N607SW

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 67,015 hrs · 53,287 cycles

AFT GALLEY AREA EMERGENCY EXIT LIGHT WIRE BROKEN. REPAIRED THE WIRE IAW WDM AND AMM.

Part: LENS — BROKEN (CABIN) · airframe 67,015 hrs · 53,287 cycles

AFT GALLEY AREA EMERGENCY EXIT LIGHT BASE AND LENS BROKEN. R&R LENS IAW AMM.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 67,015 hrs · 53,287 cycles

FORWARD GALLEY AREA EMERGENCY EXIT LIGHT WIRE BROKEN. REPAIRED THE WIRE IAW WDM AND AMM.

Part: FITTING — CRACKED (L1 DOOR) · airframe 67,015 hrs · 53,287 cycles

L1 DOOR LOWER FRAME RT SIDE CLIP CRACKED. R&R CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,015 hrs · 53,287 cycles

R1 DOOR LOWER FRAME ANGLE CRACKED. R & R THE ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 67,015 hrs · 53,287 cycles

LT WING NR 3 INBOARD FLAP OUTBOARD TRACK TRAILING EDGE ANGLE CRACKED AT RSS 268. R&R ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (LT WINGWING) · airframe 67,015 hrs · 53,287 cycles

LEFT WING TRAILING EDGE ANGLE CRACKED AT LEVEL OF RSS. 545. R & R THE ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,015 hrs · 53,287 cycles

FORWARD GALLEY AREA FLOORBEAM CRACKED AT BS 312, RBL 20. REPAIRED FLOORBEAM IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 67,015 hrs · 53,287 cycles

R1 DOOR CUTOUT STUB-FRAME CRACKED AT BS 296.4, BETWEEN STR 7R TO STR 8R . REPAIRED STUB FRAME IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,015 hrs · 53,287 cycles

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

Part: ANGLE — CRACKED (LT WING) · airframe 67,015 hrs · 53,287 cycles

LT WING TRAILING EDGE ANGLE CRACKED AT APPROXIMATE LEVEL RSS 268, LOWER SURFACE. R&R ANGLE IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 67,015 hrs · 53,287 cycles

AFT CARGO COMPARTMENT STRAP CRACKED AT BS 787, BETWEEN STR 18R TO STR 25R. R&R STRAP IAW SRM AND DWG.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 67,015 hrs · 53,287 cycles

RT WING FIXED TRAILING EDGE SKIN PANEL CRACKED ON RSS 270. R&R PLATE IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,015 hrs · 53,287 cycles

FORWARD GALLEY AREA WEB INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 32. R&R INTERCOSTAL IAW SRM AND DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 67,015 hrs · 53,287 cycles

RT WING FIXED TRAILING EDGE ANGLE CRACKED ON RSS 545. R&R ANGLE IAW SRM AND DWG.

Part: LENS — BROKEN (CABIN) · airframe 67,015 hrs · 53,287 cycles

FORWARD GALLEY EMERGENCY EXIT LIGHT LENS BROKEN. R&R LENS IAW AMM.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 67,015 hrs · 53,287 cycles

FORWARD GALLEY AREA EMERGENCY FLASHLIGHT BASE BROKEN. R&R FLASHLIGHT BASE IAW CMM.

Part: ANGLE — CRACKED (BS 277-291) · airframe 67,015 hrs · 53,287 cycles

R1 DOOR ANGLE CUTOUT CRACKED BETWEEN BS 277 TO 291.5, BETWEEN STRINGERS 10 TO 11R. REPAIRED THE ANGLE IAW EA.

Part: ANGLE — CRACKED (RT WING) · airframe 67,015 hrs · 53,287 cycles

RIGHT WING FIXED TRAILING EDGE ANGLE CRACKED ON RSS. 252. R & R THE ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,015 hrs · 53,287 cycles

ANGLE CRACKED BETWEEN BS 380 TO BS 400, BL 0. R&R ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 67,015 hrs · 53,287 cycles

RT WING FIXED TRAILING EDGE ANGLE CRACKED ON RSS 270. R&R ANGLE IAW SRM & DWG.

Part: WEB — CRACKED (NLG WW) · airframe 67,015 hrs · 53,287 cycles

LT NOSE WHEEL WELL WEB CRACKED BETWEEN BS 230 TO BS 260, BETWEEN WL 165 TO WL190. REPAIRED WEB IAW EA.

Part: WEB — CRACKED (NLG WW) · airframe 67,015 hrs · 53,287 cycles

RT NOSE WHEEL WELL WEB CRACKED BETWEEN BS 230 TO BS 260, BETWEEN WL 165 TO WL 190. REPAIRED WEB IAW EA.

Part: LENS — MISSING (CABIN) · airframe 67,015 hrs · 53,287 cycles

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

Part: SIGN — BROKEN (CABIN) · airframe 66,875 hrs · 53,199 cycles

AFT GALLEY DOOR EXIT SIGN BROKEN. REPAIRED SIGN PER SIP.

Part: SLIDE — UNSECURE (L2 DOOR) · airframe 66,706 hrs · 53,086 cycles

L2 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF ITS COMPARTMENT, DID NOT DEPLOY. REINSTALLED SLIDE IAW TC.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,680 hrs · 52,403 cycles

RIGHT CABIN EMER EXIT BULLNOSE LIGHTS INOPERATIVE, BETWEEN ROW 1 - 12. REPAIRED LIGHT ASSEMBLY IAW MM.

Part: TRANSMITTER — FAULTY (HYDRAULIC SYS) · airframe 65,241 hrs · 52,113 cycles

AT CRUISE HYD SYS A PRESS INDICATOR READ 900 PSI A HYD QTY NORMAL. ALL A SYSTEMS OPERATED NORMALLY & PRESS LIGHTS NORMAL AFTER GEAR EXTENSION, HYD SYS A INDICATION NORMAL THROUGH SHUTDOWN. R & R A HYD SYS PRESS TRANSMITTER AMM.

