N305SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,500 hrs · 69,842 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 905, STR 3L TO STR 4L. REMOVED AND REPLACED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,500 hrs · 69,842 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 905, STR 6L TO STR 7L. REMOVED AND REPLACED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,500 hrs · 69,842 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 74,235 hrs · 69,660 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 72,857 hrs · 68,642 cycles

DURING SCHEDULED 22Y CHECK, FOUND KEEL BEAM CHORD CORRODED BETWEEN BS 510D TO BS 540, RBL 6. REPAIRED CHORD PER SRM.

Part: FITTING — CRACKED (SPOILER ACTUATOR) · airframe 72,857 hrs · 68,642 cycles

DURING SCHEDULED 22Y CHECK, FOUND RIGHT WING NR 5 SPOILER INBOARD ACTUATOR FITTING WORN. REMOVED AND REPLACED FITTING PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,857 hrs · 68,642 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, RBL 11 TO RBL 13. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 72,857 hrs · 68,642 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING L/E NR 3 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 72,857 hrs · 68,642 cycles

DURING SCHEDULED 22Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 7 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 72,857 hrs · 68,642 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD CARGO DOOR FWD UPPER SKIN CRACKED. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (L/E SLAT) · airframe 72,857 hrs · 68,642 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING 36 L/E SLAT UPPER SURFACE DELAMINATED. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,857 hrs · 68,642 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 72,857 hrs · 68,642 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 72,857 hrs · 68,642 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 328 AND BS 344, STR 17R. REMOVED AND REPLACED CREASE BEAM PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 72,857 hrs · 68,642 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 72,857 hrs · 68,642 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 952 AND BS 990, STR 17R. REMOVED AND REPLACED CREASE BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 72,857 hrs · 68,642 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 5 TO RBL 46. REPAIRED FLOORBEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,857 hrs · 68,642 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 270, STR 16R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,857 hrs · 68,642 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 72,857 hrs · 68,642 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 72,857 hrs · 68,642 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,857 hrs · 68,642 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,857 hrs · 68,642 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 204, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,857 hrs · 68,642 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: MECHANISM — OUT OF ADJUST (R2 WINDOW) · airframe 72,857 hrs · 68,642 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLIGHT DECK R2 WINDOW EXTERNAL RELEASE HANDLE WILL NOT UNLOCK WINDOW. ADJUSTED RELEASE HANDLE MECHANISM PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 72,647 hrs · 68,485 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD FOREFLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,647 hrs · 68,485 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 346, STR 2L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 72,647 hrs · 68,485 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED FLAP PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,402 hrs · 68,304 cycles

DURING SCHEDULED A2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (BS 259 S19L) · airframe 71,890 hrs · 67,906 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259.5, STR 19L. REPAIRED SKIN PER SRM.

Part: CASTING — CRACKED (RT WING SPOILER) · airframe 71,675 hrs · 67,739 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD GROUND SPOILER OUTBOARD CASTING CRACKED. REMOVED AND REPLACED SPOILER PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,670 hrs · 67,734 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,512 hrs · 67,609 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FRAME — CORRODED (BS 360 S28L) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 360, STR 28L. REPAIRED FRAME PER ER.

Part: SHEAR TIE — CORRODED (BS 380 S27L) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 380, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 304) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT BS 304, WL 257. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 304) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT BS 304, WL 257. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (BS 540 S27R) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 540, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 27L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 502C, STR 20L. REPAIRED STRINGER PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER FITTING CRACKED AT BS 727, STR 24L. REMOVED AND REPLACED STR FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (BS 767 S16R) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 15R CRACKED AT BS 489. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (BS 400 S16R) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 16R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (BS 520 S16L) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 16L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 747 S13R) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 13R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 807 S18L) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 18L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 747 S18R) · airframe 69,795 hrs · 66,264 cycles

