N635SW

Part: SPAR — CRACKED (LT HORIZ STAB) · airframe 64,087 hrs · 50,181 cycles

LEFT HORIZONTAL STABILIZER CRACKED APPROXIMATELY 1" ON AFT SPAR FORWARD. REPAIRED STABILIZER IAW SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 63,334 hrs · 49,699 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER TC AND AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

FORWARD GALLEY AREA, INTERCOSTAL CRACKED, BETWEEN BS 332 - 344, STRINGER 8R. REPAIRED TEE BRACKET IAW EA.

Part: GLOWSTRIP — BROKEN (CABIN) · airframe 61,842 hrs · 48,706 cycles

AFT CABIN PHOTO LUMINESCENT FLOOR PROXIMITY LIGHTING STRIP BROKEN. R & R STRIP IAW AMM.

Part: SKIN — CRACKED (RT WING) · airframe 61,842 hrs · 48,706 cycles

RIGHT WING UPPER SKIN CRACKED AT STATION RSS 255.5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,842 hrs · 48,706 cycles

RIGHT WING UPPER SKIN CRACKED AT STATION RSS 230. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,842 hrs · 48,706 cycles

LEFT WING REAR SPAR UPPER SKIN, CRACKED IN OPEN FASTENER HOLE, LOCATED AT RSS 239. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,842 hrs · 48,706 cycles

LEFT WING REAR SPAR UPPER SKIN, CRACKED IN OPEN FASTENER HOLE, LOCATED AT RSS 267. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,842 hrs · 48,706 cycles

RIGHT WING UPPER SKIN CRACKED AT STATION RSS 155. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,842 hrs · 48,706 cycles

LEFT WING REAR SPAR UPPER SKIN, CRACKED IN OPEN FASTENER HOLE, LOCATED AT RSS 265. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,842 hrs · 48,706 cycles

LEFT WING REAR SPAR UPPER SKIN, CRACKED IN OPEN FASTENER HOLE, LOCATED AT RSS 268. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,842 hrs · 48,706 cycles

LEFT WING REAR SPAR UPPER SKIN, CRACKED IN OPEN FASTENER HOLE, LOCATED AT RSS 235. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,842 hrs · 48,706 cycles

RIGHT WING UPPER SKIN CRACKED AT STATION RSS 269. REPAIRED SKIN IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,842 hrs · 48,706 cycles

LEFT WING INBD FORE FLAP, DELAMINATED ON LOWER SURFACE. REPAIRED FORE FLAP IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 61,842 hrs · 48,706 cycles

RIGHT WING UPPER SKIN CRACKED AT STATION RSS 257. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 61,842 hrs · 48,706 cycles

RIGHT WING REAR SPAR UPPER CHORD WEB CRACKED AT THE UPPER FASTENER HOLE LOCATED RSS 223. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 61,842 hrs · 48,706 cycles

LEFT WING REAR SPAR UPPER CHORD, CRACKED AT UPPER FASTENER HOLE, LOCATED RSS 222. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 61,842 hrs · 48,706 cycles

LEFT WING REAR SPAR WEB, CRACKED AT UPPER FASTENER HOLE, LOCATED RSS 223. REPAIRED WEB IAW EA.

Part: LINK — CORRODED (TE FLAP) · airframe 61,842 hrs · 48,706 cycles

LEFT WING INBD FLAP AFT SWING LINK CORRODED. REPAIRED SWING LINK IAW CMM.

Part: SPAR — CRACKED (LT WING) · airframe 61,842 hrs · 48,706 cycles

LEFT WING REAR SPAR UPPER CHORD, CRACKED AT UPPER FASTENER HOLE, LOCATED RSS 223. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 61,842 hrs · 48,706 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED AT UPPER FASTENER HOLE, LOCATED RSS 223. REPAIRED CHORD IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

STATION 178 BULKHEAD WEB CRACKED AT LBL 17 - LBL 28. REPAIRED WEB IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

STATION 178, BULKHEAD WEB CRACKED AT LBL 17.1. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, LBL 45.5. REPAIRED BEAM IAW EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

AFT CARGO COMPARTMENT, STRINGER SPLICE CORRODED AT BS 907, STRINGER 19L. R & R SPLICE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

TIE CLIP CRACKED AT BS 727A, STRINGER 25R. R & R TIE CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

FORWARD CARGO COMPARTMENT, FRAME CORRODED AT BS 500A, BETWEEN STRINGER 28L - 28R. REPAIRED FRAME IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, LBL 45.5. REPAIRED BEAM IAW EA.

Part: FITTING — CRACKED (LT HORIZ STAB) · airframe 61,842 hrs · 48,706 cycles

LEFT HORIZONTAL STABILIZER ELEVATOR TAB FAIRING FITTING CRACKED. R & R FITTING IAW DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

AFT CARGO COMPARTMENT SUPPORT ZEE, CRACKED AT BS 747, BETWEEN STRINGER 25R - 26R. R & R SUPPORT ZEE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

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

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 61,842 hrs · 48,706 cycles

AFT CARGO COMPARTMENT, CARGO TRACK CRACKED AT BS 747, RBL 13.80. REPAIRED CARGO TRACK IAW SRM.

