JASC 2897
Service difficulty reports · 656
Reports filed under 2897 · Fuel System Wiring, newest first.
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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 CA041109008Wire · arced(CAN) FUEL QUANTITY REPORTED AS FLUCTUATING. DURING TROUBLESHOOTING PROCESS ONE OF THE WIRES ON THE RT TANK FORWARD FUEL PROBE WAS FOUND ARCING. PROBE REPLACED.SDR DL73S040888Relay · inoperativeBOTH AFT FUEL PUMP CBS POPPED. REPLACED R-19 RELAY.SDR CWQR2004001Wire Harness · burnedDURING INSPECTION, FOUND LEFT WING OUTBOARD FUEL QUANTITY TRANSMITTER WIRING HARNESS INSOLATION BURNT BETWEEN WIRE SHIELDING AND TERMINAL. FILED SERVICE CONDITION REPORT NR 161570 WITH CESSNA/CITATION. COPY OF REPORTS, SUPPORTING DOCUMENTATION AND PICTURES SSDR CQWR2004002Wire Harness · burnedDURING INSPECTION FOUND RT WING OUTBOARD FUEL QTY TRANSMITTER WIRING HARNESS BURNED BETWEEN WIRE SHIELDING AND TERMINAL. FILED SERVICE CONDITION REPORT 161544 WITH CESSNA/CITATION. COPIES OF REPORTS, SUPPORTING DOCUMENTATION AND PICTURES SENT TO PMI AND OPERSDR RAIA00408003Wire · damagedLOW FUEL TEMP WARNING INDICATION. AIRCRAFT FERRIED TO STL. MAINTENANCE REPAIRED WIRE AT LOW TEMP SWITCH.SDR 2004FA0000674Wire · damagedWHILE PERFORMING, SB550-28-14, THE FUEL BOOST PUMP WIRING INSIDE THE LT AND RT WING TANKS WAS FOUND TO HAVE RUBBED HOLES IN THE FUEL TRANSFER LINES INSIDE THE TANKS AND DAMAGED THE WIRING. THE ABOVE BULLETIN ADDRESSES THIS CONCERN AND PROVIDES INSTRUCTIONS FORSDR CWQ2004F00007Wire · misinstalledWHEN COMPLYING WITH SB ON AC, THE RT WING FUEL BOOST PUMP WIRING WAS FOUND TO BE UNACCEPTABLE IAW SB OUTER JACKET, WIRE BRAID AND WIRE INSULATION CHAFED THRU, ALSO ABOUT HALF OF WIRE WAS ALSO CHAFED. THE WIRING WAS CHAFED ON A FUEL SUPPLY TUBE PN 652635548 WHSDR 2004UALA00517Wire · failedFLIGHT DIVERTED DUE TO A STUCK FUEL CROSS-FEED VALVE CAUSING A FUEL IMBALANCE. CREW REPORTED FUEL CROSSFEED LIGHT REMAINS BRIGHT (INDICATING VALVE IS IN TRANSIT) NO MATTER WHAT POSITION THE CROSSFEED SWITCH IS IN. AND FUEL CROSS FEED VALVE POSITION LIGHT DOES SDR 2004UALA00466Wire Harness · failedFLIGHT DIVERTED DUE TO A POSSIBLE FUEL LEAK. UNWANTED FUEL TRANSFER AND DEGRADED FUEL INDICATIONS CAUSED BY LEFT HAND WING INNER FUEL QUANTITY HARNESSES FAILURE. REPLACED LEFT HAND WING INNER FUEL QUANTITY HARNESSES. OPERATIONS CHECK NORMAL.SDR AUS20040324Wire · worn(AUS) RT FUEL TANK QUANTITY WIRE CHAFED ON STRINGERS LOCATED