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

Part: FRAME — CRACKED (BS 380 S13R) · airframe 69,795 hrs · 66,264 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727B S7R) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, BETWEEN STR 13R & STR 14R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 13R. REPAIRED FRAME PER SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 17R CRACKED AT BS 810.5. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 16R CRACKED AT BS 401. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 973, STR 5R. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 25R CRACKED AT BS 945. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 947, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 9R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 985, STR 21R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (BS 908 S15R) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 908, STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 947, STR 24R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 968, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 727D S9R) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 9R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 986 S27L) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 986, STR 27L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500C S9R) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 9R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 502D, STR 16L. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (BS 440 S9LR) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 9L AND STR 9R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 927, STR 24L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 951, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 400 S9L) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 9L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 559 S9L) · airframe 69,765 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 9L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 787 S18R) · airframe 69,795 hrs · 66,264 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 18R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (BS 503 S8R) · airframe 70,365 hrs · 66,746 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 8R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 506D S7R) · airframe 70,365 hrs · 66,746 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506D, STR 7R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 706 S10L) · airframe 70,365 hrs · 66,746 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 706, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 68,735 hrs · 65,482 cycles

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

Part: SKIN — CRACKED (BS 907 S20L) · airframe 68,743 hrs · 65,482 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 907, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 937 S23L) · airframe 68,743 hrs · 65,482 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 937, STR 23L. REPAIRED SKIN PER SRM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 68,743 hrs · 65,482 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 7 ABC. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: SKIN — CRACKED (BS 516 S16R) · airframe 68,477 hrs · 365,266 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 516, STR 16R. REPAIRED SKIN PER SRM.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 68,436 hrs · 65,226 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT MLG SIDE STRUT SUPPORT FITTING LUG CORRODED AT RT BS 685. REPAIRED FITTING PER SWA EA.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 68,436 hrs · 65,226 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT MLG SIDE STRUT SUPPORT FITTING LUG CORRODED AT LT BS 685. REPAIRED FITTING PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,436 hrs · 65,226 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 67,803 hrs · 64,717 cycles

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

Part: SKIN — CRACKED (BS 413 S16L) · airframe 67,371 hrs · 64,385 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 413, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 434 S16R) · airframe 67,371 hrs · 64,385 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 434, STR 16R. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (BS 455) · airframe 66,881 hrs · 64,001 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 455, STR 16L. MX FERRY TO DAL FOR REPAIRS. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 270) · airframe 66,881 hrs · 64,001 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 270, STR 15R. MX FERRY TO DAL FOR REPAIRS. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 512B) · airframe 66,881 hrs · 64,001 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 512B, STR 16L. MX FERRY TO DAL FOR REPAIRS. REPAIRED SKIN PER SWA EA.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 66,881 hrs · 64,001 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS STRIP COVER MISSING AT ROW 8 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: TAB — CRACKED (RT ELEVATOR) · airframe 66,881 hrs · 64,001 cycles

DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR TAB CRACKED AT NR 2 HINGE CUTOUT. REMOVED AND REPLACED TAB PER MM.

Part: SKIN — CRACKED (BS 266) · airframe 66,881 hrs · 64,001 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 266, STR 9L. MX FERRY TO DAL FOR REPAIRS. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 420) · airframe 66,460 hrs · 63,670 cycles

DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 420, STR 17R. REPAIRED SKIN PER SWA EA.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 66,156 hrs · 63,434 cycles

EMERGENCY EXIT BULLNOSE LIGHT COVER MISSING AT ROW 18. INSTALLED COVER PER MM.

Part: LENS — LOOSE (CABIN) · airframe 65,927 hrs · 63,272 cycles

DURING SCHEDULED C3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: FRAME — CRACKED (BS 500C) · airframe 65,463 hrs · 62,931 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, BETWEEN STR 19R TO STR 20R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (BS 404) · airframe 65,463 hrs · 62,931 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 404, STR 17R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 700) · airframe 65,463 hrs · 62,931 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 700, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 390) · airframe 65,463 hrs · 62,931 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 390, STR 17R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 500D) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 12R. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CORRODED (BS 767) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, BETWEEN LBL 7 TO LBL 13. REPAIRED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT DOME CAP, 1 O'CLOCK POSITION. REPAIRED WEB PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 433) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 433, STR 16L. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (BS 662) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 662, RBL 24.75. REPAIRED FLOORBEAM PER SWA EA.

Part: STRINGER — CORRODED (BS 737) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 767, STR 25L. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (BS 348) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 348.2, STR 17L. REPAIRED FRAME WEB PER SRM.

Part: SKIN — CRACKED (BS 773) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 773, STR 14L. REPAIRED SKIN PER SWA EA.

Part: FLOOR SUPPORT — CORRODED (BS 859-867) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CORRODED BETWEEN BS 859 TO BS 867, LBL 8.0. REPAIRED FLOORBEAM PER SWA EA.

