Douglas DC-8-62

Service difficulty reports · 2,778

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = 'DC862'
  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 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 IXXA9700163Control Cable · out of adjAFTER TAKEOFF WHEN THE GEAR WAS RETRACTED, THE LANDING GEAR AND DOOR UNSAFE LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO KWI, MAKING AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE MAIN GEAR DOOR FOLLOW-UP CONTROL MECHANISM ONov 11, 1997 · N61CX · Doug DC862 · Landing Gear Door Retract SectionSDR IXXA9700162Control Box · defectiveDURING LANDING ROLL AT WRI, ALL HYDRAULIC BRAKING ACTION WAS LOST. THE CREW INITIATED THE EMERGENCY AIR BRAKE SYSTEM TO DECELERATE THE AIRCRAFT. NORMAL BRAKING WAS RESTORED AFTER THE CREW DISARMED THE ANTI-SKID SYSTEM. MAINTENANCE INSPECTED THE AIRCRAFT ANDNov 9, 1997 · N21CX · Doug DC862 · Brake Anti-Skid SectionSDR IXXA9700161Control Cable · misriggedAFTER TAKEOFF WHEN THE LANDING GEAR WAS RETRACTED, THE DOOR UNSAFE LIGHT REMAINED ILLUMINATED. THE CREW RECYCLED THE LANDING GEAR AND THE INDICATION REMAINED THE SAME. THE AIRCRAFT RETURNED TO FRA, MAKING AN UNEVENFUL LANDING. MAINTENANCE INSPECTED THE AIRCNov 9, 1997 · N61CX · Doug DC862 · Landing Gear Door Retract SectionSDR IXXA980014Access Panel · corrodedDURING ROUTINE D CHECK INSPECTION, CORROSION WAS FOUND ON THE RIGHT WING LEADING EDGE ACCESS PANEL LAND AT STATION XFS 361. REPAIR ACCOMPLISHED REMOVAL OF DAMAGE AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND TWO REPAIR DOUBLERS AND THIPLERS IN Nov 7, 1997 · N728PL · Doug DC862 · Wing, Plate/SkinSDR IXXA9800013Spar Cap · corrodedDURING ROUTINE D-CHECK INSPECTION, CORROSION WAS FOUND ON THE RIGHT WING LOWER LEADING EDGE SPAR CAP TEE AT STATION XFS 361. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND A REPAIR DOUBLERS, AND TRIPLER INNov 7, 1997 · N728PL · Doug DC862 · Wing SparSDR 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 IXXA980015Skin · crackedDURING ROUTINE D CHECK INSPECTION, A CRACK WAS FOUND ON THE RIGHT WING UPPER LEADING EDGE PLATING TWELVE INCHES OUTBOARD OF NUMBER THREE PYLON. REPAIR ACCOMPLISHED STOP DRILLING CRACK, FABRICATION AND INSTALLATION AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITHNov 3, 1997 · N728PL · Doug DC862 · Wing, Plate/SkinSDR IXXA9800015Plating · crackedDURING ROUTINE D-CHECK, A CRACK WAS FOUND ON THE RIGHT WING UPPER LEADING EDGE EXTERNAL PLATING, TWELVE INCHES OUTBOARD OF THE NUMBER THREE PYLON. REPAIR WAS ACCOMPLISHED BY STOP DRILLING THE CRACK, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER INov 3, 1997 · N728PL · Doug DC862 · Wing, Plate/SkinSDR IXXA9800014Plating · crackedDURING ROUTINE D-CHECK INSPECTION, A CRACK WAS FOUND ON THE RIGHT WING UPPER LEADING EDGE EXTERNAL PLATING TWELVE INCHES OUTBOARD OF NUMBER THREE PYLON. REPAIR ACCOMPLISHED BY STOP DRILLING CRACK, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN Nov 3, 1997 · N728PL · Doug DC862 · Wing, Plate/SkinSDR 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 IXXA9700160Battery Pack · dischargedAFTER ARRIVING AND ENGINE SHUTDOWN