AT STATION PWS 61.80.SDR AUS20040225Wire · chafed(AUS) RT MAIN FUEL BOOST PUMP WIRING CHAFED.SDR CA040316006Wire · chafed(CAN) RT SPAR FUEL SHUTOFF VALVE CB C1062 ACTIVATED DURING SHUTDOWN AFTER FLIGHT. CB WOULD NOT RESET, AND SPAR VALVE DISAGREEMENT LIGHT ALSO ILLUMINATED. TROUBLESHOOTING REVEALED WIRE HAD CHAFING DAMAGE AT BULKHEAD LOCATED AT STATION PP STN 208.40 VISIBLE BEHSDR 04019314Wire · chafedDURING INSPECTION THE LEFT HAND WING FUEL PROBE WIRING AT RIB 16 WAS FOUND TO BE CHAFING. THE INSULATION AND WIRE WERE RESECURED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED TO SERVICE UPON COMPLETION OF INSPECTION.SDR DHL2003781006Wire · chafedON PRE-DEPARTURE CHECK NOTICED SMOKE EMANATING BEHIND NR 2 KRUEGER FLAP. FOUND WIRE CHAFING AGAINST TANK NR 2 FWD LT FUEL PRESSURE SWITCH TUBE. REPAIRED WIRE, NOTICED TUBE HAD CHAFED THRU. REPLACED TUBE. LEAK CHECKED GOOD REPLACED SEVERAL SUSPECT ADEL CLAMSDR IF12003F00001Petcock Knob · shortedPILOT DISCREPANCY, WARNING LIGHTS POWER NR 7 CIRCUIT BREAKER POPPED. FOUND LT HP FUEL COCK KNOB SHORTING TO LEVER ARM (HANDLE IS LIGHTED) KNOB WAS PROBABLY BROKEN BY TWISTING MOTION FROM PILOT WING STARTING OR SHUTTING DOWN ENGINE. NO RECOMMENDATIONS FOR PRSDR AUS20031138Circuit Breaker · burned out(AUS) LT INNER FUEL BOOST PUMP CIRCUIT BREAKER BURNED OUT.SDR 2003UALA00824Wire Harness · damagedRT CENTER BOOST PUMP OVERRIDE CB POPS ON P6-4 PANEL. WIRING DAMAGE IN THE RH WHEEL WELL AS A RESULT OF ELECTRICAL ARCING. THE EVENT OCCURRED DURING A "C" CHECK VISIT WHEN TECHNICIANS WERE PERFORMING A ROUTINE INSULATION RESISTANCE CHECK OF THE FUEL PUMP. ANALSDR SWIA200312607Wire · chafedLEFT FORWARD FUEL BOOST PUMP HAS CHAFED WIRE. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED LEFT FORWARD FUEL BOOST PUMP IAW MM 28-21-02.SDR KBM2003F00069Circuit Breaker · malfunctionedFORWARD FUEL PUMP CIRCUIT BREAKER DOES NOT ILLUMINATE MASTER CAUTION LIGHT WHEN PULLED. REPLACED.(K)SDR CA031114007Connector · burned(CAN) WHILE THE AIRCRAFT WAS IN CRUISE FLIGHT, A BURNING ODOR WAS NOTICED IN THE CABIN. THE PILOT LANDED THE AIRCRAFT UNEVENTFULLY. THE BURNING ODOR WAS TRACED TO THE OVERHEAD LT FUEL PUMP SWITCH. WHEN THE OVERHEAD PANELS WERE REMOVED A BURNED PUMP SWITCH CONSDR 97CWWire Harness · chafedFUEL PUMP WIRING HARNESS IS NOT SUPPORTED WITHIN THE FUEL CELL AND CHAFED ON THE FUEL LINE FROM THE PRIMARY PUMP TO THE CHECK VALVE INSIDE THE FUEL CELL. THERE WAS .006 INCH DAMAGE TO THE