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.
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
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 ZIAA96066Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. MAIN CABIN INTERIOR, FRAMES, LONGERONS, TRACK FROM FS 340 THROUGH FS 1590 BOTH LT AND RT. 54 AREAS NOTED ON TASK H 57300551. REPAIREDSDR ZIAA96065Extrusion · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. RT CUSP EXTRUSION: FS 600 AT FRAME. FS 1240-1260. FS 879.375 FITTING. FS 1400-AT FRAME. FS 1442-1450 WEB. REPAIRED IAW APPLICABLESDR ZIAA96064Extrusion · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. FS 780 AT FRAME. LT CUSP EXTRUSION. FS 520 AT FRAME. FS 1340 AT FRAME. FS 600 AT FRAME. FS 1020 AT FRAME. FS 1040 AT FRAME. REPASDR ZIAA96063Hinge · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. UPPER CARGO DOOR HINGE ABOVE FWD SWIVEL DOOR AFT END. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR ZIAA96062Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. AFT ACCY COMPT-FS 1440-1500. FS 1563 LONG 18-34R. FS 1563. FS 1563 LONG 34R. FS 1564 LONG 24L. FS 1563 LONG 18L. FS 1560 LONG 18LSDR ZIAA96061Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. AFT LOWER CARGO BILGE. FS 1190 LONG 35L. FS 1085-1090 SKIN. FS 1080 LONG 35R-36R. FS 1020-CIRCUM. FS 1020 LONG 35R-36R. FS 1100-CSDR ZIAA96060Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. AFT LWR RT TUNNEL INT FS 1060 LONG 27R. FS 1040 LONG 26L-27R. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR ZIAA96059Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. AFT LWR LT TUNNEL INT. FS 1100 LONG 35L. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR ZIAA96058Extrusion · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. RT CUSP EXTRUSION. FS 460-480. FS 870-LONG 24R. FS 220-RT UPPER. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR ZIAA96057Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. FWD LWR RT TUNNEL INT FS 400-420. FS 300-320. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR ZIAA96056Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. FUSE UPPER FWD EXT SKIN LONG 20-21R. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR ZIAA96055Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. RT HOR O/B EXT. XE 290. XE 222. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR ZIAA96054Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. LT HOR O/B EXT. XE 271-273. XE 310-312.5. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR ZIAA96053Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. RT WING I/B LE EXT. WFS 200. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR ZIAA96052Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. RT INB STUB EXT. WS 163.750. SLOT PANEL. UPPER SURFACE. XFS 291.500. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR ZIAA96051Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. LT INB STUB INT. UPPER FLANGE. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR ZIAA96050Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. LT INB STUB EXT XW 223-257. XW 246-251. XW 246.519. XW 246-519 AFT INB SLOT. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR ZIAA96049Spar · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. LT WING LE SPAR XFS 500. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR ZIAA96048Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. LT WING XW 257-408. XFS 285-309. XFS 329. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR ZIAA96047Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. RT WING LE EXT. XFS 422.750. MIDDLE PANEL. XFS 566.250. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR ZIAA96046Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. LT STUB LE EXT. XFS 560-575. XFS 575. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR ZIAA96045Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. RT AIL INT XA 474-535. XA 646-678. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR ZIAA96044Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. LT WING XW 408 EXT XRS 763. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR ZIAA96043Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. RT WING LE EXT. XIS 697 SEAM. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR ZIAA96042Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. LT WING LE EXT WS 575-599. XFS 566-603. REPAIRED IAW APPLICABLE SRM'S, DWG, ETC. (X)SDR ZIAA96041Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. RT WING LE EXT CORROSION. XW 761.695-765. REPAIRED IAW APPLICABLE SRM'S, DWG, ETC. (X)SDR ZIAA96040Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. LT WING LE EXT CORROSION. XFS 710-746. XW 761.695. XFS 817-820. REPAIRED IAW APPLICABLE SRM'S, DWG, ETC. (X)SDR ABXA9600636Switch · defectiveRIGHT MAIN LANDING GEAR GREEN DOWN AND LOCKED LIGHT DID NOT ILLUMINATE AFTER GEAR HANDLE SELECTED DOWN. RECYCLED GEAR, NO HELP. RED LIGHT OUT, NO HORN AT 35 DEGREE FLAPS. GREEN LIGHT ILLUMINATED JUST PRIOR TO LANDING. REPLACED RIGHT MLG DOWN LOCK SWITCH IASDR CKSA96159Doubler · damagedPERFORM DOUBLER REWORK IAW EA 96-268A STATIC PORT STATION 390 LBL 25 TO LBC 281 DRAWING NR AIA/E/2250 REVISION ORIGINAL DATED 07/17/96. PERFORMED DOUBLER REWORK IAW EA 96-268A DRAWING NR AIA/E/2250 REVISION ORIGINAL DATED 07/17/96 STATIC PORT STATION 390 LBL SDR ARWA9609031Battery Pack · dischargedEMERGENCY EXIT LIGHT DOES NOT DISARM. DOME LIGHT STAYS ON. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECKED OK IAW MM 3-50-00.SDR ARWA9609030Relay · malfunctionedWHILE ON CLIMBOUT, LOST NR 1 DC BUS, CAPTAIN'S INSTRUMENTS LIGHTS OUT, 1 AND 2 ENGINE OIL TEMP, OIL QTY, CSD NR 1 FUEL FEED PUMP NR 1 ALT FUEL PUMP, HYD QTY. RETURNED TO MIAMI WITHOUT INCIDENT. WHEN PUT GEAR DOWN, ALL ABOVE RETURNED TO NORMAL. REMOVED AND RSDR RRXA96086Fire Loop · broken wireKDAY - FLT 228 - IN FLIGHT, NR 2 ENGINE FIRE WARNING (BOTTLES WERE NOT DISCHARGED). SHUTDOWN ENGINE IN FLIGHT. INSPECTED ALL FIRE LOOPS. FOUND BROKEN WIRE AT SPLICE ON FORWARD UPPER FIRE LOOP. REPAIRED SPLICE, HOT AIR LEAK CHECKED NR 2 ENGINE. NO LEAKS ORSDR ARWA9609029Engine · failedNR 4 ENGINE SHUT DOWN IN FLIGHT BECAUSE OF LOW OIL PRESSURE. AIRCRAFT CONTINUED INTO ELP WITHOUT INCIDENT. MAINTENANCE FOUND OIL WAS LOST OUT OF THE ENGINE TAILPIPE. AIRCRAFT FERRIED TO MIAMI WHRE NR 4 ENGINE WAS REMOVED AND REPLACED. CAUSE OF FAILURE TO BSDR TC8A96058Egt Indicator · failedNR 3 ENGINE BETWEEN 360 TO 390 DEGREES EGT DURING IDLE. REPLACED NR 3 ENGINE EGT INDICATOR, OPS CHECKED NORMAL IAW 77-20-1.SDR IXXA96157Fan · failedAFTER TAKEOFF, AN ACRID ELECTRICAL SMELL ACCOMPANIED WITH SMOKE WAS DETECTED BY THE FLIGHT CREW. THE RECIRCULATION FANS WERE TURNED OFF AND THE SMOKE AND SMELL DISIPATED. MAINTENANCE INSPECTED BOTH FANS AND FOUND THE RIGHT FAN APPEARED TO BE OVERHEATED AND ASDR RRXA96119O-Ring · failedON CLIMBOUT, LOST HYDRAULIC SYSTEM PRESSURE, STOPPED QUANTITY LOSS AT 6 GALLONS INDICATED. LOSS OF HYDRAULIC SYSTEM AND