N645SW

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 62,117 hrs · 48,639 cycles

RIGHT WING NR 6 L/E SLAT DELAMINATED AT AUX TRACK CUTOUT. REPAIRED THE SLAT IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,649 hrs · 47,620 cycles

SHEAR TIE CORRODED AT BS 727E, BETWEEN LBL 7 TO LBL 13. R & R SHEAR TIE IAW SRM.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 60,649 hrs · 47,620 cycles

RIGHT VERTICAL STABILIZER PANEL 9508 LOWER RETENTION ANGLE CRACKED. R & R ANGLE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,649 hrs · 47,620 cycles

FORWARD CARGO COMPARTMENT FRAME SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 26R TO STR 27R. R & R SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,649 hrs · 47,620 cycles

FORWARD CARGO COMPARTMENT FRAME SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,649 hrs · 47,620 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,649 hrs · 47,620 cycles

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

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 60,649 hrs · 47,620 cycles

STRINGER CLIP CORRODED AT BS 767, STR 27L. R & R CLIP IAW SRM.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 60,649 hrs · 47,620 cycles

RIGHT WING OTBD MIDFLAP, INBD MIDFLAP, TRACK CARRIAGE, CORRODED, FOUND AT BASE OF CARRIAGE SPINDLE. R & R CARRIAGE IAW MAINTENANCE.

Part: RIB — CRACKED (LT WING) · airframe 60,649 hrs · 47,620 cycles

LEFT WING RIB CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 TO STR 3. REPAIRED CHORD IAW EA.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 60,649 hrs · 47,620 cycles

FORWARD CARGO BAY FORWARD FRAME ANGLE SUPPORT BRACKET CRACKED AT BS 500C, BETWEEN STR 25R TO STR 26R. R & R BRACKET IAW SRM.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 60,649 hrs · 47,620 cycles

LEFT WING NR 2 FLAP TRACK CARRIAGE BASE OF SPINDLE CORRODED. R & R CARRIAGE IAW MT.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 60,649 hrs · 47,620 cycles

FORWARD CARGO BAY FORWARD FRAME ANGLE SUPPORT BRACKET CRACKED AT BS 500B, BETWEEN STR 25L TO STR 26L. R & R BRACKET IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,649 hrs · 47,620 cycles

FRAME SHEAR TIE CORRODED AT BS 787, STR 27R. R & R SHEAR TIE IAW SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 60,649 hrs · 47,620 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,649 hrs · 47,620 cycles

FRAME CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,649 hrs · 47,620 cycles

SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. R & R SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,648 hrs · 47,620 cycles

LEFT NOSE WW SIDE PANEL SKIN CRACKED AT BS 259.5. REPAIRED SKIN IAW SRM.

Part: RETAINER — OUT OF POSITION (L2 DOOR) · airframe 60,272 hrs · 47,374 cycles

L2 DOOR EMER EVAC SLIDE GIRT RETAINER OUT OF POSITION. REPOSITIONED RETAINER IAW MT.

Part: GIRT BAR — LOOSE (R2 DOOR) · airframe 60,203 hrs · 47,330 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR IAW AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 60,133 hrs · 47,289 cycles

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

Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 60,153 hrs · 47,302 cycles

AFT CARGO COMPARTMENT CUT OUT AFT CORNER THRESHOLD CRACKED IN RADIUS. R & R THRESHOLD IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 58,981 hrs · 46,550 cycles

RIGHT EMER LIGHT LENS LOOSE AT ROW 12. SECURED LENS IAW MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 58,911 hrs · 46,498 cycles

AFT EXIT SIGN LIGHTS ON BOTTOM INOPERATIVE. R & R BULB IAW SIP.

Part: COVER — LOOSE (CABIN) · airframe 58,558 hrs · 46,257 cycles

R2 DOOR EXIT LIGHT COVER LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 57,376 hrs · 45,390 cycles

RIGHT WING NR 5 SLAT UPPER TE WEDGE DELAMINATED AT THE OTBD END. R & R NR 5 LE SLAT IAW MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 57,376 hrs · 45,390 cycles

RIGHT WING NR 4 SLAT UPPER TE WEDGE DELAMINATED AT THE INBD END. R & R NR 4 LE SLAT IAW MM.

Part: GUSSET — CRACKED (L1 DOOR) · airframe 55,502 hrs · 44,151 cycles

L1 DOOR LOWER RT CORNER OF GUSSET CRACKED. R & R DOOR IAW MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 55,277 hrs · 43,989 cycles

L1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: WIRE — BROKEN (CABIN) · airframe 54,789 hrs · 43,631 cycles

FORWARD LAVATORY EMER LIGHT ASSEMBLY WIRE BROKEN. R & R WIRE IAW SWPM.

