Douglas DC-8-73F

Service difficulty reports · 15,471

Newest first. General aviation reporting is voluntary.

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 DHL2005807532Fitting · crackedNR 2 MAIN TANK FWD FITTING CRACK 1.000 STA XRS 74.000 AT INBD SIDE, S-51 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, AND APPLIED COATING MATERIAL AREA IAW SRM 51-1-12. INSTALLED NEW FMay 16, 2005 · N807DH · Doug DC873F · Wing Miscellaneous StructureSDR UPS05844578Longeron · corrodedINSP TYPE: C3, D PIT INTERGRANULAR CORROSION ON L34R STA 1412. REMOVED AND REPLACED LONGERON 34R STA 1390-1460 IAW SRM 51-1-21D.May 12, 2005 · N808UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2005807521Bracket · crackedRIGHT OUTBOARD SLOT MECHANISM BRACKET CRACKED. REMOVED AND REPLACED (1EA) RIGHT OUTBOARD SLOT MECHANISM BRACKET IAW MM 20-16-0 PG 201-202. REFER TO NR 036397 FOR OPS CHECK.May 12, 2005 · N807DH · Doug DC873F · Leading Edge DevicesSDR UPS05844487Longeron · crackedINSPECTION TYPE: C3, LONGERON 14L CRACKED AT STA 1746. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-2-2 FIG 11 AND 51-1-20D.May 6, 2005 · N808UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05844472Longeron · crackedINSPECTION TYPE:C3 LONGERON CRACKED 1/4 INCH LONG AT STA 1726 L15L. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED STRAPS 2 EA IAW DC-8 SRM 53-02-02, 51-1-8, 53-2-2 FIG 10 AND 51-1-20D.May 6, 2005 · N808UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05844490Rib · crackedINSPECTION TYPE: C3, LEFT L/E LWR RIB CRACKED AT XFS 816. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-3-0, 51-1-21 AND 51-1-20D.May 5, 2005 · N808UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS05844489Rib · crackedINSPECTION TYPE: C3, LT WING L/E LWR RIB CRACKED AT XFS 816. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-3-0, 51-1-21, 51-1-20D AND DWG 5769471.May 5, 2005 · N808UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS05844485Rib · crackedINSPECTION TYPE: C3, LT WING L/E AT XFS 385.000 LWR RIB CRACKED 2 INCHES LONG MIDDLE OF RIB. FABRICATED AND INSTALLED RIB FORMER AND 2 EA REPAIR ANGLES IAW DWG 5769603, SRM 51-3-2, 57-2-1 AND 51-3-2.May 5, 2005 · N808UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05844479Rib · crackedINSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED XFS 316.000. REPAIRED BY FABRICATING AND INSTALLING REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2, 51-1-21, 51-1-20D AND 51-1-15.May 5, 2005 · N808UP · Doug DC873F · Wing, Rib/BulkheadSDR DHL2005807528Floorbeam · corrodedMAIN CARGO COMPT FLOORBEAM MISDRILLED HOLE AT STA 879.000 RBL 32 AND SHOWS CORROSION ON FLANGE. PERFORMED MAJOR REPAIR IAW SRM 51-2-1 FIG 1 SHEET 7-12 TR NR 51-130. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAMay 5, 2005 · N807DH · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2005807527Floorbeam · misdrilledMAIN CARGO COMPT FLOORBEAM (2EA) MISDRILLED HOLES AT STA 980.000 BETWEEN TRACK 3 AND 4 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 51-2-1 FIG 1 SHEET 7-12, TR NR 51-130. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION IAW SRM 51-2-1 FIG 1May 5, 2005 · N807DH · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2005807526Floorbeam · corrodedMAIN CARGO COMPT FLOORBEAM CORRODED, STA 660.000 RBL 10. PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAGED SECTION IAW SMay 5, 2005 · N807DH · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2005807523Floorbeam · misdrilledMAIN CARGO COMPT FLOORBEAM MISDRILLED HOLE AT STA 960.000 LBL 38 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-28-05, EO AST050408 DATED 04-22-05. REMOVED FASTENERS FROM REPAIR AREA IAW SRM 51-1-21 PG 1. PERFORMED VISUAL DETAIL INSP, FMay 5, 2005 · N807DH · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2005807522Doubler · damagedEXTERIOR FUSELAGE NR 2 ACCESS DOOR INTERNAL DOUBLER DAMAGED. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-20-05, EO AST050407 DATED 04-16-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION IAW EO AST050407. PERFORMED NDT INSP IAW DCMay 5, 2005 · N807DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2005807524Floorbeam · wornMAIN CARGO COMPT FLOORBEAM UPPER FLANGE WORN, STA 798.000 LBL 38 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-27-05, EO AST050409 DATED 04-22-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION IAW EO AST050409. PERFOMay 5, 2005 · N807DH · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2005807518Floorbeam · misdrilledMAIN CARGO COMPT FLOORBEAM MISDRILLED HOLE AT STA 920.000 LBL 32 ON REPAIR DOUBLER. PERFORMED MAJOR REPAIR. REMOVED EXISTING REPAIR AND FASTENERS FROM AREA. FABRICATED REPAIR DOUBLER (AL7075T6 0.1000) REPAIR ANGLE EXTRUSION 7075T6 0.100 HORZ FLANGE 0.070 (VMay 5, 2005 · N807DH · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2005807520Floorbeam · corrodedAFT ACCY COMPT FLOORBEAM UPPER FLANGE CORRODED, STA 1680.000 RBL 26. PERFORMED MAJOR REPAIR. REMOVED FASTENERS FROM REPAIR AREA. REMOVED CORROSION, FOUND OUT OF LIMITS. CUT OUT DAMAGED SECTION IAW SRM 51-2-1 FIG 1 SHEET 7. PERFORMED NDT INSPECTION IAW NDTMay 5, 2005 · N807DH · Doug DC873F · Fuselage Main, Floor BeamSDR UPS05844498Rib · crackedINSPECTION TYPE:C3 LEFT WING L/E UPPER RIB CRACKED AT STA XFS 438. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EA REPAIR ANGLE DOUBLERS IAW SRM 53-02-00 FIG 001B, 51-1-21.May 4, 2005 · N808UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05844497Rib · crackedINSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED AT XFS 408. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EA REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2, 51-1-20D AND DWG 5770375.May 4, 2005 · N808UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05844496Rib · crackedINSPECTION TYPE: C3, LEFT WING L/E UPPER RIB CRACKED AT XFS 391. STOP DRILLED CRACK, FABBED AND INSTALLED 2 EA DOUBLERS IAW SRM 57-2-0 FIG 2, 57-2-0, 51-1-20D, 51-1-8 AND DWG 5770087.May 4, 2005 · N808UP · Doug DC873F · Wing, Longeron/StringerSDR UPS05844491Rib · crackedINSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED AT XFS 385.250. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS 2 EA IAW SRM 57-2-0 FIG 018, 51-1-20D, 51-1-15 AND DWG 5770087.May 4, 2005 · N808UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05844486Skin · crackedINSPECTION TYPE: C3, LT WING L/E UPPER SKIN FASTENER HOLES CRACKED .125 INCH LONG AT XFS 450. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER IAW SRM 57-2-1-0 AND 51-3-2.May 4, 2005 · N808UP · Doug DC873F · Wing, Plate/SkinSDR UPS05844470Skin · damagedINSPECTION TYPE:C3 LT WING L/E AT XFS 454, LWR SURFACE FASTENER HOLES ARE ELONGATED. REMOVE DAMAGE AND INSTALLED DOUBLER AND FILLER IAW EO DC-8 5720- 7767-A AND SRM 51-1-21.May 4, 2005 · N808UP · Doug DC873F · Wing, Plate/SkinSDR DHL2005809003O-Ring · leaking1+ 12 HR INTO FLT NR 1 ENG LOST OIL QUANTITY WITH RESULT OF LOW OIL PRESS PERFORMED ABNORMAL PROCEDURE AND ENG SHUT DOWN. REPLACED O-RING AT STARTER CASE. PER DC-8 M/M 80-10-02 OPS CHECK NORMAL ON RUNS PER JRH CH 13, P/N M83248-1-160.May 4, 2005 · N809DH · Doug DC873F · Turbine Engine Oil SystemSDR UPS05844494Rib · crackedINSPECTION TYPE: C3, LEFT WING L/E UPPER RIB CRACKED 1 INCH LONG AT XFS 828.500. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 53-2-0 FIG 1B, 57-2-0 FIG 2B, AND DWG'S 5769470-45, 576947U.May 3, 2005 · N808UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05844488Rib · crackedINSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED AT XFS 822.500 .5 INCH LONG. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2 -0, 57-2-0 FIG 2, 51-1-20D, 51-1-21 AND DWG 5769470.May 3, 2005 · N808UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05844484Rib · crackedINSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED .25 INCH LONG AT XFS 809. STOP DRILLED CRACK AND FABRICATED INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-21 AND 51-1-20D.May 3, 2005 · N808UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS05844471Rib · crackedINSPECTION TYPE:C3 LT WING L/E UPPER RIB CRACKED 1/4 INCH LONG AT XFS779. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER IAW SRM 57-2-0 FIG 2, DWG 5769470-29 AND SRM 51-1-20D,51-1-21 AND 51-1-15.May 3, 2005 · N808UP · Doug DC873F · Wing, Rib/BulkheadSDR DHL2005807525Cap · corrodedLT WING INBOARD L/E SLANT PANEL UPPER CAP CORRODED STA XFS 138.750 - 151.250. PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-3-0 PG 1. PERFORMED BLENDEOUT (7.125*1.875*0.092) FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 37. PERFORMED VISUAL DETAIL INSPECTIMay 3, 2005 · N807DH · Doug DC873F · Wing, Plate/SkinSDR DHL2005807519Skin · damagedLEFT WING CTR L/E EXTERNAL SKIN HOLES ELONGATED STA XFS 526.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-16-05, EO AST050404 DATED 04-13-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. CUT OUT DAMAGED SECTION IAW EOASMay 3, 2005 · N807DH · Doug DC873F · Wing, Plate/SkinSDR DHL2005807515Doubler · crackedMODIFICATION DOUBLER AT AFT LWR CORNER OF RT PRIMARY HEAT EXCHANGER WITH 0.75 CRACK IN IT, STA 12.000 L-27R FUSELAGE EXTERIOR. PERFORMED MAJOR REPAIR. REMOVED ALL FASTENERS WITHIN THE REPAIR AREA IAW SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. PERFORMED STOP HOLE May 3, 2005 · N807DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2005807511Skin · dentedRT INBOARD FLAP FWD LWR PLATING HAS TWO DENTS OF 6 AND 5 STA XW 43.000 - 50.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-18-05, EO AST 050403 DATED 04-12-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION IAW EO AST 050403. PERMay 3, 2005 · N807DH · Doug DC873F · Trailing Edge FlapsSDR DHL2005807510Skin · damagedRT OUTBOARD FLAP INTERIM REPAIR ON FWD UPPER PLATING, STA XF 227.000. PERFORMED MAJOR REPAIR. REMOVED ALL FASTENERS WITHIN REPAIR AREA IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED SECTION IAW EO AST-050405. PERFORMED DETAIL VISUAL INSP OF AREA, FABRICATED NEWMay 3, 2005 · N807DH · Doug DC873F · Trailing Edge FlapsSDR DHL2005807517Doubler · crackedLT PRIMARY HEAT EXCHANGER; AFT LWR CORNER MODIFICATION DOUBLER WITH 0.75 CRACK IN IT, STA 12.000 L-27L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-16-05, EO AST050401 DATED 04-12-05. REMOVED ALL FASTENERS WITHIN THE REPAIR AREA. PERFMay 3, 2005 · N807DH · Doug DC873F · Cabin Cooling SystemSDR UPS05844577Doubler · corrodedINSP TYPE: C3, A/C BAY L30R AT APPROX STA 38 TO STA 58 DOME NUTS UNDER LONGERON HAVE CORROSION OUT OF LIMITS AT ATTACH INTERNAL DOUBLER. R & R INTERNAL DOUBLER AT STA 38-58 L31R AND 2 EA LONGERONS AT STA 8 TO 70 L27R AND L30R IAW SRM 51-1-21 AND 51-1-20D.May 2, 2005 · N808UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS05844469Splice · crackedINSPECTION TYPE:C3 "D" PIT BETWEEN STA 1340-1360 L30R SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-21 AND 51-1-20D.May 2, 2005 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844685Frame · corrodedSTA 1160 SEVERE CORROSION ON BASE OF FRAME AT L33L. REMOVED, FABRICATED AND INSTALLED IAW SRM 51-1-20D, 51-1-20 D, DWG 3755842 AND SK808-785521.May 1, 2005 · N808UP · Doug DC873F · Fuselage Main, FrameSDR UPS05844483Fitting · crackedINSPECTION TYPE: C3, LWR CUSP AT STA 153 RT CUSP TO FRAME FITTING AT TORQUE BOX IS CRACKED BOTH UPPER AND LWR OF CUSP, LENGTH OF FITTING. REMOVED AND REPLACED FRAME FITTING IAW SRM 51-1-21 AND 51-1-20D.May 1, 2005 · N808UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844475Web · crackedRT MLG AFT WEB CRACKED AT GEAR CUTOUT LWR CORNER OLD REPAIR CRACKED IN RADIUS. REMOVED WEB, FAB REPLACEMENT WEB AND INSTALLED IAW SRM51-1-21, 51-1-21D, SAA FAB TRAVLER NR 0001 AND 21-1-21A.Apr 30, 2005 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844687Pressure Panel · crackedRT MLG WW FWD BULKHEAD LOWER SECTION FASTENERS HAVE MILD CORROSION IN SEVERAL PLACES RUNNING INBD TO OTBD AT SPLICE. REMOVED CORROSION FOUND TO BE WITHIN LIMITS IAW SRM 53-2-0. HFEC INSP DETECTED 3 CRACKS. FABRICATED AND INSTALLED 3 EA. REPAIR ANGLES AND 1Apr 29, 2005 · N808UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS05844474Fitting · crackedINSPECTION TYPE:C3 C-1 CARGO FITTING CRACKED AT FS 280 L32R. FOUND ON X-RAY OF DOOR CORNER EO DC8-5330-20206-B. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-2.Apr 29, 2005 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844686Web · crackedLT FWD UPPER AC BAY AT APPROX STA 8 WEB IS CRACKED APPROX 4 INCH LONG IN 2 PLACES. FABRICATED AND INSTALLED 2 DOUBLERS AND REPAIR WEB IAW SRM 53-03-03-0, 53-02-00-0 FIG 001D, 53-2-0 FIG 1D 51-1-21,51-1-20D AND 51-1-21A.Apr 28, 2005 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844508Pressure Panel · corrodedINSPECTION TYPE:C1 CORROSION ON RT W/W CEILING AT STA 863 RBL 42 AND 48 UNDER LONGERONS, ON WEB, AND DOUBLER IN MAIN CABIN IS BULGED. CUT OUT CORROSION, FABRICATED AND INSTALLED REPAIR IAW SAA SK 880-7620 56 AND EO DC-8-5310-22195-A.Apr 28, 2005 · N880UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS05844477Skin · crackedINSPECTION TYPE:C3 FUSELAGE SKIN AT APROX STA 1723 L16L HAS CRACK APROX 3/4 INCH LONG. REMOVED EXISTING DOUBLER AND FINGER DOUBLER AND FABRICATED EXTERNAL DOUBLER AND INSTALLED EXISTING FINGER DOUBLER, EXTERNAL DOUBLER AND FILLER IAW DC-8 SRM 51-1-21, 51-1-20Apr 27, 2005 · N808UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS05844476Skin · crackedINSPECTION TYPE:C3 FUSELAGE SKIN AT APROX STA 1723 RT L16 HAS CRACK APROX. 1/2 INCH LENGTH. CUT OUT DAMAGE AND INSTALLED DOUBLER, FINGER DOUBLER FILLER AND EXTERNAL DOUBLER IAW SRM 53-02-01-0 FIG 007.Apr 27, 2005 · N808UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2005807508Skin · crackedRIGHT OUTBOARD AILERON UPPER SKIN 0.500 CRACK, STA XW 698.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-8-1 FIG 4, DACO DWG 5763133. REMOVED DAMAGED PLATING IAW SRM 51-1-21 PG 1. FABRICATED NEW PLATING (AL2024T3 0.020) AND FINGER DOApr 27, 2005 · N807DH · Doug DC873F · AileronsSDR DHL2005807505Skin · dentedRIGHT INBOARD FLAP AFT LWR PLATING HAS SEVERAL DENTS (STA XW 4.000 - 91.000) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 1. REMOVED DAMAGED PLATING AND FASTENERS WITHIN REPAIR AREA IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1. FABRICApr 27, 2005 · N807DH · Doug DC873F · Trailing Edge FlapsSDR DHL2005807507Skin · crackedRT INBOARD AILERON FWD UPPER SKIN 0.500 CRACK, STA XA 502.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-8-1 FIG 1. REMOVED DAMAGED PLATING IAW SRM 51-1-21 PG 1. FABRICATED NEW PLATING (AL7075T6 0.040) IAW SRM 57-8-1 FIG 1. CLEANED,Apr 27, 2005 · N807DH · Doug DC873F · AileronsSDR UPS05844379Wire · pulledNO EMERGENCY LIGHTS ON TEST. EMERGENCY BATTERY PACK REPLACED, BUT EMERGENCY LIGHTS WOULD NOT TURN OFF WHEN DISARMED. FOUND WIRE PULLED OUT OF SOCKET NR 8 ON P1-1345. REPLACED SOCKET PER MM 20-50-01-8 AND WDM 33-50-01 PG 5. TEST GOOD PER MM 33-50-01-2.Apr 26, 2005 · N805UP · Doug DC873F · Light System WiringSDR UPS05844505Fitting · corrodedINSPECTION TYPE:C1 LONGERON SPLICE FITTING HAS HEAVY CORROSION AT STA 1270 L35R. REMOVED AND REPLACED LONGERON SPLICE FITTING IAW DC-8 SRM 51-1-20D.Apr 25, 2005 · N880UP · Doug DC873F · Fuselage Main, Attach Fittings
Back to Douglas DC-8-73F