N676SW

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,940 hrs · 62,639 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FRAME CRACKED AT BS 947, STR 21R. REPAIRED FRAME PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,399 hrs · 62,209 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 504B, STR 16L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,399 hrs · 62,209 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 514C, STR 8R. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,399 hrs · 62,209 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 504A, STR 17L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,399 hrs · 62,209 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 494, STR 17L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,399 hrs · 62,209 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 730E, STR 18R. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,913 hrs · 61,839 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 454, STR 16R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOORBEAM T-CAP CORRODED AT BS 986, RBL 42. REPAIRED BEAM PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4R. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 10R TO STR 21R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED CLIP PER SI AND ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4R. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 976, STR 22L. REPAIRED SKIN PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6R. REMOVED AND REPLACED CLIP PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 380, STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: SPAR — CORRODED (RT WING) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT WING FRONT SPAR WEB CORRODED AT UPPER INBOARD BOLT COMMON TO NR 2 FUEL TANK FWD BOOST PUMP. REPAIRED SPAR WEB PER ER AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 922, STR 25R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, RBL 10. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,635 hrs · 61,639 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 516C, STR 14R. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 914, STR 23L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500, STR 13L TO STR 14L. REPAIRED FRAME PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 508D, STR 14R. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,355 hrs · 57,649 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: LIGHT — DAMAGED (CABIN) · airframe 74,580 hrs · 61,601 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT EEPLS DAMAGED. REMOVED AND REPLACED EEPLS PER DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,541 hrs · 61,572 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,604 hrs · 36,239 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,604 hrs · 36,239 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 74,541 hrs · 61,572 cycles

DURING SCHEDULED SPV CHECK, FOUND OVERHEAD EMERGENCY EXIT SIGN BETWEEN L1 DOOR AND FWD GALLEY INOP. CHARGED BATTERY PACK PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,388 hrs · 61,451 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER CRACKED AT BS 942, STR 23R. REPAIRED STRINGER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 74,388 hrs · 61,451 cycles

DURING SCHEDULED MV2 CHECK, FOUND FRAME LOWER FITTING LUG BORE CORRODED AT BS 685 RT. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,388 hrs · 61,451 cycles

DURING SCHEDULED MV2 CHECK, FOUND FRAME LOWER FITTING LUG BORE CORRODED AT BS 685 LT. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,550 hrs · 60,824 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 505C TO BS 516C, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,550 hrs · 60,824 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BS 492, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,550 hrs · 60,824 cycles

DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 14L. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,550 hrs · 60,824 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 501D TO BS 505D, BETWEEN STR 12L TO STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,550 hrs · 60,824 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BS 480.5, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SENSOR — OUT OF ADJUST (RT MLG) · airframe 73,550 hrs · 60,824 cycles

AFTER GEAR RETRACTION, GEAR HANDLE MOVED TO OFF POSITION AND L & R GEAR INDICATED RED & GREEN. NOSE GEAR INDICATED NORMAL. CYCLED GEAR, OPERATED NORMALLY. ADJUSTED AIR SAFETY/GROUND SENSOR S106.

Part: LENS — CRACKED (CABIN) · airframe 73,127 hrs · 60,517 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EMERGENCY EXIT SIDEWALL LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 73,127 hrs · 60,517 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: STRIP — WORN (CABIN) · airframe 73,127 hrs · 60,517 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP WORN BETWEEN ROW 16 TO ROW 21. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 73,127 hrs · 60,517 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT PER MM.