Part: HOOK — FAULTY (R1 DOOR) · airframe 54,789 hrs · 43,631 cycles

R1 DOOR EMER EVAC SLIDE COVER AFT GIRT BAR HOOK FAULTY. R & R HOOK IAW SRM.

Part: STRUCTURE — CRACKED (RT WING) · airframe 54,789 hrs · 43,631 cycles

RIGHT WING LOWER CHORD CRACKED AT WBL 135.5 JUST AFT OF STRINGER 2. REPAIRED CHORD IAW EA.

Part: HOOK — LOOSE (R1 DOOR) · airframe 54,789 hrs · 43,631 cycles

R1 DOOR EMER EVAC SLIDE COVER FWD GIRT BAR HOOK LOOSE. SECURED HOOK IAW SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 54,789 hrs · 43,631 cycles

R1 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: LENS — MISSING (CABIN) · airframe 54,789 hrs · 43,631 cycles

RIGHT EELS LENS MISSING AT ROW 7. INSTALLED LENS IAW AMM.

Part: LIGHT — MISSING (CABIN) · airframe 54,789 hrs · 43,631 cycles

L1 DOOR LOWER EMER LIGHT MISSING. INSTALLED LIGHT IAW MM.

Part: LENS — MISSING (CABIN) · airframe 54,789 hrs · 43,631 cycles

RIGHT EEPLS LENS MISSING AT ROW. INSTALLED LENS IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,789 hrs · 43,631 cycles

FUSELAGE FRAME CHORD CRACKED AT BS 727 STRINGER 18A LT. REPAIRED CHORD IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,789 hrs · 43,631 cycles

FUSELAGE FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A RT. REPAIRED CHORD IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,789 hrs · 43,631 cycles

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

Part: SIGN — INOPERATIVE (CABIN) · airframe 54,589 hrs · 43,498 cycles

L2 DOOR EXTERIOR EMERGENCY AFT AISLE EXIT SIGN INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,589 hrs · 43,498 cycles

LEFT EMERGENCY EXIT LIGHTS AT OVERHEAD BULLNOSE BIN INOPERATIVE BETWEEN ROW 6 TO ROW 22. RELAMPED LIGHTS IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 54,589 hrs · 43,498 cycles

L2 DOOR EMERGENCY EXIT LIGHT SIGN OVER RT AFT DOOR INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 54,589 hrs · 43,498 cycles

L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHTS IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,589 hrs · 43,498 cycles

STRINGER CLIP CRACKED AT BS 460, STRINGER 2R. R & R CLIP IAW DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 54,589 hrs · 43,498 cycles

STRINGER CRACKED AT BS 532, STRINGER 4R. REPAIRED STRINGER IAW SB.

Part: BUTTSTRAP — CRACKED (FUSELAGE) · airframe 54,589 hrs · 43,498 cycles

BUTT STRAP CRACKED AT BS 360+.5, STRINGER 14R. REPAIRED BUTT STRAP IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,589 hrs · 43,498 cycles

SKIN CRACKED AT BS 380, STRINGER 14R. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,589 hrs · 43,498 cycles

SHEAR TIE CRACKED AT BS 540, STRINGER 10L. R & R SHEAR TIE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,589 hrs · 43,498 cycles

RIGHT BS 827+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,589 hrs · 43,498 cycles

LEFT BS 767+10 LOWER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,589 hrs · 43,498 cycles

RIGHT BS 807+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,589 hrs · 43,498 cycles

RIGHT BS 767+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,589 hrs · 43,498 cycles

LEFT BS 767+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,589 hrs · 43,498 cycles

LEFT BS 867+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,589 hrs · 43,498 cycles

LEFT BS 887+10 LOWER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,589 hrs · 43,498 cycles

RIGHT BS 867+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,589 hrs · 43,498 cycles

LEFT BS 827+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,589 hrs · 43,498 cycles

RIGHT BS 847+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,589 hrs · 43,498 cycles

LEFT BS 807+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,589 hrs · 43,498 cycles

LEFT BS 827+10 LOWER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,589 hrs · 43,498 cycles

LEFT BS 807+10 LOWER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,589 hrs · 43,498 cycles

RIGHT BS 807+10 LOWER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW SB.

Part: LENS — BROKEN (CABIN) · airframe 54,332 hrs · 43,330 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LIGHT LENS COVER BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 53,861 hrs · 43,026 cycles

LT WING NR 2 SLAT LOWER SURFACE LE CRACKED. REPAIRED NR 2 SLAT IAW SRM.

