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 DHL2007801541Skin · corrodedAFT CARGO COMPT SKIN CORRODED STA 1200.000 L-36 TO L-35L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 11-15-07, EVA D853-00021 REV "B" DATED 11-15-07. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. Nov 18, 2007 · N801DH · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA07SMN272SSupport · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE INTERNAL PART SUPPORT HAS A CRACK AT STATION XFS 430.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SUPPORT. CLEANED, TREATED AND PRIMED AREA INSTALLED NEW SUPPORT INov 16, 2007 · N604BX · Doug DC873F · Wing, Attach FittingsSDR IXXA07SMN271SAttach Angle · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE TO STABILIZER LEFT ATTACH ANGLE SHOWS CORROSION AT STATION 1754.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGES AREA. FABRICATED ANGLE. PERFORMED HEAT TREATMENT TO ANGLE. CLEANED, TREATED ANDNov 16, 2007 · N604BX · Doug DC873F · Empennage Flight Control Surfaces, Attach FittingsSDR IXXA07SMN270SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT RUDDER RIGHT SKIN AT STATION ZR 253.000 TO STATION ZR 271.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLER, BONDED PANov 16, 2007 · N604BX · Doug DC873F · Rudder, Plate/SkinSDR IXXA07SMN269SStructure · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING. NUMBER 4 STUB WING LEADING EDGE LOWER PART DOUBLER HAS A CRACK AT STATION XFS 529.000. REMOVED FASTENERS AS NEEDED TP PERFORM REPAIR. REMOVED CRACKED DOUBLER. FABRICATED EXTERNAL, INTERNAL REPAIR DOUBLER.Nov 16, 2007 · N604BX · Doug DC873F · Wing Main, Frame StructureSDR IXXA07SMN268SSupport · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE INTERNAL PART SUPPORT CRACKED AT STATION XFS 430.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SUPPORT. FABRICATED SUPPORT CLEANED, TREATED AND PRIMED AREA AND NEWNov 16, 2007 · N604BX · Doug DC873F · Wing Miscellaneous StructureSDR UPS07851189Battery Pack · dischargedFOUND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK AND OPS CK IAW MM 33-50-01.Nov 16, 2007 · N811UP · Doug DC873F · Emergency LightingSDR IXXA07SMN266SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT RUDDER RIGHT HAND SKIN AT STATION ZR 115.000 TO STATION ZR 150.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKINS AND INTERNAL AND EXTERNAL DOUBLERS. Nov 15, 2007 · N604BX · Doug DC873F · Rudder, Plate/SkinSDR IXXA07SMN265SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT RUDDER RIGHT SKIN AT STATION ZR 150.000 TO STATION ZR 178.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKINS AND INTERNAL AND EXTERNAL DOUBLERS. BONDENov 15, 2007 · N604BX · Doug DC873F · Rudder, Plate/SkinSDR IXXA07SMN264SVane · damagedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE OUTBOARD VANE WITH ELONGATED HOLES AT STATION XOLDO 67.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION NOTED. Nov 15, 2007 · N604BX · Doug DC873F · Trailing Edge FlapsSDR IXXA07SMN263SSkin · damagedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE UPPER SKIN WITH MISDRILLED HOLES AT STATION XW 408.343. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND RENov 15, 2007 · N604BX · Doug DC873F · Wing, Plate/SkinSDR IXXA07SMN262SVane · damagedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE OUTBOARD VANE WITH ELONGATED HOLES AT STATION XOLDI 6.224. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION NOTED. Nov 15, 2007 · N604BX · Doug DC873F · Trailing Edge FlapsSDR IXXA07SMN261SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT BELLY PIT CRACKED FITTING AT STATION 1230.000 LONGERON-32 RIGHT. REMOVED CRACKED FITTING. FABRICATED FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION NOTED. CLEANED, TREATED AND PRIMED AREA AND FITTINGNov 15, 2007 · N604BX · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA070064SFitting · dentedDURING ROUTINE C CHECK INSPECTION, FOUND AFT BELLY PIT INTERNAL STRUCTURE FITTING UNDER CROSS SLIDE DOOR CRACKED AT