N653SW

Part: BULB — OVERHEATED (CABIN LIGHTS) · airframe 60,277 hrs · 46,959 cycles

ELECTRICAL BURNING ODOR FOR 15 TO 20 SECONDS. R & R THE CEILING LIGHT FLUORESCENT BULB IAW AMM.

Part: LENS — DETACHED (EMERGENCY LIGHTS) · airframe 59,745 hrs · 46,589 cycles

L1 DOOR EXIT SIGN LENS COVER FELL OFF. INSTALLED LENS IAW AMM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 59,243 hrs · 46,261 cycles

L1 DOOR EXIT SIGN COVER LOOSE. SECURED SIGN IAW SIP.

Part: WEB — CRACKED (RT WING) · airframe 59,143 hrs · 46,190 cycles

RIGHT WING RSS 193, SECOND HOLE UP FROM THE BOTTOM WEB CRACKED. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 59,143 hrs · 46,190 cycles

RIGHT WING UPPER WING SKIN CRACKED ABOVE RSS 239. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 59,143 hrs · 46,190 cycles

RIGHT WING AFT SPAR WEB CRACKED AT RSS 221.1 IN UPPER FASTENER HOLE. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 59,143 hrs · 46,190 cycles

LEFT WING UPPER SKIN STATION RSS 254 AFT, FASTENER HOLE CRACKED. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (LT WING) · airframe 59,143 hrs · 46,190 cycles

LEFT WING UPPER SKIN TE CRACKED AT STATION RSS 233. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 59,143 hrs · 46,190 cycles

LEFT WING TE SKIN CRACKED AT FASTENER HOLE AT RSS 251. REPAIRED SKIN IAW SRM & EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,143 hrs · 46,190 cycles

R1 DOOR INTERCOSTAL WEB CRACKED AT BS 277, STRINGER 14R. R & R WEB IAW SRM & DWG.

Part: LINK — DAMAGED (LT MLG) · airframe 59,143 hrs · 46,190 cycles

LEFT MLG BEAM SWING LINK ASSEMBLY PITTED ON AFT FACE OF AFT FITTING LOWER BOLT HOLE. R & R SWING LINK IAW AMM.

Part: BRACKET — CRACKED (RT NACELLE) · airframe 59,143 hrs · 46,190 cycles

RIGHT AFT NAC STRUT BRACKET CRACKED AT FAIRING ATTACH POINT. R & R BRACKET IAW DWG & SRM.

Part: SPAR — CRACKED (LT WING) · airframe 59,143 hrs · 46,190 cycles

LEFT WING AFT SPAR UPPER CHORD CRACKED INDICATION IN NR 5 OPENED FASTENER HOLE. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 59,143 hrs · 46,190 cycles

RIGHT WING AFT SPAR UPPER CHORD CRACKED IN NR 5 OPENED FASTENER HOLE. REPAIRED CHORD IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 58,549 hrs · 45,804 cycles

RT OUTBOARD FLOORBEAM STRAP CRACKED BETWEEN BS 312 TO BS 328 INSIDE E/E ACCESS. REPAIRED STRAP PER SRM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 56,787 hrs · 44,576 cycles

R1 DOOR FRAME CRACKED BETWEEN FWD LOWER CAM CUT OUT. R & R FRAME IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 56,787 hrs · 44,576 cycles

RIGHT OVERHEAD BIN EMER LIGHT LENS LOOSE AT ROW 20. SECURED LENS IAW MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,787 hrs · 44,576 cycles

RIGHT WING NR 6 SLAT SKIN LOWER OUTER SURFACE CRACKED. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 56,523 hrs · 44,382 cycles

INBOARD INTERCOSTAL STIFFENER ANGLE CRACKED AT BS 294.5, STRINGER 16L. R & R ANGLE IAW SRM & DWG.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 56,523 hrs · 44,382 cycles

MLG WW PRESS WEB CRACKED AT STATION 672, LBL 42. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,523 hrs · 44,382 cycles

LEFT FUSELAGE FRAME CRACKED AT STATION 727, STRINGER 18A. REPAIRED FRAME IAW EA.

Part: LENS — MISSING (CABIN) · airframe 55,645 hrs · 43,794 cycles

LEFT EMER LIGHT LENS MISSING AT ROW 10. INSTALLED LENS IAW MM.

Part: LIGHT — BROKEN (CABIN) · airframe 55,523 hrs · 43,719 cycles

FORWARD ENTRY EMER EXIT LIGHT BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,960 hrs · 43,347 cycles

STOWAGE BIN MOUNTED EMER FLOODLIGHTS INOPERATIVE BETWEEN ROW 1 - 5. R & R BATTERY IAW AMM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 54,960 hrs · 43,347 cycles

FRAME STRAP CRACKED AT BS 348 STRINGER 16L. REPAIRED STRAP IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 54,216 hrs · 42,810 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB BL 80, 2 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

STRINGER CLIP CRACKED AT BS 559 STRINGER 1. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

STRINGER CLIP CRACKED AT BS 663 STRINGER 4L. R & R CLIP IAW SRM & DWG.

