N390SW

Part: COVER — UNSECURE (CABIN) · airframe 70,744 hrs · 56,946 cycles

L1 DOOR LOWER EXIT LIGHT COVER FELL OFF. R&R LIGHT ASSEMBLY IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,887 hrs · 56,360 cycles

LEFT OVERWING LOWER EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: LINK — CRACKED (NLG WW) · airframe 69,814 hrs · 56,315 cycles

NOSE LANDING GEAR LOCK LINK ASSEMBLY CRACKED. R & R NOSE GEAR LOCK LINK ASSEMBLY IAW MM.

Part: LENS — MISSING (CABIN) · airframe 69,532 hrs · 56,121 cycles

FORWARD GALLEY EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS IAW SIP.

Part: SIGN — MISSING (CABIN) · airframe 69,532 hrs · 56,121 cycles

AFT GALLEY MISSING EMERGENCY EXIT SIGNS. INSTALLED SIGN IAW SIP.

Part: HOSE — LOOSE (CABIN) · airframe 69,137 hrs · 55,845 cycles

DIVERSION & DECLARED EMER. BURNT RUBBER SMELL IN AFT CABIN. RECONNECTED AFT AIR CONDITIONING DISTRIBUTION DUCT HOSE IAW MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 68,958 hrs · 55,706 cycles

LEFT WING NR 2 SLAT DELAMINATED ON OTBD UPPER WEDGE SECTION. R & R NR 2 SLAT IAW AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 68,878 hrs · 55,650 cycles

LEFT WING INBD TE AFT FLAP DELAMINATED. R & R AFT FLAP IAW MM.

Part: FASTENER — LOOSE (R1 DOOR) · airframe 68,214 hrs · 55,209 cycles

R1 DOOR EMER ESCAPE SLIDE CONTAINER MOUNTING BRACKET LOOSE. SECURED FASTENER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,110 hrs · 55,151 cycles

AFT CTR EMER EXIT LIGHT INOPERATIVE. REPAIRED LIGHT IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 68,110 hrs · 55,151 cycles

CEILING MOUNTED OVERWING EXIT SIGN INOPERATIVE. R & R BATTERY IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 68,110 hrs · 55,151 cycles

CEILING MOUNTED OVERWING EXIT SIGN INOPERATIVE. R & R CHARGER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,110 hrs · 55,151 cycles

AFT RT BULLNOSE LIGHT INOPERATIVE. REPAIRED LIGHT IAW AMM.

Part: FITTING — CRACKED (LT WING) · airframe 68,110 hrs · 55,151 cycles

LEFT FWD MLG FITTING CRACKED AT FASTENER HOLE, STATION RSS 224. REPAIRED FITTING IAW EA.

Part: STIFFENER — CRACKED (LT WING) · airframe 68,110 hrs · 55,151 cycles

LEFT WING NR 3 INBD FLAP, OTBD TRACK FAIRING INBD SIDE, HOCKEY STICK, STIFFENER CRACKED. R & R STIFFENER IAW SRM & DWG.

Part: SKIN — CRACKED (LT WING) · airframe 68,110 hrs · 55,151 cycles

LEFT WING UPPER SKIN CRACKED IN REAR SPAR AREA, AFT FASTENER ROW, IN FASTENER AT RSS 248. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 68,110 hrs · 55,151 cycles

LEFT WING UPPER SKIN REAR SPAR AREA CRACKED AFT FASTENER ROW, IN FASTENER AT RSS 253. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 68,110 hrs · 55,151 cycles

LEFT WING UPPER SKIN REAR SPAR CRACKED IN FASTENER AREA AT RSS 247. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 68,110 hrs · 55,151 cycles

LEFT WING UPPER SKIN CRACKED AT REAR SPAR AREA, AFT FASTENER ROW, IN FASTENER AT RSS 267. REPAIRED SKIN IAW EA.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 68,110 hrs · 55,151 cycles

RIGHT WING UPPER SKIN PANEL, CRACKED AT RSS 238, MOST AFT OPENED STRUCTURE ATTACH FASTENER HOLE. REPAIRED SKIN IAW EA.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 68,110 hrs · 55,151 cycles

RIGHT WING UPPER SKIN PANEL, CRACKED AT RSS 254, MOST AFT OPENED ATTACH STRUCTURE. REPAIRED SKIN IAW EA.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 68,110 hrs · 55,151 cycles

RIGHT WING UPPER SKIN PANEL CRACKED AT RSS 208, MOST AFT STRUCTURE ATTACH FASTENER HOLE. REPAIRED SKIN IAW EA.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 68,110 hrs · 55,151 cycles

RIGHT WING UPPER SKIN PANEL TE CRACKED AT RSS 221. REPAIRED SKIN IAW EA.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 68,110 hrs · 55,151 cycles

RIGHT WING UPPER SKIN PANEL CRACKED AT RSS 250, MOST AFT OPENED STRUCTURE ATTACH FASTENER HOLE. REPAIRED SKIN IAW EA.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 68,110 hrs · 55,151 cycles

RIGHT WING UPPER SKIN PANEL CRACKED AT RSS 191. REAR SPAR UPPER CHORD TO WING SKIN FWD FASTENER HOLE. REPAIRED SKIN IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,110 hrs · 55,151 cycles

L1 DOOR CUT OUT UPPER HINGE AREA, CRACKED AT BS 301, WL 259. REPAIRED STRINGER IAW EA.

Part: FITTING — CRACKED (RT WING) · airframe 68,110 hrs · 55,151 cycles

RIGHT WING CLIP CRACKED AT RSS 234. R & R CLIP IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,110 hrs · 55,151 cycles

SEAT TRACK CORRODED AT BS 696, RBL 45.5. R & R SEAT TRACK IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 68,110 hrs · 55,151 cycles

LEFT WING OTBD FORE FLAP DELAMINATED AT INBD SIDE TE CORNER. REPAIRED FOR FLAP IAW SRM.

Part: STRAP — CRACKED (LT WING) · airframe 68,110 hrs · 55,151 cycles

LEFT WING REAR SPAR, UPPER STRAP AT STATION 236 CRACKED. R & R STRAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,110 hrs · 55,151 cycles

L1 DOOR HINGE FASTENER HOLE CUT OUT CRACKED AT BS 304, WL 259. REPAIRED SKIN IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 68,110 hrs · 55,151 cycles

VERTICAL ATTACH ANGLE CRACKED AT BS 328, LBL 46. REPAIRED ANGLE IAW SRM & DWG.

