N641SW

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 62,873 hrs · 49,100 cycles

FORWARD ENTRY EMERGENCY EXIT SIGN BROKEN. R&R SIGN ASSEMBLY IAW MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 62,536 hrs · 48,873 cycles

R1 DOOR EMERGENCY EXIT PLASTIC COVER CRACKED. R & R THE COVER IAW MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 62,536 hrs · 48,873 cycles

LEFT EMERGENCY EXIT BULLNOSE LENS LOOSE AT ROW 10. SECURED LENS IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,645 hrs · 48,282 cycles

WEB INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, BL 0. R & R INTERCOSTAL IAW SRM AND DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,645 hrs · 48,282 cycles

LEFT EMERGENCY EXIT HATCH BULB INOPERATIVE. R & R BULB IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 61,645 hrs · 48,282 cycles

RIGHT WING L/E NR 6 SLAT SKIN CRACKED ON LOWER SURFACE OTBD END. REPAIRED SKIN IAW SRM AND EA.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 61,645 hrs · 48,282 cycles

RIGHT WING REAR SPAR INTERNAL AREA SUPPORT ANGLE CRACKED ON RSS 537.806 + 7.2. R & R ANGLE IAW SRM AND DWG.

Part: SUPPORT FITTING — CORRODED (LT WING) · airframe 61,645 hrs · 48,282 cycles

LEFT WING MLG SUPPORT BEAM STABILIZER SUPPORT FITTING CORRODED. R & R FITTING IAW AMM.

Part: FITTING — CORRODED (LT WING) · airframe 61,645 hrs · 48,282 cycles

LEFT WING MLG SUPPORT BEAM FITTING CORRODED. R & R FITTING ASSY IAW AMM.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 61,645 hrs · 48,282 cycles

LEFT MLG BORE SUPPORT FITTING CORRODED AT BS 685. REPAIRED FITTING IAW SI AND EA.

Part: BRACKET — CORRODED (L2 DOOR) · airframe 61,645 hrs · 48,282 cycles

L2 DOOR EMERGENCY EVAC SLIDE FLOOR MOUNT BRACKET CORRODED. R & R BRACKET IAW AMM.

Part: BRACKET — CORRODED (R2 DOOR) · airframe 61,645 hrs · 48,282 cycles

R2 DOOR EMERGENCY EVAC SLIDE FLOOR MOUNT BRACKET CORRODED. R & R BRACKET IAW AMM.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 61,645 hrs · 48,282 cycles

RIGHT WING REAR SPAR MLG BEAM FORWARD SUPPORT FITTING CRACKED ON RSS 223. REPAIRED FITTING IAW EA.

Part: NUT — CORRODED (RT MLG) · airframe 61,645 hrs · 48,282 cycles

RIGHT MLG TRUNNION PIN NUT CORRODED. R & R NUT IAW AMM.

Part: SKIN — CRACKED (LT WING) · airframe 61,645 hrs · 48,282 cycles

LEFT WING TE INSPAR UPPER SKIN CRACKED ON RSS 210.00+12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,645 hrs · 48,282 cycles

LEFT WING TE INSPAR UPPER SKIN CRACKED ON RSS 260.00+5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,645 hrs · 48,282 cycles

LEFT WING TE INSPAR UPPER SKIN CRACKED ON RSS 230.00+8.5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,645 hrs · 48,282 cycles

LEFT WING TE INSPAR UPPER SKIN CRACKED ON RSS 260.00+6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,645 hrs · 48,282 cycles

LEFT WING TE INSPAR UPPER SKIN CRACKED ON RSS 230.00+17.5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,645 hrs · 48,282 cycles

LEFT WING TE INSPAR UPPER SKIN CRACKED ON RSS 224.14 +1. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,645 hrs · 48,282 cycles

LEFT WING TE INSPAR UPPER SKIN CRACKED ON RSS 260.00+3.5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,645 hrs · 48,282 cycles

LEFT WING TE INSPAR UPPER SKIN CRACKED ON RSS 260.00+9. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,645 hrs · 48,282 cycles

LEFT WING TE INSPAR UPPER SKIN CRACKED ON RSS 282.34+4.5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,645 hrs · 48,282 cycles

LEFT WING TE INSPAR UPPER SKIN CRACKED ON RSS 252.81. REPAIRED SKIN IAW EA.

Part: FITTING — CORRODED (RT MLG) · airframe 61,645 hrs · 48,282 cycles

RIGHT MLG SWING LINK FITTING CORRODED. REPAIRED FITTING IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,645 hrs · 48,282 cycles

RIGHT WING INSPAR UPPER SKIN CRACKED BETWEEN RSS 210 TO RSS 270. REPAIRED SKIN IAW EA.

Part: PLATE — CORRODED (LT MLG) · airframe 61,645 hrs · 48,282 cycles

LEFT MLG SWING LINK PLATE FACES CORRODED. REPAIRED PLATE IAW CMM.

Part: HINGE FITTING — LOOSE (RT SPOILER) · airframe 61,645 hrs · 48,282 cycles

RT WING NR 5 GROUND SPOILER INBD CENTER HINGE FITTING BEARING LOOSE. R & R HINGE IAW EA.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 61,645 hrs · 48,282 cycles

RIGHT WING NR 5 FLAP TRACK CORRODED ON HOLE ATTACH BOLT. REPAIRED NR 5 FLAP TRACK IAW CMM.

Part: FITTING — BROKEN (TE FLAP) · airframe 61,645 hrs · 48,282 cycles

RIGHT WING NR 5 FLAP TRANSMISSION END FITTING BROKEN. R & R FITTING IAW SRM.

