N642WN

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 62,923 hrs · 49,205 cycles

FORWARD FLASHLIGHT STRAP BROKEN. R&R STRAP PER M/M.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,033 hrs · 48,618 cycles

R2 DOOR EMERGENCY EXIT AISLE LIGHT INOPERATIVE. REPLACED THE BULB IAW AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,033 hrs · 48,618 cycles

L2 DOOR EMERGENCY EXIT AISLE LIGHT BULB INOPERATIVE. REPLACED THE BULB IAW AMM.

Part: BRACKET — OUT OF POSITION (L1 DOOR SLIDE) · airframe 61,662 hrs · 48,390 cycles

L1 DOOR EMERGENCY ESCAPE SLIDE FLOOR BRACKETS OUT OF POSITION. REPOSITIONED THE BRACKETS IAW AMM.

Part: ANGLE — CRACKED (LT WING) · airframe 61,632 hrs · 48,371 cycles

LEFT WING T/E OTBD NR 6 FLAP TRACK INBD ANGLE CRACKED AT WS 209. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (FLAP TRACK) · airframe 61,632 hrs · 48,371 cycles

RIGHT WING T/E OTBD OF NR 3 FLAP TRACK INBD ANGLE CRACKED AT WS 209. R & R ANGLE IAW SRM AND DWG.

Part: STRINGER — CORRODED (BS 362) · airframe 61,632 hrs · 48,371 cycles

STRINGER CORRODED AT BS 362, STRINGER 21L. R & R THE STRINGER IAW EA.

Part: STRINGER SPLICE — CORRODED (BS 360) · airframe 61,632 hrs · 48,371 cycles

STRINGER SPLICE CORRODED AT BS 360, STRINGER 21L. REPAIRED THE STRINGER SPLICE IAW EA.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

SPLICE CORRODED AT BS 360, STR 22L. R & R SPLICE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

FRAME SHEAR TIE CORRODED AT BS 360 BETWEEN STR 23L TO STR 24L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — BROKEN (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

SHEAR TIE BROKEN AT BS 360 BETWEEN STR 26L TO STR 27L. R & R SHEAR TIE IAW SRM AND DWG.

Part: LIGHT — BROKEN (CABIN) · airframe 61,632 hrs · 48,371 cycles

G-4 GALLEY EXIT LIGHT BROKEN. R & R LIGHT IAW AMM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

FUSELAGE SKIN BUTT SPLICE STRAP CORRODED AT BS 360, BETWEEN STR 27L TO STR 28L. R&R STRAP IAW EA.

Part: ATTACH BRACKET — CRACKED (TE FLAP) · airframe 61,632 hrs · 48,371 cycles

RIGHT WING NR 6 FLAP TRACK AFT FAIRING ASSEMBLY OTBD UPPER ATTACH BRACKET CRACKED ON AFT END. R & R BRACKET IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 61,632 hrs · 48,371 cycles

R1 DOOR EXIT LIGHT LENS BROKEN. R & R LENS IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 61,632 hrs · 48,371 cycles

AFT DOORS EXIT LIGHT LENS BROKEN. R & R LENS IAW AMM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

FUSELAGE SKIN CORRODED AT BS 747, BETWEEN STRINGER 27L - 26L. REPAIRED SKIN IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

L1 DOOR CUT OUT LOWER SILL INNER CHORD ASSEMBLY CORRODED. REPAIRED CHORD ASSEMBLY IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

FRAME SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27R TO STR 26R. REPAIRED SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 61,632 hrs · 48,371 cycles

LEFT UPPER WING SKIN CRACKED AT BUT PLATES STRAP AREA AT RSS 255. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,632 hrs · 48,371 cycles

RIGHT UPPER WING SKIN CRACKED AT NUT PLATE STRAP AREA AT RSS 255. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,632 hrs · 48,371 cycles

RIGHT UPPER WING SKIN CRACKED AT NUT PLATE STRAP AREA AT RSS 251. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,632 hrs · 48,371 cycles

RIGHT WING UPPER SKIN CRACKED AT NUT PLATE STRAP AREA AT RSS 266. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,632 hrs · 48,371 cycles

RIGHT WING UPPER SKIN CRACKED AT NUT PLATE STRAP AREA AT RSS 265. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,632 hrs · 48,371 cycles

LEFT UPPER WING SKIN CRACKED AT NUT PLATES STRAP AREA AT RSS 268. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,632 hrs · 48,371 cycles

LEFT UPPER WING SKIN CRACKED AT RSS 251 ON FASTENER HOLE AT NUT PLATE STRAP AREA. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,632 hrs · 48,371 cycles

RIGHT UPPER WING SKIN CRACKED AT NUT PLATE STRAP AREA AT RSS 239. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,632 hrs · 48,371 cycles

RIGHT UPPER WING SKIN CRACKED AT NUT PLATE STRAP AREA AT RSS 257. REPAIRED SKIN IAW EA.

Part: PLATE — CRACKED (LT WING) · airframe 61,632 hrs · 48,371 cycles

LT UPPER WING CRACKED FASTENER HOLE ON FOR NUT PLATE STRAP AT RSS 239. REPAIRED PLATE IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

SHEAR TIE CORRODED AT BS 767, BETWEEN STR 27L TO STR 26L. R & R SHEAR TIE IAW SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

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

Part: ACCESS DOOR — DELAMINATED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

LEFT FAIRING ACCESS DOOR 3302 DELAMINATED ON EXTERIOR SURFACE. REPAIRED DOOR IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

VERTICAL BEAM PRESS BULKHEAD CRACKED AT BS 178, LBL 5.7. REPAIRED BEAM IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

L1 DOOR CUTOUT LOWER SILL WEB CORRODED. R & R WEB IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

SHEAR TIE CORRODED AT BS 360, BETWEEN STR 27L TO STR 28L. R&R SHEAR TIE IAW SRM & EA.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 61,632 hrs · 48,371 cycles

LEFT WING MLG AFT SUPPORT FITTING CRACKED. R & R FITTING IAW EA.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 61,632 hrs · 48,371 cycles

LEFT WING REAR SPAR ATTACH ANGLE CRACKED. R & R ANGLE IAW DWG & SRM.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

ATTACH ANGLE CORRODED AT BS 328, STRINGER 20L. R & R ANGLE IAW SRM & DWG.

