Douglas DC-8-63F

Service difficulty reports · 1,883

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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 = 'DC863F'
  ORDER BY difficulty_date DESC"

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SDR ABXA060122Fitting · corrodedAFT CARGO COMPARTMENT AREA BELOW C-3 DOOR HAD FITTINGS (2 EACH) CORRODED IN BOX SECTION FS 1176, RIGHT BUTT LINE 20. REMOVED AND REPLACED FITTINGS AT AFT CARGO COMPARTMENT BELOW C-3 DOOR IAW DC8 SRM 51-1-20 AND 53-2-00.Jan 21, 2006 · N816AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA060120Fitting · crackedAFT LOWER CARGO COMPARTMENT FITTINGS (3 EACH) CRACKED, BETWEEN FS 1200 - 1220, RIGHT BUTT LINE 20, LOWER DOOR CUT OUT BOX SECTION. REMOVED AND REPLACED FITTINGS AT AFT CARGO COMPARTMENT BELOW C-3 DOOR IAW DC8 SRM 51-1-20D.Jan 20, 2006 · N816AX · Doug DC863F · Fuselage Main, Attach FittingsSDR ABXA060059Skin · corrodedFUSELAGE SKIN LOWER SIDE OF NR 3 CARGO DOOR HAD A SPOT OF CORROSION. REPAIRED NR3 CARGO DOOR JAMB SKIN IAW SRM 53-2-1, FIG. 9. PARTIAL WORK NR1-102 FOR WORK ACCOMPLISHED (W.O. 600239852) COI 50853 INITIATED FOR REPAIR REPLACEMENT IN 1000 CYCLES.Jan 20, 2006 · N811AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA060056Fitting · crackedFITTING AT LONGERON 24, FS 879, CRACKED. REPAIRED FITTING IAW REA D853-53104.Jan 16, 2006 · N812AX · Doug DC863F · Fuselage Main, Attach FittingsSDR ABXA060031Fitting · crackedINTERCOSTAL CORNER FITTING CRACKED FUSELAGE STA 50, RIGHT BUTT LINE 50, FORWARD OF FLOORBEAM. REMOVED CRACKED CORNER FITTING IAW DC8 SRM 51-1-20D. FABRICATED NEW CORNER FITTING IAW REA D853-52924 AND INSTALLED AT STA 50, RIGHT BUTT LINE 50, FORWARD OF FLOORBDec 30, 2005 · N826AX · Doug DC863F · Fuselage Main, Attach FittingsSDR ABXA060033Doubler · corrodedCORROSION ON BELLY SKIN DOUBLER IN 4 AREAS BETWEEN STA 781 AND STA 798, LEFT BUTT LINE 4 TO LEFT BUTT LINE 10. REMOVED CORROSION ON BELLY SKIN DOUBLER IAW DC8 SRM 51-1-8. THREE AREAS WITHIN LIMITS IAW DC8 SRM 53-02. REMAINING AREA OUT OF LIMITS. ACCOMPLISHDec 29, 2005 · N826AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA060030Frame · corrodedMAIN CARGO STA 1734 BUTT LINE 0, LONGERON 35 LEFT - 35 RIGHT, SURFACE CORROSION ON FRAME. REMOVED CORROSION FROM FRAME. DAMAGE WAS OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 53-2-0 FIG 2, SHT 2.Dec 22, 2005 · N826AX · Doug DC863F · Fuselage Main, FrameSDR ABXA050379Transmitter · defectiveNR 3 ENGINE OIL PRESSURE WAS 37 TO 39 PSI IN CRUISE. RETARDED THROTTLE TO IDLE TO COMPLY WITH ABNORMAL PROCEDURES, OIL PRESSURE WAS 35 PSI. OIL PRESSURE DROPPED TO 34 PSI, SECURED NR 3 ENGINE AT 0850 HRS - 10 PSI WINDMILLING OIL PRESSURE. 