Part: SKIN — DELAMINATED (LT SPOILER) · airframe 53,861 hrs · 43,026 cycles

LT WING NR 0 SPOILER UPPER SURFACE DELAMINATED. R & R NR 0 SPOILER IAW AMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 53,861 hrs · 43,026 cycles

RT WING OTBD FORE FLAP OTBD END DELAMINATED. R & R FORE FLAP IAW AMM.

Part: FAIRING — CRACKED (LT ELEVATOR TAB) · airframe 53,861 hrs · 43,026 cycles

LT ELEVATOR TAB UPPER FAIRING CRACKED. R & R FAIRING IAW DRAWING & SRM.

Part: FAIRING — DAMAGED (TE FLAP) · airframe 53,861 hrs · 43,026 cycles

RT WING NR 8 FLAP TRACK AFT FAIRING INBD HINGE RELIEF HOLE DAMAGED. REPAIRED FAIRING IAW EA.

Part: SKIN — DELAMINATED (LT SPOILER) · airframe 53,023 hrs · 42,457 cycles

LT WING NR 1 FLIGHT SPOILER TE UPPER SURFACE DELAMINATED. R & R SPOILER IAW MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 52,808 hrs · 42,298 cycles

LT WING OTBD TE FLAP DELAMINATED. R&R AFT FLAP IAW AMM.

Part: HOUSING — DEFECTIVE (CABIN) · airframe 52,651 hrs · 42,180 cycles

LT EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 17. R&R LIGHT HOUSING IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,553 hrs · 42,104 cycles

SKIN CRACKED AT BS 520 + 5, STRINGER 10L. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,553 hrs · 42,104 cycles

LT WING AFT EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 52,326 hrs · 41,930 cycles

AFT EMERGENCY BATTERY PACK FAILED OPERATIONS TEST. R&R BATTERY IAW AMM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 52,326 hrs · 41,930 cycles

SHEAR TIE CRACKED AT BS 211. R&R SHEAR TIE IAW EA & DRAWING.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 52,326 hrs · 41,930 cycles

FRAME OTBD T CHORD DAMAGED AT STATION 243, STRINGER 17L. R&R T CHORD IAW SRM & DRAWING.

Part: CREASE BEAM — MISSING (FUSELAGE) · airframe 52,326 hrs · 41,930 cycles

CREASE BEAM WEB MISSING BETWEEN STA 235 TO STA 243, STR 17L. INSTALLED WEB IAW SRM AND DWG.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 52,326 hrs · 41,930 cycles

FWD OTBD EMERGENCY FLASHLIGHT INOPERATIVE. R&R BATTERY IAW MM.

Part: ATTACH FITTING — BROKEN (LT SPOILER) · airframe 52,255 hrs · 41,875 cycles

LT WING NR 4 GROUND SPOILER ATTACH FITTING BROKEN. R & R SPOILER IAW MM.

Part: FIRE DETECTOR — FAULTY (CARGO BAY) · airframe 51,664 hrs · 41,469 cycles

AIR TURNBACK / DECLARED EMERGENCY. FWD CARGO COMPARTMENT FIRE WARN ALARM SOUNDED. C/W WITH FWD CARGO COMPT INSPECTION. NO DEFECT FOUND. REMOVED AND REPLACED FIRE WARN NR 1, 2, 3 & 4 DETECTORS PER MM.

Part: INDICATOR — FAULTY (E&E BAY) · airframe 51,150 hrs · 41,101 cycles

DECLARED EMERGENCY -- ON APPROACH SELECTING FLAPS 5, INDICATION STOPPED AT FLAPS 2 DEGREE. SELECTED FLAPS 10 DEGREE, INDICATION REMAINED AT FLAPS 2. SELECTED FLAPS 15 DEGREE, INDICATION REMAINED AT FLAPS 2. AFTER 2-3 MINUTES FLAPS INDICATION WENT TO FLAPS 15, LANDED WITH FLAPS 15 DEGREE. REMOVED AND REPLACED INDICATOR PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,321 hrs · 40,491 cycles

FUSELAGE CRACKED AT BS 500C+11, STR 10L. REPAIRED SKIN PER EA.