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 61,632 hrs · 48,371 cycles

RIGHT WING T/E PANEL NR 8715 ATTACH BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

STRINGER END CLIP CORRODED AT BS 500, STRINGER 28R. R & R CLIP IAW SRM & DWG.

Part: FITTING — CORRODED (L1 DOOR) · airframe 61,632 hrs · 48,371 cycles

L1 DOOR CUT OUT AFT GIRT BAR SUB FLOOR FITTING CORRODED. REPAIRED FITTING IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

R2 DOOR CUT OUT LOWER THRESHOLD CHORD CORRODED. R & R CHORD IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

AFT SPAR STRAP CRACKED AT BS 660, LBL 36. R & R STRAP IAW SRM AND DWG.

Part: PUCK — CORRODED (CARGO AY) · airframe 61,632 hrs · 48,371 cycles

AFT CARGO FLOOR TIE DOWN HOCKEY PUCKS CORRODED AT BS 847, BETWEEN STR 20L TO STR 22L. R & R PUCK IAW SRM.

Part: SPAR — CRACKED (LT WING) · airframe 61,632 hrs · 48,371 cycles

LEFT WING REAR SPAR WEB CRACKED AT MLG AFT SUPPORT FITTING. REPAIR WEB IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

OUTER CHORD CRACKED AT BS 360, STR 14L. R & R CHORD IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

SHEAR TIE CORRODED AT BS 747, BETWEEN STRINGER 26L - 27L. R & R FRAME IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

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

Part: SPAR — CRACKED (RT WING) · airframe 61,632 hrs · 48,371 cycles

RIGHT WING REAR SPAR WEB UNDER AFT SUPPORT FITTING CRACKED. REPAIRED WEB IAW EA.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

FORWARD CARGO AFT BULKHEAD FLOOR PANEL ATTACH ANGLE CORRODED UPPER & LOWER. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

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

Part: AXLE — CORRODED (NLG) · airframe 61,632 hrs · 48,371 cycles

NLG AXLE CORRODED ON UPPER SIDE OF LT AND RT AXLE AT 12 O'CLOCK POSITION. R & R NLG INNER CYLINDER IAW MM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 61,632 hrs · 48,371 cycles

RIGHT WING NR 5 FLAP TRACK FWD ATTACH POINT INBD AFT BOLT HOLE CORRODED. REPAIRED TRACK IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

WEB OUTER CHORD CRACKED BETWEEN BS 277 - 291.5, BETWEEN STRINGER 8R - 9R. R & R CHORD IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

WEB OUTER CHORD CRACKED BETWEEN BS 277 - 291.5, BETWEEN STRINGER 13R - 14R. R & R CHORD IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

AFT PIT SHEAR TIE CORRODED AT BS 727E, BETWEEN BL 0 - RBL 6. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

FRAME SHEAR TIE CORRODED AT BS 787, BETWEEN BL 0 - LBL 5. R & R SHEAR TIE IAW SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 61,632 hrs · 48,371 cycles

MAIN WW PRESS DECK CRACKED AT BS 673.25, RBL 41.5. REPAIRED DECK IAW SRM & EA.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

L1 DOOR LOWER AFT CORNER, BEAR STRAP CRACKED. REPAIRED BEAR STRAP IAW SRM & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,632 hrs · 48,371 cycles

L1 DOOR CUT OUT AFT TRIM RETAINING ANGLE CRACKED. R & R ANGLE MM.

Part: SPAR — CRACKED (RT WING) · airframe 61,632 hrs · 48,371 cycles

RIGHT WING REAR UPPER SPAR CHORD CRACKED AT RSS 224.14. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 61,632 hrs · 48,371 cycles

LEFT WING UPPER SPAR CHORD CRACKED AT RSS 224.14 ON CHORD. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 60,377 hrs · 47,535 cycles

RIGHT WING LE, CRACKED IN DEFLECTOR DOOR CUT OUT, JUST INBD OF PYLON. REPAIRED CUT OUT IAW SRM.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 60,377 hrs · 47,535 cycles

MAIN LANDING GEAR WW VERTICAL STIFFENER BULKHEAD CRACKED AT BS 663, RBL 6.15. REPAIRED STIFFENER IAW EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 60,377 hrs · 47,535 cycles

R2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.

Part: CASTING — CRACKED (RT SPOILER) · airframe 60,377 hrs · 47,535 cycles

RIGHT WING, INBD SPOILER CASTING CRACKED, AT FWD ATTACH FITTING. R & R CASTING IAW SRM.

Part: GIRT BAR — LOOSE (R2 DOOR) · airframe 60,286 hrs · 47,474 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR ASSEMBLY LOOSE. SECURED GIRT BAR ASSEMBLY IAW MT.

Part: LENS — LOOSE (EXIT SIGN) · airframe 59,921 hrs · 47,225 cycles

EMERGENCY EXIT SIGN LENS LOOSE NEXT TO FWD ENTRY DOOR. R & R LENS IAW SIP.