Part: FITTING — CRACKED (RT WING) · airframe 64,514 hrs · 51,664 cycles

RIGHT WING AFT MLG FITTING CRACKED AT RSS 221, COMMON TO UPPER CHORD. R & R FITTING IAW EA.

Part: ATTACH FITTING — CRACKED (LT WING) · airframe 64,514 hrs · 51,664 cycles

LEFT MLG ATTACH FITTING CRACKED AT STATION RSS 221. R & R FITTING IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,514 hrs · 51,664 cycles

LEFT WING UPPER SKIN FASTENER HOLES CRACKED, BETWEEN RSS 248 - 254. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,514 hrs · 51,664 cycles

RIGHT WING REAR SPAR WEB CRACKED AT RSS 218, IN FASTENER HOLE COMMON TO UPPER CHORD. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 64,514 hrs · 51,664 cycles

RIGHT WING UPPER SKIN TE CRACKED AT RSS 270.5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 64,514 hrs · 51,664 cycles

RIGHT WING UPPER SKIN TE CRACKED AT RSS 251. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 64,514 hrs · 51,664 cycles

RIGHT WING UPPER SKIN TE CRACKED AT RSS 241. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,514 hrs · 51,664 cycles

RIGHT WING REAR SPAR, WEB CRACKED AT RSS 224, UPPER FASTENER HOLE COMMON TO FWD & AFT MLG FITTINGS. REPAIRED WEB IAW EA.

Part: STIFFENER — CRACKED (LT WING) · airframe 64,514 hrs · 51,664 cycles

LEFT WING REAR SPAR, STIFFENER CRACKED AT RSS 194.04. REPAIRED STIFFENER IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 64,514 hrs · 51,664 cycles

LEFT WING AFT SPAR WEB CRACKED AT RSS 224, COMMON TO UPPER CHORD. REPAIRED AFT SPAR IAW EA.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 64,514 hrs · 51,664 cycles

AFT LAVATORY EMER EXIT SIGN BULB INOPERATIVE. R & R SIGN IAW AMM.

Part: SPAR — CRACKED (RT WING) · airframe 64,514 hrs · 51,664 cycles

RIGHT WING AFT SPAR, UPPER CHORD CRACKED AT RSS 224. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 64,514 hrs · 51,664 cycles

LEFT WING REAR SPAR, UPPER CHORD CRACKED AT RSS 224. REPAIRED CHORD IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,204 hrs · 51,446 cycles

AFT PRESS BULKHEAD WEB TO Y CHORD ATTACHMENT, CRACKED AT BS 1016, BETWEEN STRINGER 5L - 7L. REPAIRED WEB IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,148 hrs · 51,406 cycles

LEFT OVERWING EXIT WINDOW LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 64,074 hrs · 51,353 cycles

L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SIGN — LOOSE (CABIN) · airframe 63,652 hrs · 51,052 cycles

FORWARD ENTRY EXIT SIGN LOOSE. SECURED SIGN IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,025 hrs · 50,601 cycles

AFT RT EMER EXIT BULLNOSE LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: SKIN — DELAMINATED (LT SPOILER) · airframe 61,977 hrs · 49,877 cycles

LEFT WING NR 2 FLIGHT SPOILER UPPER SURFACE DELAMINATED. R & R NR 2 SPOILER IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 61,977 hrs · 49,877 cycles

L2 DOOR EXIT LIGHT INOPERATIVE. R & R POWER SUPPLY IAW AMM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

STRAP CRACKED AT BS 344, LBL 11.10. R & R STRAP IAW SRM & DWG.

Part: BRACKET — CRACKED (RT SPOILER) · airframe 61,977 hrs · 49,877 cycles

RIGHT WING NR 5 GND SPOILER SUPPORT FITTING BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

TIE CLIP CRACKED AT BS 947.5, STRINGER 26L. R & R TIE CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 61,977 hrs · 49,877 cycles

LEFT WING TE ANGLE CRACKED AT WBL 204. R & R ANGLE IAW SRM & DWG.

Part: PLATE — CRACKED (LT WING) · airframe 61,977 hrs · 49,877 cycles

LEFT WING TE PLATE CRACKED AT WBL 204. R & R PLATE IAW DWG & SRM.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

FORWARD GALLEY DOOR CUT OUT REVEAL CRACKED BETWEEN BS 326.5 TO 330, STRINGER 17R. R & R CUT OUT IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

FUSELAGE WEB CRACKED AT STATION 500 TO 500A, STRINGER 26L. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

FUSELAGE WEB CRACKED AT STATION 500A TO 500B, STRINGER 26L. REPAIRED WEB IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

FRAME SHEAR TIE CRACKED AT BS 967, STRINGER 27L+3. REPAIRED SHEAR TIE IAW EO & EA.

Part: TAB — DELAMINATED (LT AILERON) · airframe 61,977 hrs · 49,877 cycles

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

Part: PANEL — CORRODED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

FUSELAGE KEEL BEAM LOWER WEB PANEL CORRODED, BETWEEN BS 570 TO 587. REPAIRED PANEL IAW EO & EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,977 hrs · 49,877 cycles

RIGHT INBD AFT FLAP DELAMINATED AT LOWER SURFACE. REPAIRED FLAP IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,977 hrs · 49,877 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

FLOORBEAM CORRODED AT STATION 344, LBL 2. REPAIRED FLOORBEAM IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

SUPPORT BRACKET CRACKED AT BS 947.5, STRINGER 25R. R & R BRACKET IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

SKIN CORRODED AT BS 967, STRINGER 27L. REPAIRED SKIN IAW EO & EA.

Part: LIGHT — BROKEN (CABIN) · airframe 61,977 hrs · 49,877 cycles

FORWARD GALLEY EMER EXIT LIGHT WIRE RECEPTACLE BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: FRAME — CORRODED (RT WING) · airframe 61,977 hrs · 49,877 cycles

LEFT WING A FRAME NR 8 CORRODED AT BORES. REPAIRED FRAME IAW CMM.

