N639SW

Part: COVER — UNSECURE (EXIT SIGN) · airframe 63,690 hrs · 49,981 cycles

L1 DOOR EXIT SIGN COVER FELL OFF. R&R LIGHT ASSEMBLY PER MM.

Part: COVER — UNSECURE (CABIN) · airframe 63,584 hrs · 49,907 cycles

L1 DOOR, EXIT LIGHT COVER FELL OFF. R & R COVER IAW SIP.

Part: DOOR — DELAMINATED (RIGHT MLG) · airframe 63,456 hrs · 49,827 cycles

RIGHT MAIN LANDING GEAR INNER DOOR DELAMINATED. REPAIRED THE MLG DOOR IAW AMM.

Part: HINGE — BROKEN (LT WING SPOILER) · airframe 63,100 hrs · 49,587 cycles

LEFT WING NR 5 GROUND SPOILER 2ND HINGE FROM OUTBOARD BROKEN. R & R THE NR 5 GROUND SPOILER IAW MM.

Part: SKIN — DELAMINATED (LT WING SPOILER) · airframe 62,653 hrs · 49,296 cycles

LEFT WING NR 2 SPOILER DELAMINATED. R & R SPOILER ASSEMBLY IAW MM.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 62,319 hrs · 49,075 cycles

AFT PRESS BULKHEAD WEB OIL CANNING AT BS 1016, BETWEEN STRINGER 9R - 11R. REPAIRED BULKHEAD IAW EA.

Part: BRACKET — OUT OF POSITION (R2 DOOR) · airframe 62,089 hrs · 48,934 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR BRACKET OUT OF POSITION. REPOSITIONED BRACKET IAW SIP.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 62,049 hrs · 48,909 cycles

R2 DOOR EMER ESCAPE SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,049 hrs · 48,909 cycles

R2 DOOR EMER EXIT LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 62,049 hrs · 48,909 cycles

LEFT BIN EMER EXIT LIGHT LENS LOOSE AT ROW 18. SECURED LENS IAW AMM.

Part: SKIN — CRACKED (RT WING) · airframe 62,049 hrs · 48,909 cycles

RIGHT WING UPPER TE SKIN, AFT OF SPAR CHORD CRACKED FASTENER HOLES, BETWEEN RSS 230 - RSS 253. REPAIRED SKIN IAW EA & ER.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 670, RBL 24.8. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 670, RBL 24.8. REPAIRED BEAM IAW EA.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 62,049 hrs · 48,909 cycles

RIGHT WING MLG BEAM AFT SUPPORT FITTING CRACKED. REPAIRED FITTING IAW EA.

Part: FITTING — LOOSE (TE FLAP) · airframe 62,049 hrs · 48,909 cycles

RIGHT WING OTBD AFT FLAP, OTBD ACTUATOR FITTING LOOSE. R & R FITTING IAW CMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

AFT GALLEY DOOR, SKIN CUT OUT CRACKED AT FWD LOWER CORNER. REPAIRED SKIN IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

FUSELAGE FRAME CORRODED AT STATION 767, STRINGER 25L - 25R. REPAIRED FRAME IAW SRM.

Part: SPAR — CRACKED (RT WING) · airframe 62,049 hrs · 48,909 cycles

RIGHT WING AT 3RD UPPER HOLE, INBD OF MLG AFT SUPPORT FITTING AT RSS 219. REAR SPAR WEB CRACKED. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

FUSELAGE FRAME CRACKED, AT STATION 440, STRINGER 24R. REPAIRED FRAME IAW SRM.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 62,049 hrs · 48,909 cycles

LEFT WING TE UPPER SPAR CHORD, SPAR WEB & MLG, AFT SUPPORT FITTING CRACKED AT NR 5 FASTENER HOLE RSS 222.5. REPAIRED FITTING IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 62,049 hrs · 48,909 cycles

RIGHT WING AT MLG AFT SUPPORT FITTING, UPPER INBD NR 5 HOLE RSS 222, REAR SPAR UPPER CHORD CRACKED. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,049 hrs · 48,909 cycles

LEFT WING TE UPPER SPAR CHORD CRACKED, AT UPPER FASTENER HOLE RSS 221.5. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

LOWER FWD CORNER OF THE AFT CARGO DOOR CUTOUT SKIN CRACKED, STATION 840, STRINGER 24R. REPAIRED SKIN IAW SRM.

Part: SPAR — CRACKED (LT WING) · airframe 62,049 hrs · 48,909 cycles

LEFT WING TE UPPER SPAR CHORD & SPAR WEB CRACKED, AT LOWER FASTENER HOLE RSS 219. REPAIRED WEB IAW EA.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

STRINGER CLIP DAMAGED AT STATION 727B, STRINGER 25L. R & R CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

FRAME WEB CRACKED AT BS 277, STRINGER 16R. REPAIRED WEB IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

STRINGER CLIP CRACKED AT STATION 277, STRINGER 11R. R & R CLIP IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 665, RBL 24.8. REPAIRED CHORD IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

FUSELAGE FRAME CORRODED AT STATION 807, STRINGER 26R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

FRAME CORRODED AT BS 747, BETWEEN STRINGER 27L - 27R. REPAIRED FRAME IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

STRINGER CLIP CORRODED AT STATION 747, STRINGER 27L. R & R CLIP IAW SRM.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 62,049 hrs · 48,909 cycles

LEFT WING UPPER TE PANEL, SUPPORT BRACKET ON OTBD SIDE OF PYLON CRACKED. R & R BRACKET IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

FRAME CORRODED AT BS 887, BETWEEN STRINGER 27L - 27R. REPAIRED FRAME IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

AFT CARGO BAY STRINGER CLIP CORRODED, AT BS 787, STRINGER 27L. R & R CLIP IAW DWG & SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

SHEAR TIE CORRODED AT BS 827, BETWEEN STRINGER 27L - 27R. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

SHEAR TIE CORRODED AT BS 967, BETWEEN STRINGER 26R - 27R. REPAIRED SHEAR TIE IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