Part: SPLICE — CRACKED (LT WING) · airframe 61,645 hrs · 48,282 cycles

LEFT WING REAR SPAR UPPER CHORD SPLICE CRACKED ON RSS 223.14. REPAIRED SPLICE IAW EA.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 61,645 hrs · 48,282 cycles

LEFT WING AFT SUPPORT FITTING CRACKED ON RSS 223.14, COMMON REAR SPAR UPPER CHORD. R & R FITTING IAW SRM & DWG.

Part: SPLICE — CRACKED (LT WING) · airframe 61,645 hrs · 48,282 cycles

LEFT WING REAR SPAR WEB SPLICE CRACKED BETWEEN RSS 211 TO RSS 238 UPPER CHORD AREA. REPAIRED SPLICE IAW EA.

Part: SPLICE — CRACKED (RT WING) · airframe 61,645 hrs · 48,282 cycles

RT WING REAR SPAR UPPER CHORD SPLICE CRACKED ON RSS 223.14. REPAIRED SPLICE IAW EA.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 61,645 hrs · 48,282 cycles

RIGHT WING AFT SUPPORT FITTING CRACKED ON RSS 223.14 COMMON REAR SPAR UPPER CHORD. R & R FITTING IAW SRM AND DWG.

Part: SPLICE — CRACKED (RT WING) · airframe 61,645 hrs · 48,282 cycles

RIGHT WING REAR SPAR WEB SPLICE CRACKED BETWEEN RSS 211 TO RSS 238, UPPER CHORD AREA. REPAIRED SPLICE IAW EA.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 61,645 hrs · 48,282 cycles

LEFT WING NR 4 FLAP TRACK CORRODED ON HOLE ATTACHMENT BOLT. REPAIRED NR 4 FLAP TRACK IAW EA.

Part: FITTING — CORRODED (RT MLG) · airframe 61,645 hrs · 48,282 cycles

RIGHT MLG SWING LINK REAR FITTING CORRODED. REPAIRED FITTING IAW CMM.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 61,645 hrs · 48,282 cycles

L1 DOOR FWD LOWER CORNER REVEAL CRACKED. R & R REVEAL IAW SRM & DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 61,645 hrs · 48,282 cycles

ATTACH CLIP CRACKED AT BS 348.2, STRINGER 15L. R & R CLIP IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 61,645 hrs · 48,282 cycles

STRINGER SPLICE CRACKED AT BS 908, STRINGER 4R. R & R SPLICE IAW EA.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 61,645 hrs · 48,282 cycles

CENTER FUEL TANK SPLICE CRACKED AT BS 590, BETWEEN LBL 70.85 - 61.60. R & R SPLICE IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 61,645 hrs · 48,282 cycles

STRINGER SPLICE CRACKED AT BS 908, STRINGER 4L. R & R SPLICE IAW EA.

Part: WEB — CORRODED (CARGO DOOR) · airframe 61,645 hrs · 48,282 cycles

AFT CARGO COMPARTMENT DOOR LOWER SILL WEB CORRODED. R & R WEB IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,645 hrs · 48,282 cycles

CLIP ANGLE CRACKED AT BS 330.7+6, BETWEEN STRINGER 21L - 22L. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,645 hrs · 48,282 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 21L. R & R CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,645 hrs · 48,282 cycles

AFT CARGO COMPARTMENT ANGLE CRACKED AT BS 947.5+13, BETWEEN STRINGER 24L - 26L. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,645 hrs · 48,282 cycles

AFT CARGO COMPARTMENT ANGLE CRACKED BETWEEN BS 927 - 947.5, BL 0. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,645 hrs · 48,282 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 22L. R & R TIE CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,645 hrs · 48,282 cycles

CLIP ANGLE CRACKED AT BS 325.3+3, BETWEEN STRINGER 21L - 22L. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,645 hrs · 48,282 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STR 25R TO STR 24R. REPAIRED FRAME IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,645 hrs · 48,282 cycles

TIE CLIP CRACKED AT BS 927, STRINGER 25R. R & R TIE CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (E&E BAY) · airframe 61,645 hrs · 48,282 cycles

LEFT SIDE EQUIPMENT ELECTRONIC COMPARTMENT ANGLE CRACKED BETWEEN BS 294.5 - 312. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (R1 DOOR) · airframe 61,645 hrs · 48,282 cycles

R1 DOOR SKIN CRACKED BETWEEN BS 312 TO BS 344, BETWEEN STR 16R TO STR 18R. REPAIRED SKIN IAW EA.

Part: SPLICE — CRACKED (LT WING) · airframe 61,645 hrs · 48,282 cycles

LEFT WING REAR SPAR UPPER CHORD SPLICE CRACKED ON RSS 214.14. REPAIRED SPLICE IAW EA.

Part: SKIN — DELAMINATED (LT AILERON TAB) · airframe 61,645 hrs · 48,282 cycles

LEFT WING AILERON TAB LOWER SKIN DELAMINATED. REPAIRED TAB IAW SRM.

Part: SPLICE — CRACKED (RT WING) · airframe 61,645 hrs · 48,282 cycles

RT WING REAR SPAR UPPER CHORD SPLICE CRACKED ON RSS 224.14. REPAIRED SPLICE IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,645 hrs · 48,282 cycles

FORWARD CARGO COMPARTMENT ANGLE CLIP CRACKED AT BS 380, STRINGER 26L. R & R ANGLE CLIP IAW SRM & DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 61,645 hrs · 48,282 cycles

SHEAR TIE CRACKED AT BS 520, BETWEEN STRINGER 28L - 27L. R & R SHEAR TIE IAW SRM & DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 61,645 hrs · 48,282 cycles

LEFT HORIZONTAL STABILIZER RIB LOWER CHORD CRACKED ON STAB STATION 120.30. R & R CHORD IAW SRM & DWG.

