Douglas DC-8-71F

Service difficulty reports · 8,938

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  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 IXXA06RNG036SSkin · misrepairedDURING ROUTINE C CHECK, FOUND AN IMPROPER REPAIR ON FUSELAGE SKIN AT STATION 1450 BETWEEN LONGERONS 30 - 31 RIGHT, REPAIR PROXIMITY ISSUE WITH D-PIT DOOR BOTTOM DOUBLER. IMPROPER REPAIR WAS REMOVED, NEW FILLER AND EXTERNAL DOUBLER WERE FABRICATED AND INSTALLEApr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG035SSkin · misrepairedDURING ROUTINE C CHECK FOUND AN IMPROPER REPAIR ON FUSELAGE SKIN AT STATION 30 BETWEEN LONGERONS 6 - 7 LEFT. IMPROPER REPAIR WAS REMOVED; NEW EXTERNAL DOUBLER AND FINGER DOUBLER WERE FABRICATED AND INSTALLED IAW EWO ATI 53-063. FAA FORM 8110-3 WAS ISSUED APPRApr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG034SSkin · misrepairedDURING ROUTINE C CHECK FOUND AN IMPROPER REPAIR ON FUSELAGE SKIN AT STATION 54 LONG 28 -30 LEFT. EXISTING REPAIR WAS REMOVED; NEW EXTERNAL DOUBLER & FILLER WERE FABRICATED AND INSTALLED IAW EWO ATI 53-062. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG033SSkin · misrepairedDURING ROUTINE C CHECK, FOUND AN IMPROPER REPAIR ON SKIN AT STATION 1752 LONGERON 16.5 - LEFT. IMPROPER REPAIR WAS REMOVED AND FINGER DOUBLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW EWO ATI 53-060 AND SRM 53-2-5 FIGURE 14A.Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG032SSkin · misrepairedDURING ROUTINE C CHECK AN IMPROPER REPAIR AT PASSENGER WINDOW STATION 1310 LONGERON 16 RIGHT. IMPROPER REPAIR WAS REMOVED AND REPAIR DOUBLER WAS FABRICATED & INSTALLED IAW EWO ATI 53-059 AND SRM 53-2-0 FIGURE 22A. THIS REPAIR CONSTITUTES A MAJOR REPAIR.Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG031SSkin · misrepairedDURING ROUTINE C CHECK FOUND TWO IMPROPER REPAIRS ON PASSENGER WINDOW; STATION 1472 LONGERON 16.5 RT AND STATION 1479 LONGERON 14.5 RT. BOTH IMPROPER REPAIRS WERE REMOVED AND PERMANENT REPAIRS WERE PERFORMED IAW EWO ATI 53-058 AND SRM 53-2-0 FIGURE 22A. THIS Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG030SSkin · misrepairedDURING ROUTINE C CHECK FOUND AN IMPROPER REPAIR ON PASSENGER WINDOW, AT STATION 1290 LONGERON 17.5- RIGHT HAND.CORRECTIVE ACTION: IMPROPER REPAIR WAS REMOVED AND PERMANENT REPAIR WAS PERFORMED IAW EWO ATI 53-057 AND SRM 53-2-0 FIG 22A. THIS REPAIR CONSTITUTES Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG029SSkin · misrepairedDURING ROUTINE C CHECK, FOUND AN IMPROPER REPAIR ON SKIN OF PASSENGER WINDOW, STATION 1310 LONGERON 16 RIGHT. IMPROPER STRUCTURAL REPAIR AT STATION 1310 LONGERON 16 RIGHT WAS REMOVED AND PERMANENT REPAIR DOUBLER WAS INSTALLED IAW EWO ATI 53-056 AND SRM 53-2-0Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG025SSkin · misrepairedDURING ROUTINE C CHECK, AN IMPROPER REPAIR ON SKIN AT STATION 479, LONGERON 28-RIGHT. DAMAGED SKIN SECTION WAS REMOVED AND REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 53-055 AND SRM 53-2-5 FIGURE 14A. THIS REPAIR CONSTITUTES A MAJOR REPAIR.Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Structure (General)SDR IXXA06RNG024SSkin · misrepairedDURING ROUTINE C CHECK, FOUND AN IMPROPER REPAIR AT STATION 282 AT LONGERON 25.5R. DAMAGED SKIN SECTION WAS REMOVED AND EXTERNAL DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 53-061.Apr 19, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG050SSkin · misrepairedDURING ROUTINE C CHECK FOUND IMPROPER REPAIR AT STATION 8.00 LONGERON 33 RIGHT. REMOVED EXISTING REPAIR. FABRICATED NEW REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS. IAW TAMPA ENGINEERING WORK ORDER EWO ATI 53-052 DAApr 18, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG049SSkin · misrepairedDURING ROUTINE C CHECK FOUND IMPROPER REPAIR AT STATION 8.00 LONGERON 33 LT. REMOVED EXISTING REPAIR. FABRICATED NEW REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS. IAW TAMPA ENGINEERING WORK ORDER EWO ATI 53-052 DATEApr 18, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA060461SRepair · improperDURING ROUTINE C CHECK FOUND IMPROPER REPAIR ON FUSELAGE DRAIN DOUBLER EXTERNAL SKIN AT STATION 172 LONGERON 35.75 RIGHT. REMOVED IMPROPER REPAIR, EDDY CURRENT INSPECTIONS WERE PERFORMED AROUND REMOVED DAMAGE, AND NO CRACKS WERE FOUND, REPAIR DOUBLERS AND FINGApr 18, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06846822Skin · crackedHFEC AND VISUAL INSP DETECTED A .250" CRACK ON THE RT FWD T-1 DOOR AFT JAMB CORNER. CUT OUT DAMAGED AREA ON RT FWD T-1 DOOR AFT DOOR JAMB IAW SAA EA 008-5320-01-A0156. FABRICATED AND INSTALLED REPAIR, 1 FILLER, -2 DOUBLER, AND -3 TRIPLER IAW UPS EO DC8-5330-Apr 18, 2006 · N730UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06846779Skin · corrodedREPLACE LWR BELLY SKIN FROM STA 190 TO 450 DUE TO CORROSION AND EXISTING NON STANDARD REPAIRS. REMOVED AND REPLACED FUSE LWR BELLY SKIN STA 190 TO 450 AND FABRICATED AND INSTALLED INTERNAL DOUBLER AT STA 360-450.Apr 18, 2006 · N730UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06846763Door Frame · crackedHFEC AND VISUAL INSP DETECTED A .250" CRACK ON THE C-4 (D PIT) UPPER FWD JAMB CORNER.CUT OUT DAMAGED AREA AT UPPER FWD JAMB CORNER STA 1400 IAW SRM 53-02-00 FIG 21. FABRICATED AND INSTALLED REPAIR DOUBLER, REPAIR TRIPLER, AND FILLER IAW SRM 53-02-00 FIG 21, 5Apr 18, 2006 · N730UP · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA060176OStriker · brokenAFTER DEPARTURE FROM MMMX THE GEAR DOORS LIGHT REMAINED ILLUMINATED. CREW RECYCLED GEAR PER COM PROCEDURES AND IT HAD NO EFFECT. CREW LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BROKEN RIGHT DOOR STRIKER. REMOVED AND REPLACED THE STRIKER AND THE OPERATIONALApr 17, 2006 · N830BX · Doug DC871F · Landing Gear DoorsSDR IXXA060459SRepair · improperDURING ROUTINE C CHECK FOUND IMPROPER REPAIR ON FUSELAGE DRAIN DOUBLER EXTERNAL SKIN AT STATION 78 LONGERON 35.5 RIGHT. REMOVED IMPROPER REPAIR, EDDY CURRENT INSPECTIONS WERE PERFORMED AROUND REMOVED DAMAGE, AND NO CRACKS WERE FOUND, REPAIR DOUBLERS AND FINGERApr 16, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06846762Skin · corrodedCORROSION FOUND ON SKIN AND FASTENERS UNDER FWD ADF LOOP ANTENNA. CUTOUT CORROSION FROM SKIN UNDER ADF LOOP ANTENNA IAW SRM 51-06-08. FABRICATED AND INSTALLED FOUR FINGER DOUBLERS, AND REPAIR DOUBLER IAW SRM 53-02-01 FIG 7, 51-1-26, AND SRM 51-1-8.Apr 16, 2006 · N730UP · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG022SFitting · crackedDURING ROUTINE C CHECK, FOUND A CRACK ON THE OUTBOARD FLAP STATION XFS 339.723, INBOARD FITTING LEFT HAND. STOP DRILLED THE END OF THE CRACK. REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 57-075. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.Apr 15, 2006 · N823BX · Doug DC871F · Wing, Attach FittingsSDR UPS06846789Bulkhead · crackedFOUND TWO CRACKS ON WEB AFT SIDE OF STA 1766 RT SIDE AT L16R. STOP DRILLED TWO CRACKS AT AFT PRESS BULKHD STA 1766 L16R IAW 53-2-0. FABRICATED AND INSTALLED -1 FILLER, -2 FINGER DOUBLER -3 DOUBLER IAW UPS EO FILE NR DC8-53-20547, SAA EA NR 008-5320-01-A0158 Apr 15, 2006 · N730UP · Doug DC871F · Fuselage Main, BulkheadSDR UPS06846857Floorbeam · crackedFOUND MAIN CABIN APPROX STA 880 L22R RBL 57 FLOORBEAM CRACKED APPROX 4" FROM LIGHTNING HOLE TO FASTENER. CUT FLOORBEAM AT STA 879 RBL 49.03, FABRICATED AND INSTALLED -1,-2 -3,-4 REPAIR ANGLES, AND FLOORBEAM EXTRUSION IAW UPS RAA DC8-53- 20546, SAA EA# 008-532Apr 13, 2006 · N730UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS06846786Skin · dentedINSPECT SMALL DENT AFT OF PIT NR 34 4 FT AFT. CUT OUT DAMAGE, FABRICATED, AND INSTALLED DOUBLER, FILLER FINGER DOUBLER IAW SRM 53-2-01 FIG 7.Apr 12, 2006 · N752UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06846823Skin · corrodedAFTER REMOVAL B-PIT SCUFF PLATE TO FOM NDT INSPECTION IAW EO DC8- 5330-20206-D FOUND CORROSION ON FUSELAGE SKIN. INCREASED RADIUS TO MIN 1.0" IAW SAA EA NR 008-5320-01-A0154. FABRICATED AND INSTALLED -1, -2 SLEEVE, -3 DOUBLER, -4 TRIPLER, AND -5 FILLER IAW UApr 11, 2006 · N730UP · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG013SSkin · improperDURING INSPECTION CHECK FOUND A IMPROPER REPAIR ON PRESSURE SKIN STA 80 TO 10 LONGERON 33 AND 34 RT. IMPROPER REPAIR WAS REMOVED AND NEW REPAIR DOUBLER AND FINGER DOUBLER WERE FABRICATED AND INSTALLED IAW EWO ATI 53-050 AND SRM 53-2-5 FIGURE 14A.Apr 10, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG018SSkin · misrepairedDURING INSPECTION CHECK FOUND TWO IMPROPER REPAIRS ON NOSE SKIN AT STA 8 LONGERON 33 RT AND STA 8 LONGERON 33 LT. DAMAGED SKIN SECTION WAS REMOVED AND EXTERNAL DOUBLER WERE FABRICATED AND INSTALLED IAW EWO ATI 53-052. FAA FORM 8110-3 WAS ISSUED APPROVING THIApr 9, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG014SSkin · misrepairedDURING INSPECTION CHECK FOUND A IMPROPER REPAIR ON PRESSURE SKIN STA 460 TO 480 LONGERON 30 - 31 RT. PERMANENT REPAIR WAS PERFORMED BY FABRICATING AND INSTALLING DOUBLER AND FINGER DOUBLER IAW EWO ATI 53-049 AND SRM 53-2-5 FIGURE 14A.Apr 9, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG052SRib · crackedDURING ROUTINE C CHECK FOUND LT WING TRAILING EDGE UPPER RIB CRACKED AT STA XOLID 6.225. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED, REPAIR PARTS. IAW TAMPA ENGINEERING WORK ORDER EWO ATI 57-081 DATED MAYApr 8, 2006 · N823BX · Doug DC871F · Wing, Rib/BulkheadSDR IXXA06RNG051SRib · crackedDURING ROUTINE C CHECK FOUND LT WING TRAILING EDGE UPPER RIB CRACKED AT STATION XFS 304.0. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED, REPAIR PARTS. IAW TAMPA ENGINEERING WORK ORDER EWO ATI 57-077 DATED AApr 8, 2006 · N823BX · Doug DC871F · Wing, Rib/BulkheadSDR IXXA06RNG042SRepair · improperDURING ROUTINE C CHECK FOUND AN IMPROPER REPAIR ON FUSELAGE CENTER FRAME STATION 781 LONGERON 31 LEFT. IMPROPER REPAIR WAS REMOVED AND PERMANENT REPAIR WAS PERFORMED IAW EWO ATI-53-067 AND BOEING SERVICE REQUEST 1-184705372.Apr 8, 2006 · N823BX · Doug DC871F · Fuselage Main, FrameSDR IXXA06RNG016SSkin · crackedDURING INSPECTION CHECK FOUND A CRACK ON AFT PRESSURE BULKHEAD SKIN LONGERON 10, STA 1766 BETWEEN STIFFENER 5772638-49 AND 5772638-51 LT. DAMAGED AREA WAS CLEANED, CRACKS IN SKIN WERE REMOVED AND REPAIR DOUBLER WAS INSTALLED IAW EWO ATI 53-048 & SRM 53-2-5 FIApr 8, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06846656Smoke Goggles · damagedCAPT AND FE'S SMOKE GOGGLES ARE SCRATCHED AND HAZING. REMOVED AND REPLACED CAPT AND FE'S SMOKE GOGGLES IAW DC8 MM 25-00-00.Apr 8, 2006 · N715UP · Doug DC871F · Emergency EquipmentSDR IXXA060455SSkin · crackedDURING PREFLIGHT INSPECTION, FOUND RUNNING FUEL LEAK INBOARD OF NR 1 PYLON COMING FROM NUMBER ONE ALTERNATE FUEL TANK. THE DAMAGE WAS REMOVED AND REPAIRED PER BOEING ROD SKETCH 06-04-18-001 REF TIMCO GOODYEAR S/O 216006. OPS 27846 REPAIR APPROVED AS TEMPORARApr 7, 2006 · N821BX · Doug DC871F · Wing, Plate/SkinSDR UPS06846655Smoke Goggles · scratchedFIRST OFFICERS SMOKE GOGGLES SCRATCHED AND DIRTY. REPLACED FO'S SMOKE GOGGLES, REF AMM 25-60-05-2.Apr 7, 2006 · N729UP · Doug DC871F · Emergency EquipmentSDR IXXA06RNG041SSkin · misrepairedDURING ROUTINE C CHECK FOUND AN IMPROPER REPAIR ON INBOARD FLAP LOWER SKIN STATION XW 63.604 TO 50.232 RIGHT. IMPROPER REPAIR WAS REMOVED AND PERMANENT REPAIR WAS FABRICATED AND INSTALLED IAW EWO ATI 57-080. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.Apr 6, 2006 · N823BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06RNG040SSkin · bulgedDURING ROUTINE C CHECK, FOUND DENTED AND BULGING SKIN ON INBOARD FLAP UPPER SKIN TRAILING EDGE SKIN BETWEEN STATIONS XW 91.6564 TO 84.534 – RIGHT. DAMAGED SECTION SKIN WAS REMOVED. REPAIR SPLICE WAS MANUFACTURED AND NEW SKIN SECTION WAS FABRICATED AND INSTALApr 6, 2006 · N823BX · Doug DC871F · Trailing Edge FlapsSDR IXXA06RNG038SSkin · nickedDURING ROUTINE C CHECK, FOUND A NICK ON FUSELAGE SKIN AT STATION 1160, BETWEEN LONGERONS 30 - 31 LEFT. REMOVED DAMAGE. EXTERNAL DOUBLER AND EXTERNAL TRIPLER WERE FABRICATED AND INSTALLED IAW EWO ATI 53-066.Apr 6, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG023SSkin · crackedDURING ROUTINE C CHECK, FOUND A CRACK ON SKIN BETWEEN LONGERONS 1-2 RIGHT HAND, STATION 200. DAMAGED SKIN SECTION WAS REMOVED AND INTERNAL DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 53-053.Apr 6, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG010SSkin · crackedDURING ROUTINE C CHECK FOUND A CRACK ON FUSELAGE SKIN FWD PASSENGER DOOR UPPER AFT CORNER, STATION 55 LONGERON 9 TO 12L. CRACK WAS REMOVED AND REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW EWO ATI 53-046 & SRM 53-2-0 FIGURE 15. THIS REPAIR CONSTITUTES A Apr 6, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG011SSkin · crackedDURING INSPECTION CHECK FOUND A CRACK ON FUSELAGE SKIN AFT PASSENGER DOOR UPPER AFT CORNER STA 1660 LT, LONGERON 9 TO 12 LT. DAMAGED AREA WAS REMOVED AND REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 53-047 & SRM 53-2-0 FIGURE 18.Apr 6, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG009SSkin · crackedDURING INSPECTION CHECK WAS FOUND A CRACK ON FUSELAGE SKIN AFT PASSENGER DOOR LOWER FWD CORNER STA 1660 LT LONGERON 21 TO 23 LT. DAMAGED AREA WAS REMOVED AND REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 53-045 & SRM 53-2-0 FIGURE 18.Apr 6, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG008SSkin · crackedDURING INSPECTION CHECK WAS FOUND A CRACK ON FUSELAGE SKIN FWD SERVICE DOOR UPPER FWD CORNER STA 440 LONGERON 10 TO 12 RT. DAMAGED AREA WAS REMOVED AND REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 53-044 & SRM 53-2-0 FIGURE 14.Apr 6, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG007SSkin · crackedDURING INSPECTION CHECK FOUND A CRACK ON FUSELAGE SKIN AFT CARGO COMPARTMENT, UPPER AFT CORNER AT STA 1440.0, LONGERON 25 TO 28-RT. REPAIRED CRACK ON FUSELAGE SKIN AFT CARGO COMPARTMENT IAW EWO ATI 53-043 AND SRM 53-2-0 FIGURE 21.Apr 6, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG028SSkin · crackedDURING ROUTINE CHECK, FOUND 3 CRACKS ON LEFT WING LEADING EDGE LOWER SURFACE BETWEEN STATION XFS 422 AND XS 435. REMOVED AND REPLACED SKIN IN LEFT WING LEAD EDGE LOWER SURFACE BETWEEN STATION XFS 422 AND XS 435 IAW DOUGLAS DRAWING NR 5769857.Apr 4, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA06RNG026SSkin · corrodedDURING ROUTINE C CHECK, FOUND CORROSION ON HORIZONTAL STABILIZER LOWER SKIN AT STATION XAR 0.00 TO REAR SPAR LEFT HAND. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGE 20. THICKNESS MEASUREMENT PERFORMED AND IT WAS FOUND OUT OF LIMITS IAW DC8 SRM 55-2-0 PAGE 12. Apr 4, 2006 · N823BX · Doug DC871F · Horizontal Stabilizer, Plate/SkinSDR IXXA06RNG021SPlate · corrodedDURING ROUTINE C CHECK FOUND CORROSION ON THE INBOARD EXTENDED LEADING EDGE NOSE PLATING AROUND STATION XFS 5000 LEFT HAND. CORRODED AREA WAS REMOVED AND INTERNAL DOUBLER WAS FABRICATED & INSTALLED IAW EWO ATI 57-074. FAA FORM 8110-3 WAS ISSUED APPROVING THISApr 4, 2006 · N823BX · Doug DC871F · Wing, Plate/SkinSDR IXXA06RNG006SSkin · corrodedDURING INSPECTION CHECK FOUND A CORROSION ON FUSELAGE SKIN BETWEEN STA 35 TI 70, LONGERON 31 RT TO 31 LT. SKIN PORTION OF LOWER FUSELAGE FROM LONGERON 31 RT TO 31 LT AND STA 17 TO 70 WAS REMOVED AND REPLACED IAW DOUBLER DRAWING 5613862, AND SPLICE WAS FABRICAApr 4, 2006 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06846643Battery · dischargedEMERGENCY EXIT LIGHT BATTERY DEAD R&R EMERGENCY EXIT LIGHT BATTERY PACK W/R/T M/M 33-50-01-2 OPS CK GOOD.Apr 4, 2006 · N703UP · Doug DC871F · Emergency LightingSDR IXXA06RNG039SVane · corrodedDURING ROUTINE C CHECK, FOUND ELONGATED HOLES AND CORROSION ON EXTENDED LEADING EDGE OUTBOARD VANE BETWEEN STATIONS XILD 0.7095 XILD 40.00 RIGHT. CORRODED AREA WAS REMOVED, DAMAGED SECTION HOLES WERE CUT OUT AND PERMANENT REPAIR WAS PERFORMED IAW EWO ATI 57-0Apr 3, 2006 · N823BX · Doug DC871F · Leading Edge DevicesSDR IXXA06RNG037SAngle · corrodedDURING ROUTINE C CHECK, FOUND CORROSION ON FORMER (CAP ANGLE) AT STATION 99 - LEFT. CORRODED AREA WAS REMOVED, REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 53-065 AND SRM 53-2-5 FIG 8C-1. THIS REPAIR CONSTITUTES A MAJOR REPAIR.Apr 3, 2006 · N823BX · Doug DC871F · Fuselage Miscellaneous Structure
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