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 IXXA05SMN263SSkin Panel · misrepairedDURING C CHECK INSPECTION, EXT FS NON STANDARD REPAIR, STA 8.000 STA 17.000 BTWN L-15 AND L-16L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05447 DATED 10-05-05, SEMAN DWG # ED-4077 DATED 10-01-05 AND EO SEMAN # 20051295 DATED 10-05-05. REMOVED EXISTING DOct 13, 2005 · N829BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN262SSkin · improperDURING ROUTINE C CHECK INSPECTION, FWD FUSELAGE CTR LWR PLATING AFT OF FWD BASKET DOOR EXISTING REPAIR ALL SIDES EXCEED MAXIMUM RIVETS SPACING AT STA FS 360.000 L-36. INSTALLED HILOKS IAW FAA FORM 8110-3 # 05448 DATE 10-05-05, SEMAN DWG ED 4080 DATE 10-03-05 Oct 13, 2005 · N829BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN260SDoubler · corrodedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT MLG W/W PRESSURE PANEL DOUBLER CORRODED, STA 880.000 RBL 2’. REMOVED CORROSION FROM DOUBLER IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PG 2P. REMOVED CORRODED DOUBLER IAW DC8 SRM 51Oct 13, 2005 · N829BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN259SDoor · crackedDURING C CHECK INSPECT, LT FUSE NOSE SECTION PLATING FREON SYS EXHAUST DOOR UPPER AFT JAMB CORNER CRACK DAMAGE AT STA FS 54.000, L-28L TO L-29L. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 13. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-3-0. REMOVED DAOct 13, 2005 · N829BX · Doug DC871F · Service DoorsSDR IXXA05SMN258SFastener · improperDURING C CHECK INSPECT, EXTERNAL FS REPAIR FASTENERS IMPROPER AND RIVETS EXCEED ALLOWABLE LIMITS, STA 180.000 L-19R. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN 20051309 DATED 09-29-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 Oct 13, 2005 · N829BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN257SDoubler · unknownDURING C CHECK INSPECT, LT FUS AFT CTR SECTION LWR PLATING DOUBLER UPGRADE THICKNESS AT STA FS 1356.00 L-29 RT. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN NR 20051303 DATED 09-29-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21. REMOVEOct 13, 2005 · N829BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN256SRepair · improperDURING ROUTINE C CHECK INSPECTION, LT FUSELAGE AFT CENTER SECTION WINDOW BELT EVALUATE CONFORMITY PER SRM AT STA FS 1250.00 L-15.5 LT. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 22A, TR # 53-170, EO SEMAN # 20051302 DATED 09-28-05. REMOVED EXISTING REPAIROct 13, 2005 · N829BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN255SRepair · improperDURING C CHECK INSPECTION, LT FUSELAGE FWD CENTER SECTION WINDOW BELT EVALUATE CONFORMITY PER SRM AT STA FS 245.00 L-15.5 LT. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 22A, TR # 53-170, EO SEMAN # 20051301 DATED 09-28-05. REMOVED EXISTING REPAIR DOUBLER Oct 13, 2005 · N829BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN254SRepair · improperDURING C CHECK INSPECT, RT FUSELAGE AFT CENTER SECTION FWD OF R-2 DOOR OPENING EVALUATE CONFORMITY PER SRM AT STA FS 1550.00 L-15.5 RT. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 22A, EO SEMAN NR 20051300 DATED 09-28-05. REMOVED EXISTING REPAIR DOUBLER IAOct 13, 2005 · N829BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN253SDoubler · improperDURING C CHECK INSPECT, LT FUS FWD CTR SECTION LWR PLATING BASKET DOOR FWD JAMB EXISTING REPAIR DBLR NOT ACCOMP 3 ROWS FASTENERS PAST CUT OUT STA FS 279.000 L-35.5L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05461. REMOVED EXISTING REPAIR DOUBLER IAW DCOct 13, 2005 · N829BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN244SVane · damagedDURING C CHECK INSPECT, RT WING INNER L/E SLOT VANE HAS ELONGATED HOLES AT STA XOLDO 67.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05463. REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PAROct 13, 2005 · N829BX · Doug DC871F · Trailing Edge FlapsSDR IXXA05SMN252SRepair · misinstalledDURING C-CHECK INSPECT, RT FUSE FWD CTR SECTION LWR PLATING FWD OF A PIT DOOR EXISTING DBLR EXCEED MAX RIVETS SPACING AT BS 272.00 L-31R. PERFORMED MAJOR REPAIR IAW FORM 8110-3 NR 05451, SEMAN DWG NR ED-4078, EO SEMAN 20051296. REMOVED REPAIR DOUBLER IAW DC8Oct 13, 2005 · N829BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN251SSkin Panel · brokenDURING C CHECK INSPECTION, LT FUSELAGE NOSE SECTION LWR PLATING UPPER AFT CORNER BROKEN OFF AT BS 70 L-33. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-2 FIG 8C-2, TR NR 53-176, EO SEMAN NR 20051299 DATED 09-29-05. PERFORMED DETAIL VISUAL INSPECT. NEITHER CRACK Oct 13, 2005 · N829BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN249SRepair · misinstalledDURING C-CHECK INSPECT, LT NOSE SKIN FWD PAX DOOR JAMB EXISTING DBLR EXCEED OVERAGE RIVETS SPACING AND CHERRY MAX AT STA FS 24 L-36 LT. PERFORMED MAJOR REPAIR IAW FORM 8110-3, SEMAN DWG ED-4077 DATED 10-01-05 AND EO SEMAN 20051295 DATED 10-05-05. REMOVED EXIOct 13, 2005 · N829BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN248SRivet · out of toleranceDURING C CHECK INSPECT, LT FUSELAGE NOSE SECTION PLATING DOUBLER REPAIR EXCEED MAX RIVETS SPACING STA FS 10 L-22 LT. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05448 DATED 10-05-05, SEMAN DWG # ED 4076 DATED 10-03-05, EO SEMAN # 20051294 DATED 10-05-05. REOct 13, 2005 · N829BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN247SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, LEFT WING NR 2 MAIN TANK FITTING CRACKED, FS 74.000 S.51 (FWD INTERNAL PART). REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. CLEANED AND APPLIED POLYURETHANE TOP COATING YELLOW IAW DC8 SRM 51-1-12 PAGES 7-25. INSTALLED NEW Oct 13, 2005 · N829BX · Doug DC871F · Wing, Attach FittingsSDR IXXA05SMN246SFitting · crackedDURING ROUTINE C CHECK INSPECTION, LT WING NR 2 MAIN TANK FITTING CRACKED, FS 74.000 S.51 (FWD EXTERNAL PART). REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. CLEANED AND APPLIED POLYURETHANE TOP COATING YELLOW IAW DC8 SRM 51-1-12 PAGES 7-25. INSTALLED NEW FIOct 13, 2005 · N829BX · Doug DC871F · Wing, Attach FittingsSDR IXXA05SMN245SFitting · improperDURING ROUTINE C-CHECK INSPECTION, RIGHT MLG W/W - L-24R FITTING HAS NO STANDARD REPAIR AT STA 879.375. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 8. REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-20D. FABIRCATED (4) REPAIR FITTING (P/N 5802677-4) FROM AL7Oct 13, 2005 · N829BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA05SMN243SVane · elongatedDURING ROUTINE C CHECK INSPECTION, RT WING CTR L/E SLOT VANE HAS ELONGATED HOLES AT STA XILD 7095. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05461 DATED 10-10-05, SEMAN DWG NR ED-4081 DATED 10-08-05, EO SEMAN NR 20051290 DATED 10-10-05. REMOVED FASTENERSOct 13, 2005 · N829BX · Doug DC871F · Trailing Edge FlapsSDR IXXA05SMN242SSkin Panel · improperDURING C CHECK INSPECT, LT MLG W/W - L-24L HAS NO STANDARD REPAIR BETWEEN BS 960.000 & 980.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-2 FIG 5, TR NR 53-123, EO SEMAN NR 20051282 DATED 09-27-05. REMOVED EXISTING REPAIR IAW DC8 SRM 51-1-20D. STOP DRILLED CROct 13, 2005 · N829BX · Doug DC871F · Fuselage Main, KeelSDR IXXA05SMN241SDoubler · crackedDURING ROUTINE C CHECK INSPECTION, RT INNER WING CTR L/E INTERNAL DOUBLER CRACK 3 AT STA XFS 250.000. REMOVED CRACKED INTERNAL DOUBLER IAW DC8 SRM 51-1-21. FABRICATED NEW INTERNAL DOUBLER (AL7075T6 0.063”) IAW DC8 SRM 57-3-1 FIG 3. CLEANED, TREATED, PRIMED Oct 13, 2005 · N829BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN240SPan · crackedDURING ROUTINE C CHECK INSPECTION, RT INNER WING OUTBD L/E ZEE PAN CRACK 2” AT STA XS 250.089. REMOVED CRACKED SPLICE PAN IAW DC8 SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW SPLICE PAN IAW DC8 SRM 51-1-21, DC8 SRM 51-1-2Oct 13, 2005 · N829BX · Doug DC871F · Wing Miscellaneous StructureSDR IXXA05SMN239SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LT HORIZONTAL STABILIZER L/E UPPER SKIN DENTED, XFS 78.750 XFS 85.00. PERFORMED MAJOR REPAIR IAW DC8 SRM 55-2-1 FIG 4, EO SEMAN # 20051292 DATED 09-27-05. REMOVED EXISTING REPAIR DOUBLER NEXT DENT IAW DC8 SRM 51-1-21. REMOOct 13, 2005 · N829BX · Doug DC871F · Horizontal Stabilizer, Plate/SkinSDR IXXA05SMN238SDoubler · crackedDURING ROUTINE C-CHECK INSPECTION, LEFT WING CTR L/E LWR INTERNAL DOUBLER CRACK 2 AT STA XFS 342.500. REMOVED CRACKED INTERNAL DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. FABRICATED NEW INTERNAL DOUBLER (AL7075T6 0.090”) IAW DC8 SRM 57-3-1 FIG 4. CLEANEDOct 13, 2005 · N829BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN237SDoubler · crackedDURING C CHECK INSPECTION, LT WING CTR L/E LWR PART INTERNAL DOUBLER CRACKED 7, XFS 341.500. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05463 DATED 10-11-05, SEMAN DWG # ED-4083 DATED 10-10-05, EO SEMAN # 20051312 DATED 10-11-05. REMOVED EXISTING REPAIR DOct 13, 2005 · N829BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN236SSkin · improperDURING C CHECK INSPECTION, RT OTBD FLAP UPPER SKIN HAS NON STANDARD REPAIR, STA XF 210.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 4, TR#57-94, EO SEMAN # 20051288 DATED 09-28-05. REMOVED DAMAGED PLATING IAW DC8 SRM 57-1-0, DC8 SRM 51-1Oct 13, 2005 · N829BX · Doug DC871F · Wing StructureSDR IXXA05SMN235SSkin · improperDURING C CHECK INSPECTION, RT OTBD FLAP UPPER SKIN HAS NON STANDARD REPAIR, STA XF 230.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05447 DATED 10-05-05, SEMAN DWG # ED 4072 DATED 10-01-05, EO SEMAN # 20051298 DATED 10-05-05. REMOVED EXISTING NON STANDAROct 13, 2005 · N829BX · Doug DC871F · Leading Edge DevicesSDR IXXA05SMN234SSkin · improperDURING C CHECK INSPECTION, RT WING INBD FLAP UPPER SKIN HAS NON STANDARD REPAIR. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 1, EO SEMAN NR 20051279 DATED 09-26-05. REMOVED DAMAGED PLATING IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 51-1-21. FABRICATED NEW PLATING (Oct 13, 2005 · N829BX · Doug DC871F · Leading Edge DevicesSDR IXXA05SMN233SSkin · improperDURING C CHECK INSPECTION, LT OTBD FLAP UPPER SKIN HAS NON STANDARD REPAIR, XW 435.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 1, EO SEMAN # 20051210 DATED 09-21-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW DOct 13, 2005 · N829BX · Doug DC871F · Leading Edge DevicesSDR IXXA05SMN232SDoubler · improperDURING ROUTINE C-CHECK INSPECTION, LEFT INBOARD FLAP L/E UPPER SKIN HAS NON STANDARD REPAIR, XW 105.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1, EO SEMAN 20051209. REMOVED DAMAGED PANEL PLATING IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 51-1-21. FABOct 13, 2005 · N829BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN231SSkin · improperDURING C CHECK INSPECT, LT INBD FLAP L/E UPPER SKIN HAS NON STANDARD REPAIR, XW 91.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05446 DATED 10-05-05, SEMAN DWG # ED 4065 DATED 09-27-05, EO SEMAN # 20051208 DATED 10-05-05. REMOVED NON STANDARD REPAIR IAWOct 13, 2005 · N829BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN230SSkin · dentedDURING C CHECK INSPECT, LT INBD FLAP UPPER SKIN DENTED, XW 77.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 1, EO SEMAN #20051207 DATED 09-21-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED SECOct 13, 2005 · N829BX · Doug DC871F · Wing, Plate/SkinSDR IXXA05SMN229SRivet · improperDURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1544.000 L-35.5L, UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN # 20051200 DATED 09-20-05. REMOVED EXISTING REPOct 13, 2005 · N829BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN228SRivet · improperDURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1693.000 L-30.75L. UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN # 20051203 DATED 09-20-05. REMOVED EXISTING REOct 13, 2005 · N829BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN227SRivet · improperDURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1693 L-30.75R. UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN # 20051202 DATED 09-20-05. REMOVED EXISTING REPAIROct 13, 2005 · N829BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN226SRivet · improperDURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1384.000 L-35-75R, UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN # 20051199 DATED 09-20-05. REMOVED EXISTING REOct 13, 2005 · N829BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN225SRivet · improperDURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1254.000 L-35.5R, UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN NR 20051198 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLER IAOct 13, 2005 · N829BX · Doug DC871F · Aircraft StructuresSDR IXXA05SMN224SRivet · improperDURING C CHECK INSPECT, FWD LWR FUSELAGE BELLY, STA FS 222 L-34.75R. UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN NR 20051194 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLER IAW DOct 13, 2005 · N829BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA05SMN223SRivet · improperDURING C CHECK INSPECT, FWD LWR FUSELAGE BELLY, FS 104 L-35.75L, UPGRADE EXTERNAL DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN NR 20051192 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 Oct 13, 2005 · N829BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0500213SFitting · crackedDURING ROUTINE C-CHECK FOUND LONGERON 34 LEFT AT STATION 690 TO 778 CORRODED. REMOVED CORROSION, TREATED AND PRIMED. DURING CORROSION REMOVAL FOUND FITTING CRACKED AT LONGERON 34 LEFT STATION 765 TO 778. FABRICATED NEW FITTING, LOCATED, DRILLED, TREATED, PROct 8, 2005 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS05845559Ground Wire · shortedCARGO SMOKE LIGHT ILLUMINATED - ALL POSITIONS. T/S SYS FOUND & REPAIRED BAD GROUND WIRE 8M OHMS ON SMOKE DETECTOR UNIT NR 1. FOUND & REPAIRED BAD GND WIRE ON SDU NR 3. FOUND AND REPAIRED BAD GNU D WIRE ON SDU NR 5. ALL OTHER SDU GND WIRES CKD GOOD PER WDM 26Oct 7, 2005 · N750UP · Doug DC871F · Fire Protection System WiringSDR UPS05845558Battery Pack · weakEMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD PER AMM 33-50-01-2.Oct 6, 2005 · N703UP · Doug DC871F · Emergency LightingSDR UPS05845557Escape Rope · deployedCAPT SIDE ESCAPE ROPE DEPLOYED, COVER WON'T STAY ON. STOWED ESCAPE ROPE AND PROPERLY INSTALLED COVER ASSY. OK FOR SERVICE.Oct 6, 2005 · N729UP · Doug DC871F · Emergency EquipmentSDR IXXA0500229SFrame · corrodedDURING ROUTINE C-CHECK FOUND FRAME CORRODED AT STATION 1260 LONGERON 33 RIGHT TO LONGERON 34 RIGHT. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 51-2-1, 53-4-1, 51-1-4, 51-1-5 AND 51-1-8.Oct 5, 2005 · N825BX · Doug DC871F · Fuselage Main, FrameSDR IXXA060078SWeb · crackedDURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE FORWARD BULKHEAD UPPER WEB CRACKED AT STATION -165 BETWEEN +X17 AND +Z23. REMOVED DAMAGED AREA. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED DOUBLER, AND FASTENERS AT STATION -165 FOct 3, 2005 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA0500222SSupport · corrodedDURING ROUTINE C-CHECK FOUND SUPPORT CORRODED AT STATION 300 LONGERON 29 LEFT. FABRICATED NEW SUPPORT, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW SUPPORT AND FASTENERS IAW DC8 SRM 53-2-0, 51-1-20 AND 51-1-8.Oct 2, 2005 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS05845572Longeron · corrodedINSPECTION TYPE:SP LONGERON 36 FS 100 TO FS 190 HAS EXFOLIATION CORROSION. REMOVED AND REPLACED LONGERON 36 IAW DWG 5779925 AND SRM 51-1-20D.Sep 30, 2005 · N718UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS05845566Fitting · corrodedINSPECTION TYPE:SP FS 70 L30R END FITTING HAS EXFOLIATION CORROSION AFT CHORD SIDE. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D AND SRM 51-1-21.Sep 30, 2005 · N718UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS05845564Finger Doubler · corrodedINSPECTION TYPE: SP, FS 70 - FS 190 FINGER DOUBLER BETWEEN L30R - L32R IS CRACKED AND HAS EXFOLIATION CORROSION. REMOVED FINGER DOUBLER AT FS 70 - FS 190 L30R - L32R IAW SRM 51-1-21. FABRICATED AND INSTALLED FINGER DOUBLER AT FS 70 - FS 190 L30R - L32R IAW 5Sep 30, 2005 · N718UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS05845588Fitting · crackedINSPECTION TYPE:SP FS 70 L35L END FITTING IS CRACKED BETWEEN ATTACH FASTENER HOLES. REMOVED AND REPLACED END FITTING IAW SRM 51-3-2 AND 51-1-21.Sep 30, 2005 · N718UP · Doug DC871F · Fuselage Main, Attach Fittings
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