Part: SKIN — DELAMINATED (AILERON TAB) · airframe 61,842 hrs · 48,706 cycles

LEFT WING AILERON TAB, DELAMINATED ON UPPER SURFACE INBD TE SECTION. REPAIRED TAB IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

R1 DOOR T CHORD INTERCOSTAL CRACKED AT BS 332.1+1.5, STRINGER 8A. REPAIRED INTERCOSTAL IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

AFT CARGO COMPARTMENT, FRAME CORRODED AT BS 747, BETWEEN STRINGER 25L - 26L. REPAIRED FRAME IAW SRM.

Part: TRANSMISSION — CORRODED (TE FLAP) · airframe 61,842 hrs · 48,706 cycles

LEFT WING NR 4 FLAP TRANSMISSION BORE CORRODED. R & R FLAP IAW SRM.

Part: FITTING — CORRODED (RT HORIZ STAB) · airframe 61,842 hrs · 48,706 cycles

RIGHT HORIZONTAL STABILIZER REAR SPAR CTR SECTION ON FITTING CORRODED. REPAIRED FITTING IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

AFT CARGO COMPARTMENT, ANGLE SUPPORT CRACKED, BETWEEN BS 887 TO 907 RT SIDE. R & R ANGLE IAW SRM & DWG.

Part: TRANSMISSION — CORRODED (TE FLAP) · airframe 61,842 hrs · 48,706 cycles

LEFT WING NR 4 FLAP TRACK TRANSMISSION BORE BOLT CORRODED. REPAIRED BORE IAW CMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

FUSELAGE SKIN CRACKED AT STATION 344, STRINGER 17R. REPAIRED SKIN IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

AFT CARGO COMPARTMENT FRAME, CORRODED AT BS 727B, BETWEEN STRINGER 25L - 26L. REPAIRED FRAME IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

FORWARD GALLEY AREA STRAP CRACKED AT BS 328, RBL 44. R & R STRAP IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

WEB INTERCOSTAL CRACKED, BETWEEN BS 344 - 360, BL 0. R & R INTERCOSTAL IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

FORWARD GALLEY AREA STRAP CRACKED AT BS 328, LBL 44. R & R STRAP IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

FORWARD GALLEY AREA STRAP CRACKED AT BS 328, RBL 31. R & R STRAP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

ANGLE CRACKED, BETWEEN BS 344 - 360, LBL 10. R & R ANGLE IAW SRM & DWG.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

FORWARD GALLEY AREA REVEAL CRACKED AT BS 344 AT AFT LOWER LT. R & R REVEAL IAW SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 61,842 hrs · 48,706 cycles

RIGHT WING NR 5 SLAT SKIN DELAMINATED, INBD EDGE. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 61,842 hrs · 48,706 cycles

LEFT WING ANGLE CRACKED ON TE AT WBL 183.40. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 61,842 hrs · 48,706 cycles

RIGHT WING NR 5 SLAT SKIN, CRACKED ON LOWER INBD EDGE. REPAIRED SKIN IAW SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 61,842 hrs · 48,706 cycles

RIGHT WING NR 5 SLAT UPPER SKIN DELAMINATED AT OTBD EDGE. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (ENTRY DOOR) · airframe 61,842 hrs · 48,706 cycles

ENTRY DOOR AFT UPPER EDGE, STRUCTURE ANGLE CRACKED AT FWD GALLEY AREA. R & R ANGLE IAW SRM & DWG.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 61,842 hrs · 48,706 cycles

AFT CARGO COMPARTMENT DOOR ASSEMBLY FRAME CRACKED ON LOWER EDGE. R & R DOOR ASSEMBLY IAW AMM.

Part: SUPPORT ANGLE — CRACKED (L1 DOOR) · airframe 61,842 hrs · 48,706 cycles

L1 DOOR SUPPORT ANGLE, CRACKED AFT LOWER EDGE STRUCTURE AT AFT GALLEY AREA. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (TAILCONE) · airframe 61,842 hrs · 48,706 cycles

TAIL CONE EXTERNAL SKIN DELAMINATED AT BS 1156, BL 0. REPAIRED SKIN IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

BRACKET CRACKED AT BS 727, LOWER FUSELAGE AT LOWER FUSELAGE LT SIDE. R & R BRACKET IAW SRM & DWG.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 61,842 hrs · 48,706 cycles

REAR SPAR VERTICAL STIFFENER, CRACKED AT MAIN WW AT BS 663.75, RBL 6.15. R & R STIFFENER IAW ACO.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

CENTER WING BOX, LONGITUDINAL FLOORBEAM, UPPER CHORD CRACKED AT BS 727B, RBL 24.50. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,842 hrs · 48,706 cycles

RIGHT WING FIXED LE SKIN CRACKED AT STATION 208. REPAIRED SKIN IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, LBL 45.5. REPAIRED BEAM IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,842 hrs · 48,706 cycles

LEFT WING FIXED LE SKIN CRACKED AT STATION 208. REPAIRED SKIN IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

DOME CAP WEB CRACKED AT BS 1016, LBL 1.5. REPAIRED DOME CAP WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,842 hrs · 48,706 cycles

GROUND AIR HOOK UP DOOR CUT OUT SKIN CRACKED AT BS 520+7, LOWER LT SIDE. REPAIRED SKIN IAW EA.