Part: SKIN PANEL — DELAMINATED (LT SPOILER) · airframe 59,846 hrs · 47,174 cycles

LEFT WING NR 3 SPOILER PANEL DELAMINATED UPPER SURFACE. R & R NR 3 SPOILER IAW AMM.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 59,629 hrs · 47,014 cycles

L1 DOOR SLIDE EMER EVAC SLIDE, GIRT BAR LOOSE. SECURED GIRT BAR IAW MT & MM.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 59,629 hrs · 47,014 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR, GIRT LOOSE. SECURED GIRT BAR IAW MT & MM.

Part: LENS — LOOSE (L1 DOOR) · airframe 59,621 hrs · 47,008 cycles

L1 DOOR THRESHOLD EMER LIGHT LENS LOOSE. SECURED LENS IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 59,578 hrs · 46,974 cycles

FORWARD EMER EXIT LIGHT LENS LOOSE. SECURED LENS IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 58,757 hrs · 46,381 cycles

AFT EMER EXIT SIGN JUST OTBD OF FLIGHT ATTENDANT SEAT LOOSE. R & R LIGHT ASSEMBLY IAW AMM.

Part: LUG — DAMAGED (RT SPOILER) · airframe 58,578 hrs · 46,249 cycles

RIGHT WING NR 5 INBD GND SPOILER OTBD ACTUATOR LINK LUG DAMAGED. R & R SPOILER IAW AMM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 58,550 hrs · 46,231 cycles

R2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: SPINDLE — CORRODED (TE FLAP) · airframe 57,942 hrs · 45,821 cycles

RIGHT WING NR 7 MID FLAP CARRIAGE SPINDLE HVOF COATING CORRODED IN LOWER ROOT AREA. R & R SPINDLE IAW MT.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,119 hrs · 45,259 cycles

LEFT WING NR 3 SLAT LOWER SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 56,990 hrs · 45,180 cycles

FORWARD EXIT SIGN COVER LENS LOOSE. SECURED LENS IAW SIP.

Part: WIRE — BROKEN (CABIN) · airframe 56,473 hrs · 44,803 cycles

FORWARD LAVATORY L1 DOOR EMER LIGHT ASSEMBLY WIRE BROKEN. REPAIRED LIGHT ASSEMBLY IAW MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

FRAME SHEAR TIE CRACKED AT BS 360 BETWEEN STRINGER 14R TO 15R. REPAIRED SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

STRINGER CLIP CRACKED AT BS 727B STRINGER 8R. R & R CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

SKIN CRACKED AT BS 360 STRINGER 14R. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

LEFT BS 500B+10 FRAME FOUND TO BE CRACKED AT HOLE NR 7R. R & R FORGING IAW DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

LEFT BS 480+10 LOWER AFT WINDOW CORNER CRACKED. REPAIRED WINDOW IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

LEFT BS 500+10 UPPER FWD WINDOW CORNER CRACKED. REPAIRED WINDOW IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

LEFT BS 500B+10 UPPER FWD WINDOW CORNER CRACKED. REPAIRED WINDOW IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

LEFT BS 867+10 LOWER FWD WINDOW CORNER CRACKED. REPAIRED WINDOW IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

LEFT BS 480+10 UPPER FWD WINDOW CORNER CRACKED. REPAIRED WINDOW IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

LEFT BS 500A+10 UPPER FWD WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

LEFT BS 460+10 LOWER AFT WINDOW CORNER CRACKED. REPAIRED WINDOW IAW SB.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

LEFT CUSP WEB CORRODED AT BS 500A+14. R & R WEB IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

LEFT BS 787+10 UPPER AFT WINDOW CORNER CRACKED. REPAIRED WINDOW IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

RIGHT BS 767+10 LOWER FWD WINDOW CORNER CUT OUT CRACKED. REPAIRED WINDOW IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

LEFT BS 400+10 UPPER FWD WINDOW CORNER CRACKED. REPAIRED WINDOW IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

LEFT BS 807+10 UPPER AFT WINDOW CORNER CRACKED. REPAIRED WINDOW IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

RIGHT BS 787+10 UPPER AFT WINDOW CORNER CRACKED. REPAIRED WINDOW IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

LEFT BS 420+10 UPPER FWD WINDOW CORNER CRACKED. REPAIRED WINDOW IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

LEFT BS 827+10 UPPER AFT WINDOW CORNER CRACKED. REPAIRED WINDOW IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

LEFT BS 807+10 UPPER AFT WINDOW CORNER CRACKED. REPAIRED WINDOW IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

LEFT BS 827+10 LOWER FWD WINDOW CORNER CRACKED. REPAIRED WINDOW IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

LEFT BS 460+10 UPPER FWD WINDOW CORNER CRACKED. REPAIRED WINDOW IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 44,803 cycles

LEFT BS 787+10 LOWER FWD WINDOW CORNER CRACKED. REPAIRED WINDOW IAW EA.

Part: FITTING — LOOSE (NLG) · airframe 56,473 hrs · 44,803 cycles

LEFT NLG DOOR CONTROL ROD TRUNNION FITTING LOOSE. SECURED FITTING IAW CMM.

Part: COVER — LOOSE (CABIN) · airframe 56,322 hrs · 44,692 cycles

FORWARD GALLEY EMER EXIT LIGHT COVER LOOSE. R & R COVER IAW MM.

