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 AU000863Wire · worn(AUS) LT AND RT AUXILIARY FUEL BOOST PUMP WIRES WORN.Sep 13, 2000 · Frchld SA227DCSDR AU000864Wire · worn(AUS) LT AUXILIARY BOOST PUMP WIRE INSULATION WORN.Sep 8, 2000 · Frchld SA227DCSDR AU000737Wire · worn(AUS) CENTRE FUL TANK FLOAT SWITCH WIRING CHAFING APPROXIMATELY 100MM (4IN) FROM END. FOLLOWING REMOVAL OF THE WIRE FUEL CONTAMINATIONOF THE FLOAT SWITCH WAS EVIDENT.Sep 1, 2000 · Boeing 737376SDR ABXA000346Wire · burnedON PRE-DEPARTURE CHECK FOUND FUEL LEAKING FROM LEFT WING, INBOARD FORWARD SPAR AREA. REPLACED FUEL CONDUIT TO LEFT FORWARD BOOST PUMP. FOUND WIRING LOOSE AND BURNED AT TERMINAL STRIP NR S3-1 AND TERMINAL NR 4. SPLICED WIRES 1Q11C20A AND 1Q11E20A IAW ABX REAJul 19, 2000 · N977AX · Doug DC941SDR AU001283Wire · damaged(AUS) KAPTON WIRES LOCATED IN REFUEL PANEL HAVE DAMAGED INSULATION ALLOWING THE WIRES TO BE EXPOSED.Jun 15, 2000 · Boeing 737377SDR AALA20000728Connector · looseDFW - FLT 1044 - EN ROUTE FOR RETURN TO DFW, AFTER NR 3 ENGINE SHUTDOWN LEFT NOZZLE ON FUEL DUMP VALVE DID NOT OPEN DURING FUEL DUMP. AIRCRAFT LANDED DFW WITHOUT INCIDENT. CANNON FOR DUMP VALVE LOOSE AND DIRTY. CLEANED AND SECURED CANNON PLUG. SYSTEM GROUNMay 3, 2000 · N873AA · Boeing 727223SDR C2XA00IA100Wire · chafedRIGHT FUEL QTY INDICATOR FLUCTUATES IN FLIGHT. FOUND RIGHT NR 3 FUEL PROBE WIRING CHAFING AND SHORTING ON FUEL LINE INSIDE RIGHT FUEL TANK. INSULATED WIRE WITH HEAT SHRINK AND SECURED WIRING TO PREVENT FURTHER CHAFING IAW AWM 20-21-00. FUNCTIONAL CHECK OF FApr 10, 2000 · N15725 · Emb EMB120RTSDR 20000425SH041Wire · shortedWHILE C/W SB 8-28-31, SPECIAL INSP OF FUEL TANK BONDING, MECH RECEIVED ELEC SHOCK WHEN HE TOUCHED FUEL PROBE WIRING HARNESS CONDUIT LOCATED BETWEEN STA YW189.0 AND YW207.0 IN RT FUEL TANK. CONDUIT FOUND TO THE ''LIVE'' WITH 20 VAC. INSP REVEALED EVIDENCE OF Mar 30, 2000 · N811PH · Dhav DHC8102SDR AU000161Wire · contaminated(AUS) FUEL QUANTITY SYSTEM WIRING AND CONNECTOR CONTAMINATED WITH FUEL. THE FUEL WAS WICKING THROUGH THE WIRES BY CAPILLARY ACTION.Mar 25, 2000 · Frchld SA227DCSDR UPS00531506Wire · chafedINSPECTION TYPE:SEG, WHILE GIVING OK TO CLOSE FOUND CONDUIT AND WIRE FOR NR 2 ENGINE FUEL SHUTOFF VALVE DAMAGED AT AFT END ON CONDUIT AND WHERE WIRE PASSES THROUGH LIGHTING HOLE ON WEB JUST FWD OF 445CL. REPLACED WIRE W3484-1007-18, RAN WIRE FROM RIGHT SPAR FJan 18, 2000 · N407UP · Boeing 75724APFSDR TWAA9914605Wire · brokenWHILE THE AIRCRAFT WAS ON THE GROUND SPARKS WERE OBSERVED COMING FROM THE FUELING PANEL. REPLACED A BROKEN WIRE. CC00 9-4-99 STL.Oct 26, 1999 · N992Z · Doug DC931SDR