Part: SPAR — CRACKED (LT WING) · airframe 68,110 hrs · 55,151 cycles

LEFT WING NR 5 HOLE ONLY IN REAR SPAR RSS 222, CRACKED AT WEB. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,110 hrs · 55,151 cycles

L1 DOOR HINGE CUT OUT CRACKED, AT BS 304, WL 262. REPAIRED CUT OUT IAW SRM.

Part: TAB — DELAMINATED (LT AILERON) · airframe 68,110 hrs · 55,151 cycles

LEFT WING AILERON TAB DELAMINATED AT INBD CORNER ON TE. REPAIRED TAB IAW WO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,223 hrs · 55,214 cycles

L1 DOOR HINGE CUT OUT CRACKED AT BS 304, WL 260. REPAIRED CUT OUT IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,110 hrs · 55,151 cycles

L1 DOOR HINGE CUT OUT CRACKED AT BS 303, WL 259. REPAIRED CUT OUT IAW SRM.

Part: SPAR — CRACKED (RT WING) · airframe 68,110 hrs · 55,151 cycles

RIGHT WING NR 5 HOLE ONLY IN REAR SPAR AT RSS 222, CRACKED IN CHORD. REPAIRED CHORD IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,110 hrs · 55,151 cycles

FLOORBEAM CORRODED AT BS 986.50, BL 0. REPAIRED FLOORBEAM IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,110 hrs · 55,151 cycles

FORWARD OF L1 DOOR UPPER HINGE CUT OUT INTERCOSTAL LT ANGLE CRACKED, BETWEEN BS 303 - 294.5, STRINGER 9L. R & R LT ANGLE IAW SRM & DWG.

Part: BEAM — CORRODED (FUSELAGE) · airframe 68,110 hrs · 55,151 cycles

FLOORBEAM STUB BEAM STRAP CORRODED AT BS 967, RBL 5. REPAIRED STUB BEAM IAW SRM.

Part: SPAR — CRACKED (LT WING) · airframe 68,110 hrs · 55,151 cycles

LEFT WING REAR SPAR RSS 222, CRACKED CHORD. REPAIRED CHORD IAW EA.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 68,110 hrs · 55,151 cycles

LEFT WING OTBD FIXED TE, UPPER SURFACE PANEL ATTACH ANGLE CRACKED. R & R ANGLE IAW DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,110 hrs · 55,151 cycles

RIGHT CREASE BEAM CORRODED AT STATION 291 - 328. REPAIRED BEAM IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,110 hrs · 55,151 cycles

RIGHT CREASE BEAM CORRODED AT STATION 986 - 948. REPAIRED BEAM IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,110 hrs · 55,151 cycles

FLOOR STRUCTURE CREASE BEAM WEB CORRODED AT BETWEEN BS 827 - 847, STRINGER 17R. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,110 hrs · 55,151 cycles

LEFT CREASE BEAM WEB CORRODED, BETWEEN BS 867 - 847, STRINGER 17L. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,110 hrs · 55,151 cycles

RIGHT CREASE BEAM CORRODED AT STATION 420 - 440. REPAIRED BEAM IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,110 hrs · 55,151 cycles

FLOOR STRUCTURE CREASE BEAM WEB CORRODED, BETWEEN BS 887 - 907, STRINGER 17R. R & R WEB IAW SRM & DWG.

Part: LENS — BROKEN (CABIN) · airframe 68,082 hrs · 55,135 cycles

FORWARD EMER EXIT LENS BROKEN. R & R LENS IAW AMM.

Part: FITTING — CORRODED (LT MLG) · airframe 68,041 hrs · 55,105 cycles

LEFT MLG FRAME, LOWER FITTING FWD & AFT LUG, CORRODED AT BS 685. REPAIRED FITTING IAW EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 67,847 hrs · 54,978 cycles

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

Part: ATTACH FITTING — CORRODED (FLAP TRACK) · airframe 67,847 hrs · 54,978 cycles

RIGHT WING NR 8 AFT FLAP TRACK ATTACH FITTING CORRODED IN BORE OF OTBD HOLE. R & R FITTING IAW SRM.

Part: ATTACH FITTING — CORRODED (FLAP TRACK) · airframe 67,847 hrs · 54,978 cycles

RIGHT WING NR 1 FLAP TRACK AFT ATTACH FITTING, OTBD MOUNT BOLT HOLE CORRODED. R & R FITTING IAW SRM & EA.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 67,847 hrs · 54,978 cycles

RIGHT WING NR 5 AFT FLAP TRACK CARRIAGE, CORRODED INSIDE BORE OF HOLE FOR AFT INBD ROLLER BOLT. REPAIRED CARRIAGE IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 67,847 hrs · 54,978 cycles

AFT LT WINDSCREEN FLASHLIGHT BATTERY INDICATOR INOPERATIVE. R & R BATTERY IAW AMM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 67,847 hrs · 54,978 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT AFT SPAR 36" FROM ACFT FUSELAGE. REPAIRED SKIN IAW EA.

Part: SLAT — DELAMINATED (RT WING) · airframe 67,847 hrs · 54,978 cycles

RIGHT WING NR 5 SLAT DELAMINATED AT AFT EDGE OTBD END. REPAIRED NR 5 SLAT IAW AMM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 67,847 hrs · 54,978 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT AFT SPARE 36" FROM ACFT. REPAIRED SKIN IAW EA.

Part: SIGN — UNSECURE (CABIN) · airframe 67,599 hrs · 54,804 cycles

LEFT OVERWING EXIT SIGN ABOVE DOOR FELL OFF. R & R SIGN IAW AMM.

Part: SLIDE — BROKEN (R2 DOOR) · airframe 67,599 hrs · 54,804 cycles

R2 DOOR EMER EVAC SLIDE AIR BAR BRACKET BROKEN. R & R SLIDE IAW EA & MT.

Part: ENGINE — FAULTY (NR 1) · airframe 67,463 hrs · 54,703 cycles

DIVERSION, ON INITIAL CLIMB AT APPROX 500 FT, NR 1 ENG EGT APPROX 965' WITH ASSOCIATED RED EGT LIGHT, MOMENTARY LIGHT ILLUMINATED APPROX 1 - 3 SECONDS. R & R NR 1 ENG QEC IAW MT.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 66,713 hrs · 54,145 cycles

FORWARD PHOTO LUMINESCENT STRIP LOOSE. R &R STRIP IAW SIP.