Part: PANEL — CRACKED (LT WING) · airframe 56,031 hrs · 44,473 cycles

LEFT WING UPPER TE PANEL CRACKED AT FWD OTBD CORNER OF NR 4 SPOILER CUT OUT. REPAIRED PANEL IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

AFT PRESS BULKHEAD WEB CRACKED AT BS 1016, STRINGER 15R. REPAIRED WEB IAW ER & EA.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

AFT PRESS BULKHEAD CHANNEL STIFFENER CORRODED AT BS 1017, LBL 1. REPAIRED STIFFENER IAW ER & EA.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

AFT PRESS BULKHEAD ANGLE STIFFENER CORRODED AT BS 1016, BETWEEN RBL 6 TO LBL 10. REPAIRED STIFFENER IAW ER & EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

INTERCOSTAL CRACKED BETWEEN BS 986.5 TO BS 1006, STRINGER 21R. R & R INTERCOSTAL IAW SRM & DWG.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

AFT PRESS BULKHEAD CHANNEL STIFFENER CORRODED AT BS 1017, RBL 1. REPAIRED STIFFENER IAW EA.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

FORWARD SURFACE OF AFT PRESS BULKHEAD, PRESS WEB CORRODED AT BS 1017, BETWEEN LBL 4 TO RBL 4. REPAIRED WEB IAW ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

SHEAR TIE CORRODED AT BS 1006, BETWEEN STRINGER 27L TO 27R. R & R SHEAR TIE IAW SRM & DWG.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

AFT PRESS BULKHEAD PRESS CHORD CORRODED AT BS 1016, LBL 5. REPAIRED CHORD IAW SRM.

Part: CHANNEL — DAMAGED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

CENTER WING BOX LONGITUDINAL FLOORBEAM AT LOWER CHORD U CHANNEL DAMAGED AT BS 663, RBL 24.8. REPAIRED U CHANNEL IAW ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STRINGER 27 TO STRINGER 28L. REPAIRED SHEAR TIE IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

SIDEWALL TO FLOORBEAM CLIP CRACKED AT BS 947, LBL 21. R & R CLIP IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

FLOORBEAM CORD CRACKED AT BS 827, RBL 17. REPAIRED FLOORBEAM IAW SRM.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

CENTER WING BOX LONGITUDINAL FLOORBEAM AT LOWER CHORD L ANGLE DAMAGED AT BS 663, RBL 24.8. REPAIRED L ANGLE IAW ER.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

INTERCOSTAL CRACKED AT BS 348.5, STRINGER 16L. R & R INTERCOSTAL IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

SIDEWALL TO FLOORBEAM CLIP CRACKED AT BS 947, RBL 21. R & R CLIP IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

INTERCOSTAL CORRODED AT BS 947, LBL 21. R & R INTERCOSTAL IAW SRM & DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

ATTACH CLIP CRACKED AT BS 348.5, STRINGER 15L. R & R CLIP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

SHEAR TIE CORRODED AT BS 500C, BETWEEN STRINGER 26L TO 27L. REPAIRED SHEAR TIE IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

INTERCOSTAL INBD ATTACH ANGLE CRACKED BETWEEN BS 294.5 TO BS 303.9, STRINGER 16L. R & R ANGLE IAW DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STRINGER 27R TO STRINGER 28R. R & R SHEAR TIE IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 56,031 hrs · 44,473 cycles

RIGHT WING RSS 547, WIPER WEB ATTACH ANGLE CRACKED AT INBD CTR AILERON HINGE INBD ANGLE. R & R ANGLE IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

FLOORBEAM CRACKED AT BS 328, LBL 28. REPAIRED FLOORBEAM IAW SRM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 56,031 hrs · 44,473 cycles

RIGHT WING RSS 547 LOWER TE SUPPORT ANGLE CRACKED AT INBD CTR AILERON HINGE INBD ANGLE. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (NR 2 PYLON) · airframe 56,031 hrs · 44,473 cycles

RIGHT WING NR 2 PYLON OTBD UPPER TE SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 56,031 hrs · 44,473 cycles

MAIN WW BEADED PRESS DECK CRACKED AT BS 664, LBL 37. REPAIRED DECK IAW ER & EA.

Part: FORMER — LOOSE (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

WING TO BODY FAIRING FORMER LOOSE AT BS 727, LBL 31. R & R FORMER IAW DWG & SRM.

Part: SLIDE — UNSERVICEABLE (R1 DOOR) · airframe 56,031 hrs · 44,473 cycles

R1 DOOR EMER EVAC SLIDE PROTECTIVE COVERING OVER PULL LANYARD MISSING. R & R SLIDE IAW MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

EXTERNAL FUSELAGE SKIN CRACKED AT FWD LT CORNER OF CONDITIONED AIR DOOR CUT OUT. REPAIRED SKIN IAW SRM.

Part: PANEL — CRACKED (FUSELAGE) · airframe 56,031 hrs · 44,473 cycles

KEEL BEAM STRESS PANEL CRACKED AT BS 707, RBL 7. REPAIRED PANEL IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 55,886 hrs · 44,379 cycles

FORWARD SERVICE DOOR EMERGENCY EXIT LENS BROKEN. R & R LENS ASSEMBLY IAW MM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 55,501 hrs · 44,102 cycles

STIFFENER STRAP CRACKED AT BS 312.5, BL 40. REPAIRED STRAP IAW SRM.

Part: ACTUATOR — LEAKING (RT SPOILER) · airframe 55,501 hrs · 44,102 cycles

RT WING NR 6 SPOILER ACTUATOR LEAKED. R & R ACTUATOR IAW AMM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 55,501 hrs · 44,102 cycles

STIFFENER STRAP CRACKED AT BS 312.5, BL 35. R & R STRAP IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 55,501 hrs · 44,102 cycles

E & E COMPARTMENT STIFFENER STRAP CRACKED AT BS 328.5. R & R STRAP IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 55,357 hrs · 44,015 cycles

FWD ENTRY LOWER EMERGENCY EXIT LENS COVER LOOSE. R & R COVER IAW MM.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 54,488 hrs · 43,409 cycles

LT WING NR 2 FLAP TRACK CORRODED ON TOP SIDE NEAR REAR SPAR ATTACH POINT JUST AFT OF TAPERED SHIM. R & R NR 2 FLAP TRACK IAW AMM.