Part: SIGN — UNSECURE (CABIN) · airframe 61,137 hrs · 48,203 cycles

RIGHT OVERWING EMER EXIT ROW SIGN FELL OFF. SECURED SIGN IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 60,761 hrs · 47,927 cycles

L1 DOOR EMER EXIT LIGHT LENS MISSING. REPLACED LENS IAW MM.

Part: BOTTLE — LOW PRESSURE (EVAC SLIDE) · airframe 59,716 hrs · 47,198 cycles

R1 DOOR EMER EVAC SLIDE BOTTLE PRESS LOW. R & R SLIDE IAW MT.

Part: LENS — LOOSE (CABIN) · airframe 59,160 hrs · 46,816 cycles

L1 DOOR ENTRY EMER EXIT LIGHT LENS LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 57,254 hrs · 45,429 cycles

LEFT OVERWING EMERGENCY EXIT DOOR LIGHT LENS LOOSE. REPAIRED LENS IAW EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 56,869 hrs · 45,167 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 56,653 hrs · 45,025 cycles

INTERIOR EMERGENCY EXIT SIGN LIGHT INOPERATIVE. RELAMPED SIGN ASSEMBLY IAW AMM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 56,653 hrs · 45,025 cycles

LEFT AFT EMERGENCY EXIT SIGN ASSEMBLY INOPERATIVE. R & R SIGN ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,648 hrs · 45,024 cycles

LT EMERGENCY LIGHTS INOPERATIVE AT ROW 2. RELAMPED LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,648 hrs · 45,024 cycles

R1 DOOR EMERGENCY LIGHTS INOPERATIVE AT ROW 2. RELAMPED LIGHT IAW MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

STRINGER CLIP CRACKED AT BS 500A, STRINGER 2R. R & R CLIP IAW SRM & DRAWING.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

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

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

STRINGER DAMAGED AT BS 450, STRINGER 6L. REPAIRED STRINGER IAW SRM.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

STRINGER DAMAGED AT BS 379, STRINGER 6L. REPAIRED STRINGER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

RT BS 380+10 UPPER FWD WINDOW CORNERS SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

RT BS 400+10 UPPER FWD WINDOW CORNERS SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: FORGING — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

LT BS 747+10 WINDOW FORGING CRACKED AT HOLE NR 7. R & R FORGING IAW DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

LT BS 500A+10 LOWER AFT WINDOW CORNER CUTOUT CRACKED. REPAIRED CUTOUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

LT BS 380+10 LOWER AFT WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

LT BS 807+10 LOWER FWD WINDOW CORNER CUTOUT CRACKED. REPAIRED CUTOUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

RT BS 500+10 LOWER AFT WINDOW CORNER CUTOUT CRACKED. REPAIRED CUTOUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

LT BS 400+10 LOWER AFT WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

LT BS 500B+10 UPPER FWD WINDOW CORNER CUTOUT CRACKED. REPAIRED CUTOUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

RT BS 440+10 UPPER FWD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

RT BS 400+10 UPPER FWD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

LT BS 887+10 UPPER AFT WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

RT BS 360+10 LOWER AFT WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

LT BS 887+10 UPPER AFT WINDOW CORNER CUTOUT CRACKED. REPAIRED CUTOUT IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

LT BS 767+10 LOWER FWD WINDOW CORNER CUTOUT CRACKED. REPAIRED CUTOUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

LT BS 867+10 UPPER AFT WINDOW CORNER CUTOUT CRACKED. REPAIRED CUTOUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

RT BS 500A+10 LOWER AFT WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

FUSELAGE SKIN CRACKED AT RT STATION 430, UPPER FWD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

RT BS 500 +10 UPPER FWD WINDOW CORNER CUTOUT CRACKED. REPAIRED CUTOUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

LT BS 787+10 LOWER FWD WINDOW CORNER CUTOUT CRACKED. REPAIRED CUTOUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

FUSELAGE SKIN CRACKED AT LT STATION 877, LOWER FWD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

LT BS 500C +10 UPPER FWD WINDOW CORNER CUTOUT CRACKED. REPAIRED CUTOUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

RT BS 380+10 LOWER AFT WINDOW CORNER CUTOUT CRACKED. REPAIRED CUTOUT IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

RT BS 500C+10 LOWER AFT WINDOW CORNER SKIN CUTOUT CRACKED. REPAIR CUTOUT IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

LT BS 440 +10 UPPER FWD WINDOW CORNER CUTOUT CRACKED. REPAIRED CUTOUT IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

LT BS 460+10 LOWER AFT WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

FUSELAGE SKIN CRACKED AT RT STATION 530, UPPER FWD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

RT BS 520+10 UPPER FWD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

RT BS 500B+10 LOWER AFT WINDOW CORNER CUTOUT CRACKED. REPAIRED CUTOUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

FUSELAGE SKIN CRACKED AT LT STATION 410, UPPER FWD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

RT BS 380+10 UPPER FWD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

FUSELAGE SKIN CRACKED AT RT STATION 470, UPPER FWD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

LT BS 460+10 UPPER FWD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

LT BS 847+10 LOWER FWD WINDOW CORNER CUTOUT CRACKED. REPAIRED CUTOUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

RT BS 440+10 LOWER AFT WINDOW CORNER CUTOUT CRACKED. REPAIRED CUTOUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

RT BS 520+10 LOWER AFT WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

LT BS 440+10 LOWER AFT WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,648 hrs · 45,024 cycles

LT BS 480+10 UPPER FWD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW SB.