Part: BEAM — CORRODED (FUSELAGE) · airframe 65,760 hrs · 53,511 cycles

VERTICAL BEAM CORRODED AT BS 540, LBL 15.04. REPAIRED VERTICAL BEAM IAW EA & SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 65,760 hrs · 53,511 cycles

FORWARD CARGO SKIN LOWER CHORD CORRODED AT BS 540, LBL 13. REPAIRED CHORD IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 65,760 hrs · 53,511 cycles

RIGHT WING OTBD FORE FLAP DELAMINATED AT TE INBD OF NR 7 FLAP TRACK. REPAIRED FORE FLAP IAW MM.

Part: CASTING — CRACKED (LT SPOILER) · airframe 65,456 hrs · 53,306 cycles

LEFT WING INBD NR 4 GND SPOILER HINGE BOLT CASTING CRACKED. R & R NR 4 SPOILER IAW AMM.

Part: ROD END — CORRODED (LT ELEVATOR) · airframe 64,919 hrs · 52,922 cycles

LEFT ELEVATOR TAB INBD CONTROL ROD AFT ROD END CORRODED. R & R ROD END IAW AMM.

Part: HINGE — LOOSE (LT ELEVATOR TAB) · airframe 64,919 hrs · 52,922 cycles

LEFT ELEVATOR TAB NR 4 HINGE LOOSE. REPAIRED HINGE ASSEMBLY IAW EA.

Part: MOUNT BRACKET — CRACKED (R2 DOOR) · airframe 64,088 hrs · 52,310 cycles

R2 DOOR SLIDE FWD MOUNT BRACKET CRACKED. R & R BRACKET IAW MM.

Part: MOUNT BRACKET — CRACKED (R2 DOOR) · airframe 64,088 hrs · 52,310 cycles

R2 DOOR SLIDE AFT MOUNT BRACKET CRACKED. R & R BRACKET IAW MM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

CHANNEL CORRODED AT BS 847+13, RBL 3. REPAIRED CHANNEL IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

CHANNEL CORRODED AT BS 847+13, LBL 3. REPAIRED CHANNEL IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,016 hrs · 51,582 cycles

AFT EMERGENCY EXIT LIGHTS INOPERATIVE. R & R LIGHTS IAW MM.

Part: ANGLE — CRACKED (LT WING) · airframe 63,016 hrs · 51,582 cycles

LT WING FIXED TE ANGLE CRACKED AT WS 537.806. R & R ANGLE IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

SHEAR BEAM WEB CRACKED BETWEEN BS 711 TO BS 727, RT SIDE. R & R WEB IAW EA.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 63,016 hrs · 51,582 cycles

AFT CARGO COMPARTMENT DOOR FWD END OF CROSS BEAM WEB CRACKED. REPAIRED WEB IAW EA.

Part: FITTING — CRACKED (LT WING) · airframe 63,016 hrs · 51,582 cycles

LT WING TE NR 3 FAIRING INTERNAL AREA FITTING CRACKED. R & R FITTING IAW SRM & DRAWING.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

DOME CAP WEB CRACKED AT BS 1016, BL 0. REPAIRED WEB IAW SRM.

Part: FAIRING — DELAMINATED (LT WING) · airframe 63,016 hrs · 51,582 cycles

LT WING FAIRING ATTACHED TO CTR FAIRING DELAMINATED. REPAIRED FAIRING IAW EO & EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

R2 DOOR FWD LOWER CORNER STUD FRAME CUTOUT CRACKED. REPAIRED CUTOUT IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

SUPPORT ANGLE CRACKED AT BS 336, BETWEEN STRINGER 20L TO STRINGER 21L. R & R ANGLE IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

SUPPORT ANGLE CRACKED AT BS 351.2, LBL 13. R & R ANGLE IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

SUPPORT ANGLE CRACKED AT BS 297, RBL 15. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

ANGLE CRACKED AT BS 321, STRINGER 28L. R & R ANGLE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

TIE CLIP CRACKED AT BS 727D, STRINGER 20L. R & R TIE CLIP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

SUPPORT ANGLE CRACKED AT BS 328, BETWEEN STRINGER 20L TO STRINGER 21L. R & R ANGLE IAW SRM & DRAWING.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

STRINGER CORRODED BETWEEN BS 967 TO BS 987, STRINGER 25L. REPAIRED STRINGER IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

TIE CLIP CRACKED AT BS 727A, STRINGER 20L. R & R TIE CLIP IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

TIE CLIP CRACKED AT BS 727B, STRINGER 21L. R & R TIE CLIP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

CLIP ANGLE CRACKED AT BS 947.5, STRINGER 25L. R & R ANGLE IAW SRM & DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

SHEAR TIE CORRODED AT BS 947.5 & BETWEEN STRINGER 24L TO STRINGER 26L. R & R SHEAR TIE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

CLIP ANGLE CRACKED AT BS 947.5, STRINGER 22L. R & R ANGLE IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

SUPPORT ANGLE CRACKED AT BS 320, BETWEEN STRINGER 20L TO STRINGER 21L. R & R ANGLE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

TIE CLIP CRACKED AT BS 727A, STRINGER 19L. R & R TIE CLIP IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

ANGLE CRACKED AT BS 947.5, STRINGER 24R. R & R ANGLE IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

FRAME CORRODED AT BS 328, STRINGER 27R. R & R FRAME IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

TIE CLIP CRACKED AT BS 294.5, STRINGER 23L. R & R TIE CLIP IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

VERTICAL ANGLE CRACKED AT BS 328, STRINGER 27R. R & R ANGLE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

TIE CLIP CRACKED AT BS 727E, STRINGER 20L. R & R TIE CLIP IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360, STRINGER 15L. R & R CHANNEL IAW SRM & DRAWING.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

DOME CAP WEB CRACKED AT BS 1016, STRINGER 7L. REPAIRED WEB IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

CLIP CRACKED AT BS 380, BETWEEN STRINGER 25L TO STRINGER 26L. R & R CLIP IAW SRM & DRAWING.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

Z STIFFENER CRACKED AT BS 1016, STRINGER 5R. R & R Z STIFFENER IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

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

Part: RIB — CRACKED (LT WING) · airframe 63,016 hrs · 51,582 cycles

LT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STATION 2 TO STATION 3. REPAIRED CHORD IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

DOME CAP WEB CRACKED AT BS 1016, STRINGER 15R. REPAIRED WEB IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

CLIP CRACKED AT BS 380, BETWEEN STRINGER 25R TO STRINGER 26R. R & R CLIP IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