INTERCOSTAL CORRODED AT STATION 847 - 867, STRINGER 27R. REPAIRED INTERCOSTAL IAW SRM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 62,049 hrs · 48,909 cycles

RIGHT WING INBD SUPPORT ANGLE, CRACKED ON AFT END OF UPPER FLANGE. R & R ANGLE IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 24.8, AFT END INBD FWD FASTENER HOLE. REPAIRED CHORD IAW EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

STRINGER CLIP CORRODED AT STATION 747, STRINGER 27R. R & R CLIP IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

FRAME SHEAR TIE CORRODED, AT BS 787, BETWEEN STRINGER 27R - 25R. R & R FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

FUSELAGE FRAME CORRODED AT STATION 947, STRINGER 27L - 27R. REPAIRED FRAME IAW RM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

FRAME CORRODED AT BS 727E, BETWEEN STRINGER 25L - 25R. R & R FRAME IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

FUSELAGE FRAME CORRODED AT STATION 1006, STRINGER 26L - 27L. REPAIRED FRAME IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 62,049 hrs · 48,909 cycles

LEFT WING INBD NO STEP PANEL, SUPPORT ANGLE CRACKED AT AFT END OF UPPER FLANGE. R & R ANGLE IAW SRM.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

FORWARD CARGO BAY FAIL SAFE CHORD CORRODED AT BS 500D, LBL 12. R & R CHORD IAW DWG & SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

SHEAR TIE CORRODED AT BS 480, RBL 14. R & R SHEAR TIE IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

SHEAR TIE CORRODED AT STATION 500C, LBL 16, WL 156. REPAIRED SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

INTERCOSTAL WEB CRACKED AT BS 278, STRINGER 14R. REPAIRED INTERCOSTAL IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

SHEAR TIE CORRODED AT STATION 500A, LBL 12, WL 156. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

SHEAR TIE CORRODED AT STATION 500D, STRINGER 27R - 28R. REPAIRED SHEAR TIE IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,049 hrs · 48,909 cycles

LONGITUDINAL BEAM CRACKED AT BS 662, RBL 24. REPAIRED BEAM IAW EA.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 62,049 hrs · 48,909 cycles

LEFT WING RSS 547 AILERON WIPER WEB SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 62,049 hrs · 48,909 cycles

RIGHT WING R22. 547 AILERON WIPER WEB SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 61,656 hrs · 48,643 cycles

LEFT WING UPPER SKIN CRACKED AT WBL 141, AFT EDGE. REPAIRED SKIN IAW EA.

Part: SPOILER — DELAMINATED (RT WING) · airframe 61,398 hrs · 48,464 cycles

RIGHT WING NR 9 FLIGHT SPOILER DELAMINATED. R & R NR 9 FLIGHT SPOILER IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 61,196 hrs · 48,323 cycles

FORWARD EMER EXIT LIGHT LENS CRACKED. R & R LIGHT ASSEMBLY IAW MM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 61,121 hrs · 48,268 cycles

E & E COMPARTMENT LOWER FLOORBEAM CHORD LONGITUDINAL STRAP CRACKED AT BS 328, LBL 12. REPAIRED STRAP IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,921 hrs · 48,129 cycles

RIGHT EMER LIGHTS INOPERATIVE AT ROW 9. R & R BATTERY PACK IAW AMM.

Part: FLAP — DAMAGED (RT WING) · airframe 60,741 hrs · 48,003 cycles

RIGHT WING INBD FORE FLAP DAMAGED ON INBD END. R & R FORE FLAP IAW AMM.

Part: COVER — BROKEN (CABIN) · airframe 60,209 hrs · 47,615 cycles

L1 DOOR EMER EXIT LIGHT COVER BROKEN. R & R COVER IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 59,827 hrs · 47,349 cycles

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

Part: BEARING — LOOSE (RT MLG TRUNNION) · airframe 59,728 hrs · 47,286 cycles

RIGHT MLG FWD TRUNNION LOOSE. R & R BEARING IAW MT.

Part: BLOWER — FAILED (CABIN) · airframe 59,489 hrs · 47,120 cycles

DIVERSION, DECLARED EMER. DURING CRUISE WE SMELLED FUMES IN THE COCKPIT & IN THE CABIN. NO ABNORMAL ENG OR ELEC INDICATIONS WERE NOTED. AIR CONDITIONING SYS SEEMED NORMAL. FOUND NORMAL EQUIP COOLING FAN BLOWER FAILED & CAUSE OF ELEC SMELL. R & R NORMAL EQUIP COOLING FAN BLOWER IAW MM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 59,313 hrs · 47,018 cycles

L1 DOOR EMER EXIT SIGN LENS BROKEN. R & R LENS IAW AMM.

Part: LENS — UNSECURE (CABIN) · airframe 59,282 hrs · 46,999 cycles

L1 DOOR EMER EXIT LIGHT LENS FELL OFF. REINSTALLED LENS IAW SIP.

Part: FITTING — LOOSE (R1 DOOR) · airframe 58,975 hrs · 46,789 cycles

R1 DOOR EMER AFT FLOOR MOUNTED GIRT BAR FITTING LOOSE. SECURED FITTING IAW SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 58,895 hrs · 46,740 cycles

R1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 58,352 hrs · 46,380 cycles

R2 DOOR EVACUATION SLIDE LOOSE. SECURED SLIDE IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,221 hrs · 46,294 cycles

M1675 EMER CABIN BULLNOSE LIGHT IN FWD CABIN INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,221 hrs · 46,294 cycles

M1674 EMER CABIN BULLNOSE LIGHT IN FWD CABIN INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,112 hrs · 44,823 cycles

LT OVERWING EMERGENCY EXIT LIGHT BULB INOPERATIVE. R & R BULB IAW MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 56,112 hrs · 44,823 cycles

RT WING OTBD AFT FLAP DELAMINATED AT INBD END. R & R FLAP ASSEMBLY IAW MM.