Part: WINDOW — CRACKED (CABIN) · airframe 54,216 hrs · 42,810 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

LEFT FUSELAGE SKIN CRACKED AT STATION 727+10, PAX WINDOW LOWER FWD CUT OUT. REPAIRED SKIN IAW ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

RT BS 500A+10 UPPER FORWARD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

RIGHT BS 500+10 UPPER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

RT BS 420+10 UPPER FORWARD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

LEFT BS 360+10 UPPER FWD WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

LEFT BS 887+0 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

RT BS 400+10 LOWER AFT WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

RIGHT BS 360+10 UPPER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.

Part: WINDOW — CRACKED (CABIN) · airframe 54,216 hrs · 42,810 cycles

RIGHT BS 380+10 UPPER FWD WINDOW CORNER CRACKED. REPAIRED WINDOW IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

RT BS 480+10 UPPER FORWARD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

LT BS 400+10 UPPER FORWARD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

LEFT FUSELAGE SKIN CRACKED AT STATION 727+10, PAX WINDOW UPPER AFT CUT OUT. REPAIRED SKIN IAW ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

RT BS 400+10 UPPER FORWARD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

RT BS 520+10 UPPER FORWARD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

LEFT BS 500+10 UPPER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

RT BS 480+10 LOWER AFT WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: WINDOW — CRACKED (CABIN) · airframe 54,216 hrs · 42,810 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

LT BS 460+10 UPPER FORWARD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

LT BS 500A+10 UPPER FORWARD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

RT BS 500C+10 UPPER FORWARD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

RT BS 500B+10 UPPER FORWARD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

RIGHT BS 360+10 LOWER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

LT BS 420+10 UPPER FORWARD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

LEFT BS 520+10 UPPER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

RT BS 440+10 UPPER FORWARD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

LEFT BS 480+10 UPPER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW SB & TASK CARD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

LEFT BS 500C+10 LOWER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,216 hrs · 42,810 cycles

RIGHT BS 380+10 UPPER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW SB.

Part: FLAP — DELAMINATED (RT WING) · airframe 53,434 hrs · 42,282 cycles

RIGHT WING INBD FORE FLAP DELAMINATED. R & R FORE FLAP IAW MM.

Part: LIGHT — UNSECURE (CABIN) · airframe 52,611 hrs · 41,731 cycles

RT EEPLS FELL OFF AT ROW 13. SECURED EEPLS IAW AMM.

Part: WINDOW — ARCED (COCKPIT) · airframe 52,486 hrs · 41,639 cycles

L2 WINDOW ARCED WITH BURN SPOT ON LT SIDE-EDGE WINDOW L2 HEAT OFF. R & R WINDOW IAW AMM.

Part: GLOWSTRIP — DIRTY (CABIN) · airframe 51,442 hrs · 40,859 cycles

CABIN FLOOR PHOTO LUMINESCENT STRIPS DIRTY. CLEANED EEPLS IAW MM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 51,318 hrs · 40,776 cycles

R1 DOOR EMERGENCY EXIT SIGN LENS BROKEN. R&R LENS ASSEMBLY IAW MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

ANGLE CRACKED AT BS 500, BETWEEN STR 28L AND STR 28R. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

ANGLE CRACKED AT BS 540, STR 21R. REPAIRED ANGLE IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 294.5 TO BS 312. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

TIE CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

UPPER CHORD OF FLOORBEAM CRACKED AT BS 328, BETWEEN LBL 31 AND LBL 38. REPAIRED CHORD IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

STRAP CRACKED BETWEEN BS 312 TO BS 360, LBL 50. REMOVED AND REPLACED STRAP IAW SRM AND DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FRAME CRACKED AT BS 196.5, STR 17L. REMOVED AND REPLACED FRAME IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

VERTICAL ANGLE CRACKED AT BS 328, LBL 50. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

TIE CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED TIE CLIP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

VERTICAL ANGLE CRACKED AT BS 328, RBL 34. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

TIE CLIP CRACKED AT BS 380, STR 26L. REMOVED ANAD REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

SUPPORT ANGLE CRACKED AT BS 351.2, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

SUPPORT ANGLE CRACKED AT BS 294.5, STR 23L. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

STRAP CRACKED BETWEEN BS 312 TO BS 344, BL 0. REMOVED AND REPLACED STRAP IAW SRM AND DRAWING.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