Part: SHEAR TIE — CORRODED (BS 767) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, RBL 6. REPAIRED SHEAR TIE PER SRM.

Part: FLOOR SUPPORT — CORRODED (BS 859-867) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CORRODED BETWEEN BS 859 TO BS 867, LBL 12.0. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOOR SUPPORT — CORRODED (BS 859-867) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CORRODED BETWEEN BS 859 TO BS 867, LBL 3.0. REPAIRED FLOORBEAM PER SWA EA.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULLNOSE EMERGENCY LIGHT LENS LOOSE AT ROW 10 ABC. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (BS 950) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 950, STR 10R. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT DOME CAP, 2 O'CLOCK AND 4 O'CLOCK POSITIONS. REPAIRED WEB PER SWA EA.

Part: STRINGER — CRACKED (BS 409) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 409, STR 17R. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (BS 500D) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 12L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 259.5) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259.5, WL 210, LT SIDE. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 727D) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19L. REPAIRED SKIN PER SWA EA.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CENTER CABIN EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (BS 426.25) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 426.25, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 500A) · airframe 65,463 hrs · 62,921 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, STR 16L. REPAIRED SKIN PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 64,968 hrs · 62,534 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE KEEL BEAM CORRODED AT BS 536, LBL 6.5. REPAIRED KEEL BEAM PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 64,968 hrs · 62,534 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,732 hrs · 62,345 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 311, STR 20R. MX FERRY TO PHX, REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,349 hrs · 62,051 cycles

DURING WALK AROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 480 TO BS 500, STR 16L. REPAIRED SKIN PER SWA EA & SRM.

Part: TIRE — SEPARATED (LT MLG) · airframe 64,164 hrs · 61,907 cycles

DURING POST FLIGHT INSPECTION, FOUND LT MLG TIRE TREAD SEPARATED & AFT T/E FLAP DAMAGE. REMOVED AND REPLACED MLG TIRE ASSY & LT INBOARD AFT T/E FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,059 hrs · 61,831 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 402, STR 16R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,059 hrs · 61,831 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500 + 13, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,162 hrs · 61,160 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 500A,STRINGER 16R, CRACKED. REPAIRED SKIN PER EA.

Part: GLOWSTRIP — WORN (CABIN) · airframe 63,131 hrs · 61,126 cycles

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT PHOTOLUMINESCENT STRIP AT ROW 8 ABC, WORN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: SLIDE — OUT OF ADJUST (R1 & L1 DOORS) · airframe 63,131 hrs · 61,126 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 AND L1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED BOTH R1 AND L1 DOOR EVAC SLIDES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,875 hrs · 60,931 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 454, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,230 hrs · 60,413 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 430, STRINGER 17R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,150 hrs · 60,348 cycles

DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 749, STRINGER 19R, BS 800, STRINGER 18R. REPAIRED SKIN SECTIONS PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,142 hrs · 60,338 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C+16, ABOVE STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,785 hrs · 60,030 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 270, STRINGER 14L, CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 61,711 hrs · 59,964 cycles

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

Part: LENS — MISSING (CABIN) · airframe 60,392 hrs · 58,907 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT SIGN MISSING LENS. INSTALLED EMERGENCY EXIT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,392 hrs · 58,907 cycles

DURING SCHEDULED C1 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS AT BS 425, BS 452, STRINGER 16R, AND BS 390, STRINGER 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,392 hrs · 58,907 cycles

DURING SCHEDULED C1 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 470, STRINGER 17R, BS 500D, STRINGER 16L. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,392 hrs · 58,907 cycles

DURING SCHEDULED C1 CHECK, FOUND FLOORBEAM WEB AT BS 967, LBL 5, WL 208, CORRODED. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,344 hrs · 57,251 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED (4 EA) BS 500D, BETWEEN STR 15R AND STR 16R, BS 395 ABOVE STR 15L, BS 773 AT STR 19L AND BS 805 AT STR 19L. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663.75, BETWEEN STR 2L AND 3R. REPAIRED FRAME PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 947.5 AT STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C, ABOVE STR 15L. REPAIRED SKIN AT PAE DURING D-CHECK PER BFG ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 20L. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN BULGING AT BS 500 + 10, STR 28R. REPAIRED SKIN PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND FLOOR SUPPORT CORRODED BETWEEN BS 1006 AND BS 1016, BETWEEN LBL 5 AND LBL 10, WL 208. REPAIRED FLOOR SUPPORT PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CORRODED BETWEEN BS 807 AND BS 815, STR 26R. REMOVED AND REPLACED CORRODED SECTION OF STRINGER PER SRM.