0855 HRS OIL PRESSUREDec 21, 2005 · N816AX · Doug DC863F · Engine Oil Indicating SystemSDR ARWA20051202Actuator · leakingLOG PAGE NR 116558. ON POST FLIGHT FOUND LEAKING BY EMPANAGE LOWER SIDE REAR STRIKE PAD REAR ACCESS PANEL. REMOVED AND REPLACED RUDDER PACK ACTUATOR IAW MM 27-21-6. LEAK CHECK AND OPERATIONAL CHECK IAW MM 27-20-0 FOUND NORMAL, NO LEAKS NOTICE.Dec 20, 2005 · N441J · Doug DC863F · Rudder ActuatorSDR ABXA060029Support Bracket · corrodedAFT CARGO COMPARTMENT, TORQUE BOX FORWARD SIDE AT STA 1160, BETWEEN LONGERON 31 RIGHT & 32 RIGHT, ANGLE AND WEB HAD CORROSION. REMOVED CORROSION, TREATED AND PRIMED. FABRICATED NEW SUPPORT BRACKET, FOUND TO BE OUT OF LIMITS. WORK ACCOMPLISHED IAW REA D853-5Dec 15, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA060032Floorbeam · corrodedUPPER HORIZONTAL CAP OF FLOORBEAM CORRODED AT STA 920, LEFT BUTT LINE 10. REMOVED CORROSION. DAMAGE OUT OF LIMITS. FLOORBEAM REPAIRED IAW REA D853-52567.Dec 14, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor BeamSDR ABXA060037Intercostal · corrodedUPPER CARGO, STA 30, LEFT BUTT LINE 48, INTERCOSTAL HAD CORROSION JUST AFT OF MAIN CARGO DOOR CONTROL BOX. REMOVED CORROSION ON INTERCOSTAL BEAM AT STA 30, LEFT BUTT LINE 48, AND DETERMINED AREA WAS OUT OF LIMITS. FABRICATED DOUBLER, TREATED, PRIMED AND INSTDec 7, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA060021Frame · corrodedSTA. 1100, LONGERON 18 RT, FRAME CORRODED. REPAIRED FRAME AT STA. 1100, LONGERON 18 RT IAW SRM 53-2-0, FIGURE 2.Dec 2, 2005 · N826AX · Doug DC863F · Fuselage Main, FrameSDR ABXA060035Floorbeam · corrodedMAIN CABIN, STA 880, RIGHT BUTT LINE 63, FLOORBEAM LOWER CHORD, FORWARD SIDE CORRODED. REPAIRED FLOORBEAM STA 880, RIGHT BUTT LINE 63 IAW REA D853-52566MR.Nov 29, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor BeamSDR ABXA050293Longeron · corrodedCORROSION FOUND ON LONGERON 24 RIGHT AT STATION 879. REA D853-52752MR PERFORMS AN INTERIM REPAIR TO THE LONGERON.Nov 29, 2005 · N812AX · Doug DC863F · Fuselage Main, Longeron/StringerSDR ABXA050292Skin · corrodedCORROSION FOUND ON THE WING TO FUSELAGE SKIN AT STATION 670 AND LONGERON 36. REA D853-52756MR PERFORMS AN INTERIM REPAIR SIMILAR TO SRM 53-2-1, FIG. 7, AS OPERATIONAL SCHEDULING DID NOT ALLOW FOR A PERMANENT REPAIR.Nov 29, 2005 · N812AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA050354Stiffener · corrodedDURING REMOVAL OF LEFT LONGERON, STIFFENER AT STA 940, LONGERON 24 LEFT, LEFT WHEEL WELL, WAS FOUND CRACKED ON BOTTOM OF BASE. FABRICATED NEW STIFFENER FOR STA 940, LONGERON 24 LEFT IAW REA D853-52556, PO NR 1123110.Nov 27, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA050289Window · lack of lubeCAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. LUBRICATED CAPTAIN'S CLEARVIEW WINDOW ASSEMBLY IAW DC-8 MM 56-00-00. OPS CHECKED GOOD.Nov 21, 2005 · N812AX · Doug DC863F · Flight Compartment WindowsSDR ARWA20051102Blades · damagedUPON ENGINE SPOOL UP FOR TAKEOFF, NR 4 ENGINE COMPRESSOR STALLED. PERFORMED BOROSCOPE TO NR 4 ENGINE; FOUND BLADES DAMAGED, SECURED NR 4 ENGINE FOR FERRY FLIGHT IN ACCORDANCE WITH ARROW GMM 6-3-4/5.Nov 17, 2005 · N661AV · Doug DC863F · Turbine Engine Compressor SectionSDR ABXA050367Access Panel · leaking12 BLIND RIVETS LEAKING UPON PRESSURE CHECKS. RIGHT WING, STRINGER NR 7 NEAR ACCESS PANEL 505F. REMOVED 12 BLIND FASTENERS ON STRINGER NR 7 NEAR ACCESS PANEL 505F OF THE RIGHT WING AND WET