Part: STRIP — WORN (CABIN) · airframe 73,127 hrs · 60,517 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP WORN BETWEEN ROW 12 TO ROW 14. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,127 hrs · 60,517 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 769, STR 18L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,588 hrs · 60,140 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,588 hrs · 60,140 cycles

DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 2 TO ROW 5. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,204 hrs · 59,853 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER CRACKED AT BS 500C, STR 16R. REPAIRED STRINGER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,204 hrs · 59,853 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500C, STR 14R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,503 hrs · 58,586 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 976, STR 22L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,503 hrs · 58,586 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 976, STR 22L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,874 hrs · 58,147 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 312 AND BS 317, STR 18R AND STR 20R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,874 hrs · 58,147 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, BETWEEN STR 16R AND STR 17R. REPAIRED SKIN PER SWA EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 69,846 hrs · 58,125 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 69,829 hrs · 58,110 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,467 hrs · 57,842 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 69,087 hrs · 57,548 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 69,048 hrs · 57,515 cycles

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

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 68,815 hrs · 57,339 cycles

DURING SCHEDULED MV2 CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, LBL 33 TO LBL 36. REPAIRED PRESSURE WEB PER SWA EA.

Part: HINGE FITTING — BROKEN (NR 2 SPOILER) · airframe 68,815 hrs · 57,339 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 2 GROUND SPOILER INBOARD HINGE FITTING BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: ENGINE — FAILED (RIGHT) · airframe 68,747 hrs · 57,281 cycles

AIR TURNBACK / DECLARED EMERGENCY. IN FLIGHT SHUTDOWN EN ROUTE AT ABOUT 25,000 FT, AIRCRAFT BEGAN VIBRATING THEN HEARD EXPLOSION. SECURED NR 2 ENGINE. NR 2 ENGINE REPLACEMENT IN PROGRESS PER MM.

Part: FRAME — CRACKED (BS 291 S16R) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 291, STR 16R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 706 S8L/R) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CRACKED (BS 500D S28R) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND L1 WINDOW UPPER FRAME CRACKED AT OUTBOARD END. REPAIRED FRAME PER SRM.

Part: KEELBEAM — CORRODED (BS 500D S28R) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND KEEL BEAM CHORD CORRODED AT BS 500D, STR 28R. REPAIRED CHORD PER SRM.

Part: SHEAR TIE — CRACKED (BS 520 S27R) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 907 S8R) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (BS 517D S12R) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 517D, STR 12R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 406) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 406, RBL 3. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 783 S18L) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 783, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 426-446) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BETWEEN BS 426 AND BS 446, LBL 3 AND BL 0. REPAIRED SKIN PER ER.

Part: FRAME — CORRODED (BS 767 S27R) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, STR 27R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706 S5L) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 727E S8L/R) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (BS 783 S18L) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 783, STR 18L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FRAME — CRACKED (BS 727E S8L/R) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 804, STR 19L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 27R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 787 S13R) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 13R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 360 S8L) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 597 S8L) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500A S8L) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER — CORRODED (BS 947 S26L) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER 26L CORRODED AT BS 947. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 440 S8R) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 767 S8R) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (BS 827 S27L) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727B S3L) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 597 S7R) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727B S5L) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 578 S8L) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S6L) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727B S7L) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663 S10R) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR CENTER SKIN CRACKED AT LOWER END. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (BS 794 S26R) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 794, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CORRODED (BS 1006 S27L) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 1006, STR 27L. REPAIRED SKIN PER SRM.

Part: SKIN — CORRODED (BS 947) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 947, RBL 6. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706 S11R) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 294 S14R) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 294, STR 14R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (BS 480 S27R) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 480, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,733 hrs · 57,269 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 27L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 68,109 hrs · 56,771 cycles

R1 DOOR SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,681 hrs · 56,432 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,560 hrs · 56,342 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 19L. REPAIRED SKIN PER SRM.

Part: HYDRAULIC LINE — CHAFED (RT MLG) · airframe 67,477 hrs · 56,278 cycles

AIRTURN BACK / DECLARED EMERGENCY. THE -A- SYSTEM HYDRAULIC FLUID LOSS ON DEPARTURE FROM PHL. FOUND RIGHT MLG DOWNLOCK ACTUATOR LINE CHAFED. REMOVED AND REPLACED LINE PER MM.