Part: CHARGER — BROKEN (CABIN) · airframe 56,112 hrs · 44,823 cycles

BATTERY CHARGER HOLD DOWN BROKEN AT BS 727+18, 213 LBL. R & R CHARGER IAW AMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 56,112 hrs · 44,823 cycles

RT WING OTBD AFT FLAP INBD END DELAMINATED. R & R AFT FLAP IAW MM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 56,112 hrs · 44,823 cycles

RT WING INBD MID FLAP TE WEDGE DELAMINATED. R & R WEDGE IAW SRM.

Part: WEB — DAMAGED (FUSELAGE) · airframe 56,112 hrs · 44,823 cycles

AFT CARGO BAY DOOR CUTOUT CLOSURE WEB DAMAGED AT BS 790, RBL 27. R & R WEB IAW DRAWING & SRM.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 56,112 hrs · 44,823 cycles

NOSE WW CRACKED AT BS 258 RT SIDE UNDER DOUBLER. REPAIRED NOSE WW IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,112 hrs · 44,823 cycles

FRAME INNER CHORD CRACKED AT BS 616, FWD SIDE AT 1ST FASTENER ABOVE LT CREASE BEAM WEB. REPAIRED CHORD IAW ER & EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,112 hrs · 44,823 cycles

NR 1 LE SLAT SKIN CRACKED BETWEEN OTBD MAIN TRACK & MID AUXILIARY TRACK. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,112 hrs · 44,823 cycles

FUSELAGE FRAME CRACKED AT STATION 616, STRINGER 16L. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,112 hrs · 44,823 cycles

NR 1 LE SLAT SKIN CRACKED AT INBD END OF BULLNOSE. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,112 hrs · 44,823 cycles

FRAME WEB CRACKED AT BS 616, STRINGER 16L. REPAIRED WEB IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 56,112 hrs · 44,823 cycles

MAIN WW PRESS DECK CRACKED AT BS 672, LBL 31. REPAIRED DECK IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,112 hrs · 44,823 cycles

FRAME INNER CHORD CRACKED AT BS 616, 3RD FASTENER BELOW LT CREASE BEAM WEB. REPAIRED CHORD IAW ER & EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,106 hrs · 44,822 cycles

RT EEPLS INOPERATIVE BETWEEN ROW 1 TO ROW 5. RELAMPED EEPLS IAW MM.

Part: SUPPORT FITTING — CRACKED (RT SPOILER) · airframe 56,106 hrs · 44,822 cycles

RT WING NR 5 GND SPOILER INBD ACTUATOR FWD WING SUPPORT FITTING CRACKED AT WBL 119.25. R & R FITTING IAW SRM & DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

STRINGER CLIP CRACKED AT BS 380 STRINGER 8L. R & R CLIP IAW SRM & DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

STRINGER CLIP CRACKED AT BS 400 STRINGER 9L. R & R CLIP IAW SRM & DRAWING.

Part: FORGING — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

RT BS 440+10 UPPER FWD CORNER OF WINDOW FORGING CRACKED IN HOLE NR 7. R & R FORGING IAW BAC DRAWING.

Part: FORGING — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 520+10 UPPER FWD CORNER OF WINDOW FORGING CRACKED AT HOLE NR 7. R & R FORGING IAW BAC DRAWING.

Part: FORGING — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

RT BS 400+10 UPPER FWD CORNER OF WINDOW FORGING CRACKED IN HOLE NR 7. R & R FORGING IAW BAC DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

RT BS 887+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 827+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 5. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 867+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 5. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

RT BS 827+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 767+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE 2. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

RT BS 827+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 887+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 7. REPAIRED SKIN IAW TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

RT BS 787+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 7. REPAIRED SKIN IAW TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 767+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 4 & 5. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 867+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 7 TO 8. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 500A+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 3 TO 7. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 380+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 4 TO 6. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 460+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 520+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 3 TO 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 420+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 500A+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 500B+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 3 TO 4. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 480+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 420+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 5 TO 6. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 500C+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 360+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 2 TO 4. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 500+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 4. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 400+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 3 TO. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 360+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 7. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

RT BS 500A+10 UPPER FWD SKIN CUTOUT CRACKED BETWEEN HOLES 4 TO 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,106 hrs · 44,822 cycles

LT BS 500+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 3 & 4. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,106 hrs · 44,822 cycles

RT WING NR 5 LE SLAT LOWER SKIN OTBD AFT OF OTBD AUXILIARY TRACK CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,106 hrs · 44,822 cycles

LT WING NR 2 LE SLAT LOWER SKIN INBD AFT OF INBD AUXILIARY TRACK CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,062 hrs · 44,790 cycles

RT BS 380+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 5. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,062 hrs · 44,790 cycles

RT BS 500C+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 5. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,062 hrs · 44,790 cycles

RT BS 440+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 1 TO 7. REPAIRED SKIN IAW TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,062 hrs · 44,790 cycles

RT BS 500C+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,062 hrs · 44,790 cycles

RT BS 440+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 5 TO 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,062 hrs · 44,790 cycles

RT BS 360+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 7. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,062 hrs · 44,790 cycles

RT BS 500A+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,062 hrs · 44,790 cycles

RT BS 400+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,062 hrs · 44,790 cycles

RT BS 520+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 5 TO 6. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,062 hrs · 44,790 cycles

RT BS 500B+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 3 TO 5. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,062 hrs · 44,790 cycles

RT BS 360+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 4 TO 6. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,062 hrs · 44,790 cycles

RT BS 460+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED BETWEEN HOLE NR 3 & NR 9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,062 hrs · 44,790 cycles

RT BS 500B+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,062 hrs · 44,790 cycles

RT BS 460+10 UPPER WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 4 TO 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,062 hrs · 44,790 cycles

RT BS 480+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 4. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,062 hrs · 44,790 cycles

RT BS 500+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 4 & 5. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,062 hrs · 44,790 cycles

RT BS 420+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 4 TO 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,560 hrs · 44,443 cycles

FUSELAGE SKIN CRACKED AT BS 727E+ 5, STRINGER 4R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,560 hrs · 44,443 cycles

FUSELAGE SKIN CRACKED AT BS 727A+11, STRINGER 10L. REPAIRED SKIN IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 55,038 hrs · 44,047 cycles

FWD ENTRY LENS ON FLOOR LEVEL EMERGENCY LENS LOOSE. R&R LENS IAW SIP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,972 hrs · 44,001 cycles

SKIN CRACKED AT BS 767 +7 STRINGER 4R. REPAIRED SKIN IAW EA.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 54,972 hrs · 44,001 cycles

RT WING NR 7 FLAP TRACK CORRODED ON MATTING SURFACE. R&R FLAP TRACK IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,972 hrs · 44,001 cycles

SKIN CRACKED AT BS 727A +5 STRINGER 4R. REPAIRED SKIN IAW EA.