Part: STRUCTURE — CORRODED (AFT CABIN) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND UPPER TEE STRUCTURE CORRODED AT BS 1016, WL 208, BETWEEN LBL 5 AND LBL 28. REPAIRED TEE STRUCTURE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT STR 26R, BS 787 AND BS 792. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: DRAG ANGLE — CORRODED (VERTICAL FIN) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL FIN ATTACH CLEVIS DRAG ANGLES CORRODED LT SIDE (2 EA). REMOVED AND REPLACED VERTICAL FIN DRAG ANGLES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) BETWEEN STR 8R AND STR 9R, BS 480 AND BS 847. REPAIRED FRAMES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (3 EA) BETWEEN STR 8L AND STR 9L, BS 727E, BS 807 AND BS 847. REPAIRED FRAMES PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,939 hrs · 50,925 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CORRODED AT BS 500 + 15, STR 26R. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CORRODED AT BS 767, WL148, RBL 15. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, BETWEEN STR 8L AT STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR 8L AND STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, BETWEEN STR 8R AND STR 9R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500C, BETWEEN STR 26L AND STR 27L. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIES CORRODED (2 EA) AT BS 747, WL 148, RBL 10 AND BS 847, WL 148, BL 0. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, BETWEEN STR 7L AND STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 13R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CORRODED AT BS 500C, STR 24R. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT STR 7L, BS 727B AND BS 727D. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER TIE CLIPS CRACKED (4 EA) BS 616 AT STR 5R, BS 727 AT STR 7L, BS 727C AT STR 4R AND BS 727E AT STR 5L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND RT OUTBD LOWER VERTICAL BEAM CRACKED AT BS 188, WL 203 TO WL 214 AT RBL 30. REPAIRED VERTICAL BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, WL 14 AND RBL 9. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 178, WL 232. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED D CHECK, FOUND 2 EA STRINGER CLIPS CRACKED, STRINGER 5R, BS 727B AND BS 727E. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,482 hrs · 56,584 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 475, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,482 hrs · 56,584 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (5 EA) ABOVE STR 10R, AT BS 445, BS 470, BS 500, BS 500A AND BS 500B. REPAIRED SKIN PER SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 57,030 hrs · 56,247 cycles

DURING SCHEDULED RON, FOUND EEPLS INOP AT ROWS 9, 7 AND 11. REMOVED AND REPLACED BATTERY CHARGER AND BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,967 hrs · 56,198 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: TRUNNION PIN — CORRODED (LT & RT MLG) · airframe 56,906 hrs · 56,150 cycles

DURING SCHEDULED A2 CHECK, SWA SI 11251-32, FOUND BOTH LT AND RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT AND RT MLG TRUNNION PINS PER MM.

Part: ARM — CORRODED (LT/RT MLG) · airframe 56,906 hrs · 56,150 cycles

DURING SCHEDULED A2 CHECK, SWA SI 11251-32, FOUND BOTH LT/RT MLG CLEVIS BEAM ARMS CORRODED. REMOVED AND REPLACED BOTH LT/RT MLG CLEVIS BEAM ARMS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 53,539 hrs · 55,856 cycles

DURING SCHEDULED C1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,484 hrs · 55,807 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW CUTOUTS CRACKED AT RT WINDOWS NR 29 AND NR 35. REPAIRED SKIN PER BFG ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,484 hrs · 55,807 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 769, STR 10R. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,484 hrs · 55,807 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY EXIT LIGHTS AT ROW NR 7, NR 9, NR 11, NR 19 AND NR 20 LT INOP. REMOVED AND REPLACED BATTERY (M1135) PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,483 hrs · 55,806 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW CUTOUTS CRACKED AT WINDOWS NR 12, NR 30, NR 32 AND NR 33. REPAIRED SKIN PER BFG ER & SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,483 hrs · 55,806 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 360, STRINGER 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,483 hrs · 55,806 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIPS CRACKED (2 EA) AT STR 4L, BS 400 AND BS 420. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,483 hrs · 55,806 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT BS 767, STR 13R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,483 hrs · 55,806 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L AND STR 15L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — BROKEN (FUSELAGE) · airframe 56,483 hrs · 55,806 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME BROKEN AT BS 767, STR 13R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,483 hrs · 55,806 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 13L AND STR 14L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 55,694 hrs · 55,146 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 967, BL O. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,684 hrs · 55,139 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,601 hrs · 55,073 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (3 EA) 1.5 LONG AT STR 10R, BS 382, BS 500 PLUS 5 AND BS 500 PLUS 13. REPAIRED SKIN PER SWA RA AND SRM.

