Douglas DC-8-62

Service difficulty reports · 2,778

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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 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 RRXA99917Jamb · tornPER FAA RAMP INSP, METAL TORN AT UPPER SECTION OF MAIN CARGO DOOR JAMB. AIRCRAFT FERRIED TO KMQY FOR REPAIRS.May 13, 1999 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR 99T64R293ARSkin · crackedNR 0890 - EVALUATED REPAIR ON FUSELAGE SKIN FORWARD CABIN DOOR OPENING TOP FORWARD CORNER STA 225. REMOVED DOUBLER, FOUND SKIN CRACKED, CUT OUT CRACK IAW DC-8 SRM 53-2-2 FIG 15. FABRICATED FILLER AND DOUBLER IAW DC-8 SRM 52-2-0. INSTALLED FILLER AND DOUBLERMay 13, 1999 · N1808E · Doug DC862 · Fuselage Main, Plate/SkinSDR ABXA9900366Handle · brokenCOCKPIT DOOR HANDLE BROKEN, WOULD NOT OPEN FROM AFT SIDE. REPLACED COCKPIT DOOR HANDLE IAW DC8 SRM 51-3-0.May 12, 1999 · N803AX · Doug DC862 · Fixed Inner DoorsSDR 99T64R365ARPanel · corrodedRIGHT WING OUTBOARD SLOT PANEL HAS CORROSION EMANATING FROM SCREW HOLES XS 497.491. REMOVED CORROSION AND BLENDED AREA PER EO99-061. (M)May 11, 1999 · N1808E · Doug DC862 · Leading Edge DevicesSDR 99T64R248ARFrame · corrodedNR 1584 - CORROSION FRAME 1060 TO CHORD, ALSO SEVERAL NUTPLATES BROKEN FROM L33R-L33L. REMOVED CORROSION IAW DC-8 SRM 51-1-8. CUT OUT DAMAGED AREA, FABRICATED REPAIR STRAP PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. INSTALLED IAW DC-8 SRM 51-May 11, 1999 · N1808E · Doug DC862 · Fuselage Main, FrameSDR 99T64R359ARLongeron · corrodedFOUND CORROSION L36 BETWEEN STATION 1080-1100. REMOVED CORROSION IAW DC-8 SRM 51-1-8. NEGLIGIBLE AMOUNT MATERIAL REMOVED. FABRICATED AND INSTALLED STRAP PER EO 99-061 (DUE TO ELONGATED HOLES). (M)May 10, 1999 · N1808E · Doug DC862 · Fuselage Main, Longeron/StringerSDR 99T64R302ARSkin · corrodedNR 2175 - LEFT WING, UPPER PLATING SEVERAL AREAS CORRODED BEYOND LIMITS XRS 172-255 STRINGERS 9-11. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED TEMP DOUBLER IAW BOEING MESSAGE M-7200-99-02532, ITEMS 4, 6 AND 10 AND TTS-MQY 99-04-30-012. May 9, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR 99T64R362ARLongeron · corrodedFOUND CORROSION L35R BETWEEN STATION 1260-1240. REMOVED CORROSION, FABRICATED STRAPS AND INSTALLED PER EO 99-061. (M)May 6, 1999 · N1808E · Doug DC862 · Fuselage Main, Longeron/StringerSDR 99T64R361ARLongeron · corrodedFOUND CORROSION L35R BETWEEN 1220-1240. REMOVED CORROSION, FABRICATED STRAPS AND INSTALLED PER EO 99-061. (M)May 6, 1999 · N1808E · Doug DC862 · Fuselage Main, Longeron/StringerSDR 99T64R360ARLongeron · corrodedFOUND CORROSION L36 BETWEEN 1220-1240. REMOVED CORROSION, FABRICATED STRAP AND INSTALLED PER EO 99-061. (M)May 6, 1999 · N1808E · Doug DC862 · Fuselage Main, Longeron/StringerSDR IXXA9900009Uplatch · lack of