Part: FRAME — CORRODED (LT WING) · airframe 61,977 hrs · 49,877 cycles

LEFT WING A FRAME NR 2 CORRODED AT BORES. REPAIRED FRAME IAW CMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

STRINGER CLIP CRACKED AT STATION 380, STRINGER 22L. R & R CLIP IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

STRINGER SPLICE CORRODED AT BS 360, STRINGER 19R. R & R SPLICE IAW SRM.

Part: FRAME — CORRODED (RT WING) · airframe 61,977 hrs · 49,877 cycles

RIGHT WING A FRAME NR 7 CORRODED AT BORES. REPAIRED FRAME IAW CMM.

Part: FRAME — CORRODED (LT WING) · airframe 61,977 hrs · 49,877 cycles

LEFT WING A FRAME NR 1 CORRODED AT BORES. REPAIRED FRAME IAW CMM.

Part: SUPPORT ANGLE — CRACKED (LT PYLON) · airframe 61,977 hrs · 49,877 cycles

LEFT PYLON NACELLE SUPPORT ANGLE CRACKED ON NACELLE STRUT INBD SIDE AT STATION 277.24. R & R ANGLE IAW SRM & DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

INNER CHORD CORRODED BETWEEN BS 294.5 TO BS 344, STRINGER 17L. R & R CHORD IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, BETWEEN RBL 13 TO RBL 20. REPAIRED CHORD IAW EO & EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

WEB CORRODED BETWEEN BS 420 TO 440, STRINGER 17R. R & R WEB IAW SRM & DWG.

Part: SKIN — CRACKED (LT WING) · airframe 61,977 hrs · 49,877 cycles

LEFT WING EXTERNAL SKIN ON FIXED LE UPPER SURFACE CRACKED AT STATION 208. REPAIRED SKIN IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, BETWEEN LBL 5 TO LBL 44. REPAIRED CHORD IAW EO & EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,977 hrs · 49,877 cycles

RIGHT WING EXTERNAL SKIN CRACKED ON FIXED LE UPPER SURFACE IN LEVEL WBL 157.00. REPAIRED SKIN IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, RBL 43. REPAIRED CHORD IAW EO & EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

STRINGER CORRODED BETWEEN BS 907+5 TO 927+5, STRINGER 21R. R & R STRINGER IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

STRINGER SPLICE CRACKED AT BS 360, STRINGER 2L. R & R SPLICE IAW EO & EA.

Part: STRUCTURE — CORRODED (R2 DOOR) · airframe 61,977 hrs · 49,877 cycles

R2 DOOR INNER CHORD CORRODED BETWEEN BS 947.5+9 TO 986.5+8, STRINGER 17R. R & R CHORD IAW SRM & DWG.

Part: FITTING — CORRODED (TE FLAP) · airframe 61,977 hrs · 49,877 cycles

RIGHT WING INBD MID FLAP INBD GIMBAL CORRODED. R & R GIMBAL ASSEMBLY IAW MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

RIGHT MLG BAY ANGLE CRACKED AT LEVEL BS 663.75 + 17, STRINGER 20R. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

FRAME CORRODED AT BS 947.5, BETWEEN STRINGER 27L TO 27R. R & R FRAME IAW SRM & DWG.

Part: FITTING — CORRODED (TE FLAP) · airframe 61,977 hrs · 49,877 cycles

RIGHT WING OTBD MID FLAP INBD GIMBAL CORRODED. R & R GIMBAL ASSEMBLY IAW MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

AFT CARGO COMPARTMENT LOWER FLANGE OF FRAME CORRODED AT BS 967, BETWEEN STRINGER 27L TO 27R. REPAIRED FRAME IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

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

Part: FITTING — CORRODED (TE FLAP) · airframe 61,977 hrs · 49,877 cycles

LEFT WING INBD MID FLAP INBD GIMBAL CORRODED. R & R GIMBAL ASSEMBLY IAW MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 400, STRINGER 26L. R & R ANGLE IAW SRM & DWG.

Part: FITTING — CORRODED (TE FLAP) · airframe 61,977 hrs · 49,877 cycles

LEFT WING INBD MID FLAP OTBD GIMBAL CORRODED. R & R GIMBAL ASSEMBLY IAW MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

STRINGER CLIP CRACKED AT STATION 727B, STRINGER 22L. R & R CLIP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 61,977 hrs · 49,877 cycles

SUPPORT ANGLE CRACKED AT LT WING STATION RSS 533 + 12. R & R SUPPORT ANGLE IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

AFT CARGO COMPARTMENT SKIN CORRODED BETWEEN BS 794.3 TO 807, BETWEEN STRINGER 25R TO 26R. REPAIRED SKIN IAW EO & EA.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 61,977 hrs · 49,877 cycles

SUPPORT ANGLE CRACKED AT RT WING STATION RSS 533 + 12. R & R SUPPORT ANGLE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

FORWARD CARGO COMPARTMENT CREASE BEAM OUTER CHORD CORRODED AT BS 420+2.5, STRINGER 17R. REPAIRED CHORD IAW EA.

Part: LIGHT — DAMAGED (CABIN) · airframe 61,977 hrs · 49,877 cycles

CENTER AFT CABIN EEPLS DAMAGED. R & R EEPLS IAW DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

AFT ENTRY DOOR CUT OUT LOWER FWD CORNER STUB FRAME CRACKED AT BS 947+13, STRINGER 17L. REPAIRED STUB FRAME IAW EO & EA.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 61,977 hrs · 49,877 cycles

AFT CARGO COMPARTMENT DOOR CROSSBEAM E T CHORD CRACKED. REPAIRED T CHORD IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

FRAME CRACKED AT BS 947.5, STRINGER 26R. R & R FRAME IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

LOWER FRAME FLANGE CORRODED AT BS 747 BETWEEN STRINGER 26R TO 27R. REPAIRED FLANGE IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

TIE CLIP CRACKED AT BS 947.5, STRINGER 25R. R & R TIE CLIP IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

AFT CARGO COMPARTMENT SUPPORT ANGLE CRACKED AT BS 727D+12 BETWEEN STRINGER 27L TO 27R. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

FRAME CRACKED AT BS 947.5, STRINGER 19L. R & R FRAME IAW SRM & DWG.