Part: COVER — LOOSE (CABIN) · airframe 55,487 hrs · 54,984 cycles

OVERHEAD EMERGENCY EXIT LIGHT COVER LOOSE AT OVERWING EXIT'S. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,834 hrs · 54,431 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, ABOVE STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,269 hrs · 53,960 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 18L BETWEEN BS 779 AND BS 794, AND STR 20R BETWEEN BS 772 AND BS 785. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,979 hrs · 53,729 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 937, STR 22R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,979 hrs · 53,729 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT BS 500C, STR 10R, BS 500D, STR 4L AND BS 500C, STR 4L. REPAIREDSKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,979 hrs · 53,729 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 390, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,451 hrs · 53,311 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED ( 3 EA ) AT STRINGER 16R, BS 445,BS 465 AND BS 535. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,451 hrs · 53,311 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 752, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,451 hrs · 53,311 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 23R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,108 hrs · 53,040 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT SIDE CHORD CRACKED AT BS 210. REMOVED AND REPLACED CHORD PER SWA ACO 7342-53.

Part: TAB — DELAMINATED (LH AILERON) · airframe 53,108 hrs · 53,040 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LH AILERON TAB DELAMINATED AT T/E. R&R TAB PER MM.

Part: SKIN — CRACKED (FWD SVC DOOR) · airframe 53,108 hrs · 53,040 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SVC DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM & SWA RA 1-353-2681.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,108 hrs · 53,040 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT RH WINDOW'S JUST BELOW STR 11L, BS 384, 424, 444, 484, 500, 500A & 500B. REPAIRED SKIN PER SWA RA 1-353-2685.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,108 hrs · 53,040 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 460, STR 17B. REPAIRED STRINGER PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,108 hrs · 53,040 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 663, BL 0. REPAIRED FLOORBEAM PER SWA RA 1-357-1116.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,108 hrs · 53,040 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 767 TO 787, RBL 3. REPAIRED FLOORBEAM PER SWA RA 1-A53-2021.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,108 hrs · 53,040 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED 1.75 INCHES LONG AT BS 727D+6, ABOVE STR 20L. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 53,108 hrs · 53,040 cycles

DURING SCHEDULED 1/4D CHECK, FOUND WEB CRACKED AT BS 178, RBL 5, WL 212. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,108 hrs · 53,040 cycles

DURING SCHEDULED 142D CHECK, FOUND FWD SVC DOOR CUT OUT LWR STUB FRAME CRACKED AT BS 294.5. REPAIRED FRAME PER SRM.

Part: WEB — CRACKED (RH W/W) · airframe 53,108 hrs · 53,040 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED AT BS 663, RBL 42. REPAIRED WEB PER SWA TI-353-032.

Part: WEB — CRACKED (AFT CARGO) · airframe 53,108 hrs · 53,040 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM WEB CRACKED AT BS 727B. R&R WEB PER SRM.

Part: FRAME — CRACKED (FWD SVC DOOR) · airframe 53,108 hrs · 53,040 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR FWD CUTOUT FRAME CRACKED AT # 3 DOOR STOP. REPAIRED FRAME PER SWA T1-152-003.

Part: WEB — CRACKED (MAIN WHEEL WELL) · airframe 53,108 hrs · 53,040 cycles

DURING SCHEDULED 1/4 D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, LBL 32. REPAIRED WEB PER SWA T1-353-046.