CHANNEL CRACKED AT BS 294.5+3, RIGHT SIDE E/E COMPARTMENT. REMOVED AND REPLACED CHANNEL IAW SRM AND DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

SUPPORT ANGLE CRACKED AT BS 380, BETWEEN STR 20L TO STR 21L. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FRAME CRACKED AT BS 986.5, STR 20R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

SKIN PANEL CRACKED BETWEEN BS 540 TO BS 560. REMOVED AND REPLACED PANEL IAW EA.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 50,789 hrs · 40,387 cycles

RIGHT WING SUPPORT ANGLE CRACKED AT WBL 71.24 TRAILING EDGE AREA. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 500D TO BS 520, BL 0. REMOVED AND REPLACED ANGLE IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

SEAT TRACK INBOARD FLANGE CRACKED AT BS 520, LBL 24.5. REPAIRED SEAT TRACK IAW EO.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

CHANNEL CRACKED AT BS 540, BETWEEN RBL 24.7 TO RBL 45.5. REMOVED AND REPLACED CHANNEL IAW SRM & DRAWING.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

CREASE BEAM CRACKED AT BS 520, LBL 63.5. REPAIRED CHORD IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

WEB CRACKED AT BS 520+6, BETWEEN STR 21L TO STR 24L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: RIB — CRACKED (LT WING) · airframe 50,789 hrs · 40,387 cycles

LEFT WING RIB LOWER CHORD BETWEEN STRINGER 2 AND STRINGER 3 OF WBL 135.5 CRACKED. REPAIRED CHORD IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FRAME CORRODED AT BS 947.5, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED FRAME PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

SUPPORT Z CORRODED BETWEEN BS 727 TO BS 827, STR 25L. REMOVED AND REPLACED SUPPORT "Z" IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 344 TO BS 360, LBL 12. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

WEB CRACKED BETWEEN BS 312 TO BS 328, RBL 34. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 328, LBL 24. REPAIRED CHORD IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FLOORBEAM CORRODED AT BS 986.5, RBL 43.5. REPAIRED BEAM IAW SRM.

Part: SILL — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FWD GALLEY SILL WEB CRACKED AT BS 294.5+3, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

WEB CRACKED BETWEEN BS 344 TO BS 360, LBL 2.5. REMOVED AND REPLACED WEB PER SRM AND DRAWING.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 312, RBL 24. REPAIRED CHORD PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 947.5, LBL 53.5. REPAIRED CHORD IAW EO AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STR 24R TO STR 25R. REMOVED AND REPLACED FRAME IAW SRM AND DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FITTING CRACKED AT BS 332, STR 8R. REMOVED AND REPLACED FITTING PER SRM AND DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FRAME CRACKED AT BS 616, BETWEEN STR 8L AND STR 9L. REPAIRED FRAME IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED SPLICE IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

ANGLE CRACKED BETWEEN BS 277 TO BS 291.5, BETWEEN STR 12R TO STR 13R. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FITTING CRACKED AT BS 294.5, STR 8R. REMOVED AND REPLACED FITTING IAW EA.

Part: PLATE — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

PLATE CRACKED BETWEEN BS 520 TO BS 540, STR 17L. REMOVED AND REPLACED PLATE IAW SRM AND DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DRAWING.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FLOORBEAM WEB CRACKED AT BS 706+2.5, RBL 24.8. REPAIRED WEB PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FLOORBEAM WEB CRACKED AT BS 706+4.25, RBL 24.8. REPAIRED WEB PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FLOORBEAM WEB CRACKED AT BS 706+2.5, RBL 24.8. REPAIRED WEB PER EA.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 50,789 hrs · 40,387 cycles

RIGHT WING SUPPORT ANGLE CRACKED TRAILING EDGE AT LEVEL WBL 71.24. REMOVED AND REPLACED ANGLE IAW SRM.

Part: PLATE — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

PLATE CRACKED AT THE FWD ENTRY DOOR CUTOUT, LOWER HINGE AREA, BS 303.9. REMOVED AND REPLACED PLATE IAW SRM AND DRAWING.

Part: BEARING — LOOSE (TE FLAP) · airframe 50,789 hrs · 40,387 cycles

LEFT WING NR 1 A FRAME OF FLAP TRACK CARRIAGE BEARINGS LOOSE. REMOVED AND REPLACED BEARINGS IAW CMM AND SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

CHANNEL CORRODED BETWEEN BS 767 TO BS 787, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: BEARING — LOOSE (FLAP TRACK) · airframe 50,789 hrs · 40,387 cycles

LEFT WING NR 2 FLAP TRACK CARRIAGE A-FRAME BEARING LOOSE. REMOVED AND REPLACED BEARING IAW CMM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 50,789 hrs · 40,387 cycles