Part: STRAP — FRAYED (CABIN) · airframe 61,977 hrs · 49,877 cycles

FRAYED ESCAPE STRAP LOCATED ON CUT OUT AREA OF LT EMER EXIT. REPLACED ESCAPE STRAP IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

SKIN CRACKED AT BS 947+11, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

BEAR STRAP SKIN CRACKED AT BS 947+10.5", STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

LONGITUDINAL BEAM UPPER CHORD CRACKED AT BS 671.25, RBL 24.5. REPAIRED CHORD IAW EA.

Part: LIGHT — BROKEN (CABIN) · airframe 61,977 hrs · 49,877 cycles

NUMBER 4 GALLEY EMER EXIT LIGHT ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 666, LBL 24.5. REPAIRED CHORD IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,977 hrs · 49,877 cycles

R1 DOOR OUTER SKIN UPPER CORNER OF LOWER HINGE CUT OUT CRACKED. REPAIRED CUT OUT IAW EO & EA.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 61,658 hrs · 49,662 cycles

FLIGHT DECK EMER LIGHT, ABOVE OBSERVER SEAT INOPERATIVE. R & R LIGHT IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,658 hrs · 49,662 cycles

INTERCOSTAL ASSEMBLY CRACKED AT BS 348.2 STRINGER 16L. R & R INTERCOSTAL IAW DWG & SRM.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 61,658 hrs · 49,662 cycles

FORWARD CARGO DOOR CUT OUT FWD LOWER CORNER REVEALED CRACK. REPAIRED REVEAL IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,658 hrs · 49,662 cycles

LOWER ANGLE CRACKED AT BS 348 STRINGER 15L. R & R ANGLE IAW DWG & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,658 hrs · 49,662 cycles

AFT CARGO DOOR CUT OUT FWD LOWER CORNER CRACKED. REPAIRED CUT OUT IAW EA.

Part: LENS — CRACKED (CABIN) · airframe 61,597 hrs · 49,620 cycles

L1 DOOR LOWER EMER EXIT LIGHT LENS CRACKED. R & R LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 61,597 hrs · 49,620 cycles

R1 DOOR LOWER EMER EXIT LIGHT LENS CRACKED. R & R LENS IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 61,597 hrs · 49,620 cycles

CABIN FWD EMER EXIT LIGHT LENS LOOSE. R & R LENS ASSEMBLY IAW AMM.

Part: ANGLE — CRACKED (LT WING) · airframe 61,597 hrs · 49,620 cycles

LEFT WING TE UPPER SHELF PANEL CRACKED ANGLE AT INBD FLAP OTBD TRACK ATTACHMENT. R & R ANGLE IAW SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,318 hrs · 49,421 cycles

FORWARD ENTRY FLASHLIGHT BATTERY INOPERATIVE. R & R BATTERY IAW MM.

Part: COVER — MISSING (EXIT SIGN) · airframe 60,754 hrs · 49,011 cycles

FORWARD PAX CABIN EXIT SIGN ABOVE THE CTR AISLE MISSING COVER. R & R COVER IAW MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 60,239 hrs · 48,666 cycles

FORWARD INBD FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 59,834 hrs · 48,401 cycles

LEFT CABIN OVERHEAD BIN BULLNOSE EMERGENCY LIGHT LENS MISSING AT ROW 18. INSTALLED LENS IAW MM.

Part: SIGN — UNSECURE (CABIN) · airframe 59,225 hrs · 48,001 cycles

OVERWING EMERGENCY EXIT SIGN FELL OFF. REINSTALLED SIGN IAW SIP.

Part: LENS — BROKEN (CABIN) · airframe 59,218 hrs · 47,996 cycles

LT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. R & R LENS IAW SIP.

Part: SIGN — LOOSE (CABIN) · airframe 58,878 hrs · 47,752 cycles

CENTER CABIN CEILING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN IAW AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 58,068 hrs · 47,147 cycles

LT WING OTBD FORE FLAP DELAMINATED. R&R FORE FLAP IAW AMM.

Part: LUG — BROKEN (LT SPOILER) · airframe 57,485 hrs · 46,726 cycles

LEFT WING INBD GROUND SPOILER CENTER INBD LUG BROKEN. R & R SPOILER IAW AMM.

Part: SPOILER — CRACKED (RT WING) · airframe 57,472 hrs · 46,720 cycles

RIGHT WING INBD GROUND SPOILER NR 5 INBD CRACKED. R & R SPOILER IAW MM.

Part: COVER — CRACKED (L1 DOOR) · airframe 56,083 hrs · 45,742 cycles

L1 DOOR LINER, PLASTIC DOOR HANDLE COVER IS CRACKED. REPLACED FORWARD ENTRY DOOR LINER PLASTIC HANDLE COVER IAW AMM TASK 52-11-31-404-009.

Part: PLATE — CRACKED (FLAP FAIRING) · airframe 56,083 hrs · 45,742 cycles

LEFT WING NR 3 FLAP FAIRING DOOR SPRING CRACKED IN TWO PLACES ON EDGE. REMOVED AND REPLACED PLATE IAW SRM AND BOEING DRAWING.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 56,083 hrs · 45,742 cycles

PIT STA 492, DOOR CUTOUT FRAME CLOSE OUT WEB, LOWER END CRACKED. REPAIRED WEB IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,083 hrs · 45,742 cycles

FRAME AT STA 807, S-25R TO 26R CORRODED ON FORWARD SIDE COMMON TO FUSELAGE SKIN. REPAIRED FRAME IAW SRM AND AMM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 56,083 hrs · 45,742 cycles

AFT PIT DOOR CUTOUT, STA 847, STR 25R TO 26R, WEB SUPPORT ANGLE COMMON TO FRAME CORRODED. REMOVED AND REPLACED ANGLE PER SRM.