Part: ENGINE — FAILED (LEFT) · airframe 49,710 hrs · 40,035 cycles

INFLIGHT SHUTDOWN/DECLARED EMERGENCY. NR 2 ENGINE ROLLED BACK TO 18 PERCENT N1 AT 34K FLT. NO RESTART ATTEMPT MADE DUE TO SUSPECTED SMOKE REPORTED BY PAX. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: LENS — BROKEN (CABIN) · airframe 49,676 hrs · 40,007 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 49,676 hrs · 40,007 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS IAW AMM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

STIFFENER CRACKED AT BS 663, LBL 24.8. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

FRAME CRACKED AT BS 616, BETWEEN STR 7R TO STR 8R. REPAIRED FRAME IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

TIE CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

STRINGER SPLICE CRACKED AT BS 360, STR 3R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

TIE CLIP CRACKED AT BS 578, STR 10R. REMOVED AND REPLACED TIE CLIP IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

CLIP CRACKED AT BS 685+8, LBL 24.75. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

TIE CLIP CRACKED AT BS 597, STR 10R. REMOVED AND REPLACED TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

FRAME CRACKED AT BS 188 AT LEVEL FLOOR AREA IN FLIGHT CREW COMPARTMENT. REPAIRED FRAME IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

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

Part: STRAP — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

STRAP CORRODED BETWEEN BS 360 TO BS 380, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED DOUBLER IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

CLIP CRACKED AT BS 685+8, RBL 24. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

TIE CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

SHEAR TIE CORRODED AT BS 360, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

STRINGER SPLICE CORRODED BETWEEN BS 887+14 TO BS 907+8, STR 19R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

STRINGER SPLICE CORRODED BETWEEN BS 887+14 TO BS 907+8, STR 21R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 49,676 hrs · 40,007 cycles

LEFT WING NR 2 SLAT SKIN DELAMINATED. REPAIRED SKIN IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

VERTICAL BEAM WEB CRACKED AT BS 178, LBL 5.7. REPAIRED WEB IAW EO AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

WEB ANGLE CRACKED AT BS 380, STR 26R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 49,676 hrs · 40,007 cycles

LEFT WING NR 2 SLAT SKIN CRACKED BETWEEN WBL 329.75 TO WBL 355. REPAIRED SKIN IAW SRM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

SUPPORT CLIP CRACKED AT BS 947.5, STR 25L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

SHEAR TIE CORRODED AT BS 867, BETWEEN STR 25L TO STR 24L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

SHEAR TIE CORRODED AT BS 520, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 49,676 hrs · 40,007 cycles

LEFT WING NR 1 SLAT SKIN CRACKED BETWEEN WS 505 TO WS 530. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

FRAME CRACKED AT BS 947.5, STR 19L. REMOVED AND REPLACED FRAME IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

FRAME CORRODED AT BS 787, BETWEEN STR 26L TO STR 25L. REPAIRED FRAME IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

STRINGER CORRODED BETWEEN BS 967 TO BS 986.5, STR 25L. REPAIRED STRINGER IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

SUPPORT ANGLE CORRODED AT BS 787, STR 25R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

SPLICE CORRODED BETWEEN BS 887+14 TO BS 907+8, STR 23L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

FRAME CRACKED AT BS 520, BETWEEN STR 21L TO STR 22L. REPAIRED FRAME IAW EO AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

FRAME CORRODED AT BS 907, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

STRINGER CORRODED AT BS 747, STR 27R. REPAIRED STRINGER IAW SRM.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

TIE CLIP CORRODED AT BS 793.5, STR 26R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

CLIP CRACKED AT BS 540, LBL 3. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: CABLE — FRAYED (R2 DOOR) · airframe 49,676 hrs · 40,007 cycles

R2 DOOR EMERGENCY ESCAPE SLIDE LATCH CABLE FRAYED. REMOVED AND REPLACED CABLE IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

STUB FRAME CRACKED AT BS 294.5, STR 7R. REPAIRED STUB FRAME IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

FRAME CORRODED AT BS 807, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 947.5, LBL 54. REPAIRED CHORD IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

CLIP CRACKED AT BS 540, RBL 3. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

FRAME CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM 68.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STR 24R TO STR 25R. REPAIRED FRAME IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

TIE CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED TIE CLIP IAW EA AND EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

SKIN CRACKED AT BS 520+7, RBL 5. REPAIRED SKIN IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

FRAME CORRODED AT BS 500B, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

SKIN CRACKED AT BS 211.8, STR 9L. REPAIRED SKIN IAW EO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

SKIN CRACKED AT BS 360+18, LBL 3. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

FRAME CORRODED AT BS 500A, BETWEEN STR 27L TO STR 28L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

FRAME CORRODED AT BS 500C, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,676 hrs · 40,007 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 660 TO BS 680, LBL 24.5. REPAIRED CHORD IAW EA AND EO.