FRAME WEB CRACKED AT BS 328, BETWEEN STRINGER 20R TO STRINGER 21R. R & R FRAME IAW SRM & DRAWING.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

ANGLE CORRODED AT BS 807, BETWEEN STRINGER 25R TO STRINGER 26R. R & R ANGLE IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

FWD GALLEY AREA UNDER FLOOR STRUCTURE STRAP CRACKED AT BS 328, RBL 45. R & R STRAP IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

WEB CRACKED AT BS 328, RBL 31.6. R & R WEB IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

FRAME CORRODED AT BS 807, BETWEEN STRINGER 27L & STRINGER 27R. REPAIRED FRAME IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

CHANNEL CORRODED AT BS 767+5, LBL 12.50. REPAIRED CHANNEL IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360, STRINGER 15L. R & R CHANNEL IAW SRM & DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

SHEAR TIE CORRODED AT BS 867, BETWEEN STRINGER 27L TO STRINGER 27R. REPAIRED SHEAR TIE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

L1 DOOR RETAINER ANGLE CRACKED AT BS 348, BETWEEN STRINGER 8L TO STRINGER 9L. R & R ANGLE IAW SRM & DRAWING.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

AFT CARGO COMPARTMENT T SPLICE CRACKED AT BS 727D+6.5, BETWEEN STRINGER 25R TO STRINGER 25L. R & R T SPLICE IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

FRAME CORRODED AT BS 947.5, & BETWEEN STRINGER 22R TO STRINGER 23R. R & R FRAME IAW SRM & DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

CLIP CRACKED AT BS 360, STRINGER 8L. R & R CLIP IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

FWD GALLEY AREA UNDER FLOOR STRUCTURE STRAP CRACKED AT BS 312, BL 0. R & R STRAP IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

SHEAR TIE CORRODED AT BS 500, BETWEEN STRINGER 26R TO STRINGER 27R. R & R SHEAR TIE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

ANGLE CRACKED BETWEEN BS 294.5 TO BS 303.9, STRINGER 16L. R & R ANGLE IAW SRM & DRAWING.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

CHANNEL CORRODED AT BS 767+5, LBL 8.10. REPAIRED CHANNEL IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

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

Part: BRACKET — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

L1 DOOR CUTOUT BRACKET CRACKED AT BS 303.8+5, STRINGER 15L. R & R BRACKET IAW SRM & DRAWING.

Part: PLATE — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

FWD ENTRY DOOR LOWER HINGE CUT OUT PLATE CRACKED AT BS 303, BETWEEN STRINGER 13L TO STRINGER 14L. R & R PLATE IAW SRM & DRAWING.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

SUPPORT CLIP CRACKED AT BS 947.5, STRINGER 25R. R & R CLIP IAW SRM & DRAWING.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

CHANNEL CORRODED AT BS 767+5, RBL 3. REPAIRED CHANNEL IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

CHANNEL CORRODED AT BS 767+5, LBL 3. REPAIRED CHANNEL IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

UNDER FLOOR STRUCTURE VERTICAL ANGLE CRACKED AT BS 328, RBL 31.6. R & R ANGLE IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

FRAME CRACKED AT BS 500C, BETWEEN STRINGER 20L TO STRINGER 21L. REPAIRED FRAME IAW SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 63,016 hrs · 51,582 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75+9, RBL 24.5+17. REPAIRED WEB IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,016 hrs · 51,582 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75+9, LBL 24.5+14. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

FUSELAGE SKIN CRACKED AT BS 967-6.5, STRINGER 17R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

SKIN CRACKED AT BS 794.5+4, STRINGER 24R. REPAIRED SKIN IAW EA.

Part: SUPPORT ANGLE — CRACKED (LT PYLON) · airframe 63,016 hrs · 51,582 cycles

LT PYLON ACCESS PANEL 5758L SUPPORT ANGLE CRACKED AT INTERNAL CAVITY. R & R ANGLE IAW SRM & DRAWING.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 63,016 hrs · 51,582 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75+9, RBL 24.5+14. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 712, RBL 24.8. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

FUSELAGE SKIN CRACKED AT BS 328, STRINGER 16R. REPAIRED SKIN IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,016 hrs · 51,582 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 663.75+1, LBL 24.5+6. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

L2 DOOR SKIN CUTOUT FWD LOWER CORNER CRACKED AT BS 947.5+14.5, STRINGER 17L. REPAIRED SKIN IAW EA & EO.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 63,016 hrs · 51,582 cycles

MAIN WW PRESS DECK CRACKED AT BS 663.75+1, RBL 24.5+14. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 709, RBL 24.8. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

FUSELAGE SKIN CRACKED AT BS 328+4.5, STRINGER 17R. REPAIRED SKIN IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 713, RBL 24.8. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 714, RBL 24.8. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

SKIN CRACKED AT BS 967-5.5, STRINGER 17R. REPAIRED SKIN IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 709, RBL 24.8. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 710, RBL 24.8. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

FUSELAGE SKIN CRACKED AT BS 947.5+12.5, STRINGER 17R. REPAIRED SKIN IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT PYLON) · airframe 63,016 hrs · 51,582 cycles

LT PYLON ACCESS PANEL 5757L SUPPORT ANGLE CRACKED AT INTERNAL CAVITY. R & R ANGLE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

FUSELAGE SKIN CRACKED AT BS 328, STRINGER 16R. REPAIRED SKIN IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 713, RBL 24.8. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

L2 DOOR SKIN CUTOUT FWD LOWER CORNER CRACKED AT BS 947.5+13.5, STRINGER 17L. REPAIRED SKIN IAW EA & EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

FRAME CHORD CRACKED AT BS 727, STRINGER 18A LT. R & R CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

L2 DOOR SKIN CUTOUT FWD LOWER CORNER CRACKED AT BS 960, STRINGER 17L. REPAIRED SKIN IAW EA & EO.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 705+3.5, LBL 24.8. REPAIRED WEB IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

FLOOR BEAM CRACKED BETWEEN BS 666 TO BS 670, LBL 24.5. REPAIRED BEAM IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

FRAME CHORD CRACKED AT BS 727, STRINGER 18A. R & R CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED BETWEEN BS 707 TO BS 708, RBL 24.8. REPAIRED WEB IAW EA.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 63,016 hrs · 51,582 cycles

LT MAIN WW ANGLE CRACKED AT BS 727, BETWEEN STRINGER 26L TO STRINGER 27L. R & R ANGLE IAW SRM & DRAWING.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

FLOOR BEAM CRACKED AT BS 669, LBL 24.5. REPAIRED BEAM IAW EA.

