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 UPS07850405Battery · dischargedINSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY UNIT PER MM 33-50-01-2. OPS CHECK GOOD.Aug 7, 2007 · N818UP · Doug DC873F · Emergency LightingSDR DHL2007804524Skin · crackedLWR FUSELAGE EXTERNAL SKIN HAS TWO CRACKS OF 0.250" AND 0.500", STA 60.000 L-35.8R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 08-02-07, EVA D853-00011 REV IR DATED 03-18-07, DWG AD79-53-103 REV IR DATED 07-19-07. REMOVED FASTENERS IAW SRM 51-1-21. CUAug 6, 2007 · N804DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2007804523Skin · damagedRT OUTER WING INBD L/E HOLES ELONGATED STA XW 485.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 08-02-07, EVA D857-0009 REV IR DATED 06-13-07, DWG AD79-57-102 REV IR DATED 07-13-07. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. CUT OUAug 6, 2007 · N804DH · Doug DC873F · Wing, Plate/SkinSDR DHL2007804522Skin · wornRT OUTBD FLAP UPPER SKIN WORN 1/2", STA XF 226.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 08-02-07, ASTAR EV D853-00008 REV IR DATED 07-10-07, REV IR, COTNEY DOC EDW27-5, RELEASE DATE 07-21-04 REV IR, DWG NR W27-R05 IR DATE 07-21-04.Aug 6, 2007 · N804DH · Doug DC873F · Trailing Edge FlapsSDR UPS07850484Fitting · crackedINSPECTION TYPE:C1 FITTING CRACKED AT STA 1260 L20R. REMOVED AND REPLACED FITTING AT STA 1260 L20R IAW SRM 51-01-20D AND SRM 51-3-2.Aug 6, 2007 · N874UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07850483Fitting · crackedINSPECTION TYPE:C1 STA 1060 FRAME FITTING IS GOUGED. REMOVED FRAME FITTING AT STA 1060 IAW SRM 51-3-0. LOCATED, DRILLED UP AND INSTALLED NEW FRAME FITTING AT STA 1060 IAW SRM 51-03-02 AND SRM 51-1-20D.Aug 6, 2007 · N874UP · Doug DC873F · Fuselage Main, FrameSDR UPS07850465Web · crackedINSPECTION TYPE:C1 FWD LWR CORNER OF FWD RIGHT SERVICE DOOR HAS CRACK IN WEB. CUT OUT DAMAGED AREA ON FWD LWR CORNER WEB ON RIGHT FWD SERVICE DOOR IAW SRM 52-02-00 FIG 4. FABRICATED AND INSTALLED REPAIR DOUBLER ON RIGHT FWD SERVICE DOOR FWD LWR CORNER IAW SRAug 6, 2007 · N874UP · Doug DC873F · Service DoorsSDR UPS07850464Web · damagedINSPECTION TYPE:C1 LARGE PUNCTURE AND 2EA CRACKS IN WEB AT AFT UPPER SECTION OF INTERIOR OF RIGHT FWD SERVICE DOOR. CUT OUT DAMAGED AREA FROM WEB ON RIGHT FWD SERVICE DOOR IAW SRM 52-02-00 FIG 4. FABRICATED AND INSTALLED REPAIR DOUBLER ON RIGHT FWD SERVICE DAug 6, 2007 · N874UP · Doug DC873F · Service DoorsSDR UPS07850463Web · damagedINSPECTION TYPE:C1 HOLE DRILLED THROUGH FASTENER AND INTO FWD CENTER WEB OF RIGHT FWD SERVICE DOOR INTERIOR. CUT OUT DAMAGED AREA FROM CENTER WEB ON RIGHT FWD SERVICE DOOR IAW SRM 52-02-00 FIG 4. FABRICATED AND INSTALLED REPAIR DOUBLER ON CENTER WEB OF THE RAug 6, 2007 · N874UP · Doug DC873F · Service DoorsSDR UPS07850461Fitting · crackedINSPECTION TYPE:C1 FITTING CRACKED AT STA 1240 L20R. REMOVED CRACKED FITTING AT STA 1240 L20R IAW SRM 51-01-20D. FABRICATED AND INSTALLED REPAIR FITTING AT STA 1240 L20R IAW DWG 4750419, AND SRM 51-01-24-0 FIG 002.Aug 6, 2007 · N874UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07850451Web · puncturedINSPECTION TYPE:C1 HOLE PUNCTURED IN INTERIOR WEB OF RIGHT FWD SERVICE DOOR FWD CENTER AREA. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM5 2-02-00 FIG 4, SRM 52-03-01 FIG 3, 52-02-00, 51-01-21, AND 51-01-11.Aug 6, 2007 · N874UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS07850442Finger Doubler · crackedINSPECTION TYPE:C1 CENTER WING BOX SUBFLOOR FINGER DOUBLER CRACKED AT STA 890 LBL 5. REMOVED CRACKED FINGER DOUBLER AT STA 890 LBL 5 IAW SRM 51-1-20D, FABRICATED AND INSTALLED REPAIR FINGER DOUBLER AT STA 890 LBL 5 IAW SRM 53-07-03-0 FIG 004.Aug 6, 2007 · N874UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07850432Web · crackedINSPECTION TYPE:C1 WEB CRACKED ON RIGHT AFT SERVICE DOOR AFT SIDE BELOW BAYONET. STOP DRILLED END OF CRACK ON WEB IAW SRM 52-02-00 FIG 02. FABRICATED AND INSTALLED REPAIR DOUBLER ON RIGHT AFT SERVICE DOOR WEB IAW SRM 52-02- 00 FIG 02.Aug 5, 2007 · N874UP · Doug DC873F · Service DoorsSDR UPS07850592Seat Track · gougedINSPECTION TYPE:C1 SEAT TRACK GOUGED AT STA 317 RBL 60. REMOVED DAMAGED SEAT TRACK AT STA 317 RBL 60 IAW EO DC8-5340-7779. INSTALLED SEAT TRACK PLUG AT STA 317 RBL 60 IAW EO DC8-5340-7779 APPX A AND SRM 53-2-3 FIG 6D.Aug 4, 2007 · N874UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007804521Doubler · corrodedFWD CARGO COMPT INNER DOUBLER CORRODED STA 70.000 L-36 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW JC EC-00423 (WO 1616), DWG DOUGLAS NR 4646945. REMOVED CORROSION IAW SRM 51-1-8B PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED DOUBLER Aug 4, 2007 · N804DH · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07850506Seat Track · gougedINSPECTION TYPE:C1 SEAT TRACK GOUGED OUT OF LIMITS AT STA 240 BL 0. REMOVED AND REPLACED SEAT TRACK SECTION FROM STA 230-250 BL 0 IAW SRM 53-02-03-0 FIG 014, 53-07-03 FIG 2B, AND DWG S2400463.Aug 4, 2007 · N874UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS07850466Fitting · crackedINSPECTION TYPE:C1 FITTING CRACKED AT STA 1230 TO STA 1240 L19R. REMOVED CRACKED FITTING AT STA 1230 TO 1240 L19R IAW SRM 51-01-20D, FABRICATED AND INSTALLED REPAIR FITTING AT STA 1230 TO 1240 L19R IAW SRM 51-01-20D, AND DWG 3758513.Aug 4, 2007 · N874UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2007804511Structure · misrepairedPERFORMED DETAILED VISUAL INSPECTION AND FOUND PREVIOUS REPAIR NOT IN ACCORDANCE WITH SRM. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1, 3. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLAug 3, 2007 · N804DH · Doug DC873F · Fuselage Main, StructureSDR DHL2007804510Structure · misrepairedPERFORMED DETAILED VISUAL INSPECTION AND FOUND PREVIOUS REPAIR NOT IN ACCORDANCE WITH SRM. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1, 5. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED REPAug 3, 2007 · N804DH · Doug DC873F · Fuselage Main, StructureSDR DHL2007804508Skin · crackedRT WING UPPER SKIN CRACKED 1 1/4" AT STA XCW 69.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 20 SHEET 1. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW SRM 57-2-1 FIG 20 SHEET 1. PERFORMED NDT INSPECTION IAW DAug 3, 2007 · N804DH · Doug DC873F · Wing, Plate/SkinSDR DHL2007804507Structure · misrepairedPERFORMED DETAILED VISUAL INSPECTION AND FOUND PREVIOUS REPAIR NOT IN ACCORDANCE WITH SRM. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1-5. REMOVED EXISTING NON-STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED REPAAug 3, 2007 · N804DH · Doug DC873F · Fuselage Main, StructureSDR DHL2007804506Structure · misrepairedPPERFORMED DETAILED VISUAL INSPECTION AND FOUND A PREVIOUS REPAIR NOT IN ACCORDANCE WITH SRM. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1, 4. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED REPAIR DOUBLER (AL7075T6 0.0Aug 3, 2007 · N804DH · Doug DC873F · Fuselage Main, StructureSDR UPS07850482Fitting · crackedINSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 680 L9L FWD. REMOVED CRACKED END FITTING AT STA 680 L9L IAW SRM 51-1-21. LOCATED, DRILLED UP, AND INSTALLED NEW LONGERON END FITTING AT STA 680 L9L IAW SRM 51-01-20D, AND DWG 377972.Aug 3, 2007 · N874UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS07850431Fitting · crackedINSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 902 L9L AFT. REMOVED AND REPLACED LONGERON END FITTING AT STA 902 L9L AFT IAW SRM 51-1-20D, AND SRM 51-3-1.Aug 3, 2007 · N874UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS07850427Bulkhead · crackedINSPECTION TYPE:C1 AFT PRESS BULKHEAD CRACKED RBL 24 L10R TO L12R. CUT OUT DAMAGED AREA ON AFT PRESS BULKHEAD STA 1766 RBL 24 L10R TO L12R IAW SRM 53-2-5. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER AT AFT PRESS BULKHEAD STA 1766 L10R TO L12R IAW SRM Aug 3, 2007 · N874UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS07850419Fitting · crackedINSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 680 L10R FWD. REMOVED AND REPLACED LONGERON END FITTING AT STA 680 L10R FWD IAW SRM 51-3-0, SRM 51-1-21D, AND 51-01-23.Aug 3, 2007 · N874UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS07850536Rib · crackedINSPECTION TYPE:C2 LT HORIZ STAB L/E RIB CRACKED, AFT LWR, STA XFS 140. REPAIRED CRACKED RIB ON L/H HORIZ. STAB L/E AT STA XFS 140 BY INSTALLING DOUBLER IAW SRM 55-02-00, AND SRM 51-1-20D.Aug 1, 2007 · N801UP · Doug DC873F · Horizontal Stabilizer, Spar/RibSDR DHL2007804509Door Frame · cracked"B" CARGO DOOR FWD LWR JAMB CORNER CRACKED 1/2" STA 521.000 L-31R TO L-32R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 07-20-07, BOEING MSG NR 1-425040944-2 DATED 07-20-07, AD2005-18-07, DOUGLAS DWG NR 57507776, ASTAR EVAD852-00012 REV IRAug 1, 2007 · N804DH · Doug DC873F · Fuselage Main, StructureSDR DHL2007804505Panel · corrodedLT WING T/E UPPER SURFACE PANEL CORRODED, STA XRS 74.000. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. REMOVED CORRODED PANEL ASSY IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEAug 1, 2007 · N804DH · Doug DC873F · Wing, Plate/SkinSDR UPS07850472Web · crackedINSPECTION TYPE:C2 RUDDER HAS 1.5 INCH CRACK IN LWR STRUCTURE JUST AFT OF TORQUE TUBE MOUNTING. REMOVED CRACKED WEB ON RUDDER IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR WEB ON RUDDER STA ZR 59.54 IAW SRM 51-03-00-0, AND DWG 5701251.Aug 1, 2007 · N851UP · Doug DC873F · Rudder Miscellaneous StructureSDR UPS07850574Frame · corrodedINSPECTION TYPE:C2 HEAVY CORROSION ON LWR FLANGE OF FRAME AT STA 1240 L35R. CUT OUT CORRODED AREA OF LWR FLANGE ON FRAME STA 1240 L35R PER SAA EA 008-5330-01-A0995. REPAIRED LWR FLANGE ON FRAME STA 1240 L35R PER SAA EA 008-5330-01-A0995, UPS RAA DC8-53-20650Jul 31, 2007 · N851UP · Doug DC873F · Fuselage Main, FrameSDR UPS07850363Structure · tornAPPROX 1 INCH TEAR IN FLOOR OF PIT 33 APPROX 24 INCHES A/C LEFT OF CENTER & APPROX 36 INCHES FROM AFT BULKHEAD. C/W UPS EO DC8-5320-8724 APPROX A. D355594 ISSUED BY AMC. REPAIRED PIT 33 FLOOR PER EO DC8-5320-8724. PERMANENT REPAIR INSTALLED. D355594 CLEARED.Jul 31, 2007 · N811UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07850361Escape Rope · out of positionINSPECTION TYPE:N/A ESCAPE ROPE CAPTAINS SIDE FELL OUT ON SHORT FINAL. REPACKED CAPTAINS ESCAPE TAPE PER MM 25-60-02-2.Jul 31, 2007 · N868UP · Doug DC873F · Emergency EquipmentSDR DHL2007804504Skin · damagedLT OUTER WING INBD L/E SKIN HOLES ELONGATED, STA XFS 710.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-25-07, DWG NR AD79-57-101 REV IR DATED 07-13-07. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW DWGJul 28, 2007 · N804DH · Doug DC873F · Wing, Plate/SkinSDR UPS07850344Battery Pack · inoperativeINSPECTION TYPE: N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-50-01-2. OPS CHECK NORMAL.Jul 28, 2007 · N868UP · Doug DC873F · Emergency LightingSDR UPS07850552Longeron · corrodedINSPECTION TYPE:C2 L-35R CORRODED FROM STA 1220-1260 ON INBD LONGERON. REMOVED AND REPLACED LONGERON AND BATHTUB FITTINGS FROM STA 1210 TO 12 0 IAW SRM 53-2-0 AND DWG 5750322.Jul 26, 2007 · N851UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2007804503Channel · crackedRT MLG, ZEE CHANNEL OF FAIRING CRACKED 4", STA XW 3.125. REMOVED CRACKED ZEE CHANNEL IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED ZEE CHANNEL (P/N 5651221-14SP) IAW SRM 51-1-21. REFER TO JC EC-00426-001 (WO 1616) FOR FABRICAJul 26, 2007 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07850287Thrust Reverser · inoperativeNUMBER 2 ENG DUE TO THRUST REVERSER WOULD NOT STOW COMPLETED ALL CHECKLIST. PER CAPTAIN ENGINE HAD POSITIVE OIL PRESSURE REMAINDER OF FLIGHT. DEF NR M 355263 OPENED. DEFERRED NR 2 ENG THRUST REVERSER ACCOMPLISHED DEACTIVATION PROCEDURES REF MEL 78-1 AND M/MJul 26, 2007 · N803UP · Doug DC873F · Engine Thrust ReverserSDR UPS07850444Fitting · crackedINSPECTION TYPE:C2 L-31R END FITTING CRACKED AT STA 1690. REMOVED AND REPLACED LONGERON END FITTING AT STA 1690 L31R IAW SRM 51-1-21, AND SRM 51-3-0.Jul 25, 2007 · N851UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS07850337Web · puncturedINSPECTION TYPE: C2 WEB PUNCTURED AT STA 70 L21L. CUT OUT DAMAGED AREA ON WEB AT STA 70 L21L IAW SRM 53-02-00-0 FIG1F FABRICATED AND INSTALLED