JASC 5797
Service difficulty reports · 81
Reports filed under 5797 · Wing 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 = '5797' 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 = '5797' 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 UIEA2017041400575Wire · chafedFOUND WIRES CHAFED AT THE NR 3 WING LEADING EDGE COVER. SPLICED THE WIRES AND PERFORMED CONTINUITY CHECK IAW SWPM 26-30-12, REV 64, WDM 73-21-83, 73-21-35, AND 26-11-34, REV 41. THE RESULT WAS SATISFACTORY. PERFORMED NR 3 ENGINE EEC SATISFACTORY TEST AND TSDR AALA201609169003Connector · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON LT WING INBD FLAP INTERCONNECTING STRUT ELECTRICAL CONNECTOR. REPLACED INTERCONNECTING STRUT IAW AMM 27-51-44-820-001-A.SDR CA151113007Connector · corroded(CAN) ON REAR SPAR OF WING CORROSION FOUND INSIDE CONNECTORS. QTY FOUND CONDITION OF CORROSION ON MANY CONNECTORS ON REAR SPAR OF WING, PN 1005701001-001. FINISH CODE OF CONNECTOR`S BACKSHELLS IS M-ALUMINIUM ELECTROLESS NICKEL CONDUCTIVE 48 HRS SALT SPAY.SDR IEYR2014102100001Wire · shortedDURING TROUBLESHOOTING A NAVIGATION LIGHT ISSUE, FOUND SMALL MINOR BURN MARKS ON MULTIPLE RIBS IN BOTH WINGS WHERE THE WIRING HAD CAME OUT OF THE STRINGER FROM AN STC. THE EFFECTED STC WOULD BE EITHER STC SA03913AT OF THE WING NAVIGATION LIGHTS OR STC SA02723SDR SWIA201439611Shield · contaminatedLEFT WING L/E WIRE HARNESS, BRAIDED SHIELD IS CONTAMINATED, DISCOLORED UNDER PLASTIC SHEATH, LWS 242.00. C-CHECK, REMOVED OUTER JACKET INSULATION FROM APPROXIMATELY LWS 230.00 TO LWS 250.00 AND WIPED DISCOLORATION OFF WITH ISOPROPYL ALCHOHOL AND A RAG. REPAISDR RAIA201407040003Bonding Strap · corrodedFECU ACCESS PANEL BONDING STRIPS ARE CORRODED. MAINTENANCE REMOVED CORROSION AND REINSTALLED FECU PANEL.SDR CA131002006Pcb · burned(CAN) SPEEDBRAKE CIRCUIT BREAKER POPS OUT ON FINAL. SPEEDBRAKE EXTEND ANNUNCIATOR COMES ON, ON FINAL.SDR CALA2013081490453Connector · worn3 INCHES FROM LT WING PROBE, NR 12 CONNECTOR, THE YELLOW HARNESS WIRE HAS INSULATION THAT IS WORN THROUGH TO CORE WIRE. ACCOMPLISHED REPAIR OF WIRING AT LT WING PROBE IAW AMM. ACCOMPLISHED UNIMATIC REPORTING AS REQUIRED.SDR CALA2013081490431Wire · damaged3 INCHES FROM LEFT WING PROBE NR 12 CONNECTOR, THE YELLOW HARNESS WIRE HAS INSULATION THAT IS WORN THROUGH TO CORE WIRE. ACCOMPLISHED REPAIR OF WIRING AT LT WING PROBE IAW AMM.SDR REXA2013071001086Bonding Jumper · out of positionLEFT INBD FLAP CENTER VANE ACTUATOR BONDING JUMPER POSITIONED INCORRECTLY CAUSING CHAFE DAMAGE TO UPPER SKIN. REPAIRED IAW SRM 57-00-31 AND 51-12-00.SDR CA130527007Wire Harness · damaged(CAN) DURING CRUISE, THE FLIGHT CREW REPORTED THE RT SIDE WING-BODY OVERHEAT ANNUNCIATOR ILLUMINATE AND THEN EXTINGUISH