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 RRXA10948Structure · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT WING W/W TOP OF W/W O/B ABOVE AFT OF FLAP BUSS CABLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRApr 11, 2001 · N602AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA10947Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BATHTUB FITTING AT STA 1160 TO 1220 AND L34R TO L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND 53Apr 11, 2001 · N602AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA10946Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT WING LOWER T/E PANEL O/B OF FLAP HINGE 410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. NO DELAMINATION NOTED, NO ACTION REQUIRED.Apr 11, 2001 · N602AL · Doug DC873F · Wing, Plate/SkinSDR RRXA10945Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H WING O/B L/E UPPER SKIN AT XFS 703.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1, FIG 38.Apr 11, 2001 · N602AL · Doug DC873F · Wing, Plate/SkinSDR RRXA10944Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK BETWEEN LONBERON 28L AND 29L AT STA 1160, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 2D.Apr 11, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR RRXA10943Doubler · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE TEE DOUBLER LOWER LT WING AT STA XW 467, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DH SK 602-746 AND 8110-3.Apr 10, 2001 · N602AL · Doug DC873F · Wing, Plate/SkinSDR RRXA10942Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE L/H WING #1 SPOILER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1Apr 10, 2001 · N602AL · Doug DC873F · Drag Control SystemSDR RRXA10941Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LEFT WING O/B L/E SKIN BETWEEN STA'S XFS 578.75 TO 641.25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INApr 10, 2001 · N602AL · Doug DC873F · Wing, Plate/SkinSDR RRXA10940Cap · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE UNDER SKIN OF C-PIT ON BEAVER TAIL (KEEL CAP) AT STA 1080 L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRMApr 10, 2001 · N602AL · Doug DC873F · Fuselage Main, KeelSDR RRXA10939Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE R/H WING UPPER T/E PANEL AFT OF REAR SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-Apr 10, 2001 · N602AL · Doug DC873F · Wing, Plate/SkinSDR RRXA10938Retainer · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE C-PIT DOOR LOWER RETAINER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND DH SK602-787.Apr 10, 2001 · N602AL · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2001806636Angle · crackedC-CHECK - FUSELAGE - CUSP EXTRUSION - AFT DOOR FRAME JOINT ANGLE AT STA 1614.000 L-21 (LT) SHOWS CRACK OF 2 INCHES. REMOVED CRACKED ANGLE IAW SRM 51-1-20D PAGE 21. FABRICATED ANGLE IAW ATM 044210 A, EA 2001134, DWG 9750448. CLEANED, TREATED, AND PRIMED IAW Apr 10, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806631Angle · crackedC-CHECK - AFT CARGO COMPARTMENT SHROUD ASSY ANGLE CRACKED 8 INCHES. REMOVE CRACKED ANGLE IAW SRM 51-1-21 PAGE 1. CLEANED, TREATED, AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21 PAGE 1.Apr 10, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA11020Seat Track · wornDURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 146-156 AND LBL48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG14Apr 9, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR DHL2001806629Skin · crackedC-CHECK - RT AFT OVERWING EMERGENCY EXIT DOOR SKIN HAS 1 INCH CRACK AT RT FWD LWR CORNER. CUT OUT DAMAGED SKIN IAW DHL EO 010402, EO 2405, EO 2001124. CLEANED, TREATED, AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER (ALCLAD 7075 T6 0.071) IAW DHL EO 01Apr 9, 2001 · N806DH · Doug DC873F · Emergency ExitsSDR DHL2001806626Skin · dentedC-CHECK - LT ELEVATOR UPPER EXTERNAL SKIN SHOWS DENT AND DEFORMATION STA XE 0.00 - XE 132.00. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, REMOVED DAMAGED SKIN IAW EO DHL 010405, EO 2410, EO 2001099. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATEDApr 9, 2001 · N806DH · Doug DC873F · Elevator, Plate/SkinSDR DHL2001806621Angle · crackedC-CHECK - RT MLG W/W ANGLE LWR PART CRACKED 2 INCHES WITH STOP HOLE BETWEEN STA 920.000 TO STA 940.000 AND L-30R4. FABRICATED REINFORCEMENT ANGLE WITH ALCLAD (7075 T6 0.050) IAW SRM 53-2-0 FIG 1B. TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCEMENT Apr 9, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835760Fitting · corrodedINSPECTION TYPE:C2 AFT PIT AT FS 1160 L33R FITTING IS CORRODED ***CPCP*** REMOVED CORROSION AND FOUND TO BE OUT OF LIMIT REMOVE OLD FITTING INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D & 51-3-2Apr 9, 2001 · N805UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835759Fitting · corrodedINSPECTION TYPE:C2 AFT PIT AT FS 1220 L33R FITTING IS CORRODED ***CPCP*** REMOVED CORROSION IAW DC8 SRM 51-1-8 ORIGINAL THICKNESS 0.125 MINIMUM REMAINING THICKNESS IS 0.063 & FOUND TO BE OUT OF LIMITS RMVD CORROSION LOCATED & DRILL NEW FITTING IAW DC8 SRM Apr 9, 2001 · N805UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA10937Attach Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING CENTER L/E VERT. ATTACH ANGLE AT LOWER END AT STA XS 520, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAAW DC-8 SRM 51-1-20D AND DWG 9753297.Apr 8, 2001 · N602AL · Doug DC873F · Wing, Attach FittingsSDR RRXA10935Track · crackedDURING A MAINTENANCE VISIT FOUND A/C DOOR #12 FWD TRACK MISSING A PIECE OF METAL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-1-0, 51-1-21 AND DWG 5613836.Apr 8, 2001 · N602AL · Doug DC873F · Service DoorsSDR RRXA10936Clip · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H WING CENTER L/E O/B END ATTACH CLIP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0 AND DWG 5769928.Apr 8, 2001 · N602AL · Doug DC873F · Wing Miscellaneous StructureSDR RRXA10934Support · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT MLG W/W PRESSURE WEB SUPPORT ANGLE AT STA 860 LBL 55.0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D AND DWG 5645332.Apr 8, 2001 · N602AL · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806627Skin · dentedC-CHECK - LT ELEVATOR UPPER EXTERNAL SKIN DEFORMED AND DENTED FROM STA XE 210 TO XE 246. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, REMOVED DAMAGED SKIN IAW EO DHL 010403, EO 2408, EO 2001123. CLEANED, TREATED, AND REPAIRED AREA IAW SRM 51-1-8B. FABRICATED NApr 8, 2001 · N806DH · Doug DC873F · Elevator, Plate/SkinSDR DHL2001806624Skin · crackedC-CHECK - FUSELAGE NOSE SECTION EXTERNAL SKIN CRACKED 1 INCH AT FS -40 L-32R. REMOVED FASTENERS IAW SRM 51-3-0 PAGE 1, 2 SRM 51-1-20D PAGE 21. CUT DAMAGED SKIN IAW DHL EO 010330, EO 2406, EO 2001076. CLEANED, TREATED, AND PRIMED AREA IAW SRM 51-1-8B. FABRIApr 8, 2001 · N806DH · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA010031Indicator · faultyNR 4 ENGINE DURING SPOOL UP, N1 RPM INDICATOR HANGS UP BETWEEN 50 TO 70 PERCENT. REMOVED AND REPLACED NR 4 N1 INDICATOR IAW DC-8 MM CH 77-00. OPS CHECKS GOOD ON ENGINE RUN-UP.Apr 8, 2001 · N605AL · Doug DC873F · Engine RPM Indicating SystemSDR RRXA10933Finger Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FINGER DOUBLER AT STA 70 TO 80 AND L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PARApr 7, 2001 · N602AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA10932Seat Track · damagedDURING A MAINTENANCE VISIT FOUND BROKEN LUGS ON THE SEAT TRACK AT STA 1590 AND 1640 LBL 48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-3-0 AND 53-2-3, FIG 8A.Apr 7, 2001 · N602AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA10931Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LOWER FLANGE OF LONGERON AT FS 1255 L31L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PAApr 7, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR RRXA10930Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MAIN CARGO FLOOR PANEL FROM STA 580 TO 867 LBL 24 TO LBL 48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATApr 7, 2001 · N602AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA10929Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE FRAME ON THE R/H NOSE TUNNEL AT STA 67, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 23 AND 51-1-8.Apr 7, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR RRXA10928Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE STRAP ON THE L/H WING LOWER SKIN SIDE JUST INBD OF #1 PYLON AT STA XFS 430, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND 57-2-1, FApr 7, 2001 · N602AL · Doug DC873F · Wing, Plate/SkinSDR RRXA10927Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BATHTUB FITTING AT STA 1160 & 1180 AND L30L TO L31L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART ANApr 7, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR RRXA10925Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE FRAME ON THE R/H