LEFT WING SUPPORT ANGLE CRACKED AT BS 540, BL 71.24. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED SPLICE IAW SRM AND DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

WEB CRACKED BETWEEN BS 277 TO BS 291.5, STR 14R. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

TIE CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

TIE CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

ANGLE CORRODED AT BS 767, STR 27R. REMOVED AND REPLACED CLIP IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

TIE CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (LT WING) · airframe 50,789 hrs · 40,387 cycles

LEFT WING TRAILING EDGE AREA SUPPORT VERTICAL ANGLE CRACKED AT RSS 533+10. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

ANGLE CRACKED BETWEEN BS 277 TO BS 291.5, BETWEEN STR 13R TO STR 14R. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

CHANNEL CORRODED BETWEEN BS 767 TO BS 787, RBL 3.00. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

CHANNEL CORRODED BETWEEN BS 767 TO BS 787, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FORWARD PRESSURE BULKHEAD CRACKED AT BS 178, LBL 5.7. REPAIRED BULKHEAD IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FRAME CORRODED AT BS 767, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FLOORBEAM WEB CRACKED AT BS 706+8.5, RBL 24.8. REPAIRED WEB PER EA.

Part: PLATE — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FORWARD ENTRY DOOR CUTOUT PLATE CRACKED AT BS 303.9. REMOVED AND REPLACED PLATE IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FRAME CORRODED AT BS 727E, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

TIE CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

TIE CLIP CRACKED AT BS 500B, STR 22R. REMOVED AND REPLACED TIE CLIP IAW SRM & DRAWING.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

WEB CORRODED BETWEEN BS 420 TO BS 440, STR 17L. REMOVED AND REPLACED WEB IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

CHANNEL CRACKED AT BS 540, RBL 2. REMOVED AND REPLACED CHANNEL IAW SRM AND DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

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

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

KEEL BEAM CORRODED BETWEEN BS 500C+15 TO BS 520, STR 28L. REMOVED AND REPLACED BEAM IAW SRM AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

STRINGER CRACKED BETWEEN BS 492.4 TO BS 500, STR 22R. REPAIRED STRINGER IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708, RBL 24.8. REPAIRED WEB PER EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

WEB CORRODED BETWEEN BS 380 TO BS 400, STR 17R. REPAIRED WEB IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

STRINGER CRACKED BETWEEN BS 492.4 TO BS 500, STR 23R. REPAIRED STRINGER IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 710, RBL 24.8. REPAIRED WEB PER EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

CHANNEL CRACKED AT BS 540, LBL 2. REMOVED AND REPLACED CHANNEL IAW SRM & DRAWING.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 712, BBL 0.07. REPAIRED WEB IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FLOORBEAM CRACKED AT BS 708, BBL 0.07. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (R WING) · airframe 50,789 hrs · 40,387 cycles

RIGHT WING FIXED LEADING EDGE SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 707, BBL 0.07. REPAIRED WEB IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FLOORBEAM WEB CRACKED AT BS 709, BBL 0.07. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

SKIN CRACKED AT BS 327, STR 17R. REPAIRED SKIN IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 50,789 hrs · 40,387 cycles

MAIN WHEEL PRESSURE DECK WEB CRACKED BETWEEN BS 664 TO BS 675, LBL 24.50+6". REPAIRED WEB IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 670, RBL 24.8. REPAIRED CHORD IAW SI AND EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,789 hrs · 40,387 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 710, BBL 0.07. REPAIRED WEB IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 50,489 hrs · 40,184 cycles

FORWARD SERVICE DOOR EMERGENCY EXIT LENS TAPED IN PLACE LIGHTS ARE SERVICEABLE. COMPLIED WITH EA 1-A33-0129.

Part: PANEL — CRACKED (RT WING) · airframe 50,024 hrs · 39,858 cycles

OUTBOARD OF THE RIGHT WING INBOARD GROUND SPOILER, THE UPPER WING PANEL IS CRACKED. REMOVED AND REPLACED UPPER WING PANEL OUTBOARD OF THE RIGHT WING INBOARD GROUND SPOILER IAW SRM 51-40-02.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 50,024 hrs · 39,858 cycles

LEFT WING O/B TRAILING EDGE FLAP IS DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED OUTBOARD AFT FLAP AS PER AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 50,024 hrs · 39,858 cycles

AFT GALLEY BOTH EMERGENCY FLASHLIGHTS LOW ON CHARGE AND NEED BATTERIES CHANGED. REMOVED AND REPLACED EMERGENCY FLASHLIGHTS BATTERIES, OPS CHECK GOOD PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,988 hrs · 39,833 cycles

FUSELAGE SKIN CRACK INDICATION AT B5 787+9 ABOVE STR 10R USING C-SCAN PROCEDURE REF NDT MANUAL PART 6, SUBJECT 53-30-25. VERIFIED SUBSURFACE CRACK INDICATION USING MFEC REF 737 NDT MANUAL PART 6, SUBJECT 53-30-18. CRACK MEASURES 2.5" IN LENGTH

Part: SKIN — CRACKED (FUSLEAGE) · airframe 49,507 hrs · 39,481 cycles

FUSELAGE SKIN CRACKED AT BS 727B+10, STR 10R. REPAIRED SKIN PER EA.

