Douglas DC-8-63F

Service difficulty reports · 1,883

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 = 'DC863F'
  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 ARWA0001219Skin · dentedN/R 702 - DURING C CHECK INSPECTION, FOUND THE FOLLOWING: DENTED RT WING INBOARD FLAP LOWER SECTION. CORRECTIVE ACTION: REMOVED AND REPLACED NEW SKIN IAW E.O. AS11209, AND SEALED AREA IAWSRA 51-1-15.Dec 4, 2000 · N661AV · Doug DC863F · Trailing Edge FlapsSDR ARWA0001218Skin · dentedN/R 275 - DURING C CHECK INSPECTION, FOUND THE FOLLOWING: DENTED EXTERIOR FUSELAGE SKIN AT STA.270.0 L24R AND L25R. CORRECTIVE ACTION: REPAIRED IAW E.O. # 0011201, DATED 11/20/00; PRIME IAW SRM 51-1-8 AND INSTALLED IAW SRM51-1-20DDec 4, 2000 · N661AV · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA0001217Floorbeam · corrodedN/R 629 - DURING C CHECK INSPECTION, FOUND THE FOLLOWING: MAIN CARGO COMPARTMENT FLOORBEAM AT STA LBL 45 & FS 1680 CORRODED. CORRECTIVE ACTION: CORROSION REPAIR IAW BOEING MESSAGE INW-LIM-00-00147H, DATED 10/23/00.Dec 4, 2000 · N661AV · Doug DC863F · Fuselage Main, Floor BeamSDR ARWA0001216Skin · scratchedN/R 1004 - DURING C CHECK INSPECTION, FOUND THE FOLLOWING: EXTERIOR FUSELAGE SKIN SHOWS 2 INCH INCH LONG SCRATCH AND 0.065 DEEP AT STA.1400 LONGERON 31R. CORRECTIVE ACTION: CUT SKIN FOR SKIN REPLACEMENT IAW AS ELEVEN DRAWING AS11215, DATED 11/02/00, PRIMED ANDDec 4, 2000 · N661AV · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA0001215Skin · corrodedN/R 278 - DURING C CHECK INSPECTION, FOUND THE FOLLOWING: CORRODED AFT CARGO COMPARTMENT INNER SKIN BETWEEN STA 1216 AND 1227 L35L & L35R.CORRECTIVE ACTION: REMOVED CORROSION IAW SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW 53-2-0. REPAIRED CORROSION IAW BOEING MDec 4, 2000 · N661AV · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA0001214Doubler · damagedN/R 958 - DURING C CHECK INSPECTION, FOUND THE FOLLOWING: COCKPIT SUBFLOOR FINGER DOUBLER WITH CORROSION NEAR LONGERON 22L FS STA 32/52. CORRECTIVE ACTION: CUT OUT DAMAGE AREA AND INSTALLED DOUBLER REPAIR IAW BOEING MESSAGE INW-LIM-00 000145H, DATED 10/19/00.Dec 4, 2000 · N661AV · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA0001213Fitting · crackedN/R 133 - DURING C CHECK INSPECTION FOUND THE FOLLOWING: FOWARD CARGO COMPARTMENT 3/4 INCH CUT BETWEEN STA 80 AND 85, LONG.27L. REMOVED DAMAGE LONGERON SECTION FABRICATED NEW SECTION SPLICE FITTING, ANGLES AND EXTERNAL DOUBLER IAW BOEING MESSAGE INM-LIM-00-001Dec 4, 2000 · N661AV · Doug DC863F · Fuselage Main, BulkheadSDR ARWA0001212Skin · damagedN/R 785 - DURING C CHECK INSPECTION FOUND THE FOLLOWING: RT HORIZONTAL STABILIZER LEADING EDGE SHOWS TEMP REPAIR. REMOVED I/B L/E; FABRICATED & INSTALLED REPAIRED IAW DRAWING AS11212, DATED 10/07/00, SEALED AREA IAW SRM 51-1-15 AND INSTALLED LEADING EDGE IAW Dec 4, 2000 · N661AV · Doug DC863F · Horizontal Stabilizer, Plate/SkinSDR ARWA0001210Panel · corrodedN/R 288 - DURING C CHECK INSPECTION, FOUND THE FOLLOWING: LEVEL I CORROSION AT LT HORIZONTAL STABILIZER LOWER PANEL AT STA.XE 260.00.REMOVED AND REPLACED SKIN PANEL IAW DRAWING AS11210, DATED 10/07/00, SEALED AREA IAW SRM 51-1-15.Dec 4, 2000 · N661AV · Doug DC863F · Horizontal Stabilizer, Plate/SkinSDR ARWA0001209Panel · corrodedN/R 257 - DURING C CHECK INSPECTION FOUND THE FOLLOWING: LEVEL I CORROSION AT UPPER PANEL RT HORIZONTAL STABILIZER AT STA.XE 1272.00 TO 219.979. REMOVED AND REPLACED PANEL IAW DRAWING AS11210, DATED 10/07/00, SEALED AREA IAW SRM 51-1-15.Dec 4, 2000 · N661AV · Doug DC863F · Horizontal Stabilizer, Plate/SkinSDR ARWA0001208Panel · corrodedN/R 252 - DURING C CHECK INSPECTION FOUND THE FOLLOWING: LEVEL I CORROSION AT UPPER L/H HORIZONTAL STABILIZER AT STA.XE 312.500.CORRECTIVE ACTION: REMOVED AND REPLACED SKIN PANEL IAW DRAWING # AS11210, DATED 10/07/00, SEALED AREA IAW SRM 51-1-8.Dec 4, 2000 · N661AV · Doug DC863F · Horizontal Stabilizer, Plate/SkinSDR ARWA0001207Fitting · crackedN/R 216 - DURING C CHECK INSPECTION, FOUND THE FOLLOWING: FORWARD CARGO COMPARTMENT SHOWS 3/4 INCH CRACKED FITTING AT STA 320, LONG.27L.REMOVED & REPLACED FITTING IAW BOEING MESSAGE INW-LIM-00-00135H, DATED 10/02/00.Dec 4, 2000 · N661AV · Doug DC863F · Fuselage Main, Attach FittingsSDR IXXA0000042Control Valve · defectiveENROUTE FROM TOL TO DFW, THE GEAR DOOR NOT LATCH LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE GEAR, BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO DFW FOR AN UNEVENTFUL