AFTER 20 SECONDS. DUE TO FORECAST ICING CONDITIONS WHICH WOULD LIMIT THE ACFT OPERATIONALLY UNDER MEL 26-13-1, WING-BODY OVERHEAT DETECTOR SDR UALA2013051403342Wire · damagedWHILE INSPECTING FLAP TRACK FOR LUBRICATION, OBSERVED ELEMENT EROSION OF EXPOSED WIRE CONDUITS THAT WOULD NORMALLY BE PROTECTED BY REMOVING CANOE FAIRING. WEAR THRU ALL LAYERS IN TWO PLACES EXPOSING CORE LEADS. NOT ABLE TO ANCHOR CONDUITS LEADS TO SEVERE BUSDR CA130321002Wire · chafed(CAN) DURING MAINTENANCE INSPECTION, CHAFING WAS DISCOVERED ON THE SPIRAL ELECTRICAL CORD LOCATED IN THE OTBD TELESCOPIC DUCT OF THE RT WING L/E. THE SAME WAS FOUND AT THE LT WING OTBD LOCATION. BOTH SPIRAL CORDS TO BE REPLACED IAW CMM 30-11-07.SDR CA130304012Wire Harness · chafed(CAN) DURING TROUBLESHOOTING OF AN INOPERATIVE GALLEY OVEN, SEVERE DAMAGE WAS FOUND TO A WIRE BUNDLE AT THE LT INBD WING REAR SPAR, AT WING STATION YW117,20. DAMAGE HAS APPARENTLY STARTED WITH CHAFED WIRE INSULATION AND HAS PROGRESSED TO AN OVERHEAT DAMAGE OFSDR CA130225012Wire · chafed(CAN) DURING MAINTENANCE INSPECTION, CHAFING WAS DISCOVERED ON THE SPIRAL ELECTRICAL CORD LOCATED IN THE INBD TELESCOPIC DUCT OF THE LT WING L/E. THE SAME WAS FOUND AT THE INBD AND OTBD RT WING L/E LOCATIONS. THE CHAFED SPIRAL CORDS WILL BE REPLACED IAW CMM 3SDR CA130214005Feeder Cable · chafed(CAN) DURING MAINTENANCE INSPECTION CHAFING WAS DISCOVERED ON THE SPIRAL ELECTRICAL CORD LOCATED IN THE INBD TELESCOPIC DUCT OF THE RT WING L/E. THE SAME WAS FOUND AT THE LT WING OTBD LOCATION. BOTH SPIRAL CORD HARNESSES WERE REPLACE IAW CMM 30-11-07.SDR CA120217005Feeder Cable · chafed(CAN) DURING INSPECTION, CHAFING WAS DISCOVERED ON THE SPIRAL ELECTRICAL CORD LOCATED IN THE OTBD TELESCOPIC DUCT IN THE LT L/E. THE SPIRAL ELECTRICAL CORD MAKES THE CONNECTIONS FOR THE SLAT DISCONNECT SENSORS, THE ANTI-ICE TEMPERATURE SENSORS, AND THE BLEED SDR CA120111001Wire Harness · chafed(CAN) THE HARNESS WAS RUBBING ON A BRACKET, PN 170-31533-401, SRM 57-50-00, AT THE WING ROOT. THE 4 WIRES DAMAGED ARE W502-00178-24 GOES FROM P0589-P1249 THE LT OTBD FLAP SKEW SENSOR T4, W502-00046-24 GOES FROM P0589-P0915 GROUND SPOILER PROX SENSOR, W502-000SDR UALA2012010300025Bonding Strap · looseBONDING WIRE BROKE LOOSE ON T/E FLAP. REMOVED DAMAGED SEAL FROM LT INBD CANOE. REPLACED SEAL.SDR IPXA10559587Wire Harness · burnedFOUND (2) WIRES BURNED IN RT WING L/E JUST INBD OF RT ENGINE PYLON. REPLACED SHIELDED WIRE HARNESS IN RT WING INBD L/E FROM CONNECTOR D42340 TO D40148.SDR CA091221006Wire · burned(CAN) ENROUTE FLIGHT 7729, BOTH AC GENERATOR KICKED OFF LINE. AT THE SAME TIME, LT AND RT TRUS, LT AND RT ELEVATOR HORN HEAT, AND STALL WARNING CAUTION LIGHTS ILLUMINATED. FLIGHT CREW PERFORMED AN AC GEN RESET AND