WITH NO EXTERNAL ELECTRICAL POWER, THE COCKPIT AND PASSENGER COMPARTMENT DOOR OVERHEAD EMERGENCY LIGHTING FAILED TO ILLUMINATE. MAINTENANCE INSPECTED THE EMERGENCY LIGHTING SYSTEM AND FOUND TWO BATTERY PACKS DEFECTIVE, WHICNov 1, 1997 · N21CX · Doug DC862 · Emergency LightingSDR 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/SkinSDR ARWA971006Filter · defectiveNR 2 ENGINE OIL PRESSURE ILLUMINATED, PERFORMED ABNORMAL CHECKLIST, LIGHT GOES OUT AFTER THROTTLE RETRACTED PARAMETERS MONITORED CONTINUED NORMAL OPERATION. DURING APPROACH LIGHT CAME ON, ENGINE PRECAUTIONARY SHUT DOWN AT 05044 Z. REMOVED AND REPLACED MAIN OOct 29, 1997 · N1804 · Doug DC862 · Turbine Engine Oil SystemSDR ABXA9701895Angle · corrodedINTERCOSTAL AT LONGERON 35L, JUST FWD OF STA 1000 LOWER ANGLE OF LONGERON IS CORRODED BEYOND LIMITS. INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-20 AND DWG 564586.Oct 28, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA701918Angle · corrodedINTERCOSTAL AT LONGERON 35L JUST FWD OF STA 1000 LOWER ANGLE IN LONGERON CORRODED BEYOND LIMITS. REPAIRED IAW SRM 51-1-20 AND DWG 564586.Oct 28, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9701933Longeron · crackedLONGERON 35R CRACKED AT STA 1185 INBOARD FLANGE. REPAIRED IAW DC8 SRM 53-2-2 AND ABX REA D853-21175.Oct 27, 1997 · N808AX · Doug DC862 · Fuselage Main, Longeron/StringerSDR ABXA9701930Clip · crackedINTERCOASTAL TO HORIZONTAL INTERCOASTAL CLIP CRACKED JUST ABOVE LONGERON 35R BTWN STA 1160 TO 180. REPAIRED IAW DC8 SRM 53-1-0 AND 51-1-20.Oct 27, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9701926Clip · corrodedINTERCOSTAL TO FLOOR SUPPORT CLIP HAS HEAVY CORROSION AT STA 983 LONGERON 33R. REPAIRED IAW DC8 SRM 51-1-20D.Oct 27, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9701925Skin · crackedLEFT WING UPPER SKIN AT STA XRS-74 AND STRINGER 9 IS CRACKED. REPAIRED IAW DC8 SRM 57-2-1 AND 51-1-2.Oct 27, 1997 · N808AX · Doug DC862 · Wing, Plate/SkinSDR ABXA9701910Fitting · crackedSTA 900 FRAME, FWD SIDE AT STRINGER 18R TIE FITTING IS CRACKED. REPLACED FITTING IAW SRM 51-1-21.Oct 27, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9701887Skin · crackedLEFT WING UPPER SKIN AT STA XRS-74 AND STRINGER 9 IS CRACKED. REPAIRED IAW SRM 51-1-21 AND 51-1-8.Oct 27, 1997 · N808AX · Doug DC862 · Wing, Plate/SkinSDR ABXA9701886Clip · corrodedINTERCOSTAL TO FLOAT SUPPORT CLIP HAS HEAVY CORROSION AT STA 983 LONGERON 33R. REPAIRED IAW SRM 51-1-20D.Oct 27, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9701880Longeron · crackedLONGERON 35R CRACKED AT STA 1185 INBOARD FLANGE. REPAIRED IAW SRM 53-2-2 AND ABX REA D853-21175.Oct 27, 1997 · N808AX · Doug DC862 · Fuselage Main, Longeron/StringerSDR ABXA9701859Fitting · crackedSTA 900 FRAME, FWD SIDE AT STR 18R, TIE FITTING IS CRACKED. REPAIRED FITTING IAW SRM 51-1-21.Oct 27, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9701922Rib · crackedLEFT WING LEADING EDGE AT STA XFS 354 IS CRACKED AT AFT UPPER END. REPAIRED IAW DC8 SRM 51-1-8 AND DWG KO5056.Oct 26, 1997 · N808AX · Doug DC862 · Wing, Rib/Bulkhead
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