Part: DUCT — CRUSHED (FUSELAGE) · airframe 67,107 hrs · 55,998 cycles

AT FL 240, CABIN ALT HORN SOUNDED, ALT CLIMBED TO 15,000 FT AND MASKS DEPLOYED. FOUND AFT PRESSURE BULKHEAD APU PNEUMATIC DUCT CRUSHED. REMOVED AND REPLACED AFT PRESSURE BULKHEAD APU PNEUMATIC DUCT PER MM.

Part: MOTOR — SHEARED (NR 2 ENGINE) · airframe 66,726 hrs · 55,713 cycles

AT FL 370 NR 2 ENGINE WILL NOT ATTAIN MAX CLIMB POWER. FOUND VBV MOTOR SHAFT SHEARED. REMOVED AND REPLACED VBV DRIVE MOTOR PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 66,307 hrs · 55,368 cycles

BULL NOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 19 DEF. SECURED LIGHT ASSY AND REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,870 hrs · 55,049 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 768, STR 18L. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 64,934 hrs · 54,335 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT SIGN LENS MISSING AT ROW 2 DEF. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,934 hrs · 54,335 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT BULL NOSE LIGHT INOP AT ROW 12 DEF. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (BS 517D S16R) · airframe 64,557 hrs · 54,030 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 517D, STR 16R. REPAIRED SKIN PER SWA EA.

Part: ATTACH FITTING — CRACKED (NLG ACTUATOR) · airframe 64,365 hrs · 53,889 cycles

DURING SCHEDULED MV2 CHECK, FOUND NLG ACTUATOR UPPER ATTACH FITTING GUSSETT CRACKED IN RADIUS. REMOVED AND REPLACED NLG GUSSETT FITTING PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 64,350 hrs · 53,873 cycles

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

Part: KEELBEAM — CORRODED (BS 520) · airframe 64,042 hrs · 53,623 cycles

DURING SCHEDULED SPV CHECK, FOUND KEELBEAM CORRODED AT BS 520, LBL 6.50. REPAIRED CHORD PER ER.

Part: RIB — CRACKED (RT WING) · airframe 64,042 hrs · 53,623 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING RIB UPPER CHORD CRACKED AT WBL 114, STR 2. REPAIRED WING CHORD PER ER.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 64,042 hrs · 53,623 cycles

DURING SCHEDULED SPV CHECK, FOUND LOWER TORQUE BOX INBOARD CHORD CORRODED AT BS 1088 TO BS 1092, LBL 25. REPAIRED CHORD PER ER AND SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 64,042 hrs · 53,623 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CORRODED AT LEFT KEEL BEAM, BS 500C, STR 28L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (BS 500C) · airframe 64,042 hrs · 53,623 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, LBL 8 TO RBL 8. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (BS 967 S6L) · airframe 64,042 hrs · 53,623 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 6L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 64,042 hrs · 53,623 cycles

DURING SCHEDULED SPV CHECK, FOUND RIGHT WING NR 5 SLAT T/E WEDGE DELAMINATED. REPAIRED NR 5 SLAT T/E WEDGE PER SRM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 64,042 hrs · 53,623 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EXIT EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED EVAC SLIDE AFT GIRT BAR HOOK PER SRM.

Part: FRAME — CRACKED (AFT CARGO DOOR) · airframe 64,042 hrs · 53,623 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR UPPER FRAME CRACKED. REMOVED AND REPLACED AFT CARGO DOOR UPPER FRAME SECTION PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 64,042 hrs · 53,623 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14 L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SKIN — CRACKED (BS 505C) · airframe 63,367 hrs · 53,116 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505C, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 63,206 hrs · 52,989 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER WHEN PROVISIONING OPENED DOOR. REINSTALLED SLIDE PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 63,118 hrs · 52,915 cycles

DURING SCHEDULED RON CHECK, FOUND EEPLS STRIP DAMAGED BETWEEN ROW 6 TO ROW 8, RT SIDE. REMOVED AND REPLACED STRIP PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,731 hrs · 52,584 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT ROW 12 DEF. RELAMPED LIGHT PER MM.