Part: RETAINER — LOOSE (GIRT BAR) · airframe 49,676 hrs · 40,007 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER CLIP LOOSE. REMOVED AND REPLACED CLIP IAW AND DWG.

Part: RETAINING CLIP — LOOSE (GIRT BAR) · airframe 49,676 hrs · 40,007 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER CLIP LOOSE. REMOVED AND REPLACED CLIP IAW SRM.

Part: ACTUATOR — LEAKING (RT SPOILER) · airframe 49,563 hrs · 39,912 cycles

RIGHT WING NR 6 SPOILER ACTUATOR LEAKED. REMOVED AND REPLACED ACTUATOR PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 48,954 hrs · 39,445 cycles

CENTER AISLE EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED BATTERY PACK CHARGER ASSY IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 48,954 hrs · 39,445 cycles

RIGHT OVERWING UPPER EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED BATTERY PACK CHARGER ASSY IAW AMM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 48,953 hrs · 39,444 cycles

VERTICAL STIFFENER ANGLE CRACKED AT BS 727, LBL 5. REMOVED & REPLACED STIFFENER IAW BAC DWG.

Part: KEELBEAM — WORN (FUSELAGE) · airframe 48,953 hrs · 39,444 cycles

LT KEEL BEAM WORN BETWEEN BS 625 TO BS 727+14. REPAIRED BEAM IAW SRM.

Part: MOUNT — CRACKED (R2 DOOR SLIDE) · airframe 48,952 hrs · 39,443 cycles

R2 DOOR EMERENCY EVAC SLIDE FWD SLIDE MOUNT CRACKED. REMOVED AND REPLACED MOUNT PER MM.

Part: BRACKET — LOOSE (R2 DOOR SLIDE) · airframe 48,952 hrs · 39,443 cycles

R2 DOOR EMERGENCY EVAC SLIDE BRACKET LOOSE. REMOVED AND REPLACED BRACKET PER MM.

Part: CONTROL VALVE — LEAKING (NR 2 ENGINE) · airframe 48,175 hrs · 38,878 cycles

DECLARED EMERGENCY - NR 2 ENGINE HYDRAULIC 'LOW PRESSURE' LIGHT ILLUMINATED IN FLIGHT. FOUND AUTO BRAKE CONTROL VALVE LEAKED. REMOVED AND REPLACED VALVE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 47,291 hrs · 38,191 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,291 hrs · 38,191 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 520+10, STR 28L. REPAIRED SKIN PER EA.

Part: SPOILER — DELAMINATED (RT WING) · airframe 47,291 hrs · 38,191 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 8 SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 47,006 hrs · 37,966 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. REMOVED AND REPLACED HOOK ASSY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 46,451 hrs · 37,557 cycles

DURING SCHEDULED CV CHECK FOUND FWD CABIN EMERGENCY EXIT LIGHT LENS ABOVE FWD LAV DOOR LOOSE. TIGHTENED EMERGENCY LIGHT LENS PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,542 hrs · 36,855 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLIGHT DECK FLOOR WEB CRACKED AT FWD I/B MOUNTING HOLE FOR OPC CRADLE. REPAIRED WEB PER ACO.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,542 hrs · 36,855 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLIGHT DECK FLOOR WEB CRACKED AT FWD O/B MOUNTING HOLE FOR OPC CRADLE. REPAIRED WEB PER ACO.

Part: FLAP — DELAMINATED (LT WING) · airframe 45,542 hrs · 36,855 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,542 hrs · 36,855 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 45,542 hrs · 36,855 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM ENTIRE UPPER FLANGE CORRODED AT BS 986. REPAIRED BEAM PER EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 45,542 hrs · 36,855 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE 4R CRACKED AT BS 907. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: STRUCTURE — CRACKED (L1 DOOR) · airframe 45,490 hrs · 36,816 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND L1 DOOR LOWER HINGE BOX CRACKED IN RADIUS. REMOVED AND REPLACED HINGE BOX PER SRM.

Part: CASTING — CRACKED (FUSELAGE) · airframe 45,431 hrs · 36,766 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CASTING. REMOVED AND REPLACED CASTING PER MM AND SRM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 44,687 hrs · 36,172 cycles

DURING SCHEDULED CV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 44,551 hrs · 36,071 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 44,551 hrs · 36,071 cycles

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

Part: SIGN — DAMAGED (CABIN) · airframe 43,968 hrs · 35,624 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 43,848 hrs · 35,531 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING OUTBOARD AFT FLAP DELAMINATED AT I/B END. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — PUNCTURED (MIDFLAP) · airframe 43,848 hrs · 35,531 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING I/B MID FLAP LOWER SKIN PUNCTURED. REPAIRED FLAP PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 43,849 hrs · 35,531 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT MLG CEILING PRESSURE WEB CRACKED AT BS 663, LBL 39. REPAIRED WEB PER EA AND SRM.