CA991007002Wire · broken(CAN) NR 2 ENGINE LOW FUEL PRESSURE LIGHT DOESN'T ALWAYS ILLUMINATE ON ENGINE SHUT DOWN. BROKEN WIRE FOUND AT CANNON PLUG BACKSHELL.Sep 23, 1999 · Dhav DHC8311SDR 99ZZZM651Wire · damagedGATE RETURN FOR NR 2 ENGINE FLAME OUT AFTER ONE MINUTE AFTER START. RT ENGINE VALVE AND SPAR VALVE LIGHT ILLUMINATED AND EICAS MESSAGE. RT FUEL SPAR VLV AND RT ENGINE FUEL VLV DISPLAYED, WITH FUEL CONTROL SWITCH IN RUN. NO FUEL FLOW INDICATED. REPAIR BAD WSep 1, 1999 · N908AW · Boeing 7572G7SDR USAASB99150Wire Harness · failedRDU - FLT 2826 - EN ROUTE FROM MCO TO BOS, DURING CRUISE, CAPT REPORTED PROBLEMS WITH THE NR 2 FUEL GAUGE. GAUGE WAS UNRELIABLE WITH ITS READINGS AND THE NR 1 FUEL GAUGE WAS ALREADY ON MEL. CREW TRIED RESETTING CIRCUIT BREAKER WITH NO HELP. THE NR 2 FUEL GAJun 20, 1999 · N268AU · Boeing 7372B7SDR AALA990840Wire · looseJFK - FLT 1540 - EN ROUTE JFK-PAP - DURING CRUISE LEFT INNER FUEL QTY DROPPED BY 10,000 LBS AND REMAINED LOW THE REMAINEDER OF THE FLIGHT. WHEN LEFT INNER FUEL TANK REACHED ZERO, XX'S WERE DISPLAYED FOR REMAINDER OF FLIGHT. LANDED JFK WITHOUT INCIDENT. RESEMay 24, 1999 · N70072 · Airbus A300B4605RSDR USAAD99065Wire Harness · damagedLGA-MCO - FLT 259 - EN ROUTE THE AFT LEFT FUEL BOOST PUMP, 'A' PHASE AND THE FORWARD LEFT FUEL BOOST PUMP, 'A' PHASE CIRCUIT BREAKERS TRIPPED. SHORTLY AFTERWARDS BOTH BOOST PUMPS FAILED ON THE LEFT SIDE AS WELL AT THE RIGHT AFT BOOST PUMP. ALL THREE PHASES OMay 16, 1999 · N822US · Doug DC982SDR 99ZZZX1987Wire · shortedPILOT DISCREPANCY: LEFT LANDING LIGHT CIRCUIT BREAKER TRIPPED, RESET TO NO AVAIL. INVESTIGATION REVEALED SHIELDED POWER WIRE SHORTED TO SHIELD AT CRIMP ENTERING PUMP, EVIDENCE OF EXCESSIVE HEAT.Apr 27, 1999 · Cessna 310RSDR AU990561Wire · faulty(AUS) NR 2 MAIN AFT BOOST PUMP WIRING INSULATION FAULTY.Apr 9, 1999 · Boeing 747312SDR CA990308015Wire · chafed(CAN) THE THREADS OF THE UPPER HORIZONTAL PANEL SUPPORT ATTACHMENT SCREW CHAFING ON AN UNPROTECTED WIRE BUNDLE CAUSING TWO WIRES TO ARC BETWEEN EACH OTHER AND MELTING THE INSULATION. SMOKE NOT REPORTED BY PILOT, BUT WAS NOTED DURING TROUBLESHOOTING. WIRING RMar 1, 1999 · Cessna 550SDR CA990308024Wire · shorted(CAN) RIGHT WING NR 1 FUEL BOOST PUMP ELECTRICAL SUPPLY WIRES FOUND ARCING AGAINST WING PLANK CAUSING SIGNIFICANT MATERIAL LOSS IN WING STRUCTURE AND DAMAGE TO WIRE INSULATION.Feb 10, 1999 · Airbus A320211SDR CA990310056Wire · chafed(CAN) DURING AD COMPLIANCE, WIRES FOUND CHAFED IN CENTER TANK FUEL LEVEL SWITCH. CHAFE LOCATED AT FRONT SPAR CONDUIT EXIT POINT AND MEASURED 1.25 INCHES IN LENGTH. STRANDS WERE BROKEN AND PROTUDING, NO VISIBLE