Part: FRAME — CRACKED (RT PYLON) · airframe 52,704 hrs · 52,698 cycles

DURING SCHEDULED A1 CHECK, FOUND NR 2 ENG PYLON STRUT AFT INBOARD CHORD CRACKED, NAC STA 354. REPAIRED CHORD PER SWA RA 1-354-0388.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 52,570 hrs · 52,577 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,129 hrs · 52,188 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 480, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,129 hrs · 52,188 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,129 hrs · 52,188 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 20R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,129 hrs · 52,188 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 420, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,913 hrs · 51,997 cycles

DURING SCHEDULED RON CHECK, FOUND FUSE SKIN CRACKED BETWEEN BS 360 & BS 380, JUST ABOVE STR 15L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,811 hrs · 51,910 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 455, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,193 hrs · 51,377 cycles

DURING SCHEDULED C3 CHECK, FOUND 3 EXTERNAL FUSELAGE SKIN CRACKS AT STR 20L, BS 747, 1.5 LONG, BS 787+5, 2.25 LONG & BS 787+13, 2.5 LONG. REPAIRED SKIN PER SRM.

Part: CAP — MISSING (CABIN) · airframe 51,193 hrs · 51,377 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS FWD END CAP MISSING. INSTALLED END CAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,193 hrs · 51,377 cycles

DURING SCHEDULED C3 CHECK, FOUND 3 EXTERNAL FUSELAGE SKIN CRACK AT BS 480, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 51,193 hrs · 51,377 cycles

DURING SCHEDULED C3 CHECK, FOUND .75 INCH LONG RT HORIZ STAB LOWER SKIN CRACK AT AFT SPAR, 64 OUTBOARD OF FUSELAGE. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,215 hrs · 50,583 cycles

DURING SCHEDULED C2 CHECK, FOUND 3 EA. EXTERNAL FUSELAGE SKIN CRACKS AT STR 10R, BS 500D, STR 4L, BS 480 & STR 4L, BS 500B. REPAIRED SKIN PER SRM.

Part: CAP — MISSING (CABIN) · airframe 50,215 hrs · 50,583 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD EEPLS END CAP MISSING. REPLACED END CAP PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 49,673 hrs · 50,130 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKS AT LBL 5.7, WL 184 & BL 0, WL 186. REPAIRED BULKHEAD PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 49,300 hrs · 49,833 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS LOOSE AT FWD SECTION. SECURED LIGHT TRACK ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,191 hrs · 49,734 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 CRACKS AT FUSELAGE SKIN, BS 927 - 947, STRINGER 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,906 hrs · 49,497 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, STRINGER 15L, BS 520 AND STRINGER 15R, BS 500A. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 48,459 hrs · 49,123 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NR 1, 2, 3 L/E SLATS DELAMINATED. REMOVED AND REPLACED L/E SLATS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 48,105 hrs · 48,828 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (BS 740)

DURING SCHEDULED RON, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 740, STRINGER 18L, AND BS 500B, STRINGER 16R. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (ROW 16)

DURING SCHEDULED C3 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LOOSE AT ROW 16 DEF. RESECURED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (BS 767 - 787)

DURING SCHEDULED RON, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 767-787, STRINGER 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 787 & 480)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 787, STRINGER 19L AND BS 480, STRINGER 10R. REPAIRED FUSELAGE SKIN PER SRM.

Part: SLIDE ASSY — RING PULLED (FWD SERVC DOOR)

DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT BAR CHAIN ATTACH RING PULLED APPART. REMOVED AND REPLACED SLIDE ASSY.

Part: SKIN — CRACKED (BS 807)

DURING SCHEDULED RON, FOUND FUSELAGE EXTERNAL SKIN CRACKED APPROX BS 807, STRINGER 10R. REPAIRED SKIN PER SRM.

Part: SLIDE — DETACHED (SERVICE DOORWAY)

DURING SCHEDULED RON, FOUND FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: FUEL OIL COOLER — FAILED (NR 1 ENGINE)

DECLARED EMERGENCY WHEN NR 1 ENG OIL TEMP LIGHT ILLUMINATED WITH ENGINE RETARDED TO IDLE. REMOVED AND REPLACED NR 1 ENG FUEL OIL HEAT EXCHANGER PER MM.

Part: FLOORBEAM — CORRODED (BS 987)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM, BS 987, LBL 40 - 43, INSIDE CABIN. REPAIRED BEAM PER EO 99-5313.

Part: FRAME — CORRODED (BS 1016)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FRAME AT BS 1016, WL 192, RT SIDE. REPAIRED FRAME PER EO 99-532P.

Part: FLOORBEAM — CORRODED (BS 947)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM AROUND FASTENER HOLES AT BS 947, LBL 5-RBL 5. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (BS 328)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FRAME AT BS 328 , WL 184. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (BS 986)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FRAME AT BS 986 , WL 208. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM, BS 312,LBL 14 - RBL 14, INSIDE CABIN. REPAIRED PER SRM.