Part: PLATE — CRACKED (RT WING) · airframe 63,016 hrs · 51,582 cycles

RT WING ACCESS PANEL 3678R PLATE CRACKED AT BS 727, STRINGER 22R. R & R PLATE IAW SRM & DRAWING.

Part: SKIN — CRACKED (RT WING) · airframe 63,016 hrs · 51,582 cycles

RT WING LE SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,016 hrs · 51,582 cycles

FRAME CHORD CRACKED AT BS 727, STRINGER 18A RT. R & R CHORD IAW EA.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 62,596 hrs · 51,305 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: FLAP TRACK — CORRODED (RT WING) · airframe 62,226 hrs · 51,033 cycles

RT WING NR 7 FLAP TRACK CORROSION FOUND ON THE UPPER & LOWER FLANGES OF THE FLAP TRACKS. R & R NR 7 FLAP TRACK IAW MM.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 62,226 hrs · 51,033 cycles

LT WING NR 2 FLAP TRACK CORROSION FOUND ON THE UPPER & LOWER TRACK FLANGES. R & R NR 2 FLAP TRACK IAW MM.

Part: LENS — MISSING (CABIN) · airframe 59,836 hrs · 49,295 cycles

EMERGENCY EGRESS LIGHTING IN BULLNOSE ABOVE 19 DEF MISSING LENS. INSTALLED LENS PER AMM

Part: LENS — LOOSE (CABIN) · airframe 59,500 hrs · 49,046 cycles

CTR FORWARD OVERHEAD EXIT LIGHT LENS IS UNSECURE. INSTALLED/SECURED LENS IAW MM.

Part: PUMP — LEAKING (NR 1 ENGINE) · airframe 59,416 hrs · 48,985 cycles

AIR TURNBACK. 'A' HYDRAULIC SYSTEM LIGHT ILLUMINATED ON TAKEOFF. A SYSTEM HYDRAULIC QUANTITY DROPPED TO 1/3 AIR RETURN TO GSO, TURNED 'A' SYSTEM HYDRAULIC PUMP OFF TO PREVENT FURTHER LOSS OF FLUID. REMOVED AND REPLACED NR 1 ENGINE ENGINE DRIVEN PUMP IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 59,416 hrs · 48,984 cycles

FORWARD LEFT LAV EEPLS LENS MISSING. INSTALLED LENS IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 59,416 hrs · 48,984 cycles

RIGHT EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED LENS IAW AMM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED SPLICE IAW BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

STRINGER CLIP CRACKED AT BS 500A, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

L2 DOOR AFT UPPER CORNER OF CUTOUT CRACKED IN BEAR STRAP. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

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

Part: HYDRAULIC LINE — FAULTY (NR 1 ENGINE) · airframe 59,416 hrs · 48,984 cycles

AIR TURNBACK -- ON CLIMBOUT, NOTICED SMALL FLICKER ON ENGINE 1 LOW PRESSURE. AT LEVEL OFF GOT LOW PRESSURE HYD A ENG 1 LIGHT. REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP PRESSURE LINE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,179 hrs · 48,802 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 461 TO BS 462, STR 15R. REPAIRED SKIN REPAIRED IAW EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 59,150 hrs · 48,780 cycles

RIGHT EEPLS INOP BETWEEN ROW 8 TO ROW 15. REMOVED AND REPLACED BATTERY IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,150 hrs · 48,780 cycles

SKIN CRACKED AT BS 827, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,150 hrs · 48,780 cycles

SKIN CRACKED AT BS 767, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,150 hrs · 48,780 cycles

SKIN CRACKED AT BS 815, STR 8L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,150 hrs · 48,780 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 808 TO BS 817, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,150 hrs · 48,780 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 828+4 TO BS 832, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 59,065 hrs · 48,720 cycles

LEFT HORIZONTAL STABILIZER CRACKED ON LOWER SKIN. REPAIRED SKIN PER EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 59,065 hrs · 48,720 cycles

RIGHT WING O/B AFT FLAP DELAMINATED AT I/B SIDE. REMOVED AND REPLACED AFT FLAP IAW M/M.

Part: COVER — MISSING (CABIN) · airframe 58,580 hrs · 48,335 cycles

FWD GALLEY WALL EMERGENCY LIGHT COVER MISSING. REMOVED AND REPLACED COVER PER M/M.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 58,495 hrs · 48,268 cycles

L1 DOOR EXTERIOR EMERGENCY EGRESS LIGHT INOP. REMOVED AND REPLACED LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,495 hrs · 48,268 cycles

LEFT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP IAW AMM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 58,495 hrs · 48,268 cycles

SHEAR TIE CRACKED AT BS 400, STR 15L. REPAIRED SHEAR TIE IAW DWG & EA.

Part: BEAM — CORRODED (FUSELAGE) · airframe 58,495 hrs · 48,268 cycles

LONGITUDINAL BEAM CORRODED BETWEEN BS 807 TO BS 847, RBL 16. REMOVED AND REPLACED BEAM IAW SRM AND DWG.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 57,985 hrs · 47,864 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTENT DEPLOYED. REMOVED AND REPLACED SLIDE PER MT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,586 hrs · 47,583 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME IAW SRM.

Part: LENS — MISSING (CABIN) · airframe 56,099 hrs · 46,457 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,060 hrs · 46,425 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 500C+15, STR 1L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,416 hrs · 48,984 cycles

SKIN CRACKED AT BS 500C+15, STR 1L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,664 hrs · 46,125 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500B+6, STR 10L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 55,456 hrs · 45,962 cycles

DURING SCHEDULED 2HC2 CHECK FOUND, FWD CARGO DOOR, EXTERIOR SKIN IS CRACKED AT AFT FASTENER HOLE TO EDGE OF SKIN. REMOVED AND REPLACED DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,775 hrs · 45,464 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 790, STR 4R. REPAIRED SKIN PER EA.

Part: LIGHT — BROKEN (CABIN) · airframe 54,605 hrs · 45,339 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 53,656 hrs · 44,655 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 663, LBL 24.8. REPAIRED WEB PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 767, RBL 21. REPAIRED FRAME PER ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727E, RBL 21. REPAIRED FRAME PER ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, RBL 21. REPAIRED FRAME PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, BETWEEN BBL 0 TO RBL 45. REPAIRED BEAM PER ER.