Part: SKIN — CRACKED (TE FLAP) · airframe 56,083 hrs · 45,742 cycles

LEFT WING I/B FORE FLAP SIDE SKIN CRACKED. REPLACED FORE FLAP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,083 hrs · 45,742 cycles

STR 12L CLIP OF L1 ENTRY DOOR CRACKED ON BOTTOM SIDE. REMOVED AND REPLACED CLIP IAW BOEING DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 56,083 hrs · 45,742 cycles

RIGHT WING TRAILING EDGE SUPPORT ANGLE CRACKED AT THIRD FASTENER HOLE FROM TOP. REMOVED AND REPLACED ANGLE IAW BOEING DWG.

Part: PLATE — CRACKED (LT HORIZ STAB) · airframe 56,083 hrs · 45,742 cycles

LEFT HORIZONTAL STABILIZER, PANEL 9126L, SHORT METAL SEAL PLATE CRACKED (MARKED). REMOVED AND REPLACED SHORT METAL SEAL PLATES ON LEFT HORZ STAB PANEL 9126L IAW SOPM 20-50-01.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 56,083 hrs · 45,742 cycles

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

Part: RUB STRIP — DAMAGED (LT PYLON) · airframe 56,083 hrs · 45,742 cycles

LEFT PYLON UPPER SURFACE RUB STRIP CRACKED. REMOVED AND REPLACED RUB STRIP IAW SRM 5 AND DWG.

Part: COVER — CRACKED (RT WING) · airframe 56,083 hrs · 45,742 cycles

RIGHT WING TRAILING EDGE TORQUE BOX COVER CRACKED O/B OF NR 6 FLAP TRACK FAIRING. REMOVED AND REPLACED COVER IAW BOEING DWG.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 56,083 hrs · 45,742 cycles

PASSENGER CABIN PRESSURE DECK CRACKED NEAR STA 666, LBL 30. REMOVED AND REPLACED PRESSURE DECK IAW SRM.

Part: SLAT TRACK — CRACKED (LE SLAT) · airframe 56,083 hrs · 45,742 cycles

LEFT WING NR 2 SLAT LOWER SURFACE, AT I/B AUX TRACK CRACKED AT 2 EA FASTENER HOLES IN SKIN. REMOVED AND REPLACED TRACK IAW SRM.

Part: COVER — CRACKED (R1 DOOR) · airframe 56,083 hrs · 45,742 cycles

FWD GALLEY DOOR CUTOUT AFT FRAME UPPER LATCH FITTING DOOR WARNING SWITCH COVER IS CRACKED. REMOVED CRACKED R1 DOOR WARNING SWITCH COVER AND INSTALLED NEW COVER 284N1061-11 IAW SRM 51-40-02.

Part: COVER — CRACKED (L1 DOOR) · airframe 56,083 hrs · 45,742 cycles

ENTRY DOOR LOWER HINGE ARM COVER CRACKED. REPAIRED COVER IAW SRM AND DWG.

Part: SIGN — LOOSE (CABIN) · airframe 55,665 hrs · 45,440 cycles

MID CABIN OVERHEAD EMERGENCY EXIT SIGN LOOSE. SECURED LIGHT ASSY PER M/M.

Part: PLATE — BROKEN (R1 DOOR) · airframe 55,679 hrs · 45,450 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LATCH BROKEN. SECURED FLOOR PLATE PER M/M.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 55,477 hrs · 45,298 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: LENS — MISSING (CABIN) · airframe 55,407 hrs · 45,244 cycles

AFT EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS IAW AMM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

SHEAR TIE CRACKED AT BS 927, BETWEEN STR 10L AND STR 11L. REPAIRED SHEAR TIE IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

STRINGER CRACKED BETWEEN BS 360 TO BS 380, STR 2L. REPAIRED STRINGER IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

STRINGER CLIP CRACKED AT BS 500D, STR 2L. REMOVED AND REPLACED CLIP IAW SRM & BAC DWG.

Part: STRINGER — PUNCTURED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

STRINGER PUNCTURED AT BS 360+6, STR 2R. REPAIRED STRINGER PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

STRINGER CLIP CRACKED AT BS 400, STR 7R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 360+10 UPPER FORWARD CORNER CUTOUT. REMOVED AND REPLACED SKIN IAW BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 847+10 UPPER AFT CORNER CUTOUT. REMOVED AND REPLACED SKIN IAW BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 807+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 867+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 787+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 767+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 727B+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 807+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 727+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA AND REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 867+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 827+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB AND TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 727B+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 767+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 847+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 787+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 727A+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW TC AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 827+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB AND TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 887+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 727+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 887+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 727E+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 847+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 887+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW TC & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 787+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB AND TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 420+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 440+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 360+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500A+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB & TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 480+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 767+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB AND TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500A+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 420+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 827+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 480+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 400+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 767+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB AND TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 360+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 727C+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW TC & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKD AT BS 360+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 460+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 440+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 520+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 440+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500B+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB & TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 400+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 867+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA AND REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 460+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500B+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW REO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 460+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW REO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 380+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 400+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 420+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 867+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW TC & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 380+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 400+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 380+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: STRINGER — PUNCTURED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

STRINGER PUNCTURED AT BS 500D+16, STR 8L. REPAIRED STRINGER IAW REO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 360+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW REO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 420+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500B+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW REO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 440+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW TC & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 807+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 727+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA AND REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 847+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 500C+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 787+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB AND TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 847+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 727+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 380+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 460+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 400+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 807+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 480+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN AIW TC & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 520+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 480+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 887+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 520+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 500C+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN PER SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,407 hrs · 45,244 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 520+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,115 hrs · 45,016 cycles

SKIN CRACKED AT BS 908+1.5, STR 10L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,115 hrs · 45,016 cycles