Part: LENS — BROKEN (EXIT SIGN) · airframe 54,432 hrs · 43,613 cycles

L1 DOOR EXIT LOWER SIGN COVER BROKEN. R&R LENS IAW MM.

Part: WEB — CRACKED (NLG WW) · airframe 53,645 hrs · 43,051 cycles

LEFT W/W WALL CRACKED AT FS 258, WL 174. REPAIRED WEB PER EA.

Part: COVER — BROKEN (CABIN) · airframe 53,559 hrs · 42,990 cycles

EXIT LIGHT COVER BROKEN OFF AT FWD ENTRY, BETWEEN FLIGHT ATTENDANT JUMP SEAT AND L1 DOOR. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 52,679 hrs · 42,361 cycles

L-1 DOOR EMERGENCY EXIT FLOOR LIGHT BROKEN OFF. REMOVED AND REPLACED L-1 DOOR EMERGENCY EXIT FLOOR LIGHT ASSY PER M/M. OPS CHECK GOOD.

Part: LIGHT — LOOSE (EXIT SIGN) · airframe 52,235 hrs · 42,043 cycles

FORWARD EMERGENCY EXIT SIGN LIGHT LOOSE. SECURED LIGHT ASSY PER THE AMM.

Part: LENS — CRACKED (CABIN) · airframe 52,235 hrs · 42,043 cycles

LEFT EMERGENCY EXIT HATCH "EXIT" LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER THE AMM.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 5,140 hrs · 41,432 cycles

DECLARED EMERGENCY -- FLIGHT ATTENDANTS REPORTED ELECTRICAL SMELL FROM ROWS 14 TO 17. REMOVED AND REPLACED GASPER FAN PER M/M.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 51,364 hrs · 41,381 cycles

L1 DOOR EXTERNAL EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 51,093 hrs · 41,170 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

WEB CRACKED BETWEEN BS 351.2 TO BS 360, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 50,505 hrs · 40,728 cycles

LT WING NR 2 SLAT SKIN DELAMINATED ON I/B END. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

STUB FRAME CRACKED AT BS 947+13.5, STR 17L. REPAIRED STUB FRAME IAW EO AND EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

TIE CLIP CRACKED AT BS 380, STR 24L. REMOVED AND REPLACED CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

TIE CLIP CRACK ON AT BS 380, STR 23L. REMOVED AND REPLACED CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

STR CLIP CRACKED AT BS 380, STR 20L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB IAW.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

WEB CRACKED BS 303, BETWEEN STR 27R TO STR 28L. REMOVED AND REPLACED WEB IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

STRINGER CORRODED BETWEEN BS 1088 TO BS 1138 INTERNAL STRUCTURE OF TORQUE BOX. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: TIE CLIP — BROKEN (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

TIE CLIP BROKEN AT BS 787, STR 8R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

WEB CRACKED AT BS 178, RBL 25. REMOVED AND REPLACED WEB IAW SRM AND SI.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

WEB CRACKED AT BS 178, LBL 25. REMOVED AND REPLACED WEB IAW SRM AND SI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

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

Part: BEAM — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

STUB BEAM CRACKED AT BS 685, LBL 47. REPAIR BEAM IAW EO AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

FRAME WEB CRACKED AT BS 747, STR 13R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

ANGLE CRACKED AT BS 727A, BETWEEN STR 13R TO STR 14R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

FRAME CRACKED AT BS 947.5, STR 19L. REMOVED AND REPLACED FRAME SECTION IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

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

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

STIFFENER CRACKED AT BS 727, STR 27R. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

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

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

STIFFENER CRACKED AT BS 727, STR 27L. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 50,505 hrs · 40,728 cycles

LT WING NR 2 SLAT DELAMINATED ON OUTBOARD END UPPER SURFACE. REPAIRED SLAT IAW SRM.

Part: SKIN — CRACKED (LT SPOILER) · airframe 50,505 hrs · 40,728 cycles

LT WING NR 4 SPOILER LOWER SURFACE CRACKED. REPAIRED SPOILER PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

TIE CLIP CRACKED AT BS 727B, STR 21R. REMOVED AND REPLACED CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

WEB CRACKED BETWEEN BS 294.5 TO BS 303.9, STR 4L. REMOVED AND REPLACED IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

TIE CLIP CRACKED AT BS 440, STR 27L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,505 hrs · 40,728 cycles

RT WING NR 5 SLAT SKIN CRACKED ON LOWER SIDE. REPAIRED SKIN IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

TIE CLIP CRACKED AT BS 400, STR 27L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

FLOORBEAM CRACKED ON UPPER CHORD AT BS 947.5 , LBL 53.5. REPAIRED CHORD IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

CRACK ON STUB FRAME AT BS 296.5, STR 7R. REPAIRED STUB FRAME PER EO & EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

TIE CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FASTENER — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

FRAME FASTENER CRACKED AT BS 727B, STR 25. REMOVED AND REPLACED FASTENER IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

FRAME CRACKED AT BS 767, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

TIE CLIP CRACKED AT BS 500B, STR 27L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 664 TO BS 675, LBL 24.5. REPAIRED BEAM IAW EO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

CLIP CRACKED AT BS 380, BETWEEN STR 26L TO STR 25L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,505 hrs · 40,728 cycles

CRACK ON LONGITUDINAL BEAM WEB LOCATED ON BS 707, LBL 24.8. REPAIRED LONGITUDINAL FLOORBEAM PER EA AND EO.