Part: BRACKET — CRACKED (R2 DOOR) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD MOUNTING BRACKET CRACKED. REPAIRED BRACKET PER ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULE 16Y CHECK, FOUND FRAME CORRODED AT BS 993, RBL 47. REPAIRED FRAME PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULE 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 492, STR 27R. REPAIRED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

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

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 400, STR 8R. REPAIRED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULE 16Y CHECK, FOUND SKIN CRACKED AT BS 742D, WL 150. REPAIRED SKIN PER ER.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULE 16Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 887, STR 4L. REPAIRED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727D, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: SUPPORT — CORRODED (EVAC SLIDE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR SUPPORT CORRODED AT BS 312, LBL 54. REMOVED AND REPLACED SUPPORT PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 616, STR 17R. REPAIRED FRAME PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 951, STR 11L. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 270 TO BS 275, RBL 40. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CHORD CRACKED AT BS 348, LBL 50. REPAIRED CHORD PER SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND COMPRESSION BEAM UPPER ATTACH FITTING CRACKED AT BS 727, LBL 45. REMOVED AND REPLACED FITTING PER SRM AND BAC DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CRACKED AT BS 951, STR 11L. REPAIRED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 797, LBL 70. REPAIRED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 406, RBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 19R TO STR 22R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 53,120 hrs · 44,230 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND STUB BEAM ATTACH ANGLE CRACKED AT BS 634, LBL 45.5. REPAIRED BEAM PER SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 53,120 hrs · 44,230 cycles

DURING SCHEDULED 16Y CHECK, FOUND STUB BEAM ATTACH ANGLE CRACKED AT BS 634, RBL 45.5. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,547 hrs · 50,502 cycles

STRINGER CLIP CRACKED AT BS 887, STRINGER 4L. R&R CLIP IAW SRM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 52,219 hrs · 43,552 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: CABLE — LOOSE (EVAC SLIDE) · airframe 52,019 hrs · 43,396 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE LOOSE. SECURED CABLE PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 52,019 hrs · 43,396 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING I/B AFT FLAP LOWER SKIN DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 51,705 hrs · 43,162 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,710 hrs · 40,966 cycles

DURING SCHEDULED 14Y CHECK, FOUND RADIO ALTIMETER CUTOUT SKIN CRACKED AT BS 407, RBL 3. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,710 hrs · 40,966 cycles

DURING SCHEDULED 14Y CHECK, FOUND RADIO ALTIMETER CUTOUT BELLY SKIN CRACKED AT BS 747, RBL 3. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,710 hrs · 40,966 cycles

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

Part: FITTING — WORN (GIRT BAR) · airframe 48,710 hrs · 40,966 cycles

DURING SCHEDULED 14Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING WORN. REMOVED AND REPLACED FITTING PER MM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 48,710 hrs · 40,966 cycles

DURING SCHEDULED 14Y CHECK, R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: MOUNT FITTING — CORRODED (GIRT BAR) · airframe 48,710 hrs · 40,966 cycles

DURING SCHEDULED 14Y CHECK, FOUND L2 DOOR EMERGENCY EVAC GIRT BAR FITTING MOUNTING PLATES CORRODED. REMOVED AND REPLACED FITTINGS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,710 hrs · 40,966 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BETWEEN BS 302 TO BS 304. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,710 hrs · 40,966 cycles

DURING SCHEDULED 14Y CHECK, FOUND BELLY SKIN CRACKED AT BS 407, RBL 3. REPAIRED SKIN PER EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 48,710 hrs · 40,966 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 28L. REMOVED AND REPLACED SPLICE PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 48,710 hrs · 40,966 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING T/E AT AFT INBOARD FLAP DELAMINATED. REPAIRED FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,710 hrs · 40,966 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,710 hrs · 40,966 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,710 hrs · 40,966 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,710 hrs · 40,966 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,710 hrs · 40,966 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,710 hrs · 40,966 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,710 hrs · 40,966 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,710 hrs · 40,966 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,710 hrs · 40,966 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,710 hrs · 40,966 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,710 hrs · 40,966 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,710 hrs · 40,966 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,710 hrs · 40,966 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,710 hrs · 40,966 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 787, STR. 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,710 hrs · 40,966 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 48,638 hrs · 40,916 cycles

R1 EMERGENCY EVACUATION DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,578 hrs · 40,172 cycles

L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 47,399 hrs · 40,041 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,399 hrs · 40,041 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 46,766 hrs · 39,575 cycles

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

Part: SHEAR TIE — BROKEN (RT WING) · airframe 43,671 hrs · 37,236 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING SHEAR TIE BROKEN AT RIB 505, FWD SPAR. REMOVED AND REPLACED SHEAR TIE PER BAC DRAWING.

Part: FAN — FAULTY (E&E BAY) · airframe 42,313 hrs · 36,195 cycles

F/A REPORT ELECTRICAL SMELL IN MID CABIN. TURNED OFF GASPER FAN SMELL DISSIPATED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 42,273 hrs · 36,165 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. FOUND BROKEN WIRE, REPAIRED WIRE W1150-062-20 PER WDM.

Part: FITTING — CORRODED (LT WING) · airframe 42,266 hrs · 36,156 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT MLG STABILIZER FITTING CORRODED. REMOVED AND REPLACED MLG STABILIZER FITTING PER MM.

Part: ATTACH FITTING — LOOSE (NR 6 SPOILER) · airframe 42,263 hrs · 36,154 cycles

DURING SCHEDULED 122Y CHECK, FOUND RIGHT WING NR 6 GROUND SPOILER ACTUATOR ATTACH POINT LOOSE. REMOVED AND REPLACED SPOILER PER MM.

Part: HINGE FITTING — LOOSE (NR 4 SPOILER) · airframe 42,263 hrs · 36,154 cycles

DURING SCHEDULED 122Y CHECK, FOUND LEFT WING NR 4 GROUND SPOILER CENTER HINGE ATTACH POINT LOOSE. REMOVED AND REPLACED SPOILER PER MM.

Part: ARM — CORRODED (RT MLG) · airframe 42,263 hrs · 36,154 cycles

DURING SCHEDULED 12Y CHECK, FOUND RIGHT MLG WALKING BEAM ACTUATOR ARM CORRODED. REMOVED AND REPLACED ACTUATOR ARM PER MM.

