED BROKEN WIRE PER STANDARD WIRING PRACTICES CHAPTER 28-31-01. OPS CHECK GOOD.SDR GLBA2001200Wire · chafedRIGHT WING FUEL QUANTITY WIRING CHAFED ON LIGHTENING HOLE OUTBOARD OF NR 4 FUEL STICK AND RIB NR 20.SDR GLBA2001201Wire · chafedRIGHT WING FUEL QUANTITY WIRES CHAFED ON FUEL VENT LINE (TUBE) AT RIB NR 20.SDR GLBA2001198Wire · chafedFUEL QUANTITY WIRES CHAFING ON LINE (TUBE) BY LEFT VENT VALVE BETWEEN RIBS NR 24 & 25.SDR 2001F00290Wire · chafedFLT - 9262 - FPO-PBI - ON LANDING, LEFT FUEL VENT CIRCUIT BREAKER BEGAN TO EMIT SMOKE. MANUALLY PULLED CIRCUIT BREAKER. SMOKE STOPPED. CONTINUED TO LAND WITHOUT INCIDENT. DETERMINED WIRING ON LEFT FUEL VENT ASSEMBLY TO BE CHAFED. REPLACED LEFT FUEL VENT ASDR 20010514SG002Wire · burnedDURING FLIGHT PLS/JFK, LEFT DUMP NOZZLE VALVE CAME ON INTERMITTENTLY. DEACTIVATED LEFT FUEL NOZZLE DUMP VALVE CLOSED AND SAFETIED IAW MEL 28-9, TRANSFERRED TO DMI SLIP 1226. NO POWER TO PIN B AT CANNON PLUG. OPENED WING PANELS FOR INSPECTION. FOUND BURNED SDR ABXA010118Wire · chafedLEFT WING FUEL QUANTITY PROBE WIRING AT ACCESS PANEL 531BB WAS CHAFED DOWN TO BARE WIRE. MAINTENANCE INSPECTED AND REPLACED THE LEFT AUX FUEL QUANTITY WIRING HARNESS.SDR AU010260Wire · shorted(AUS) FUEL SYSTEM CONTROL VALVE WIRE PNO W6400-008-18R LOCATED IN NR 4 STRUT KNEE CAP DISCONNECT PLUG D14300P CHAFED AND SHORT CIRCUITING TO GROUND.SDR VNAA0103007Coax · defectiveDURING REPOSITION FLIGHT 9405 GSP-ELM THE FLIGHT CREW RECEIVED A RIGHT FUEL QUANTITY FAIL AND LEFT FUEL LOW FAIL WARNING MESSAGES. THE FLIGHT CREW DIVERTED TO PIT WHERE A NORMAL LANDING WAS MADE. MAINTENANCE INSPECTED AND REPLACED THE COAXIAL CABLE REDUCER ISDR AU010011Wire · chafed(AUS) LT FUEL TANK BOOST PUMP WIRING CHAFED THROUGH TO BARE WIRE.SDR AU010064Wire · damaged(AUS) KAPTON WIRES LOCATED IN REFUEL PANEL HAVE DAMAGED INSULATION ALLOWING THE WIRES TO BE EXPOSED.SDR AU001284Wire · damaged(AUS) KAPTON WIRES LOCATED IN REFUEL PANEL HAVE DAMAGED INSULATION ALLOWING THE WIRES TO BE EXPOSED.SDR AALA20001635Wire · damagedSJU - FLT 1014 - EN ROUTE SJU-MIA, NR 1 ENGINE FUEL CROSS FEED VALVE STUCK IN THE CLOSED POSITION. RETURNED SJU AND LANDED WITHOUT INCIDENT. REPLACED NR 1 SIDE ENGINE CROSS FEED VALVE. REPAIRED WIRES AT NR 1 SIDE ENGINE CROSS FEED VALVE CANNON PLUG. SYSTEM SDR AU000970Wire · faulty(AUS) NO2 FUEL TANK QUANTITY GAUGE OVER-READING DUE TO DEFECTIVE WIRING AT NO2 FUEL QUANTITY TRANSMITTER. NO2 ENGINE FAILED DUE TO FUEL EXHAUSTION.SDR AU000866Wire · worn(AUS) RT MAIN FUEL BOOST PUMP AND RT AUXILIARY FUEL BOOST PUMP WIRESWORN.SDR AU000867Wire · worn(AUS) LT FUEL BOOST PUMP WIRE INSULATION WORN.SDR AU000865Wire · worn(AUS) LT AUXILIARY FUEL BOOST PUMP AND LT MAIN FUEL BOOST PUMP WIRING DAMAGED.SDR AU000862Wire · worn(AUS) LT AUXILIARY BOOST PUMP WIRE WORN. LT MAIN BOOST PUMP WIRE INSULATION WORN.
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