REPAIR DOUBLER AT STA 70 L21L IAW SRM 53-03 -03-0.Jul 25, 2007 · N851UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07850244Battery Pack · dischargedINSPECTION TYPE:SP EMERGENCY LIGHTING FAILED OPS CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK IAW DC8 AMM 33-50-01-2. OPS CHECK GOOD.Jul 25, 2007 · N868UP · Doug DC873F · Emergency LightingSDR UPS07850613Skin · corrodedINSPECTION TYPE:C2 C-PIT STA 1240-1260 BETWEEN L36 AND L34R INTERNAL DOUBLER HAS CORROSION AND EXTENDS UNDER L35R. REPAIRED FUSELAGE SKIN AND INTERNAL DOUBLER AT STA 1242 L35R IAW SAA EA 008-5330-01-A0985, UPS RAA DC8-53-20644, AD FAA FORM 8100-9.Jul 24, 2007 · N851UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2007804513Floor Support · corrodedMAIN CARGO COMPT FLOOR PANEL SUPPORT ANGLE CORRODED (STA 8.000 - 70.000, RBL 8" TO 46"). REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT CORRODED SECTION OF ANGLE AND FABRICATED REINFORCING ANGLE (EXTRUSION P/N SJul 24, 2007 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07850474Splice · crackedINSPECTION TYPE:C2 L36 SPLICE BETWEEN STA 1260 AND 1280 CRACKED. REMOVED AND REPLACED FITTING IAW SAA EA 008-5310-01-A0987.Jul 24, 2007 · N851UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07850372Skin · canningINSPECTION TYPE:C2 LEFT ELEVATOR UPPER SKIN INBOARD OIL CANNED. REMOVED, FABRICATED, AND INSTALLED ELEVATOR SKIN IAW SRM 51-1-21, 55-0 2-01, 51-1-8 AND 51-1-21A.Jul 24, 2007 · N851UP · Doug DC873F · Elevator, Plate/SkinSDR UPS07850371Floorbeam · corrodedINSPECTION TYPE:C2 FLOORBEAM STA 1300 RBL 24 CRACKED AND CORRODED. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER & DOUBLER IAW SRM 5 3-2-0, 51-02-00 FIG 1, 51-1-8, 51-1-20D, AND DWG 2759472.Jul 24, 2007 · N851UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS07850350Battery · dischargedINSPECTION TYPE:N/A ON PREFLIGHT AIRCRAFT FAILED EMERGENCY EXIT LIGHTS CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY & RELAY PACK IAW DC8 MM 33-50-1-2. OPS CHECKS NORMAL.Jul 24, 2007 · N819UP · Doug DC873F · Emergency LightingSDR UPS07850394Floorbeam · gougedINSPECTION TYPE:C2 A-PIT STA 120 LBL 26 FLOORBEAM GOUGED AND FASTENER SHEARED. CUT OUT DAMAGED AREA ON FLOORBEAM AT STA 120 LBL 26 IAW SRM 51-02-00, FABRICATED AND INSTALLED REPAIR ANGLES AT STA 120 LBL 26 IAW SRM 51-02-00 FIG 1, AND SRM 53-02-00 FIG 1F.Jul 23, 2007 · N851UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS07850338Angle · crackedINSPECTION TYPE: C2 C-PIT FWD BULKHEAD STA 986 LBL 46, ANGLE CRACKED. STOP DRILLED CRACKED ANGLE AT STA 986 LBL 46 IAW SRM 53-02-00-0 FIG 001B. FABRICATED AND INSTALLED REPAIR ANGLE AT STA 986 LBL 46 IAW SRM 53-02-00-0, AND DWG 5704721Jul 23, 2007 · N851UP · Doug DC873F · Fuselage Main, StructureSDR UPS07850443Attach Angle · crackedINSPECTION TYPE:C2 LEFT SIDE OF VERT STAB LWR ATTACH ANGLE CRACKED AT STA 1766. REPAIRED LEFT SIDE OF VERT STAB LWR ATTACH ANGLE AT STA 1766 IAW SRM 53-02-05-0 FIG 016A.Jul 22, 2007 · N851UP · Doug DC873F · Vertical Stabilizer Miscellaneous Structure
Back to Douglas DC-8-73F