Douglas DC-8-71F

Service difficulty reports · 8,938

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 = 'DC871F'
  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 UPS00833953Splice · crackedINSPECTION TYPE:C123, STA 8 RT PRESS BULKHEAD REPAIR SPLICE AT TOP CRACKED NOSE WW RT TUNNEL AREA. REMOVED AND REPLACED PACK DOORS ACTUATOR. REMOVED AND REPLACED TWO LOUVER PACK DOORS. REMOVED AND REPLACED REPAIR SPLICE FTG.Sep 19, 2000 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003131Web · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE SIDE CUSP WEB AT STA 880 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 AND 51-1-21.Sep 18, 2000 · N8076U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003132Web · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CUSP WEB AT STA 880 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21 AND 53-2-0.Sep 16, 2000 · N8076U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003133Intercostal · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL AND DOUBLER BETWEEN FLOORBEAMS AT STA 320 - 324 AND X+40 Z-2, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRMSep 15, 2000 · N8076U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003825Former · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO BOTTOM T/E FORMER AT STA. XFS163.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 5Sep 14, 2000 · N500MH · Doug DC871F · Wing, Plate/SkinSDR RRXA003762Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FRAME AFT OF "B"-PIT DOOR AT STA 560 Z=0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLESep 14, 2000 · N500MH · Doug DC871F · Fuselage Main, FrameSDR RRXA003045Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H O/B L/E TOP T/E FORMER AT STA XFS 728.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IASep 14, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003043Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H WING L/E TOP T/E FORMER AT STA XFS 660, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DSep 14, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003042Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H WING L/E TOP T/E FORMER AT STA XFS 666, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DSep 14, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003041Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H WING L/E TOP T/E FORMER AT STA XFS 678.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED ISep 14, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003040Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H WING L/E BOTTOM T/E FORMER AT STA XFS 678.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLESep 14, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003039Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H WING L/E BOTTOM T/E FORMER AT STA XFS 647.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLESep 14, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003038Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H L/E BOTTOM T/E FORMER AT STA XFS 297.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAWSep 14, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003037Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H L/E TOP T/E FORMER AT STA XFS 347.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DCSep 14, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003036Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H L/E TOP T/E FORMER AT STA XFS 354, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SSep 14, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003035Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H L/E TOP T/E FORMER AT STA XFS 360.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DCSep 14, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003034Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H L/E TOP T/E FORMER AT STA XFS 435.789, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DCSep 14, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003033Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H L/E TOP T/E FORMER AT STA XFS 442.185, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DCSep 14, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003032Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H L/E TOP T/E FORMER AT STA XFS 461.372, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DCSep 14, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003031Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H L/E TOP T/E FORMER AT STA XFS 810, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SSep 14, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003030Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H WING L/E TOP I/B-T/E FORMER AT STA XFS 766.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLESep 14, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003029Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H WING L/E TOP I/B-T/E FORMER AT STA XFS 822.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLSep 14, 2000 · N500MH · Doug DC871F · Wing Miscellaneous StructureSDR RRXA003028Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H WING L/E BOTTOM I/B-T/E FORMER AT STA XFS 791.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTSep 14, 2000 · N500MH · Doug DC871F · Wing Miscellaneous StructureSDR RRXA003027Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H WING L/E TOP I/B-T/E FORMER AT STA XFS 728.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLSep 14, 2000 · N500MH · Doug DC871F · Wing Miscellaneous StructureSDR RRXA003021Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H WING L/E TOP I/B-T/E FORMER AT STA XFS 562, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED ISep 14, 2000 · N500MH · Doug DC871F · Wing Miscellaneous StructureSDR RRXA003020Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H L/E O/B-I/B SECTION TOP T/E FORMER AT STA XFS 578.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND Sep 14, 2000 · N500MH · Doug DC871F · Wing Miscellaneous StructureSDR RRXA003019Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H L/E O/B-I/B SECTION TOP T/E FORMER AT STA XFS 597.