Part: BRACKET — LOOSE (L2 DOOR) · airframe 54,169 hrs · 43,184 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOLDER LOOSE. SECURED BRACKET IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 53,834 hrs · 42,931 cycles

R1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY LOOSE. SECURED SIGN IAW MM.

Part: FITTING — CRACKED (RT AILERON) · airframe 53,834 hrs · 42,931 cycles

RT WING VERTICAL ANGLE CRACKED IN AILERON BALANCE BAY FWD & INBD OF NR 2 AILERON HINGE FITTING. R&R FITTING IW SRM.

Part: HINGE FITTING — CRACKED (LT AILERON) · airframe 53,834 hrs · 42,931 cycles

LT WING TE AILERON BALANCE BAY VERTICAL ANGLE INBD & FWD OF NR 2 HINGE FITTING CRACKED. R&R FITTING IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 53,448 hrs · 42,645 cycles

RT OVERWING EMERGENCY EXIT SIGN LIGHT COVER LOOSE. R&R LENS PER SIP.

Part: SIGN — LOOSE (CABIN) · airframe 52,793 hrs · 42,156 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER M/M.

Part: SIGN — UNSECURE (CABIN) · airframe 52,438 hrs · 41,905 cycles

RIGHT OVERWING EXIT SIGN NEEDS RE-SECURING. SECURED SIGN PER M/M.

Part: BUMPER — CRACKED (LT WING) · airframe 52,042 hrs · 41,631 cycles

LEFT WING AFT SPAR FWD DRAG BRACE BUMPER CRACKED. REMOVAL AND REPLACEMENT OF LEFT WING AFT SPAR FWD DRAG BRACE BUMPER.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,435 hrs · 41,189 cycles

RIGHT AFT EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 50,830 hrs · 40,717 cycles

AFTER TAKEOFF PUT LANDING GEAR LEVER UP AND RIGHT MAIN UNSAFE LIGHT REMAINED ILLUMINATED. CYCLED GEAR DOWN- 3 GREEN, NO RED RETRACTED GEAR AGAIN, RIGHT MAIN UNSAFE LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED RIGHT MLG UPLOCK ACTUATOR PER MM.

Part: LENS — MISSING (CABIN) · airframe 50,792 hrs · 40,688 cycles

LEFT OVERWING EMERGENCY EXIT LENS MISSING. INSTALLED LENS PER.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 50,815 hrs · 40,708 cycles

AIR TURNBACK -- RED RIGHT MAIN GEAR LIGHT REMAINED ON WITH GEAR LEVER IN UP POSITION. PUT GEAR LEVER IN OFF POSITION LIGHT REMAINED ON. PUT GEAR LEVER BACK IN UP POSITION AND GOT GREEN LIGHT WITH RED LIGHT. GREEN THEN EXTINGUISHED AND RED LIGHT WENT OUT MINUTES LATER. REMOVED AND REPLACED RIGHT MLG DOWNLOCK SENSOR AND UPLOCK ACTUATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,618 cycles

FUSELAGE SKIN CRACKED AT BS 727D+2, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,709 hrs · 40,618 cycles

FUSELAGE SKIN CRACKED AT BS 709, STR 4R. REPAIRED SKIN PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,118 hrs · 40,171 cycles

FWD OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 50,118 hrs · 40,171 cycles

SKIN CORRODED AT BS 360, RBL 1. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,118 hrs · 40,171 cycles

FLOORBEAM CORRODED AT BS 344, RBL 1. REMOVED AND REPLACED T-CAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,118 hrs · 40,171 cycles

FLOORBEAM CORRODED AT BS 344, RBL 8. REMOVED AND REPLACED T-CAP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,118 hrs · 40,171 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 664, RBL 24.8. REPAIRED CHORD PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,118 hrs · 40,171 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 661, LBL 24.8. REPAIRED CHORD PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,118 hrs · 40,171 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 668, LBL 24.8. REPAIRED CHORD PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,118 hrs · 40,171 cycles

L-ANGLE CRACKED AT BS 638, RBL 64. REMOVED AND REPLACED L-ANGLE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,118 hrs · 40,171 cycles

STRINGER CORRODED AT BS 314, STR 28R. REPAIRED STRINGER PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,118 hrs · 40,171 cycles

FLOORBEAM CORRODED AT BS 344, LBL 11. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,118 hrs · 40,171 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 664, LBL 24.8. REPAIRED CHORD PER EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 50,118 hrs · 40,171 cycles

R1 DOOR CUTOUT FRAME CRACKED AT BS 297, STR 7R. REPAIRED FRAME PER EA.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 50,118 hrs · 40,171 cycles

RIGHT WING NR 5 SLAT T/E WEDGE UPPER SKIN DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,118 hrs · 40,171 cycles

FLOORBEAM CRACKED AT BS 947, LBL 54. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,118 hrs · 40,171 cycles

FRAME CRACKED AT BS 312, STR 6L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (R2 DOOR) · airframe 50,118 hrs · 40,171 cycles

R2 DOOR LOWER FWD CORNER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,118 hrs · 40,171 cycles

L2 DOOR LOWER FORWARD CORNER CUTOUT CRACKED. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,118 hrs · 40,171 cycles

SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26L TO STR 2L. REPAIRED SHEAR TIE PER SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 50,118 hrs · 40,171 cycles

BEAM CRACKED AT BS 328, RBL 21. REPAIRED BEAM PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 50,118 hrs · 40,171 cycles