Part: FLASHLIGHT — CRACKED (CABIN) · airframe 61,645 hrs · 48,282 cycles

FORWARD GALLEY AREA FLASHLIGHT BASE CRACKED. R & R FLASHLIGHT ASSEMBLY IAW CMM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 61,645 hrs · 48,282 cycles

STRINGER SPLICE CRACKED AT BS 360, STRINGER 14L. R & R SPLICE IAW SRM.

Part: HINGE FITTING — CORRODED (RT HORIZ STAB) · airframe 61,645 hrs · 48,282 cycles

RIGHT HORIZONTAL STABILIZER CENTER SECTION HINGE FITTING CORRODED AT FORWARD LOWER LUG OTBD SIDE. REPAIRED FITTING IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,645 hrs · 48,282 cycles

RIGHT WING INBD FORE FLAP UPPER SKIN DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: SKIN — DELAMINATED (LT AILERON TAB) · airframe 61,645 hrs · 48,282 cycles

LEFT WING AILERON TAB LOWER SKIN DELAMINATED. REPAIRED SKIN IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,645 hrs · 48,282 cycles

RIGHT WING OTBD FORE FLAP DELAMINATED AT UPPER SURFACE 84 INCHES OF INBD END. REPAIRED FORE FLAP IAW SRM.

Part: HINGE FITTING — CORRODED (RT HORIZ STAB) · airframe 61,645 hrs · 48,282 cycles

RIGHT HORIZONTAL STABILIZER CENTER SECTION HINGE BEARING FITTING CORRODED ON INNER RACE. REPAIRED FITTING IAW EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 61,645 hrs · 48,282 cycles

SPLICE CHANNEL CRACKED AT BS 360, STRINGER 14L. R & R CHANNEL IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,645 hrs · 48,282 cycles

FRAME CORRODED AT BS 867, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,645 hrs · 48,282 cycles

SKIN CRACKED AT BS 520+9.5, LBL 5. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 61,645 hrs · 48,282 cycles

L1 DOOR AFT SIDE UPPER SURFACE ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 61,156 hrs · 47,964 cycles

L1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM.

Part: RETAINER — CRACKED (FLASHLIGHT) · airframe 60,318 hrs · 47,391 cycles

FORWARD CABIN OTBD FLASHLIGHT RETAINER CRACKED. R & R RETAINER IAW SIP.

Part: SPOILER — DELAMINATED (RT WING) · airframe 60,213 hrs · 47,320 cycles

RIGHT WING NR 7 FLIGHT SPOILER DELAMINATED AT TE OF SPOILER. R & R SPOILER IAW AMM.

Part: SLIDING WINDOW — FAULTY (COCKPIT) · airframe 60,145 hrs · 47,277 cycles

DIVERSION, FIRST OFFICERS SLIDING WINDOW CAME OPEN ON TAKEOFF. R & R SLIDING WINDOW IAW MT.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 60,114 hrs · 47,250 cycles

R1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SPOILER — DELAMINATED (LT WING) · airframe 59,569 hrs · 46,868 cycles

LEFT WING NR 3 SPOILER DELAMINATED, OTBD OF NR 1 ENG. R & R NR 3 SPOILER IAW MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 59,403 hrs · 46,756 cycles

RIGHT WING INBOARD AFT FLAP DELAMINATED ON TRAILING EDGE. R & R AFT FLAP IAW MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 59,380 hrs · 46,734 cycles

R2 DOOR EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: LENS — LOOSE (CABIN) · airframe 58,898 hrs · 46,369 cycles

R2 DOOR EXIT LIGHT LENS LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 57,645 hrs · 45,503 cycles

STRINGER CLIP CORRODED AT BS 538, STRINGER 27R. R & R CLIP IAW SRM.

Part: LENS — DIRTY (CABIN) · airframe 57,645 hrs · 45,503 cycles

OVERWING EMER EXIT LIGHT LENS DISCOLORED. CLEANED LENS IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 57,645 hrs · 45,503 cycles

LEFT CABIN EMER EXIT LIGHT LENS LOOSE AT ROW 1. SECURED LENS IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 56,954 hrs · 45,032 cycles

EMERGENCY BULLNOSE LIGHT LENS LOOSE AT 9 DEF. SECURED LENS IAW MM.

Part: TERMINAL — LOOSE (CABIN) · airframe 56,906 hrs · 45,000 cycles

AFT OVER DOOR EXIT SIGN INOPERATIVE. FOUND GND TERMINAL LOOSE. SECURED GND TERMINAL IAW MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

STRINGER CLIP CRACKED AT BS 380 STRINGER 9L. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

STRINGER CLIP CRACKED AT BS 400 STRINGER 9L. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

STRINGER CLIP CRACKED AT BS 400 STRINGER 8L. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

STRINGER CLIP CRACKED AT BS 440 STRINGER 8L. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

STRINGER CLIP CRACKED AT BS 597 STRINGER 7L. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

STRINGER CLIP CRACKED AT BS 767 STRINGER 11L. R & R CLIP IAW DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

SKIN CRACKED AT BS 380 STRINGER 14R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

SKIN CRACKED AT BS 786 STRINGER 14R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

SKIN CRACKED AT BS 727D+7 STRINGER 14R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

LEFT BS 380 LOWER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

LEFT BS 500A UPPER FWD WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

LEFT BS 500 LOWER AFT WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

LEFT BS 500C UPPER FWD WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

LEFT BS 480 LOWER AFT WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

LEFT BS 500B UPPER FWD WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

LEFT BS 440 UPPER FWD WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

LEFT BS 500C LOWER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

LEFT BS 500B LOWER AFT WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

LEFT BS 520 LOWER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

LEFT BS 500 UPPER FWD WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

LEFT BS 360 UPPER FWD WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

LEFT BS 500A LOWER AFT WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

LEFT BS 480 UPPER FWD WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,906 hrs · 45,000 cycles