lubeAFTER TAKEOFF FROM AVB EN ROUTE TO FRA, WHEN THE LANDING GEAR WAS RETRACTED THE MAIN GEAR DOOR NOT LATCHED LIGHT REMAINED ILLUMINATED. THE FLIGHT CREW CYCLED THE LANDING GEAR WITH THE WARNING INDICATION REMAINING THE SAME. THE FLIGHT CONTINUED TO FRA FOR AN May 4, 1999 · N61CX · Doug DC862 · Landing Gear Retraction/Extension SystemSDR 99T64R249ARSkin · corrodedNR 1928 - EXTERIOR CORROSION AROUND ACCESS DOOR CUT OUT AT STA 1620. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED REPAIR DOUBLER AND INSTALLED PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X)May 4, 1999 · N1808E · Doug DC862 · Fuselage Main, Plate/SkinSDR 99T64R340ARClip · missingMAIN CARGO DOOR UPPER JAM INSTALLATION STATION 500 CLIPS MISSING 2 EACH. FABRICATED CLIPS AND INSTALLED IAW DWG AS11035 AND DC-8 SRM 51-1-8. (M)May 3, 1999 · N1808E · Doug DC862 · Fuselage Miscellaneous StructureSDR 99T64R338ARClip · missingMAIN CARGO DOOR, UPPER JAM INSTALLATION CLIPS MISSING 2 EACH. FABRICATED CLIPS AND INSTALLED IAW DWG AS11035 AND DC-8 SRM 51-1-8. (M)May 3, 1999 · N1808E · Doug DC862 · Fuselage Miscellaneous StructureSDR 99T64R391ARFastener · looseFOUND DURING C-CHECK, MISSING, BROKEN AND/OR LOOSE FASTENER AND MISSING SHIMS (JOGGLE). REPLACED RIVETS, BROKEN/LOOSE FASTENERS AND MISSING SHIMS IAW DWG AS11041. (M)Apr 30, 1999 · N1808E · Doug DC862 · Cargo/Baggage DoorsSDR 99T64R352ARSpar · crackedINBOARD LOWER AUX SPAR CAP CRACKED AT OUTBOARD END WHERE IT ATTACHES TO GEAR TRUNNION RIGHT GEAR LARGE PIN LUG. REMOVED AND INSTALLED NEW AUX SPAR CAP IAW DC-8 S/B 57-85R1. (M)Apr 29, 1999 · N1808E · Doug DC862 · Wing SparSDR IXXA9900008Bulb · failedTHE FLIGHT CREW PERFORMED A POST FLIGHT CHECK LIST AT OKO, WHICH REVEALED TWO PASSENGERS EMERGENCY EXIT AISLE PATHWAY LIGHTS INOPERATIVE. MAINTENANCE REPLACED TWO LIGHT BULBS AND PERFORMED A SUCCESSFUL OPERATIONAL CHECK.Apr 29, 1999 · N31CX · Doug DC862 · Emergency LightingSDR 99T64R291ARFrame · misrepairedNR 2824 - NOSE FUSELAGE SECTION STA 44 2 O'CLOCK POSITION JUST AFT PRESSURE BULKHEAD FRAME 44 ILLEGAL SKIN AND FRAME REPAIR. REMOVED SKIN/FRAME REPAIR, FABRICATED NEW FILLER AND DOUBLER IAW DC-8 SRM 53-2-1. INSTALLED IAW DC-8 SRM'S 53-2-0 AND 53-2-1. REF: Apr 28, 1999 · N1808E · Doug DC862 · Fuselage Main, FrameSDR 99T64R237ARFitting · corrodedNR 0076 - LT INBOARD FLAP WEDGE CORROSION AROUND ATTACH FITTINGS. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS PER EO 99-061 WITH APPROVEDF FAA FORM 8110-3 DATED 6-8-99. REF: ARROW AIR, ARWA. (X)Apr 27, 1999 · N1808E · Doug DC862 · Trailing Edge FlapsSDR 99T64R111ARSkin · corrodedFOUND PIT SKIN CORROSION BETWEEN FRAME 580-600 L26R AND L27R. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED DOUBLERS AND INSTALLED PER EO 99-019. (M)Apr 26, 1999 · N1808E · Doug DC862 · Fuselage Main, Plate/SkinSDR 99T64R110ARSkin · corrodedLEFT OUTBOARD L/E SECTION CORROSION IN SCREW HOLES, T/E XFS 810 - XFS 960. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED FILLER AND DOUBLER IAW DC-8 SRM 57-2-1 AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-22 AND 57-2-1. (M)Apr 26, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR 99T64R109ARSkin · corrodedLEFT WING TOP OUTBOARD TIP LEADING EDGE. CORROSION AROUND SCREWS STATION 695 XW 761. CORROSION REMOVED IAW DC-8 SRM 51-1-8. FABRICATED FILLER AND DOUBLER IAW DC-8 SRM 57-2-1 AND INSTALLED IAW DC-8 SRM 51-1-21. (M)Apr 26, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR 99T64R390ARShim · missingFOUND DURING C-CHECK, MISSING, BROKEN AND/OR LOOSE FASTENER AND MISSING SHIMS (JOGGLE). REPLACED SHIMS IAW DWG AS11041. (M)Apr 26, 1999 · N1808E · Doug DC862 · Cargo/Baggage DoorsSDR 99T64R301ARSkin · corrodedNR 2178 - LEFT WING UPPER PLATING AREAS CORRODED BEYOND LIMITS XRS 340-358 AT STRINGER 7. REMOVED CORROSION IAW DC-8 SRM 51-1-8. BLENDED AREA IAW BOEING MESSAGE M-7200-99-02532 PAGE 4 OF 4, ITEMS 2/3 DATED 4-22-99. ARROW AIR (M)Apr 26, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR 99T64R115ARAnchor Nut · missingNR 0525 - ONE EACH ANCHOR NUTPLATE MISSING, NR 1 PYLON REMOVABLE PLANK. INSTALLED JO-BOLT IAW EO 99-026 WITH APPROVED FAA FORM 8110-3 DATED 2-9-99. REF: ARROW AIR, ARWA. (X)Apr 26, 1999 · N1808E · Doug DC862 · Nacelle/Pylon, Plate/SkinSDR 99T64R114ARAnchor Nut · missingNR 0524 - 2 EACH, ANCHOR NUTPLATES MISSING NR 2 PYLON REMOVABLE PLANK. INSTALLED JO-BOLTS IAW EO 99-026 WITH APPROVED FAA FORM 8110-3 DATED 2-9-99. REF: ARROW AIR, ARWA. (X)Apr 26, 1999 · N1808E · Doug DC862 · Nacelle/Pylon, Plate/SkinSDR 99T64R113ARAnchor Nut · missingNR 0523 - ONE EACH, ANCHOR NUTPLATES MISSING NR 3 PYLON REMOVABLE PLANK. INSTALLED JO-BOLT IAW EO 99-026 WITH APPROVED FAA FORM 8110-3 DATED 2-9-99. REF: ARROW AIR, ARWA. (X)Apr 26, 1999 · N1808E · Doug DC862 · Nacelle/Pylon, Plate/SkinSDR 99T64R112ARSplice · corrodedNR 0416 - CORROSION L24R SPLICE BETWEEN FRAMES 400-420 RT. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED 2 EACH, SPLICE FITTINGS. REPLACED LONGERON AND INSTALLED PER DC-8 SRM'S 53-2-2 AND 51-3-2. REF: ARROW AIR, ARWA. (X)Apr 26, 1999 · N1808E · Doug DC862 · Fuselage Miscellaneous StructureSDR 99T64R273ARFrame · corrodedNR 2654 - FRAME STA 188 CORROSION AT L6R. REMOVED CORROSION IAW 51-1-8. REMOVED DAMAGED AREA IAW DC-8 SRM 53-2-0. FABRICATED DOUBLER IAW DC-8 SRM 53-2-0 AND INSTALLED IAW DC-8 SRM 53-2-0 REF: ARROW AIR, ARWA. (X)Apr 22, 1999 · N1808E · Doug DC862 · Fuselage Main, FrameSDR 99T64R259ARFrame · corrodedNR 2602 - CORROSION BETWEEN STA 1080 - STA 1100 LT AFT DOUBLER ABOVE L28L. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER AND INSTALLED PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X)Apr 22, 1999 · N1808E · Doug DC862 · Fuselage Main, FrameSDR 99T64R289ARFrame · corrodedNR 0997 - CORROSION FRAME 1520 LOWER CHORD BETWEEN L24R - L26R. REMOVED DAMAGED SECTION IAW DC-8 SRM 53-2-0. FABRICATED NEW SECTION OF FRAME IAW DC-8 SRM 53-2-0. TREATED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED IAW DC-8 SRM 53-2-0. REF: ARROW AIR, ARWA.Apr 21, 1999 · N1808E · Doug DC862 · Fuselage Main, FrameSDR 99T64R262ARShim · crackedNR 2680 - LT WING BOTTOM FRONT SPAR CAP SHIM PLATE CRACKED XS 510.222. REMOVED SHIM, BLENDED SMOOTH THE CRACKED SURFACE, ALODINED AND PRIMED. RE-INSTALLED SHIM AND SEALED WITH PR 1422 B 1/2 PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARApr 21, 1999 · N1808E · Doug DC862 · Wing Miscellaneous StructureSDR IXXA9900007Turbine · failedEN ROUTE FROM PKWA TO PHIK DURING CLIMB, A LOUD NOISE WAS HEARD FROM THE NUMBER TWO ENGINE, ACCOMPANIED BY INCREASING ENGINE GAS TEMPERATURE AND A DECLINE IN OIL PRESSURE. THE FLIGHT CREW SECURED THE ENGINE FOLLOWING COMPANY PROCEDURES AND CONTINUED TO PHIK FApr 20, 1999 · N728PL · Doug DC862 · Turbine SectionSDR 99T64R279ARConduit · crackedNR 2869 - GENERATOR LEADS CONDUIT DENTED NR 2 PYLON JUST FORWARD OF WING LEADING EDGE, YN 260. CUT OUT DAMAGED AREA IAW EO AS11047. INSPECTED WIRING INSULATION, NO DAMAGE. FABRICATED DOUBLER AND INSTALLED PER EO AS11047 WITH APROVED FAA FORM 8110-3, DATED 5Apr 20, 1999 · N1808E · Doug DC862 · Nacelle/Pylon StructureSDR 99T64R263ARShim · crackedNR 2681 - RT WING BOTTOM FRONT SPAR CAP SHIM PLATE CRACKED APPROXIMATELY 1 FOOT INBOARD NR 4 PYLON XS 510.222. REMOVED SHIM, BLENDED SMOOTH THE CRACKED SURFACE, ALODINED AND PRIMED. RE-INSTALLED SHIM AND SEALED WITH PR 1422 B 1/2 PER EO 99-061 WITH APPROVED Apr 20, 1999 · N1808E · Doug DC862 · Wing Miscellaneous StructureSDR 99T64R261ARSkin · corrodedNR 2651 - LT WING, OUTBOARD STUB WING UPPER TRAILING EDGE CORRODED XW 485.000. CUT OUT DAMAGED AREA, FABRICATED FILLERS AND DOUBLERS, INSTALLED PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X)Apr 20, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR 99T64R257ARSkin · damagedNR 2520 - RT INBOARD FLAP WEDGE, SKIN WORN THROUGH AT CORNER ATTACH HOLE XW 122. FABRICATED REPAIR DOUBLERS AND INSTALLED PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X)Apr 20, 1999 · N1808E · Doug DC862 · Trailing Edge FlapsSDR 99T64R247ARSkin · damagedNR 1554 - REMOVED AND REPLACED RT INBOARD FLAP WEDGE LOWER SKIN DUE TO EXCESSIVE DAMAGE. FABRICATED NEW RT INBOARD FLAP WEDGE LOWER SKIN PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. INSTALLED IAW DC-8 SRM 51-1-21. REF: ARROW AIR, ARWA. (X)Apr 20, 1999 · N1808E · Doug DC862 · Trailing Edge FlapsSDR 99T64R351ARPlate · corrodedARROW AIR - RIGHT WING UPPER SURFACE CORROSION AT TRUNNION FITTING FASTENERS. REMOVED CORROSION AND BLENDED