Part: LIGHT — BROKEN (CABIN) · airframe 49,500 hrs · 39,475 cycles

RIGHT EEPLS BROKEN AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 48,797 hrs · 38,934 cycles

LEFT OVERWING EMERGENCY EXIT SIGN LENS LOOSE. REPAIRED LENS PER EA.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 48,496 hrs · 38,707 cycles

DIVERSION/EMERGENCY DECLARED -- MULTIPLE LIGHTS ILLUMINATED WITH SMELL IN FLIGHT DECK. REMOVED AND REPLACED ENGINE/APU FIRE CONTROL PANEL IAW MM.

Part: MOTOR — FAILED (FUEL SYSTEM) · airframe 48,496 hrs · 38,707 cycles

FUEL CROSSFEED VALVED FAILED IN CLOSED POSITION. REMOVED AND REPLACED FUEL CROSSFEED MOTOR AND CONNECTOR PER M/M.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 47,898 hrs · 38,262 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,684 hrs · 38,095 cycles

R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY LIGHT PER M/M.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 46,671 hrs · 37,335 cycles

DURING SCHEDULED OTS CHECK, FOUND MAIN WHEEL WELL PRESSURE DECK WEB CRACKED AT BS 664, RBL 39. REPAIRED WEB IAW SRM.

Part: STRUCTURE — DAMAGED (LE SLAT) · airframe 46,667 hrs · 37,334 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 6 I/B SLAT CAN DAMAGED. REPAIRED SLAT CAN IAW EA.

Part: LENS — BROKEN (EXIT SIGN) · airframe 46,667 hrs · 37,334 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 46,589 hrs · 37,272 cycles

RT EEPLS DAMAGED AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 46,268 hrs · 37,013 cycles

DURING SCHEDULED 14Y CHECK, FOUND VERTICAL WEB CRACKED BETWEEN BS 705 TO BS 709, LBL 24.8. REPAIRED WEB PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,732 hrs · 36,611 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 24.8. REPAIRED WEB IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,732 hrs · 36,611 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM LOWER CHORD CRACKED AT BS 639, RBL 45.5. REPAIRED CHORD IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,732 hrs · 36,611 cycles

DURING SCHEDULED 14Y CHECK, FOUND CENTER WING BOX FLOORBEAM WEB CRACKED BETWEEN BS 705 TO BS 710, LBL 24.8. REPAIRED WEB IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,732 hrs · 36,611 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM LOWER CRACKED AT BS 639, RBL 46. REPAIRED BEAM PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 45,732 hrs · 36,611 cycles

DURING SCHEDULED 14Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, BETWEEN LBL 5.7 TO LBL 17.REPAIRED WEB PER ACO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,731 hrs · 36,611 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT AFT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,732 hrs · 36,611 cycles

DURING SCHEDULED 14Y CHECK, FOUND R1 DOOR FORWARD LOWER DOOR WEB CRACKED. REMOVED AND REPLACED WEB IAW SRM.

Part: SIGN — BROKEN (CABIN) · airframe 45,724 hrs · 36,605 cycles

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

Part: MOTOR — SHEARED (NR 1 ENGINE) · airframe 44,759 hrs · 35,894 cycles

ABORTED TAKEOFF, INITIAL INPUT NORMAL, AT 89 PERCENT NR 1 ENGINE FAILED TO ADVANCE N1 ANY FURTHER. REMOVED AND REPLACED NR 1 ENGINE VBV MOTOR AND SHAFT PER MM.

Part: COVER — BROKEN (CABIN) · airframe 44,711 hrs · 35,854 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 43,951 hrs · 35,291 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 43,600 hrs · 35,009 cycles

RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT BROKEN AT ROW 12. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 41,551 hrs · 33,425 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: ACTUATOR — FAULTY (LT MLG) · airframe 40,532 hrs · 32,642 cycles

ON TAKEOFF FROM SAN, LT MLG UNSAFE LIGHT STAYED ON. RECYCLED GEAR, LIGHT REMAINED ON AFTER HANDLE POSITIONED OFF. BOTH RED & GREEN LIGHTS ON. HANDLE LEFT IN THE UP POSITION (LIGHT OUT). REMOVED AND REPLACED LT MLG PRIORITY MODULAR VALVE AND LT MLG UPLOCK ACTUATOR PER MM.