Part: CONTROLLER — FAULTY (E&E BAY) · airframe 43,678 hrs · 35,412 cycles

DIVERSION - DURING FLIGHT, PASSENGERS AND FLIGHT ATTENDANT REPORTED "HEAT SMELL" IN FWD CABIN. SIDEWALL PANEL ROW 8 ON F/O'S SIDE BECAME EXTREMELY WARM. REMOVED AND REPLACED CABIN TEMP CONTROLLER, RT A/C MIX VALVE, AND RT ANTICIPATOR SENSOR, AND T415 SENSOR PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,576 hrs · 35,334 cycles

DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY BULL NOSE LIGHT INOP BETWEEN ROW 10 TO 17. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 43,438 hrs · 35,237 cycles

RT EEPLS MISSING AT ROW 16. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,066 hrs · 34,971 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 510D, STR 10R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,617 hrs · 33,912 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 511D, STR 10L. REPAIRED SKIN PER SWA EA.

Part: LIGHT — BROKEN (CABIN) · airframe 40,460 hrs · 33,036 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,417 hrs · 33,005 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EMERGENCY EXIT SIGN INOP. INSTALLED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,417 hrs · 33,005 cycles

DURING SCHEDULED 12Y CHECK, FOUND R2 DOOR EMERGENCY EXIT SIGN INOP. INSTALLED BATTERY PACK PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 40,417 hrs · 33,005 cycles

DURING SCHEDULED 12Y CHECK, FOUND EEPLS STRIP LOOSE BETWEEN ROW 13 TO ROW 15. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,417 hrs · 33,005 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT OVERHEAD EMERGENCY EXIT SIGN INOP. INSTALLED BATTERY PACK PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 40,417 hrs · 33,005 cycles

DURING SCHEDULED 12Y CHECK, FOUND KEEL BEAM CORRODED AT BS 613, WL 148. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,417 hrs · 33,005 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 40,417 hrs · 33,005 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 847, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,417 hrs · 33,005 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,417 hrs · 33,005 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 18R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 38,916 hrs · 31,971 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING INBOARD FORE FLAP DELAMINATED. REPAIRED FLAP PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 38,553 hrs · 31,700 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 38,041 hrs · 31,310 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,765 hrs · 31,095 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 37,565 hrs · 30,955 cycles

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

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 37,565 hrs · 30,955 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 37,427 hrs · 30,853 cycles

FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: LENS — BROKEN (CABIN) · airframe 36,816 hrs · 30,403 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 35,939 hrs · 25,743 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 35,745 hrs · 29,595 cycles

DURING SCHEDULED HC1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 34,882 hrs · 28,908 cycles

DURING SCHEDULED MV4 CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: TORQUE TUBE — CORRODED (RT WING TE FLAP) · airframe 33,979 hrs · 28,191 cycles

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

Part: TORQUE TUBE — CORRODED (RT WING TE FLAP) · airframe 33,979 hrs · 28,191 cycles

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

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 33,979 hrs · 28,191 cycles

DURING SCHEDULED 10Y CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER SURFACE. REPAIRED FLAP PER SRM.

Part: VERTICAL BEAM — CRACKED (BS 184) · airframe 33,979 hrs · 28,191 cycles

DURING SCHEDULED 10Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 184, LBL 17.1. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (BS 827 S8L) · airframe 33,979 hrs · 28,191 cycles

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

Part: FRAME — CRACKED (BS 787 S8 L/R) · airframe 33,979 hrs · 28,191 cycles

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

Part: FRAME — CRACKED (BS 727D S8L) · airframe 33,979 hrs · 28,191 cycles

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

Part: FRAME — CRACKED (BS 867 S8L/R) · airframe 33,979 hrs · 28,191 cycles

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

Part: FRAME — CRACKED (BS 480 S8L) · airframe 33,979 hrs · 28,191 cycles

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

Part: FRAME — CRACKED (BS 520 S8L) · airframe 33,979 hrs · 28,191 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 360 S8R) · airframe 33,979 hrs · 28,191 cycles