Part: BRAKE — DEFECTIVE (LT MLG) · airframe 50,224 hrs · 40,526 cycles

DURING TAXIING OUT NOTICED CHATTER AND VIBRATION WHEN PRESSURE WAS APPLIED TO LT BRAKE PEDAL. REMOVED AND REPLACED NR 2 BRAKE AND NR 2 MAIN WHEEL ASSY PER MM.

Part: SIGN — DAMAGED (CABIN) · airframe 50,209 hrs · 40,514 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 50,192 hrs · 40,498 cycles

FWD ENTRY EMERGENCY EXIT SIGN LIGHT LOOSE. SECURED LIGHT IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 49,871 hrs · 40,248 cycles

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

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 48,813 hrs · 39,422 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOOR CUTOUT MOUNT HOLE FOR COMPUTER CRADLE CRACKED AT BS 251, RBL 24. REPAIRED DOUBLER IAW ACO.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 48,813 hrs · 39,422 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOOR CUTOUT MOUNT HOLE FOR COMPUTER CRADLE CRACKED AT BS 251, RBL 17. REPAIRED DOUBLER IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,813 hrs · 39,422 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 616, RBL 70.85. REPAIRED FRAME IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,813 hrs · 39,422 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, RBL 45.5. REMOVED AND REPLACED CLIP IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,813 hrs · 39,422 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME WEB CRACKED AT BS 178, RBL 17.0. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 48,813 hrs · 39,422 cycles

DURING SCHEDULED SPV CHECK, FOUND WEB CRACKED AT BS 178, LBL 17.0. REPAIRED WEB PER SRM.

Part: COVER — BROKEN (CABIN) · airframe 48,628 hrs · 39,276 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,170 hrs · 38,923 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,861 hrs · 38,703 cycles

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

Part: SIGN — LOOSE (CABIN) · airframe 47,310 hrs · 38,300 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 47,285 hrs · 38,284 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 8R. REMOVED AND REPLACED CLIP PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED AT UPPER AFT CORNER OF PASSENGER WINDOW AT BS 797, LT SIDE. REPAIRED SKIN PER EA.

Part: HANDLE — BROKEN (EMERGENCY EXIT) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT OVERWING EMERGENCY EXIT HATCH HANDLE BROKEN. REMOVED AND REPLACED HANDLE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED AT UPPER AFT CORNER OF PASSENGER WINDOW AT BS 530, LT SIDE. REPAIRED SKIN PER EA.

Part: SIGN — INOPERATIVE (CABIN) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT EMERGENCY EXIT SIGN BULBS INOP. RELAMPED PER MM.

Part: LIGHT — DELAMINATED (CABIN) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS DELAMINATED. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND FWD EMERGENCY EXIT LIGHT SIGN LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED AT BS 510C, STR 13L. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CRACKED AT BS 639, STR 4R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 42 TO RBL 50. REPAIRED BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT CREASE BEAM CORRODED AT BS 986.5. REMOVED AND REPLACED BEAM PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: FITTING — BROKEN (GIRT BAR) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD AND AFT GIRT RETAINER CLIPS BROKEN. REMOVED AND REPLACED CLIP ASSY PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED CLIP PER SI.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 46,707 hrs · 37,842 cycles

DURING SCHEDULED 14Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: COVER — LOOSE (CABIN) · airframe 46,356 hrs · 37,575 cycles

L1 DOOR EMERGENCY EXIT SIGN COVER LOOSE. SECURED COVER PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 45,987 hrs · 37,289 cycles

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

Part: LENS — DAMAGED (CABIN) · airframe 44,762 hrs · 36,403 cycles

DURING SCHEDULED CV CHECK, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS LETTERING PEELED. RE-APPLIED LETTERING PER MM.

Part: LENS — DAMAGED (CABIN) · airframe 44,762 hrs · 36,403 cycles

DURING SCHEDULED CV CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS LETTERING PEELED. RE-APPLIED LETTERING PER MM.

Part: COVER — BROKEN (CABIN) · airframe 44,623 hrs · 36,299 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 43,468 hrs · 35,462 cycles

L1 DOOR EXIT LIGHT COVER LOOSE. INSTALLED COVER PER MM.

Part: LENS — BROKEN (CABIN) · airframe 42,101 hrs · 34,482 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 41,703 hrs · 34,198 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD EMERGENCY EXIT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 41,173 hrs · 33,818 cycles

FOUND R1 DOOR EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED SIGN PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 40,734 hrs · 33,504 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 293, BETWEEN STR 12L TO 13L. REPAIRED SHEAR TIE PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,734 hrs · 33,504 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 40,734 hrs · 33,504 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, RBL 14. REPAIRED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,734 hrs · 33,504 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 379, BL 0. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,734 hrs · 33,504 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR SKIN CUTOUT CRACKED AT LOWER HINGE. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,734 hrs · 33,504 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED BETWEEN BS 387.5 TO BS 452.75. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,734 hrs · 33,504 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 39,284 hrs · 32,412 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 38,884 hrs · 32,127 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 16R CRACKED AT BS 487. REPAIRED STRINGER PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 38,884 hrs · 32,127 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER ACO.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 38,884 hrs · 32,127 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 38,424 hrs · 31,780 cycles

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

Part: LENS — BROKEN (EMERGENCY LIGHTS) · airframe 38,112 hrs · 31,538 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,560 hrs · 31,133 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT AIR CONDITIONER HOOK UP CUTOUT, BS 510, STR 28L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,560 hrs · 31,133 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT KEEL BEAM PANEL CRACKED AT BS 685. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,560 hrs · 31,133 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT KEEL BEAM PANEL CRACKED AT BS 700. REPAIRED SKIN PER SRM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 50,504 hrs · 40,728 cycles

RT KEEL BEAM CRACKED BETWEEN BS 700 TO BS 722. REPAIRED BEAM IAW SRM.

Part: PANEL — CRACKED (FUSELAGE) · airframe 50,504 hrs · 40,728 cycles

LT FUSELAGE, KEEL BEAM LWR PANEL CRACKED AT BS 700. REPAIRED PANEL IAW SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 37,458 hrs · 31,045 cycles

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

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 37,323 hrs · 30,937 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 7 DEF. SECURED STRIP PER MM.