SKIN CRACKED AT BS 907, STR 10L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,115 hrs · 45,016 cycles

SKIN CRACKED AT BS 908, STR 10L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,115 hrs · 45,016 cycles

SKIN CRACKED AT BS 907-12, STR 10L. REPAIRED SKIN IAW EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 54,978 hrs · 44,908 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 54,674 hrs · 44,673 cycles

RIGHT WING OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP ASSY PER AMM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 54,674 hrs · 44,673 cycles

R1 DOOR CRACKED LOWER FRAME AFT CORNER. REMOVED AND REPLACED R1 DOOR PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,565 hrs · 44,589 cycles

FUSELAGE SKIN CRACKED AT BS 727C + 13, STRINGER 3L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,565 hrs · 44,589 cycles

FUSELAGE SKIN CRACKED AT BS 727C + 10, STRINGER 4R. REPAIRED SKIN PER EA.

Part: WINDOW — ARCED (COCKPIT) · airframe 54,227 hrs · 44,327 cycles

R1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED R1 WINDOW PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 54,049 hrs · 44,192 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. INSTALLED SLIDE PER MT.

Part: LIGHT — BROKEN (CABIN) · airframe 53,217 hrs · 43,551 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,115 hrs · 43,466 cycles

DURING SCHEDULED RON CHECK, FOUND RT EEPLS INOP BETWEEN ROW 8 TO ROW 15. RELAMPED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,115 hrs · 43,466 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 500D+14, STR 4L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 61,977 hrs · 49,877 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 120.30 +5.25 JUST FWD OF AFT SPAR. REPAIRED SKIN IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 51,656 hrs · 42,352 cycles

R1 DOOR EMERGENCY LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 51,218 hrs · 42,014 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 51,090 hrs · 41,919 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EXTERNAL EXIT LIGHT INOP. SECURED LAMP PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 670, LBL 24.5. REPAIRED CHORD PER EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 1 TO ROW 3. REMOVED AND REPLACED BATTERY ASSY PER MM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 758 TO BS 793, RBL 3.0. REPAIRED CHANNEL PER EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT LAV WALL EMERGENCY EXIT INOP. REMOVED AND REPLACED BATTERY ASSY PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT SKIN CRACKED. REPAIRED NR 2 SLAT PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 993, STR 17R. REPAIRED FRAME PER EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING O/B AFT FLAP I/B EDGE LOWER SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, BETWEEN LBL 17 TO RBL 40. REPAIRED BEAM PER EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD GALLEY EMERGENCY EXIT INOP. REMOVED AND REPLACED BATTERY ASSY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD GALLEY EMERGENCY EXIT INOP. REMOVED AND REPLACED BATTERY ASSY PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED AT BS 294.5, RBL 54. REPAIRED BEAM PER EO AND EA.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 1 SLAT I/B UPPER EDGE SURFACE DELAMINATED. REMOVED AND REPLACED NR 1 SLAT PER MM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CORRODED BETWEEN BS 986.5 TO BS 993, STR 17R. REPAIRED ANGLE PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT GALLEY EMERGENCY EXIT INOP. REMOVED AND REPLACED BATTERY ASSY PER MM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 3 SLAT I/B UPPER EDGE SURFACE DELAMINATED. REMOVED AND REPLACED NR 3 SLAT PER MM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 3 SLAT O/B EDGE UPPER SURFACED DELAMINATED. REPAIRED NR 3 SLAT PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500C, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 203.8, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 807, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER EO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN STR 27R AND RT KEEL BEAM OF FWD CARGO COMPARTMENT. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 727 BULKHEAD LOWER AREA. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727A, STR 19L. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CRACKED AT BS 380, STR 5L. REPAIRED STRINGER PER SRM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CORRODED AT BS 1016, BBL 0. REPAIRED STIFFENER PER ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 27L TO STR 28L. REPAIRED FRAME PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 500C TO BS 500D, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 296.4, STR 17R. REPAIRED FRAME PER EA.

Part: LENS — BROKEN (EXIT SIGN) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD LAVATORY WALL EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 380 TO BS 400, STR 17R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5, LBL 5. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND ANGLE CORRODED AT BS 337, STR 21L. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT DELAMINATED. REPAIRED NR 2 SLAT PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING O/B MID FLAP DELAMINATED. REPAIRED MID FLAP PER SRM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FRAME DOUBLER CORRODED AT BS 793, STR 25R. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CORRODED BETWEEN BS 727D TO BS 727E, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SKIN PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT DELAMINATED. REPAIRED NR 5 SLAT PER SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CORRODED AT BS 1016, STR 17R. REMOVED AND REPLACED ANGLE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND ANGLE CORRODED AT BS 321, STR 21L. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER TIE CRACKED AT BS 400, STR 27L. REMOVED AND REPLACED STRINGER TIE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 12L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING O/B END OF I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

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

Part: SKIN — DELAMINATED (LE SLAT) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING I/B EDGE UPPER SURFACE SLAT DELAMINATED. REPAIRED SLAT PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 28L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 11L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SLAT — DELAMINATED (RT WING) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT I/B EDGE DELAMINATED. REPAIRED SLAT PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING O/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT O/B EDGE DELAMINATED. REPAIRED SLAT PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 50,927 hrs · 41,796 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 4 SLAT I/B EDGE DELAMINATED. REPAIRED SLAT PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,721 hrs · 41,639 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER CRACKED AT BS 932, STR 5R. REPAIRED STRINGER PER EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 49,830 hrs · 40,947 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REMOVED AND REPLACED SLIDE PER MT.

