Douglas DC-8-71F

Service difficulty reports · 8,938

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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 = 'DC871F'
  ORDER BY difficulty_date DESC"

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SDR IXXA060186OActuator · malfunctionedON TAKEOFF UNABLE TO KEEP AIRCRAFT ON CENTERLINE WITH RUDDER PEDALS. REJECTED TAKEOFF AT 90 KTS IN NOSE WHEEL STEERING RUDDER PEDALS VERY SLOW TO REACT. MAINTENANCE REMOVED AND REPLACED BOTH LT AND RT STEERING ACTUATORS RE-RIGGED SYSTEM AND OP CHECK OK. AIRMay 23, 2006 · N829BX · Doug DC871F · Landing Gear Steering SystemSDR UPS06847086Stiffener · crackedINSPECTION TYPE:C3 BROKEN STIFFENING ANGLE INSIDE LEFT CTR L/E, AT INBOARD END OF SLOT DOOR COVE, STA XW 408. REMOVED BROKEN STIFFENER AT STA XW 408 IAW SRM 51-3-0, FABRICATED AND INSTALLED STIFFENER AT STA XW 408 LEFT CTR L/E IAW DWG 3770673 AND SRM 51-01-20May 20, 2006 · N715UP · Doug DC871F · Wing Miscellaneous StructureSDR IXXA06SMN146SRepair · improperDURING ROUTINE C CHECK INSPECTION FOUND RIGHT HAND WING CENTER LEADING EDGE HAS NON STANDARD REPAIR FROM STATION XFS 310.250 TO STATION XFS 316.000. PERFORMED MAJOR REPAIR REMOVED IMPROPER REPAIR. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, ANMay 19, 2006 · N830BX · Doug DC871F · Wing, Plate/SkinSDR IXXA06SMN159SFinger Doubler · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT HAND HORIZONTAL STABILIZER RIGHT HAND ELEVATOR CENTER LOWER PANEL FINGER DOUBLER WITH SPOTS OF CORROSION, FROM STATION XE 132.750 TO STATION XE 251.562. PERFORMED MAJOR REPAIR IAW DC-8 SRM 55-4-1 FIGURE 1 SHEET 1,May 19, 2006 · N830BX · Doug DC871F · Horizontal Stabilizer, Plate/SkinSDR IXXA06SMN158SRepair · improperDURING ROUTINE C CHECK INSPECTION FOUND RUDDER LEADING EDGE LEFT HAND SKIN WITH NON STANDARD REPAIR AT STATION ZR 96.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 55-6-1 FIGURE 1. REMOVED EXISTING SKIN WITH NON STANDARD REPAIR IAW DC-8 SRM 51-1-21, DC-8 SRM 55-1-0May 19, 2006 · N830BX · Doug DC871F · Rudder, Plate/SkinSDR IXXA06SMN157SPanel · deformedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT HAND ELEVATOR LT UPPER PANEL DEFORMED, TRAILING EDGE BROKEN 2 INCHES AND DELAMINATED AT STATION 28.843. PERFORMED MAJOR REPAIR IAW DC-8 SRM 55-4-1 SHEET 1, AND 2. REMOVED DAMAGED PANEL IAW DC-8 SRM 55-1-0, DC-8 SRMay 19, 2006 · N830BX · Doug DC871F · Elevator, Plate/SkinSDR IXXA06SMN154SRepair · improperDURING ROUTINE C CHECK INSPECTION FOUND RUDDER LEADING EDGE LT SKIN WITH IMPROPER REPAIR AT STATION ZR 159.094. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIGURE 1. REMOVED SKIN WITH NON STANDARD REPAIR IAW SRM 51-1-21, DC-8 SRM 55-1-0 PAGE 1. FABRICATED NEW SKIN May 19, 2006 · N830BX · Doug DC871F · Rudder, Plate/SkinSDR IXXA06SMN153SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FORWARD PASSENGER DOOR SKIN WITH 03 CRACKS APPROXIMATELY ¾ INCH LONG. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NUMBER 06282 DATE 06-06-06, SEMAN DRAWING NUMBER ED 4238 DATED 06-03-06. REMOVED FASTENERS AS NEEDED TO REMOVE May 19, 2006 · N830BX · Doug DC871F · Passenger/Crew DoorsSDR IXXA06SMN150SDoor Frame · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT PASSENGER DOOR JAMB FORWARD UPPER CORNER CRACKED 1 INCH. PERFORMED MAJOR REPAIR IAW AD 2000-20-08, SB 53-075, DOUGLAS DRAWING SR 08530021, 5750776. REMOVED DAMAGED AREA IAW DOUGLAS DRAWING SR 08530021. PERFORMED NDMay 19, 2006 · N830BX · Doug DC871F · Fuselage Main, StructureSDR IXXA06SMN148SSpar Cap · corrodedDURING ROUTINE C CHECK INSPECTION, RUDDER LEFT HAND CAP CORRODED AT HINGE SUPPORT AT STATION ZR 103.