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 UPS07849765Door Frame · misrepairedINSPECTION TYPE:C1 L1 DOOR CUTOUT HAS RIVET WITH NO ED AT LWR HINGE CUTOUT. REMOVED, FABRICATED, AND INSTALLED L1 DOOR JAMB FRAME IAW SRM 51-1-21, 0D, 51-03-02,51-1-8,51-01-14, AND 51-3-0.Apr 12, 2007 · N819UP · Doug DC873F · Fuselage Main, StructureSDR DHL2007806548Fitting · crackedMAIN CARGO COMPT FITTING CRACKED 1" STA 759.000 L-13R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE).Apr 12, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806569Fitting · crackedSTRUCTURE UNDER "A" CROSS-SLIDE CARGO DOOR, FITTING CRACKED 0.500" STA 320.000 L-27L. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CUT OUT NEW FITTING AND FABRICATED REPAIR ANGLE (7075T6511 0.125") IAW SRM 53-2-0 FIG 2D. CLEANED, TREATED AND PRIMED AREA AND REApr 12, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806557Skin · delaminatedNR 1 LT SPOILER PANEL LWR SKIN DELAMINATED. REMOVED AND REPLACED NR 1 LT SPOILER PANEL IAW MM 27-61-1 PG 201-206. REFER TO NR 075764 FOR OPS CHECK.Apr 12, 2007 · N806DH · Doug DC873F · SpoilersSDR DHL2007806572Hinge · crackedRT MLG OUTBD DOOR HINGE CRACKED. REMOVED AND REPLACED RT MLG OUTBD DOOR IAW MM 31-12-1 PG 405. REFER TO JC 8-32-00-003 FOR OPS CHECK.Apr 12, 2007 · N806DH · Doug DC873F · Landing Gear DoorsSDR UPS07849684Channel · crackedINSPECTION TYPE:C1 T-CHANNEL CRACKED UPPER SURFACE AT XRS 204 BETWEEN STRINGERS 60 AND 59. STOPPED DRILLED CRACK AT XRS 204 BETWEEN STRINGERS 59 & 60 IN NR 4 MAIN TANK IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00-0, AND SRApr 12, 2007 · N819UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS07849826Skin · crackedINSPECTION TYPE:C1 LEFT WING UPPER REAR SPAR SKIN CRACKED 5 INCHES AT STA XCW 69. REPAIRED LEFT WING UPPER AFT SPAR AT STA XCW 69.5 IAW SAA EA 008- 5710-01-A0835, UPS EO DC8-5730-26787-A, AND FAA FORM 8100-9.Apr 11, 2007 · N819UP · Doug DC873F · Wing, Plate/SkinSDR UPS07849791Spar Cap · crackedINSPECTION TYPE:C1 CRACK ON LWR CENTER SPAR CAP FLANGE NEAR XRS 172 NR 2 MAIN TANK. REPAIRED WING CENTER LWR CAP AND WEB AT STA XRS 168 NR 2 MAIN TANK IAW SAA EA 008-5710-01-A0808, UPS EO DC8-5710-26734-A, SRO8570015, AND FAA FORM 8100-9.Apr 11, 2007 · N819UP · Doug DC873F · Wing SparSDR UPS07849790Angle · crackedINSPECTION TYPE:C1 CENTER SECTION EXTERIOR L-ANGLE CRACKED THRU STOP DRILLED HOLE AT STA 855 LBL 65. REMOVED CRACKED L-ANGLE AT STA 855 LBL 65 IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPAIR FILLER, AND ANGLE DOUBLER AT STA 855 LBL 65 IAW SRM 53-02-00 FApr 11, 2007 · N819UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2007806552Fitting · crackedAFT CARGO COMPT BILGE FITTING CRACKED STA 1240.000 L-35R. REMOVED AND REPLACED CRACKED FITTING AT AFT CARGO COMPT BILGE STA 1240.000 L-35R IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE).Apr 11, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806576Skin · damagedRT ELEVATOR UPPER SKIN DEFLECTED (STA XE 22.875 - 228.031) MAJOR REPAIR (DAMAGED). PERFORMED MAJOR REPAIR IAW SRM 55-4-1 FIG 1 (SHEET 1-2). REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-0Apr 11, 2007 · N806DH · Doug DC873F · Elevator, Plate/SkinSDR DHL2007806560Fitting · crackedFOUND MAIN CARGO COMPT FITTING CRACKED 0.500" STA 834.500 L-13R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 PG 2A (TORQUE). REFER TO JC EC-00271-001 (WO 470Apr 10, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806547Fitting · corrodedMAIN CARGO COMPT FITTING CORRODED STA 100.000 L-21R. REMOVED CORROSION FROM FITTING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IApr 10, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806553Fitting · crackedAFT CARGO COMPT BILGE FITTING CRACKED STA 1140.000 L-33R TO L-32R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). REFER TO JC EC-00259-001 (WO 470) FOApr 10, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806540Angle · crackedNR 1 STUB WING FORMER ANGLE CRACKED STA XS 527.000. REMOVED CRACKED ANGLE IAW SRM 51-1-21. FABRICATED NEW ANGLE (7075"0" 0.080") IAW DOUGLAS DWG NR 9753297. HEAT TREATED ANGLE FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED ARApr 10, 2007 · N806DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL2007806561Fitting · crackedFOUND MAIN CARGO COMPT FITTING 0.500" CRACKED STA 834.500 L-18R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 PG 2A (TORQUE) REFER TO JC EC-00245-001 (WO 470) Apr 10, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806559Fitting · crackedMAIN CARGO COMPT FITTING CRACKED 0.500" STA 742.250 L-13R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 PG 2A (TORQUE). REFER TO JC EA-00252-001 (WO 470) FOR Apr 10, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806568Frame · damagedMAIN CARGO COMPT FRAME HAS A MISDRILLED HOLE AT STA 742.250 L-20R TO L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-04-07, JC EC-00283-001, REPAIR ORDER NR 2-50701-801 DATED 04-04-07 (ED-4497). PERFORMED NDT INSPECTION IAW DC8 NDT Apr 10, 2007 · N806DH · Doug DC873F · Fuselage Main, FrameSDR DHL2007806566Frame · damagedMAIN CARGO COMPT FRAME HAS A MISDRILLED HOLE STA 920.000 L-6R TO L-7R. PERFORMED MAJOR REPAIR IAW FAA FORM8110-3 DATED 04-04-07, JC EC-00283-001, REPAIR ORDER NR 2-50701-801 DATED 04-04-07 (ED-4499). PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001Apr 10, 2007 · N806DH · Doug DC873F · Fuselage Main, FrameSDR DHL2007806564Fitting · crackedMAIN CARGO COMPT FITTING 1 INCH CRACK STA 781.500 L-18L. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 PG 2A (TORQUE). REFER TO JC EC-00255-001 (WO 470) FOR FIApr 10, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806563Fitting · crackedMAIN CARGO COMPT FITTING CRACKED 0.500", STA 857.125 L-19R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 PG 2A (TORQUE). REFER TO JC EC-00260.001 (WO 470) FORApr 10, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806551Fitting · crackedLT HORIZ STAB LWR FITTING CRACKED, STA XFS 60.000. REMOVED CRACKED FITTING IAW SRM 51-1-21, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1Apr 10, 2007 · N806DH · Doug DC873F · Horizontal Stabilizer, Attach FittingsSDR DHL2007806550Stiffener · crackedLT HORIZ STAB STIFFENER CRACKED 1" STA XFS 47.500. REMOVED CRACKED STIFFENER IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW STIFFENER IAW SRM 51-1-21.Apr 10, 2007 · N806DH · Doug DC873F · Horizontal Stabilizer Miscellaneous StructureSDR DHL2007806558Fitting · crackedMAIN CARGO COMPT FITTING CRACK 1" STA 781.500 L-18R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 PG 2A (TORQUE). REFER TO JC EC-00253-001 (WO 470) FOR FITTINApr 10, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS07849745Skin · corrodedINSPECTION TYPE:C1 EVIDENCE OF CORROSION UNDER VERT STAB SKIN, RIGHT SIDE LARGE AREA OF PILLOWED SKIN WITH SEVERAL FAILED RIVETS. EXTERIOR ZR252-296 ALONG REAR SPAR. REMOVED AND REPLACED RIGHT VERT STAB SKIN IAW SRM 51-1-21, 51-1-20D, AND 51-3-0.Apr 10, 2007 · N819UP · Doug DC873F · Vertical Stabilizer, Plate/SkinSDR DHL2007806549Fitting · cracked"C" CARGO DOOR JAMB FITTING 0.500" CRACK STA 1220.000 L-34R - L-35R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CUT OUT NEW FITTING AND FABRICATED REPAIR ANGLE (AL7075T6 511 0.125") IAW SRM 53-2-0 FIG 2D. CLEANED, TREATED AND PRIMED AREA AND REPAIR ANGLE IAWApr 9, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806567Cusp Web · corrodedMAIN CARGO COMPT UPPER CUSP CORRODED (STA 35.000 - 60.000, L-21R) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW BOEING MSG NR 1-307875056-2 DATED 03-28-07. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED CUSApr 9, 2007 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2007806536Fitting · corrodedFOUND MAIN CARGO COMPT FITTING CORRODED STA 25.000 L-21R. REMOVED CORROSION FROM FITTING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALApr 9, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806542Doubler · corrodedAFT ACCY COMPT INTERNAL DOUBLER CORRODED, STA 1665.000 L-25L TO L-26L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-05-07, DWG NR AD08-53-101 REV IR DATED 03-30-07. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRMApr 9, 2007 · N806DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2007806556Fitting · corrodedLT MLG WW L-24 FRAME FITTING CORRODED STA 879.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 8 SHEET 1, 3, 6. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 FIG 1F SHEET 3. REMOVED CORRODED FRAME FITTING IAW SRApr 9, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806541Fitting · corroded"C" CARGO DOOR JAMB FITTING CORRODED STA 1220.000 L-35R TO L-36. REMOVED CORROSION FROM "C" CARGO DOOR JAMB FITTING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FITTING IAW SRM 51-1-20D. CUT OUT NEW FITTING AND FABRICApr 9, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806534Fitting · corrodedMAIN CARGO COMPT FITTING CORRODED STA 35.000 L-21R. REMOVED CORROSION FROM FITTING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEApr 9, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806533Doubler · corrodedMAIN CARGO COMPT INTERNAL DOUBLER CORRODED (STA 8.000 - 25.000 L-21R). REMOVED CORROSION FROM INTERNAL DOUBLER IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED INTERNAL DOUBLER IAW SRM 53-1-0 PG 1,SRM 51-1-21. FABRICATED NEW INTERApr 9, 2007 · N806DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2007806535Fitting · corrodedFOUND MAIN CARGO COMPT FITTING CORRODED STA 55.000 L-21R. REMOVED CORROSION FROM FITTING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALApr 9, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806539Frame · deformedMAIN CARGO COMPT FRAME DEFORMED STA 1580.000 L-21L. PERFORMED MAJOR REPAIR IAW SRM 53-4-1 FIG 51. REMOVED DAMAGED FRAME SEGMENT IAW SRM 53-1-0 PG 1, SRM 51-1-20D. FABRICATED NEW FRAME SEGMENT P/N 2645791 (7075"0" 0.071") IAW SRM 53-4-1 FIG 51 SHEET 21 ITEM Apr 8, 2007 · N806DH · Doug DC873F · Fuselage Main, FrameSDR DHL2007806546Skin · wornRT OTBD FLAP UPPER SKIN WORN STA XF 226.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-30-07, ASTAR DRAWING NR D857R1020 DATED 03-28-07. REMOVED EXISTING DAMAGED REPAIR SEGMENT AND INTERNAL SPLICE IAW SRM 51-1-21. FABRICATED NEW REPApr 8, 2007 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2007806555Skin · damagedRT WING CTR L/E LOWER SKIN HOLES ELONGATED STA XFS 526.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-06-07, ENGINEERING VARIATION AUTHORIZATION NR D857-00006 REV IR DATED 03-28-07. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED REPAApr 8, 2007 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2007806554Skin · damagedRT CTR L/E OTBD SLOT HOLES ELONGATED, STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-05-07, ENGINEERING VARIATION AUTHORIZATION NR D852-00003 DATED 03-18-07 REV IR. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTApr 8, 2007 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2007806597Skin · wornRT OTBD FLAP UPPER SKIN WORN STA XF 226.000 (MAJOR REPAIR.). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-30-07, ASTAR DWG NR D857R1020 DATED 03-28-07. REMOVED EXISTING DAMAGED REPAIR SEGMENT AND INTERNAL SPLICE IAW SRM 51-1-21. FABRICATED NEW REPAIRApr 8, 2007 · N806DH · Doug DC873F · Trailing Edge FlapsSDR DHL2007806538Frame · deformedMAIN CARGO COMPT FRAME DEFORMED STA 1580.000 L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-4-1 FIG 51. REMOVED DAMAGED FRAME SEGMENT IAW SRM 53-1-0 PG 1, SRM 51-1-20D. FABRICATED NEW FRAME SEGMENT P/N 2645791 (7075"0" 0.071") IAW SRM 53-4-1 FIG 51Apr 8, 2007 · N806DH · Doug DC873F · Fuselage Main, FrameSDR UPS07849744Cusp Web · crackedINSPECTION TYPE:C2, 6 INCH CRACK ON CUSP AT FS 1220 RIGHT SIDE FLOORBEAM FITTING L21R. REPAIRED CUSP AT STA 1133 - 1248 L21R IAW SAA EA008-5330-01-A0815, UPS RAA DC8-53-20622, SRM TR 53-180, AND FAA FORM 8100-9.Apr 7, 2007 · N805UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2007806505Fitting · crackedSTRUCTURE UNDER NR 3 CROSS SLIDE CARGO DOOR HAS A CRACKED FITTING STA 1180.000 L-28L. REMOVED AND REPLACED CRACKED FITTING AT STA 1180.000 L-28L, STRUCTURE UNDER NR 3 CROSS SLIDE CARGO DOOR IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE).Apr 5, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007806603Frame · damagedMAIN CARGO COMPT FRAME HAS A MISDRILLED HOLE STA 1680.000 L-21L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-30-07. REPAIR ORDER NR 2-50561-801 DATED 03-29-07 (ED-4504). PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. NOApr 5, 2007 · N806DH · Doug DC873F · Fuselage Main, FrameSDR DHL2007806544Frame · damagedMAIN CARGO COMPT FRAME HAS A MISDRILLED HOLE STA 980.000 L-12L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-30-07, REPAIR ORDER NR 2-50561-801 DATED 03-29-07 (ED4502). PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. NO CRAApr 5, 2007 · N806DH · Doug DC873F · Fuselage Main, FrameSDR DHL2007806537Cargo Track · wornFOUND UPPER CARGO COMPT NR 2 TRACK LUG WORN (STA 280.000 - 300.000). REMOVED WORN SEGMENT OF TRACK NR 2 AND EXISTING SPLICES IAW SRM 53-2-3, SRM 51-3-0, SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA AND EXISTING SPLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK Apr 5, 2007 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007806545Frame · damagedMAIN CARGO COMPT FRAME HAS A MISDRILLED HOLE STA 960.000 L-20L TO L-21L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-30-07, REPAIR ORDER NR 2-50561-801 DATED 03-29-07 (ED-4500). PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-00Apr 5, 2007 · N806DH · Doug DC873F · Fuselage Main, FrameSDR DHL2007806514Fitting · crackedFWD CARGO COMPT FITTING CRACKED 0.500", STA 320.000 L-26L TO L-27L. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE).Apr 5, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS07849594Skin · dentedCARGO DOOR DENT OUT OF SRM LIMITS. ACCOMPLISHED INTERIM REPAIR ACTIONS AS PER EO DC8-5230-26519. ACCOMPLISHED HFEC PER DC-8 NDTM 51-00-019. NO CRACKS FOUND. OK FOR CONTINUED SERVICE.Apr 5, 2007 · N809UP · Doug DC873F · Cargo/Baggage DoorsSDR DHL2007806525Floorbeam · damagedMAIN CARGO COMPT FLOORBEAM HAS A MISDRILLED HOLE, STA 600.000 RBL 38" (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 51-2-1 FIG 1, TR NR 51-130 DATED 01-26-04. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION IAW SRM 51-2-1 FIG 1, TR NR 51-130 SHEApr 4, 2007 · N806DH · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2007806527Fitting · crackedMAIN CARGO COMPT AFT FITTING CRACK 1" STA 902 125 L-19R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 PG 2A.Apr 4, 2007 · N806DH · Doug DC873F · Fuselage Main, Attach Fittings
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