LEFT BS 360 LOWER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,906 hrs · 45,000 cycles

RIGHT WING NR 4 SLAT LOWER LE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: BEARING — BROKEN (LT SPOILER) · airframe 56,234 hrs · 44,512 cycles

LEFT WING NR 4 SPOILER OTBD ACTUATOR UPPER HINGE ATTACH BEARING BROKEN. R & R NR 4 SPOILER IAW AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 56,234 hrs · 44,512 cycles

RIGHT EMER EXIT LIGHT OF G4 QUICK DISCONNECT PLUG LOOSE. R & R LIGHT ASSEMBLY IAW SWPM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 56,234 hrs · 44,512 cycles

LEFT CREASE BEAM CRACKED AT BS 639, WL 208. REPAIRED BEAM IAW EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 56,234 hrs · 44,512 cycles

RIGHT CREASE BEAM INNER CHORD CRACKED AT BS 616, WL 208. REPAIRED CHORD IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 56,234 hrs · 44,512 cycles

FORWARD ENTRY DOOR CUT OUT LOWER CORNER SCUFF PLATE SUPPORT ANGLE CRACKED AT LOWER END. REPAIRED ANGLE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,234 hrs · 44,512 cycles

SHEAR TIE CORRODED AT BS 500B, LBL 18. R & R SHEAR TIE IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 56,234 hrs · 44,512 cycles

MAIN WW PRESS DECK CRACKED AT BS 672.5, LBL 40. REPAIRED DECK IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 56,234 hrs · 44,512 cycles

RIGHT WING INBD AFT FLAP DELAMINATED ON LOWER INBD CORNER. REPAIRED AFT FLAP IAW SRM.

Part: PANEL — DELAMINATED (TE FLAP) · airframe 56,234 hrs · 44,512 cycles

RIGHT WING TE FLAP TRACK FAIRING PANEL 3601 DELAMINATED ON FWD LOWER EDGE. REPAIRED PANEL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,234 hrs · 44,512 cycles

RIGHT FRAME OTBD CHORD FWD LOWER FASTENER HOLE CRACKED AT BS 727, STRINGER 18A. REPAIRED CHORD IAW EA.

Part: PANEL — CRACKED (RT MLG WW) · airframe 56,234 hrs · 44,512 cycles

RIGHT MLG WW FWD LOWER CUT OUT PANEL CRACKED AT CORNER NEXT TO FASTENER. REPAIRED PANEL IAW SRM.

Part: BRACKET — CRACKED (L1 DOOR) · airframe 56,234 hrs · 44,512 cycles

L1 DOOR AFT FRAME BRACKET AT DOOR STOP PIN FITTING NR 3 FROM TOP CRACKED. R & R BRACKET IAW SRM.

Part: COVER — LOOSE (CABIN) · airframe 53,114 hrs · 42,241 cycles

FORWARD EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED COVER IAW M/M.

Part: CONTROL UNIT — FAULTY (E&E BAY) · airframe 51,704 hrs · 41,225 cycles

DECLARED EMERGENCY -- FLAPS WOULD NOT EXTEND HYDRAULICALLY (ON APPROACH). EXTEND FLAPS ELECTRICALLY (ALTERNATE FLAP EXTENSION). VIA QRH PROCEDURE - FLAPS EXTENDED TO POS 15 FOR APPROACH AND LANDING. REMOVED AND REPLACED FLAP MOTOR HYD UNIT. SYS CHECKS NORMAL PER MM.

Part: LENS — LOOSE (CABIN) · airframe 51,648 hrs · 41,180 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,046 hrs · 40,739 cycles

L2 DOOR EMERGENCY EXIT LIGHT BULB INOP. RELAMPED LIGHT ASSY PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,046 hrs · 40,739 cycles

L2 DOOR EMERGENCY EXIT LIGHT BULB INOP. RELAMPED LIGHT ASSY PER AMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 51,046 hrs · 40,739 cycles

RIGHT WING O/B FOR FLAP UPPER SURFACE DELAMINATED. REPAIRED FOR FLAP IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 51,046 hrs · 40,739 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FLOOR SUPPORT CHANNEL CRACKED BETWEEN BS 180 AND BS 181, LBL 5.7. REPAIRED CHANNEL IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 294.3, RBL 55. REPAIRED CHORD IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

WEB CRACKED BETWEEN BS 344 TO BS 360, BL 0. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

LEFT SIDE E/E COMPARTMENT ANGLE LOCATED ABOVE OF RACK E1 CRACKED. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

ANGLES CRACKED AT BS 540, BETWEEN STR 28R TO STR 28L. REMOVED AND REPLACED ANGLES IAW SRM AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

STRINGER CRACKED AT BS 595, STR 15R. REPAIRED STRINGER IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

ANGLE CRACKED AT BS 727B, BL 0. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FLOORBEAM WEB CRACKED AT BS 663.75, RBL 45.5. REPAIRED WEB IAW EA AND.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

TIE CLIP CRACKED AT BS 663, STR 10R. REPAIRED TIE CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

VERTICAL ANGLE CRACKED AT BS 693, RBL 24.5. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

TIE CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

ANGLE CRACKED AT BS 578, STR 17R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

ANGLE CRACKED BETWEEN BS 927 TO BS 947, BL 0. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 54,127 hrs · 43,021 cycles

RT FORWARD WING TO BODY FAIRING UPPER DRAG ANGLE CRACKED AT BS 540, STRINGER 21L. REPAIRED ANGLE IAW SRM.