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 55-6-1 FIGURE 2, SHEET 1, AND 3, DOUGLAS DRAWING 5655068. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17, 18. FOUND OUTMay 19, 2006 · N830BX · Doug DC871F · Rudder, Spar/RibSDR IXXA06SMN147SRepair · improperDURING ROUTINE C CHECK INSPECTION FOUND RIGHT HAND WING CENTER LEADING EDGE EXTERNAL HAS NON STANDARD REPAIR AT STATION XFS 297.750. REMOVED FASTENERS AS NEEDED TO REMOVE IMPROPER REPAIR. FABRICATED NEW REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED,May 19, 2006 · N830BX · Doug DC871F · Wing, Plate/SkinSDR IXXA06SMN145SSkin · crackedDURING ROUTINE C CHECK INSPECTION, RIGHT HAND WING CENTER LEADING EDGE EXTERNAL SKIN CRACKED AT STATION XF 283.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 55-6-1 FIGURE 2 SHEET 1, AND 3, DOUGLAS DRAWING NUMBER 5655068. REMOVED DAMAGE IAW DC8 SRM 51-1-8 PAGES 17,May 19, 2006 · N830BX · Doug DC871F · Wing, Plate/SkinSDR IXXA06SMN144SSkin · canningDURING ROUTINE C CHECK INSPECTION, RT ELEVATOR UPPER SKIN OIL CANNED, BETWEEN STATIONS XE 139.000 AND XE 252.000. PERFORMED MAJOR REPAIR IAW SRM 55-4-1 FIGURE 1 SHEET 1, AND 2. REMOVED DAMAGED SKIN, AND FINGER DOUBLER IAW SRM 51-1-21, SRM 55-1-0 PAGE 1. FABRMay 19, 2006 · N830BX · Doug DC871F · Elevator, Plate/SkinSDR IXXA06SMN166SSpar Cap · corrodedDURING ROUTINE C CHECK INSPECTION, RUDDER RIGHT HAND CAP CORRODED NEXT TO SUPPORT HINGE HOUSING AT STATION ZR 103.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 55-6-1 FIG. 2, DOUGLAS DRAWING NUMBER 5655068. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17, 18. FOUNDMay 19, 2006 · N830BX · Doug DC871F · Rudder, Spar/RibSDR IXXA06SMN165SRepair · improperDURING ROUTINE C CHECK INSPECTION, LEFT HAND INNER WING EXTENDED LEADING EDGE SLOT OUTER PLATING LOWER SIDE EXISTING REPAIR IMPROPER AT STATION XFS 341.500. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NUMBER 06245 DATE 05-22-06, SEMAN DRAWING NUMBER ED 4220 DAMay 19, 2006 · N830BX · Doug DC871F · Leading Edge DevicesSDR IXXA06SMN162SRepair · improperDURING ROUTINE C CHECK INSPECTION, UPGRADE REPAIR OF DENT ON FORWARD LOWER FUSELAGE PLATING AFT OF NLG WW RT AFT CORNERS AT STA 16, L35R IAW EO 53-DC8-2428. MAJOR REPAIR. COMPLETED FAA FORM 8110-3 NUMBER 06260 DATED 05-29-06, SEMAN DRAWING NUMBER ED 4231 DATEMay 19, 2006 · N830BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN151SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD AILERON LEADING EDGE SKIN DENTED, AND CRACKED AT STATION XA 475.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-8-1 FIG 1. REMOVED DAMAGED SKIN IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 51-1-21. FABRICATED May 19, 2006 · N830BX · Doug DC871F · AileronsSDR IXXA06SMN140SSkin · damagedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT HAND INBOARD FLAP DENTED AT SEVERAL SPOTS AND NON STANDARD REPAIR ON LOWER. SKIN BETWEEN STATIONS XW 2.000 AND XW 104.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-7-1 FIG 1. REMOVED DAMAGED SKIN IAW DC-8 SRM 57-1-May 19, 2006 · N830BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06SMN138SSkin · dentedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT HAND OUTBOARD FLAP LOWER SKIN DENTED AT STATION XF 440.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-7-1 FIG 4 TEMPORARY REVISION NUMBER 57-94 DATED 10-01-02. REMOVED DAMAGE IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 51-May 19, 2006 · N830BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06SMN164SSkin · misrepairedDURING INSPECT, FOUND LT INNER WING EXTENDED L/E SLOT OUTER SKIN EXISTING REPAIR IMPROPER AT STA XFS 310.000. PERFORMED MAJOR REPAIR. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21. REMOVED DAMAGED AREA IAW SEMAN DWG NR ED 4233. PERFORMED NDT INSPECTMay 19, 2006 · N830BX · Doug DC871F · Leading Edge DevicesSDR IXXA06SMN143SVane · elongatedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD SLOT VANE HOLES ELONGATED AT STATION XS 240.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NUMBER 06237 DATE 05-15-06, SEMAN DRAWING NUMBER ED 4211 DATE 05-10-06. REMOVED EXISTING REPAIR DOUBLER IAWMay 19, 2006 · N830BX · Doug DC871F · Leading Edge Slat Control SystemSDR IXXA06SMN141SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE EXT SKIN HAS A NON STANDARD REPAIR AT STATION 55.000, LONGERON 9 LEFT. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NUMBER 06245 DATED 05-22-06, SEMAN DRAWING NUMBER ED 4225 DATED 05-18-06. REMOVED NON STANDARDMay 19, 2006 · N830BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN160SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT HAND WING CENTER LEADING EDGE LOWER SKIN WITH NON STANDARD REPAIR AT STATION XOLDI 6.225. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 06242 DATE 05-18-06, SEMAN DRAWING NR ED 4224 DATE 05-10-06. REMOVED NON STAMay 19, 2006 · N830BX · Doug DC871F · Wing, Plate/SkinSDR IXXA06SMN156SDoubler · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND EXTERNAL FUSELAGE REPAIR DOUBLER IMPROPER, FROM STATION 1540.000 TO STATION 1560.000 BETWEEN LONGERONS 35 RIGHT TO LONGERON 35 LEFT. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7. REMOVED EXISTING REPAIR DOUBLER IAMay 19, 2006 · N830BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06SMN155SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE LOWER SKIN WITH NON STANDARD REPAIR AT STATION XFS 341.500. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NUMBER 06237 DATE 05-15-06, SEMAN DRAWING NUMBER ED 4217 DATE 05-10-06. REMOVED EXMay 19, 2006 · N830BX · Doug DC871F · Wing, Plate/SkinSDR IXXA06SMN152SSkin · misrepairedDURING C CHECK, FOUND LT WING CENTER LEADING LWR SKIN HAS NON STANDARD REPAIR AT STA XOLDL 6.225. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NUMBER 06237 DATE 05-15-06, SEMAN DRAWING NUMBER ED 4210 DATE 05-12-06. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM May 19, 2006 · N830BX · Doug DC871F · Wing, Plate/SkinSDR IXXA06SMN149SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT LOWER CARGO COMPARTMENT FITTING CRACKED BETWEEN STATION 1160.000 AND STATION 1170.000 LONGERON 35 RIGHT. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. FABRICATED NEW FITTING IAW ATI REPAIR SPECIFICATION NUMBER 200May 19, 2006 · N830BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA06SMN142SDoubler · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE INTERNAL SPLICE DOUBLER CRACKED AT STATION XOLDI 6.225. PERFORMED MAJOR REPAIR IAW BOEING MESSAGE NR 1-190592 951-3 DATE 05-12-06. REMOVED DAMAGED INTERNAL SPLICE DOUBLER IAW DC-8 SRM 57-May 19, 2006 · N830BX · Doug DC871F · Wing, Plate/SkinSDR IXXA06SMN163SSkin · damagedDURING C CHECK, FOUND RT OUTER WING INBD EXTENDED L/E OUTER SKIN LWR SIDE, 3 EXISTING DOUBLER REPAIRS BETWEEN XW 485.000 AND XFS 591.250. REMOVED EXISTING REPAIR DOUBLERS IAW DC-8 SRM 51-1-21. REMOVED DAMAGED AREA IAW SEMAN DRAWING NUMBER ED 4228. PERFORMEDMay 19, 2006 · N830BX · Doug DC871F · Leading Edge DevicesSDR IXXA06SMN139SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT OUTBOARD FLAP LOWER SKIN DENTED AT STATION XF 360.