Part: SHEAR TIE — CORRODED (BS 767 S25R) · airframe 37,131 hrs · 30,780 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 25R. REPAIRED SHEAR TIE PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 37,005 hrs · 30,684 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 35,779 hrs · 29,734 cycles

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

Part: BEARING — FAILED (RT MLG) · airframe 34,230 hrs · 28,528 cycles

NR 4 WHEEL INNER BEARING FAILED. REMOVED AND REPLACED NR 4 BRAKE AND WHEEL, AXLE SLEEVE AND BRAKE SPACER PER MM. REMOVED AND REPLACED RIGHT MLG INNER CYLINDER PER MM.

Part: FRAME — CRACKED (BS 500A S8L) · airframe 34,041 hrs · 28,389 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 787 S8L) · airframe 34,041 hrs · 28,389 cycles

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

Part: FRAME — CRACKED (BS 480 S8L) · airframe 34,041 hrs · 28,389 cycles

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

Part: FRAME — CRACKED (BS 827 S8L) · airframe 34,041 hrs · 28,389 cycles

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

Part: FRAME — CRACKED (BS 380 S8L) · airframe 34,041 hrs · 28,389 cycles

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

Part: FRAME — CRACKED (BS 400 S8L) · airframe 34,041 hrs · 28,389 cycles

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

Part: FRAME — CRACKED (BS 440 S8L) · airframe 34,041 hrs · 28,389 cycles

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

Part: RIB — CRACKED (RT WING) · airframe 34,041 hrs · 28,389 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING RIB AFT LOWER CHORD CRACKED AT WBL 135.5. REPAIRED CHORD PER ACO.

Part: BUSHING — WORN (LT ELEVATOR TAB) · airframe 34,041 hrs · 28,389 cycles

DURING SCHEDULED 10Y CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BUSHING PER MM.

Part: FITTING — CORRODED (L1 DOOR GIRT BAR) · airframe 34,041 hrs · 28,389 cycles

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

Part: BEARING — WORN (RT ELEVATOR TAB) · airframe 34,041 hrs · 28,389 cycles

DURING SCHEDULED 10Y CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BUSHING AND BEARING PER MM.

Part: BEARING — WORN (LT ELEVATOR TAB) · airframe 34,041 hrs · 28,389 cycles

DURING SCHEDULED 10Y CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPALCED NR 1 TAB HINGE BUSHING AND CONTROL ROD BEARING PER MM.

Part: FITTING — CORRODED (L2 DOOR GIRT BAR) · airframe 34,041 hrs · 28,389 cycles

DURING SCHEDULED 10Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FWD GIRT BAR FITTING PER SRM.

Part: FITTING — CORRODED (L2 DOOR GIRT BAR) · airframe 34,041 hrs · 28,389 cycles

DURING SCHEDULED 10Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED AFT GIRT BAR FITTING PER SRM.

Part: FITTING — CORRODED (R2 DOOR GIRT BAR) · airframe 34,041 hrs · 28,389 cycles

DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED AFT GIRT BAR FITTING PER SRM.

Part: FITTING — CORRODED (R2 DOOR GIRT BAR) · airframe 34,041 hrs · 28,389 cycles

DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FWD GIRT BAR FITTING PER SRM.

Part: FRAME — CRACKED (BS 480 S9R) · airframe 34,041 hrs · 28,389 cycles

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

Part: FRAME — CRACKED (BS 500A S9R) · airframe 34,041 hrs · 28,389 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 9R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 907 S9R) · airframe 34,041 hrs · 28,389 cycles

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

Part: FRAME — CRACKED (BS 827 S8R) · airframe 34,041 hrs · 28,389 cycles

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

Part: FRAME — CRACKED (BS 867 S8R) · airframe 34,041 hrs · 28,389 cycles

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

Part: FRAME — CRACKED (BS 787 S8R) · airframe 34,041 hrs · 28,389 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 34,041 hrs · 28,389 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 348, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 34,041 hrs · 28,389 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 1042 S14L) · airframe 34,041 hrs · 28,389 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1042, STR 14L. REPAIRED SKIN PER SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 32,825 hrs · 27,412 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR UPPER HINGE BOX CRACKED INTO RADIUS. R&R UPPER HINGE BOX PER SRM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 31,573 hrs · 26,431 cycles

DURING SCHEDULED RON CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (NR 2 SLAT) · airframe 31,101 hrs · 26,026 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND NR 2 L/E SLAT LOWER SKIN CRACKED AT OUTBD END. REPAIRED SKIN PER SRM.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 31,029 hrs · 25,964 cycles

DIVERSION/DECLARED EMERGENCY CABIN ALTITUDE WARNING HORN SOUNDED. ALTERNATE & MANUAL POSITIONS INOP. REMOVED AND REPLACED AFT OUTFLOW VALVE PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 30,752 hrs · 25,738 cycles

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

Part: LENS — BROKEN (EMERTENCY LIGHT) · airframe 30,315 hrs · 25,383 cycles

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

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 30,030 hrs · 25,157 cycles

FWD ENTRY DOOR LOWER EMERGENCY LIGHT LENS COVER LOOSE. SECURED COVER PER MM.

Part: BOLT — BROKEN (FLAP TRACK) · airframe 30,020 hrs · 25,149 cycles

BROKEN BOLT AND MISSING FLAP TRACK ROLLER FOUND AT LT WING OUTBOARD T/E FLAP, OUTBOARD ROLLER. INSTALLED BOLT & ROLLER PER MM.

Part: STRIP — MISSING (CABIN) · airframe 29,867 hrs · 25,040 cycles

DURING SCHEDULED C1 CHECK, FOUND PHOTOLUMINESCENT LIGHT STRIP LENS MISSING AT ROWS 6 ABC TO ROWS 8 ABC. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 28,982 hrs · 24,329 cycles

DURING SCHEDULED C4 CHECK, FOUND OUTBOARD END NR 2 L/E SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 28,432 hrs · 23,918 cycles

R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 28,136 hrs · 23,707 cycles

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

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 27,992 hrs · 23,602 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING OUTBOARD T/E AFT FLAP PER MM.