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

Part: FRAME — CRACKED (BS 907 S8L) · airframe 33,979 hrs · 28,191 cycles

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

Part: VERTICAL BEAM — CRACKED (FUSELAGE) · airframe 33,979 hrs · 28,191 cycles

DURING SCHEDULED 10Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 184, RBL 17.1. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 33,979 hrs · 28,191 cycles

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

Part: FRAME — CRACKED (BS 440 S8R) · airframe 33,979 hrs · 28,191 cycles

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

Part: FRAME — CRACKED (BS 907 S8R) · airframe 33,979 hrs · 28,191 cycles

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

Part: FRAME — CRACKED (BS 616 S17L/R) · airframe 33,979 hrs · 28,191 cycles

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

Part: STRINGER CLIP — CRACKED (BS 663 S10R) · airframe 33,979 hrs · 28,191 cycles

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

Part: ATTACH FITTING — CORRODED (L1 DOOR) · airframe 33,979 hrs · 28,191 cycles

DURING SCHEDULED BRDG CHECK, L1 DOOR EVACUATION SLIDE GIRT BAR FWD FLOOR ATTACH FITTING CORRODED. REMOVED AND REPLACED FWD FITTING PER SRM.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 33,979 hrs · 28,191 cycles

DURING SCHEDULED BRDG CHECK, L1 DOOR EVACUATION SLIDE GIRT BAR AFT FLOOR ATTACH FITTING CORRODED. REMOVED AND REPLACED AFT FITTING PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 33,504 hrs · 27,837 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 33,504 hrs · 27,837 cycles

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

Part: CONTROLLER — FAILED (COCKPIT WINDOW) · airframe 32,915 hrs · 27,378 cycles

FIRST OFFICER NOTICED ARCHING ON FLIGHT DECK R2 WINDOW. REMOVED AND REPLACED WINDOW AND HEAT CONTROLLER PER MM.

Part: SKIN — CRACKED (BS 680-716) · airframe 32,520 hrs · 27,062 cycles

DURING SCHEDULED C4 CHECK, FOUND KEEL BEAM SKIN CRACKED AT BS 680 TO BS 716, RBL 1.5. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 32,520 hrs · 27,062 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 32,520 hrs · 27,062 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT OUTBOARD T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 5 L/E SLAT PER MM.

Part: BOLT — WORN (ELEVATOR TAB) · airframe 31,684 hrs · 26,411 cycles

DURING SCHEDULED C3 CHECK, LT ELEVATOR CONTROL TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED OUTBOARD ELEVATOR TAB ROD END BOLT PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 30,114 hrs · 25,230 cycles

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

Part: FRAME — CRACKED (BS 178) · airframe 29,832 hrs · 24,998 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BLKHD SIDE CHORDS CRACKED AT WL 207. REMOVED AND REPLACED SIDE CHORDS PER SRM AND SWA ACO.

Part: FRAME — CRACKED (AFT CARGO) · airframe 29,832 hrs · 24,998 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT AFT CARGO DOOR CUTOUT, FWD FRAME NR 5 STOP FITTING. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 29,318 hrs · 24,600 cycles

AFT GALLEY EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 29,144 hrs · 24,458 cycles

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

Part: LENS — MISSING (CABIN) · airframe 28,814 hrs · 24,181 cycles

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING ABOVE ROW 2 DEF. INSTALLED LENS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,013 hrs · 22,780 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 26,116 hrs · 22,072 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE DOOR GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 25,616 hrs · 21,653 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 663, LBL 33, CRACKED. REPAIRED WEB PER SRM.

Part: FITTING — CORRODED (RT & LT MLG) · airframe 25,474 hrs · 21,529 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT AND LT MLG FWD OUTBOARD HANGER FITTINGS CORRODED. REMOVED AND REPLACED MLG FITTINGS PER EA.

Part: FITTING — CORRODED (LT MLG) · airframe 25,474 hrs · 21,529 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT MLG FWD AND AFT STABILIZER FITTINGS CORRODED. REMOVED AND REPLACED LT MLG FWD AND AFT STABILIZER FITTINGS PER MM.

Part: HOOK — LOOSE (R1 DOOR GIRT BAR) · airframe 25,375 hrs · 21,446 cycles

R1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED R1 DOOR EVAC SLIDE GIRT BAR HOOKS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,257 hrs · 21,340 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 25,024 hrs · 21,142 cycles

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

Part: SLIDE — LOOSE (R2 DOOR) · airframe 25,017 hrs · 21,136 cycles

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

Part: COVER — DETERIORATED (EMERGENCY LIGHT) · airframe 23,837 hrs · 20,200 cycles

EEPLS COVER DETERIORATED AT THE RT SIDE OF AFT CABIN. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 23,735 hrs · 20,128 cycles

L1 DOOR EVAC SLIDE LOW PRESSURE INDICATION. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM.