Part: ROD END — BROKEN (LT WING SPOILER) · airframe 62,648 hrs · 52,517 cycles

FOUND LT WING NR 4 GROUND SPOILER OTBD ACTUATOR ROD END BROKEN. REMOVED AND REPLACED GROUND SPOILER OTBD ACTUATOR PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 62,441 hrs · 52,345 cycles

BULLNOSE EMERGENCY LIGHT LENS MISSING AT ROW 12. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 62,385 hrs · 52,293 cycles

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

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 61,829 hrs · 51,859 cycles

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

Part: SKIN — CRACKED (BS 940) · airframe 61,822 hrs · 51,853 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 21L. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,385 hrs · 51,486 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 18R. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 61,385 hrs · 51,486 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 500D, STR 23L. REPAIRED STRINGER PER SRM.

Part: TAB — WORN (LT ELEVATOR) · airframe 60,409 hrs · 50,690 cycles

DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB HAD EXCESSIVE PLAY. REMOVED AND REPLACED LT ELEVATOR TAB PER MM.

Part: TAB — WORN (RT ELEVATOR) · airframe 60,409 hrs · 50,690 cycles

DURING SCHEDULED C1 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB PER MM.

Part: COVER — DISLODGED (EMERGENCY LIGHT) · airframe 59,956 hrs · 50,329 cycles

EMERGENCY EXIT LIGHT COVER AT ROW 13 ABC, FEEL OFF. REMOVED AND REPLACED LIGHT COVER PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 59,447 hrs · 49,925 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,099 hrs · 48,871 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR OVERHEAD EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 57,403 hrs · 48,302 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,537 hrs · 47,621 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING FROM BULLNOSE AT 8D. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,537 hrs · 47,621 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STRINGER 18R. REPAIRED SKIN PER SRM.

Part: CHANNEL — CRACKED (DOOR FRAME) · airframe 56,528 hrs · 47,622 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR FRAME CUTOUT H-CHANNEL CRACKED AT UPPER HINGE. REPAIRED PER EA.

Part: BEAM — CRACKED (CABIN FLOOR) · airframe 56,087 hrs · 47,282 cycles

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL BEAM CRECKED AT BS 663, BL 0, WL 208. REPAIRED BEAM PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,087 hrs · 47,282 cycles

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAMES AT STR 9L, BS 747, 787, 827, 907 AND STR 9R, BS 787, 827, 847, 887. REPAIRED FRAMES PER BFG ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,087 hrs · 47,282 cycles

DURING SCHEDULED D CHECK, FOUND CORROSION ON FLOORBEAM UPPER CHORD AT BS 947, RBL 42, WL 208. REPAIRED DAMAGED AREA PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,087 hrs · 47,282 cycles

DURING SCHEDULED D CHECK, FOUND CORROSION ON SHEAR TIE BS 947.5, STR 23L AND 24L. REPAIRED SHEAR TIE PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,087 hrs · 47,282 cycles

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT STR 9L, BS 400 AND 480, AND STR 9R, BS 400 AND 480. REPAIRED DAMAGED AREA PER BFG ER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,087 hrs · 47,282 cycles

DURING SCHEDULED D CHECK, FOUND CRACKED STR 6R AT BS 1011. REPAIRED DAMAGED AREA PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,087 hrs · 47,282 cycles

DURING SCHEDULED D CHECK, FOUND LOWER EXT FUSELAGE SKIN BULGED AT BS 527, LBL 7. REPAIRED DAMAGED AREA PER BFG ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 565,086 hrs · 47,281 cycles

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708, LBL 25, WL 206. REPAIRED BEAM PER BFG ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,086 hrs · 47,281 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 500, RBL 10, WL 148.5. REPAIRED SHEAR TIE PER SRM.