SIGNS OF ARCING AT CHAFE POINT. FUEL WAS DISCOJan 29, 1999 · Boeing 737275SDR 99ZZZX352Wire · chafedDURING ANNUAL INSPECTION, TOP INSPECTION PANEL ON THE RT WING AUXILIARY TANK WAS LEAKING FUEL. UPON REMOVAL OF THE PANEL TO REPLACE THE GASKET, NOTICED THE FUEL QUANTITY SENDING UNIT WIRES INSIDE THE FUEL TANK WERE EXCEPTIONALLY LONG. UPON EXAMINATION OF THEDec 21, 1998 · N4919A · Cessna 310RSDR CA990111030Wire · chafed(CAN) DUE TO REPEAT/INTERMITTENT RIGHT FUEL INDICATION FLUCTUATION SNAG. INVESTIGATION FOUND FUEL QUANTITY SYSTEM WIRING IN RIGHT HAND FUEL TANK AREA CHAFING AGAINST A FUEL PROBE.Dec 13, 1998 · Dhav DHC8301SDR CA981125009Wire · chafed(CAN) FUEL QUANTITY SYSTEM WIRING FOUND CHAFED. CHAFING IS WHERE WIRING FROM TANK SENSOR PASSES THROUGH TY WRAPS.Nov 12, 1998 · Bag BAE146200ASDR CA981109048Wire · chafed(CAN) RIGHT HAND FUEL QUANTITY INDICATOR INTERMITTENTLY ROTATES CLOCKWISE. FUEL PROBE REPLACED AT WS 115.9 AND WIRE REPAIRED BETWEEN CENTER TUBE AND THE TOP TERMINAL PROBE.Oct 25, 1998 · Swrngn SA226TCSDR COMA9810229Wire Harness · out of positionDURING 2C INSPECTION, TASK 5720-622-01I, REVEALED THE WIRE HARNESS FOR THE RIGHT WING FORWARD FUEL BOOST PUMP TO BE CHAFFING ON THE METAL BRAIDED FUEL LINE. PUMP WIRE INSULATION WAS NOT DAMAGED ONLY WIRE HARNESS PROTECTIVE COVERING. REMOVED PUMP AND HARNESS Oct 7, 1998 · N247CA · Emb EMB120RTSDR CA980916026Wire · chafed(CAN) AFTER TAKEOFF, THE GROUND REFUEL AND FUEL TANK FILL VALVE AND BATTERY BUS SENSING CIRCUIT BREAKERS TRIPPED. ALSO, BATTERY BUS OFF LIGHT CAME ON. BOTH CIRCUIT BREAKERS RESET AND TRIPPED AGAIN, AIRCRAFT RETURNED. FOUND WIRE CHAFED AT EXTERNAL REFUEL PANSep 6, 1998 · Doug DC1030SDR DHL98803001Wire · brokenNR 4 ALT QUAN LOW LIGHT ILLUMINATED. USED ABNORMAL PROCEDURE AND LIGHT WOULD NOT EXTINGUISH. NR 4 ALT SHUT OFF VALVE CLOSED AND LIGHT WOULD NOT EXTINGUISH WHILE USING ABNORMAL PROCEDURE. FOUND BROKEN WIRE AT CANNON PLUG P1-113 TO ALT NR 4 REFILL SOLENOID. May 22, 1998 · N803DH · Doug DC873FSDR 98ZZZX1285Wire · shortedPILOT REPORTED FIRE ERUPTED FROM THE FUEL VENT IN-FLIGHT. AIRCRAFT LANDED SAFELY WITH NO VISIBLE DAMAGE. TROUBLESHOT CAUSE TO SENDING UNIT POWER WIRE CHAFING AT LT WING ROOT RIB. REPLACED WIRING FROM SENDING UNIT TO GAUGE.Mar 12, 1998 · N25053 · Cessna 152SDR 97ZZZX4862Wire · chafedTEB - WHILE IN-FLIGHT, LEFT ALTERNATE BOOST PUMP FAIL LIGHT ILLUMINATED. ON GROUND, MAINTENANCE FOUND PUMP INOPERABLE AND WIRE Q127A8 CHAFED AND ARCING ON DUCT P/N 1159AC-20507-1 IN RT WING ROOT. REPLACED WIRE Q127A8 AND THREE OTHERS IN WIRE BUNDLE W300. RENov 13, 1997 · N118NP · Gulstm G1159SDR 97ZZZM1147Wire · wrong partEN ROUTE FROM DET TO MMU - THE LOW FUEL LIGHT FLICKERED ON. THE FUEL GAUGES INDICATED MORE THEN SUFFICIENT FUEL WITH RESERVES TO COMPLETE THE FLIGHT. THE FLIGHT CREW ELECTED TO DIVERT TO ELM AND LANDED WITHOUT INCIDENT. SUBSEQUENT INVESTIGATION REVEALED THAOct 11, 1997 · N165G · Gulstm G1159ASDR AU970760Wire · failed(AUS) NO2 FUEL BOOST PUMP ELECTRICAL WIRING INSULATION FAILED DUE TO CONDUCTIVE CORROSION AT THE WIRE TERMINAL ASSEMBLYApr 24, 1997 · Boeing 747312SDR PNSA970311Wire · brokenLEFT FUEL JET PUMP FAIL LIGHT CAME ON DURING CLIMB. REPAIRED WIRE ON TRANSFER SELECT SWITCH.Mar 25, 1997 · N544AL · Cessna 441SDR AU970164Wire · worn(AUS) RH FUEL TANK CAPACITANCE PROBE WIRES CHAFING ON FUEL PLUMBING IN THREE DIFFERENT AREASFeb 10, 1997 · Emb EMB120SDR CALA9601558Wire Harness · chafedTHE AFT LEFT FUEL TANK BOOST PUMP AND FORWARD LEFT FUEL TANK BOOST PUMP CIRCUIT BREAKERS TRIPPED ON FINAL APPROACH TO MIA. THE AFT LEFT FUEL BOOST PUMP CIRCUIT BREAKER COULD NOT BE RESET. THE FORWARD LEFT FUEL TANK BOOST PUMP CIRCUIT BREAKER WAS RESET, BUT THENov 4, 1996 · N77827 · Doug DC982SDR USAABB96025Wire · shortedPIT - FL 114 - AFTER TAKEOFF FROM PIT, CREW RECEIVED EICAS MESSAGE 'L FUEL SPAR VAL'. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE WIRE TO THE SPAR VALVE AT THE CONNECTOR SHORTING TO THE SHIELDING. THE WIRE WAS REPAIRED.Aug 23, 1996 · N633AU · Boeing 7572B7SDR AU960535Wire · worn(AUS) WING TIP FUEL TANK CONTENTS WIRE WORN BY TIP TANK LOWER SKIN INNER SURFACE - WIRE WAS INADEQUATELY RESTRAINED AND CLAMPEDApr 29, 1996 · Cessna 402BSDR AU960177Wire · damaged(AUS) WIRES DAMAGED IN AREA BEHIND FLIGHT ENGINEERS PANEL - WIRES DAMAGED WERE:- 1. SINGLE TWISTED WIRE WITH TWO WIRES SEVERED - P61 RH SIDE PANEL WIRE NO W062-209R18 - FUEL TEMPERATURE INDICATOR - ATA 28 WIRE NOW062-209R18 - FUEL TEMPERATURE INDICATOR - ATAJan 31, 1996 · Boeing 767277SDR A6WR95046Wire · corrodedDURING C-CHECK, FOUND NR 4 ENGINE LOW PRESSURE FUEL COCK CABLE CIRCUIT CORRODED. FOUR CABLES FROM FUSELAGE FRAME 18 TO L.P. COCK. REPLACED CABLES. REFERENCE CONTROL NR 95ZZZX6266, NR 95ZZZX6267, AND NR 95ZZZX6268. (X)Oct 17, 1995 · N2FOR · Bag BAE146100ASDR A6WR95040Wire · corrodedDURING C-CHECK, FOUND NR 3 ENGINE LOW PRESSURE FUEL COCK CABLE CIRCUIT CORRODED. FOUR CABLES FROM FUSELAGE FRAME 18 TO L.P. COCK. REPLACED CABLES. REFERENCE CONTROL NR 95ZZZX6263, NR 95ZZZX6264, AND NR 95ZZZX6265. (X)Oct 17, 1995 · N2FOR · Bag BAE146100ASDR A6WR95036Wire · corrodedDURING C-CHECK, FOUND NR 2 ENGINE LOW PRESSURE FUEL COCK CABLE CIRCUIT AT CENTER AREA OF LT WING CORRODED. REPLACED CABLES. REFERENCE CONTROL NR 95ZZZX6255, NR 