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 RRXA003805Cover · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO C-PIT CROSS SLIDE DOOR COVER AT STA. 1160-1220 AND L33R-L27L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW MA-AM 5274-01-00.Nov 30, 2000 · N795FT · Doug DC873F · Cargo/Baggage DoorsSDR RRXA003802Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA. 879 AND L24R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REICED PART AND INSTALLED IAW DC-8 SRM 51-3-2 & Nov 30, 2000 · N795FT · Doug DC873F · Fuselage Main, BulkheadSDR RRXA003651Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE MAIN CABIN FLOOR BEAM ATTACH ANGLE FWD SIDE AT FS 55 X+44, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IANov 30, 2000 · N603AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA003617Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE UNDER DOOR SCUFF PLATE ON THE FUSELAGE EXTERIOR D CARGO COMPT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED Nov 30, 2000 · N603AL · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL200080222CFloor Support · crackedAT C CHECK; AFT CARGO COMPT. FLOOR SUPPORT CRACKED AT STA 1340 L-35R. PERFORMED STOP DRILL IAW SRM 53-2-0 PG 2E/2F, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 PAGE 2E/2F. REF: N/R 2119.Nov 30, 2000 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080220CSupport · crackedAT C CHECK; NLG DOOR SUPPORT PLATE CRACKED 1/4 INCH STA 19.000 NEAR L-31-32 RH. REMOVED DAMAGED PLATE IAW SRM 51-1-21 PG 1, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED PLATE IAW SRM 51-1-21, PG 1. REF: N/R 2043.Nov 30, 2000 · N802DH · Doug DC873F · Landing Gear DoorsSDR DHL200080211CFitting · crackedAT C CHECK; MAIN CARGO COMPARTMENT AFT BULKHEAD FITTING FWD PART CRACKED 1 INCH AT STA 1766 LONGERON 17R. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG 1, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, INSTALLED NEW FITTING IAW SRM 51-3-0 PG 1. REF: N/R Nov 30, 2000 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080206CFrame · crackedAT C CHECK; MAIN CARGO COMPARTMENT FRAME ANGLE STA 1300.000 BL 36L TO BL 40L, LOWER PART CRACKED 1 INCH . CUTOUT DAMAGED AREA IAW SRM 53-2-0 FIG 2, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED SPLICE AND FILLER IAW SRM 53-2Nov 30, 2000 · N802DH · Doug DC873F · Fuselage Main, FrameSDR UPS00834518Girt Bar · looseINSPECTION TYPE:N/A GIRTH BAR ON MAIN ENTRY DOOR WILL NOT CONNECT REPOSITIONED SLIDE AND CONNECTED BARNov 30, 2000 · N807UP · Doug DC873F · Escape SlideSDR RRXA003801Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RT. WW LONGERON 24 AT STA. 902-920, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DOUGLAS REPLACEMENNov 29, 2000 · N795FT · Doug DC873F · Wing, Nacelle/Pylon Attach FittingsSDR DHL200080219CFloor Support · crackedAT C CHECK; AFT CARGO COMPARTMENT FLOOR SUPPORT CRACKED STA 1360 BETWEEN LONGERON 35 RT. PERFORMED STOP DRILL IAW SRM 53-2-3, FIG 5, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-5, FIG 5. REF: N/R 2021.Nov 29, 2000 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080215CIntercostal · crackedAT C CHECK; MAIN CARGO COMPARTMENT INTERCOSTAL CRACKED 1 INCH AT FS-2 BL 9 RT. PERFORMED STOP DRILL IAW SRM 53-2-0 FIG 1B, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B. REF: N/R 1396.Nov 29, 2000 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003564Longeron · crackedDURING A MAINTENANCE VISIT FOUND A CRACK 5" TO THE R/H LONGERON 24, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////Nov 29, 2000 · N795FT · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA003563Seat Track · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED HOLES TO THE FE/S LT SEAT TRACK LOCK HOLES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////Nov 29, 2000 · N795FT · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003551Attach Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE R/H LONGERON ATTACH FITTING AT STA 960 AND X=59 Y=960 Z=-10, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////Nov 29, 2000 · N795FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003550Seat Track · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED LOCK HOLES ON THE 2ND OBS LEFT SEAT TRACK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////Nov 29, 2000 · N795FT · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003549Seat Track · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED HOLES TO THE FE'S RT SEAT TRACK LOCK HOLES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////Nov 