Douglas DC-8-73F

Service difficulty reports · 15,471

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  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 UPS00832087Seat Track · corrodedINSPECTION TYPE:C 123 CORROSION ON FLOORBEAM, UPPER FLOOR SKIN & SEAT TRACK NEAR CUSP RT FS 1580 AFT ACCES BAY. SEAT TRACK CORRODED OUT OF LIMITS IAW DC8 SRM 53-2-3. REMOVED CORROSION FROM FLOORBEAM & SKIN. FOUND TO BE IN LIMITS IAW DC8 SR M 53-2-0. REMOMar 8, 2000 · N804UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003430Bracket · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BRACKET SUPPORT CEILING LT SIDE AT STA 500 TO 510, 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 51-1Mar 7, 2000 · N2674U · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000696Channel · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO RIB STIFFNER 16 IN. INBD OF LT MLG ACTUATOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW STIFFNER.Mar 7, 2000 · N831AL · Doug DC873F · Wing Miscellaneous StructureSDR RRXA000695Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE VERTICAL STABILIZER LWR L/E RIB NR 11 FROM TOP LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 55-5-1 FIG 2.Mar 7, 2000 · N831AL · Doug DC873F · Vertical Stabilizer, Spar/RibSDR RRXA000694Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE VERTICAL STABILIZER LOWER L/E RIB NR 12 TOP LT DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 55-5-1 FIG 2.Mar 7, 2000 · N831AL · Doug DC873F · Vertical Stabilizer, Spar/RibSDR RRXA003735Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT LOWER CARGO BILGE DOUBLER AT STA 1480 TO 1500 L32L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED, ALODINED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAMar 7, 2000 · N961R · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA000594Beam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LT CUSP BEAM AT STA 1320, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED IAW DC-8 SRM 53-2-5 FIG 15. (CORROSION DAMAGE RECORDED IN EWA CMar 7, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000576Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO EXTERIOR FUSELAGE SKIN AT STA -8 TO 70 AND BETWEEN LONGERON 31 LEFT TO 31 RIGHT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED SECTION OF SKIN IAW DCMar 7, 2000 · N831AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA000571Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SKIN AT STA 120 AND LONGERON 36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER, FINGER DOUBLER AND FILLER AND INSTALLED IAW DC-8 SRM 53-2-1Mar 7, 2000 · N831AL · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS00832205Floorbeam · corrodedINSPECTION TYPE: C123, FS 878, FLOORBEAM HAS CORROSION BETWEEN SEAT TRACKS F AND G TOP SIDE. FOUND TO BE CORRODED OUT OF LIMITS, TRIMMED OUT DAMAGED AREAS, INSTALLED REPAIR IAW REO-G07202.Mar 7, 2000 · N804UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS00832094Intercostal · crackedINSPECTION TYPE: C 123 INTERCOSTAL CRACKED. REMOVED INTERCOSTAL IAW DC8 SRM 51-1-21. MATERIAL ID .040 7075-0 P/O NR 318790. HEAT TREATED TO .040 7075-T6 IAW DAC DWG NR 5755032. FAB IAW SRM 51-1 -21 BY INSTALLING RIVETS ON FWD SIDE OF INTERCOSTAL.Mar 7, 2000 · N804UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832001Intercostal · crackedINSPECTION TYPE:C123, RT AFT SERVICE DOOR HAS A CRACK INTERCOSTAL. STOP DRILLED CRACK AND REPAIRED AREA IAW DC8 SRM 52-2-0.Mar 7, 2000 · N804UP · Doug DC873F · Service DoorsSDR RRXA003432Floor