Part: TIE CLIP — MISSING (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

TIE CLIP MISSING AT BS 927, STR 14L. INSTALLED TIE CLIP IAW SRM AND DWG.

Part: LIGHT — DAMAGED (CABIN) · airframe 50,467 hrs · 40,292 cycles

EEPLS DAMAGED. REMOVED AND REPLACED EEPLS IAW AMM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FLOORBEAM CORRODED AT BS 986.5, RBL 45.50. REMOVED AND REPLACED BEAM IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

ANGLE CRACKED AT BS 747, STR 13R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 50,467 hrs · 40,292 cycles

STIFFENER CRACKED AT BS 540, BETWEEN BL 0 TO RBL 24.5. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 50,467 hrs · 40,292 cycles

STIFFENER CRACKED AT BS 540, BETWEEN RBL 25.5 TO RBL 45.5. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 50,467 hrs · 40,292 cycles

STIFFENER CRACKED AT BS 540, BETWEEN BL 0 TO LBL 24.5. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17. REPAIRED BEAM IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 380 TO BS 400, BL 0. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 50,467 hrs · 40,292 cycles

STIFFENER CRACKED AT BS 540, BETWEEN LBL 45.5 TO LBL 70.5. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

SUPPORT ANGLE CRACKED AT BS 967, STR 3L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 50,467 hrs · 40,292 cycles

STIFFENER CRACKED AT BS 540, BETWEEN RBL 45.5 TO RBL 70.53. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

CLIP CRACKED AT BS 685, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FLOORBEAM CORRODED AT BS 312, RBL 11. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FLOORBEAM CORRODED AT BS 360, RBL 2. REPAIRED BEAM IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

CLIP CRACKED AT BS 706, STR 13R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

STRINGER CORRODED AT TORQUE BOX RIGHT SIDE BETWEEN BS 1113 TO BS 1121. REMOVED AND REPLACED STRINGER IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

TIE CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

STRINGER CORRODED AT BS 986.5, 27L. REPAIRED STRINGER IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FLOORBEAM CORRODED AT BS 344, BETWEEN LBL 5 TO LBL 13. REPAIRED BEAM IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

Z-ANGLE CORRODED BETWEEN BS 270 TO BS 360, RBL 56. REPAIRED Z-ANGLE IAW EA AND EO.

Part: ANGLE — CRACKED (RT WING) · airframe 50,467 hrs · 40,292 cycles

RIGHT WING FIXED TRAILING EDGE ANGLE CRACKED BETWEEN WBL 203.00 AND WBL 212. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 50,467 hrs · 40,292 cycles

LEFT WING NR 2 SLAT SKIN DELAMINATED ON OUTBOARD EDGE OF TRAILING EDGE. REPAIRED SKIN IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FRAME CORRODED AT BS 500C, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME IAW SRM.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 50,467 hrs · 40,292 cycles

RIGHT WING NR 6 SPOILER UPPER SKIN DELAMINATED. REMOVED AND REPLACED SPOILER IAW AMM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FITTING CRACKED AT BS 332.1, STR 8R. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

ANGLE CRACKED BETWEEN BS 294.5 TO BS 303.9, STR 16L. REMOVED AND REPLACED ANGLE IAM SRM AND DWG.

Part: FITTING — CORRODED (GIRT BAR) · airframe 50,467 hrs · 40,292 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING BOLTS CORRODED. REMOVED AND REPLACED FITTING ASSY IAW AMM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 50,467 hrs · 40,292 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING BOLTS CORRODED. REMOVED AND REPLACED FITTING ASSY IAW AMM.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

TIE CLIP CORRODED AT BS 947.5, STR 20L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FRAME CRACKED AT BS 312, BETWEEN STR 5L TO STR 6L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FRAME SHEAR TIE CORRODED AT BS 767, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED FRAME IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FRAME SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED FRAME IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FRAME SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED FRAME IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FRAME SHEAR TIE CORRODED AT BS 767, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED FRAME IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FRAME CRACKED AT BS 727C, STR 27R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FRAME CORRODED AT BS 727D, BETWEEN STR 25L AND STR 26R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FRAME SHEAR TIE CORRODED AT BS 747, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED FRAME IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FUSELAGE FRAME CORRODED AT BS 787, BETWEEN STR 26R & STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FRAME SHEAR TIE CORRODED AT BS 767, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED FRAME IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FUSELAGE FRAME CORRODED AT BS 787, BETWEEN STR 27L & STR 27R. REPAIRED FRAME PER SRM.

Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 52,382 hrs · 41,713 cycles

CRACK ON UPPER DRAG ANGLE AT BS 540 LEVEL OF STR 21L LOCATED LEFT FORWARD WING TO BODY FAIRING. PERFORMED REPAIRED ON UPPER DRAG ANGLE AT BS 540 LEVEL OF STR 211 LOCATED LEFT FORWARD WING TO BODY FAIRING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FUSELAGE FRAME CORRODED AT BS 727E, BETWEEN STR 25R & STR 26R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FRAME SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED FRAME IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FRAME CORRODED AT BS 727B, STR 27L. REPAIRED FRAME IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

SUPPORT ANGLE CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 660 TO BS 670, RBL 24.5. REPAIRED CHORD IAW EA AND EO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

SUPPORT ANGLE CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FLOORBEAM CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM IAW EO AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FLOORBEAM WEB CRACKED BETWEEN BS 707 TO 709, RBL 24.5. REPAIRED WEB IAW EA AND EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

