N320SW

Part: BATTERY — DISCHARGED (CABIN) · airframe 68,977 hrs · 63,993 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,421 hrs · 63,583 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515D, STR 15L. REPAIRED SKIN PER SWA EA.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 68,421 hrs · 63,583 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR LOWER FRAME CRACKED AT AFT END. REMOVED AND REPLACED DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,421 hrs · 63,583 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 792, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 506C S14R) · airframe 68,366 hrs · 63,538 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506C, STR 14R. REPAIRED SKIN PER SWA EA.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 68,295 hrs · 63,490 cycles

DIVERSION / DECLARED EMERGENCY. AFTER CROSS FEEDING FUEL, TURNED OFF CROSS FEED VALVE, NOTICED LIGHT STAYED ILLUMINATED. NOTICED START OF FUEL IMBALANCE. REMOVED AND REPLACED CROSS FEED VALVE ACTUATOR AND CONNECTOR PER MM.

Part: BATTERY PACK — DISCHARGED (L1 DOOR) · airframe 68,041 hrs · 63,290 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,023 hrs · 61,665 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 375, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,312 hrs · 61,118 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 495, STR 16L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 13R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 13L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 14L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 14R AND STR 14L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727C, STR 14R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 14R. REPAIRED FRAME SECTION PER SWA EA.

Part: TORQUE TUBE — CORRODED (FORE FLAP) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD FORE FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: FRAME — CRACKED (BS 277 S10R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED FRAME SECTION PER ER.

Part: FRAME — CRACKED (BS 663 S2L) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 2L. REMOVED AND REPLACED FRAME SECTION PER ER.

Part: FRAME — CRACKED (BS 520 S13L) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 13L. REMOVED AND REPLACED FRAME SECTION PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD CARGO DOOR CUTOUT LOWER AFT CORNER. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (BS 847 S8L) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REMOVED AND REPLACED FRAME SECTION PER SWA EA.

Part: SHEAR TIE — CRACKED (BS 559 S13L) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 559, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STAB LOWER RIB CRACKED AT STA 138.70. REMOVED AND REPLACED RIB PER SRM AND BOEING DRAWING.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STAB LOWER AFT INBOARD SKIN CRACKED. REPAIRED SKIN PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 270, LBL 11 TO RBL 11. REPAIRED FLOORBEAM CHORD PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 259, LBL 8 TO RBL 8. REPAIRED FLOORBEAM CHORD PER ER.

Part: FITTING — CORRODED (L1 DOOR) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, LBL 12 TO RBL 40. REPAIRED FLOORBEAM PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 908, STR 13R. REPAIRED FRAME SECTION PER SWA EA.

Part: BEARING — CORRODED (ELEVATOR TAB) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT ELEVATOR TAB FWD CONTROL ROD ENDS CORRODED. REMOVED AND REPLACED ROD END BEARINGS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 13L. REPAIRED FRAME SECTION PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 4 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 420, STR 13R. REPAIRED FRAME SECTION PER SWA EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 1040, STR 3L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 578, STR 13R. REPAIRED FRAME SECTION PER SWA EA.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT AND LT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED STAB FITTING PER SRM.

Part: BEARING — CORRODED (ELEVATOR TAB) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT ELEVATOR TAB FWD CONTROL ROD ENDS CORRODED. REMOVED AND REPLACED ROD END BEARINGS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 13R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 13L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 13L. REPAIRED FRAME SECTION PER SWA EA.

Part: TORQUE TUBE — CORRODED (RT WING TE FLAP) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: STRINGER SPLICE — CRACKED (BS 907 S4L) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (BS 1040 S3R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 1040, STR 3R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 360 S14R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 14R. REPAIRED FRAME SECTION PER SRM.

Part: SKIN — DEBONDED (TE FLAP) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD AFT FLAP LOWER SKIN SURFACE DISBONDED AT INBOARD T/E. REPAIRED FLAP PER SRM.

Part: FLOORBEAM — CRACKED (BS 744A) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 744A, RBL 45. REPAIRED FLOORBEAM PER ER.

Part: TORQUE TUBE — CORRODED (LT WING TE FLAP) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: TORQUE TUBE — CORRODED (RT WING TE FLAP) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: FLOORBEAM — CRACKED (BS 744A) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 744A, RBL 25. REPAIRED FLOORBEAM PER ER.