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 56,086 hrs · 47,281 cycles

DURING SCHEDULED D CHECK, FOUND LT HORIZONTAL STAB REAR SPAR LOWER CHORD CORRODED. REPAIRED SPAR PER SRM.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 56,086 hrs · 47,281 cycles

DURING SCHEDULED D-CHECK, FOUND FLOOR WEB CRACKED AT BS 986.5 AND BS 1016, RBL 41. REPAIRED FLOORWEB PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,086 hrs · 47,281 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER 15 L CRACKED AT BS 380 FRAME. REPAIRED STRINGER PER SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 56,086 hrs · 47,281 cycles

DURING SCHEDULED D CHECK, FOUND CORROSION IN AFT CARGO COMP BS 1011, STRINGER 20 R, AT 1016 BULKHEAD ATTACHMENT. REPAIRED BULKHEAD ATTACHMENT PER SRM.

Part: FRAME — CORRODED (AFT FUSELAGE) · airframe 56,086 hrs · 47,281 cycles

DURING SCHEDULED D CHECK, FOUND CORROSION ON RT AFT GALLEY DOOR FRAME AT BS 996, RBL 48, WL 208. REPAIRED FRAME PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,086 hrs

PAE - DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 178.5, LBL 24, WL 207. REPAIRED PER SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED D-CHECK, FOUND CORROSION ON TORQUE BOX UPPER SUPPORT CHORD BS 1088 WL 250, RBL 20. REPAIRED PER SRM. (M)

Part: ANGLE — CRACKED (FWD FUSELAGE) · airframe 56,086 hrs · 47,281 cycles

DURING SCHEDULED D CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 178, WL 207, LBL 5. REPAIRED PER SRM.

Part: FRAME — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED D-CHECK, FOUND CORROSION ON AFT CARGO COMP FRAME BS 847 RBL 4 TO LBL 4, WL 154. REPAIRED PER SRM. (M)

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,086 hrs · 47,281 cycles

PAE - DURING SCHEDULED D-CHECK, FOUND CORROSION ON BS 272 STRINGER 22. REPAIRED PER SRM. (M)

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,086 hrs · 47,281 cycles

DURING SCHEDULED D CHECK, FOUND BOTH LEFT AND RIGHT FRAMES CRACKED AT BS 188. REPAIRED FRAMES PER SRM.

Part: BEAM — CORRODED (FUSELAGE) · airframe 56,086 hrs · 47,281 cycles

DURING SCHEDULED D CHECK, FOUND STUB BEAM INBOARD CHORD CORRODED AT BS 616, LBL 65. REPAIRED BEAM PER SRM AND BOEING SB.

Part: RIB — CRACKED (LT WING) · airframe 560,861 hrs · 47,281 cycles

DURING SCHEDULED D CHECK, FOUND NR 3 SLAT LWR T/E SPAR CRACKED AT IB RIB OF ACTUATOR ATTACH POINT. REMOVED AND REPLACED NR 3 SLAT LWR T/E SPAR CORD PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 560,861 hrs · 47,281 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 312 LBL 11 TO RBL 37, WL 208 CORRODED. REPAIRED FLOORBEAM PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,086 hrs · 47,281 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 807 LBL 1 WL 149. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,086 hrs · 47,281 cycles

DURING SCHEDULED D CHECK, FOUND 2 EACH SHEAR TIES CORRODED AT BS 747 AND 827, RBL 1 AND RBL 5, BOTH AT WL 147. REPAIRED SHEAR TIES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,086 hrs · 47,281 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 663, STRINGER 1. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,086 hrs · 47,281 cycles

DURING SCHEDULED D CHECK, 3 EACH STRINGER CLIPS CRACKED AT BS 747, STR 11R, BS 767, STR 13R, BS 767, STR 11R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,086 hrs · 47,281 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER 25R CORRODED AT BS 903 TO 910. REMOVED AND REPLACED PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 56,086 hrs · 47,287 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED AT BS 727C+8, LT SIDE, BS 727B+8, RT SIDE. REPAIRED CREASE BEAM SECTIONS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,647 hrs · 46,956 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUT OUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,647 hrs · 46,956 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR UPPER HINGE CUT OUT. REPAIRED SKIN PER SRM.