FRAME CORRODED BETWEEN BS 500A, BETWEEN STR 27L TO STR 28L. REPAIRED FRAME IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

WEB CRACKED BETWEEN BS 500A TO BS 500B, STR 26R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,467 hrs · 40,292 cycles

LEFT WING NR 1 SLAT SKIN CRACKED ON LEADING EDGE. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,467 hrs · 40,292 cycles

SKIN CRACKED AT BS 520+8, STR 28R. REPAIRED SKIN IAW EA.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 50,467 hrs · 40,292 cycles

LEFT WING NR 2 SLAT SKIN TRAILING EDGE DELAMINATED. REPAIRED SKIN IAW SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 50,467 hrs · 40,292 cycles

RIGHT WING NR 5 SLAT SKIN OF UPPER SURFACE INBOARD EDGE DELAMINATED. REPAIRED SKIN IAW SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 50,467 hrs · 40,292 cycles

RIGHT WING NR 4 SLAT INBOARD EDGE DELAMINATED. REPAIRED NR 4 SLAT IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 50,047 hrs · 39,967 cycles

L1 DOOR EMERGENCY EXIT LIGHT LOOSE. SECURED LENS PER MM.

Part: SIGN — CRACKED (CABIN) · airframe 49,462 hrs · 39,543 cycles

L1 DOOR LOWER EMERGENCY EXIT SIGN CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: LENS — BROKEN (CABIN) · airframe 48,194 hrs · 38,581 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,194 hrs · 38,581 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED PER MM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 47,535 hrs · 38,078 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. RE-INSTALLED LENS PER MM.

Part: SKIN — CRACKED (LT WING) · airframe 47,374 hrs · 37,959 cycles

DURING SCHEDULED SPV CHECK FOUND, LT WING L/E CRACKED AT STA 208. REPAIRED WING PER EA.

Part: COVER — BROKEN (EXIT SIGN) · airframe 47,412 hrs · 37,985 cycles

LEFT GALLEY EMERGENCY EXIT SIGN COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,370 hrs · 37,958 cycles

DURING SCHEDULED OTS CHECK FOUND, SKIN CRACKED AT 380-1, STR 28L. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,374 hrs · 37,959 cycles

DURING SCHEDULED SPV CHECK FOUND, LONGITUDINAL FLOORBEAM ANGLE CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED ANGLE PER BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,374 hrs · 37,959 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 380-1, STR 28L. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,374 hrs · 37,959 cycles

DURING SCHEDULED SPV CHECK FOUND, LONGITUDINAL FLOORBEAM ANGLE CRACKED AT BS 639, RBL 45.5. REMOVED AND REPLACED ANGLE PER BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,370 hrs · 37,958 cycles

DURING SCHEDULED 2HC2 CHECK FOUND, SKIN CRACKED AT BS 379, STR 28L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,467 hrs · 40,292 cycles

LEFT WING NR 1 SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER MM.

Part: HOSE — FRAYED (MLG WW) · airframe 47,249 hrs · 37,871 cycles

DIVERSION - LOSS OF HYD B-SYS. FOUND ACOUSTIC FILTER HYD HOSE FRAYED & LEAKING. REMOVED AND REPLACED HOSE PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CORRODED AT BS 1016, BETWEEN STR 26L TO STR 27R. REPAIRED FRAME PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 1008 TO BS 1010, STR 26R. REMOVED AND REPLACED STRINGER PER SRM AND BAC DWG.

Part: LENS — LOOSE (CABIN) · airframe 46,288 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT FWD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 947, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 44.5. REPAIRED CHORD PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED AT BS 961.5, STR 17R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER ER & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6L. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7L. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 2R. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER ER & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER ER & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10R. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 3R. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8L. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 3R. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5L. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 10R. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7L. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10R. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED CLIP PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM UPPER CHORD LOWER SURFACE CORRODED AT BS 987, RBL 45. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 947, STR 27L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,289 hrs · 37,144 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 44,828 hrs · 36,025 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 44,111 hrs · 35,516 cycles

L1 DOOR EMERGENCY EXIT SIGN COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 43,996 hrs · 35,434 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT UPPER WEDGE SKIN DELAMINATED. REMOVED AND REPLACED NR 5 SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,677 hrs · 35,201 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 510D, STR 10R. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 43,468 hrs · 35,046 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,483 hrs · 34,332 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED BETWEEN BS 843 TO BS 845, STR 1. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 42,484 hrs · 34,332 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SIGN — BROKEN (CABIN) · airframe 41,561 hrs · 33,662 cycles

L2 DOOR EMERGENCY EXIT SIGN BROKEN. R&R SIGN PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 41,006 hrs · 33,254 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD T/E FORE FLAP DELAMINATED AT UPPER SKIN. REMOVED AND REPLACED FORE FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,952 hrs · 33,213 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,904 hrs · 33,177 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,904 hrs · 33,177 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, LBL 9. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,904 hrs · 33,177 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,904 hrs · 33,177 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, LBL 5. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,904 hrs · 33,177 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN RBL 3 TO RBL 9. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 40,904 hrs · 33,177 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CRACKED AT BS 492, STR 22R. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 40,904 hrs · 33,177 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CRACKED AT BS 492, STR 23R. REPAIRED STRINGER PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 40,904 hrs · 33,177 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT KEEL BEAM CORRODED BETWEEN BS 715 TO BS 725. REPAIRED BEAM PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,904 hrs · 33,177 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN LBL 4 TO RBL 5. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,904 hrs · 33,177 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,904 hrs · 33,177 cycles

DURING SCHEDULED 12Y CHECK, FOUND RADIO ALTIMETER ANTENNA SKIN CUTOUT CRACKED AT BS 407, RBL 3. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,904 hrs · 33,177 cycles