Part: SIGN — CRACKED (EMERGENCY LIGHT) · airframe 27,740 hrs · 23,393 cycles

FWD EMERGENCY EXIT SIGN LENS CRACKED. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM.

Part: FITTING — CRACKED (L1 DOOR FRAME) · airframe 26,085 hrs · 22,072 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR JAMB LOWER FWD HINGE BOX FITTING, CRACKED. REMOVED AND REPLACED HINGE BOX FITTING PER EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 25,935 hrs · 21,940 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 24,134 hrs · 20,520 cycles

EEPLS SECTION LOOSE IN CABIN. SECURED EEPLS SECTION PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 24,094 hrs · 20,492 cycles

DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 1 AND NR 2 HINGE ATTACH HARDWARE PER MM.

Part: FITTING — LOOSE (AFT SVC DOOR) · airframe 22,270 hrs · 19,035 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD ATTACH FITTING LOOSE. SECURED ATTACH FITTING PER MM,

Part: SLIDE — OUT OF ADJUST (FWD CABIN DOORS) · airframe 22,270 hrs · 19,035 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED BOTH FWD CABIN DOOR SLIDES PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 22,262 hrs · 19,029 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 21,981 hrs · 18,814 cycles

DURING CRUISE R1 COCKPIT WINDOW CRACKED WITH ASSOCIATED ARCING. REMOVED AND REPLACED R1 COCKPIT WINDOW AND WINDOW HEAT CONTROLLER PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 21,354 hrs · 18,329 cycles

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

Part: TRUNNION PIN — SHEARED (RT MLG) · airframe 20,370 hrs · 17,558 cycles

DURING DEPARTURE RT MLG WOULD NOT RETRACT. FOUND LANDING GEAR ACTUATOR TRUNNION PIN SHEARED. REMOVED AND REPLACED RT MLG TRUNNION PIN PER MM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 20,344 hrs · 17,532 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 20,240 hrs · 17,441 cycles

EEPLS LOOSE AT ROWS NR 9 AND NR 10. SECURED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,733 hrs · 42,430 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH AFT CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. RELAMPED EXIT LIGHTS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 18,373 hrs · 15,876 cycles

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

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 17,332 hrs · 15,062 cycles

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

Part: HANDLE — BROKEN (O/W EXIT DOOR) · airframe 17,225 hrs · 14,974 cycles

LH OVER WING EMERGENCY EXIT DOOR HANDLE BROKEN. R&R HANDLE PER MM.

Part: BUSHING — WORN (LH ELEVATOR) · airframe 17,225 hrs · 14,973 cycles

DURING SCHEDULED 1/2D CHECK AT DALFORT, FOUND LH ELEVATOR TAB # 2 HINGE WORN. R&R TAB BUSHING PER MM.

Part: FLAP — DELAMINATED (LH WING) · airframe 17,225 hrs · 14,973 cycles

DURING SCHEDULED 1/4D CHECK AT DALFORT, FOUND LH T/E OTBD FLAP DELAMINATED AT UPPER INBD SURFACE. REPAIRED FLAP PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 16,767 hrs · 14,585 cycles

EEPLS TRACK COVER LOOSE AT ROW 18. REMOVED AND REPLACED EEPLS TRACK COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 16,755 hrs · 14,576 cycles

EEPLS LOOSE & MISSING COVERS AT MID CABIN. SECURED EEPLS & INSTALLED COVERS PER MM.

Part: TRACK — LOOSE (CABIN) · airframe 16,237 hrs · 14,101 cycles

EEPLS TRACK LOOSE AT MID CABIN. SECURED EEPLS TRACK PER MM.

Part: COVER — LOOSE (CABIN) · airframe 16,071 hrs · 13,965 cycles

EEPLS COVER LOOSE AT ROW 11. SECURED COVER PER MM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 15,827 hrs · 13,763 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBD AFT FLAP LOWER SURFACE DELAMINATED AT INBD END. R&R AFT FLAP PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 15,739 hrs · 13,692 cycles

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

Part: WIRE — EXPOSED (CABIN) · airframe 15,461 hrs · 13,464 cycles

EEPLS WIRING EXPOSED AT OVERWING EXIT ROW. SECURED WIRING PER MM.

Part: LENS — BROKEN (CABIN) · airframe 15,394 hrs · 13,411 cycles

EEPLS RED TRACK COVER LENS BROKEN. REMOVED AND REPLACED TRACK COVER LENS PER MM.

Part: CONTROL PANEL — INOPERATIVE (COCKPIT) · airframe 15,019 hrs · 13,099 cycles

AIR TURNBACK, PASSING FL 270, AUTO PILOT C/B TRIPPED OFF AND WOULD NOT RE-ENGAGE IN A OR B-MODE. MCP PANEL WOULD NOT RESPOND TO ANY CHANGES. REMOVED AND REPLACED MCP PER MM. OPS CHECK GOOD.

Part: LIGHT — DISCONNECTED (CABIN FLOOR) · airframe 14,840 hrs · 12,957 cycles

EEPLS INOP AT ROWS 14 - 19. RECONNECTED WIRE TERMINALS. OPS CK GOOD PER MM.

Part: GIRT BAR — OUT OF ADJ (AFT SVC DOOR) · airframe 14,794 hrs · 12,915 cycles

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

Part: RETAINER — LOOSE (ESCAPE SLIDE) · airframe 14,794 hrs · 12,915 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY RETAINER LOOSE. SECURED RETAINER PER MM.

Part: WIRE — EXPOSED (CABIN FLOOR) · airframe 14,771 hrs · 12,894 cycles

EEPLS RED LIGHTS AND 5 WHITE LIGHTS INOP AND WIRES EXPOSED AT ROWS 12 & 13. RECONNECTED AND SECURED WIRING PER MM.