Part: LENS — BROKEN (CABIN) · airframe 49,348 hrs · 40,561 cycles

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

Part: LENS — MISSING (CABIN) · airframe 49,160 hrs · 40,411 cycles

RT OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING BETWEEN ROW 15 TO ROW 16. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,240 hrs · 39,753 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 514D, STR 10L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,406 hrs · 45,244 cycles

FUSELAGE SKIN CRACKED AT BS 500D+14, STR 10L. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 48,229 hrs · 39,746 cycles

L2 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 47,945 hrs · 39,542 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 2 SLAT UPPER WEDGE SKIN DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 47,945 hrs · 39,542 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 5 SLAT UPPER WEDGE SKIN DELAMINATED. REMOVED AND REPLACED NR 5 SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,927 hrs · 39,528 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 510, STR 8L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,936 hrs · 39,536 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 510, STR 8L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,406 hrs · 45,244 cycles

CROWN SKIN CRACKED AT BS 510, STR 8L. REPAIRED SKIN PER EA.

Part: LENS — CRACKED (CABIN) · airframe 47,268 hrs · 39,042 cycles

R2 DOOR EMERGENCY EXIT SIGN LENS CRACKED. REMOVED AND REPLACED LENS ASSY PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 46,502 hrs · 38,474 cycles

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

Part: LIGHT — WORN (CABIN) · airframe 46,439 hrs · 38,425 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND EEPLS STRIP WORN BETWEEN ROW 21 TO ROW 23. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 46,439 hrs · 38,425 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 46,439 hrs · 38,425 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: ACTUATOR — INOPERATIVE (RT MLG) · airframe 45,947 hrs · 38,064 cycles

AIR TURNBACK, RT MLG EXTENDED WITH GEAR HANDLE IN OFF POSITION. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED AT BS 180, STR 23R. REPAIRED SKIN PER PAE ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND NOSE WHEEL WELL UPPER SKIN PANEL CRACKED AT BS 249.5, RBL 7.75. REPAIRED SKIN PER ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,719 hrs · 37,894 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: CABLE — OUT OF ADJUST (BLEED VALVE) · airframe 45,636 hrs · 37,841 cycles

AIR TURNBACK / DECLARED EMERGENCY. CRUISING AT 10,000 FT, AFTER DEPARTING OUT OF PHL, NR 2 ENGINE HAD A COMPRESSOR STALL OR BACKFIRED. RETURNING TO PHX EVERY TIME THE NR 2 THRUST WAS RETARDED, IT WOULD OCCUR AGAIN. BOROSCOPE NR 2 ENG PER MT. NO DAMAGE FOUND. ADJUSTED AND RIGGED VBV CABLE PER MM.

Part: COVER — MISSING (CABIN) · airframe 45,333 hrs · 37,628 cycles

LT OVERWING EMERGENCY EXIT SIGN COVER MISSING. INSTALLED LIGHT PER MM.

Part: PCU — LEAKING (AILERON) · airframe 45,306 hrs · 37,609 cycles

DIVERSION, A-SYSTEM HYDRAULIC QUANTITY DROPPED TO 1/4. REMOVED AND REPLACED A-AILERON PCU PER MM.

Part: MOTOR — FAULTY (NR 2 ENGINE) · airframe 45,269 hrs · 37,583 cycles

NR 2 ENGINE FAILED TO ACHIEVE CLIMB THRUST ABOVE 30,000 FT NEEDED 94.0 PERCENT N1 ONLY 93 PERCENT, WHEN AT STOP LIMITS AND 100 PERCENT N2. REMOVED AND REPLACED VBV MOTOR PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 43,000 hrs · 35,953 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,000 hrs · 35,953 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,000 hrs · 35,953 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 43,000 hrs · 35,953 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 41,285 hrs · 34,668 cycles

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

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 41,275 hrs · 34,661 cycles

DURING SCHEDULED BRDG CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 9 DEF. SECURED STRIP PER MM.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 40,621 hrs · 34,118 cycles

EEPLS PHOTOLUMINESCENT STRIP CRACKED BETWEEN ROW 8 DEF AND ROW 10 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 40,306 hrs · 33,854 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DOOR WAS NOT DISARMED, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: UPLOCK ACTUATOR — FAULTY (LT MLG) · airframe 39,847 hrs · 33,485 cycles

UNSAFE GEAR POSITION INDICATED UPON GEAR RETRACTION. FERRIED TO HOU FOR TROUBLESHOOTING. REMOVED AND REPLACED LT MLG UPLOCK ACTUATOR PER MM.

Part: LENS — DAMAGED (CABIN) · airframe 37,721 hrs · 31,875 cycles

DURING SCHEDULED A2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT LENS NOT LEGIBLE. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 36,578 hrs · 31,081 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED UPPER HINGE BOX FITTING PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 36,758 hrs · 31,081 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 35,000 hrs · 29,748 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 34,774 hrs · 29,552 cycles

BULLNOSE EMERGENCY LIGHT LENS LOOSE AT ROW 6. SECURED LENS PER MM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION AT BS 270, SUPPORT ANGLE CHORD, BETWEEN RBL 11 TO LBL 11. REPAIRED CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 24R. REPAIRED FRAME PER PAE ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE SHEAR TIE AT B3 767, LBL 8, WL 148. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, LBL 64, WL 202. REPAIRED FRAME PER PAE ER.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA SHEAR TIES CORRODED AT BS 767, RBL 8 & BS 787, RBL 10 TO LBL 8. REPAIRED SHEAR TIES PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB AT BS 300, WL 208, RBL 50. REPAIRED WEB PER SRM.

Part: WEDGE — DELAMINATED (RT WING SLAT) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND RT WING, NR 4 L/E SLAT, INBOARD END T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 370, STR 17L. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,842 hrs · 28,031 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB AT BS 385, STR 17L. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: ANGLE — CRACKED (FUELAGE) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE ANGLE CRACKED AT BS 294, RBL 55, WL 208. REMOVED AND REPLACED ANGLE PER SRM.