AREA IAW BOEING MESSAGE M-7200-99-02208 ITEM 18 WITH APPROVED FAA FORM 8110.3 DATED 4-19-99. INSTALLED FASTENERS IAW DC-8 SRM 51-1-20D. (M0Apr 15, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR 99T64R356ARPanel · corrodedRIGHT FLAP NR 1 REMOVED LEADING EDGE PANEL LIGHT SURFACE CORROSION. REMOVED CORROSION, FABRICATED DOUBLER AND FILLER AND INSTALLED PER EO 99-061. (M)Apr 14, 1999 · N1808E · Doug DC862 · Trailing Edge FlapsSDR 99T64R299ARSkin · corrodedNR 2176 - LEFT WING UPPER PLATING SEVERAL AREAS CORRODED BEYOND LIMITS XRS 375-454 STRINGERS 10 AND 11. REMOVED CORROSION IAW DC-8 SRM 51-1-8. BLENDED AREAS IAW BOEING MESSAGE M-7200-99-02532 ITEM 16, 17, 19, 28. ARROW AIR (M)Apr 14, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR 99T64R290ARSkin · dentedNR 2786 - REPAIR DENT IN FUSELAGE EXTERNAL SKIN BETWEEN STA 1260 AND STA 1280 BETWEEN L34L AND L33L. REMOVED DENT BY CUT-OUT IAW DC-8 SRM 53-2-1. FABRICATED DOUBLER IAW DC-8 SRM 53-2-1. INSTALLED DOUBLER IAW DC-8 SRM'S 51-1-21 AND 51-1-20. REF: ARROW AIR,Apr 13, 1999 · N1808E · Doug DC862 · Fuselage Main, Plate/SkinSDR 99T64R255ARWeb · damagedNR 2484 - LT FLAP WELL WEB DAMAGED XCW 69.5 BS 980 - BS 1020. REMOVED WEB, FABRICATED NEW WEB AND INSTALLED PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X)Apr 13, 1999 · N1808E · Doug DC862 · Wing Miscellaneous StructureSDR 99T64R245ARChafe Strip · crackedNR 1248 - RT INBOARD CHAFE STRIP DAMAGED AND CRACKED XW 138. REMOVED DAMAGED CHAFE STRIP, FABRICATED NEW STRIP AND INSTALLED PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X)Apr 13, 1999 · N1808E · Doug DC862 · Trailing Edge FlapsSDR 99T64R286ARSkin · crackedNR 1738 - CRACK L2 DOOR CUT OUT UPPER REAR CORNER STATION 1500. CUT OUT DAMAGED AREA IAW DC-8 SRM 53-2-0. FABRICATED FILLER AND DOUBLERS IAW DC-8 SRM 53-2-0. TREATED AND PRIMED IAW DC-8 SRM 51-1-8 AND INSTALLED IAW DC-8 SRM 53-2-0. ARROW AIR (M)Apr 9, 1999 · N1808E · Doug DC862 · Fuselage Main, Plate/SkinSDR 99T64R303ARSkin · corrodedNR 2798, STRINGER 13 AT XRS 100 CORROSION AT FASTENERS RIGHT WING. REMOVED CORROSION IAW 51-1-8. BLENDED AREA IAW BOEING MESSAGE M-7200-99-02208 RED D ITEM 6. ARROW AIR (M)Apr 9, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR 99T64R300ARSkin · corrodedNR 2795, CORROSION STRINGER 11XRS 3411 FASTENER HOLE. REMOVED CORROSION IAW DC-8 SRM 51-1-8. BLENDED AREA IAW BOEING MESSAGE M-7200-99-02208 REF D ITEMS 11-15. ARROW AIR (M)Apr 8, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR 99T64R355ARPlate · dentedLEFT WING LEADING EDGE DENT AT BOTTOM FORWARD STATION 32. VERIFIED NO CRACKS BY NDT METHOD. FABRICATED DOUBLER AND INSTALLED PER EO 99-061. (M)Apr 7, 1999 · N1808E · Doug DC862 · Wing, Plate/SkinSDR 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 System
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