EVERYTHING CAME BACK ON LINE. FOLLOWING AN SDR SWIA200921353Wire · corrodedDURING C-CHECK, RIGHT INBOARD FLAP WELL WIRE SPLICE CORRODED. REPLACED WIRE SPLICE.SDR DXTA200803053Connector · contaminatedNO TAKEOFF WARNING AND HORN , CAME ON AFTER JUST PASSING 70 KNTS. C/W FUNCTIONAL CHECK OF THE NO TAKEOFF SYSTEM. NO FAULTS FOUND. INSPECTED SPEEDBRAKE STOW SWITCHES & CONNCETORS. FOUND LT STOW SWITCH CONNECTOR IN SPEEDBRAKE COVE FULL OF WATER. CLEANED COSDR 08FDEA01466Wire Harness · chafedRIGHT WING ABOVE THE NR 2 ENGINE PYLON INSIDE THE WING FIXED L/E; A WIRE BUNDLE HAS SEVERAL WIRES WITH THE INSULATION CHAFED THROUGH EXPOSING INDIVIDUAL WIRES. PREVIOUS REPAIR IS CHAFED THROUGH & TORN. INSTALLED A PROTECTIVE SLEEVE ON THE WIRES REF ESPM 20-5SDR CA070822005Wire Harness · chafed(CAN) WHILE DOING SKIN REPAIRS ON RT WING WE FOUND WIRES CHAFED IN THE FLAP BAY AREA WHERE THE BUNDLE WAS TY WRAPPED TO A NYLON ANCHOR. THE TY WRAP WAS ONLY PUT THROUGH ON LEG OF THE ANCHOR NOT BOTH. THE CONDITION WAS FOUND AT 4 ANCHORS. THE LT WING WAS INSPECSDR PRI2007F00000Wire Harness · damagedDURING A ROUTINE BLOCK INSPECTION, A VISUAL INSPECTION OF THE WINGS REVEALED MULTIPLE WIRES SHOWING DAMAGE IN THE FLAP WELL AREA, FWD OF THE IB FLAPS. THE CAUSE DAMAGE TO THE WIRE BUNDLES F50B602101A1 AND F50B602102A1 COULD NOT BE DETERMINED. SOME SHOWED SIGSDR 2007UALA00211Wire · chafedLEFT WING AFT SPAR BAY, WS 300, WIRING BUNDLE CHAFING HARD AGAINST HYD B-NUT, OUTER SHIELD ON BUNDLE IS TORN. REROUTED WIRE BUNDLE TO ENSURE ADEQUATE SEPARATION AND REPLACED OUTER SHIELD FOR BETTER PROTECTION.SDR 2005FA0000811Wire · shortedRT WING EXPLODED ON TAKEOFF ROLL DUE TO IGNITED FUEL VAPORS TRAPPED IN EMPTY WING CAVITY OR OF FUEL CELLS. INSP REVEALED; RT MAIN FUEL CELL VENT NIPPLE WAS BROKEN OFF, VERY BRITTLE AND DETERIORATED, ALLOWING FUEL VAPORS TO ACCUMULATE IN THIS CAVITY. PREVIOUSSDR 04FDEA01892Wire Harness · arcedRT WING INSIDE NR 3 FUEL TANK THRU ACCESS PANEL NR 634 AT FUEL PROBE WIRE HARNESS HAS CUT WIRE WITH EVIDENCE OF ARCING, LOCATED JUST BELOW ACCESS PANEL. REMOVED AND REPLACED WIRE BUNDLE IAW DC10 MM 20-30-01-2.SDR 2003FA0000882Wire · wornNAV LIGHT CIRCUIT BREAKER POPPED. TROUBLESHOT, FOUND WIRES IN RIGHT FLAP AREA HAD WORN THROUGH PROTECTIVE SLEEVE AND WIRE INSULATION. FOUND BARE SPOTS ON OTHER WIRES IN SAME AREA. RECOMMEND THAT THESE AREA BE INSPECTED CLOSELY FOR INSULATION SLEEVE BEING WOSDR 97ZZZX4504Wire · looseSEVERAL LOOSE WING DRAG AND ANTI-DRAG WIRES DISCOVERED DURING ANNUAL INSPECTION OF A HOMEBUILT PITTS S1C. IN ORDER TO CHECK ALL WIRES, ADDITIONAL INSPECTION HOLES HAD TO BE MADE IN THE WINGS. WITH ALL WIRES ACCESSIBLE FURTHER INSP REVEALED ALL 8 DRAG WIRES A
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