STATION 1180.000 AROUND LONGERON-34 RIGHT. REMOVED CRACKED INTERNAL STRUCTURE FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, AND 51-3-1.Nov 15, 2007 · N604BX · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA07SMN260SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT BELLY PIT INTERNAL STRUCTURE FITTING UNDER CROSS SLIDE DOOR CRACKED AT STATION 1180.000 AROUND LONGERON-33 RIGHT. REMOVED CRACKED INTERNAL STRUCTURE FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, AND 51-3-1.Nov 15, 2007 · N604BX · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA07SMN259SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE WITH DENT AT STATION XFS 242.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA, REPAIR PARTSNov 15, 2007 · N604BX · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR IXXA07SMN258SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE HAS A IMPROPER REPAIR AT STATION XFS 178.750. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACNov 15, 2007 · N604BX · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR IXXA07SMN256SFrame · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT HAS A IMPROPER REPAIR AND DENT ON FRAME AT STATION 1580.000 LONGERON-20 RIGHT REMOVED FASTENER AS NEEDED TO PERFORM REPAIR. REMOVED FRAME SEGMENT WITH EXISTING REPAIR. FABRICATED FRAME SEGMENT, Nov 15, 2007 · N604BX · Doug DC873F · Fuselage Main, FrameSDR IXXA070063SFrame · dentedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT HAS A IMPROPER REPAIR AND DENT ON FRAME AT STATION 1580.000 LONGERON-21RIGHT REMOVED FASTENER AS NEEDED TO PERFORM REPAIR. REMOVED FRAME SEGMENT WITH EXISTING REPAIR. FABRICATED FRAME SEGMENT, ANov 15, 2007 · N604BX · Doug DC873F · Fuselage Main, FrameSDR IXXA07SMN247SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT "B" DOOR OUTER SKIN HAS A CRACK, WEAR DAMAGE, AND SEVERAL DENTS AT STATION 480.000 TO STATION 560.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKINov 15, 2007 · N604BX · Doug DC873F · Cargo/Baggage DoorsSDR IXXA07SMN257SFitting · damagedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT MISSDRILLED HOLE ON FLANGE OF FRAME FITTING AT STATION 879.000 LONGERON-21 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PLUGGED MISDRILLED HOLE WITH RIVET. PERFORMED NDT INSPECTION. NONov 15, 2007 · N604BX · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA070061SFrame · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT HAS A IMPROPER REPAIR AND DENT ON FRAME AT STATION 240.000 LONGERON-21 RIGHT. REMOVED FASTNER AS NEEDED TO PERFORM REPAIR.REMOVED EXISTING REPAIR.FABRICATED FRAME SEGMENT, SPLICE AND ANGLE.PERFORMNov 15, 2007 · N604BX · Doug DC873F · Fuselage Main, FrameSDR IXXA07SMN255SFrame · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT HAS A IMPROPER REPAIR AND DENT ON FRAME AT STATION 240.000 LONGERON 20 RIGHT. REMOVED FASTENER AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED FRAME SEGMENT, SPLICE AND ANGLE. Nov 15, 2007 · N604BX · Doug DC873F · Fuselage Main, FrameSDR IXXA070060SSkin · crackedDURING ROUTINE C CHECK INSPECTION, NOSE SECTION FUSELAGE FREON EXHAUST SYSTEM FORWARD UPPER CORNER CRACKED AT STATION FS 40.000 LONGERON 28 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED EXTERNAL REPAIR DOUBLER, AND FINov 15, 2007 · N604BX · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA07SMN254SSkin · crackedDURING ROUTINE C CHECK INSPECTION, NOSE SECTION FUSELAGE FREON EXHAUST SYSTEM FORWARD UPPER CORNER CRACKED AT STATION FS 40.000 L27L. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR.REMOVED DAMAGED AREA.FABRICATED EXTERNAL REPAIR DOUBLER , AND FILLER. CLEANED, Nov 15, 2007 · N604BX · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA07SMN253SFrame · dentedDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT FRAME WITH DENT AND MISDRILLED AT STATION 200.000 LONGERON31 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED FRAME SEGMENT. FABRICATED FRAME SEGMENT ANGLE AND SPLICE. PNov 15, 2007 · N604BX · Doug DC873F · Fuselage Main, FrameSDR IXXA07SMN252SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE SPLICE FITTING CRACKED AT STATION 1766.000 LONGERON 17 RIGHT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, 51-3-0, 51-3-1. Nov 15, 2007 · N604BX · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA07SMN251SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE A CRACK AT SPLICE FITTING AT STATION 1766.000 LONGERON17 LEFT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-3-0, 51-3-1.Nov 15, 2007 · N604BX · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA07SMN250SSkin · crackedDURING ROUTINE C CHECK INSPECTION, AFT FUSELAGE FOUND A CRACK AT LONGERON 17 RIGHT AT STATION 1769.000. REMOVED CRACKED LONGERON. FABRICATED LONGERON. CLEANED, TREATED AND PRIMED AREA AND NEW LONGERON. INSTALLED NEW LONGERON IAW DC8 SRM 51-1-11, 51-3-1, DCNov 15, 2007 · N604BX · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA07SMN249SSkin · crackedDURING ROUTINE C CHECK INSPECTION, AFT FUSELAGE FOUND A CRACK AT LONGERON 17 LEFT AT STATION 1769.000. REMOVED CRACKED LONGERON. FABRICATED NEW LONGERON. CLEANED, TREATED AND PRIMED AREA AND NEW LONGERON. INSTALLED NEW LONGERON IAW DC8 SRM 51-1-11, 51-1-21Nov 15, 2007 · N604BX · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA07SMN248SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, LEFT HORIZONTAL STABILIZER LEADING EDGE UPPER SKIN SHOWS CORROSION AT STATION XFS 177.750. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECNov 15, 2007 · N604BX · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR IXXA07SMN246SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND IN MAIN CARGO COMPARTMENT A CRACKED FITTING BETWEEN STATION 960.000 AND STATION 980.000 RIGHT BOTTOM LINE 25". REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, AND DC8 SRM 51-3-1. Nov 15, 2007 · N604BX · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS07851177Slide · dislodgedINSPECTION TYPE:N/A THE MAIN ENTRY DOOR EMERGENCY ESCAPE SLIDE NEEDS TO BE ADJUSTED IN THE HOLDING CASE AS IT APPEARS TO BE SLIDING OUT AND IT IS DIFFICULT TO READ SLIDE PRESSURE. REPOSITIONED MAIN ENTRY DOOR EVACUATION SLIDE IN CONTAINER AND RE-INSTALLED W/RNov 15, 2007 · N819UP · Doug DC873F · Escape SlideSDR DHL2007801539Skin · crackedNR 4 ENG NACELLE INLET COWL LT EXTERNAL SKIN CRACKED 1" STA YN 132.000 AT 9 O'CLOCK POS. (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 10-16-07, EVA B271-00015 REV IR DATED 10-12-07. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-21A, CUT OUTNov 14, 2007 · N801DH · Doug DC873F · Nacelle/Pylon, Plate/SkinSDR DHL2007801533Skin · damagedITEM REF. NR. 101138: UPPER RUDDER T/E BROKEN AT STA ZR 335.250 (FIBERGLASS) DAMAGE CAUSED BY SEMAN. STAGGERED CUT BACK BY A/2" TO A INCH PER PLY FROM THE CRACK THROUGH ALL DAMAGED PLIES OF THE CLOTH IAW SRM 51-1-19 PG 3. REPLACED THE CUT OUT CLOTH WITH A NENov 14, 2007 · N801DH · Doug DC873F · Wing, Nacelle/Pylon Attach FittingsSDR DHL2007801526Skin · delaminatedRT WING LWR T/E PANEL INTERNAL/EXTERNAL SKIN DELAMINATED (STA XF 409.000 - XRS 456.000). REMOVED AND REPLACED RT WING T/E LWR PANEL (STA XF 409.000 - XRS 456.000) IAW SRM 51-3-0, SRM 51-3-1.Nov 14, 2007 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL2007801538Skin · crackedLT WING MAIN TANK NR 1 LWR SIDE CRACKED 1" STA XRS 84.000 S-59. PERFORMED MAJOR REPAIR IAW MSG NR 1-654248500-2 DATED 10-19-07, SRM 57-2-2 FIG 3D SHEET 1, 2, 3, TR NR 57-86 DATED 05-15-01. REMOVED EXISTING CLIPS AND CUT OUT DAMAGED STRINGER SEGMENT IAW MSG NNov 14, 2007 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL2007801535Frame · crackedMAIN CARGO COMPT FRAME SEGMENT CRACKED 5" STA 240.000 L20R TO L21R. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG. 2 SHEET 2.6. REMOVED DAMAGED FRAME SEGMENT, SPLICES AND EXISTING ANGLES IAW SRM 51-1-20D. FABRICATED NEW FRAME SEGMENT P/N S2537716 IAW SRM 53-2-0Nov 14, 2007 · N801DH · Doug DC873F · Fuselage Main, FrameSDR DHL2007801536Skin · corrodedAFT ACCY COMPT SKIN CORRODED STA 1690.000 - 1700.000 L-30L TO L-32R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 11-13-07, ENGINEERING VARIATION AUTHORIZATION NR D853-00024 REV IR DATED 11-06-07. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. REMOVEDNov 13, 2007 · N801DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2007801534Structure · damagedINSPECT REPAIR AT FUSELAGE STA 280 LONGERON 29R PER INSPECTION REQUIREMENTS OF DC8 SRM 53-2-1 CLASS II TYPE REPAIR. REPAIR ACCOMPLISHED AUG 94. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 11-12-07, ENGINEERING VARIATION AUTHORIZATION NR D853-00023 REVNov 12, 2007 · N801DH · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA07SMN267SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT RUDDER RIGHT AT STATION ZR 87.000 TO STA ZR 115.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING PAIR. FABRICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLER. BONDED PARTS AS NEEDENov 11, 2007 · N604BX · Doug DC873F · Rudder, Plate/SkinSDR DHL2007801528Structure · damagedLT INNER WING OUTBD EXTENDED LEADING EDGE SLOT LWR PLATING ELONGATED HOLES AT STA XILD 42.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 11-12-07, ENGINEERING VARIATION AUTHORIZATION NR D857-00020 REV IR DATED 10-20-07. REMOVED FASTENERSNov 11, 2007 · N801DH · Doug DC873F · Leading Edge DevicesSDR IXXA070062SSkin Panel · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LOWER FUSELAGE NOSE SECTION HAS IMPROPER REPAIR AT STATION 165.000 TO STATION 70.000 LONGERON 31 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKINS AND INTERNAL DOUBLERNov 10, 2007 · N604BX · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA07SMN233SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LOWER FUSELAGE NOSE SECTION HAS IMPROPER REPAIR AT STATION 165.000 TO STATION 70.000 LONGERON 31 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKINS AND INTERNAL DOUBLERNov 10, 2007 · N604BX · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA07SMN245SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND IN MAIN CARGO COMPARTMENT A CRACKED FITTING AT STATION 781.500 LEFT BOTTOM LINE 25". REMOVED CRACKED FITTING.CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-3-0, 51-1-20D, 51-3-1, DC8 SRM 51-3-0, Nov 10, 2007 · N604BX · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA07SMN244SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND IN MAIN CARGO COMPARTMENT A CRACKED FITTING AT STATION 702.875 RIGHT BOTTOM LINE 25". REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-3-0, DC8 SRM 51-1-8B, DC8 SRM 51-1Nov 10, 2007 · N604BX · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA07SMN243SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND IN MAIN CARGO COMPARTMENT A CRACKED FITTING AT STATION 822.500 RIGHT BOTTOM LINE 25". REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, 51-3-1,DC8 SRM 51-1-20D, SRNov 10, 2007 · N604BX · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA07SMN242SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOIND IN MAIN CARGO COMPARTMENT A CRACKED FITTING AT STATION 798.000 LEFT BOTTOM LINE 25". REMOVED CRACKED FITTING. FABRICATED FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED Nov 10, 2007 · N604BX · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA07SMN241SSkin · crackedDURING ROUTINE C CHECK INSPECTION, EXTERNAL SKIN SHOWS CRACK AT STATION FS 1750.000 LONGERON 15 LEFT. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER INTERNAL FINGER DOUBLER. PERFORMED NDT INSPECTION. NO CRACK NO CORROSION FOUND. CLEANED, TREATED AND PRIMENov 10, 2007 · N604BX · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA07SMN240SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT FUSELAGE NOSE SECTION ACS MODIFICATION DOUBLER HEAT INTERCHARGER COMPARTMENT LOWER AFT JAMB CORNER DAMAGE AT STATION FS 12.000 LONGERON 27 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED ARNov 10, 2007 · N604BX · Doug DC873F · Fuselage Main, Plate/Skin
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