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-7-1 FIG 4 TR NR 57-94 DATE 10-01-02. REMOVED DAMAGED SKIN IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 51-1-21. FABRICATED NMay 19, 2006 · N830BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06SMN161SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CHANNEL CRACKED AT STATION 680.000 LBL 45. REMOVED CRACKED FITTING IAW DC-8 SRM 53--1-0 PAGE 1, DC-8 SRM 51-1-20D. FABRICATED NEW FITTING IAW ATI REPAIR SPECIFICATION NUMBER 2003-05. DWMay 19, 2006 · N830BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA06SMN137SSkin · wornDURING INSPECTION, FOUND EXT FUSELAGE C PIT BELLY DOOR EXTERNAL SKIN WORN. PERFORMED MAJOR REPAIR IAW DC-8 SRM 52-2-0 FIG 4 (SHEET 3). REMOVED FASTENERS IAW DC-8 SRM 51-1-2. REMOVED DAMAGED AREA IAW DC-8 SRM 52-2-0 FIG 4 (SHEET 3). PERFORMED DETAILED VISUAMay 19, 2006 · N830BX · Doug DC871F · Cargo/Baggage DoorsSDR IXXA06RNG048SSkin · corrodedDURING ROUTINE C CHECK, FOUND CORROSION ON HORIZONTAL STABILIZER UPPER SKIN LEADING EDGE FROM STATION XFS 178.00 TO STATION 203.750 TO THE RIGHT HAND REAR. DAMAGED AREA WAS CLEANED AND EXTERNAL DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 55-018.May 18, 2006 · N823BX · Doug DC871F · Horizontal Stabilizer, Plate/SkinSDR IXXA06SMN130SFitting · crackedDURING ROUTINE C CHECK INSPECTION FOUND MAIN CARGO COMPARTMENT FITTING CRACKED 1INCH FROM STATION 1100.000 TO STATION 1110.000 AT LONGERON 16 RIGHT. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. FABRICATED NEW FITTING IAW ATI REPAIR SPECIFICATION NUMBER 2003-May 11, 2006 · N830BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA06SMN120SRepair · improperDURING ROUTINE C CHECK INSPECTION, EXTERNAL FUSELAGE LEFT HAND FORWARD PASSENGER DOOR LOWER AFT JAMB CORNER HAS NON STANDARD REPAIR AT STATION 55.000 FROM LONGERON-20 LEFT TO LONGERON 22 LEFT. PERFORMED MAJOR REPAIR IAW AD 2000-20-08, SB DC8 53-075, DOUGLAS DMay 11, 2006 · N830BX · Doug DC871F · Fuselage Main, StructureSDR IXXA06SMN119SRepair · improperDURING ROUTINE C CHECK INSPECTION, EXTERNAL FUSELAGE LEFT HAND FORWARD PASSENGER DOOR UPPER FORWARD JAMB CORNER HAS NON STANDARD REPAIR AT STATION 25.000, FROM LONGERON-9 LEFT TO LONGERON 11 LEFT. PERFORMED MAJOR REPAIR IAW AD 2000-20-08, SB DC8 53-075, DOUGLMay 11, 2006 · N830BX · Doug DC871F · Fuselage Main, StructureSDR IXXA06SMN118SRepair · improperDURING ROUTINE C CHECK INSPECTION, EXTERNAL FUSELAGE LEFT HAND FORWARD PASSENGER DOOR UPPER AFT JAMB CORNER HAS NON STANDARD REPAIR AT STATION 55.000, FROM LONGERON-9 LEFT, TO LONGERON-11LEFT. PERFORMED MAJOR REPAIR IAW AD 2000-20-08, SB DC8 53-075, DOUGLAS DMay 11, 2006 · N830BX · Doug DC871F · Fuselage Main, StructureSDR IXXA06SMN109SDoor Frame · crackedDURING ROUTINE C CHECK INSPECTION, EXTERNAL FUSELAGE AFT PASSENGER DOOR LEFT HAND LOWER CORNER CRACKED 2". PERFORMED MAJOR REPAIR IAW AD 2000-20-08, SB DC8 53-075, DOUGLAS DRAWING SR 08530021, S750776. REMOVED EXISTING FASTENERS IAW DC8 SRM 51-1-2L, DC-8 SRM May 11, 2006 · N830BX · Doug DC871F · Fuselage Main, StructureSDR IXXA06SMN108SFitting · crackedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPARTMENT- AFT FITTING CRACKED 3",AT STATION 680.000, LONGERON 11 RIGHT. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D. FABRICATED NEW FITTING IAW ATI REPAIR SPECIFICATION NR 2003-05, DOUGLAS DRAWING NR 4751625.May 11, 2006 · N830BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA06SMN105SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, RIGHT HAND WING- INBOARD AILERON TRIM TAB UPPER AND LOWER SKIN DELAMINATED. CLEANED AND BONDED RIGHT HAND INBOARD AILERON TRIM TAB UPPER AND LOWER SKIN EDGE WITH HYSOL IAW DC8 SRM 51-1-9.May 11, 2006 · N830BX · Doug DC871F · Aileron TabsSDR IXXA06SMN125SSkin · crackedDURING ROUTINE C CHECK FOUND RIGHT HAND WING UPPER SKIN CRACKED AT STATION XRS 74.000 - 9.