Part: LENS — MISSING (CABIN) · airframe 56,648 hrs · 45,024 cycles

OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS IAW AMM.

Part: FUSE — INOPERATIVE (CABIN) · airframe 56,184 hrs · 44,729 cycles

RT BATTERY CHARGER FUSES INOPERATIVE. R & R FUSES IAW MM.

Part: RIB — CRACKED (LT WING) · airframe 56,184 hrs · 44,729 cycles

LT WING RIB LOWER CHORD AT WBL 135.5 CRACKED ON AFT END BETWEEN STRINGER 2 & STRINGER 3. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 44,729 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 794.5 TO BS 796.25, STRINGER 10R. REPAIRED SKIN IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 56,184 hrs · 44,729 cycles

MLG WW PRESS WEB CRACKED AT BS 665, LBL 31. REPAIRED WEB IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,184 hrs · 44,729 cycles

FUSELAGE FRAME CORRODED AT BS 907, BL 0, WL 164. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 44,729 cycles

RT NLG WW SKIN CRACKED AT BS 258.5, APPROXIMATELY 8 INCHES DOWN FROM THE TOP OF THE DOUBLER, JUST UNDER THE FWD EDGE OF THE DOUBLER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,250 hrs · 44,012 cycles

SKIN CRACKED AT STATION 767+8, STRINGER 10R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,250 hrs · 44,012 cycles

SKIN CRACKED AT STATION 727G+10, STRINGER 10R. REPAIRED SKIN IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 55,241 hrs · 44,005 cycles

RT WING OTBD AFT FLAP DELAMINATED. R&R AFT FLAP IAW AMM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 54,749 hrs · 43,626 cycles

FORWARD ENTRY EMERGENCY EXIT SIGN COVER LOOSE. R & R LENS IAW MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 53,874 hrs · 43,029 cycles

FOUND FWD GALLEY RIGHT SLIDE EMERGENCY LIGHT INOP. FOUND WIRES DISCONNECTED DISPLACED FWD GALLEY FOM RESTORED WIRES REINSTALLED FWD GALLEY PER MM OPS CHECK EMERGENCY LIGHT CHECK GOOD.

Part: LENS — LOOSE (CABIN) · airframe 53,835 hrs · 43,004 cycles

FORWARD ENTRY DOOR MISSING FWD EMERGENCY LIGHT LENS LOOSE. ADJUSTED PER AMM

Part: SNUBBER — OUT OF POSITION (R1 DOOR) · airframe 53,835 hrs · 43,004 cycles

CREW REPORTS GALLEY DOOR HITS FUSELAGE WHEN OPENED. R & R SNUBBER IAW SRM MM.

Part: SIGN — LOOSE (CABIN) · airframe 52,971 hrs · 42,386 cycles

RIGHT EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 52,953 hrs · 42,373 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 52,182 hrs · 41,785 cycles

RIGHT WHEEL WELL BEADED WEB CRACKED AT BS 663. REPAIRED WEB IAW SRM & EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 52,182 hrs · 41,785 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE IAW MT.

Part: LENS — MISSING (EXIT SIGN) · airframe 50,750 hrs · 40,698 cycles

RIGHT EMERGENCY SIDE MISSING EXIT SIGN. RE-INSTALLED LENS PER MM. (SUBMITTED AS A SUPPLEMENT, COULDN`T FIND ORIGINAL CONTROL NUMBER.)