Part: SKIN — DELAMINATED (ELEVATOR TAB) · airframe 42,263 hrs · 36,154 cycles

DURING SCHEDULED 12Y CHECK, FOUND LEFT ELEVATOR TAB DELAMINATED LOWER END. REPAIRED TAB PER SRM.

Part: BEARING — WORN (ELEVATOR TAB) · airframe 42,263 hrs · 36,154 cycles

DURING SCHEDULED 12Y CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB BEARING PER MM.

Part: BEARING — WORN (ELEVATOR TAB) · airframe 42,263 hrs · 36,154 cycles

DURING SCHEDULED 12Y CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB BEARING PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 42,263 hrs · 36,154 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD CABIN EEPPLS PHOTOLUMINESCENT STRIP WORN. REMOVED AND REPLACED STRIP PER MM.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 42,263 hrs · 36,154 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR UPPER HINGE FITTING CRACKED LOWER SIDE. REMOVED AND REPLACED UPPER HINGE FITTING PER SWA EA.

Part: MOUNT — LOOSE (CABIN) · airframe 42,263 hrs · 36,154 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT FLOOR MOUNT LOOSE. SECURED FLOOR MOUNT PER MM.

Part: MOUNT — LOOSE (CABIN) · airframe 42,263 hrs · 36,154 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD FLOOR MOUNT LOOSE. SECURED FLOOR MOUNT PER MM.

Part: SKIN — CRACKED (BS 378) · airframe 42,204 hrs · 36,103 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 378.5, LBL 2.8 EQUIPMENT COOLING EXHAUST CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 520) · airframe 42,204 hrs · 36,103 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, LBL 3, AC GROUND RECEPTACLE FWD RADIUS. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,204 hrs · 36,103 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR CUTOUT, UPPER AFT CORNER. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 41,168 hrs · 35,277 cycles

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

Part: CABLE — MISROUTED (R2 DOOR SLIDE) · airframe 39,262 hrs · 33,729 cycles

DURING SCHEDULED A2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 38,857 hrs · 33,432 cycles

R2 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 38,222 hrs · 32,927 cycles

BULLNOSE EMERGENCY LIGHT COVER MISSING AT ROW 8. INSTALLED COVER PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 37,371 hrs · 32,251 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 35,802 hrs · 31,027 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING DOOR EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED SIGN PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,570 hrs · 30,856 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 COCKPIT WINDOW POST UPPER CORNER, CRACKED. REPAIRED WINDOW POST PER SRM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 35,000 hrs · 30,393 cycles

FWD SERVICE DOOR LOWER EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SLIDE — BROKEN (L2 DOOR) · airframe 34,965 hrs · 30,368 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE BROKEN. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 34,520 hrs · 30,017 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPAIRED GROUND WIRE TO AIRFRAME AND RELAMPED PER MM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB FITTING LUGS CORRODED. REPAIRED VERTICAL STAB PER ER.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL FIN BODY FITTING LUGS CORRODED. REPAIRED VERTICAL FIN PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 947.5, LBL 53, CRACKED. REPAIRED FLOORBEAM PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 1016, RBL 14 TO RBL 25, CORRODED. REMOVED AND REPLACED FLOORBEAM PER ER.

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D-CHECK, FOUND RT & LT HORIZONTAL STAB, CENTER SECTION FWD & AFT SPAR LUGS, CORRODED. REPAIRED HORIZONTAL STAB CENTER SECTION LUGS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 727D, STRINGER 8L & STRINGER 8R, CRACKED. REPAIRED FRAME SECTIONS PER SRM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D-CHECK, FOUND LT WING NR 3 L/E SLAT WEDGE OUTBOARD UPPER END, DELAMINATED. REPAIRED LT WING NR 3 L/E SLAT PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 685, STRINGER 11L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D-CHECK, FOUND R1 DOOR CUTOUT STUB FRAME AT BS 296, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 500A, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT RIGHT BS 460 TO RIGHT BS 480, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 303, STRINGER 16L, CRACKED. REPAIRED FRAME SECTION PER SB.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,293 hrs · 29,545 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS AT BS 706, STRINGER 11R AND STRINGER 11L CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,923 hrs · 28,545 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES AT BS 188, STRINGER 17R, BS 188, STRINGER 17L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 400, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FLOORBEAM — CRACKED (188) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAMS AT BS 188 TO BS 198, STRINGER 17R TO STRINGER 17L CRACKED. REMOVED AND REPLACED FLOORBEAM SECTION PER BAC DRAWING AND SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR CUTOUT FRAME LOWER CLOSE OUT WEB AFT EDGE CRACKED. REMOVED AND REPLACED DOOR CUTOUT FRAME WEB PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR CUTOUT FRAME UPPER CLOSE OUT WEB LOWER AREA, CORRODED. REMOVED AND REPLACED DOOR CUTOUT FRAME WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,923 hrs · 28,545 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 294.5, RBL 45, CORRODED. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 440, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 616, LBL 64 WL 200, CRACKED. REMOVED AND REPLACED FRAME CHORD PER SB.

Part: FRAME — CRACKED (BS 907) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 907 STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,923 hrs · 29,545 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — DELAMINATED (RT WING FOREFLAP) · airframe 32,708 hrs · 28,569 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD T/E FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED INBOARD FOREFLAP PER MM.

Part: SKIN — DELAMINATED (LT WING LE FLAP) · airframe 30,290 hrs · 26,645 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT AFT OUTBD T/E FLAP DELAMINATED. REMOVED AND REPLACED OUTBD T/E FLAP PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 29,533 hrs · 26,020 cycles

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

Part: BATTERY — WEAK (CABIN) · airframe 29,468 hrs · 25,957 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT EMERGENCY FLASHLIGHT BATTERY WEAK. REMOVED AND REPLACEDFLASHLIGHT BATTERY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,072 hrs · 25,649 cycles

DURING SCHEDULED C1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 8 DEF. RELAMPED PER MM.

Part: SLIDE — DEPLOYED (FWD ENTRY DOOR) · airframe 27,448 hrs · 24,324 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE DEPLOYED BY FLIGHT ATTENDANT. REMOVED AND REPLACED SLIDE PER MM.

Part: MEC — FAILED (NR 2 ENGINE) · airframe 27,071 hrs · 24,009 cycles

INFLIGHT SHUT DOWN, DECLARED EMERGENCY, DIVERSION, DURING CRUISE NR 2 ENGINE FAILED. REMOVED AND REPLACED NR 2 ENGINE MEC AND FUEL PUMP PER MM.