Support · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE FLOOR SUPPORT AT STA 1240-1260 BETWEEN L34L-L35L, 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 51-1-20, 51-1-Mar 6, 2000 · N2674U · Doug DC873F · Fuselage Floor PanelSDR RRXA002048Skin · damagedDURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH THE LT L/E CENTER SECTION AT STA XFS 310 TO 422, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20DMar 6, 2000 · N961R · Doug DC873F · Wing, Center BoxSDR RRXA000698Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN THE BORE FOR FWD BOLT AT LONGERON 24R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DAC DWG 5750198.Mar 6, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000693Floorboard · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE MAIN CABIN FLOOR BOARD AT STA 145 AND RBL 22, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 53-20, 51-1-20 AND 53-2-3.Mar 6, 2000 · N831AL · Doug DC873F · Fuselage Floor PanelSDR RRXA000692Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING L/E RIB AT UPPER END (AFT) AT STA XFS 753.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLEMar 6, 2000 · N831AL · Doug DC873F · Wing Miscellaneous StructureSDR RRXA000691Floor Support · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE VERTICAL LOWER FLOOR BEAM SUPPORT STRUT AT STA 280 RBL 46, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW SUPPORT AND INSTALLED IAW DC-8 SRM 51-1-20D ANDMar 6, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000574Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO END FITTINGS JUST FWD OF STA 70 AND LONGERON 3 RIGHT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DC-8 SRM 51-1-20D DMar 6, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832134Bracket · corrodedINSPECTION TYPE: C123, FLOORBEAM BRACKET STA 1700, LBL 30, CORRODED. REMOVED BRACKET, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. FORMED BRACKET IAW DAC DWG NR 5755032. LOADED, DRILLED & DEBURRED IAW DC8 SRM 51-1-24. ALODINED & PRIMED IAW DC8 SRM 51Mar 6, 2000 · N804UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832133Cargo Track · corrodedINSPECTION TYPE:C123 LOWER AFT CARGO BAY GILLINER SUPPORT & CARGO TRACK CORRODED AT BS 1000 - 1140. REMOVED CORRODED CARGO TRACK, DRILLED & COUNTERSUNK NEW CARGO TRACK AND INSTALLED IAW DC8 SRM 51-3-2, 51-1-22 & 51-3-0.Mar 6, 2000 · N804UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832131Skin · crackedINSPECTION TYPE: C123, WING SKIN AT STRINGER 64 END FITTING ON LT WING HAS CRACKS AT MOST OUTBOARD AND INBOARD HOLES. FABBED DOUBLER & FILLER IAW EO DC8 5730-9004-D. ALODINED & PRIMED I AW DC8 SRM 51-1-8, INSTALLED DOUBLER, FILLER & LONICALS IAW DC8 SRM 5Mar 6, 2000 · N804UP · Doug DC873F · Wing, Plate/SkinSDR UPS00832119Floorboard · corrodedINSPECTION TYPE: C123, FLOOR PANEL, STA 580 - 759 HAS CORROSION ON UPPER SKIN. REMOVED CORROSION, FOUND OUT OF LIMITS FROM FS 620 - 759 IAW 53-20-0 FIG 1F. REPLACE FLOOR PANEL PN 52772658-15300. DRILLED IAW 51-1-21. ALODINED & PRIMED IAW DC8 SRM 51-1-8Mar 6, 2000 · N804UP · Doug DC873F · Fuselage Floor PanelSDR UPS00832118Fairing · chafedINSPECTION TYPE: C123, RT UPPER HORIZONTAL FILLET PANEL IS CHAFED. REMOVED DAMAGE, FOUND TO EXCEED LIMITS PER DC8 SRM 55-2-0. FABBED DOUBLER PER DC8 SRM 55-2-0. ALODINED & PRIMED PER DC8 SRM 51-1-8. INSTALLED PER DC8 SRM 51-1-21.Mar 6, 2000 · N804UP · Doug DC873F · Horizontal Stabilizer StructureSDR RRXA000686Rib · crackedDURING A MAINTENANCE VISIT FOUND 2 CRACKS AT THE VERTICAL STABILIZER L/E RIB NR13 FROM TOP (1 LT AND 1 R/H) ON END OF RIBS, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DMar 5, 2000 · N831AL · Doug DC873F · Vertical Stabilizer, Spar/RibSDR RRXA000684Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT THE RT WING L/E RIB AT THE AFT LOWER FASTENER AT XF 722.