N463AP, cancelled Sep 2, 2004
Service difficulty reports · 84
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N463AP' AND deregistration_id = 'N463AP-2004-09-02' 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 n_number = 'N463AP' AND deregistration_id = 'N463AP-2004-09-02' 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 A6WA200100059Fcu · malfunctionedUNABLE TO CONTROL POWER ON NR 2 ENGINE. POWER INCREASED REGARDLESS OF THRUST LEVER POSITION SHUTDOWN ENGINE WITH T-HANDLE. MAINTENANCE REMOVED AND REPLACED FUEL CONTROL UNIT.SDR A6WA200100037Screw · missingUPPER HINGE COVER PANEL ON LEFT HAND ELEVATOR HELD ON BY ONLY ONE SCREW; FOUR SCREWS MISSING. MAINTENANCE REMOVED AND REPLACED MISSING SCREWS.SDR A6WA9900049Angle · crackedFORWARD PASSENGER DOOR, INTERNAL ANGLE CRACKED. REPLACED ANGLE. (X)SDR A6WA9900048Skin · damagedREPAIR TO RIGHT SIDE OF FUSELAGE AT FRAMES 11-13 AT LAP 'E' AREA. C/W REPAIR IAW BAE 146 SRM AND FAX CW/RJ/0754-99, CW/RJ/0761-99 AND DRAWING HC537H9411. (X)SDR A6WA9900054Stiffener · crackedLEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER NR 176 BEWEEN RIBS 7 AND 8 CRACKED, FORWARD END. REPLACED LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER BETWEEN RIBS 7 AND 8. (X)SDR A6WA9900053Stiffener · crackedRIGHT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER, NR 176 BETWEEN RIBS 7 AND 8, CRACKED FORWARD END. REPAIRED RT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER BETWEEN RIBS 7 AND 8 IAW BAE FAX DJR/RJ0630-98. (X)SDR A6WA9900052Stiffener · crackedRIGHT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER, NR 172 BETWEEN RIBS 3 AND 4, CRACKED FORWARD END. REPLACED RT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER BETWEEN RIBS 3 AND 4. (X)SDR A6WA9900051Stiffener · crackedLEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER, NR 178 BETWEN RIBS 8 AND 9, CRACKED FORWARD END. REPLACED LT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER BETWEEN RIBS 8 AND 9. (X)SDR 17WA9900050Stiffener · crackedLEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER NR 177 BETWEEN RIBS 8 AND 9 CRACKED FORWARD END. REPAIRED LEFT WING SKIN TRAILING EDGE, UPPER WING SKIN TRAILING EDGE STIFFENER BETWEEN RIBS 8 AND 9 IAW BAE FAX DJR/RJ0630-98. (X)SDR A6WA9900055Stiffener · crackedUPPER WING SKIN TRAILING EDGE STIFFENER IS CRACKED AT FORWARD END LOCATED BETWEEN RIBS 9 AND 10, LEFT WING. REPAIRED LT WING SKIN TRAILING EDGE UPPER WING SKIN STIFFENER BETWEEN RIBS 9 AND 10 IAW BAE FAX DJR/RJ0630-98. (X)SDR 99ZZZX2700Slide · deployedORD - FLT 545 - WHILE INSPECTING GIVE BAR MECHANISM ON FORWARD PASSENGER DOOR, SLIDE PARTIALLY DEPLOYED. REMOVED AND REPLACED FORWARD PASSENGER DOOR SLIDE IAW MM.SDR 99ZZZM548Slide · out of positionWHILE INSPECTIONG GIVE BAR MECHANISM ON FORWARD