29, 2000 · N795FT · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS00834516Skin · corrodedINSPECTION TYPE:C FUSELAGE BULGING AND POPPING HI-LOCKS BOTTOM OF BELLY AFT NR 3 PIT AREA. THIS ITEM TRANSFERRED FROM B-CHECK NON-ROUTINE 273672 CUTOUT CORRODED AREA AND INST DOUBLERAND TRIPER PER EO. DC8-5330-13596-ANov 29, 2000 · N851UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL200180263CFloor Support · crackedAFT CARGO COMPT FLOOR SUPPORT CRACKED BETWEEN STA 1480 AND LONGERON 34 LT TO 34 RT. STOP DRILLED CRACK PER SRM 53-2-3. FABRICATED DOUBLER PER SRM 53-2-3. INSTALLED DOUBLER PER SRM 53-2-3.Nov 28, 2000 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200180262CFloor Support · crackedAFT CARGO COMPT FLOOR SUPPORT CRACKED BETWEEN STA 1480 AND BETWEEN LONGERON 34 LT TO 34 RT. STOP DRILLED CRACK PER SRM 53-2-3. FABRICATED DOUBLER PER SRM 53-2-3. INSTALLED DOUBLER PER SRM 53-2-3.Nov 28, 2000 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200180261CDoubler · crackedAFT CARGO COMPT DOOR SUPPORT FRAME DOUBLER CRACKED 1/2 IN AT STA 1420.000.REMOVED DETEREATED ANGLE PER SRM 51-1-21. FABRICATED NEW ANGLE PER SRM 53-2-0. TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED NEW ANGLE PER SRM 51-1-21.Nov 28, 2000 · N802DH · Doug DC873F · Fuselage Main, FrameSDR DHL200180253CCargo Track · damagedMIAN CARGO COMPT NR 3 TRACK FLANGE SHOWS CORROSION FS 759.000. REMOVED CORROSION PER SRM 51-1-8. BLENDED OUT,FOUND TO BE OUT OF LIMITS PER SRM 53-2-0. FABRICATED DOUBLER PER SRM 53-2-0. TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED REPAIR PER SRM 53-2-0Nov 28, 2000 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL200080232CFloor Support · crackedAT C CK; AFT CARGO COMPARTMENT FLOOR SUPPORT CRACKED 1 INCH, 1440 BETWEEN LONGERON 34 TO 36 RT. PERFORMED STOP DRILL IAW SRM 53-2-3, FIG 5, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-3, FIG 5. REF: N/R 2018.Nov 28, 2000 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080216CFloor Panel · crackedAT C CHECK; MAIN CARGO COMPARTMENT SUB FLOOR SKIN CRACKED 16 INCHES BETWEEN FS 20 AND FS 40. CUT AFFECTED AREA IAW SRM 53-2-3, FIG 5, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 53-2-3 FIG 5. REFNov 28, 2000 · N802DH · Doug DC873F · Fuselage Floor PanelSDR DHL200080214CSkin · crackedAT C CHECK; INTERIOR CABIN-FWD GALLEY SHOWS LT LOWER SIDE CRACKED. REMOVED SKIN IAW SRM 51-1-21A, PG 4, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, INSTALLED NEW SKIN IAW SRM 51-1-21A, PG 3. REF: N/R 1331.Nov 28, 2000 · N802DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL200080213CFitting · crackedAT C CHECK; MAIN CARGO COMPARTMENT AFT BULKHEAD FITTING AFT PART CRACKED 1 INCH AT STA 1766 LONGERON 10R. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG 1, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, INSTALLED NEW FITTING IAW SRM 51-3-0, PG 1. REF: N/RNov 28, 2000 · N802DH · Doug DC873F · Fuselage Main, BulkheadSDR DHL200080209CFloorbeam · crackedAT C CHECK; MAIN CARGO COMPARTMENT FLOOR ATTACH ANGLE BROKEN 1/2 INCH, STA 1726.00 BLD. REMOVED AFFECTED AREA IAW SRM 53-2-0 FIG 1B, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED FILLER AND "U" ANGLE IAW SRM 53-2-0, FIG 1B. Nov 28, 2000 · N802DH · Doug DC873F · Fuselage Main, Floor BeamSDR DHL200080208CFrame · crackedAT C CHECK; MAIN CARGO COMPT. FORMER ANGLE CRACKED 3 INCHES, STA 1700-1705, BL 42L. CUTOUT DAMAGED FORMER ANGLE IAW SRM 53-2-0, FIG 2, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED FILLER AND SPLICE IAW SRM 53-2-0, FIG 2. RENov 28, 2000 · N802DH · Doug DC873F · Fuselage Main, FrameSDR DHL200080202CAngle · crackedAT C CHECK; FLIGHT COMPARTMENT- 682A FLOOR PANEL SHOWS ANGLE CRACKED (LOWER PART) AT FS 235.000. REMOVED CRACKED ANGLE IAW SRM 53-2-3 FIG 5, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 53-2-3, FIG 5. RENov 28, 2000 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003562Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND DETERIORATED RIVET HEADS TO THE L/E BOTTOM SURFACE AT STA XFS 20 TO XFS 35, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////Nov 28, 2000 · N795FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003561Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT WING NR 2 GROUND SPOILER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Nov 28, 2000 · N795FT · Doug DC873F · SpoilersSDR RRXA003560Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT WING T/E I/B AFT PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////Nov 28, 2000 · N795FT · Doug DC873F · Wing, Plate/SkinSDR RRXA003559Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT WING T/E I/B FWD PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////Nov 28, 2000 · N795FT · Doug DC873F · Wing, Plate/SkinSDR RRXA003558Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT WING #1 FLT SPOILER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////Nov 28, 2000 · N795FT · Doug DC873F · SpoilersSDR RRXA003557Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT WING #2 FLIGHT SPOILER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////Nov 28, 2000 · N795FT · Doug DC873F · SpoilersSDR RRXA003556Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT WING T/E PANEL 2ND FROM O/B, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////Nov 28, 2000 · N795FT · Doug DC873F · Wing, Plate/SkinSDR RRXA003555Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT WING T/E PANEL I/B FWD, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////Nov 28, 2000 · N795FT · Doug DC873F · Wing, Plate/SkinSDR RRXA003554Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT WING T/E FWD OF I/B AFT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////Nov 28, 2000 · N795FT · Doug DC873F · Wing, Plate/SkinSDR RRXA003553Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT WING T/E FWD OF I/B AILERON O/B PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////Nov 28, 2000 · N795FT · Doug DC873F · AileronsSDR RRXA003552Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE #2 SPOILER L/H WING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////Nov 28, 2000 · N795FT · Doug DC873F · SpoilersSDR RRXA003808Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RT WING UPPER SKIN AT STA 727 AND STRINGER NR 1, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-20-0 & 53-2-0.Nov 27, 2000 · N795FT · Doug DC873F · Wing, Plate/SkinSDR RRXA003804Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA. 920 AMD L24 AND LT WW, 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 Nov 27, 2000 · N795FT · Doug DC873F · Wing, Nacelle/Pylon Attach FittingsSDR RRXA003667Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SEAT TRACK AT STA 930-1130 AND RBL-X45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SNov 27, 2000 · N603AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003666Structure · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AND BREAK TO THE OUTER SHROUD OF THE RT SCOOP INLET DUCT IN THE FWD NOSE COMPT AT STA 165, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IANov 27, 2000 · N603AL · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200180266CAngle · crackedMAIN CARGO COMPT ANGLE CRACKED 1 IN AT STA 1700 BL 48R. REMOVED DAMAGED ANGLE PER SRM 53-2-0. FABRICATED ANGLE PER SRM 53-2-0. CLEANED,TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 51-3-0.Nov 27, 2000 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200180264CFloor Support · crackedMAIN CARGO COMPT FLOOR SUPPORT CRACKED 5 IN FS 50.000 BL 10 RT. STOP DRILLED CRACK AND FABRICATED DOUBLER PER SRM 53-2-0. CLEANED,TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLER PER SRM 53-2-0.Nov 27, 2000 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200180256CCargo Track · damagedMAIN CARGO COMPT FLOOR TRACK 2 RT WORN AT STA FS 206. CUT OUT FLOOR TRACK 2 RT DAMAGED AREA AS REQUIRED PER SRM 53-2-3. FABRICATED PLUG AND CHANNEL PER SRM 53-2-3. CLEANED ,TREATED AND PRIMED PLUG AND CHANNEL PER SRM 51-1-8B. INSTALLED PLUG AND CHANNEL PERNov 27, 2000 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL200180255CPlate · crackedNOSE LANDING GEAR LT SIDE DOOR SUPPORT PLATES CRACKED AT STA 60.000.REMOVED PLATE PER SRM 53-2-0. FABRICATED NEW PLATE PER SRM 53-2-0. TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED PLATES PER SRM 53-2-0.Nov 27, 2000 · N802DH · Doug DC873F · Landing Gear DoorsSDR DHL200180243CCargo Track · damagedDURING C CHECK FOUND MAIN CARGO FLOOR TRACK 1 LT WORN AT STA FS 450.CUT OUT DAMAGED AREA PER SRM 53-2-3.FABRICATED TRACK PLUG PER SRM 53-2-3. FABRICATED CHANNEL WITH EXTUSSION, CLEANED, TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED CHANNEL AND PLUG PER SRM 53-2Nov 27, 2000 · N802DH · Doug DC873F · Cargo CompartmentsSDR DHL200080212CRib · crackedAT C CHECK; RADOME-BULKHEAD RIB CRACKED 1/2 INCH AT STA 165.000 (RT). PERFORMED STOP DRILL IAW SRM 53-2-0, FIG 1B, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B. REF: N/R 1236.Nov 27, 2000 · N802DH · Doug DC873F · Fuselage Miscellaneous Structure
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