FWD BULKHEAD STIFFENER CRACKED AT BS 1016, AT 1 O'CLOCK POSITION. REPAIRED STIFFENER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,118 hrs · 40,171 cycles

FRAME CORRODED AT BS 540, LBL 8. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,118 hrs · 40,171 cycles

SHEAR TIE CORRODED AT BS 887, RBL 0. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,118 hrs · 40,171 cycles

SHEAR TIE CORRODED AT BS 807, RBL 3. REPAIRED SHEAR TIE PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 49,136 hrs · 39,457 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 48,734 hrs · 39,151 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 48,611 hrs · 39,053 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITION SLIDE PER MT.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 47,842 hrs · 38,475 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,502 hrs · 38,222 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 427, STR 4R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,502 hrs · 38,222 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR. REMOVED AND REPLACED DOOR IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,499 hrs · 38,221 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 427, STR 4R. REPAIRED SKIN PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 46,974 hrs · 37,834 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 4 SLAT T/E WEDGE I/B END DELAMINATED. REMOVED AND REPLACED WEDGE PER MM.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 46,974 hrs · 37,834 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING I/B FORE FLAP I/B LOWER SIDE PUNCTURED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SLAT — CRACKED (RT WING) · airframe 50,127 hrs · 40,177 cycles

RIGHT WING NR 6 SLAT LOWER AFT TRAILING EDGE CRACKED. REMOVED AND REPLACED NR 6 SLAT PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 46,634 hrs · 37,572 cycles

FWD EMERGENCY I/B FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,145 hrs · 37,210 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT, STA 290, BETWEEN WL 237 TO WL 234.5. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,135 hrs · 37,202 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, LBL 3. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,135 hrs · 37,202 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, LBL 3. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,135 hrs · 37,202 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, BETWEEN STR 3L AND STR 2L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,135 hrs · 37,202 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 3L. REPAIRED SKIN PER SWA EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 46,135 hrs · 37,202 cycles

DURING SCHEDULED 14Y CHECK, FOUND COCKPIT FLOOR WEB CRACKED AT FWD INBD OPC MOUNT CUTOUT. REPAIRED WEB PER SWA ACO.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 46,135 hrs · 37,202 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CRACKED AT BS 907, STR 4R. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 46,135 hrs · 37,202 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CRACKED AT BS 500C, STR 4R. REPAIRED STRINGER PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 46,135 hrs · 37,202 cycles

DURING SCHEDULED 14Y CHECK, FOUND BEADED WEB CRACKED AT BS 663, LBL 31. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,135 hrs · 37,202 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,135 hrs · 37,202 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,135 hrs · 37,202 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 45,811 hrs · 36,937 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: LENS — MISSING (CABIN) · airframe 45,494 hrs · 36,688 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 23. INSTALLED LENS PER MM.

Part: BRACKET — CRACKED (EVAC SLIDE) · airframe 45,168 hrs · 36,430 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD MOUNT BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 45,168 hrs · 36,430 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND RT HORIZONTAL STABILIZER SKIN CRACKED AT STA 124.3. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 45,168 hrs · 36,430 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 44,662 hrs · 36,043 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 44,512 hrs · 35,926 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 44,256 hrs · 35,738 cycles

AFT O/B EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — MISSING (CABIN) · airframe 43,657 hrs · 35,280 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 23. INSTALLED LENS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 43,535 hrs · 35,190 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT LENS COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 43,535 hrs · 35,190 cycles

DURING SCHEDULED HC2 CHECK, FOUND OVERHEAD CENTER EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT ASSY PER MM.

Part: SIGN — MISSING (CABIN) · airframe 43,448 hrs · 35,120 cycles

LT OVERWING EMERGENCY EXIT SIGN MISSING AT ROW 11. REMOVED AND REPLACED LENS ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,878 hrs · 34,719 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 42,699 hrs · 34,600 cycles

AFT GALLEY O/B FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: COVER — BROKEN (CABIN) · airframe 42,648 hrs · 34,560 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,571 hrs · 34,508 cycles

DURING SCHEDULED MV4 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 42,524 hrs · 34,469 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 41,889 hrs · 34,028 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,189 hrs · 33,540 cycles

FWD ENTRY EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 440,143 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 186, RBL 5.7. REPAIRED WEB PER SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 440,143 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB PER SWA EA.

Part: COVER — BROKEN (CABIN) · airframe 40,177 hrs · 32,825 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 26R TO STR 25R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26R TO STR 25R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,142 hrs · 32,802 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,142 hrs · 32,802 cycles

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

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND BEAR STRAP SKIN CORRODED AT AFT CARGO COMPARTMENT, BS 789, RBL 20. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (BS 727D S26-27L) · airframe 40,142 hrs · 32,802 cycles

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

Part: SKIN — CORRODED (BS 846 S26R) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND BEAR STRAP SKIN CORRODED AT BS 846, STR. 26R. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (BS 847) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND CARGO DOOR CUTOUT AFT FRAME CORRODED AT BS 847. REMOVED AND REPLACED FRAME PER ACO.

Part: FRAME — CORRODED (BS 500A) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD CARGO FRAME CORRODED AT BS 500A, BETWEEN LBL 5 TO RBL 3. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (BS 253) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND NOSE WHEEL WELL SKIN CEILING CRACKED AT BS 253, BETWEEN RBL 7.75 TO LBL 7.75. REPAIRED SKIN PER ACO.

Part: BULKHEAD — CRACKED (BS 178) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7, WL 186. REPAIRED WEB PER SWA EA.

