Douglas DC-8-73F

Service difficulty reports · 15,471

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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 = 'DC873F'
  ORDER BY difficulty_date DESC"

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SDR DHL2002806839Skin · corrodedREMOVED CORROSION FROM RT WING OUTBOARD L/E UPPER SURFACE IAW SRM 51-1-8 PG 17-18, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. CUT OUT DAMAGED AREA IAW SRM 57-2-1 PG 2 FIG 38. FABRICATED AND INSTALLED FILLER & DOUBLER IAW SRM 57-2-1 PG 2 FIG 38, SRM 51-1-21 PGJul 3, 2002 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2002806532Skin · corrodedRT WING OUTBOARD LEADING EDGE UPPER SURFACE SKIN CORRODED XFS 566.000 TO XFS 660.000. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16 ,CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER IAW SRM 57-2-1 PG 2 FIG 38.Jul 3, 2002 · N806DH · Doug DC873F · Wing, Plate/SkinSDR UPS02838902Fitting · corrodedINSPECTION TYPE:C2 MAIN CABIN LONG 32R END FITTING CORRODED AT FS 1760. REMOVED CORRODED FITTING IAW DC8 SRM 51-1-21, LOCATED DRILLED DEBURRED NEW FITTING IAW 53-2-0, INSTALLED FITTING IAW DC8 SRM 51-1-21 & 51-1-20D, 51-1-17.Jul 3, 2002 · N802UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2002806508Skin · crackedFOUND AT C-CHECK RT ELEVATOR T/E SKIN HAS A .5 INCH CRACK AT STA XE 136.000. STOP DRILLED CRACK PER SRM 55-2-0 FIG 2. FABRICATED DOUBLER PER SRM 55-2-0 FIG 2. INSTALLED DOUBLER PER SRM 55-2-0 FIG 2.Jul 2, 2002 · N806DH · Doug DC873F · Elevator, Plate/SkinSDR UPS02838911Skin · corrodedINSPECTION TYPE:C2 AIR COND PRESS COMPT AT FS 56 BETWEEN L32R - 34R BETWEEN, UNDER AND AROUND SHEAR TIE SKIN IS CORRODED. REMOVED CORROSION FROM FUSELAGE SKIN, FAB NEW SECTION OF INNER DOUBLER, FAB SPLICE PLATE DOUBLER IAW DC8 53-2-0, INSTALLED INNER DOUBLER Jul 2, 2002 · N802UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS02838901Seat Track · wornINSPECTION TYPE:C2 CABIN STA 70 SEAT TRACK-E IS WORN. BLEND GOUGE IAW SRM 53-2-0 FIG 14. FOUND OUT OF LIMITS IAW 53-2-3. REMOVED DAMAGED SECTION AND FABBED NEW SEAT TRACK IAW DC8 SRM 53-2-3. INSTALLED NEW SEAT TRACK IAW DC8 SRM 53-2-3.Jul 2, 2002 · N802UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS02838900Seat Track · damagedINSPECTION TYPE:C2 ACP SRM REPAIR TO SEAT TRACK AT POS 2L/3L SUPERLOCK INSTALLED IAW EO M-2550-4101. CUT OUT DAMAGED SEAT TRACK SECTION, FABBED AND DRILLED NEW SEAT TRACK SECTION AND 2 SPLICES IAW DC8 SRM 53-2-3. INSTALLED NEW SEAT TRACK SECTION, SPLICES IAWJul 2, 2002 · N802UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2002806838Skin · corrodedRT WING CENTER LEADING EDGE UPPER SURFACE SKIN SHOWS CORROSION XFS 304.000 - 335.250. REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. CUT CORRODED AREA IAW SRM 57-2-1 PG 2 FIG 38. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-21-1 PG 2 Jul 1, 2002 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2002806513Skin · crackedFOUND AT C-CHECK, LT INBOARD SLOT L/E INTERNAL SKIN CRACKED 4 INCHES AT STA XFS 250.000. PERFORMED MAJOR REPAIR PER SRM 57-3-3 PG 9-11. REMOVED DAMAGED SKIN PER SRM 51-1-21 PG 1. FABRICATED NEW SKIN PER SRM 57-3-3 PG 9-11. INSTALLED NEW INTERNAL SKIN PER SJul 1, 2002 · N806DH · Doug DC873F · Leading Edge DevicesSDR DHL2002806530Doubler · damagedFOUND DURING C-CHECK, FUSELAGE EXTERIOR OVERLAP REPAIR DOUBLER EDGE GAUGED AND DENTED AT STA 1440.000 L-31R AFT CARGO DOOR FRAME. REMOVED DAMAGED REPAIR DOUBLER. FABRICATED AND INSTALLED DOUBLER PER EO DHL 020618, EO3108, EO SEMAN 2002722.Jun 30, 2002 · N806DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2002806506Former · crackedDURING C-CHECK FOUND RT WING CTR L/E LOWER FORMER 1 INCH CRACK STA XFS 329.000. STOP DRILLED CRACK PER SRM 57-2-0 FIG 2. FABRICATED DOUBLER PER SRM 57-2-0 FIG 2. INSTALLED DOUBLER PER SRM 57-2-0 FIG 2.Jun 30, 2002 · N806DH · Doug DC873F · Wing Main, Frame StructureSDR DHL2002806500Skin · damagedDURING C-CHECK FOUND FUSELAGE EXTERIOR, AFT CARGO COMPARTMENT DOOR JAMB SHOWS DAMAGED SKIN REPAIR STA FS 1400.000 AND L-31R. FABRICATED A NEW REPAIR DOUBLER PER EO DHL 020619, EO 3109, EO SEMAN 2002723. INSTALLED NEW DOUBLER PER EODHL020619, EO 3109, EO SEMAJun 30, 2002 · N806DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2002806524Former · crackedAT C-CHECK, FOUND RT WING CTR L/E FORMER 1 INCH CRACK STA XFS 310.250. STOP DRILLED CRACK PER SRM 57-2-0 FIG 2. FABRICATED AND INSTALLED DOUBLER PER SRM 57-2-0 FIG 2.Jun 30, 2002 · N806DH · Doug DC873F · Wing Main, Frame StructureSDR DHL2002806521Former · crackedFOUND DURING C-CHECK, RT WING CTR L/E LWR FORMER 1 INCH CRACK STA XFS347.750. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10. INSTALLED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10.Jun 30, 2002 · N806DH · Doug DC873F · Wing Main, Frame StructureSDR DHL2002806520Skin · crackedFOUND DURING C-CHECK, RT WING O/B LEADING EDGE LWR SURFACE .375 INCH CRACK STA XFS 597.000. STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER PER EO DHL020608, DWG EO3104 EO SEMAN2002693.Jun 30, 2002 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2002806525Former · crackedDURING C-CHECK, FOUND RT WING O/B LEADING EDGE UPPER PART FORMER CRACKED .5 INCH AT STA XFS 697.500. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED AND INSTALLED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10 AND SRM 51-1-21 PG 7.Jun 29, 2002 · N806DH · Doug DC873F · Wing Main, Frame StructureSDR DHL2002806507Former · crackedDURING C-CHECK FOUND RT WING O/B LEADING EDGE UPPER PART FORMER CRACKED 1 INCH AT XFS 603.750. STOP DRILLED CRACK PER SRM 57-2-0 FIG 2. FABRICATED DOUBLER PER SRM 57-2-0 FIG 2. INSTALLED NEW DOUBLER PER SRM 57-2-0 FIG 2.Jun 29, 2002 · N806DH · Doug DC873F · Wing Main, Frame StructureSDR DHL2002806523Former · crackedDURING C-CHECK, FOUND RT WING O/B LEADING EDGE UPPER PART FORMER CRACKED .25 INCH XFS 691.250. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED AND INSTALLED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10 AND SRM 51-1-21 PG 1.Jun 29, 2002 · N806DH · Doug DC873F · Wing Main, Frame StructureSDR DHL2002806522Former · crackedDURING C-CHECK, FOUND RT WING O/B LEADING EDGE UPPER PART FORMER CRACKED .5 INCH XFS 622.500. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED AND INSTALLED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10 AND SRM 51-1-21 PG 1.Jun 29, 2002 · N806DH · Doug DC873F · Wing Main, Frame StructureSDR DHL2002806528Rib · crackedAT C-CHECK, FOUND LT WING I/B JOINT FLAP LINK RIB SHOWS 4 CRACKS 1 INCH XW 138.000. REMOVED CRACKED RIB PER SRM 51-1-21 PAGE 1. FABRICATED AND INSTALLED PER ATM 00111590, DWG 5652796, EA SEMAN 2002729, SRM 57-7-1 PG 6 AND SRM 51-1-21 PG 1.Jun 28, 2002 · N806DH · Doug DC873F · Trailing Edge FlapsSDR DHL2002807009Connector · looseDOOR NOT LATCHED LIGHT ILLUMINATED AFTER GEAR RETRACTION. PERFORMED ABNORMAL, CYCLED 4 TIMES AND NO EFFECTS. CONTINUED FLIGHT WITH 230 KIAS/ .65M LIMITATION. FOUND LIGHT SOCKET CONNECTIONS LOOSE. CLEANED AND SECURED CONNECTION. RELAMPED, PERFORMED GEAR SWJun 28, 2002 · N807DH · Doug DC873F · Landing Gear Position and WarningSDR DHL2002806516Former · crackedDURING C-CHECK, FOUND RT WING O/B LEADING EDGE UPPER PART FORMER CRACKED .625 INCH AT XFS 641.250. STOP DRILLED CRACK PER SRM 57-2-0 PG 9. FABRICATED REINFORCING ANGLE PER SRM 57-2-0 PG 9-10. INSTALLED NEW ANGLE AND FASTENERS PER SRM 57-2-0 PG 9-10 AND SRM Jun 27, 2002 · N806DH · Doug DC873F · Wing Main, Frame StructureSDR DHL2002806526Intercostal · crackedFOUND AT C-CHECK, D BELLY DOOR INTERCOSTAL THAT SUPPORTS HINGES SHOWS DOUBLER CRACKED .5 INCH. REMOVED CRACKED DOUBLER PER SRM 53-2-0. FABRICATED AND INSTALLED NEW DOUBLER PER SRM 53-2-0 FIG 1B.Jun 27, 2002 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2002806519Structure · damagedDURING C-CHECK, FOUND LT WING I/B SLOT UPPER SURFACE SKIN HOLES ELONGATED XS 250.000. CUT OUT DAMAGED AREA. FABRICATED DOUBLERS AND FILLER PER EODHL020606, EO-3088, EO SEMAN2002671. INSTALLED FILLERS AND DOUBLERS PER EODHL020606, EO-3088, EO SEMAN2002671.Jun 27, 2002 · N806DH · Doug DC873F · Leading Edge DevicesSDR UPS02838909Fitting · crackedINSPECTION TYPE:C2 L17R END FITTING CRACKED AT FS 1769. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-21.Jun 27, 2002 · N802UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS02838908Fitting · crackedINSPECTION TYPE:C2 L17L END FITTING CRACKED FS 1769. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-21.Jun 27, 2002 · N802UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS02838768Angle · corrodedINSPECTION TYPE:C2 C PIT DOOR JAMB T-ANGLE HAS CORROSION FROM STA 1250 L33R. REMOVED CORRODED T-ANGLE, LOCATED & DRILLED NEW ANGLE IAW DC8 SRM 51-1-24. INSTALLED NEW T-ANGLE IAW DC8 SRM 51-1-20D.Jun 27, 2002 · N802UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS02838709Light · inoperativeINSPECTION TYPE:N/A, 1 BULB INOP CREW ENTRY EMERGENCY LIGHT. RELAMPED AS REQUIRED.Jun 27, 2002 · N805UP · Doug DC873F · Emergency LightingSDR DHL2002807008Striker · defectiveGEAR DOOR LIGHT ILLUMINATED AFTER GEAR RETRACTION, CYCLED GEAR SEVERAL TIMES PER ABNORMAL PROCEDURES. LIGHT STAYED ILLUMINATED. MAIN GEAR DOOR LIGHT SWITCH NEXT TO F/E'S PANEL HAD NO EFFECT ON DETERMINING WHICH DOOR. REPLACED