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 947.5 TO BS 980, BETWEEN STR 15R TO STR 19R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 947.5 TO BS 969, BETWEEN STR 15L TO STR 19L. REPAIRED SKIN IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 1006, BETWEEN STR 20R TO STR 22R. REPAIRED FRAME IAW EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT FUSELAGE SKIN CRACKED AT BS 213.8 WINDSHIELD UPPER AREA. REPAIRED SKIN IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 666 TO BS 670, LBL 24.5. REPAIRED CHORD IAW EO AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 670, RBL 24.5. REPAIRED CHORD IAW EO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 379, STR 28L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 312 TO BS 337, BETWEEN STR 15R TO STR 18R. REPAIRED SKIN IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND ATTACHMENT CLIP CRACKED AT BS 639, RBL 45.5. REMOVED AND REPLACED CLIP IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT INNER CHORD CRACKED AT BS 616, WL 208. REPAIRED CHORD PER SW EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CORRODED BETWEEN BS 312 TO BS 344, LBL 64. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR FRAME CRACKED AT UPPER EDGE OF LOWER INNER SKIN. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND CROSS BEAM CORRODED AT BS 344, BETWEEN LBL 34 TO RBL 14. REPAIRED BEAM IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND PRESSURE DECK ANGLE CRACKED AT BS 540, LBL 57. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND CROSS BEAM CORRODED AT BS 328, BETWEEN LBL 13 TO RBL 57. REPAIRED BEAM IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND PRESSURE DECK ANGLE CRACKED BETWEEN BS 540 TO BS 548, LBL 32. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT ANGLE CORRODED AT BS 773, LBL 12.5. REMOVED AND REPLACED ANGLE IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT ANGLE CORRODED AT BS 773, LBL 3.0. REMOVED AND REPLACED ANGLE IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 22R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND VERTICAL ANGLE CRACKED AT BS 727, STR 27L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT ANGLE CORRODED BETWEEN BS 540 TO BS 548, RBL 31.5. REMOVED AND REPLACED ANGLE IAW EA AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT ANGLE CORRODED AT BS 773, RBL 3.0. REMOVED AND REPLACED ANGLE IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED AT BS 947.5, LBL 454.5+8. REPAIRED BEAM IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 540, BL 0. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND DOUBLER CORRODED BETWEEN BS 967 TO BS 986.5, BETWEEN STR 22R TO STR 25R. REMOVED AND REPLACED DOUBLER IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 947.5, STR 19L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 500D TO BS 500C, BETWEEN LBL 64 TO LBL 70. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING AFT FLAP LOWER SKIN DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT LAV WALL EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE FRAYED. REMOVED AND REPLACED CABLE IAW DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,669 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: BRACKET — CORRODED (L1 DOOR) · airframe 50,383 hrs · 40,431 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH BRACKET CORRODED. REMOVED AND REPLACED BRACKET PER SRM.

Part: BLOCK — LOOSE (GIRT BAR) · airframe 46,766 hrs · 37,694 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR RETAINING BLOCK LOOSE. SECURED BLOCK PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 46,714 hrs · 37,655 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING I/B AFT FLAP O/B END TRAILING EDGE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 46,714 hrs · 37,655 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 6 SLAT OUTER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 46,714 hrs · 37,655 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 45,923 hrs · 37,035 cycles

DURING SCHEDULED CV CHECK, FOUND L1 DOOR EVAC GIRT ASSY FRAYED. REMOVED AND REPLACED SLIDE ASSY PER MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 45,923 hrs · 37,035 cycles

DURING SCHEDULED CV CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF POSITION. REMOVED AND REPLACED SLIDE ASSY PER MT.

Part: FLAP — DELAMINATED (LT WING) · airframe 45,249 hrs · 36,536 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,249 hrs · 36,536 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 668, RBL 24. REPAIRED BEAM PER ER.

Part: FLAP — DELAMINATED (RT WING) · airframe 45,249 hrs · 36,536 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING I/B AFT FLAP DELAMINATED ON O/B END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FLAP — CHAFED (LT WING) · airframe 45,249 hrs · 36,536 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING O/B MID FLAP L/E CHAFED. REMOVED AND REPLACED MID FLAP PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,249 hrs · 36,536 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708, LBL 24.5. REPAIRED WEB PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,249 hrs · 36,536 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 657 TO BS 669, LBL 24. REPAIRED BEAM PER ER.

Part: WIRE — DAMAGED (COCKPIT) · airframe 45,249 hrs · 36,536 cycles

DURING SCHEDULED 14Y CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REPAIRED WIRE PER WDM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,249 hrs · 36,536 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD AFT END CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM PER ER.

Part: TAB — DELAMINATED (AILERON) · airframe 45,249 hrs · 36,536 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING AILERON TAB LOWER SURFACE O/B END DELAMINATED. REMOVED AND REPLACED TAB PER MM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 45,249 hrs · 36,536 cycles

DURING SCHEDULED 14Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 185, LBL 17. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,249 hrs · 36,536 cycles

DURING SCHEDULED 14Y CHECK, FOUND VERTICAL BEAM WEB CRACKED BETWEEN BS 178 TO BS 183, RBL 17. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,249 hrs · 36,536 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,249 hrs · 36,536 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,249 hrs · 36,536 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,249 hrs · 36,536 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 45,249 hrs · 36,536 cycles

DURING SCHEDULED 14Y CHECK, FOUND ANGLE CRACKED AT BS 293, BETWEEN STR 9R TO STR 10R. REMOVED AND REPLACED ANGLE PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 45,249 hrs · 36,536 cycles

DURING SCHEDULED 14Y CHECK, FOUND ANGLE CRACKED AT BS 293, BETWEEN STR 12R TO STR 13R. REMOVED AND REPLACED ANGLE PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 45,249 hrs · 36,536 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE ANGLE CRACKED AT R1 DOOR UPPER HINGE CUTOUT, BS 291, WL 255. REMOVED AND REPLACED ANGLE PER SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 43,610 hrs · 35,310 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN DAMAGED AT BS 1048, BETWEEN STR 24L TO STR 25L. REPAIRED SKIN PER SWA EA.

Part: HOLDER — OUT OF ADJUST (GIRT BAR) · airframe 42,387 hrs · 34,402 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOLDER OUT OF ADJUST. ADJUSTED HOLDER PER MM.