WALL OF THE FUEL LINE AND THE PUMP HARNESS SHIELDING WAS CHAFED THROUGHSDR HN62003F00001Wire · arcedWHILE WORKING SB NR 767-28A0077, THE MECHANIC REMOVED 2 EACH LT WING AND 2 EACH RT WING FUEL BOOST PUMPS. HE DISCOVERED ELECTRICAL ARCING DAMAGE ON BOTH LT WING AND BOTH RT WING BOOST PUMPS. UPON FURTHER INVESTIGATION FOUND ADDITIONAL ELECTRICAL ARCING ON BSDR CA031021002Wire · damaged(CAN) DURING A MTCE PREP VISIT FOR RETURNING THE A/C BACK TO LESSOR , MTCE IDENTIFIED A PROBLEM WITH NR 2 ENGINE LP VALVE DURING THE OPERATIONAL TEST OF THE VALVE IAW TASK 28-24-00-790-003. FURTHER TROUBLESHOOTING IDENTIFIED WIRE DL-20-AE-FR-F, SPEC MIL-W-250SDR 97CW1Wire Harness · chafedTHE FUEL PUMP WIRING HARNESS IS NOT SUPPORTED WITHIN THE FUEL CELL AND CHAFED ON THE ALUMINUM FUEL LINE FROM THE PRIMARY PUMP TO THE CHECK VALVE INSIDE THE FUEL CELL. THERE WAS .006 INCHES DAMAGE TO THE WALL OF THE FUEL LINE AND THE SHIELDING ON THE PUMP WIRISDR B30R20033017Wire Harness · chafedIN TROUBLESHOOTING A SUBMERGED FUEL BOOST PUMP CIRCUIT BREAKER POPPING, MAINTENANCE TECHNICIANS DISCOVERED THE FUEL BOOST PUMP ELECTRICAL HARNESS HAD CHAFFED THROUGH THE BUNDLE INSULATION AND WAS ARCING ON ALUMINUM FUEL LINE P/N 6526355-37 INSIDE THE WET WING.SDR B30R20033018Wire · arcedIN TROUBLESHOOTING A SUBMERGED FUEL BOOST PUMP CIRCUIT BREAKER POPPING, MAINTENANCE TECHNICIANS DISCOVERED THE FUEL BOOST PUMP ELECTRICAL HARNESSES HAD CHAFED THROUGH THE BUNDLE INSULATION AND WAS ARCING ON ALUMINUM FUEL LINES P/N 6526355-37 INSIDE BOTH THE LESDR ABXA030370Wire · burnedLEFT AFT BOOST PUMP AND RADIO RACK COOLING VALVE WIRES CHARRED AT STATION 237 (P1-1061L). REPAIRED WIRES HV-Q 13A20B, HV-Q 12A20C, H 211A24 IAW W.D. MANUAL 28-21-00 AND 21-21-00. LEFT AFT BOOST PUMP AND RADIO RACK COOLING VALVE. OPS CHECK GOOD.SDR 030926DWire Harness · chafedDURING INTERNAL INSPECTION OF THE FUEL BAYS FOUND FUEL PUMP WIRING HARNESSES IN RIGHT WING WAS DAMAGED BY CHAFFING THROUGH THE WIRING INSULATION. WIRING WAS CHAFFING AGAINST ALUMINUM FUEL LINE INSIDE TANK. CHAFFING CAUSED WEAR BEYOND LIMITS TO ALUMINUM FUEL SDR 030926CWire Harness · chafedDURING INTERNAL INSPECTION OF THE FUEL BAYS FOUND FUEL PUMP WIRING HARNESSES IN RIGHT WING WAS DAMAGED BY CHAFFING THROUGH THE WIRING INSULATION TO BEAR WIRE. WIRING WAS CHAFFING AGAINST ALUMINUM FUEL LINE INSIDE TANK. CHAFFING CAUSED WEAR BEYOND LIMITS TO ASDR 030926BWire Harness · chafedDURING INTERNAL INSPECTION OF THE FUEL BAYS