Part: ACTUATOR — FAULTY (LT MLG) · airframe 40,482 hrs · 32,605 cycles

DIVERSION - LT MLG RED LIGHT INDICATION. REMOVED AND REPLACED LT MLG UPLOCK ACTUATOR PER MM.

Part: UPLOCK SENSOR — FAULTY (LT MLG) · airframe 40,482 hrs · 32,605 cycles

LEFT MLG UNSAFE LIGHT IND. CYCLED THE GEAR LEVER AND INDICATION LIGHT REMAINED RED. REMOVED AND REPLACED LEFT MLG UPLOCK SENSOR, M986, M988 LANDING GEAR LOGIC CARDS PER MM.

Part: UPLOCK SENSOR — FAULTY (RT MLG) · airframe 40,050 hrs · 32,298 cycles

ON DEPARTURE, AFTER PLACING GEAR HANDLE TO OFF, THE RED "RIGHT GEAR" INDICATOR LIGHT REMAINED ON. REMOVED AND REPLACED RT MLG UPLOCK SENSOR PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 40,026 hrs · 32,281 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT KEEL BEAM CORRODED FROM BS 540 TO BS 741. REMOVED AND REPLACED BEAM PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 40,026 hrs · 32,281 cycles

DURING SCHEDULED 12Y CHECK, FOUND KEEL BEAM CORRODED AT BS 508D, LBL 7. REPAIRED KEEL BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,026 hrs · 32,281 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER HINGE CUTOUT, BS 302.75, WL 34. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,026 hrs · 32,281 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN LBL 5 TO RBL 5. R&R SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,026 hrs · 32,281 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, LBL 17 TO LBL 24. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,026 hrs · 32,281 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CORRODED AT BS 787, LBL 1 TO LBL 14. REMOVED AND REPLACED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,026 hrs · 32,281 cycles

DURING SCHEDULED 12Y CHECK, FOUND BELLY SKIN CRACKED AT RADIO ALTIMETER CUTOUT, BS 413, RBL 3. REMOVED AND REPLACED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,026 hrs · 32,281 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO SHEAR TIE CORRODED AT BS 747, BETWEEN RBL 0 TO LBL 5. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,026 hrs · 32,281 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO SHEAR TIE CORRODED AT BS 727E, BETWEEN LBL 7 TO LBL 11. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 40,026 hrs · 32,281 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO, STRINGER CLIP CORRODED AT BS 787, RBL 14. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,026 hrs · 32,281 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO, SHEAR TIE CORRODED AT BS 727E, BETWEEN LBL 10 TO LBL 15. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 520) · airframe 40,026 hrs · 32,281 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, LBL 8. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 767) · airframe 40,026 hrs · 32,281 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO SHEAR TIE CORRODED AT BS 767, BETWEEN LBL 7 TO LBL 14. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S4L) · airframe 40,026 hrs · 32,281 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706 S4L) · airframe 40,026 hrs · 32,281 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 39,998 hrs · 32,260 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT FWD FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT ASSY PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 39,628 hrs · 31,996 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT FLOOR FITTINGS LOOSE. SECURED FITTINGS PER SRM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 39,001 hrs · 31,551 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 38,799 hrs · 31,402 cycles

AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: LENS — MISSING (CABIN) · airframe 38,753 hrs · 31,360 cycles

DURING SCHEDULED HC1 CHECK, FOUND SEVERAL BULLNOSE EMERGENCY EXIT LIGHT LENSES MISSING. INSTALLED LENSES PER MM.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 38,460 hrs · 31,151 cycles

RT MLG EXTENSION SHOWED UNSAFE INDICATION. CYCLED GEAR AND GOT THREE GREEN AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED UPLOCK ACTUATOR PER MM.

Part: SENSOR — LOOSE (RT MLG) · airframe 38,469 hrs · 31,156 cycles

RED RIGHT GEAR LIGHT ILLUMINATED DURING CONFIGURATING A/C ON FINAL APPROACH, GO-AROUND INITIATED, GEAR HANDLE BROUGHT UP. DURING NEXT GEAR EXTENSION THE GREEN RIGHT GEAR LIGHT ILLUMINATED, 3 GREEN - NORMAL LANDING. FOUND SENSOR LOOSE. SECURED SENSOR PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 38,401 hrs · 31,104 cycles

DURING SCHEDULED MV3 CHECK, FOUND L2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: DOOR — CRACKED (FWD CARGO DOOR) · airframe 38,401 hrs · 31,104 cycles

DURING SCHEDULED MV3 CHECK, FOUND FWD CARGO DOOR LOWER AFT CORNER CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: COVER — CRACKED (CABIN) · airframe 38,401 hrs · 31,104 cycles

DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT COVER CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 37,654 hrs · 30,585 cycles

FOUND L1 DOOR SLIDE PARTIALLY PULLED OUT OF CASE. INSTALLED SLIDE PER MT.