Part: BRACKET — OUT OF POSITION (AFT ENTRY) · airframe 55,422 hrs · 46,793 cycles

AFT ENTRY DOOR EVACUATION SLIDE GIRT BAR WOULD NOT LOCK PROPERLY AT FLOOR BRACKETS. REPAIRED FLOOR BRACKETS PER SWA EA.

Part: BUSHING — WORN (ELEVATOR TABS) · airframe 55,247 hrs · 46,629 cycles

AIRFRAME VIBRATION ON CLIMB-OUT AND DESCENT, REMOVED AND REPLACED HARDWARE AND BUSHINGS ON BOTH LT AND RT ELEVATOR TAB ROD ENDS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,990 hrs · 46,419 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 619, STR 4L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,984 hrs · 46,416 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIPS CRACKED (2 EA) AT STR 4L, BS 620 AND BS 680. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 54,795 hrs · 46,265 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT CABIN CENTER EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,795 hrs · 46,265 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST AND BATTERY PER MM.

Part: LINK — LOOSE (NLG) · airframe 54,435 hrs · 45,971 cycles

SEVERE VIBRATION FELT FROM NOSE GEAR UPON LANDING. REMOVED AND REPLACED BOTH NLG UPPER & LOWER TORSION LINKS PER MM.

Part: ELEVATOR — WORN (TAIL) · airframe 53,859 hrs · 45,539 cycles

DURING SCHEDULED C2 CHECK, SWA SI 11139-55, BOTH LH & RH ELEVATORS FAILED FREE PLAY CHECK. R&R BOTH LH & RH ELEVATORS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,855 hrs · 45,536 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,855 hrs · 45,536 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,855 hrs · 45,536 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,413 hrs · 45,186 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 20L. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 53,413 hrs · 45,186 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD EMERGENCY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 52,931 hrs · 44,807 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT CARGO DOOR EXTERNAL SKIN CRACKED AT HANDLE CUT OUT, UPPER AFT CORNER. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,362 hrs · 43,543 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 500 PLUS 16, STR 10R AND BS 500D PLUS 18, 12L. REPAIRED SKIN PER SWA RA.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 51,158 hrs · 43,373 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (AFT ENTRY DOOR) · airframe 50,246 hrs · 42,636 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR SKIN CRACKED AT LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA T1.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 50,246 hrs · 42,676 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: TAB — WORN (ELEVATOR) · airframe 48,537 hrs · 41,232 cycles

DURING SCHEDULED C4 CHECK, FOUND PLAY AT RH ELEVATOR TAB ATTACH ASSY. R&R ELEVATOR TAB PER MM.

Part: COVER — MISSING (CABIN) · airframe 49,605 hrs · 44,106 cycles

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

Part: STIFFENER — CRACKED (MAIN WHEEL WELL) · airframe 48,106 hrs · 40,873 cycles

DURING SCHEDULED 1/4D CHECK, FOUND MLG WHEEL WELL BULKHEAD VERTICAL STIFFENER CRACKED BS 663, LBL6.15. R&R STIFFENER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 48,106 hrs · 40,873 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CORRODED AT BS 515, STR 27R. REPAIRED STR PER SRM.