INSTALLED NEW FASTENERS IAW DC8 SRM 51-1-21 USING 1422 B1/2 SEALANT.Nov 16, 2005 · N826AX · Doug DC863F · Wing, Plate/SkinSDR ABXA050368Access Panel · leaking16 BLIND RIVETS LEAKING UPON PRESSURE CHECKS. RIGHT WING, STRINGER NR 5 NEAR ACCESS PANEL 505F. REMOVED 16 BLIND FASTENERS ON STRINGER NR 5 NEAR ACCESS PANEL 505F OF THE RIGHT WING AND WET INSTALLED NEW FASTENERS IAW DC8 SRM 51-1-21 USING 1422 B1/2 SEALANT.Nov 16, 2005 · N826AX · Doug DC863F · Wing, Plate/SkinSDR ABXA050308Floorbeam · corrodedMAIN CABIN, STA 798, BUTT LINE 0 - RT BUTT LINE 48, FLOORBEAM CORRODED. REMOVED NUT PLATES, CLEANED CORROSION ON FLOORBEAM AT STA 798, BUTT LINE 0 - RT BUTT LINE 48, BLENDED AREA, OUT OF LIMITS AT .088 INCH MATERIAL REMAINING FROM ORIGINAL THICKNESS OF .186 INov 11, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor BeamSDR ARWA20051101Control Cable · damagedDURING PRE-FLIGHT, FOUND RUDDER POWER LEVER STIFF; "RUDDER CONTROL MANUAL" LIGHT REMAINS ILLUMINATED WITH LEVER IN "ON" POSITION. REMOVED AND REPLACED RUDDER SHUT-OFF VALVE CONTROL CABLE RUN NR 67-C IN ACCORDANCE WITH DC8 M/M 27-22-1; RIGGED AND OPERATIONAL CNov 11, 2005 · N661AV · Doug DC863F · Rudder Control SystemSDR ABXA060036Floor Support · crackedFLOOR SUPPORT HAT CHANNEL AT APPROXIMATELY LEFT BUTT LINE 34 BETWEEN STA 25 AND STA 35 WAS CRACKED AND HOLES DAMAGED. REMOVED DAMAGED HAT CHANNEL AND SHIM FROM STA 25 - 35, LEFT BUTT LINE 34. DAMAGE BEYOND REPAIRABLE LIMITS. FABRICATED NEW HAT CHANNEL AND SNov 9, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA050307Web · corrodedCENTERLINE WEB AT STA 800 - 857, BUTT LINE O CORRODED. FABRICATED WEB AT STA 800 - 857, BUTT LINE 0 IAW REA D853-52543. MATERIAL USED .080 7075-T6, P/O NR 1113384.Nov 9, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA050309Tripler · corrodedEXISTING TRIPLER CORRODED AT STA 857, RT BUTT LINE 50. FABRICATED TRIPLER AT STA 857, RT BUTT LINE 50 IAW REA D853-52539. MATERIAL USED .190 7075-T6, P/O NR 1073367.Nov 8, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA050306Angle · corrodedLOWER CHORD AT STA 857, RT BUTT LINE 23 CORRODED. FABRICATED CHORD AT STA 857, RT BUTT LINE 23 IAW REA D853-52537. MATERIAL USED P/N: AND-10134-1407, P/O NR1122772.Nov 7, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA050301Web · corrodedWEB CORRODED AT STA 857, LT BUTT LINE 46. FABRICATED WEB AT STA 857, LT BUTT LINE 46 USING .063 7075-T6, PO NR 1118787 IAW REA D853-52535.Nov 7, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA050304Attach Angle · corrodedRT PRESSURE PANEL AT STA 857, RT BUTT LINE 40 ATTACH ANGLE CORRODED. FABRICATED ATTACH ANGLE RT PRESSURE PANEL AT STA 857, P/N: 5644678 IAW REA D853-52534.Nov 7, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA050303Web · corrodedWEB CORRODED AT STA 857, RT BUTT LINE 46. FABRICATED WEB AT STA 857, RT BUTT LINE 46 USING .071 7075-T6, P/O NR 1084025 IAW REA D853-52538.Nov 7, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA050302Splice · corrodedSHIM SPLICE CORRODED AT STA 857, LEFT BUTT LINE 20. FABRICATED SHIM AT STA 