Douglas DC-8-73F

Service difficulty reports · 15,471

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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 = 'DC873F'
  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 DHL2003805544Frame · crackedRIGHT WING OUTBD L/E FORMER 0.500 CRACKED, STA XFS 753.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-Jul 31, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805506Frame · crackedRT OUTER WING OTBOARD L/E LOWER PART SHOWS FRAME CRACKED (1.000) STA XFS 841.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIJul 31, 2003 · N805DH · Doug DC873F · Wing SparSDR UPS03841016Seal · damagedLOST PRESSURIZATION IN FLIGHT - CABIN ALTITUDE CLIMBED AT A RAPID RATEJul 31, 2003 · N868UP · Doug DC873F · Cargo/Baggage DoorsSDR DHL2003806013Latch · lack of lubeCOCKPIT DOOR LATCH HARD TO OPEN. LUBED COCKPIT DOOR. OPS CHECKED GOOD IAW MM 52-10-00.Jul 31, 2003 · N806DH · Doug DC873F · Fixed Inner DoorsSDR DHL2003805569Seat Track · wornMAIN CARGO COMPT NR 1 SEAT TRACK LUG WORN AT STA 327.000. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-3 PG 17-18. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND PLUG IAW SRM 53-2-3 PG 17, 18, 19.Jul 30, 2003 · N805DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2003805567Skin · corrodedLEFT WING CTR L/E CORRODED BETWEEN STA XFS 422.750 AND XOLDI-6.225 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12.Jul 30, 2003 · N805DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003805518Frame · crackedRIGHT WING CTR L/E FORMER 1.000 CRACKED, STA XFS 497.491 (UPPER SECTION). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLJul 30, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805592Skin · corrodedRIGHT WING CTR L/E UPPER SKIN CORRODED AT XFS 423.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED OUTJul 29, 2003 · N805DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003805558Frame · crackedRIGHT WING CTR L/E FORMER CRACKED 1.000, STA XFS 404.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, 2. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLERS (02 EA) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGJul 29, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805557Frame · crackedLEFT OUTER WING OTBD L/E FORMER CRACKED 0.500 AT STA XFS 828.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANJul 29, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805551Frame · crackedLEFT OUTER WING INBD L/E FORMER CRACKED 0.500 AT STA XFS.578.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 8. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLEJul 29, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805570Frame · crackedRIGHT WING CTR L/E FORMER 0.250 CRACKED, STA XFS 316.500. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER AND AREA IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER Jul 29, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805555Frame · crackedLEFT OUTER WING OTBD L/E FORMER CRACKED 0.500 AT STA XFS 822.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANJul 29, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805535Frame · crackedLEFT OUTER WING INBD L/E FORMER CRACKED 0.500, STA XFS 616.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLJul 29, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805556Frame · crackedRIGHT WING CTR L/E FORMER 1.000 CRACKED, STA XFS.410.250 (UPPER SECTION). REMOVED FASTENERS IAW SRM 51-1-21 PG 1, 2. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLERS 2 EA IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMEDJul 29, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805554Frame · crackedLEFT OUTER WING INBD L/E FORMER CRACKED 0.500 STA XFS.622.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. IJul 29, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805553Frame · crackedLEFT OUTER WING INBD L/E FORMER CRACKED 0.500, STA XFS 610.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. Jul 29, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805540Frame · crackedLEFT OUTER WING OUTBD L/E FRAME CRACKED 0.500 AT STA XFS 835.