Part: SIGN — MISSING (CABIN) · airframe 35,946 hrs · 29,311 cycles

AFT CABIN EMERGENCY EXIT SIGN MISSING. INSTALLED EXIT SIGN PER MM.

Part: VALVE — FAULTY (MLG WW) · airframe 35,867 hrs · 29,255 cycles

LEFT MLG WOULD NOT EXTEND NORMALLY. LOWERED GEAR WITH MANUAL GEAR EXTENSION. REMOVED AND REPLACED LEFT MLG MODULAR VALVE PER MM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 35,567 hrs · 29,027 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 178, STR 17L. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 35,567 hrs · 29,027 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 178, STR 17R. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 35,558 hrs · 29,019 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD BULKHEAD RT LOWER CHORD CRACKED AT BS 178. REMOVED AND REPLACED CHORD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 35,558 hrs · 29,019 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD BULKHEAD LT LOWER CHORD CRACKED AT BS 178. REMOVED AND REPLACED CHORD PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,455 hrs · 28,938 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 34,891 hrs · 28,514 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: SWITCH — FAULTY (COCKPIT) · airframe 33,627 hrs · 27,528 cycles

ON FINAL APPROACH LANDING GEAR SELECTED DOWN. THREE GREEN AND THREE RED LIGHTS ILLUMINATED. CYCLED GEAR HANDLE, THREE GREEN LIGHTS ILLUMINATED. REMOVED AND REPLACED LANDING GEAR LEVER SWITCH PER MM.

Part: FRAME — CRACKED (BS 827 S8L) · airframe 33,574 hrs · 27,493 cycles

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

Part: STRUCTURE — CRACKED (NR 1 SLAT) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 33,574 hrs · 27,493 cycles

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

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: FRAME — CRACKED (BS 639) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 18L. REPAIRED FRAME PER EA.

Part: RIB — CRACKED (RT WING) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND RIGHT WING RIB CRACKED AT STA 135.5, BETWEEN S2 AND S3. REPAIRED RIB PER ACO.

Part: FRAME — CRACKED (BS 616) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, STR 17R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,574 hrs · 27,493 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 33,574 hrs · 27,493 cycles

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

Part: FRAME — CRACKED (BS 727B S8R) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 907 S8R) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, S8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 747 S8R) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 360) · airframe 33,574 hrs · 27,493 cycles

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

Part: FRAME — CRACKED (BS 727 S8L) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 787 S8L) · airframe 33,574 hrs · 27,493 cycles

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

Part: FRAME — CRACKED (BS 727A S8L) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 580 S8L) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 580, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 827 S8R) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, S8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,574 hrs · 27,493 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,574 hrs · 27,493 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,574 hrs · 27,493 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,574 hrs · 27,493 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,574 hrs · 27,493 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,574 hrs · 27,493 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,574 hrs · 27,493 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,574 hrs · 27,493 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA.

Part: FITTING — LOOSE (L2 DOOR) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 727E, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 33,574 hrs · 27,493 cycles

DURING SCHEDULED 10Y CHECK, FOUND MID CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,574 hrs · 27,493 cycles

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

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 32,112 hrs · 26,358 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED EVAC SLIDE CABLE PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 31,288 hrs · 25,713 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, STR 27R TO 27L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 31,288 hrs · 25,713 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, STR 26L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 31,288 hrs · 25,713 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 29,278 hrs · 24,172 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 26,450 hrs · 21,922 cycles

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

Part: FITTING — CORRODED (LT MLG) · airframe 25,665 hrs · 21,330 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT MLG FWD OUTBOARD HAGER FITTING, CORRODED. REPAIRED FITTING PER EA.

Part: STRUCTURE — CORRODED (LT MLG) · airframe 25,665 hrs · 21,330 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT GEAR, LT STAB ASSY, CORRODED. REMOVED AND REPLACED LT STAB ASSY PER MM.