FOUND FUEL PUMP WIRING HARNESSES IN RIGHT WING WAS DAMAGED BY CHAFFING THROUGH THE WIRING INSULATION. WIRING WAS CHAFFING AGAINST ALUMINUM FUEL LINE INSIDE TANK. CHAFFING CAUSED WEAR BEYOND LIMITS TO ALUMINUM FUEL SDR 030926AWire Harness · chafedDURING INTERNAL INSPECTION OF THE FUEL BAYS FOUND FUEL PUMP WIRING HARNESSES IN BOTH WINGS WERE DAMAGED BY CHAFFING THROUGH THE WIRING INSULATION. WIRING WAS CHAFFING AGAINST ALUMINUM FUEL LINES AND PUMP BODY INSIDE TANK. CHAFFING CAUSED WEAR BEYOND LIMITS TSDR VERTEX2Wire · sparksRIGHT BOOST PUMP WIRING CHAFED ON MOTIVE FLOW FEED LINE IN FUEL BAY. CHAFED WIRE CAUSED ELECTRICAL ARC DAMAGE TO FUEL LINE. THIS APPEARS TO BE AN ORIGINAL BOOST PUMP. PROBLEM WAS NOTED DURING DEFUELING USING THE BOOST PUMP TO REMOVE FUEL FOR MAINTENANCE. THE 1SDR CA030903017Connector · burned(CAN) PILOT'S SELECTED RT MAIN BOOST PUMP ON AND CIRCUIT BREAKER POPPED. CIRCUIT BREAKER POPPED AGAIN AND WAS LEFT ALONE FOR REMAINDER OF FLIGHT. THE BOOST PUMP WAS REMOVED AND FOUND THAT THE CONNECTOR ON THE PUMP AND THE AIRFRAME WIRING HAD SHORTED INTERNALLYSDR AUS20030820Wire · chafed(AUS) FUEL BOOST PUMP WIRING CHAFING NEAR PLUG. FOUND DURING INSPECTION IAW SB PC12/37.SDR AUS20030798Wire Harness · worn(AUS) BOOST PUMP WIRING HARNESS CHAFED. FOUND DURING INSPECTION IAW AD/SWSA226/88.SDR AUS20030819Wire · worn(AUS) FUEL BOOST PUMP WIRING CHAFING. FOUND DURING INSPECTION IAW SBPC12/37.SDR AUS20030818Wire · chafed(AUS) LT AND RT FUEL BOOST PUMP WIRING CHAFING. FOUND DURING INSPECTION IAW SB PC12/37.SDR MEX2003258Wire · failedDURING FUELING SERVICE, WAS DETECTED THE REFUELING CONTROL PANEL OUT OF SERVICE. DURING REVISION WAS DETECTED THE BREAKER E-5 OF PANEL P-11 DAMAGED. THE REFUELING CONTROL PANEL WAS DEFERRED IAW MEL 28-41-6. THE REFUELING CONTROL PANEL WIRING WAS REPAIRED IASDR CALA0300334Wire Harness · burnedTHE AFT FUEL BOOST PUMP LOW PRESSURE LIGHT LEFT SIDE ILLUMINATED AFTER LANDING AT DFW. WHILE TROUBLESHOOTING THE PUMP THE WIRE BUNDLE AT STA 254 IN COCKPIT WAS FOUND BURNED. OVERHEATING OF THE PUMP WAS SUSPECTED TO BE THE CAUSE OF THE BURNT WIRING. THE FUELSDR HEEA086977Connector · corrodedFUEL FILTER PIN IN CONNECTOR CORRODED OUT. REPLACED.SDR U30A200300015Connector · arcedDURING MAINTENANCE INSPECTION, DURING ENGINE RUN, AN ECAM MESSAGE FOR THE RT FUEL TANK PUMP NR 2, LOW PRESSURE. FURTHER TROUBLESHOOTING REVEALED ELECTRICAL ARCING AT THE RT WING FUEL PUMP WIRE HARNESS CONNECTOR. RELATED