NOSE TUNNEL AT STA 58, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 23 AND 51-1-21.Apr 7, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR DHL2001804001Fire Loop · malfunctionedRECEIVED FIRE WARNING, ENGINE NR 2 DURING CRUISE. FOLLOWED PROCEDURE AND SECURED ENGINE. WARNING DID NOT REAPPEAR (ALL ENGINE INSTRUMENTS NORMAL DURING EVENT). R&R LEFT O/B FIRE BOTTLE AND DEFEARED B LOOP. STATUS-OPEN.Apr 7, 2001 · N804DH · Doug DC873F · Fire DetectionSDR RRXA10926Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE BATHTUB FITTING ON FWD SIDE OF STA 340 BETWEEN L34R-35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 2D AND 51-1-20D.Apr 6, 2001 · N602AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA10924Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE UNDER THE FUSELAGE SKIN B-PIT SCUFF PLATE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAWApr 6, 2001 · N602AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA10923Doubler · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERNAL DOUBLER LOWER SKIN L/H WING L/E AT STA XFS 304, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-1-21, 51-1-20D AND DWG 5641252.Apr 6, 2001 · N602AL · Doug DC873F · Wing, Plate/SkinSDR RRXA10922Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H CENTER L/E SLOT ANGLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-1-21 .Apr 6, 2001 · N602AL · Doug DC873F · Wing Main, Frame StructureSDR RRXA10921Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FITTING AT LONGERON 33L AT STA 8, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-Apr 6, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR RRXA10920Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE A-PIT DOOR FRAME LWR #5 LATCH FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAApr 6, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR RRXA10919Rib · chafedDURING A MAINTENANCE VISIT FOUND A HOLD CHAFFED THROUGH THE RIB ON THE LT L/E AT STA 5510, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.Apr 6, 2001 · N602AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA10918Frame · crackedDURING A MAINTENANCE VISIT FOUND DAMAGE TO THE FRAME ON THE R/H FWD SERVICE DOOR JAMB AFT AT STA 190 BETWEEN L10R-L11R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED AND INSTALLED PART IAW DC-8 SRM 53-2-0, FIG 2 AND 51-1-21.Apr 6, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR DHL2001806618Fitting · crackedC-CHECK - MAIN CARGO FLOOR PANELS CUSP EXTRUSION TO FRAME FITTING CRACKED 1 INCH STA 25.000 RT. REMOVED CRACKED FITTING. CLEANED, TREATED & PRIMED AREA AND INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 21, 9, SRM 51-1-8B.Apr 6, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806617Fitting · crackedC-CHECK - FWD CARGO COMPT. FITTING CRACKED 1/2 INCH AT STA 200 L26R. REMOVED CRACKED FITTING, CLEANED, TREATED AND PRIMED AREA AND INSTALLED NEW FITTING AT STA 200 L-26RH IAW SRM 51-3-0 PAGE 1, 2, SRM 51-1-8B.Apr 6, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001804002Servo · failedAUTO PILOT SERVO INDICATOR FOR ELEV ERRATIC IN SMOOTH FLIGHT. R&R ELEVATOR SERVO. CHECKED NORMAL IAW 22-10-00 ON GND. STATUS-CLOSED.Apr 6, 2001 · N804DH · Doug DC873F · Autopilot Trim ServoSDR RRXA10917Skin · crackedDURING A MAINTENANCE VISIT FOUND A 1/2" CRACK ON THE LEFT WING UPPER SKIN AT STA XRS 721 AND STRINGER 3, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 57-2-1, FIG 10 AND 51-1-11.Apr 5, 2001 · N602AL · Doug DC873F · Wing, Plate/SkinSDR DHL2001806630Fitting · crackedC-CHECK - AFT CARGO COMPARTMENT - SPLICE FITTING CRACKED 3 INCHES FROM STA 1040.000 TO STA 1060.000 L-31L. REMOVED CRACKED FITTING FROM AFT CARGO COMPARTMENT (STA 1040 - 1060 L-31L) IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. Apr 5, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835753Angle · crackedINSPECTION TYPE: C2, AFT CARGO PIT AT FS 1420 AT BL0 IN CEILING AT D PIT DOOR COVER ATTACH BRACKET IS CRACKED REMOVED CRACKED ATTACH ANGLE IAW DC8 SRM 51-1-21 AND 51-1-20D CVD NEW P ART 5616673-64 ANGLE LOCATED AND DRILLED HOLES IAW DC8 SRM 51-1-24 INSTALLApr 5, 2001 · N805UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835752Seat Track · wornINSPECTION TYPE:C2 MAIN CABIN STA 1306 AT X=0 (TRACK D) TRACK SCALLOP IS WORN AS MARKED. TRIMMED OUT DAMAGED AREA AND INSTALLED PLUG IAW DC8 SRM 53-2-3Apr 5, 2001 · N805UP · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
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