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND ISep 14, 2000 · N500MH · Doug DC871F · Wing Miscellaneous StructureSDR RRXA003135Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE FAIRING ATTACH ANGLE AT STA 640, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-24 AND 51-1-21.Sep 14, 2000 · N8076U · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833776Frame · crackedINSPECTION TYPE:C123, STA 55 FRAME IS CRACKED AT LONG 24R. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.Sep 14, 2000 · N729UP · Doug DC871F · Fuselage Main, FrameSDR RRXA003764Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FINGER DOUBLER AT STA 1340 TO 1360 L36 TO L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALSep 13, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003763Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE L-1 DOOR FLOOR PANEL 1ST PANEL INSIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PSep 13, 2000 · N500MH · Doug DC871F · Fuselage Floor PanelSDR RRXA003751Floorboard · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOOR BOARD AT STA 70 X=-46 Z=0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 53-2-0 FIG 1F.Sep 13, 2000 · N500MH · Doug DC871F · Fuselage Floor PanelSDR RRXA003743Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE TOILET TUBE PANEL AT STA 80 AND L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PANEL IAW DC-8 SRM 51-1-21 AND 53-2Sep 13, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003738Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO COCKPIT PANEL 682A Y=-12, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-1-21 AND 53-2-0 FIG 1F.Sep 13, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003026Doubler · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE DOUBLER ON THE R/H MLG DOOR LWR FWD, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW EO#00-25Sep 13, 2000 · N500MH · Doug DC871F · Landing Gear DoorsSDR RRXA003025Fitting · misdrilledDURING A MAINTENANCE VISIT FOUND A DRILLED AREA IN THE MAIN CABIN CIRCUMFERENTIAL FRAME FITTING AT STA 640 AND L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DSep 13, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003024Longeron · crackedDURING A MAINTENANCE VISIT FOUND A CRACK THROUGH LARGE BOLT HOLE AND CRACK APPROX 3/4 INCHES IN LENGTH UNDER VERTICAL LEG IN THE R/H W/W AT STA 857 AND L24R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-Sep 13, 2000 · N500MH · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA003023Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN C-PIT TO FRAME TO LONGERON ATTACH FITTING AT STA 1168 AND L30R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART ANSep 13, 2000 · N500MH · Doug DC871F · Fuselage Main, FrameSDR RRXA003022Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE C-PIT FRAME TO LONGERON ATTACH FITTING AT STA 1168 AND L30L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART ANSep 13, 2000 · N500MH · Doug DC871F · Fuselage Main, FrameSDR UPS00833870Fitting · crackedINSPECTION TYPE:C123, AFT PIT FS 1180 FITTING AT L35R - L34R CRACK. REMOVED FITTING RCVD NEW FITTING (P/N 3755843-501N) MAT ID FOR REPAIR ANGLE 60-436 .125 7075-T6 ANGLE PO 288271 IAW DC8 SRM 53-2-0. FABED REPAIR ANGLES IAW DC8 SRM 53-2-0 LOCATED AND DRILLEDSep 13, 2000 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA0000032Filter · contaminatedEN ROUTE FROM TOL TO DFW, THE NUMBER ONE ENGINE EXPERIENCED A ROLL BACK AT THE TOP OF DESCENT. NO THROTTLE RESPONCE WAS MOMENTARILY NOTED THEN ALL ENGINE PARAMETERS RETURNED TO NORMAL. THE FLIGHT CONTINUED TO DFW FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPESep 13, 2000 · N826BX · Doug DC871F · Aircraft Fuel Filter/StrainerSDR UPS00833792Longeron · crackedINSPECTION TYPE:C123, STA 1640 AFT SIDELONG 34L IS CRACKED. REMOVED, FABRICATED, AND REPLACED LONGERON SEGMENT IAW DWG 3647110 AND SRM 51-1-20D, 51-1-21.Sep 13, 2000 · N729UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA003759Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND A CRACK TO THE ATTACH ANGLE REAR SPAR UPPER CENTER WING IN CABIN Z-21 AT STA 857 +25 TO -45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA ISep 12, 2000 · N500MH · Doug DC871F · Wing, Attach FittingsSDR UPS00833761Beam · corrodedINSPECTION TYPE:C123 A PITT CROSSLIDE DOOR FRAME/BEAM IS CORRODED BEYOND LIMITS AT STA. 330 LONG. 22R ON DOOR REPAIRED FRAME I.A.W. SRM. 52-2-0 FIG. 2Sep 12, 2000 · N729UP · Doug DC871F · Fuselage Main, StructureSDR UPS00833954Frame · corrodedINSPECTION TYPE:C123, FS 80 AT L1L & L2L FRAME HAS EXFOLIATED CORROSION ON FWD SIDE. REPAIRED IAW DC8 SRM 53-2-0 FIG 2.Sep 11, 2000 · N798UP · Doug DC871F · Fuselage Main, FrameSDR UPS00833760Frame · corrodedINSPECTION TYPE:C123, STA 1380 FRAME IS CORRODED BEYOND LIMITS AT LONG 36. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.Sep 11, 2000 · N729UP · Doug DC871F · Fuselage Main, FrameSDR UPS00833755Skin · corrodedINSPECTION TYPE:C123, LEFT HORIZONTAL STAB L/E SKIN IS CORRODED BEYOND LIMITS AT XFS 172.5. REPAIRED SKIN IAW SRM 55-2-1 FIG 4.Sep 11, 2000 · N729UP · Doug DC871F · Horizontal Stabilizer, Plate/SkinSDR RRXA003321Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE TRACK AT FASTENER HOLE AT FS 1482 AND X=50R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG 1F. (CORROSSep 10, 2000 · N8076U · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS00833950Rivet · shearedINSPECTION TYPE:C123, EVIDENCE OF CORROSION 3 RIVETS SHEARED OFF STA 12 CEILING STIFFENER AT FRAME NOSE WW RT TUNNEL AREA. REPAIRED IAW REO G07615.Sep 10, 2000 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833965Angle · crackedINSPECTION TYPE:C123, RT INBOARD PRESSURE PANEL LWR ATTACH ANGLE IS CRACKED, STA 857.0 ABOVE CTR WING TANK UPPER SKIN RWW. CLEANED SEALANT FROM AREA, FABED REPAIR ANGLE AND STRAPS IAW DC8 SRM 53-2-5. ALODINED AND PRIMED IAW 51-1-8, INSTALLED REPAIR PARTS IAWSep 9, 2000 · N798UP · Doug DC871F · Wing Miscellaneous Structure
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