LANDING. MAINTENANCE PERFORMED AN OPNov 23, 2000 · N867BX · Doug DC863F · Landing Gear Retraction/Extension SystemSDR ABXA000492Connector · looseRIGHT MAIN LANDING GEAR DOWN AND LOCKED INDICATION LIGHT FAILED TO ILLUMINATE WHEN GEAR SELECTED DOWN. THE FLIGHT CREW CYCLED GEAR, AND THE LIGHT ILLUMINATED. MAINTENANCE INSPECTED, CLEANED AND TIGHTEND THE RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH CANNON PLUGNov 12, 2000 · N816AX · Doug DC863F · Landing Gear Position and WarningSDR ABXA000489Valve · leakingAIRCRAFT HAD A LOSS OF HYDRAULIC QUANTITY ON TAKEOFF, DOWN TO STANDPIPE. CREW ELECTED TO USE AIR BRAKES UPON LANDING. REPLACED BRAKE CONTROL VALVE AND O-RINGS IAW DC8 MM.Nov 7, 2000 · N811AX · Doug DC863F · Hydraulic System, MainSDR RRXA003351Panel · delaminatedDURING A MAINTENANCE VISIT FOUND A DELAMINATED PANEL ON THE LT WING LWR T/E AT STA XW 5.00 TO XW 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 30, 2000 · N957R · Doug DC863F · Wing, Plate/SkinSDR RRXA003350Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION AND A DENTED HOLE TO THE LT WING LWR SURFACE T/E PANEL UNDER HYD TANK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 30, 2000 · N957R · Doug DC863F · Wing, Plate/SkinSDR RRXA003349Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE LT WING LWR SURFACE T/E PANEL AT STA 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 30, 2000 · N957R · Doug DC863F · Wing, Plate/SkinSDR RRXA003348Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE LT WING LWR SURFACE T/E PANEL AT STA XW 98 TO XW 138, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 30, 2000 · N957R · Doug DC863F · Wing, Plate/SkinSDR RRXA003347Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE LT WING LWR SURFACE T/E PANEL AT STA 138 TO 214, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 30, 2000 · N957R · Doug DC863F · Wing, Plate/SkinSDR RRXA003346Skin · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE LEFT WING LWR SURFACE T/E PANEL NR 577B, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 30, 2000 · N957R · Doug DC863F · Wing, Plate/SkinSDR RRXA003345Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE O/B FLAP O/B EXHAUST GATE FLANGE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 30, 2000 · N957R · Doug DC863F · Trailing Edge FlapsSDR RRXA003344Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP RIB ANGLE AT THE LEFT O/B FLAP I/B SCISSOR LINK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 30, 2000 · N957R · Doug DC863F · Trailing Edge FlapsSDR RRXA003343Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE SKIN AT THE LEFT I/B FLAP BOTTOM, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 30, 2000 · N957R · Doug DC863F · Trailing Edge FlapsSDR RRXA003342Channel · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LEFT I/B FLAP I/B TRAILING EDGE WEDGE CHANNEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 30, 2000 · N957R · Doug DC863F · Trailing Edge FlapsSDR RRXA003341Floor Panel · crackedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND A CRACK TO THE COCKPIT FLOOR PANEL NR 677, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 30, 2000 · N957R · Doug DC863F · Fuselage Floor PanelSDR RRXA003340Floor Panel · crackedDURING A MAINTENANCE VISIT FOUND CORROSION AND A CRACK TO THE TOP AND BOTTOM OF THE COCKPIT FLOOR PANEL 679, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 30, 2000 · N957R · Doug DC863F · Fuselage Floor PanelSDR RRXA003339Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BOTH SIDES OF THE COCKPIT FLOOR PANEL UNDER F/E''S DESK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 30, 2000 · N957R · Doug DC863F · Fuselage Floor PanelSDR RRXA003338Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE COCKPIT FLOOR PANEL UNDER FE''S CONSOLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 30, 2000 · N957R · Doug DC863F · Fuselage Floor PanelSDR RRXA003337Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CIRCUMFERENTIAL FRAME FITTING AT STA 1480 AND L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 30, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA003336Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMGE TO THE FRAME TO CUSP FITTING AT STA 1460 AND L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 30, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA003335Finger Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND POPPED RIVET HEADS TO THE UPPER SURFACE W/W FINGER