LT GEAR DOOR STRIKER AND PERFORJun 27, 2002 · N807DH · Doug DC873F · Landing Gear Position and WarningSDR DHL2002806529Door Frame · crackedDURING C-CHECK, FOUND .5 INCH CRACK IN NR 3 CROSS SLIDE DOOR INNER EDGE. STOP DRILLED CRACK PER SRM 53-2-0 FIG 1B. FABRICATED DOUBLER PER SRM 51-1-8B FIG 1B. INSTALLED DOUBLER PER SRM 53-2-0 FIG 7B.Jun 26, 2002 · N806DH · Doug DC873F · Fuselage Main, StructureSDR DHL2002806527Skin · dentedDURING C-CHECK, FOUND RT ELEVATOR UPPER SKIN WITH SEVERAL DENTS STA XE 132.750 TO 242.187. REMOVED DETERIORATED SKIN. FABRICATED AND INSTALLED NEW SKIN PER EO DHL020602 DWG EO 3084 EO SEMAN 2002687.Jun 26, 2002 · N806DH · Doug DC873F · Elevator, Plate/SkinSDR DHL2002806515Fitting · crackedDURING C-CHECK, FOUND MAIN CARGO COMPARTMENT FLOOR PANEL CENTER TRACK FITTING CRACKED STA 200.000. REMOVED CRACKED FITTING PER SRM 51-1-20D PG 21. INSTALLED NEW FITTING PER SRM 51-1-20D PG 9.Jun 26, 2002 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2002806514Structure · damagedDURING C-CHECK, FOUND RT INBOARD SLOT WITH ELONGATED HOLES AT STA XFS 250.000. TRIMMED OUT DAMAGED AREA. FABRICATED DOUBLERS AND A FILLER PER EODHL020620, EO3093, EO SEMAN 2002682. INSTALLED FILLER AND DOUBLER PER EODHL020620, EO3093, EO SEMAN 2002682.Jun 26, 2002 · N806DH · Doug DC873F · Leading Edge DevicesSDR DHL2002806510Panel · delaminatedDURING C-CHECK FOUND RT WING T/E UPPER PANEL SKIN DELAMINATED STA XA 681.000-613.000. REMOVED AND REPLACED PANEL PER SRM 51-3-0 PG 1.Jun 26, 2002 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2002806503PanelDURING C CHECK FOUND L/H WING T/E LWR PANEL EXTERNAL SKIN DELAMINATED BETWEEN XF 339.000 TO XF 409.000.REMOVED AND REPLACED DELAMINATED PANEL PER SRM 51-1-21 PG 7.Jun 26, 2002 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2002806502PanelDURING C CHECK FOUND R/H WING LWR PANEL EXTERNAL SKIN DELAMINATED (STA XF 339.000-409.000)REMOVED AND REPLACED EXTERNAL SKIN PANSL PER SRM 52-3-0 PG 1.Jun 26, 2002 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2002806518Skin · damagedDURING C-CHECK, FOUND RT WING T/E UPPER SKIN DEFECT XW 761.695. REMOVED DAMAGED SKIN PANEL. FABRICATED AND INSTALLED NEW SKIN PANEL PER EODHL 020601, EO3082, EO SEMAN2002679.Jun 26, 2002 · N806DH · Doug DC873F · Wing, Plate/SkinSDR UPS02838910Fitting · crackedINSPECTION TYPE:C2 TAIL CONE ATTACH FITTING HAS CRACK AT L10L. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-21.Jun 26, 2002 · N802UP · Doug DC873F · Aerodynamic FairingsSDR UPS02838903Frame · corrodedINSPECTION TYPE:C2 MAIN CABIN FRAME CORRODED AT FS 1740 BETWEEN L33L TO L33R. REMOVED DAMAGED SECTION OF FRAME AND SPLICED IN NEW SECTION IAW DC8 SRM 53-2-0.Jun 26, 2002 · N802UP · Doug DC873F · Fuselage Main, FrameSDR UPS02838880Fitting · crackedINSPECTION TYPE:C2 MAIN CABIN LONGERON END FITTING CRACKED AT FS 1690 L26RT. REMOVED FITTING, CLEANED, ALODINED & PRIMED IAW DC8 SRM 51-1-8. LOCATED, DRILLED & DEBURRED NEW FITTING IAW DC8 SRM 51-3-2. INSTALLED FITTING IAW DC8 SRM 51-1-21, 51-1-20D & 51-1-Jun 26, 2002 · N802UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS02838774Fitting · crackedINSPECTION TYPE:C2 C3 CROSS SLIDE DOOR JAMB HAS CRACKED BANANA FITTING AT STA 1260 LONGERON L33R. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.Jun 26, 2002 · N802UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS02838772Fitting · corrodedINSPECTION TYPE:C2 C3 CROSS SLIDE DOOR LWR T-BOLT BACK UP FITTING CORRODED AT STA 1242. REMOVED CORRODED FITTING LOCATED, DRILLED UP MODIFIED FITTING AND CLIPS IAW DC8 SRM 53-2-0 FIG 2D. INSTALLED FITTING AND 2 CLIPS IAW DC8 SRM 53-2-0 FIG 2D & 51-1-20D.Jun 26, 2002 · N802UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS02838707Battery Pack · not seatedINSPECTION TYPE:N/A, EMERGENCY LIGHT REMAIN ON AND CANNOT BE EXTINGUISHED. RESET EMERGENCY LIGHTS BATTERY PACK, OPS CHECKS GOOD.Jun 26, 2002 · N852UP · Doug DC873F · Emergency LightingSDR DHL2002806512Skin · delaminatedFOUND DURING C-CHECK, LT WING MLG DOOR LWR SKIN DELAMINATED. REMOVED OUTER DOOR FROM MLG PER SRM 51-3-0 PG 1. INSTALLED NEW OUTER DOOR ON MLG PER SRM 51-3-0 PG 1 AND SRM 51-3-1 PG 1.Jun 25, 2002 · N806DH · Doug DC873F · Landing Gear DoorsSDR DHL2002806501Panel · delaminatedDURING C CHECK FOUND R/H WING T/E LWR PANEL DELAMINATED.REMOVED AND REPLACED R/H WING LWR PANEL FROM STA XF219.000-339.000, PER SRM 51-3-0 PAGE 4.Jun 25, 2002 · N806DH · Doug DC873F · Wing, Plate/SkinSDR UPS02838907Fitting · crackedINSPECTION TYPE:C2 AFT PIT STA 1220 AT L27L Z-FITTING CRACK. REMOVED FITTING, FABBED REPAIR ANGLES, LOCATED DRILLED ANGLES & FITTINGS IAW DC8 SRM 53-2-0 FIG 20. INSTALLED FITTING ANGLES IAW DC8 SRM 53-2-0 FIG 20.Jun 25, 2002 · N802UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS02838906Fitting · corrodedINSPECTION TYPE:C2 AFT PIT AFT SIDE OF Z-FITTING CORRODED AT PREV GROUND AREA. REMOVED CORRODED Z-FITTING, LOCATED DRILLED NEW FITTING AND FABBED 2 SPLICE REPAIR ANGLES. INSTALLED NEW FITTING AND SPLICE REPAIR ANGLES IAW DC8 SRM 53-2-0 FIG 2D & 51-1-20D.Jun 25, 2002 · N802UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS02838905Clip · crackedINSPECTION TYPE:C2 AFT SIDE OF FS 683 WEB LWR CHORD CRACKED BETWEEN LONGERON 30L AND 32L LOCATED BETWEEN WING CENTER SECTION LWR SURFACE AND FUSELAGE LWR LOBE VIEWED THROUGH REMOVED STRESS PNLS. REMOVED 1 CLIP STA 683 L30L AND 2 CLIP L30L & 31L RCD LOCATED ANJun 25, 2002 · N802UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS02838904Intercostal · corrodedINSPECTION TYPE:C2 AFT CARGO CORRODED INTERCOSTAL STR 35R AT LIGHTENING HOLE STA 1085. REMOVED CORRODED INTERCOSTAL IAW DC8 SRM 51-1-21, FABBED NEW INTERCOSTAL IAW DAC DWG 9758507, INSTALLED INTERCOSTAL IAW 51-1-21.Jun 25, 2002 · N802UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS02838879Longeron · crackedINSPECTION TYPE:C2 AT O/B SIDE OF LONG 24L STA 857 POSSIBLE CRACK ON LWR FLAT OF BATHTUB FITTING. NDT TO VERIFY REMOVED LONG 24 AND TRAP FITTING IAW DC8 SRM 51-1-20D. DRILLED LOCATED NEW LONG 24 IAW DC8 SRM 51-1-24. INSTALLED NEW LONGERON AND TRAP FITTING IJun 25, 2002 · N802UP · Doug DC873F · Fuselage Main, Longeron/Stringer
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