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION/////REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-8-1. RECEIVED REPAIRED DOUBLER AND INSTALMar 5, 2000 · N831AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA000564Seat Track · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN DECK SEAT TRACK AT STA 990 TO 1390 AND RBL 24, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SEAT TRACK SECTION IAW DC-8 SRM 53Mar 5, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS00832138Fitting · crackedINSPECTION TYPE: C123, LT O/B AILERON I/B HINGE FITTING IS CRACKED. REMOVED & REPLACED FITTING IAW DC8 SRM 51-1-21 & 51-3-0.Mar 5, 2000 · N804UP · Doug DC873F · AileronsSDR RRXA003433Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MAIN CABIN FLOOR PANEL AT FS 742-743 AND LBL 44-45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 5Mar 4, 2000 · N2674U · Doug DC873F · Fuselage Floor PanelSDR RRXA003431Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MAIN CABIN FLOOR PLANK AT FS 490-492 AND 520-522 AND LBL 28-29, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAMar 4, 2000 · N2674U · Doug DC873F · Fuselage Floor PanelSDR RRXA000569Frame · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME AT STA 1100 BETWEEN LONGERONS 36 TO 35 LEFT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED DAMAGED AREA IAW DC-8 SRM 5Mar 4, 2000 · N831AL · Doug DC873F · Fuselage Main, FrameSDR RRXA000563Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 70 AND RBL 53, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 51-1-21 DAC DWG 35890314. (CORRMar 4, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832204Strap · corrodedINSPECTION TYPE: C123, INSIDE VENT STAB LOWER ACCESS HOLE FUSELAGE BACKSTRAP DOUBLER HAS AREAS OF EXCESSIVE CORROSION.Mar 4, 2000 · N804UP · Doug DC873F · Vertical StabilizerSDR UPS00832203Frame · damagedINSPECTION TYPE: C123, CARGO DOOR FWD TORQUE BOX FWD FRAME IS DAMAGED. REMOVED LOWER TORQUE BOX WEB & INTERCOSTAL, TRIMMED OUT DAMAGE & PLUGGED DISCREPANT HOLES IAW REO-G07197. FABBED UPPER & LOWER REPAIR DOUBLERS, REPAIR ANGLE & FILLERS IAW REO G0719Mar 4, 2000 · N804UP · Doug DC873F · Cargo/Baggage DoorsSDR UPS00832163Frame · crackedINSPECTION TYPE: C123, MAIN CARGO DOOR AFT TORQUE BOX FRAME IS DAMAGED. REMOVED LOWER WEB INTERCOSTALS AT LONGERON 16 & 17 LT & LWR FRAME FITTING. FABED UPPER AND LOWER REPAIR ANGLE, FILLERS AND TRIMMED OUT DAMAGE IAW REO-G0 7188 REV B. INSTALLED UPPER &Mar 4, 2000 · N804UP · Doug DC873F · Fuselage Main, FrameSDR DHL2000804002Computer · malfunctionedNR 1 INS FAILED ACCURACY CHECK 10 MIN AFTER TAKEOFF. NR 2 INS FAILED LIGHT ILLUMINATED 15 MIN AFTER TAKEOFF. REMOVED AND REPLACED NR 1 AND NR 2 INU PER MM 34-44-00..Mar 4, 2000 · N804DH · Doug DC873F · Inertial Guidance SystemSDR DHL200080373CTrim Tab · delaminatedAT C-CHECK, LT WING I/B AILERON TRIM TAB UPPER SKIN DELAMINATED. REMOVED AND REPLACED TRIM CONTROL TAB IAW MM 27-13-1, OPERATIONAL CHECK GOOD IAW MM 27-10-0. N/R 1007Mar 4, 2000 · N803DH · Doug DC873F · AileronsSDR DHL200080370CSkin · delaminatedAT C-CHECK, RT WING NR 3 SPOILER DELAMINATED. REMOVED AND REPLACED NR 3 RT SPOILER IAW MM 27-61-1 PG 201, 202. OPERATIONAL CHECK IAW MM 27-60-0. N/R 