Part: STRAP — CORRODED (BS 1016) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD UPPER AFT STRAP CORRODED AT BS 1016, LBL 16. REMOVED AND REPLACED AFT STRAP PER SRM.

Part: STRINGER CLIP — BROKEN (BS 616 S2R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 616, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND NLG W/W UPPER LT CEILING PANEL CUTOUT CRACKED AT AFT RT CORNER. REPAIRED CEILING PANEL PER ACO.

Part: CREASE BEAM — CORRODED (BS 747-767) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT CREASE BEAM WEB CORRODED AT BS 747 TO BS 767, WL 208. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: RIB — CRACKED (LT WING) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING RIB UPPER AFT CHORD CRACKED AT WBL 114. REPAIRED CHORD PER ER.

Part: FRAME — CRACKED (BS 727D S8R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 578 S11L) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 847 S8R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 867 S4L-4R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4L AND STR 4R. REMOVED AND REPLACED STRINGER CLIP IAW SRM.

Part: FRAME — CRACKED (BS 867 S8R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 639 S1) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED STRINGER CLIP IAW SRM.

Part: FRAME — CRACKED (BS 827 S8L) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 639 S2R-2L) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R AND STR 2L. REMOVED AND REPLACED STRINGER CLIP IAW SRM.

Part: FRAME — CRACKED (BS 807 S8R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 277 S15R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 616 S2L) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2L. REMOVED AND REPLACED STRINGER CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 706 S11L) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 277 S10R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP IAW SRM.

Part: FRAME — CRACKED (BS 767 S8R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 616 S1) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED STRINGER CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 294 S13L) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STRINGER CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 639 S3R-3L) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3L AND STR 3R. REMOVED AND REPLACED STRINGER CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S2L) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S10L) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S7L) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 380 S8R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 727D S8R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 480 S8R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 807 S8L) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT LOWER DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER ACO.

Part: SHEAR TIE — CORRODED (BS 747) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, RBL 26 TO RBL 27. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (BS 847 S24R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME CORRODED AT BS 847, STR 24R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (BS 927) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, LBL 23. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (BS 500 S28R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 500C S28R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 500A S8R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME SECTION IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 727E S8L) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8L. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 787 S8R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME SECTION IAW SRM.

Part: FRAME — CRACKED (BS 747 S8L-8R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L AND STR 8R. REPAIRED FRAME SECTION IAW SRM.

Part: FRAME — CRACKED (BS 500C S8L) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME SECTION IAW SRM.

Part: FRAME — CRACKED (BS 520 S8R) · airframe 64,906 hrs · 60,778 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME SECTION IAW SRM.

Part: COVER — CRACKED (CABIN) · airframe 64,953 hrs · 60,535 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT COVER CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 64,953 hrs · 60,535 cycles

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

Part: GLOWSTRIP — WORN (CABIN) · airframe 64,593 hrs · 60,535 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT RH OVERWING EXIT. REMOVED AND REPLACED EEPLS PHOTOLUMINESCENT STRIP PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 64,508 hrs · 60,468 cycles

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

Part: BOLT — WORN (RT WING) · airframe 64,460 hrs · 60,432 cycles

DURING SCHEDULED A1 CHECK, FOUND RT MLG CLEVIS BEAM ATTACH BOLT WORN. REMOVED AND REPLACED ATTACH BOLT PER MM.

Part: SKIN — CRACKED (BS 935 S23L) · airframe 64,365 hrs · 60,356 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 935, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,098 hrs · 60,137 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 502, STR 12R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,098 hrs · 60,137 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 741, STR 14L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,098 hrs · 60,137 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 754, STR 14L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,098 hrs · 60,137 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 300, STR 19R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,089 hrs · 60,137 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 300, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — DEBONDED (RT FOREFLAP) · airframe 64,098 hrs · 60,137 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,535 hrs · 59,711 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503C, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,535 hrs · 59,711 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 251.6, BETWEEN STR 24L TO STR 25L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 251) · airframe 62,664 hrs · 59,058 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 251.6, BETWEEN STR 24L TO STR 25L. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 62,664 hrs · 59,058 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 5 LEADING EDGE SLAT TRAILING EDGE WEDGE DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,664 hrs · 59,058 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503C, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 773) · airframe 62,664 hrs · 59,058 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 773, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 303) · airframe 62,664 hrs · 59,058 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 303, STR 13L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 503D) · airframe 62,664 hrs · 59,058 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,664 hrs · 59,058 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 270) · airframe 62,664 hrs · 59,058 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 270, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 62,664 hrs · 59,058 cycles

DURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT OUTBOARD AFT SPAR. REPAIRED HORIZONTAL STAB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,664 hrs · 59,058 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 60,133 hrs · 57,097 cycles

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

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 59,712 hrs · 56,755 cycles

DURING SCHEDULED C1 CHECK, FOUND LT KEELBEAM CORRODED AT BS 540. REPAIRED KEEL BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,710 hrs · 56,754 cycles

DURING SCHEDULED C1 CHECK, FOUND SKIN CRACKED ON RT SIDE OF NLG WW AT BS 259, WL 174. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,725 hrs · 55,994 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 515, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,332 hrs · 63,264 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 947, STRINGER 4R, CRACKED. REPAIRED SKIN PER EA.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 57,821 hrs · 55,271 cycles

DURING SCHEDULED C3 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 1 DEF, LOOSE. SECURED EMERGENCY EXIT LIGHT LENS PER MM.

Part: LENS — MISSING (ROW 6C) · airframe 57,472 hrs · 54,982 cycles

BULLNOSE EMERGENCY EXIT LIGHT AT ROW 6C, MISSING. REPLACED LIGHT LENS PER MM.

Part: GLOWSTRIP — OUT OF POSITION (CABIN) · airframe 56,647 hrs · 54,327 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT GALLEY PHOTOLUMINESCENT EXIT STRIP OUT OF POSITION. REPOSITIONED PHOTOLUMINESCENT EXIT STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,646 hrs · 54,325 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 957, STRINGER 17L, CRACKED. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,646 hrs · 54,325 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 947, LBL 55.5, CRACKED. REPAIRED FLOORBEAM SECTION PER SRM.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 56,646 hrs · 54,325 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BELT FRAME AT BS 947.5, STRINGER 18L, CRACKED. REMOVED AND REPLACED BELT FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,646 hrs · 54,325 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 867, RT AFT CARGO COMPARTMENT TRACK TO FRAME CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 56,646 hrs · 54,325 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RADIAL STIFFENER AT BS 1016, BL 0, 6 O'CLOCK POS, CORRODED. REPAIRED STIFFENER PER EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,646 hrs · 54,325 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 996, STRINGER 27L, CORRODED. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,646 hrs · 54,325 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 27L, AT BS 996, CORRODED. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,646 hrs · 54,325 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L-1 DOOR CUTOUT FUSELAGE SKIN AFT UPPER SIDE CRACKED. REPAIRED SKIN PER EA.

Part: CLIP — CRACKED (FUSELAGE) · airframe 56,646 hrs · 54,325 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIPS AT BS 767, STRINGER 25L, BS 907, STRINGER 25R AND BS 727B, STRINGER 25R, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,646 hrs · 54,325 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 500D, STRINGER 26L, CORRODED. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,601 hrs · 52,629 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 10, STR 18R. REPAIRED SKIN PER SRM.

Part: PROXIMITY SENSOR — FAULTY (L/E FLAP) · airframe 54,601 hrs · 52,629 cycles

AIR TURNBACK, NR 2 L/E FLAP AMBER LIGHT AND L/E FLAP TRANSIT LIGHT REMAINED ILLUMINATED AFTER FLAP RETRACTION. REMOVED AND REPLACED UP PROXIMITY SENSOR PER MM.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 54,429 hrs · 52,484 cycles

DURING CLIMB-OUT RT MLG EXTENDED. CYCLED LANDING GEAR DOWN THEN UP. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM.

Part: VALVE — FAULTY (RT MLG) · airframe 54,429 hrs · 52,484 cycles

AFTER TAKEOFF GEAR RETRACTED NORMALLY, WHEN GEAR HANDLE PLACED FROM UP TO OFF, RT MLG EXTENDED (BOTH RED AND GREEN LIGHTS) RETRACTED GEAR AGAIN, GEAR RETRACTED NORMALLY. REMOVED AND REPLACED RT MLG PRIORITY MODULAR VALVE PER MM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 52,148 hrs · 50,641 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIP CRACKED AT BS 727B, STR 4L. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,148 hrs · 50,641 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW CUTOUT CRACKED AT RT WINDOW NR 28. REPAIRED CUTOUT PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 52,148 hrs · 50,641 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIP CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM.