PASSENGER DOOR SLIDE PARTIALLY DEPLOYED. REMOVED AND REPLACED FORWARD PASSENGER DOOR SLIDE IAW MM. (M)SDR 99ZZZM471Handle · out of adjustFORWARD PAX DOOR, SLIDE ARMING HANDLE HITS THE HANDLE RECESS NOT ALLOWING THE GIRT BAR TO FULLY ENGAGE INTO LUGS. REMOVED UPPER DOOR COVER AND ARMING HANDLE RECESS RECONTURED RECESS PAINTED AND REINSTALLED RECESS AND UPPER DOOR COVER, OPS CHECKED GOOD. (M)SDR 99ZZZM461Bracket · crackedLEFT WING, FORWARD HYD LINE CLAMP BRACKET, RIB 5, CRACKED. REPLACED BRACKET. (M)SDR 99ZZZM457Stiffener · crackedRIGHT WING TE LOWER SHROUD SKIN STIFFENER CRACKED BETWEEN RIB 7/8. REPLACED STIFFENER IN RIGHT WING TE LOWER SHROUD SKIN BETWEEN RIBS 7/8. (M)SDR 99ZZZM449Door · damagedNR 3 ENGINE AFT INBOARD FAN DOOR LOWER DOOR SPLITTER AREA HAS CHAFED STIFFENER, 2ND FROM FORWARD. REPLACED ABOVE STIFFENER PER SRM. (M)SDR 99ZZZM448Skin · chafedNR 3 ENGINE AFT INBOARD FAN DOOR INNER TITANIUM SKIN CHAFED THROUGH. REPLACED PAN AND PATCHED SMALL AREA 2.25 BY 3.5 USING TAZ PER PSI. (M)SDR 99ZZZM446Door · crackedNR 1 ENGINE AFT LEFT COWL DOOR SECOND STIFFENER ON LOWER SPLITTER ASSY CRACKED. REPLACED SECOND STIFFENER ON NR 1 ENGINE LEFT COWL DOOR. (M)SDR 99ZZZM445Bulkhead · crackedNR 1 ENGINE LEFT AFT COWL DOOR BULKHEAD AT VENT TUBE AREA CRACKED. REPAIRED CRACK IN FLANGE OF BULKHEAD BY PATCHING IAW BAE/AIR WISC SRM STANDARD PRACTICES. (M)SDR 99ZZZM472Bulkhd Longeron · crackedFRAME 29 MAIN LANDING GEAR BAY ROOF PRESSURE BULKHEAD, LONGERONS NR 3, NR 9, NR 15 CRACKED. REPAIRED PRESS BULKHEAD LONGERONS NR 3, NR 9, AND NR 15 PER REPAIR DRAWING HC536H9211 AND SRM, AND FAX'S NUMBERED D-JH/R-JO419-98, D-JH/R-J0421-98, AND D-JH/R-J0422-98SDR 99ZZZM470Mask · tornCAIN OXYGEN MASKS FOR PASSENGERS FILTERS TORN SEAT 3A, 10B, 12A, 12B, 14C, 15C, 13E, 10F. REMOVED AND REPLACED FILTER TO PER COMPONENT MM TO 3A, 10B, 12A, 12B, 14C, 15C, 13E, 10F. (M)SDR 99ZZZM464Stiffener · crackedRIGHT WING TE SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 7/8. REPAIRED RIGHT WING TE TOP SHROUD SKIN STIFFENER BETWEEN RIBS 7/8. (M)SDR 99ZZZM459Stiffener · crackedLEFT WING TE SHROUD TO PSKIN STIFFENERS ARE CRACKED AT FORWARD END IN AREA BETWEEN RIBS 8/9. REPAIRED LEFT WING TE SHROUD TO SKIN STIFFENER BETWEEN RIBS 8/9. (M)SDR 99ZZZM458Stiffener · crackedLEFT WING TE TOP SKIN STIFFENER IS CRACKED AT FORWARD END IN AREA BETWEEN RIBS 7/8. REPAIRED LEFT WING TE TOP SKIN STIFFENER BETWEEN RIBS 7/8 IAW BAE FAX NR JM/RJO417-98. REF W/C 5022 FOR REINSPECTION. (M)SDR 99ZZZM455Bracket · crackedANGLE BRACKET, P/N HC361JO137-006 CRACKED. LOCATED AT RIGHT ECS DUCT FRAME 45 SUPPORT OVERTEMP SWITCH BRACKET. MANUFACTURED BRACKET IAW AIR WISC/BAE SRM STANDARD PRACTICES. DRILLED TO FIT IAW BAE FAX JM/RJ 0418-98. ALODINED AND PRIMED. SEE ADDITIONAL W/C SDR 