DURING SCHEDULED 12Y CHECK, FOUND RADIO ALTIMETER ANTENNA SKIN CUTOUT CRACKED AT BS 413, RBL 3. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,904 hrs · 33,177 cycles

DURING SCHEDULED 12Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 673, LBL 24. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,904 hrs · 33,177 cycles

DURING SCHEDULED 12Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BETWEEN BS 664 TO BS 668, LBL 24. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,904 hrs · 33,177 cycles

DURING SCHEDULED 12Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 662, RBL 24. REPAIRED BEAM PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,904 hrs · 33,177 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 787, BETWEEN STR 24L TO STR 25L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,904 hrs · 33,177 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,904 hrs · 33,177 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CRACKED AT BS 312, BETWEEN RBL 20 TO RBL 22. REPAIRED BEAM PER SRM.

Part: WINDOW — ARCED (COCKPIT) · airframe 40,345 hrs · 32,791 cycles

DURING SCHEDULED MV1 CHECK, COCKPIT L1 WINDOW ARCED. REMOVED AND REPLACED L1 WINDOW ASSY PER MM.

Part: FITTING — CRACKED (LT MLG) · airframe 39,526 hrs · 32,197 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT MLG FWD WALKING BEAM FITTING CRACKED. R&R FITTING PER MM.

Part: BEAM — CRACKED (178 BULKHEAD) · airframe 39,364 hrs · 32,068 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD PRESSURE BULKHEAD VERTICAL BEAM CRACKED AT BS 178, LBL 17. REPAIRED BEAM PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 39,314 hrs · 32,029 cycles

L1 DOOR EMERGENCY EXIT LOWER LIGHT LOOSE. SECURED LIGHT PER SWA EA.

Part: ENGINE — DISTORTED (NR 1) · airframe 35,914 hrs · 29,448 cycles

DURING SCHEDULED HC1 CHECK, FOUND NR 1 ENGINE 1ST STAGE LPT BLADES DISTORTED. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM WEB CORRODED AT BS 1003, RBL 50. REMOVED AND REPLACED FLOORBEAM WEB PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — CRACKED (CABIN) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 64, WL 200. REPAIRED FRAME SECTION PER ER.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR CUTOUT FWD FRAME UPPER HINGE FITTING UPPER HALF CRACKED. REMOVED AND REPLACED HINGE FITTING PER SWA EA.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR CUTOUT FWD FRAME LOWER HINGE FITTING UPPER HALF CRACKED. REMOVED AND REPLACED HINGE FITTING PER SWA EA AND SB.

Part: FLOORBEAM — CRACKED (BS 947) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 54, WL 207. REPAIRED FLOORBEAM PER ER.

Part: STRINGER CLIP — CRACKED (BS 360 S11L) · airframe 34,520 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: DOOR FRAME — CRACKED (BS 348) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR CUTOUT AFT LOWER FRAME CRACKED AT BS 348, WL 209. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SHEAR TIE — CORRODED (BS 807) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807 LBL 10. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: GIRT BAR — CORRODED (R1 DOOR) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FWD GIRT BAR FITTING PER SRM.

Part: GIRT BAR — CORRODED (R1 DOOR) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED AFT GIRT BAR FITTING PER SRM.

Part: FRAME — CRACKED (BS 344 S16L) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 344, STR 16L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 360) · airframe 35,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB) · airframe 35,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT AND LT HORIZONTAL STAB FITTING CLEVIS LUG FACES CORRODED. REPAIRED HORIZONTAL STAB PER SRM.

Part: SKIN — CHAFED (TAIL) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SKIN CHAFED AT BS 1148, BELOW RT HORIZONTAL STAB REAR LUGS. REPAIRED SKIN PER BOEING DRAWING AND SRM.

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD MID FLAP INBOARD CARRIAGE CORRODED AT TORQUE TUBE ATTACHMENT BORE. REMOVED AND REPLACED INBOARD CARRIAGE PER MM.

Part: CARRIAGE — CORRODED (T/E FLAP) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD MID FLAP OUTBOARD CARRIAGE CORRODED AT TORQUE TUBE ATTACHMENT BORE. REMOVED AND REPLACED OUTBOARD CARRIAGE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — DEBONDED (T/E FLAP) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP LOWER SKIN DISBONDED AT OUTBOARD T/E. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME SECTION CRACKED AT BS 400, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: TORQUE TUBE — CORRODED (T/E FLAP) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD MID FLAP, OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME SECTION CRACKED AT BS 480, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME SECTION CRACKED AT BS 440, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME SECTION CRACKED AT BS 867, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME SECTION CRACKED AT BS 787, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: TORQUE TUBE — CORRODED (T/E FLAP) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD MID FLAP, INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 14 TO RBL 44. REPAIRED FLOORBEAM PER SRM.

Part: TORQUE TUBE — LOOSE (T/E FLAP) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND LEFT WING INBOARD FOREFLAP OUTBOARD TORQUE TUBE LOOSE. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: TORQUE TUBE — CORRODED (T/E FLAP) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD MIDFLAP TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: HOOK — LOOSE (R2 DOOR GIRT BAR) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. REMOVED AND REPLACED AFT GIRT BAR HOOK PER SRM.

Part: SHEAR TIE — CORRODED (BS 986 S24R) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986.5, STR 24R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986.5, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 34,250 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CRACKED AT BS 328, LBL 29. REPAIRED FLOORBEAM PER SRM.

Part: ARM — CORRODED (RT WING CARRIAGE) · airframe 34,280 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD MID FLAP OUTBOARD CARRIAGE OUTBOARD ARM CORRODED. REMOVED AND REPLACED CARRIAGE ARM PER MM.