Part: FRAME — CRACKED (BS 727E S26-27R) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727E, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (BS 500B) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD CARGO FRAME CORRODED AT BS 500B, BETWEEN LBL 1 TO LBL 2. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 947 S24R) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS. 947, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CORRODED AT BS 500, BETWEEN LBL 3 TO RBL 3. REMOVED AND REPLACED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN LBL 6 TO RBL 6. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB PER SWA EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND VERTICAL WEB CRACKED AT BS 180, LBL 17, WL 230. REPAIRED WEB PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CRACKED AT BS 484, STR 22R. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 178) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT CHORD CRACKED AT BS 178, RBL 28, WL 207. REPAIRED CHORD PER ACO.

Part: FRAME — CRACKED (BS 727D S8L) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER — CRACKED (BS 484 S23R) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CRACKED AT BS 484, STR 23R. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BULKHEAD) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT CHORD CRACKED AT BS 178, RBL 28, WL 207. REPAIRED CHORD PER ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,142 hrs · 32,802 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,142 hrs · 32,802 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,142 hrs · 32,802 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,142 hrs · 32,802 cycles

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

Part: SENSOR — FAULTY (MLG) · airframe 39,549 hrs · 32,372 cycles

AIR TURNBACK HAD TO USE LOCK OVERIDE TRIGGER TO RAISE GEAR, CYCLED GEAR, THEN GOT THE CONFIGURATION WARNING HORN ADVANCING THRUST REVERSERS. CONFIGURED FOR FLAPS 30LDG RETURNED TO SLC. REMOVED AND REPLACED S106 GROUND SHIFT SENSOR PER MM.

Part: STRINGER — CRACKED (RT WING) · airframe 39,367 hrs · 32,229 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING U9 STRINGER CRACKED AT WING STA 583, ON VERTICAL LEG. REMOVED AND REPLACED STRINGER PER IND EA.

Part: HINGE — BROKEN (NR 5 SPOILER) · airframe 39,027 hrs · 31,989 cycles

RT WING NR 5 GROUND SPOILER HINGE BROKEN. R&R SPOILER PER MM.

Part: TAB — DELAMINATED (RT AILERON) · airframe 38,802 hrs · 31,823 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT WING AILERON TAB DELAMINATED. REMOVED AND REPLACED TAB PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 37,073 hrs · 30,531 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED AT OUTBOARD CORNER. REMOVED AND REPLACED SLAT PER MM.

Part: LINK — CRACKED (L1 DOOR) · airframe 34,406 hrs · 28,420 cycles

L1 DOOR WILL NOT COMPLETELY OPEN. REMOVED AND REPLACED CRACKED LOWER GUIDE ARM LINK, REINSTALLED PIN PER MM.

Part: KEELBEAM — CRACKED (BS 682) · airframe 33,605 hrs · 27,834 cycles

DURING SCHEDULED 10Y CHECK, FOUND KEEL BEAM CHORD CRACKED AT BS 682, RBL 5. REMOVED AND REPLACED CHORD PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 988, RBL 40. REPAIRED FLOORBEAM PER BOEING DRAWING AND SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 43 TO RBL 43. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM ZEE CHORD CORRODED AT BS 270, LBL 0 TO LBL 11. REMOVED AND REPLACED ZEE CHORD PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 508A, LBL 70. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: TORQUE TUBE — CORRODED (T/E FLAP) · airframe 33,605 hrs · 27,834 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 691, LBL 70. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 33,605 hrs · 27,834 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED AFT GIRT BAR FITTING PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT OVERWING DOOR CUTOUT FWD FRAME CRACKED AT BS 616, WL 202. REPAIRED FRAME SECTION PER ER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 842, LBL 71. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT OVERWING DOOR CUTOUT FWD FRAME CRACKED AT BS 616, WL 202. REPAIRED FRAME SECTION PER ER.

Part: TORQUE TUBE — CORRODED (FOREFLAP) · airframe 33,605 hrs · 27,834 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 33,605 hrs · 27,834 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD FORE FLAP INBOARD FWD CORNER DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 730B, LBL 71. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: SKIN — DEBONDED (FORE FLAP) · airframe 33,605 hrs · 27,834 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SURFACE DISBONDED. REPAIRED FORE FLAP PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

DURING SCHEDULED 10Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

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

Part: FITTING — CORRODED (HORIZ STAB) · airframe 33,605 hrs · 27,834 cycles

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

Part: TORQUE TUBE — CORRODED (RT MID FLAP) · airframe 33,605 hrs · 27,834 cycles

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

Part: TORQUE TUBE — CORRODED (LT MID FLAP) · airframe 33,605 hrs · 27,834 cycles

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

Part: TORQUE TUBE — CORRODED (LT MID FLAP) · airframe 33,605 hrs · 27,834 cycles

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

Part: TORQUE TUBE — CORRODED (RT MID FLAP) · airframe 33,605 hrs · 27,834 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 9L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 9R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9R AND STR 9L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 9R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 9R AND STR 9L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,605 hrs · 27,834 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 33,410 hrs · 27,689 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 32,971 hrs · 27,338 cycles

DURING SCHEDULED MV1 CHECK, FOUND LOWER EMERGENCY EXIT LIGHT LENS BROKEN AT L1 DOOR. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 32,449 hrs · 26,902 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 31,441 hrs · 26,148 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: HOOK — LOOSE (L1 DOOR GIRT BAR) · airframe 29,739 hrs · 24,830 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: HOOK — LOOSE (R2 DOOR SLIDE) · airframe 29,505 hrs · 24,632 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: LATCH — OUT OF ADJUST (GIRT BAR) · airframe 28,653 hrs · 23,943 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LATCH ASSY OUT OF ADJUST. ADJUSTED LATCH ASSY PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 28,653 hrs · 23,943 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 26,841 hrs · 22,540 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 & R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1 AND R2 DOOR EVAC SLIDES PER MM.