CIRCUIT BREAKER DID NOT TRIP. REPLACED FSDR CA030508001Wire · chafed(CAN) DUE TO PREVIOUS FIND OF FUEL BOOST PUMP WITH A CHAFED WIRING HARNESS, THE BOOST PUMPS WERE REMOVED FOR PRECAUTIONARY INSPECTION. CHAFED WIRES ON HARNESS WERE FOUND ON THERIGHT SIDE PUMP. LT PUMP WAS OLD STYLE PUMP STILL INSTALLED WITH HARNESS COMING OUTSDR CA030422001Wire · chafed(CAN) AIRCRAFT WAS INSPECTED DUE TO FINDINGS ON PREVIUOS AIRCRAFT IN OUR FLEET. BOTH THE LT AND RT AIRFRAME FUEL BOOST PUMPS WERE FOUND WITH CHAFED WIRES IN THE HARNESS. A VERY CLOSE VISUAL INSPECTION WAS NEEDED TO FIND THE DAMAGE.PILATUS HAS BEEN CONTACTED SDR CA030425010Wire · burned(CAN) MAINTENANCE FOUND NR 2 MAIN AFT FUEL LOW PRESSURE LIGHT ILLUMINATED DURING OVERNIGHT MAINTENANCE. SYSTEM INSPECTED, RELATED CIRCUIT BREAKER FOUND POPPED. AIRCRAFT RELEASED UNDER MEL 28-1-1. MAINTENANCE REPLACED NR 2 AFT FUEL BOOST PUMP - SYSTEM DID NOT SDR CA030330001Circuit Breaker · shorted(CAN) IN CRUISE, THE FLIGHT CREW REPORTED A CROSSFLOW PUMP CAUTION MESSAGE ALONG WITH AUTO CROSSFLOW INHIBIT STATUS MESSAGE. SHORTLY AFTER, THE FUEL IMBALANCE CAUTION MESSAGE APPEARED. A 500 KG IMBALANCE DEVELOPED. THE TANKS READOUT WAS LT 2300, CTR 0, RT 1SDR 2003FA0000205Wire · chafedTHE WIRE PROVIDING A NEUTRAL AND POWER TO THE PUMP EXITS/ENTERS PUMP USING A SEALED AN FLARE FITTING CAUSING CHAFING TO OCCUR.SDR DHL2003741002Connector · contaminatedIN CRUISE, FL290 BOTH AFT BOOST PUMP LOW PSI LIGHTS ILLUMINATED IN THE FUEL TANK NR 2 AT THE SAME TIME BOTH CIRCUIT BREAKERS POPPED. PERFORMED ABNORMAL PROCEDURES. INSPECTED FUEL PUMPS AND PLUG CONNECTIONS, CLEANED AND RESET PLUGS, RESET BREAKERS, OPERATED PSDR CA030224002Wire · chafed(CAN) A FUEL BOOST PUMP WAS REPLACED FOR ITS SCHEDULED OVERHAUL REPLACEMENT AT 3500 HOURS.A WIRE WAS FOUND CHAFED TO BARE WIRE THROUGH ROUGHLY MIDWAY OF THE MANUFACTURER SUPPLIED HARNESS. THIS COULD HAVE THE POTENTIAL TO IGNITE THE FUEL TANK IF SPARKS WERE PRSDR AUS20030411Wire Harness · worn(AUS) LEFT FORWARD BOOST PUMP LOOM CHAFED AGAINST RIGID FUEL LINE PN 120-08735-047 LOCATED IN THE TANK. LOOM INCORRECTLY ROUTED.SDR CA030203005Wire · broken(CAN) PUMP WAS INSTALLED ON JANURAY 13, 2003. AIRCRAFT WAS RUN FOR 1.5HRS OVER THE 16TH, 17TH, 18TH OF JANUARY.ON THE 19TH THE PILOT NOTED THAT THE NR 2 PUMP WAS OPERATING INTERMITTENTLY. INSPECTION REVEALEDTHAT THE HOLE IN THE COVER FOR THE WIRE WAS OUT BY 1
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