Part: ARM — CORRODED (RT WING CARRIAGE) · airframe 34,280 hrs · 28,171 cycles

DURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD MID FLAP OUTBOARD CARRIAGE INBOARD ARM CORRODED. REMOVED AND REPLACED CARRIAGE ARM PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 34,056 hrs · 28,012 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 34,056 hrs · 28,012 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FRAME — CRACKED (BS 178) · airframe 32,298 hrs · 26,634 cycles

DURING SCHEDULED SPV CHECK, FOUND LT SIDE FRAME CRACKED AT BS 178, WL 207. REMOVED AND REPLACED LT FRAME PER ACO.

Part: FRAME — CRACKED (BS 178) · airframe 32,298 hrs · 26,634 cycles

DURING SCHEDULED SPV CHECK, FOUND RT SIDE FRAME CRACKED AT BS 178, WL 207. REMOVED AND REPLACED RT FRAME PER ACO.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 31,385 hrs · 25,925 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF LIMITS (L1 DOOR) · airframe 31,320 hrs · 25,880 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATED OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 30,806 hrs · 25,459 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT COVER CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 30,040 hrs · 24,882 cycles

DURING SCHEDULED RON CHECK, FOUND FWD CABIN PHOTOLUMINESCENT STRIP DAMAGED. REMOVED AND REPLACED STRIP PER MM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 29,726 hrs · 24,624 cycles

DURING SCHEDULED RON CHECK, FOUND FWD CABIN PHOTOLUMINESCENT STRIP LOOSE AT FWD END. REMOVED AND REPLACED STRIP PER MM.

Part: SHUTOFF VALVE — FAILED (NR 2 ENGINE) · airframe 26,644 hrs · 22,161 cycles

INFLIGHT SHUTDOWN, AT FL 330, NR 2 ENGINE RPM'S ROLLED BACK JUST PRIOR TO TOP OF DESCENT. ENGINE SHUT DOWN AND INFLIGHT ENGINE START PROCEDURES ACCOMPLISHED. ALL ENGINE PARAMETERS NORMAL. REMOVED AND REPLACED NR 2 ENGINE FUEL SHUTOFF VALVE ACTUATOR AND CANNON PLUG D790 PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 25,831 hrs · 21,500 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB AT BS 672, LBL 31, CRACKED. REPAIRED WEB PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 25,831 hrs · 21,500 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR CUTOUT AFT FRAME DOOR, CRACKED. REPAIRED DOOR FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,831 hrs · 21,500 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 944, RBL 13.8, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,831 hrs · 21,500 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 860 LBL 17 TO RBL 13.8, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 25,831 hrs · 21,500 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FRAMES AT BS 770, STRINGER 8L AND STRINGER 12L, CORRODED. REPAIRED FRAME SECTIONS PER EA.

Part: FITTING — CORRODED (RT MLG) · airframe 25,572 hrs · 21,296 cycles

DURING RON CHECK, FOUND RT MLG FWD INBOARD STABILIZER FITTING CORRODED. REPAIRED RT MLG INBOARD FITTING PER EA.

Part: FITTING — CORRODED (RT MLG) · airframe 25,572 hrs · 21,296 cycles

DURING RON CHECK, FOUND RT MLG WALKING BEAM FWD FITTING CORRODED. REPAIRED RT MLG WALKING BEAM FITTING PER EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 23,953 hrs · 20,031 cycles

R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 22,984 hrs · 19,250 cycles

DURING SCHEDULED C2 CHECK, FOUND RT OUTBD T/E AFT FLAP DELAMINATED AT INBD END. REMOVED AND REPLACED RT OUTBD T/E AFT FLAP PER MM.

Part: SKIN — DELAMINATED (RT WING LE FLAP) · airframe 22,984 hrs · 19,250 cycles

DURING SCHEDULED C2 CHECK, FOUND RT INBD T/E FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED RT INBD T/E FORE FLAP PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 20,731 hrs · 17,455 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SLIDE — DEPLOYED (FWD SVC DOOR) · airframe 20,447 hrs · 17,249 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE DEPLOYED WHILE OPENING DOOR. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (ALL CABIN DOORS) · airframe 19,150 hrs · 16,199 cycles

DURING SCHEDULED C2 CHECK, FOUND ALL 4 CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: SLAT — CRACKED (RT WING) · airframe 19,141 hrs · 16,195 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 6 L/E SLAT CRACKED ON LOWER SKIN. REMOVED AND REPLACED NR 6 L/E SLAT PER MM.

Part: BRACKET — LOOSE (FWD ENTRY DOOR) · airframe 18,781 hrs · 15,882 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED BRACKET PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 18,712 hrs · 15,825 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 18,237 hrs · 15,469 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LENS — LOOSE (FUSELAGE) · airframe 17,872 hrs · 15,196 cycles

DURING SCHEDULED RON, FOUND LT OVERWING EXTERIOR EMERGENCY EXIT LOWER LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 17,144 hrs · 14,620 cycles

DURING SCHEDULED A2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: COVER — MISSING (CABIN) · airframe 17,025 hrs · 14,512 cycles

FOUND EEPLS WIRE COVER MISSING. INSTALLED EEPLS WIRE COVER.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 16,619 hrs · 14,161 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: COVER — MISSING (CABIN) · airframe 16,748 hrs · 14,568 cycles

EEPLS LOOSE AND COVER MISSING AT OVERWING EXIT. INSTALLED COVER AND SECURED EEPLS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 15,915 hrs · 13,542 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 15,285 hrs · 12,998 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE ASSY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 15,264 hrs · 12,982 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R&R LENS PER MM.