Part: GUSSET — CRACKED (PAX DOOR) · airframe 25,602 hrs · 21,277 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT LWR CORNER GUSSET, CRACKED. REMOVED AND REPLACED SERVICE DOOR PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 25,602 hrs · 21,277 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LEFT T/E AFT FLAP PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 25,602 hrs · 21,277 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 EACH SHEAR TIES BETWEEN BS 747E AND BS 767, BETWEEN STRINGERS 27R AND 26R, CORRODED. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 25,602 hrs · 21,277 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FRAME AT AFT LOWER CORNER CRACKED. REMOVED AND REPLACED FWD SERVICE DOOR PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,991 hrs · 20,777 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BEARING — BROKEN (RT WING TE FLAPS) · airframe 24,983 hrs · 20,695 cycles

SUSPECT SINGLE SPINDLE T/E FLAPS FAILURE, AT FLAPS 5 180 KNOTS HEARD LOUD POP, EXPERIENCED SLIGHT YAW AND SLIGHT ROLL, VERY CONTROLLABLE. NORMAL LANDING. REMOVED AND REPLACED RT INBOARD T/E FLAP BOOM CABLE DRUM BEARING PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,829 hrs · 20,638 cycles

DURING SCHEDULED RON, FOUND BULL NOSE EMERGENCY EXIT LIGHTS AT ROWS 1 ABC AND 5 ABC INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FAN — FAULTY (E/E BAY) · airframe 23,970 hrs · 19,931 cycles

AIR TURNBACK, GASPER FAN CAUSED A BURNING SMELL THROUGHOUT CABIN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: ENGINE — LEAKING (LT WING) · airframe 23,484 hrs · 19,534 cycles

ON TAKEOFF FROM SEA HAD AN OILY ODOR WENT AWAY IMMEDIATLEY. ON DESCENT INTO LAS OIL SMELL WAS WORSE. REMOVED AND REPLACED NR 1 ENGINE ASSEMBLY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 22,630 hrs · 18,852 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: LENS — BROKEN (CABIN) · airframe 20,861 hrs · 17,388 cycles

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT LIGHT LENS BROKEN AT FWD F/A'S SEAT. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 19,052 hrs · 15,940 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 18,104 hrs · 15,220 cycles

DURING SCHEDULED C4 CHECK, FOUND RT INBD AFT T/E FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED RT INBD AFT T/E FLAP PER MM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 17,233 hrs · 14,550 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. SECURED LOOSE CONNECTOR PER MM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 17,233 hrs · 145,550 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT EMERGENCY EXIT LIGHTS INOP. SECURED CANNON PLUG TO BATTERY. OPS CK GOOD PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 17,233 hrs · 14,550 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: COFFEEMAKER — OVERHEATED (GALLEY) · airframe 16,340 hrs · 13,832 cycles

BURNING, SMOKE SMELL COMING FROM AFT GALLEY. REMOVED AND REPLACED AFT RT COFFEEMAKER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 15,123 hrs · 12,847 cycles

DURING SCHEDULED C1 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED IN FWD CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: MECHANISM — WORN (RH ELEVATOR) · airframe 14,228 hrs · 12,129 cycles

DURING SCHEDULED C4 CHECK, RH ELEVATOR TAB FAILED FREE PLAY CHECK. R&R RH ELEVATOR LOCK MECHANISM PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 14,236 hrs · 12,138 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS INOP BETWEEN ROW 11 & 17. REMOVED AND REPLACED BATTERY PER MM.

Part: COVER — LOOSE (CABIN) · airframe 12,815 hrs · 10,947 cycles

EEPLS TRACK COVER LOOSE AT ROW 14. R&R TRACK COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 12,285 hrs · 10,497 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS RED LENS MISSING AT AFT END. REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,285 hrs · 10,497 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AT ROW 20. RELAMPED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,630 hrs · 9,108 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT MID CABIN. REMOVED AND REPLACED LIGHT ASSY''S PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED A1 CHECK, FOUND SEVERAL EEPLS INOP. REPAIRED EEPLS WIRING PER MM.

Part: YAW DAMPER — MALFUNCTIONED (TAIL)

ACFT EXPERIENCED A MOMENTARY UNCOMMANDED YAW DURING APPROACH. REMOVED AND REPLACED YAW DAMPER COUPLER, P/N 4036952-906, S/N 94023899, RUDDER PCU, P/N 65-44861-12, S/N 3425AC, AND SOLENOID VALVE, P/N 881600-1001, S/N 16126 PER MM.

Part: OIL SYST — CONTAMINATED (NR 2 ENGINE)

AIR TURNBACK, DURING CLIMB, NR 2 ENGINE OIL QTY WENT TO ZERO AND OIL PRESS DROPPED TO 20 PSI. REMOVED AND REPLACED NR 2 ENG OIL SUPPLY FILTER AND SCAVANGE FILTER, NO CONTAMINATION ON FILTERS. FOUND POLYMIDE MATERIAL IN FWD SCAVANGE OIL SUMP. REMOVED MATERIAL, DRAINED, FLUSHED AND SERVICED SYSTEM PER MM.

Part: WIRE — EXPOSED (CABIN)

DURING SCHEDULED C4 CHECK, FOUND EXPOSED FLOOR TRACK LIGHT WIRING AT ROWS 19 AND 211. REMOVED AND REPLACED FLOOR TRACK COVERS AS PER BOEING MM.