Part: SKIN — CRACKED (AFT ENTRY DOOR) · airframe 52,083 hrs · 50,572 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR LOWER HINGE CUTOUT DOUBLER AND BEAR STRAP CRACKED. REPAIRED SKIN PER SWA EA AND SRM.

Part: LENS — MISSING (CABIN) · airframe 52,083 hrs · 50,572 cycles

DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW NR 7 ABC. INSTALLED LENS PER MM.

Part: TRACK — LOOSE (CABIN) · airframe 52,083 hrs · 50,572 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK LOOSE AT ROW NR 9. SECURED EEPLS PER MM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 51,213 hrs · 49,841 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,674 hrs · 49,420 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 25R, BETWEEN BS 932 AND 943. REPAIRED SKIN PER SRM.

Part: BUSHING — WORN (ELEVATORS) · airframe 50,673 hrs · 49,419 cycles

DURING SCHEDULED A2 CHECK, SWA SI 11111-55, LT AND RT ELEVATOR TAB LOCK OUT MECHANISMS HAVE EXCESSIVE PLAY AT FWD ATTACH POINTS. REMOVED AND REPLACED BOTH LT AND RT ELEVATOR LOCK OUT MECHANISM LINK BUSHINGS PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 50,673 hrs · 49,419 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 3 AND NR 4 RT ELEVATOR TAB HINGE BUSHINGS PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 50,292 hrs · 49,113 cycles

DURING SCHEDULED C3 CHECK, FOUND LT T/E OUTBOARD AFT FLAP DELAMINATED NEAR OUTBOARD END, UPPER AND LOWER SURFACES. REMOVED AND REPLACED T/E OUTBOARD AFT FLAP PER MM, ROUTED FLAP TO SHOP FOR REPAIR. REPAIRED FLAP PER SWA RA.

Part: WEB — CRACKED (NLG W/W) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CEILING PRESS PANEL CUTOUT CRACKED (1 INCH ) IN NOSE W/W AFT INBD CORNER. REPAIRED PANEL CUTOUT PER SWA T1-235-001.

Part: WEB — CRACKED (FUSELAGE) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BEADED FLOOR WEB CRACKED ( 2 EA ) AT BS 665, RBL 39.5 & LBL 39. REPAIRED WEB PER SWA RA 1-353-2644.

Part: CLIP — CRACKED (FUSELAGE) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294.5, STR 8L. R&R STR CLIP PER SRM.

Part: FRAME — CRACKED (AFT CARGO DOOR) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR FRAME CRACKED AT FWD LWR CORNER. REPAIRED DOOR FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: SLAT — CRACKED (WING) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED 1/2D CHECK, FOUND #5 L/E SLAT DOUBLER PATCH CRACKED ON THE OUTBD END. R & R DOUBLER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT LH OVERWING EMERGENCY EXIT, BS 616, WL 202. REPAIRED FRAME PER SWA T1-153-018.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 30 TO RBL 60. REPAIRED FLOORBEAM PER SWA T1-553-005.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 294, RBL 40 TO RBL 46. REPAIRED FLOORBEAM PER SRM.

Part: BRACKET — CORRODED (ENTRY DOOR) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR GIRT BAR, FWD AND AFT FLOOR ATTACH BRACKETS CORRODED. REMOVED AND REPLACED ATTACH BRACKETS PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED 1 INCH LONG AT BS 665, LBL 25. REPAIRED BEAM PER SWA RA 1-353-2650.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR LOWER FWD CUT OUT. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BL 0 TO RBL 15. REPAIRED FLOORBEAM PER SRM.

Part: CABLE — FRAYED (AFT ENTRY DOOR) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT ENTRY DOOR EVAC SLIDE CABLE FRAYED. R&R EVAC SLIDE CABLE PER MM.

Part: TEE CHORD — CRACKED (FUSELAGE) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED 1/2D CHECK, FOUND T-CHORD CRACKED AT BS 178, LBL 6 & WL 184. REMOVED AND REPLACED T-CHORD PER SWA ACO 7154-53.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED 1/2D CHECK, FOUND TIE CLIPS CRACKED (2 EA) AT BS 663, STR 10R & 10L. REMOVED AND REPLACED TIE CLIPS PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 2 FLOORBEAMS CORRODED AT BS 859, LBL 3 & RBL 14. REPAIRED FLOORBEAMS PER SWA 1-A53-2021.