Part: SKIN — CRACKED (BS 717)

DURING SCHEDULED 1/2D CHECK, FOUND KEEL BEAM LOWER SKIN CUT OUT AT BS 717 CRACKED. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND 4 EA CRACKS AT BS 178 BULKHEAD, BETWEEN LBL 10 - RBL 13. REPAIRED CRACKS PER SRM.

Part: FLOORBEAM — CORRODED (BS 294.5)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM, BS 294.5, LBL 14-RBL 11. REPAIRED BEAM PER SRM.

Part: BRACKET — CORRODED (PAX DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY GIRT BAR ATTACH BRACKET CORRODED AT FLOOR. REMOVED AND REPLACED BRACKET PER MM.

Part: SKIN — CRACKED (BS 500)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 8 INCHES LONG AT BS 500C, STRINGER 3L. REPAIRED PER SRM.

Part: SKIN — CRACKED (BS 745)

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 745, BETWEEN S19 AND 20L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING WALKAROUND CHECK, FOUND APPROX 4 INCHES SKIN CRACKED, LEFT SIDE BETWEEN CABIN WINDOWS 11 AND 12. REPAIRED PER BOEING SRM.

Part: END CAP — MISSING (CABIN)

DURING SCHEDULED CI CHECK, FOUND EMERGENCY EXIT TRACK LIGHTING FWD END CAP MISSING. INSTALLED MISSING EGRESS LIGHTING END CAP AT FWD END PER BOEING MM.

Part: WEB — CRACKED (NLG WW)

DURING SCHEDULED CI CHECK, FOUND NOSE GEAR ACTUATOR VERTICAL WEB ATTACH CRACKED 2 LONG, 6 IN FROM FWD END. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (NLG WW)

DURING SCHEDULED CI CHECK, FOUND UPPER WEB CRACKED AT NUT PLATE HOLE RIVET RT AND LT. REPAIRED PER BOEING TI-A53-001.

Part: SKIN — CRACKED (FUSELAGE)

DURING WALKAROUND CHECK, FOUND A 3 INCH CRACK LT SIDE BETWEEN CABIN WINDOWS 8 AND 9. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED B/C2 CHECK, FOUND AFT SERVICE DOORWAY HINGE CUTOUT CRACKED IN UPPER AND LOWER RADIUS. REPAIRED PER SWA RA 1-353-1717.

Part: STRINGER — CRACKED (BS 294.5)

DURING SCHEDULED SERVICE CHECK, FOUND STRINGER 25R CRACKED AT BS 294.5. REPLACED PER BOEING M/M.

Part: SKIN — DAMAGED (FUSELAGE)

GROUND EQUIPMENT CONTACTED RIGHT SIDE OF AIRCRAFT JUST BEHIND AND ABOVE RIGHT NOSE GEAR DOOR. REPAIRED SKIN PER BOEING SRM.

Part: SKIN — DAMAGE (FUSELAGE)

FUSELAGE SKIN DAMAGED BY GROUND EQUIPMENT BELOW AFT CARGO BIN DOOR. TEMP REPAIRED FOR MX FERRY FLIGHT TO TRAMCO AT SEA. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 727)

DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 727D PLUS 5, WL 156, RBL 6. REPLACED CORRODED SECTION PER BOEING SRM.

Part: SKIN — GOUGED (BS 967)

DURING SCHEDULED BC1 CHECK, FOUND FUSELAGE SKIN REPAIR DOUBLER BELOW AFT ENTRY DOOR GOUGED AT BS 967. REPLACED PER SWA RA 1-353-1510.

Part: SKIN — CRACKED (FWD SERV DOOR)

DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR SKIN CRACKED AT TOP AFT CORNER AT UPPER RIVET. REPAIRED PER BOEING SRM.

Part: RELAY — MALFUNCTIONED (NR 1 BUSS)

EN ROUTE, NUMBER 1 TRANSFER BUSS CIRCUIT BREAKER TRIPPED. RESET BREAKER, BUT TRIPPED AGAIN. CABIN PRESSURE BEGAN TO CLIMB IN AUTO. AIRCRAFT DESCENDED TO 10,000, DIVERTED TO DAL AND MADE AN UNEVENTFUL LANDING. INSPECTED, REPLACED R3 RELAY AND PERFORMED BUSS TRANSFER CHECK.