857, LEFT BUTT LINE 20 IAW DC8 REA D853-52536. MATERIAL USED .090 P/O NR 1112038.Nov 7, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA050305Web · corrodedPSI WEB FROM STA 847, LEFT BUTT LINE 40 - 60 CORRODED. FABRICATED PSI WEB FROM STA 847, LEFT BUTT LINE 40 - 60 IAW DC8 REA D853-52534. MATERIAL USED .063 2024-T3, P/O NR 1118786.Nov 7, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA050300Doubler · corrodedCORROSION ON TOP OF LONGERON REINFORCEMENT DOUBLER IN AFT CARGO BILGE AT STA 1180, LONGERON 36 TO 34 RIGHT. REMOVED DOUBLER AT STA 1200 LONGERON 34 RIGHT TO 36. REMOVED CORROSION FROM DOUBLER. FOUND TO BE OUT OF LIMITS. FABRICATED, TREATED, PRIMED AND INSTNov 4, 2005 · N826AX · Doug DC863F · Fuselage Main, Longeron/StringerSDR U2RA0809Transformer · brokenPILOTS OVERHEAD PANEL LIGHTS INOP, GLOW FUSE ON FOLLOWED BY SMOKE.Nov 4, 2005 · N865F · Doug DC863F · Flight Compartment LightingSDR ABXA050346Floorbeam · corrodedFOUND MAIN CABIN FLOORBEAM AT STA 120, RIGHT BUTT LINE 51, FORWARD SIDE OF T CAP, CORRODED. REMOVED DAMAGED AREA AND REPLACED WITH ANGLE DOUBLER REPAIR ON FLOORBEAM STA 120, RIGHT BUTT LINE 51 IAW DC8 SRM 51-1-8, 53-2-0, 51-3-0, 53-7-3, 53-0, 51-2-0, 51-1-8, Nov 2, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor BeamSDR ABXA050294Finger Doubler · damagedINSIDE CENTER TANK, STA 857, LT BUTT LINE 20, AFT FINGER TAB OF DOUBLER BROKEN OFF. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW REA D853-52530.Nov 2, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA060028Floorbeam · corrodedMAIN CARGO, STA 55, LEFT BUTT LINE 20, CORROSION ON UPPER FLANGE FLOORBEAM. REMOVED 3.5 X .75 INCH SECTION OF UPPER FLANGE FLOORBEAM. ACCOMPLISHED FLOORBEAM REPAIR IAW SSRM DWG K04881.Nov 1, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor BeamSDR ABXA060019Floorbeam · corrodedMAIN CARGO, STA. 55, LBL 20, CORROSION ON UNDERSIDE OF FLOORBEAM CORNER. REMOVED A 3.5 INCH X .7500 INCH SECTION OF UPPER FLANGE FLOORBEAM AT STA. 55, LBL 20 IAW SRM DWG K04881. FABRICATED REPAIR ANGLE, SHIM AND FILLER IAW SRM DWG K04881.Nov 1, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor BeamSDR ABXA050313Doubler · corrodedDOUBLER CORRODED TOP OF WING CENTER SECTION PRESSURE DECK, STA 683, LONGERON 22 LEFT, LEFT BUTT LINE 10. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 51-1-8 AND REA D853-52529.Nov 1, 2005 · N826AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA050299Doubler · corrodedDOUBLER CORRODED TOP OF WING CENTER SECTION PRESSURE DECK, STA. 683, RT BUTT LINE 10. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-1-8 AND REA D853-52529.Nov 1, 2005 · N826AX · Doug DC863F · Wing, Center BoxSDR ABXA050342Skin · misdrilledFOUND UPPER CARGO STA 857, LEFT BUTT LINE 60 - RIGHT BUTT LINE 60, 5 FASTENERS MIS-DRILLED IN TOP OF CENTER TANK TO SPAR SKIN. REAMED HOLES TO REMOVE DAMAGE, FABRICATED REPAIR BUSHINGS FOR 11 HOLES. INSTALLED REPAIR BUSHINGS WITH WET SEALANT IN HOLES. CONTOOct 31, 2005 · N826AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA050343Skin · misdrilledFOUND