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.

SDR HEEA083739Connector · damaged"B" PIN LOOSE CAUSING FUEL FILTER LIGHT IN COCKPIT TO ILLUMINATE ON CAUTION PANEL.Jan 15, 2003 · N501PH · Bell 407SDR 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.Jan 13, 2003 · Dhav DHC8102SDR AUS20030030Wire Harness · chafed(AUS) LT WING FUEL CAPACITANCE LOOM CHAFING ON THE UPPER SURFACE OFTHE LOWER WING SKIN AT THE INBOARD END.Jan 7, 2003 · Cessna 402CSDR 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 STDec 25, 2002 · N677CX · Gulstm G1159BSDR 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.Nov 5, 2002 · N293SW · Emb EMB120ERSDR 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 CONOct 4, 2002 · N528UP · Boeing 747200SDR 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 AMOct 2, 2002 · N27XJ · Saab SF340ASDR A152Wire · corrodedDURING INSPECTION OF FUEL PANEL DIODES: FOUND FUEL PANEL DIODES AND WIRING CONNECTION CORRODED: CLEANED , TREATED AND REINSTALLED PANEL.Sep 9, 2002 · N5462G · Beech E90SDR AUS20021015Harness · worn(AUS) NO2 FUEL TANK ELECTRICAL HARNESS CHAFING.Aug 20, 2002 · Boeing 737376SDR 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.Jul 9, 2002 · N137NJ · Doug DC982SDR 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.Jun 13, 2002 · N620FE · Doug MD11SDR HEEA080064Wire Harness · chafedCHAFING 20 INCHES FROM TOP FUEL PROBE CONNECTORS.Jun 11, 2002 · N499PH · Bell 407SDR 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, BUJun 10, 2002 · Cessna 441SDR AUS20020530Wire Harness · chafed(AUS) FUEL BOOST PUMP WIRING HARNESSES CHAFED. FOUND DURING INSPECTION IAW AD/CESSNA400/111 (SB CQB02-1R1).May 31, 2002 · Cessna 441SDR HEEA079014Pressure Switch · corrodedFUEL BOOST PUMP PRESSURE SWITCH WIRES CORRODED AND BROKEN.May 15, 2002 · N493PH · Bell 407SDR AUS20020464Harness · worn(AUS) LT FUEL BOOST PUMP WIRING HARNESS CHAFED. FOUND DURING INSPECTION IAW SB CQB02-1.May 13, 2002 · Cessna 441SDR AUS20020408Harness · chafed(AUS) LT FUEL TANK HARNESS WIRE CHAFFED BUT WITHIN ACCEPTABLE LIMITS OF SB CQB02-1. HARNESS MODIFIED IAW SB AND REINSTALLED.May 4, 2002 · Cessna 441SDR AUS20020409Harness · chafed(AUS) RT FUEL TANK HARNESS WIRE CHAFED BUT WITHIN ACCEPTABLE LIMITS OF SB CQB02-1. HARNESS MODIFIED IAW SB AND REINSTALLED.May 3, 2002 · Cessna 441SDR EHA2002F00000Wire · defectiveFLOW SWITCH HAD A BROKEN WIRE FROM STOCK. CAUSED AIRCRAFT TO HAVE LATE DEPARTUREApr 29, 2002 · N5017H · Bell 212SDR AUS20020388Wire · loose(AUS) FUEL CROSSFEED SELECTOR LIGHT ILLUMINATED WITH SELECTOR CLOSED. PROBLEM TRACED TO AN INTERMITTENT FAULT IN WIRING BEHIND THE PLUG.Apr 23, 2002 · Boeing 737376SDR 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 Mar 20, 2002 · N441M · Cessna 441SDR 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 THEMar 15, 2002 · N2624D · Cessna 441SDR 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 Mar 5, 2002 · N791AS · Boeing 737490SDR 2002FA0000398Wire · chafedFOUND RT WING AUXILLARY BOOST PUMP WIRING, CHAFING ON BOOST PUMP HOUSING CAUSING AN ELECTRICAL ARCING INSIDE OF FUEL BAY.Mar 1, 2002 · N441SX · Cessna 