Part: LENS — MISSING (CABIN) · airframe 14,661 hrs · 12,802 cycles

EEPLS LENS MISSING AT MID CABIN. REPLACED TRACK COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 14,630 hrs · 12,783 cycles

2 EA. EEPLS TRACK COVERS MISSING AT ROW 22. REPLACED TRACK COVERS PER MM.

Part: WIRE — BROKEN (CABIN FLOOR) · airframe 14,395 hrs · 12,581 cycles

EEPLS WIRING EXPOSED AT MID CABIN AND AFT CABIN WITH SEVERAL LIGHTS INOP. REPAIRED AND SECURED EEPLS WIRING PER MM.

Part: WIRE — EXPOSED (ROW 10) · airframe 14,130 hrs · 12,373 cycles

EEPLS WIRING EXPOSED AT ROW 10. SECURED WIRING PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 13,931 hrs · 12,205 cycles

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

Part: COVER — MISSING (CABIN) · airframe 13,781 hrs · 12,058 cycles

ONE PIECE OF EEPLS FLOOR TRACK COVERING MISSING. REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,431 hrs · 11,787 cycles

EEPLS INOP AT ROW 20. RECONNECTED WIRES AT ROW 22. OPS CHECK GOOD.

Part: WIRE — EXPOSED (CABIN) · airframe 13,308 hrs · 11,673 cycles

EEPLS WIRES SHOWING AT ROW 12. REPAIRED AND SECURED WIRING PER MM.

Part: COVER — MISSING (CABIN) · airframe 13,091 hrs · 11,474 cycles

EEPLS TRACK COVER MISSING AT ROW 21. INSTALLED AND SECURED TRACK COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,543 hrs · 11,014 cycles

EEPLS INOP BETWEEN ROWS 18 & 19. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,429 hrs · 10,921 cycles

EEPLS INOP IN SEVERAL AREAS. REMOVED AND REPLACED EEPLS TRACKS, LENSES AND REPAIRED WIRING PER MM.

Part: SLIDE — LOOSE (PAX DOOR)

DURING SCHEDULED C2 CHECK, FOUND BOTH ENTRY DOOR EVACUATION SLIDE GIRT ASSY'S OUT OF ADJUSTMENT. REINSTALLED BOTH SLIDES PER MM.

Part: LIGHT — INOPERATIVE (ROW 11 - 13)

EEPLS INOP AT ROW 11-12. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — MISSING (CABIN)

EEPLS TRACK COVER MISSING AT FWD END. REMOVED AND REPLACED TRACK COVER PER MM.

Part: FIRE DETECTOR — ERRATIC (E/E BAY)

ABORTED TAKEOFF, NR 2 ENG OVERHEAT LIGHT ILLUMINATED, REDUCED THRUST TO IDLE AND LIGHT EXTINGUISHED. REMOVED AND REPLACED P-8 FIRE CONTROL PANEL AND FIRE DETECTOR UNIT PER MM.

Part: COVER — MISSING (CABIN)

EEPLS MISSING COVER AT OVERWING EXIT. REPLACED COVER PER MM.

Part: LENS — MISSING (CABIN)

EEPLS MISSING LENS AT OVERWING DOOR. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOP (CABIN)

DURING SCHEDULED A2 CHECK, FOUND EEPLS INOP BY OVERWING EXITS. RECONNECTED WIRE PER MM.

Part: LENS — MISSING (CABIN)

EEPLS MISSING AFT LENS. REMOVED AND REPLACED LENS PER MM.

Part: COVER — MISSING (ROW 19)

EEPLS LIGHT COVER FELL OUT AT ROW 19. REPAIRED WIRING AND REPLACED LIGHT COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

EEPLS LIGHTS AND WIRING OUT OF TRACKS. REPAIRED LIGHTS AND WIRING PER MM.

Part: LIGHT — BROKEN (CABIN)

EEPLS LIGHTS COMING APART ON FLOOR. REPAIRED LIGHTING PER MM.

Part: LIGHT — LOOSE (CABIN)

AFT EMERGENCY ESCAPE FLOOR TRACK LIGHTING PULLED LOOSE. REPAIRED TRACK LIGHTING PER MM.

Part: WIRE — DISCONNECTED (CABIN)

EMERGENCY ESCAPE FLOOR TRACK LIGHT, FWD COVER MISSING. REPLACED COVER, ALSO FOUND WIRES DISCONNECTED. RECONNECTED WIRES PER MM.

Part: LIGHT — LOOSE (CABIN)

EMERGENCY ESCAPE TRACK LIGHT LOOSE IN AFT CABIN. SECURED TRACK LIGHTING PER MM.

Part: LIGHT — LOOSE (ROW 22)

EMERGENCY ESCAPE TRACK LIGHTING LOOSE AT ROW 22. SECURED TRACK LIGHTING PER MM.

Part: WIRE — BROKEN (ROW 20)

EMERGENCY EXIT LIGHTS AT FLOOR TRACK ROW 20 HAD BROKEN WIRES. REPAIRED WIRES PER MM.

Part: WIRE — DAMAGED (CABIN)

LIGHTS INOP ON AIRCRAFT FLOOR EMERGENCY EXIT. REPAIRED DAMAGED WIRES PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR LIGHTS BY LEFT EMERGENCY EXIT DOOR INOP. RECONNECTED LOOSE CONNECTIONS TO LIGHTS PER BOEING MM.

Part: LIGHTS — INOPERATIVE (CABIN)

DURING SCHEDULED RON CHECK, FOUND A SECTION WITH EMERGENCY TRACK LIGHTING INOP. INSTALLED AND RECONNECTED LIGHT ASSEMBLIES AND OP CHECKED PER BOEING MM.

Part: WIRE — BROKEN (CABIN)

DURING WALKAROUND INSPECTION, FOUND AISLE EMERGENCY EXIT LIGHT WIRES BROKEN. REPAIRED PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED C1 CHECK, AFT FLOOR SECTION EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. REPAIRED BROKEN WIRE AND OP CHECKED PER BOEING M/M.

Part: WIRE — DISCONNECTED (CABIN)

DURING SCHEDULED RON, FOUND EMERGENCY EXIT FLOOR TRACK LIGHTING INOPERATIVE AT ROW 21. RECONNECTED WIRES AND OP CHECKED PER BOEING M/M.