99ZZZM454Stiffener · crackedLEFT WING TRAILING EDGE SHROUD TOP SKIN STIFFENER IN AREA BETWEEN RIBS 9/10 IS CRACKED AT FORWARD END. REPAIRED LEFT WITH TE SHROUD TOP SKIN STIFFENER BETWEEN RIBS 9/10 IAW BAE FAX NR JM/RJO417-98, REF REINSPECTION W/C 5020. (M)SDR 99ZZZM451Door · damagedNR 4 ENGINE AFT OUTBOARD FAN DOOR LOWER DOOR SPLITTER AREA 2ND STIFFENER FROM FORWARD CHAFED. REPLACED NR 4 ENGINE AFT OUTBOARD FAN DOOR LOWER DOOR SPLITTER AREA, 2ND STIFFENER FROM FORWARD. (M)SDR 99ZZZM450Door · damagedNR 4 ENGINE AFT OUTBOARD FAN DOOR LOWER DOOR SPLITTER AREA, STIFFENER AT FORWARD CORNER CHAFED BADLY. REPLACED NR 4 ENGINE AFT OUTBOARD FAN DOOR LOWER DOOR SPLITTER AREA, STIFFENER AT FORWARD CORNER. (M)SDR 99ZZZM436Stiffener · crackedRIGHT WING TE TOP SHROUD SKIN STIFFENER CRACKED AT FORWARD END INBOARD OF RIB 9. REPAIRED RIGHT WING TE TOP SHROUD SKIN STIFFENER BETWEEN RIBS 8/9 IAW BAE FAX NR JM/RJ0417-98. (M)SDR 99ZZZM463False Spar · crackedRIGHT WING TE HAS TEMP REPAIR (STOP DRILL) TO CRACK IN FALSE SPAR CAP BETWEEN RIBS 7/8, NEEDS PERM REPAIR. REPAIRED RIGHT WING TE BETWEEN RIBS 7/8. (M)SDR 99ZZZM462Stiffener · crackedTOP RIGHT WING T/E SKIN STIFFENER TWIX WING RIBS 3/4 CRACKED AT AFT END. REPAIRED RIGHT WING TE TOP SHROUD SKIN STIFFENER BETWEEN RIBS 3/4. (M)SDR 99ZZZM460Stiffener · crackedLEFT WING TE SHROUD BOTTOM SKIN STIFFENER CLEATS ARE CRACKED IN AREA BETWEEN RIBS 8/9. REPLACED BOTH CLEATS AS PER POSITIONS ABOVE USING BAE STANDARD PRACTICES AND PROCEDURES. (M)SDR 99ZZZM440Gusset · corrodedNR 2 GUSSET PLATES CORRODED LEFT SIDE FRAME 15 FLOORBEAM. REPLACED TWO GUSSET PLATES LEFT SIDE FRAME 15 FLOORBEAM. (M)SDR 99ZZZM469Floorbeam · corrodedFORWARD VESTIBULE FLOORBEAM AT FRAME 15 HAS A SMALL SPOT OF CORROSION APPROX 5 INCHES OUTBOARD OF 3RD INTERCOSTAL FROM LEFT SIDE, INLINE WITH CLOSET WALL AT C/PIT ENTRANCE AND IS MARKED WITH BLACK PEN. BLENDED AREA TO LIMITS AND SURFACE TREATMENT AS PER BAE SSDR 99ZZZM468Gussett · corrodedFORWARD VESTIBULE, CENTER GUSSET PLATE ON THE 2ND INTERCOSTAL FROM RIGHT SIDE IS CORRODED. REPLACED FORWARD VESTIBULE GUSSET PLATE CENTER ON NR 2 INTERCOSTAL FROM RIGHT. (M)SDR 99ZZZM467Gusset · corrodedFORWARD VESTIBULE, GUSSET PLATE ON FLOORBEAM AT FRAME 15 AND 2ND INTERCOSTAL FROM RIGHT SIDE HAS SOME SURFACE CORROSION AND APPEARS TO BE MADE OF TOO THIN OF MATERIAL AREA IS MARKED WITH BLACK PEN. REPLACED GUSSET PLATE FORWARD VESTIBULE FRAME 15 2ND INTERCOSSDR 99ZZZM466Frame · corrodedFORWARD VESTIBULE, FLOOR PANEL (UNDER GALLEY UNIT) HAS SOME SURFACE CORROSION IN A COUPLE SPOTS ALONG AFT EDGE. REMOVED SURFACE CORROSION FORWARD VESTIBULE AT AFT EDGE OF GALLEY ASSY FRAME 15 TREATED AND PAINTED. (M)SDR 99ZZZM456Stiffener · crackedRIGHT WING TE SHROUD LOWER SKIN STIFFENER CLEATS CRACKED BETWEEN RIBS 8/9, AFT