441SDR COMA0260087Fuel Tank · damagedWHEN L/H BOOST PUMP CANISTER WAS REMOVED FOR REPAIR, FOUND THE WIRING INSULATION PULLED BACK AND WIRE CONDUCTORS EXPOSED.REPLACED CANISTER.Jan 28, 2002 · N918CA · Cndair CL6002B19SDR 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, MAINTENJan 23, 2002 · Cndair CL6002B19SDR 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.Jan 15, 2002 · N988CA · Cndair CL6002B19SDR 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.Jan 5, 2002 · N987CA · Cndair CL6002B19SDR 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 LIGHTOct 22, 2001 · Braero HS7482ASDR SWIA200110323Wire · damagedVENT VALVE WIRING LINE INSIDE FUEL TANK NEAR LEFT WING TIP HAS DAMAGE. REPLACED LEFT VENT VALVE WIRING LINE ASSY.Oct 22, 2001 · N565SW · Emb EMB120ERSDR 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 Oct 20, 2001 · Beech 99SDR 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 INTEROct 2, 2001 · Pilats PC1245SDR 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.Sep 11, 2001 · N684CA · Boeing 7272S7SDR GLBA2001200Wire · chafedRIGHT WING FUEL QUANTITY WIRING CHAFED ON LIGHTENING HOLE OUTBOARD OF NR 4 FUEL STICK AND RIB NR 20.Sep 5, 2001 · N96ZK · Emb EMB120ERSDR GLBA2001201Wire · chafedRIGHT WING FUEL QUANTITY WIRES CHAFED ON FUEL VENT LINE (TUBE) AT RIB NR 20.Sep 5, 2001 · N96ZK · Emb EMB120ERSDR GLBA2001198Wire · chafedFUEL QUANTITY WIRES CHAFING ON LINE (TUBE) BY LEFT VENT VALVE BETWEEN RIBS NR 24 & 25.Sep 5, 2001 · N96ZK · Emb EMB120ERSDR 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 AAug 9, 2001 · N151GA · Beech 1900CSDR 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 Apr 6, 2001 · N804MA · Boeing 727225SDR 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.Apr 5, 2001 · N713AX · Boeing 767205SDR 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.Mar 18, 2001 · Boeing 747438SDR 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 IMar 3, 2001 · N440JS · Dorner DO328100SDR AU010011Wire · chafed(AUS) LT FUEL TANK BOOST PUMP WIRING CHAFED THROUGH TO BARE WIRE.Jan 10, 2001 · Cessna 441SDR AU010064Wire · damaged(AUS) KAPTON WIRES LOCATED IN REFUEL PANEL HAVE DAMAGED INSULATION ALLOWING THE WIRES TO BE EXPOSED.Jan 9, 2001 · Boeing 737377SDR AU001284Wire · damaged(AUS) KAPTON WIRES LOCATED IN REFUEL PANEL HAVE DAMAGED INSULATION ALLOWING THE WIRES TO BE EXPOSED.Nov 25, 2000 · Boeing 737377SDR 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 Oct 3, 2000 · N894AA · Boeing 727223SDR 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.Oct 3, 2000 · Aerosp SA365CSDR AU000866Wire · worn(AUS) RT MAIN FUEL BOOST PUMP AND RT AUXILIARY FUEL BOOST PUMP WIRESWORN.Sep 15, 2000 · Frchld SA227DCSDR AU000867Wire · worn(AUS) LT FUEL BOOST PUMP WIRE INSULATION WORN.Sep 14, 2000 · Frchld SA227DCSDR AU000865Wire · worn(AUS) LT AUXILIARY FUEL BOOST PUMP AND LT MAIN FUEL BOOST PUMP WIRING DAMAGED.Sep 14, 2000 · Frchld SA227DCSDR AU000862Wire · worn(AUS) LT AUXILIARY BOOST PUMP WIRE WORN. LT MAIN BOOST PUMP WIRE INSULATION WORN.Sep 14, 2000 · Frchld SA227DC
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