Part: BEAM — CORRODED (FUSELAGE) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO BIN FLOOR BEAMS CORRODED ( 2 EA ) AT BS 859, LBL 12 & LBL 8. REPAIRED FLOOR BEAMS PER SWA RA 1-A53-2021.

Part: BEAM — CORRODED (FUSELAGE) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO BIN FLOOR BEAMS CORRODED ( 3 EA ) AT BS'S 795, 813 & 826, LBL3. REPAIRED FLOOR BEAMS PER SWA RA 1-A53-2021.

Part: WEB — CRACKED (FUSELAGE) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL BEAM WEBS CRACKED ( 2 EA ) AT BS 178, WL 230, RBL 17.1 & LBL 17.1. R&R VERTICAL BEAM WEBS PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STR CLIP CRACKED AT BS 1137, LH APU TORQUE BOX. R&R STR CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,496 hrs · 47,600 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED (3 INCHES LONG) AT BS 727C, STRINGER 18R. REPAIRED SKIN PER SRM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 47,628 hrs · 46,855 cycles

DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR TAB INBD HINGE BUSHING WORN. REMOVED AND REPLACED TAB INBD HINGE BUSHING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,602 hrs · 45,975 cycles

DURING SCHEDULED C3 CHECK, FOUND .1875 INCH EXTERNAL FUSELAGE SKIN CRACK AT AFT SVC DOOR UPPER CUTOUT. REPAIRED SKIN PER RA.

Part: RETAINER — LOOSE (ENTRY DOOR) · airframe 46,602 hrs · 45,975 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER LOOSE. REMOVED AND REPLACED RETAINER RIVETS PER SRM.

Part: SLIDE — LOOSE (GALLEY DOOR) · airframe 45,671 hrs · 45,184 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR GIRT ASSY PLAYOUT EXCESSIVE. ADJUSTED SLIDE ASSY PER MM.

Part: SLIDE — LOOSE (PAX DOOR) · airframe 45,671 hrs · 45,184 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR GIRT ASSY PLAYOUT EXCESSIVE. ADJUSTED SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 45,225 hrs · 44,773 cycles

AFT SERVICE DOOR EVACUATION SLIDE PARTIALLY OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 45,177 hrs · 44,738 cycles

AFT SERVICE DOOR EVACUATION SLIDE PARTIALLY FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 44,787 hrs · 44,381 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 44,005 hrs · 43,714 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING TRAILING EDGE I/B FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FORE FLAP ASSY PER MM.

Part: SKIN — CRACKED (BS 500A)

DURING SCHEDULED C3 CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED, BS 500A, STRINGER 10L. REPAIRED SKIN PER SRM.

Part: WINDOW — LEAKING (COCKPIT)

AIR TURNBACK- DURING CLIMB HEARD A LOUD PRESS LEAK NOISE FROM L1 WINDOW. RESEALED LT SIDE OF L1 WINDOW PER MM, LEAK CHECKED GOOD.

Part: ENGINE — BIRD STRIKE (NR 2)

ABORTED TAKEOFF, NR 2 ENG ENCOUNTERED BIRD STRIKE AND ABORTED THE TAKEOFF AT 110 KNOTS DUE TO VIBRATION ON THE ENG. REMOVED AND REPLACED NR 35 AND NR 36 DAMAGED FAN BLADES ON NR 2 ENG. ALSO, REMOVED AND REPLACED CSD OIL COOLER PER MM.

Part: T CAP — CRACKED (BS 663)

DURING SCHEDULED 1/4D CHECK, FOUND UPPER T CAP CRACKED AT BS 663, BL 0. REPAIRED T CAP PER ACO NR 658-57.

Part: TAB — DELAMINATION (LT AILERON)

DURING SCHEDULED BC4 CHECK, FOUND LT AILERON TAB DELAMINATED AT TRAILING EDGE I/B SIDE. REMOVED AND REPLACED TAB PER MM.

Part: SENSOR — OUT OF ADJUST (LT MLG)

AIR TURNBACK DUE TO LT MAIN LANDING GEAR WARNING LIGHT REMAINED ON AFTER RETRACTION. ADJUSTED LT MAIN GEAR UP PROX SENSOR PER MM.