Part: FITTING — WORN (MLG WW) · airframe 25,598 hrs · 21,498 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT AND RT MLG FWD AND AFT STAB FITTINGS WORN. REPAIRED LT AND RT MLG STAB FITTINGS PER EA AND OHM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,323 hrs · 21,279 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD DOME CAP AT BS 1016, BL 0, CRACKED. REPAIRED DOME CAP PER EA.

Part: HOOK — LOOSE (GIRT BAR) · airframe 25,323 hrs · 21,279 cycles

DURING SCHEDULED RON, FOUND R1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. REMOVED AND REPLACED R1 DOOR EVAC SLIDE GIRT BAR HOOKS PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 & R2 DOORS) · airframe 25,323 hrs · 21,279 cycles

DURING SCHEDULED RON, FOUND R1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1 AND R2 DOOR EVAC SLIDES PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,323 hrs · 21,279 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM SUPPORTS AT BS 859, LBL 3, BS 794, LBL 3, CORRODED. REPAIRED FLOORBEAMS PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,323 hrs · 21,279 cycles

DURING SCHEDULED RON, FOUND R1 DOOR CUTOUT UPPER AFT STOP SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,323 hrs · 21,279 cycles

DURING RON CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 14 ABC, INOP. RELAMPED LIGHT PER MM.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 25,223 hrs · 21,190 cycles

DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHT AT R1 DOOR, INOP. SECURED GROUND WIRE PER MM.

Part: DOOR — DAMAGED (MLG) · airframe 25,223 hrs · 21,190 cycles

AIR TURNBACK, AFTER GEAR RETRACTION ON TAKEOFF, RT GEAR LIGHT ILLUMINATED RED. CYCLED GEAR, NO HELP. FOUND BOTH RT CENTER AND INNER GEAR DOORS DAMAGED. REMOVED AND REPLACED BOTH RT GEAR DOORS PER MM.

Part: LIGHT — INOPERATIVE (ROW 10) · airframe 25,223 hrs · 21,190 cycles

DURING SCHEDULED PM CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT AT ROW 10 ABC, INOP. RELAMPED LIGHT PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 25,099 hrs · 21,097 cycles

DURING SCHEDULED C4 CHECK, FOUND PHOTOLUMINESCENT STRIPS AT 10 D AND 15 C, WORN. REMOVED AND REPLACED STRIPS PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,838 hrs · 20,091 cycles

AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED AFT LIGHT BATTERY PACK.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 23,051 hrs · 19,470 cycles

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

Part: PIN — CORRODED (RT MLG) · airframe 21,228 hrs · 17,998 cycles

DURING SCHEDULED C4 CHECK, FOUND RT MLG TRUNION PIN CORRODED. REMOVED AND REPLACED RT MLG TRUNION PIN PER MM.

Part: ENGINE — LEAKING (NR 2) · airframe 20,742 hrs · 17,627 cycles

ODOR IN CABIN DURING RT A/C PACK SYS IN USE. TERMINATED FLT AT TPA FOR INSPECTION OF NR 2 ENG AND FOUND OIL LEAK AT 6 O'CLOCK POSITION IN COMPRESSOR SECTION. REMOVED AND REPLACED NR 2 ENG PER MM.

Part: ROD — WORN (ELEVATOR) · airframe 19,356 hrs · 16,489 cycles

DURING SCHEDULED C2 CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR PUSH ROD AFT END ROD ASSY PER MM.

Part: SLIDE — LOW (FWD ENTRY DOOR) · airframe 17,589 hrs · 15,037 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 16,695 hrs · 14,289 cycles

EEPLS INOP FROM ROW 16 TO ROW 18. RECONNECTED WIRES PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 17,619 hrs · 15,255 cycles

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

Part: TRACK — LOOSE (CABIN) · airframe 15,325 hrs · 13,142 cycles

EEPLS TRACK LOOSE AT ROW 14. SECURED EEPLS PER MM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 15,009 hrs · 12,888 cycles

EMERGENCY EXIT LIGHT LENS OUT OF POSITION. REPOSITIONED LENS PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 14,898 hrs · 12,800 cycles

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

Part: PANEL — OVERHEATED (COCKPIT) · airframe 14,635 hrs · 12,565 cycles

AIR TURNBACK, DECLARED EMERGENCY. ELECTRICAL FUMES AND SMOKE IN COCKPIT WHILE CLIMBING THROUGH FL 250. REMOVED AND REPLACED BUS PROTECTION PANEL, ACCOMPLISHED COCKPIT CHECK AND ENG RUNS, OPS CHECK GOOD PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 14,550 hrs · 12,503 cycles

EEPLS WIRING EXPOSED AT ROW 14. SECURED WIRING PER MM.

Part: COVER — OUT OF POSITION (CABIN) · airframe 14,523 hrs · 12,479 cycles

EEPLS WIRING EXPOSED. REPOSITIONED TRACK COVERS AND INSTALLED LENS PER MM.

Part: RETAINER — LOOSE (SERVICE DOOR) · airframe 13,864 hrs · 11,961 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE AFT GIRT ASSY RETAINER HOOK LOOSE. SECURED RETAINER HOOK PER MM.

Part: SLIDE ASSY — SAGGING (FWD DOORS)

DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. ADJUSTED SLIDE ASSY'S PER MM.

Part: DOOR WARNING — ILLUMINATED (COCKPIT)

ABORTED TAKEOFF, AFT ENTRY DOOR LIGHT ILLUMINATED 80 KNOTS DURING TAKEOFF. OPERATED AND INSPECTED AFT ENTRY DOOR SEVERAL TIMES PER MM. OPS CK GOOD.