END OF STIFFENER. REPLACED BOTH CLEATS OF RT WING TE SHROUD LOWER SKIN STIFFENER, CLEATS CRACKED BETWEEN RIBS 8/9, AFT END. (M)SDR 99ZZZM442Sill · corrodedFORWARD VESTIBULE, SERVICE DOOR SILL PLATE HAS SEVERAL SMALL SPOTS OF SURFACE CORROSION. REMOVED AND REPLACED SILL PLATE WITH NEW. (M)SDR 99ZZZM439Floor Strip · corrodedFLOOR STRIPS FOR FORWARD CABIN BULKHEADS NEED CLEANED, CORROSION REMOVED, PAINTED, ETC. CLEANED, REMOVED CORROSION ALODINED, PRIMED, PAINTED, AND REATTACHED PHONELLIC STRIPS. (M)SDR 99ZZZM465Frame · corrodedFORWARD VESTIBULE, FORWARD END OF SEAT RAIL, INBOARD RIGHT FLOORBEAM AT FRAME 18 IS CORRODED. REMOVED SURFACE CORROSION FORWARD VESTIBULE FRAME 18 INBOARD SEAT RAIL RIGHT SIDE TREATED, PRIMED AND PAINTED. (M)SDR 99ZZZM452Plate · wornWHILE CMP/WITH SSI 52-82-101-WEAR WAS DICV'D ON BOTTOM AFT CORNERS OF NOSE GEAR DOORS WHERE THEY ABUT TAB ON SPADE DOOR. TAB IS ALSO WORN. MANUFACTURED 2 BUTMENT PLATES FOR LT/RT NOSEGEAR DOORS IAW BAE DRAWING HC528H0161. INSTALLED LT/RT NOSEGEAR DOOR ABUTMSDR 99ZZZM443Bracket · corrodedFORWARD VESTIBULE, STEW SEAT MOUNT BRACKETS ON 2ND AND 3RD INTERCOSTALS FROM LEFT SIDE ARE LIGHTLY CORRODED. REMOVED CORROSION TREATED PRIMED AND PAINTED FORWARD F/A SEAT MOUNT BRACKETS. (M)SDR 99ZZZM453Bracket · crackedMLG DOOR UPLOCK COVER BRACKET ON THE RIGHT SIDE OF WEB AT FRAME 32 IN MLG BAY IS CRACKED. REPLACED SAID BRACKET P/N HC536H0826-000U. (M)SDR 99ZZZM438Intercostal · crackedAFT VEST, UNDER FLOOR INTERCOSTAL BETWEEN FRAMES 41 AND 42 IS CRACKED, CENTER INTERCOSTAL, CRACK IS APPROX 2.5 TO 3 INCHES LONG. COMPLIED WITH PATCH REPAIR IAW AIR WISC/BAE SRM STANDARD PRACTICES REF CHAPTER 51. COMPLIED WITH ALODINE, PRIMER AND PAINTING. (SDR 99ZZZM473Spring · failedFORWARD VESTIBULE TRASH BIN DOOR ASSY, NEEDS CLEANED. ANGLE REPAIR, DOOR SPRINGS, ETC. REMOVED AND REPLACED SPRINGS. REPAIRED ANGLE AND CLEANED AND INSPECTED. (M)SDR 99ZZZM447Bracket · crackedNR 3 ENGINE NOSE COWL INBOARD FIREBOTTLE HAS ONE ATTACH BRACKET MOUNTED TO FIREWALL THAT IS CRACKED BADLY. REMOVED NR 3 NOSE AND TRANSFERRED DISCREPANCY TO W/C. (M)SDR 99ZZZM444Rib · crackedNR 2 PYLON BOX STRUCTURE HAS A CRACK IN THE LOWER OUTBOARD FLANGE OF RIB NR 5 THAT IS APPROX .5 INCH LONG. NR 2 PYLON CRACK OF APPROX .5 INCH LONG IS ACCEPTABLE AND HAS BEEN REPORTED TO BAE RDO PER P/C HC646H9018. GENERATED W/C FOR REINSPECTION. (M)SDR 99ZZZM441Sill · corrodedPASSENGER DOOR SILL PLATE CORRODED FRAME 15. REMOVED AND REPLACED FORWARD PAX DOOR SILL PLATE. (M)SDR 99ZZZM437Bracket · crackedSTRUCTURAL INSPECTION MLG BAY, POS N/A WEB AT FRAME 32, DETAILED VISUAL INSPECTION. PERFORMED DV ON WEB AT FRAME 32 IN LEFT AND RIGHT MLG BAY. FOUND CRACKED BRACKET RT MLG DOOR UPLOCK CVR, FOUND MINOR NICKS SURFACE WEB.
Back to N463AP, cancelled Sep 2, 2004