Part: STIFFENER — CRACKED (MAIN WHEEL WELL) · airframe 48,106 hrs · 40,873 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL STIFFENER CRACKED IN MAIN WHEEL WELL BULKHEAD BS 663, RBL 615. REPAIRED STIFFENER PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,106 hrs · 40,873 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 48,106 hrs · 40,873 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CORRODED, AT BS 500D, STR 26R. REPAIRED STR PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 48,106 hrs · 40,873 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AFT CARGO BS 787, STR 27R. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,106 hrs · 40,873 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAMS AFT CARGO AT BS 860, LBL 8, RBL 3 & RBL 8. REPAIRED FLOORBEAMS PER SWA RA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,106 hrs · 40,873 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED IN AFT CARGO AT BS 807 & BS 860, LBL 17. REPAIRED FLOORBEAMS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,106 hrs · 40,873 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 21L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,106 hrs · 40,873 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STR CLIP CRACKED AT BS 500C, STR 27L. Removed and replaced STR CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,106 hrs · 40,873 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FITTING — CORRODED (LT & RT MLG) · airframe 48,046 hrs · 40,815 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT & RT WALKING BEAM HANGER FITTINGS CORRODED AT FWD OTBD, LT & RT MLG. REMOVED AND REPLACED BOTH WALKING BEAM HANGER FITTINGS PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 47,731 hrs · 40,547 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP. R&R BATTERY CHARGER PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,578 hrs · 40,429 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS INOP AT AFT SECTION. R&R BATTERY PACK PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 47,578 hrs · 40,429 cycles

DURING SCHEDULED C3 CHECK, FOUND NR 5 L/E SLAT DELAMINATED AT OUTBD UPPER T/E SURFACE. R&R NR 5 SLAT PER MM.

Part: CAP — MISSING (CABIN) · airframe 47,578 hrs · 40,429 cycles

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

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 47,578 hrs · 40,429 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. R&R EVAC SLIDE ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,523 hrs · 40,384 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS DIM AT AFT CABIN. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 47,253 hrs · 40,179 cycles

ELECTRIC BURNING ODOR AT ROWS 17 TO 18, RIGHT SIDE. FOUND WINDOW LIGHT BALLAST INOP. REMOVED AND REPLACED BALLAST PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,721 hrs · 39,717 cycles

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

Part: SKIN — CRACKED (HORIZ STAB) · airframe 46,599 hrs · 39,611 cycles

DURING SCHEDULED C2 CHECK, FOUND 2 CRACK AT LT HORIZ STAB SKIN, 4 FT OTBD AT AFT SPAR. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 46,599 hrs · 39,611 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. READJUSTED EVAC SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,599 hrs · 39,611 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AT ROW 10, LOOSE AT ROW 1 & WIRING EXPOSED AT ROW 3. REPAIRED EEPLS PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,252 hrs · 39,304 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD VERTICAL BEAMS CRACKED AT LBL 17.1, WL 229.5 & RBL 10, WL 234. REPAIRED BULKHEAD PER ER 00-1268.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,252 hrs · 39,304 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD VERTICAL WEBS CRACKED AT LBL 17.1, WL 182 & RBL 17.1, WL 182. REPAIRED BULKHEAD PER ER 00-1282 & ER 12-1283.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,252 hrs · 39,303 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKED AT WL 218, RBL 11 TO RBL 12. REPAIRED BULKHEAD PER SRM.

Part: COVER — LOOSE (ESCAPE SLIDE) · airframe 45,261 hrs · 38,444 cycles

FWD SERVICE DOOR EVACUATION SLIDE SHELL OPENED WHEN DOOR WAS OPENED. RE-INSTALLED SLIDE ASSY PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 44,782 hrs · 38,037 cycles

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

Part: LIGHT — INOPERATIVE (CABIN)

AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (TE FLAP)

DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD AFT FLAP CRACKED ON LOWER SKIN. REPAIRED FLAP PER SWA RA NR 1-357-0771.

Part: BATTERY — INOP (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER PER MM.

Part: COVER — DAMAGED (CABIN)

DURING SCHEDULED BC1 CHECK, FOUND EEPLS COVER DAMAGED AT FWD SECTION AND MISSING AT CENTER SECTION. REPLACED BOTH COVERS PER MM.