Part: LENS — CRACKED (CABIN) · airframe 42,014 hrs · 34,138 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT SIGN LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 42,014 hrs · 34,138 cycles

DURING SCHEDULED HC1 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT PER MM.

Part: TRACK — DAMAGED (CABIN) · airframe 42,014 hrs · 34,138 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT EEPLS TRACK DAMAGED BETWEEN ROW 12 TO ROW 13. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 41,890 hrs · 34,057 cycles

L1 DOOR EMERGENCY EXIT LIGHT BROKEN. R&R LIGHT PER MM.

Part: LENS — LOOSE (CABIN) · airframe 39,368 hrs · 32,268 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,108 hrs · 32,068 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,108 hrs · 32,068 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,108 hrs · 32,068 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500C, STR 27L TO STR 26R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,108 hrs · 32,068 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,108 hrs · 32,068 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,108 hrs · 32,068 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 787, STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,108 hrs · 32,068 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,108 hrs · 32,068 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,108 hrs · 32,068 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,108 hrs · 32,068 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 38,876 hrs · 31,896 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,876 hrs · 31,896 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 38,509 hrs · 31,616 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 38,165 hrs · 31,330 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 36,454 hrs · 30,022 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 34,676 hrs · 28,648 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 34,572 hrs · 28,565 cycles

RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,970 hrs · 28,112 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: RIB — CRACKED (RT WING) · airframe 32,900 hrs · 27,263 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING RIB CRACKED AT WBL 135.5, BETWEEN STR 2 AND STR 3. REPAIRED WING RIB PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663 S9L) · airframe 32,900 hrs · 27,263 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 32,900 hrs · 27,263 cycles

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

Part: STRINGER CLIP — CRACKED (BS 663 S10R) · airframe 32,900 hrs · 27,263 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLAP TRACK — CORRODED (RT WING) · airframe 32,900 hrs · 27,263 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING T/E MID FLAP CETER FORE FLAP TRACK CORRODED. REMOVED AND REPLACED FORE FLAP TRACK PER CMM AND SRM.

Part: FRAME — CRACKED (BS 727D S8L-8R) · airframe 32,900 hrs · 27,263 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, AT STR 8L AND STR 8R. REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: FLOORBEAM — CORRODED (BS 989) · airframe 32,900 hrs · 27,263 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM WEB CORRODED AT BS 989, RBL 48. REMOVED AND REPLACED FLOORBEAM WEB PER SRM.

Part: FLOORBEAM — CORRODED (BS 987) · airframe 32,900 hrs · 27,263 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, FROM LBL 55 TO RBL 55. REPAIRED FLOORBEAM PER ER.

Part: HINGE FITTING — CORRODED (FUSELAGE) · airframe 32,900 hrs · 27,263 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR LOWER HINGE FITTING CORRODED. REMOVED AND REPLACED L1 DOOR HINGE FITTING PER SWA EA AND SRM.

Part: FRAME — CRACKED (BS 907 S8R) · airframe 32,900 hrs · 27,263 cycles

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

Part: FLOORBEAM — CRACKED (BS 246) · airframe 32,900 hrs · 27,263 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 246, RBL 23, WL 208. REPAIRED FLOORBEAM WEB PER SRM.

Part: FRAME — CRACKED (BS 867 S8R) · airframe 32,900 hrs · 27,263 cycles

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

Part: TORQUE TUBE — CORRODED (RT WING TE FLAP) · airframe 32,900 hrs · 27,263 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING T/E MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED INBOARD TORQUE TUBE PER CMM AND SRM.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 32,900 hrs · 27,263 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING T/E INBOARD FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: FRAME — CRACKED (BS 727B) · airframe 32,900 hrs · 27,263 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, AT STR 8L AND STR 8R. REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: TORQUE TUBE — CORRODED (RT WING TE FLAP) · airframe 32,900 hrs · 27,263 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING T/E MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED OUTBOARD TORQUE TUBE PER CMM AND SRM.

Part: FRAME — CRACKED (BS 787 S9L) · airframe 32,900 hrs · 27,262 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 9L. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 32,900 hrs · 27,262 cycles

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

Part: DOOR FRAME — CRACKED (BS 296 S6R) · airframe 32,900 hrs · 27,263 cycles

DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR FRAME CUTOUT CRACKED AT BS 296.5, STR 6R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (BS 685 S10R) · airframe 32,900 hrs · 27,262 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 380 S9L) · airframe 32,900 hrs · 27,262 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 9L. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 360 S9R) · airframe 32,900 hrs · 27,262 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 9R. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706 S10R) · airframe 32,900 hrs · 27,262 cycles

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

Part: FRAME — CRACKED (BS 400 S9L) · airframe 32,900 hrs · 27,262 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 9L. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 827 S9L) · airframe 32,900 hrs · 27,262 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED BS 827, STR 9L. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706 S13R) · airframe 32,900 hrs · 27,262 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 13R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 747 S9R) · airframe 32,900 hrs · 27,262 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9R. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 616) · airframe 32,900 hrs · 27,262 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 60, WL 200. REPAIRED FRAME SECTION PER ER.

