N808AX, cancelled Mar 12, 2004

Service difficulty reports · 74

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 = 'N808AX' AND deregistration_id = 'N808AX-2004-03-12'
  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 ABXA000493Valve · leakingFLIGHT CREW REPORTED A LOSS OF HYDRAULIC PRESSURE WITH AN ASSOCIATED HYDRAULIC QUANTITY LOSS INDICATION. THE FLIGHT CREW PERFORMED EMERGENCY PROCEDURES. MAINTENANCE INSPECTED AND REPLACED THE SLOT CONTROL VALVE IAW DC-8 MM 27-80-00. OPS CHECKED GOOD.Nov 13, 2000 · N808AX · Doug DC862 · Hydraulic System, MainSDR ABXA9900754Generator · defectiveFAULT ON NR 4 GENERATOR. UNABLE TO RESET IAW ABNORMAL CHECKLIST. SECURED ENGINE, MAINTAINED POSITIVE ENGINE OIL PRESSURE. INSPECTED MAIN OIL FILTER, FOUND NO CONTAMINATION. CHECKED OIL QUANTITY, RAN ALL ENGINES, ENGINE RUN WAS NORMAL. CHECKED AIRCRAFT WIRIOct 28, 1999 · N808AX · Doug DC862 · AC Generator-AlternatorSDR ABXA9900691Skin · corrodedSKIN CORRODED AT STATION 240, BELOW LONGERON 3 LEFT. REPAIRED IAW ABX REA D853-32664MR.Sep 2, 1999 · N808AX · Doug DC862 · Fuselage Main, Plate/SkinSDR ABXA9900690Fitting · crackedLONGERON SPLICE FITTING CRACKED AT STATION 390 AND LONGERON 33 -35 RIGHT. REPAIRED IAW ABX REA D853-32693MR.Sep 2, 1999 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9900368Duct · rupturedON LEVEL OFF AT 37,000 FEET, CABIN STARTED TO CLIMB AT 3,000 FEET PER MINUTE. COULD NOT CONTROL CABIN RATE. DESCENDED TO 24,000 FEET AND REGAINED CONTROL OF CABIN. MAINTAINED CABIN AT 9,000 FEET. HEARD LOUD NOISE BY THE RIGHT HAND CTC'S AT 37,000. OXYGEN May 14, 1999 · N808AX · Doug DC862 · Cabin Pressure Control SystemSDR ABXA9900280Pump · leakingDURING CRUISE, ONE HOUR AND TWENTY MINUTES INTO FLIGHT EXPERIENCED LOSS OF HYDRAULIC QUANTITY DOWN TO STANDPIPE. PERFORMED LOSS OF HYDRAULICS PROCEDURES. REPLACED STANDBY RUDDER PUMP IAW DC8 MM 29-27-00, OPS CHECKED GOOD.Apr 7, 1999 · N808AX · Doug DC862 · Rudder Control SystemSDR ABXA9900038Latch · out of adjustDURING POSTFLIGHT CHECK, CABIN DOOR LOCK WAS STUCK IN LOCKED POSITION. FOUND OUTER LATCH ASSEMBLY MISADJUSTED 180 DEGREES. READJUSTED LATCH TO PROPER POSITION, OPS CHECKED GOOD.Jan 26, 1999 · N808AX · Doug DC862 · Fixed Inner DoorsSDR ABXA9900039Latch · out of adjustDURING POSTFLIGHT, FOUND COCKPIT DOOR KNOB STUCK. ADJUSTED AND LUBRICATED INTERNAL MECHANISM IAW DC8 SRM.Jan 21, 1999 · N808AX · Doug DC862 · Fixed Inner DoorsSDR ABXA9701937Frame · corrosionFRAME 1020, UPPER FLANGE AT LONGERON 34R IS CORRODED BEYOND LIMITS. REPAIRED IAW DC8 SRM 53-2-0 AND 51-1-21.Nov 22, 1997 · N808AX · Doug DC862 · Fuselage Main, FrameSDR ABXA9701936Fitting · crackedSTA 860 FWD SIDE AT STRINGER 18R TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Nov 22, 1997 · N808AX · Doug DC862 · Fuselage Main, StructureSDR ABXA9701935Fitting · crackedSTA 900 AFT SIDE STRINGER 18R INTERCOSTAL TIE FITTING IS CRACKED. INSTALLED INTERCOSTAL TIE FITTING IAW DWG 4750428 AND SRM 51-1-20D.Nov 22, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9701934Fitting · crackedLEFT STA 410 FLAP CANOE FITTING INBOARD SIDE SUPPORT FITTING IS CRACKED. REPAIRED IAW SRM 51-2-0.Nov 22, 1997 · N808AX · Doug DC862 · Trailing Edge FlapsSDR ABXA9701879Fitting · crackedSTA 900 INTERCOSTAL TIE FITTING IS CRACKED AT AFT SIDE AT STR 18R. REPAIRED IAW SWG 4750428 AND SRM 51-1-20D.Nov 22, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9701878Fitting · crackedSTA 860 FWD SIDE AT STRINGER 18R TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Nov 22, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9701877Frame · corrodedFRAME 1020 UPPER FLANGE AT LONGERON 34R HAS CORROSION BEYOND LIMITS. REPAIRED IAW SRM 53-2-0 AND 51-1-21.Nov 22, 1997 · N808AX · Doug DC862 · Fuselage Main, FrameSDR ABXA9701889Cap · crackedNR 2 PYLON CAP IS CRACKED AT SCREW HOLE, OUTBOARD UPPER SIDE, JUST FWD OF TOMBSTONE FITTING. REPAIRED IAW SRM 54-2-2.Nov 14, 1997 · N808AX · Doug DC862 · Nacelle/Pylon StructureSDR ABXA9701927Channel · crackedCANTED WEB CHANNEL HAS CRACK IN NR 4 ALT TANK, AT RT WING STA 508.977. REPAIRED IAW DWG 56 1326 AND DC8 SRM 51-1-21.Nov 13, 1997 · N808AX · Doug DC862 · Wing Miscellaneous StructureSDR ABXA9701885Channel · crackedCANTED WEB CHANNEL HAS CRACK AT NR 4 ALT TANK, AT RT WING STA 508.977. REPAIRED IAW SRM 51-1-21 AND DWG 56-1326.Nov 13, 1997 · N808AX · Doug DC862 · Wing Miscellaneous StructureSDR ABXA9701919Skin · crackedTHE RT ELEVATOR LWR SKIN AT STA XE 55.012 AND JUST FWD OF THE TRAILING EDGE IS CRACKED. THE CRACK IS APPROX 1.8 LONG. REPAIRED IAW DC8 SRM 53-2-1.Nov 12, 1997 · N808AX · Doug DC862 · Elevator, Plate/SkinSDR ABXA9701917Angle · corrodedUPPER ANGLE OF INTERCOSTAL AT FS 980 TO 1000 LONGERON 35L CORRODED BEYOND LIMITS. INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-0, 51-1-20D.Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9701916Angle · corrodedLOWER L-ANGLE IN KEEL BEAM AREA BETWEEN WHEEL WELL DOORS, 2ND FROM FRONT (APPROX FS 890) CORRODED BEYOND ALLOWABLE LIMITS. FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-0, 51-1-20D AND 51-1-21.Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9701915Longeron · crackedLONGERON 35R CRACKED AT FS 1195 AT INBOARD FLANGE. REPLACED DAMAGED SECTION OF LONGERON IAW ABX REA D853-21175.Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Main, Longeron/StringerSDR ABXA9701914Longeron · corrodedLONGERON 22R CORRODED BEYOND LIMITS FROM STA 270 TO 280. REPLACED SECTION OF LONGERON IAW SRM 53-2-2 AND SRM 53-4-1.Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Main, Longeron/StringerSDR ABXA9701913Fitting · crackedSTA 860 AFT SIDE AT STR 18R TIE FITTING IS CRACKED. INSTALLED NEW FITTING IAW SRM 51-1-20D AND DWG 4750422.Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9701912Fitting · crackedSTA 440 TO 460 STR 31L SPLICE FITTING IS CRACKED. REPLACED SPLICE FITTING PER SRM 53-1-0 AND 51-1-20.Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9701911Fitting · crackedACCESSORY COMP STA 680 BL 0, THE SEAT TRACK SUPPORT FITTING IS CRACKED. REPAIRED IAW SRM 51-1-20D, DWG 4645517 AND SRM 51-1-8.Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9701898Longeron · crackedLONGERON 35R CRACKED AT FS 1195, INBOARD FLANGE. REPLACED DAMAGED SECTION OF LONGERON 35R IAW REA D853-21175.Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Main, Longeron/StringerSDR ABXA9701897Angle · corrodedLOWER L-ANGLE IN KEEL BEAM AREA, BETWEEN WHEEL WELL DOORS, 2ND FROM FRONT (APPROX FS 890) CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-0, 51-1-20D AND 51-1-21.Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9701896Angle · corrodedUPPER ANGLE OF INTERCOSTAL AT FS 980 TO 1000 LONGERON 35L CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-0, 51-1-20D.Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9701875Longeron · corrosionLONGERON 22R CORRODED BEYOND LIMITS AT STA 270-280. REPAIRED IAW SRM 53-2-2, AND SRM 53-4-1.Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Main, Longeron/StringerSDR ABXA9701858Fitting · crackedSEAT TRACK SUPPORT FITTING IS CRACKED, IN ASSY COMPARTMENT, STA 680 AT BL O. REPAIRED IAW SRM 51-1-20D, DWG 4645517 AND SRM 51-1-8.Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9701857Fitting · crackedSTA 440-460, STR 31L, SPLICE FITTING IS CRACKED. REPAIRED IAW SRM 53-1-0 AND 51-1-20.Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9701856Fitting · crackedSTA 860, AFT SIDE AT STR 18R, TIE FITTING IS CRACKED. REPAIRED IAW SRM 51-1-20D AND DWG 4750422.Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9701923Skin · crackedLEFT WING FLAP TRAILING EDGE CRACKED AT STA XW 191. REPAIRED IAW DC8 SRM 57-7-0 AND 51-1-21.Nov 4, 1997 · N808AX · Doug DC862 · Trailing Edge FlapsSDR ABXA9701920Rib · crackedLEFT WING LEADING EDGE UPPER RIB CRACKED AT FS XFS 303. REPAIRED IAW DC8 SRM 57-2-0 AND DWG KO 5606.Nov 4, 1997 · N808AX · Doug DC862 · Wing, Rib/BulkheadSDR ABXA9701909Angle · corrodedFRAME SUPPORT ANGLE ON FWD SIDE OF FRAME 1280 HAS HEAVY CORROSION ABOVE LONGERON 36. REPLACED ANGLE IAW SRM 53-4-1.Nov 4, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9701894Rib · crackedLEFT WING, LEADING EDGE UPPER RIB CRACKED AT FS XFS 303. REPAIRED IAW SRM 57-2-0, 51-1-20D, AND DWG K O 5056.Nov 4, 1997 · N808AX · Doug DC862 · Wing, Rib/BulkheadSDR ABXA9701891Flap · crackedLEFT WING FLAP, TRAILING EDGE CRACKED AT STA XW 191. REPAIRED IAW SRM 57-7-0 AND 51-1-21.Nov 4, 1997 · N808AX · Doug DC862 · Trailing Edge FlapsSDR ABXA9701860Angle · corrodedFRAME SUPPORT ANGLE ON FWD SIDE OF FRAME 1280 HAS HEAVY CORROSION ABOVE LONGERON 36. REPLACED ANGLE IAW SRM 53-4-1.Nov 4, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9701932Rib · crackedLEFT WING LEADING EDGE UPPER RIB CRACKED AT XFS 331. REPAIRED IAW DC8 SRM 57-2-0 AND 51-1-20D.Nov 3, 1997 · N808AX · Doug DC862 · Wing, Rib/BulkheadSDR ABXA9701929Rib · crackedLEFT WING LEADING EDGE UPPER RIB CRACKED AT XFS 432. REPAIRED IAW DC8 SRM 57-2-0 AND 51-1-20D.Nov 3, 1997 · N808AX · Doug DC862 · Wing, Rib/BulkheadSDR ABXA9701928Rib · crackedLEFT WING LEADING EDGE UPPER RIB CRACKED AT XFS 341. REPAIRED IAW DC8 SRM 57-2-0 AND 51-1-20D.Nov 3, 1997 · N808AX · Doug DC862 · Wing, Rib/BulkheadSDR ABXA9701924Rib · crackedUPPER RIB CRACKED AT STA XFS 415 LEFT WING LEADING EDGE. REPAIRED IAW DC8 SRM 57-2-0 AND DWG KO5056.Nov 3, 1997 · N808AX · Doug DC862 · Wing, Rib/BulkheadSDR ABXA9701921Rib · crackedLEFT WING UPPER RIB CRACKED AT STA XFS 360. REPAIRED IAW DC8 SRM 57-2-0 AND DWG KO 5056.Nov 3, 1997 · N808AX · Doug DC862 · Wing, Rib/BulkheadSDR ABXA9701893Rib · crackedLEFT WING, LEADING EDGE HAS CRACKED UPPER RIB AT STA XFS 360. REPAIRED IAW SRM 57-2-0, 51-1-20, AND DWG K O 5056.Nov 3, 1997 · N808AX · Doug DC862 · Wing, Rib/BulkheadSDR ABXA9701890Rib · crackedLEFT WING LEADING EDGE, UPPER RIB CRACKED XFS 415. REPAIRED IAW SRM 57-2-0, 51-1-8 AND DWG K O 5056.Nov 3, 1997 · N808AX · Doug DC862 · Wing, Rib/BulkheadSDR ABXA9701884Rib · crackedLEFT WING, LEADING EDGE UPPER RIB CRACKED AT XFS 341. REPAIRED IAW SRM 57-2-0 AND 51-1-20D.Nov 3, 1997 · N808AX · Doug DC862 · Wing StructureSDR ABXA9701883Rib · crackedLEFT WING LEADING EDGE RIB CRACKED AT XFS 432. REPAIRED IAW SRM 51-1-120D AND 51-1-8.Nov 3, 1997 · N808AX · Doug DC862 · Wing, Rib/BulkheadSDR ABXA9701881Rib · crackedLEFT WING, LEADING EDGE RIB CRACKED AT XFS 331. REPAIRED IAW SRM 51-1-20D AND 51-1-8.Nov 3, 1997 · N808AX · Doug DC862 · Wing, Rib/BulkheadSDR ABXA9701888Skin · corrodedRIGHT HORIZONTAL STABILIZER LEADING EDGE SKIN IS CORRODED AT STA XFS 178. REPAIRED IAW SRM 51-1-21 AND 51-1-26.Oct 31, 1997 · N808AX · Doug DC862 · Horizontal Stabilizer, Plate/Skin
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