Part: GIRT BAR — CORRODED (L1 DOOR) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON L1 DOOR EVAC SLIDE, FWD & AFT GIRT BAR FLOOR FITTINGS. REMOVED AND REPLACED GIRT BAR FITTINGS PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB BETWEEN BS 747 TO BS 767, LBL 70, WL 208. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 9R. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE CREASE BEAM WEB AT BS 410, STR 17R. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 9L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,842 hrs · 28,031 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 1006, BL 0, WL 180. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED FITTINGS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, ABOVE STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR, UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: WEDGE — DELAMINATED (L/E SLAT) · airframe 32,842 hrs · 28,031 cycles

DURING SCHEDULED D-CHECK, FOUND RT WING, NR 5 L/E SLAT, I/B END T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 5 L/E SLAT ASSY PER MM.

Part: FIRE DETECTOR — FALSE INDICATION (CARGO BAY) · airframe 32,842 hrs · 28,031 cycles

DIVERSION, DECLARED EMERGENCY. FWD CARGO FIRE LIGHT ILLUMINATED ON DEPARTURE, DISCHARGED BOTH BOTTLES. INSPECTED BOTH FWD AND AFT CARGO BINS, PER MM, NO DEFECTS NOTED.

Part: TAB — CRACKED (RT ELEVATOR) · airframe 32,024 hrs · 27,397 cycles

DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR TAB CRACKED AT INBOARD HINGE CUTOUT. REMOVED AND REPLACED ELEV TAB PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 32,024 hrs · 27,397 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 32,024 hrs · 27,397 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE ASSY PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 32,024 hrs · 27,397 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: RELAY — FAULTY (INSTRUMENT PANEL) · airframe 31,991 hrs · 27,370 cycles

AIR TURNBACK, DURING ROTATION ACFT LOST ALL N1, EGT INDS, & ANNUNCIATOR LIGHTS. LANDING GEAR LEVER WOULD NOT MOVE UP. REMOVED AND REPLACED R1 RELAY, (BAT BUS AUTO RELAY) PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,519 hrs · 26,995 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 378, STRINGER 28L, CRACKED. REPAIRED SKIN PER EA.

Part: SIGN — DISLODGED (EMERGENCY EXIT) · airframe 31,298 hrs · 26,820 cycles

DURING SCHEDULED RON, MID CABIN EMERGENCY EXIT SIGN, FELL DOWN. REINSTALLED SIGN PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 31,155 hrs · 26,706 cycles

L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM.

Part: STRUCTURE — CRACKED (HINGE BOX) · airframe 31,072 hrs · 26,636 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR LOWER HINGE BOX CRACKED. REMOVED AND REPLACED HINGE BOX PER SRM.

Part: BRACKET — CRACKED (R2 DOOR) · airframe 29,213 hrs · 25,140 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE FWD MOUNT BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: SLIDE — LOOSE (FWD ENTRY DOOR) · airframe 27,990 hrs · 24,123 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 27,355 hrs · 23,610 cycles

DURING SCHEDULED C3 CHECK, FOUND LOOSE RIVETS AT FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER HOOK. REMOVED AND REPLACED RETAINER HOOK RIVETS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,269 hrs · 21,994 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT UPPER OTBD CORNER ON L-1 COCKPIT WINDOW. REPAIRED SKIN PER SRM.

Part: SLIDE — LOOSE (FWD ENTRY DOOR) · airframe 25,018 hrs · 21,793 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE VIEWING WINDOW LOOSE. SECURED VIEWING WINDOW PER MM.

Part: CABLE — MISROUTED (AFT ENTRY DOOR) · airframe 24,496 hrs · 21,352 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SLIDE — LOOSE (FWD SVC DOOR) · airframe 21,165 hrs · 18,616 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED EVAC SLIDE PER MM.

Part: SLIDE — LOOSE (FWD SVC DOOR) · airframe 21,165 hrs · 18,616 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: COVER — LOOSE (SERVICE DOOR) · airframe 20,673 hrs · 18,196 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND VIEW COVER LOOSE. SECURED VIEW COVER PER MM.

Part: SKIN — DELAMINATED (ELEVATOR) · airframe 20,002 hrs · 17,651 cycles

DURING SCHEDULED C3 CHECK, FOUND LT ELEVATOR DELAMINATED IN THREE AREAS. REPAIRED LT ELEVATOR PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 19,759 hrs · 17,445 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 19,149 hrs · 16,930 cycles

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

Part: LIGHT — CRACKED (CABIN) · airframe 18,983 hrs · 16,795 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 18,525 hrs · 16,421 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT INBD T/E AFT FLAP DELAMINATED. R&R T/E AFT FLAP PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 17,036 hrs · 15,166 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 847 FLOORBEAM UPPER SURFACE CRACKED ON RT OUTBOARD END. REPAIRED BEAM PER SRM.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 16,350 hrs · 14,585 cycles

FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: WIRE — LOOSE (CABIN)

SEVERAL EEPLS WIRES LOOSE AND LENSES MISSING. RESECURED WIRES AND REPLACED LENSES PER MM.

Part: ENGINE — FOD (NR 1)

ABORTED TO TAKEOFF DUE TO AS POWER WAS APPLIED DURING TAKEOFF ROLL, A LARGE BANG TYPE NOISE WAS HEARD, SUSPECTED FOD. THE AIRCRAFT WAS STOPPED AND RETURNED TO THE GATE. MAXIMUM SPEED REACHED ON TAKEOFF ROLL APPROX 15 MPH. ALL ENGINE INSTRUMENT WERE NORMAL WITH INDICATIONS. PERFORMED ENG INSP PER BOEING MM. NO DAMAGE NOTED. SUSPECT FOD INGESTION NR 1 (STYROFOAM) NR 1 ENG ON 10 CYCLE FLYBACK FOR BOROSCOPE INSP. BOROSCOPE INSPECTION PER BOEING MM. NO DEFECTS NOTED PER SAM 451. OK TO CONTINUE.(LP215646)

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED TERM CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE AT AFT ENTRY. RELAMPED PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED A1-CHECK, FOUND RT EMERGENCY EXIT LIGHTS INOP. REPLACED LIGHT HOUSING PER BOEING MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.