Part: STRINGER CLIP — CRACKED (BS 616 S4R) · airframe 32,900 hrs · 27,263 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BEARING — BINDING (CENTER BOX) · airframe 31,255 hrs · 26,012 cycles

SHUDDERING AND BINDING FELT IN AILERONS DURING FLIGHT CONTROL CHECK. REMOVED AND REPLACED AILERON CENTERING MECHANISM ROLLER BEARING IAW MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 30,986 hrs · 25,787 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD GALLEY EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 30,986 hrs · 25,787 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR BRACKETS LOOSE. SECURED BRACKETS PER MM.

Part: STRUCTURE — CORRODED (COCKPIT FLOOR) · airframe 30,986 hrs · 25,787 cycles

DURING SCHEDULED C3 CHECK, FOUND COCKPIT FLOOR Z-CHORD CORRODED AT BS 270, BETWEEN LBL 54 TO RBL 54. MX FERRY TO DALLAS. REMOVED AND REPLACED Z-CHORD PER SRM.

Part: FUSE — FAILED (BATTERY CHARGER) · airframe 30,986 hrs · 25,787 cycles

DURING SCHEDULED C3 CHECK, FOUND RT AFT EXTERIOR EMERGENCY LIGHT INOP. REMOVED & REPLACED BATTERY CHARGER FUSE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 30,113 hrs · 25,084 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SOLENOID — FAULTY (MLG HANDLE) · airframe 29,902 hrs · 24,912 cycles

AIR TURNBACK, LANDING GEAR HANDLE WOULD NOT RAISE PAST OFF POSITION. CYCLED LANDING GEARS AND SAME PROBLEM. USED GEAR LEVER OVERRIDE TRIGGER TO RAISE GEARS. REMOVED AND REPLACED LANDING GEAR HANDLE LOCK OUT SOLENOID PER MM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 28,217 hrs · 23,620 cycles

DURING SCHEDULED C4 CHECK, FOUND LT KEELBEAM WEB CRACKED BETWEEN BS 700 TO BS 710. REPAIRED KEELBEAM PER SRM.

Part: HYDRAULIC LINE — LEAKING (NR 2 ENGINE) · airframe 26,521 hrs · 22,263 cycles

AIR TURNBACK, NR 2 ENGINE B-HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED AND B-SYSTEM QUANTITY DROPPED TO 1/4 FULL. REMOVED AND REPLACED NR 2 ENGINE B-SYSTEM HYDRAULIC SUPPLY LINE PER MM.

Part: HYDRAULIC LINE — LEAKING (NR 2 ENGINE) · airframe 26,519 hrs · 22,261 cycles

AIR TURNBACK, DECLARED EMERGENCY. DURING CLIMB NR 2 ENGINE HYD PUMP LOW PRESSURE LIGHT ILLUMINATED, ACCOMPANIED BY HYDRAULIC FLUID QUANTITY INDICATING 1/3 FULL. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PRESSURE LINE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,739 hrs · 21,620 cycles

R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,739 hrs · 21,620 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: FITTING — CORRODED (RT MLG) · airframe 25,616 hrs · 21,537 cycles

DURING SCHEDULED RON CHECK, FOUND RT MLG FORWARD HANGER FITTING PITTED. REPAIRED HANGER FITTING PER EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,461 hrs · 21,428 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: HOOK — SHEARED (L1 DOOR GIRT BAR) · airframe 25,461 hrs · 21,428 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR HOOK FASTENER SHEARED. REMOVED AND REPLACED RETAINER HOOK PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,298 hrs · 21,299 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,298 hrs · 21,299 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: WEDGE — DELAMINATED (L/E SLAT) · airframe 24,533 hrs · 20,668 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT T/E WEDGE DELAMINATED AT OUTBD END. REPAIRED WEDGE PER SRM.

Part: INDICATOR — OUT OF POSITION (SLIDE) · airframe 24,272 hrs · 20,458 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 23,143 hrs · 19,571 cycles

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

Part: LENS — CRACKED (CABIN) · airframe 22,644 hrs · 19,159 cycles

DURING SCHEDULED C2 CHECK, FOUND CEILING EMERGENCY EXIT LIGHT LENS CRACKED IN AFT CABIN. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — DELAMINATED (T/E FOREFLAP) · airframe 22,644 hrs · 19,159 cycles

DURING SCHEDULED C2 CHECK, FOUND LT INBD T/E FOREFLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED LEFT INBD FOREFLAP PER MM.

Part: ROD END — WORN (ELEVATOR TAB) · airframe 19,562 hrs · 16,695 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, ELEVATOR TABS FAILED FREE PLAY INSPECTION. REMOVED AND REPLACED ROD END ASSY'S ON BOTH TABS.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 19,043 hrs · 16,287 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: FRAME — CRACKED (AFT ENTRY DOOR) · airframe 16,729 hrs · 14,436 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT ENTRY DOOR FWD FRAME CRACKED AT CUTOUT FOR #2 STOP. REPAIRED FRAME PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,367 hrs · 14,128 cycles

DURING SCHEDULED PMC CHECK, FOUND TWO EEPLS END CAPS MISSING, AND TWO EEPLS LIGHTS INOP. INSTALLED END CAPS AND RELAMPED EEPLS LIGHTS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 16,273 hrs · 14,043 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT FWD CABIN. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,208 hrs · 13,978 cycles

EEPLS INOP AT ROWS 4 TO 7 AND LOOSE AT ROW 9. REPAIRED AND RESECURED EEPLS PER MM.