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 0.032). INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG 9-10Jul 29, 2003 · N805DH · Doug DC873F · Wing SparSDR DHL2003805539Splice · crackedRIGHT OUTER WING INBD L/E SPLICE PLATE UPPER PART CRACKED 14.000, STA XFS 710.000. REMOVED CRACKED SPLICE PLATE IAW SRM 51-1-21. FABRICATED SPLICE PLATE (7075-T6 0.090) IAW SRM 57-1-0 PG 1, SRM 57-3-3 PG 18. CLEANED, TREATED AND PRIMED AREA AND SPLICE PLATEJul 29, 2003 · N805DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL2003805541Frame · crackedRIGHT WING CTR L/R FORMER 1.000 CRACKED, STA XFS 304.000 (LWR SECTION). PERFORMED STOP HOLE ON CRACK END (0.250) IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED ANGLE DOUBJul 29, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805536Frame · crackedLEFT OUTER WING OTBD L/E FORMER CRACKED 0.500 AT STA XFS 816.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANJul 29, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805525Frame · crackedRIGHT WING CTR L/E FORMER 1.000 CRACKED, STA XFS 379.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1-2. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLERS (02 EA) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLJul 29, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805524Frame · crackedRIGHT WING CTR L/E FORMER 1.000 CRACKED, STA XFS 484.000 (UPPER SECTION). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM Jul 29, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805521Frame · crackedRIGHT WING CTR L/E FORMER CRACKED 1.000 AT STA XS 467.323 (LWR PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE WITH NEW FASTENERS Jul 29, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805520Frame · crackedRIGHT WING CTR L/E FORMER 1.000 CRACKED, STA XFS 461.372 (UPPER SECTION). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRMJul 29, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805537Frame · crackedLEFT OUTER WING OTBD L/E FORMER CRACKED 0.500 AT STA XFS 803.750. REMOVED FASTENERS IAW SRM 51-1-21G PG 1. STOP HOLE CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLJul 28, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805552Frame · crackedLEFT OUTER WING OTBD L/E FORMER CRACKED 0.500 AT STA 797.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP HOLE CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUJul 28, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805550Frame · crackedLEFT OUTER WING OTBD L/E FORMER CRACKED 0.500 AT STA XFS 778.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP HOLE CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLEJul 28, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805549Frame · crackedLEFT OUTER WING OTBD L/E FORMER CRACKED 0.500 AT STA XFS 791.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP HOLE CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLEJul 28, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805547Frame · crackedLEFT OUTER WING OUTBD L/E FRAME 0.500 CRACKED STA XFS 747.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP HOLE CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INJul 28, 2003 · N805DH · Doug DC873F · Wing SparSDR DHL2003805538Frame · crackedLEFT OUTER WING OTBD L/E FRAME CRACKED 0.500 AT STA XFS 785.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP HOLE CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. Jul 28, 2003 · N805DH · Doug DC873F · Wing SparSDR DHL2003805545Frame · crackedLEFT OUTER WING OUTBD L/E FORMER 0.500 CRACKED, STA XFS 766.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP HOLE CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE Jul 28, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805602Seat Track · wornMAIN CARGO COMPT NR 6 SEAT TRACK LUG WORN AT STA 207.000. CUT OUT NR 6 DAMAGED AREA IAW SRM 53-2-3 PG 17 FIG 6D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND PLUG IAW SRM 53-2-3 PG 17 FIG 6D, SRM 51-3-0 PG 1.Jul 28, 2003 · N805DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2003805511Cargo Track · wornMAIN CARGO COMPT NR 7 CARGO TRACK LUG WORN AT STA 228.000. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-3 PG 17 FIG 6D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND PLUG IAW SRM 53-2-3 PG 17 FIG 6D, SRM 51-3-0 PG 1.Jul 26, 2003 · N805DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS03841110Frame · corrodedINSPECTION TYPE: C2, MAIN CABIN CANTED FRAME IS CORRODED BEYOND LIMITS AT STA 1746 AT LONG 26L. REMOVED CANTED FRAME BETWEEN LONG 26L TO 36, FABRICATED AND INSTALLED FRAME AND SPLICES IAW DWG 5612148 AND SRM 53-2-0 FIG 2.Jul 26, 2003 · N874UP · Doug DC873F · Fuselage Main, FrameSDR UPS03841108Longeron · corrodedINSPECTION TYPE:C2 MAIN CABIN LONGERON 5R IS CORRODED BEYOND LIMITS AT STA. 1745. CUTOUT DAMAGED AREA,FABRICATED AND INSTALLED FILLER AND REPAIR ANGLE IAW SRM. 53-2-2 FIG. 12Jul 26, 2003 · N874UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03841091Longeron · crackedINSPECTION TYPE: C2 STATION 1754 LONG. 14R IS CRACKED. REMOVED DAMAGED LONGERON SECTION BETWEEN STA. 1742 TO 1765, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION I.A.W. SRM. 53-2-2 FIG. 10Jul 26, 2003 · N874UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03841090Longeron · crackedINSPECTION TYPE: C2 STATION 1750 LONGERON 15R IS CRACKED. CUTOUT DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE I.A.W. SRM. 53-2-2 FIG. 12Jul 26, 2003 · N874UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03841025Skin · corrodedINSPECTION TYPE:C2 RIGHT HORIZONTAL STAB L/E UPPER SKIN IS CORRODED BEYOND LIMITS BETWEEN XFS 172.5 TO XFS 178. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 55-2-0 FIG 2, 51-1-21 FIG 33.Jul 26, 2003 · N874UP · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR UPS03841023Longeron · crackedINSPECTION TYPE:C2 MAIN CABIN LONGERON 16L IS CRACKED AT STA 1750. REMOVED LONGERON SECTION STATION 1742 TO 1765, FABRICATED AND INSTALLED LONGERON SECTION, SPLICE FITTING AND STRAPS IAW SRM 53-2-2 FIG 11.Jul 26, 2003 · N874UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03841001Seat Track · wornINSPECTION TYPE:N/A CAPTS SEAT SLIDES AFT ON TAKEOFF ROLL. INSTALLED NEW BOTH AFT SEAT TRACKS REF EO DC8-5340-0741E SRM 53-2-3 FIG 11, REMOVED AND REPLACED CAPT SEAT PER DC8 MM 25-11-01. OPS CHECK GOOD.Jul 26, 2003 · N804UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2003805512Cargo Track · wornMAIN CARGO COMPT NR 6 CARGO TRACK PLUG WORN AT STA 250.000. REMOVED WORN PLUG IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG ON MAIN CARGO COMPT NR 6 SEAT TRACK, STA 250.000 IAW SRM 51-3-0 PG 1.Jul 25, 2003 · N805DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS03841109Web · corrodedINSPECTION TYPE: C2, VERTICLE WEB IN COCKPIT SUBFLOOR IS CORRODED BEYOND LIMITS AT STA -80 LBL 50 AT FUSELAGE SKIN. REMOVED, FABRICATED AND REPLACED WEB/DOUBLER IAW DWG 5613785 AND SRM 51-1-20D, 51-1-21.Jul 25, 2003 · N874UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS03841086Skin · crackedINSPECTION TYPE:C2 LEFT AFT HEAT EXCHANGER EXTERNAL FUSELAGE SKIN LOWER AFT CORNER IS CRACKED STA. -12 AT LONG. 27L CUTOUT DAMAGE,NDT VERIFIED NO CRACKS AT CUTOUT,FABRICATED AND INSTALLED DOUBLER AND FILLER I.A.W. E.O. DC8-5330-4732Jul 25, 2003 · N874UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03841027Seat Track · corrodedINSPECTION TYPE:C2 MAIN CABIN SEAT TRACK IS CORRODED BEYOND LIMITS AT STA 260 AT LBL 60. CUT OUT DAMAGE AND INSTALLED SEAT TRACK PLUG IAW SRM 53-2-3 FIG 6D.Jul 25, 2003 · N874UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2003604756Door Frame · damagedTWO INTERIM REPAIRS ON LT AFT LWR CORNER OF MAIN CARGO DOOR STA 270.000 BETWEEN L-20L AND L-22L. REMOVED FASTENERS AND INTERIM REPAIR. TRIMMED OUT DAMAGED AREA IAW EODHL-030584 ED-3486. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. Jul 24, 2003 · N604AL · Doug DC873F · Fuselage Main, StructureSDR UPS03841096Attach Angle · crackedINSPECTION TYPE:C2 RT HORIZONTAL STAB. FRONT SPAR AT STA. XFS322. RIB ATTACH ANGLE IS CRACKED REMOVED, FABRICATED AND REPLACED ATTACH ANGLE I.A.W. DWG.4653025 AND SRM. 51-1-20D.Jul 24, 2003 · N874UP · Doug DC873F · Horizontal Stabilizer Miscellaneous StructureSDR UPS03841095Skin · crackedINSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED AT STA. -12 AT LONG. 27R. CUTOUT DAMAGE,NDT VERIFIED NO CRACKS AT CUTOUT,FABRICATED AND INSTALLED DOUBLER AND FILLER I.A.W. E.O. DC8-5330-4732-DJul 24, 2003 · N874UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03841093Fitting · crackedINSPECTION TYPE:C2 STATION 1690 LONG. 24L TO FRAME FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. SRM. 51-1-21,53-1-0,AND DWG. 4641324Jul 24, 2003 · N874UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS03841089Longeron · crackedINSPECTION TYPE:C2 STATION 1766 LONG. 17R LONGERON AND END FITTING ARE CRACKED. REMOVED,FABRICATED AND INSTALLED LONGERON SECTION,AND REPLACED END FITTING IAW DWG 5649327,4772397 AND SRM. 51-1-20DJul 24, 2003 · N874UP · Doug DC873F · Fuselage Main, Longeron/Stringer
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