Part: DOOR FRAME — CRACKED (SERVICE DOOR) · airframe 26,265 hrs · 23,355 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR FRAME CRACKED AT AFT LOWER STOP CUTOUT. REMOVED AND REPLACED DOOR PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 25,540 hrs · 22,763 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAMS CRACKED (3 EA) AT BS 747, RBL 14, BS 787, RBL 14 AND BS 945, RBL 3. REPAIRED FLOORBEAMS PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,540 hrs · 22,763 cycles

DURING SCHEDULED 1/4D CHECK, FOUND WEB CRACKED 1.0 INCH AT BS 178, WL 201 AND RBL 5.0. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,540 hrs · 22,763 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT BULKHEAD WEB CRACKED AT BS 178. REMOVED AND REPLACED WEB PER SRM AND SWA ACO.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 25,540 hrs · 22,763 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CORRODED AT BS 787, STR 27R. REPAIRED STR PER SWA RA.

Part: WEB — CRACKED (FUSELAGE) · airframe 25,540 hrs · 96 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 184, WL 233 AND LBL 17.1. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,540 hrs · 22,763 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT SIDE CHORD CRACKED AT BS 178, WL 207 AND RBL 28. REMOVED AND REPLACED CHORD PER SWA ACO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 25,540 hrs · 22,763 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 867, RBL 14. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: ACTUATOR — FAILED (L/E FLAP) · airframe 24,231 hrs · 21,676 cycles

AIR TURNBACK, AFTER TAKEOFF THE RT INBOARD L/E FLAP WOULD NOT RETRACT. REMOVED AND REPLACED NR 3 KRUEGER FLAP ACTUATOR PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 24,073 hrs · 21,544 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND 2 EA CRACKS AT BULKHEAD WEB, BS 178, LBL 5.5, WL 202-201 & WL 199.5-199.0. REPAIRED WEB PER SRM.

Part: COVER — CRACKED (CABIN FLOOR) · airframe 23,724 hrs · 21,240 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED BETWEEN ROWS 5 TO 24. R&R EEPLS COVERS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 23,176 hrs · 20,792 cycles

EEPLS TRACK COVER LOOSE AT MID CABIN. R&R TRACK COVER PER MM.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 23,060 hrs · 20,699 cycles

DIVERTED, DECLARED EMERGENCY, AT FL 370, PRESSURIZATION AURAL WARNING SOUNDED. PRESS VALVE CLOSED, EMERGENCY DESCENT KEPT CABIN ALT BELOW 11,500FT. R&R PRESS CONTROLLER PER MM, OPS CHECK GOOD.

Part: COVER — BROKEN (CABIN) · airframe 21,697 hrs · 19,570 cycles

DURING SCHEDULED C1 CHECK, FOUND SEVERAL EEPLS TRACK COVERS LOOSE & BROKEN. SECURED/R&R BROKEN COVERS PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 21,670 hrs · 19,549 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER WHEN DOOR OPENED UPON ARRIVAL. RE-INSTALLED SLIDE ASSY PER MM.

Part: LAMP — INOPERATIVE (CABIN) · airframe 21,364 hrs · 19,301 cycles

DURING SCHEDULED A1 CHECK, FOUND RT OVERWING EXIT SIGN LIGHTS INOP. RELAMPED LIGHT PER MM.

Part: ENGINE — BIRD STRIKE (NR 2) · airframe 19,456 hrs · 17,743 cycles

AIR TURNBACK - NR 2 ENGINE SUFFERED BIRD STRIKE DURING CLIMB. COMPLIED WITH BIRD STRIKE INSPECTION AND BORESCOPE INSP NO DEFECT NOTED PER MM.

Part: CHAIN — BROKEN (SLIDE)

FWD ENTRY DOOR EVACUATION SLIDE LATCH CHAIN BROKEN. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: RIB — CRACKED (RT WING)

DURING SCHEDULED 1/2D CHECK, FOUND .250 INCH LONG CRACK ON RT WING RIB LOWER CHORD, WBL 135.5. REPAIRED RIB PER SWA RA NR 1-357-0730.

Part: CLIP — CRACKED (BS 663)

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED, BS 663, STRINGER 10L. REMOVED AND REPLACED STRINGER CLIP PER MM.

Part: LIGHT — INOP (EMER EXIT)

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY FLOOR RED LIGHTS INOP AT OVERWING EXIT. INSTALLED NEW SOCKET PER MM.

Part: CONNECTOR — DIRTY (CABIN)

DURING SERVICE CHECK CHECK, FOUND FLOOR TRACK LIGHTING OUT ON MID CABIN. CLEANED AND RESEATED SOCKET CONNECTORS PER MM.

Part: SKIN — DENTED (LT ENGINE)

DURING SCHEDULED C3 CHECK, FOUND INLET ACOUSTIC SKIN DENTED AT 5:00 DENT MEASURES .75 WIDE, 2 LONG AND 0:060 DEEP. REPAIRED PER BOEING SRM.

Part: MECHANISM — OUT OF ADJUST (NLG/LT MLG DOOR)

AFTER TAKEOFF, CREW REPORTED A VERY PRONOUNCED SIDE TO SIDE VIBRATION, YAW DAMPER WAS THEN TURNED OFF, NO HELP. DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING. REPLACED RUDDER PCU AND YAW DAMPER COUPLING AS A PRECAUTION PER BOEING M/M. AFTER FURTHER TROUBLESHOOTING AND TEST FLIGHTS, DURING GROUND GEAR RETRACTION TEST, FOUND NOSE GEAR AND LEFT MAIN GEAR DOORS OUT OF ADJUSTMENT.

Part: ENGINE — BIRDSTRIKE (NR 2)

EXPERIENCED BIRSTRIKE TO NR 2 ENGINE DURING CLIMB-OUT, AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND 3 FAN BLADES DAMGED, BUT NO CORE ENTRY. REPLACED BLADES AND COMPLIED WITH ENGINE RUN OK PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT AT ROW 18 INOP. RELAMPED PER BOEING M/M.

Part: WIRE — DISCONNECTED (CABIN)

DURING SCHEDULED RON, FOUND EMERGENCY LIGHTING INOPERATIVE AT FORWARD EMERGENCY EXIT. REPAIRED WIRING PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED RON, FOUND AFT EMERGENCY FLASHLIGHT WEAK AT AFT CABIN. REPLACED BATTERY PER BOEING M/M.