DOUBLER BETWEEN STA 902 - 920 AND LBL 4 LBL -4 Z AXIS -10, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 30, 2000 · N957R · Doug DC863F · Fuselage Main, Plate/SkinSDR RRXA003334Panel · delaminatedDURING A MAINTENANCE VISIT FOUND THE COCKPIT FLOOR SEPARATED AT STA -12 TO -32, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 30, 2000 · N957R · Doug DC863F · Fuselage Floor PanelSDR IXXA0000037Panel · defectiveEN ROUTE FROM LRD TO BRO, DURING DESCENT LOST OF ALL GENERATOR ELECTRICAL POWER WAS EXPERIENCED. THE FLT CREW FOLLOWED COMPANY PROCEDURES AND ALL ELECTRICAL POWER WAS RESTORED. ALL GENERATOR OPERATING PARAMETERS WERE NORMAL. SEVERAL MINUTES LATER ELECTRICALOct 28, 2000 · N870BX · Doug DC863F · AC Generation SystemSDR RRXA003352Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ALONG THE MOUNTING SURFACE OF THE NR 2 ADF AT STA 145 - 170 AND L36 TO L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 25, 2000 · N957R · Doug DC863F · Fuselage Main, Plate/SkinSDR RRXA003290Rib · crackedDURING A MAINTENANCE VISIT FOUND CORROSION AT RIGHT I/B FLAP-RIB-LOC AT STA XW 64 18 - 20 INCHES AFT OF FLAP FRONT SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 20, 2000 · N957R · Doug DC863F · Trailing Edge FlapsSDR RRXA003289Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE ATTACH ANGLE AT THE RIGHT W/W AT STA XWO ABOVE L24R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 20, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA003291Fitting · misdrilledDURING A MAINTENANCE VISIT FOUND A DRILLED AREA TO THE CIRCUMFERENTIAL FRAME FITTING AT STA 640 AND L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 18, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA003292Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL ATTACH FITTING BETWEEN MLG DOORS AT STA 930, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 16, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA003299Stringer · chafedDURING A MAINTENANCE VISIT FOUND A CHAFED STRINGER SIDEWALL AND HOLES ELONGATED ON THE NR 4 THRUST REVERSER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 13, 2000 · N957R · Doug DC863F · Engine Thrust ReverserSDR RRXA003298Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AND MISSING FASTENERS TO THE A & B PIT CENTER DIVIDER WALL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 13, 2000 · N957R · Doug DC863F · Fuselage Main, BulkheadSDR RRXA003297Intercostal · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED INTERCOSTAL BETWEEN MLG DOORS AND LT AND RT ATTACH FITTINGS AT STA 902, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 13, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA003296Intercostal · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL BETWEEN MLG DOORS AT STA 940, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 13, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA003295Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL ATTACH FITTINGS BETWEEN MLG DOORS AT STA 960, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 13, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA003294Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL ATTACH FITTING BETWEEN MLG DOORS AT STA 950, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 13, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA003293Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL ATTACH FITTINGS BETWEEN MLG DOORS AT STA 890, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 13, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA003308Web · tool damageDURING A MAINTENANCE VISIT FOUND DRILL HOLES AND DRILL STARTS IN WEB AT STA 1340 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 12, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA003307Frame · misdrilledDURING A MAINTENANCE VISIT FOUND A DRILL START AT FLOOR LEVEL AT STA 1280 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 12, 2000 · N957R · Doug DC863F · Fuselage Main, FrameSDR RRXA003306Longeron · misdrilledDURING A MAINTENANCE VISIT FOUND DRILL STARTS AND HOLES IN STRINGER AT STA 440 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 12, 2000 · N957R · Doug DC863F · Fuselage Main, Longeron/StringerSDR RRXA003305Web · misdrilledDURING A MAINTENANCE VISIT FOUND HOLES IN WEB BETWEEN STA 260 - 280 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 12, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous Structure
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