95ZZZX6256, AND NR 95ZZZX6257. (X)Oct 17, 1995 · N2FOR · Bag BAE146100ASDR A6WR95035Wire · corrodedDURING C-CHECK, FOUND NR 1 ENGINE LOW PRESSURE FUEL COCK CABLE CIRCUIT CORRODED. ALL FOUR CABLES FROM FUSELAGE FRAME 18 TO L.P. COCK. REPLACED CABLES. REFERENCE OPERATOR CONTROL NR 95ZZZX6258, NR 95ZZZX6259, AND NR 95ZZZX6260. (X)Oct 17, 1995 · N2FOR · Bag BAE146100ASDR 95ZZZX6268Wire · corrodedDURING C-CHECK, FOUND NR 4 ENGINE LOW PRESSURE FUEL COCK CABLE CIRCUIT CORRODED. FOUR CABLES FROM FUSELAGE FRAME 18 TO L.P. COCK. REPLACED CABLES. REFERENCE CONTROL A6WR95046, NR 95ZZZX6266, AND NR 95ZZZX6267.Oct 17, 1995 · N2FOR · Bag BAE146100ASDR 95ZZZX6267Wire · corrodedDURING C-CHECK, FOUND NR 4 ENGINE LOW PRESSURE FUEL COCK CABLE CIRCUIT CORRODED. FOUR CABLES FROM FUSELAGE FRAME 18 TO L.P. COCK. REPLACED CABLES. REFERENCE CONTROL A6WR95046, NR 95ZZZX6266, AND NR 95ZZZX6268.Oct 17, 1995 · N2FOR · Bag BAE146100ASDR 95ZZZX6266Wire · corrodedDURING C-CHECK, FOUND NR 4 ENGINE LOW PRESSURE FUEL COCK CABLE CIRCUIT CORRODED. FOUR CABLES FROM FUSELAGE FRAME 18 TO L.P. COCK. REPLACED CABLES. REFERENCE CONTROL A6WR95046, NR 95ZZZX6267, AND NR 95ZZZX6268.Oct 17, 1995 · N2FOR · Bag BAE146100ASDR 95ZZZX6265Wire · corrodedDURING C-CHECK, FOUND NR 3 ENGINE LOW PRESSURE FUEL COCK CABLE CIRCUIT CORRODED. FOUR CABLES FROM FUSELAGE FRAME 18 TO L.P. COCK. REPLACED CABLES. REFERENCE CONTROL A6WR95040, NR 95ZZZX6263, AND NR 95ZZZX6264.Oct 17, 1995 · N2FOR · Bag BAE146100ASDR 95ZZZX6264Wire · corrodedDURING C-CHECK, FOUND NR 3 ENGINE LOW PRESSURE FUEL COCK CABLE CIRCUIT CORRODED. FOUR CABLES FROM FUSELAGE FRAME 18 TO L.P. COCK. REPLACED CABLES. REFERENCE CONTROL A6WR95040, NR 95ZZZX6263, AND NR 95ZZZX6265.Oct 17, 1995 · N2FOR · Bag BAE146100ASDR 95ZZZX6263Wire · corrodedDURING C-CHECK, FOUND NR 3 ENGINE LOW PRESSURE FUEL COCK CABLE CIRCUIT CORRODED. FOUR CABLES FROM FUSELAGE FRAME 18 TO L.P. COCK. REPLACED CABLES. REFERENCE CONTROL A6WR95040, NR 95ZZZX6264, AND NR 95ZZZX6265.Oct 17, 1995 · N2FOR · Bag BAE146100ASDR 95ZZZX6260Wire · corrodedDURING C-CHECK, FOUND NR 1 ENGINE LOW PRESSURE FUEL COCK CABLE CIRCUIT CORRODED. ALL FOUR CABLES FROM FUSELAGE FRAME 18 TO L.P. COCK. REPLACED CABLES. REFERENCE OPERATOR CONTROL NR A6WR95035, NR 95ZZZX6258, AND NR 95ZZZX6259.Oct 17, 1995 · N2FOR · Bag BAE146100ASDR 95ZZZX6259Wire · corrodedDURING C-CHECK, FOUND NR 1 ENGINE LOW PRESSURE FUEL COCK CABLE CIRCUIT CORRODED. ALL FOUR CABLES FROM FUSELAGE FRAME 18 TO L.P. COCK. REPLACED CABLES. REFERENCE OPERATOR CONTROL NR A6WR95035, NR 95ZZZX6258, AND NR 95ZZZX6260.Oct 17, 1995 · N2FOR · Bag BAE146100A
Back to JASC 2897