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-1 FIG 17. REMOVED FASTENERS IAW DC-8 SRM 51-1-20D. REMOVED DAMAGED AREA IAW DC-8 SRM 57-2-1 FIG 17. PERFORMED NDT INSPECMay 11, 2006 · N830BX · Doug DC871F · Wing, Plate/SkinSDR IXXA06SMN127SSkin · misrepairedDURING ROUTINE C CHECK, FOUND LEFT WING INBOARD FLAP UPPER PANEL HAS NON STANDARD REPAIR BETWEEN STATIONS XW 104.000 AND XW 115.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-7-1 FIG 1. REMOVED PANEL PLATING WITH NON STANDARD REPAIR IAW DC-8 SRM 57-1-0 PAGE 1, May 11, 2006 · N830BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06SMN122SSkin · misrepairedDURING ROUTINE C CHECK FOUND LEFT HAND WING INBOARD FLAP HAS NON STANDARD REPAIR AND DENTS FROM STATIONS XW 3.000 TO XW 92.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-7-1 FIG 1. REMOVED DAMAGED PANEL PLATING IAW DC-8 SRM 57-1-0, DC-8 SRM 51-1-21. FABRICATED NMay 11, 2006 · N830BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06SMN124SSkin · misrepairedDURING ROUTINE C CHECK FOUND LEFT HAND WING INBOARD FLAP PLATING HAS NON STANDARD REPAIR BETWEEN STATIONS XW 104.000 AND XW 122.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-7-1 FIG 1. REMOVED EXISTING PLATING WITH NON-STANDARD REPAIR IAW DC-8 SRM 57-1-0 PAGE May 11, 2006 · N830BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06SMN123SSkin · misrepairedDURING ROUTINE C CHECK FOUND LEFT HAND WING INBOARD FLAP PLATING HAS NON STANDARD REPAIR FROM STATIONS XW 122.000 TO XW 125.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-7-1 FIG 1. REMOVED EXISTING PLATING WITH NON-STANDARD REPAIR IAW DC-8 SRM 57-1-0 PAGE 1, DMay 11, 2006 · N830BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06SMN134SFitting · crackedDURING ROUTINE C CHECK INSPECTION FOUND FITTING CRACKED AT STATION 1766.000 LONGERON 17 RIGHT. REPLACED FITTING AT STATION 1766.000 LONGERON 17 RIGHT IAW DC8 SRM 51-1-21.May 11, 2006 · N830BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA06SMN136SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT BILGE INTERIOR SPLICE FITTING CRACKED FROM STATION 1040.000 STATION 1060.000 LONGERON 31 LEFT. REPLACED BILGE INTERIOR SPLICE FITTING FROM STATION 1040.000 TO STATION 1060.000 LONGERON 31 RIGHT IAMay 11, 2006 · N830BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA06SMN135SSplice · crackedDURING ROUTINE C CHECK INSPECTION FOUND AFT CARGO COMPARTMENT BILGE INTERIOR SPLICE FITTING CRACKED FROM STATION 1040.000 TO STATION 1060.000 LONGERON 31 RIGHT. REPLACED BILGE INTERIOR SPLICE FITTING FROM STATION 1040.000 TO STATION 1060.000 LONGERON 31 LEFT May 11, 2006 · N830BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA06SMN133SFrame · misdrilledDURING C CHECK, FOUND MAIN CARGO COMPT FRAME FLANGE HOLE MISDRILLED AT STA 200.000 BETWEEN LONGERONS 14 RT AND LONGERON 15 RT. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 06242 DATE 05-18-06, SEMAN DRAWING NR ED 4220 DATE 05-12-06. REMOVED DAMAGED CLIP, DCMay 11, 2006 · N830BX · Doug DC871F · Fuselage Main, FrameSDR IXXA06SMN132SIntercostal · crackedDURING ROUTINE C CHECK INSPECTION FOUND MAIN CARGO COMPARTMENT FORWARD INTERCOSTAL CRACKED 3 INCHES AT STATION 902.000 LONGERON 19 RIGHT. REMOVED CRACKED INTERCOSTAL IAW DC8 SRM 51-1-20D. FABRICATED NEW INTERCOSTAL IAW ATI REPAIR SPECIFICATION NUMBER 2003-05May 11, 2006 · N830BX · Doug DC871F · Fuselage Miscellaneous Structure
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