Part: LINE — LEAKING (RT MLG)

DURING CLIMB, HYD A-SYSTEM LOW PRESS LIGHT ILLUMINATED AT NR 1 ENGINE. HYD QTY READS EMPTY. HYD BRAKE PRESSURE AND MAIN SYSTEM PRESSURE OK. FOUND LEAKING HYD LINE. REMOVED AND REPLACED RT MLG DOWN HYD LINE PER MM.

Part: AIR DIST — ODOR (CABIN)

AFTER ENGINE START, F/A INFORMED FLIGHT CREW, THAT SEVERAL PAX AND F/A SMELLED SOMETHING BURNING. A/C RETURNED TO GATE FOR MAINTENANCE. ODOR IDENTIFIED AS LPS SPRAYED AFT OF BAG BIN, CLEANED UP. OK TO CONTINUE PER M/M.

Part: BASE — INOP (CABIN)

DURING 1/2 D-CHECK, FOUND AFT EMERGENCY FLOOR TRACK LIGHTING BATTERY PACK BASE INOP. REMOVED AND REPLACED BATTERY PACK BASE PER MM. PREFLIGHT, FOUND EMERGENCY FLOOR TRACK HAS TWO LIGHTS INOP. RELAMPED AND OPS CKS GOOD PER M/M.

Part: SKIN — CRACKED (BS 520)

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN BULGING AT RIVETS AFT OF BS 520C, S28R LOWER FUSELAGE. INSTALLED DOUBLER AND TRIPLER PER SWA RA 1-353-1961.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT LOWER CORNER OF FWD SERVICE DOOR. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD LOWER CORNER OF AFT SERVICE DOOR. REPAIRED PER BOEING SRM.

Part: SKIN — CORROSION (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND EXTERIOR FUSE SKIN BULGING AND RIVETS PULLING THROUGH, INDICATING CORROSION BETWEEN SKIN LAYERS AT BS 663 AT S27R, KEEL BEAM CHORD. INSTALLED REPAIR PER SRM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORROSION AT BS 312, RBL 36. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178, WL 200, LBL 5.7. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED 1 INCH AFT OF LOWER VHF ANTENNA CUTOUT APPROX 1.5 LONG. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178, WL 200, RBL 5.7. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178, WL 189, RBL 1. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 294)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 294, LBL 8. REPAIRED PER SWA RA 1-353-1953.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178, WL 202, LBL 5.7. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178, WL 189, LBL 1. REPAIRED PER BOEING SRM.

Part: VALVE — LEAKING (A HYD SYST)

AFTER T/O LAX, AFTER RAISING L/G BOTH SYS A HYD LOW PRESSURE LIGHTS ILLUMINATED FOR ABOUT 5-10 SEC. HYD FLUID SYS A FLUID WENT BELOW REFILL MARK FROM FULL AND CONTINUED TO DECREASE TO 1/2. AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED A SYSTEM ISOLATION VALVE ASSY. LEAK CHECK OPS, CHECK GOOD PER BOEING M/M.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C3 CHECK, FOUND A .156 INCH LONG CRACK IN FUSELAGE SKIN AT L2 DOOR AT UPPER HINGE CUTOUT. REPAIRED PER SWA RA 1-353-1764.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND FWD ENTRY SLIDE LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: SKIN — DENTED (BS 1024)

DURING SCHEDULED QD-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1024, RIGHT SIDE AT S17 AND AT BS 1064, RBL 7, WL 203. INSTALLED REPAIR DOUBLERS PER BOEING SRM.

Part: SKIN — CORRODED (BS 520)

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN BULGING AT RIVETS AFT OF BS 520C, S28L. REPAIRED PER SWA RA 1-353-1465.

Part: FLOORBEAM — CRACKED (BS 344)

DURING SCHEDULED B/C1 CHECK, FOUND FLOORBEAM STRAP CRACKED AT BS 344, JUST O/B AND ABOVE BATTERY. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.