Part: COVER — MISSING (CABIN) · airframe 16,178 hrs · 13,956 cycles

EEPLS TRACK COVER MISSING ROWS 9&15. REPLACED COVERS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,156 hrs · 13,938 cycles

EEPLS INOP AT ROW 14. REPAIRED EEPLS PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 15,973 hrs · 13,784 cycles

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

Part: LENS — MISSING (CABIN) · airframe 15,396 hrs · 13,332 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS MISSING RED LENS AT REAR SECTION OF CABIN. INSTALLED TRACK COVER ASSY PER MM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 15,073 hrs · 13,070 cycles

EEPLS TRACK COVER LOOSE AT ROW 15. SECURED TRACK COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 14,972 hrs · 12,987 cycles

EEPLS TRACK COVER MISSING AT MID CABIN. REPLACED TRACK COVER PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 14,823 hrs · 12,863 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REPOSITIONED EVAC SLIDE ASSY PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 14,728 hrs · 12,780 cycles

EEPLS WIRES EXPOSED & DISCONNECTED AT ROW 17. RECONNECTED & STOWED WIRES PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 14,704 hrs · 12,754 cycles

EEPLS WIRES EXPOSED AT CENTER CABIN. RESECURED EEPLS WIRING PER MM.

Part: COVER — MISSING (CABIN FLOOR) · airframe 14,629 hrs · 12,689 cycles

EEPLS TRACK MISSING COVER. REPLACED COVER PER MM.

Part: WIRE — EXPOSED (CABIN FLOOR) · airframe 14,402 hrs · 12,506 cycles

EEPLS WIRES EXPOSED AT ROW 1. REPAIRED TRACK COVERS PER MM.

Part: LIGHT — INOPERATIVE (ROW 12) · airframe 13,964 hrs · 12,142 cycles

EEPLS INOP AT ROW 12. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,515 hrs · 11,736 cycles

EEPLS FWD SECTION INOP. REPAIRED WIRING AND RELAMPED PER MM.

Part: LENS — MISSING (CABIN) · airframe 12,668 hrs · 10,999 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS LENS MISSING NEAR OVERWING EXIT. REPLACED LENS ASSY PER MM.

Part: SLIDE — DISLODGED (ESCAPE SLIDE) · airframe 12,668 hrs · 10,999 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: LIGHT — LOOSE (CABIN)

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK ASSY LOOSE AT FWD END. RESECURED LIGHT ASSY PER MM.

Part: SKIN — DISBONDED (TE FLAP)

DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBD AFT FLAP DISBONDED ON INBD END. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

EEPLS INOP. REPAIRED BROKEN WIRE PER MM.

Part: WIRE — DAMAGED (CABIN)

DURING SCHEDULED WALKAROUND CHECK, FOUND TRACK LIGHTING MISSING COVER. REPAIRED TRACK WIRING PER BOING MM AND REINSTALLED LENS COVER. OPS CKS GOOD.

Part: LIGHT — DAMAGED (CABIN)

DURING SCHEDULED BC1 CHECK, FOUND FLOOR PATH EMERGENCY LIGHT STRIPS HAVE GAPS AND ARE TAPED. INSTALLED NEW FLOOR PATH EMERGENCY LIGHT STRIPS PER BOEING MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND ROW 12 TO 15 FLOOR TRACK LIGHTING INOP. RECONNECTED LOOSE WIRES PER BOEING MM.

Part: SOCKET — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FLOOR TRACK LIGHTS AT ROW 10, 17 HAVE SEVERAL LIGHTS INOP. REPLACED SOCKET ASSY AT ROW 10 AND 17 PER BOEING MM.

Part: SKIN — DENTED (LT HORIZ STAB)

DURING SERVICE CHECK, FOUND LT HORIZONTAL STABILIZER LEADING EDGE DENTED 3 FT OUTBD OF INBD SIDE. REPAIRED PER BOEING SRM.

Part: LIGHTS — INOPERATIVE (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AFT CABIN. FOUND WIRES LOOSE AND DISCONNECTED AT 3 LOCATIONS. RECONNECTED WIRES AND OPS CHK GOOD.

Part: CONNECTORS — LOOSE (CABIN)

ON ARRIVAL, FOUND 5 ROWS OF EMERGENCY EXIT LIGHT INOP AND WIRES DISCONNECTED. RECONNECTED EMERGENCY LIGHT SEGMENT CONNECTOR PINS AND OP CHECKED PER BOEING M/M.

Part: WIRE — LOOSE (CABIN)

DURING SCHEDULED A2 CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT MID CABIN AREA. RESECURED LIGHT WIRES AND OP CHECKED PER BOEING M/M.

Part: LIGHTS — DISCONNECTED (CABIN)

DURING SCHEDULED RON CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOP AT MID CABIN INOP. REINSTALLED WIRING AND OP CHECKED PER BOEING M/M.