PRESSURE EMERGENCY CHECKLIST FOLLOWED. MAINTENANCE REPLACED THE O-RING IN THE SLOT CONTROL VALVE MOUNT, SERVICED THE HYDRAULIC SYSTEM. HYSDR ABXA9600615Retract Mech · lack of lubeVIBRATION AND BUFFETING OCCURS IN FLIGHT IN GEAR UP/DOWN AND FLAPS UP/ DOWN CONFIGURATION. GREATER AT HIGHER AIRSPEEDS UP TO 210 KNOTS. FOUND RIGHT NOSE GEAR DOOR OPEN ON ARRIVAL. LUBED ALL FITTINGS, CLOSED DOOR SEVERAL TIMES AND NO DEFECTS NOTED.SDR IXXA96154Cusp · corrodedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT CUSP EXTRUSTION WAS FOUND CORRODED BETWEEN FUSELAGE STATIONS 225 AND 245. THE CUSP WAS REPAIRED IAW FAA DER APPROVED DRAWING B12-R10. (M)SDR IXXA96153Skin · crackedDURING ROUTINE C-CHECK INSPECTION, A 1 INCH CRACK WAS FOUND IN THE LEFT WING LEADING EDGE, THE CRACK WAS LOCATED 6 INCHES FORWARD OF THE FORWARD SPAR AT WING STATION XFS 422. THE DAMAGE WAS REPAIRED IAW FAA DER APPROVED DRAWING B12-R05. (M)SDR IXXA96152Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, THE LEFT WING, LEADING EDGE, INNER SLOT CUTOUT WAS FOUND TO BE CORRODED. REPAIR WAS ACCOMPLISHED IAW FAA DER APPROVED DRAWING B12-R03. (M)SDR IXXA96151Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT INBOARD AILERON LOWER PLATING WAS FOUND TO BE CORRODED. REPAIR TO THE PLATING WAS ACCOMPLISHED IAW FAA DER APPROVED REPAIR B12-R09. (M)SDR IXXA96148Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, THE LEFT WING CENER LEADING EDGE SLOT PLATING WAS FOUND CORRODED. REPAIR OF THE PLATING WAS ACCOMPLISHED IAW FAA DER APPROVED DRAWING B12-R02. (M)SDR IXXA96147Skin · crackedDURING ROUTINE C-CHECK INSPECTION, A 6 INCH CRACK WAS FOUND AT THE LEFT WING SLOT PLATING AT STATION 341.5. THE PLATING WAS REPAIRED IAW FAA DER APPROVED DRAWING B12-R01. (M)SDR ABXA9600645Fitting · crackedDURING 'C' CHECK, FOUND LEFT WING FLAP SUPPORT FITTING CRACKED AT XW 340. REMOVED CRACKED FLAP SUPPORT FITTING AND INSTALLED SERVICEABLE FLAP SUPPORT FITTING.SDR ABXA9600644Fitting · crackedDURING 'C' CHECK, FOUND RIGHT WING SUPPORT FITTING CRACKED AT XW 340. REPAIRED RIGHT WING SUPPORT FITTING IAW REA NR D827-16054.SDR IXXA96150Bulkhead · crackedDURING ROUTINE C-CHECK INSPECTION, AN 8 INCH CRACK WAS FOUND IN THE PRESSURE BULKHEAD (CABLE FEED THROUGH) AT FUSELAGE STATION 680 LEFT. THE PRESSURE BULKHEAD WAS REPLACED. (M)SDR IXXA96149Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT MAIN LANDING GEAR ATTACH FITTING WAS FOUND TO HAVE CRACKED. THE 1 INCH CRACK IS TYPICAL AND ILLUSTRATED IN VIEW FF OF S/B 57-94. THE MAIN LANDING GEAR FITTING WAS REPLACED IAW THE SRM AND DOUGLAS FITTING CHANGE GUSDR ARWA9608003Instrument Amp · failedEN ROUTE FROM JFK TO SJU, NR 2 ADI GYRO FLAG IN VIEW. RESET CIRCUIT BREAKER, NO HELP. INTERMITTENT FLAG IN CRUISE, FLAG IN VIEW AT ALL TIMES DURING DESCENT, DIVERTED TO MIA. REMOVED AND REPLACED NR 2 INSTRUMENT AMP. SYSTEM OPS NORMAL I.A.W. DC-8 MM 34-25-0SDR ARWA9608002T3 Disc · crackedDURING ROUTINE ACCOMPLISHMENT OF AD 82-14-02, ENGINE S/N 669162, NR 4 POSITION, EDDY CURRENT INSPECTION INDICATED T3 DISK CRACKED THROUGH ONE TIEBOLT HOLE. T3 DISK ASSEMBLY WAS REMOVED AND REPLACED I.A.W. OA 1349 AND JT3D MAINTENANCE MANUAL CHAPTER 72. INSTASDR TC8A96052Egt Temp Ind · malfunctionedNR 3 ENGINE IDLE EGT 400 DEGREES CELCIUS. CHECKED EGT INDICATION SYSTEM AS PER MM 77-20-0 NORMAL. ALSO, CHECKED THERMO COUPLE PROBES AND HARNESS, NORMAL. CARRIED OUT AN ENGINE TEST AS PER MM 71-00, ENGINE OPERATING LIMITS FOUND NORMAL.
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