Part: INDICATOR — FAULTY (NR 1 ENG TEMP) · airframe 23,513 hrs · 19,958 cycles

INFLIGHT SHUTDOWN/DECLARED EMERGENCY, DURING FLIGHT NR 1 ENGINE OIL TEMP GAUGE READ 180-190C. ENGINE WAS SHUT DOWN IAW QRH. REMOVED AND REPLACED TEMP GAUGE PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 22,214 hrs · 18,942 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT SECTION MISSING BETWEEN ROW NR 19 ABC AND ROW NR 21 ABC. INSTALLED STRIP PER MM.

Part: TRUNNION — CORRODED (LT MLG) · airframe 20,881 hrs · 17,869 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED LT MLG TRUNNION PIN PER MM.

Part: STRUT — CORRODED (LT MLG) · airframe 20,881 hrs · 17,869 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT MLG UPPER OUTER CYLINDER CORRODED. REMOVED AND REPLACED LT MLG UPPER OUTER CYLINDER PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 19,465 hrs · 16,735 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 19,468 hrs · 16,735 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: ENGINE — FLAMED OUT (RT WING) · airframe 19,389 hrs · 16,670 cycles

NR 2 ENGINE FLAMEOUT, DECLARED EMERGENCY, AIR TURNBACK, NR 2 ENGINE FLAMED OUT DURING CLIMB. REMOVED AND REPLACED MEC AND FUEL PUMP, PROBLEMS STILL EXIST. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 18,209 hrs · 15,638 cycles

RT OVERWING EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EXIT LIGHT ASSY.

Part: COVER — CRACKED (CABIN) · airframe 17,735 hrs · 15,218 cycles

DURING SCHEDULED A2 CHECK, FOUND EEPLS COVERS CRACKED AT ROW'S 12 AND 9. REMOVED AND REPLACED COVERS PER MM.

Part: SLIDE — UNSERVICEABLE (AFT ENTRY DOOR) · airframe 17,405 hrs · 14,950 cycles

DURING SCHEDULED A2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: COVER — LOOSE (CABIN) · airframe 17,238 hrs · 14,814 cycles

EEPLS COVER LOOSE AT ROW NR 6. SECURED COVER PER MM.

Part: FLOORBEAM — CORRODED (AFT CABIN) · airframe 17,221 hrs · 14,802 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5, LBL 5. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 17,221 hrs · 14,802 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 807, LBL 8. REPAIRED FLOORBEAM PER SWA RA.

Part: LIGHT — LOOSE (CABIN) · airframe 16,851 hrs · 14,502 cycles

DURING SCHEDULED BC3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 16,420 hrs · 14,160 cycles

EEPLS COVER MISSING. INSTALLED COVER PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 15,883 hrs · 13,730 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 15,254 hrs · 13,186 cycles

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

Part: ACTUATOR — FAILED (L/E FLAP) · airframe 15,235 hrs · 13,168 cycles

AIR TURNBACK, RT WING L/E FLAP TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 3 L/E FLAP ACTUATOR PER MM.

Part: LENS — MISSING (CABIN) · airframe 14,986 hrs · 12,962 cycles

DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 23. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 14,869 hrs · 12,869 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,021 hrs · 12,163 cycles

DURING SCHEDULED C4 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 16 DEF. RELAMPED PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 13,017 hrs · 11,327 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING OTBD AFT FLAP DELAMINATED AT LOWER INBD END. R&R FLAP ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,017 hrs · 11,327 cycles

DURING SCHEDULED C3 CHECK, FOUND BULLNOSE EMERGENCY LIGHT INOP AT ROW 9R. RELAMPED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (ROW 14) · airframe 11,215 hrs · 9,778 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 14 LT. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED RON CHECK, FOUND EMERGENCY PROXIMITY LIGHT NEAR FWD SERVICE DOOR INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: PCU — MALFUNCTIONED (RUDDER)

DURING CLIMB, 20000 FEET, 295 KTS, B AUTOPILOT IN USE. AIRCRAFT WAS IN SMOOTH AIR WHEN A SHORT KICK WAS EXPERIENCE. RUDDER KICK WINGS REMAINED LEVEL AT ALL TIMES. NO RUDDER INPUT BY PILOT WAS NOTED. REMOVED AND REPLACED RUDDER PCU ENGAGE SOLENOID PER MM.