UPPER CARGO STA 834, BUTT LINE 0, 4 FASTENERS MIS-DRILLED IN TOP OF CENTER WING SKIN ON TANK. MIS-DRILLED HOLES CLEANED UP, HOLES OPENED UP TO 0.312" AND 0.308", FASTENERS INSTALLED IAW DC8 SRM 51-1-20 ON SPLICE DOUBLER INSTALLATION.Oct 31, 2005 · N826AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA050358Pressure Panel · corrodedCORROSION FOUND UNDER THREE FASTENERS ON PRESSURE WEB IN RT WHEEL WELL, STA. 857, RT BUTT LINE 27. CORROSION FOUND TO BE OUT OF LIMITS ON PRESSURE WEB IN RT WHEEL WELL, STA. 857, RT BUTT LINE 27 IAW SRM 51-1-8 AND 53-2-0. FABRICATED AND INSTALLED REPAIR IAW ROct 30, 2005 · N826AX · Doug DC863F · Fuselage Main, BulkheadSDR ABXA060020Floorbeam · corrodedMAIN CABIN, STA. 857, LBL 12, FLOORBEAM UPPER CAP CORRODED. REMOVED CORROSION ON FLOORBEAM STA. 857, LBL 12. MATERIAL LOSS OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM DWG K04881.Oct 26, 2005 · N826AX · Doug DC863F · Fuselage Main, Floor BeamSDR ABXA050345Doubler · corrodedCORROSION ON TOP OF LONGERON REINFORCEMENT DOUBLER IN AFT CARGO BILGE AT STA 1180, LONGERON 35 RIGHT. REMOVED CORROSION AT STA 1180, LONGERON 35 RIGHT. FOUND TO BE OUT OF LIMITS. FABRICATED, TREATED, PRIMED AND INSTALLED NEW DOUBLER FROM 7075-T6, 0.125", PO Oct 26, 2005 · N826AX · Doug DC863F · Fuselage Main, StructureSDR ABXA050310Longeron · corrodedCORROSION FOUND ON STR 31 L (LONGERON) FROM STA. 610 - 730 IN MID ACCESSORY COMPARTMENT. REMOVED AND REPLACED LONGERON 31 LT FROM STA. 610-730 REF SRM 51-1-20 AND DPS 3.67-22.Oct 26, 2005 · N826AX · Doug DC863F · Fuselage Main, Longeron/StringerSDR ABXA050355Shear Tie · crackedFOUND SHEAR TIE CRACKED AT STA 440, LONGERON 31 RIGHT (REF. NRC HY-275). REMOVED AREA STRUCTURE FOR ACCESS, REMOVED DAMAGED AREA OF FORMER SECTION/SHEAR TIE, LONGERON 30 RIGHT AND LONGERON 31 RIGHT, STA 440. FABRICATED REPAIR PARTS: 1 FORMER SECTION FROM 0.07Oct 25, 2005 · N826AX · Doug DC863F · Fuselage Internal Mounting StructureSDR ABXA050353Bulkhead · corrodedFOUND CORROSION ON RIGHT WHEEL WELL, STA 980, LONGERON 24 RIGHT, AFT BULKHEAD UNDER LOWER SIDE OF DIAGONAL FRAME. REMOVED BRACKET AT STA 980 IAW DC8 SRM 51-3-0, 51-1-S0D. REMOVED CORROSION IAW DC8 SRM 53-2-0. ORIGINAL MATERIAL MEASURED .047" AND .046", OUT Oct 25, 2005 · N826AX · Doug DC863F · Fuselage Main, BulkheadSDR ABXA050344Attach Fitting · crackedFOUND CORNER FITTING OF CENTER WING BOX UPPER SURFACE AT STA 680, RIGHT BUTT LINE 62 WAS CRACKED. REMOVED CRACKED FITTING AT CENTER WING BOX UPPER SURFACE STA 680, RIGHT BUTT LINE 62 IAW DC8 SRM 51-1-20D AND SRM 51-3-1, DRILLED, REAMED AND COUNTERSUNK CORNER Oct 25, 2005 · N826AX · Doug DC863F · Fuselage Main, Attach FittingsSDR ABXA050295Keelbeam · corrodedKEEL BEAM CORRODED AT AFT BULKHEAD OF MID ACCESSORY COMPARTMENT, STA 680, BUTT LINE 0, CORROSION APPEARED TO EXTEND UNDER WING CENTER SECTION. REMOVED CORROSION AT KEEL BEAM STA 620 FWD OF BULKHEAD AND UNDER BULKHEAD AS REQUIRED REF SRM 51-1-8, REF REA D853-Oct 25, 2005 · N826AX · Doug DC863F · Fuselage Main, Keel
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