Part: SWITCH — OUT OF POSITION (COCKPIT)

DURING CRUISE, SMELLED AND SAW WHITE SMOKE COMING FROM F/O NR 3 WINDOW AREA. SHUT OFF F/O'S FWD AND SIDE WINDOW HEAT SWITCHES, SMOKE STOPPED. ALSO, FOUND GALLEY C/B TRIPPED ON P18-3 PANEL ROW B. CHECKED UNDER P5 OVERHEAD PANEL, CHECKED ALL RT SIDE WINDOWS AND HEAT CONNECTORS, REPOSITIONED SWITCH ON NR R5 WINDOW, RELAMPED RT SIDE C/B. INSPECTED LIGHT WITH CORRECT BULB, ACC OPS CK NORMAL IAW M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED A1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT ROW NR 3 LT INOP. RELAMPED OPS CHECK NORMAL PER BOEING MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED A1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT ROW NR 5 RT INOP. RELAMPED OPS CHECK NORMAL PER BOEING MM.

Part: LIGHT — MALFUNCTIONED (CABIN)

DURING WALKAROUND INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS REMAINING ON DIM AFTER LIGHTS SWITCHED OFF. REPOWERED AND LIGHTS OPERATED NORMALLY.

Part: SKIN — CRACKED (BS 500-520)

DURING SCHEDULEDC4 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 500D AND 520 AT S12R. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 986-994)

DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 986 TO 994, WL 208. REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 927)

DURING SCHEDULED D-CHECK, FOUND UPPER ATTACH ANGLE ON SHEAR WEB CRACKED AT BS 927 TO 947. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 400-420/500)

DURING SCHEDULED D-CHECK, FOUND FLOOR TO SIDEWALL SUPPORT PLATE CORRODED AROUND NUTPLATE HOLES AT BS 500 TO 500A AND BS 420 TO 400. REPAIRED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD BS 178 PRESSURE WEB CRACKED AT RBL 4.7. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 834/331)

DURING SCHEDULED D-CHECK, FOUND FUSLAGE SKIN DENTED AT BS 834, RBL 8, BETWEEN S26 TO 27 AND AT BS 331 BETWEEN S21 AND 22. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 312, WL 208 AND AT BS 344, WL 208.1. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (SERV DOORWAY)

DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR LOWER AFT SKIN CUTOUT CRACKED AT BS 328, RBL 65, WL 210. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 SIDE CHORD LT AND RT SIDES CRACKED. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 907/400)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT HAT SECTION ANGLE AT BS 907, BETWEEN S9 AND 8L, AND AT BS 400, BETWEEN S9 AND 8L. REPAIRED PER BOEING SRM.

Part: CLIP — CRACKED (BS 500/663/908)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 663, S10R AT BS 500D, S19R AND AT BS 908, S4L. REPLACED PER BOEING SRM.

Part: STRINGER — DAMAGED (BS 335)

DURING SCHEDULED D-CHECK, FOUND STRINGER 8R DAMAGED AT BS 335. REPLACED DAMAGED SECTION PER BOEING SRM.

Part: SKIN — DENTED (BS 360-380)

DURING SCHEDULED D-CHECK, FOUND MULTIPLE FUSELAGE SKIN DENTS AT FROM BS 360 TO 380, BETWEEN S17 AND 19L. REPAIRED PER BOEING SRM.

Part: MOPSILL — CORRODED (BS 947-986)

DURING SCHEDULED D- CHECK, FOUND AFT GALLEY DOORWAY MOPSILL CORRODED FROM BS 947 TO 986 AND AT FWD SERVICE DOOR MOPSILL FROM BS 294 TO 338. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 368)

DURING SCHEDULED D-CHECK, FUSELAGE SKIN GOUGED AT BS 368, BELOW S4L. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 637)

DURING SCHEDULED D-CHECK, WEB CRACKED BELOW LEFT EMERGENCY EXIT CUTOUT AT BS 637. REPLACED PER BOEING SRM.

Part: CHANNEL — CORRODED (BS 727/772)

DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CHANNELS CORRODED AT BS 727D PLUS 5 AND AT 772, LBL 12.5, LBL 3, 8 , 12.5, 8.10. REPAIRED PER BOEING SRM.

Part: CASTING — CRACKED (FWD ENTRY)

DURING SCHEDULED C1 CHECK, FOUND CRACK IN UPPER FWD CORNER OF FWD ENTRY DOOR LOWER CAM PLATE SUPPORT CASTING. REPAIRED PER SWA RA 1-353-1331 AND BOEING STRUCTURAL REPAIR MANUAL.