1013Mar 4, 2000 · N803DH · Doug DC873F · SpoilersSDR DHL200080369CSkin · delaminatedAT C-CHECK, RT WING NR 4 SPOILER UPPER PART DELAMINATED. REMOVED SPOILER AND INSTALLED SERVICEABLE SPOILER IAW MM 27-60-0. CLEARANCE CHECK GOOD. N/R 1014Mar 4, 2000 · N803DH · Doug DC873F · SpoilersSDR RRXA003412Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE VERTICAL STABILIZER RT LOWER DRAG ANGLE AT FWD SPAR INTERSECTION AT STA 1760 AND L3R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLEMar 3, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003411Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE C-PIT TORQUE BOX BATHTUB FITTING AT FS 1180 AND L35R TO L34R, 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 53-2-0Mar 3, 2000 · N831AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA000683Flange · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT THE TAIL CONE FLANGE AT FLANGE SUPPORT ATTACH POINT R/H SIDE AT STA 1945, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED RMar 3, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832127Finger Doubler · crackedINSPECTION TYPE: C123, FINGER DOUBLER FWD OF STA 940 CRACKED AROUND RIVET. REMOVED AND REPLACED FINGER DOUBLER IAW REO-G07215. REMOVED CORROSION IAW DC8 SRM 51-1-8. REMAINING MATERIAL ACCEPTABLE IAW REO-G07215. ALODINED & PRIMED IAW DC8 SRM 51-1-8.Mar 3, 2000 · N804UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832089Angle · crackedINSPECTION TYPE: C 123 RUDDER LEADING EDGE ATTACH ANGLE CRACKED AT 2 RT 284.750. REMOVED CRACKED ANGLE. MATERIAL VERIFICATION PO NR 318067 7075-0.071 IAW DC8 SR M55-5-0. MATERIAL FABRICATION OF NEW ATTACH ANGLE IAW DC8 SRM 55-5-0.HEAT TREAT VERIFICATION 7Mar 3, 2000 · N804UP · Doug DC873F · Rudder StructureSDR RRXA000682Web · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AND A TEAR TO THE 'C' PIT DOOR INBD WEB AT FWD END, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED DOUBLER IAW DC-8 SRM 52-20, 51-1-20, Mar 2, 2000 · N831AL · Doug DC873F · Cargo/Baggage DoorsSDR RRXA000681Stiffener · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H WING ROOT AT ACCESS DOOR WEB STIFFNER BELOW CONTROL TRAP FITTING AT STA XW-0 AND LONGERON 54R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICMar 2, 2000 · N831AL · Doug DC873F · Wing Miscellaneous StructureSDR UPS00832202Bulkhead · crackedINSPECTION TYPE: C123, CRACK IN MLG PRESSURE DECK AT STA 860 RBL 63 REPAIRED AREA IAW REO-G07239. ALODINED & PRIMED IAW DC8 SRM 51-1-8.Mar 2, 2000 · N804UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS00832200Bulkhead · crackedINSPECTION TYPE: C123, CRACK IN MLG PRESSURE DECK AT FS 860 LBL63. STOP DRILLED CRACK IAW DC8 SRM 53-2-0. FABRICATED REPAIR ANGLE IAW REO-G07210 REV A. LOCATED, DRILLED & DEBURRED IAW DC8 SRM 51-1-29. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLEDMar 2, 2000 · N804UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS00832162Intercostal · corrodedINSPECTION TYPE: C123, FWD CARGO BAY AT FS 500 - 520 INTERCOSTAL AT LONGERON 33 RT IS CORRODED. CORROSION BEYOND LIMITS IAW DC8 SR7 53-7-0.REMOVED INTERCOSTAL FROM A/C.Mar 2, 2000 · N804UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832126Fitting · crackedINSPECTION TYPE: C123, AFT CARGO BAY, FS 1240 FITTING AT LONGERON 35 RT CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-20D. LOCATED & DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D.Mar 2, 2000 · N804UP · Doug DC873F · Fuselage Miscellaneous Structure
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