N307SW

Part: SKIN — CRACKED (RT WING SPOILER) · airframe 76,715 hrs · 71,542 cycles

DURING SCHEDULED OTS CHECK, FOUND RT WING I/B GROUND SPOILER CRACKED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,312 hrs · 71,250 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 782A, STR 7L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,349 hrs · 71,271 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 741, STR 2R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,272 hrs · 71,218 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP AT ROW 10. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,698 hrs · 70,784 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 265, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,698 hrs · 70,784 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 266, STR 9L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,698 hrs · 70,784 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 272, STR 15L. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 75,698 hrs · 70,784 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR LOWER FIXED FRAME CRACKED. REMOVED AND REPLACED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,698 hrs · 70,784 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 272, STR 15L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,698 hrs · 70,784 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 265, STR 17L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,702 hrs · 70,785 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 259, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,702 hrs · 70,785 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 259, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,702 hrs · 70,785 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 259, STR 12L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,702 hrs · 70,785 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 266, STR 9L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 75,698 hrs · 70,784 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PULL HANDLE COVER OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,658 hrs · 70,756 cycles

DURING SCHEDULED SPV CHECK, FOUND EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: GIMBAL JOINT — FAILED (TE FLAP) · airframe 75,657 hrs · 70,755 cycles

T/E FLAPS LOCKED OUT DUE TO NR 8 FLAP JACKSCREW GIMBAL FAILURE. REPAIR IN PROGRESS. REMOVED AND REPLACED NR 8 TRANSMISSION & JACKSCREW ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 13R. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 13R. REPAIRED FRAME PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,070 hrs · 70,324 cycles

DURING MV4 CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 500C + 16, STR 16R. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 616, RBL 64 BETWEEN WL 210 TO WL 202. REPAIRED FRAME PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED BETWEEN BS 727C +3 TO BS 727C +8, STR 5L. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 616, LBL 64. REPAIRED FRAME PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE BELLY SKIN CORRODED AT BS 827, STR 25L. REPAIRED SKIN PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 616, LBL 45. REPAIRED BEAM PER ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT DOME CAP, BS 1016, BETWEEN BL 0 TO LBL 10. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP CRACKED AT BS 1016, LBL 9.5. REPAIRED CAP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BETWEEN BS 706 TO BS 714, BL 0. REPAIRED BEAM PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 18R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 340, LBL 10, WL 207. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOKS LOOSE. REMOVED AND REPLACED HOOKS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 75,050 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT CREASE BEAM I/B CHORD CRACKED AT BS 616, WL 208. REPAIRED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,050 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 20R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 18R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 28L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 747, STR 21R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 14R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 500B, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,051 hrs · 70,307 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 79,791 hrs · 73,935 cycles

AFT PRESSURE BULKHEAD DOME CAP CRACKED AT BS 1016, LBL 9.5. R&R WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,794 hrs · 70,110 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 584, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT WING) · airframe 74,794 hrs · 70,110 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT UPPER WING SKIN CRACKED AT BS WBL 173. REPAIRED SKIN PER SWA EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT STA 360, STR 21R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,265 hrs · 98,278 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 326, STR 26R. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 8L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 25L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 25L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 20L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 520, STR 23R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 26R CORRODED AT BS 510A. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 271, STR 16L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 16R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 19R CORRODED BETWEEN BS 312 AND BS 360. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 16R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 16R CRACKED AT BS 500C. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 23R CRACKED AT BS 328. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 18L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500B, STR 15L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 13L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 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 72,265 hrs · 68,278 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,265 hrs · 68,278 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,152 hrs · 68,192 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: TORQUE TUBE — WORN (LT ELEVATOR) · airframe 72,152 hrs · 68,192 cycles

DURING SCHEDULED 22Y CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TORQUE TUBE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,152 hrs · 68,192 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 72,152 hrs · 68,192 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT ASSY CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,152 hrs · 68,192 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 270, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,152 hrs · 68,192 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT AIR CONDITIONING BAY CUTOUT BETWEEN RT BS 590 AND RT BS 616. REPAIRED SKIN PER EA.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 72,152 hrs · 68,192 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT HORIZONTAL STABILIZER UPPER SKIN OUTBOARD SURFACE CORRODED. REPAIRED STABILIZER PER SRM.

Part: LIGHT — BROKEN (L1 DOOR) · airframe 72,152 hrs · 68,192 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: SUPPORT BEAM — CRACKED (CENTER WING) · airframe 72,152 hrs · 68,192 cycles

DURING SCHEDULED 22Y CHECK, FOUND WING CENTER SECTION SUPPORT BEAM WEB CRACKED AT BS 616, BL 40.8. REPAIRED WEB PER AAR EA.

Part: SLIDE — FRAYED (R2 DOOR) · airframe 72,152 hrs · 68,192 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT SKIRT FRAYED. REMOVED AND REPLACED VAC SLIDE PER MM.

Part: TAB — CRACKED (RT WING AILERON) · airframe 72,152 hrs · 68,192 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING AILERON TAB CRACKED. REMOVED AND REPLACED TAB PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,152 hrs · 68,192 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 270, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 72,152 hrs · 68,192 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING OUTBOARD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 72,152 hrs · 68,192 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 12. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,152 hrs · 68,192 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 966, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 72,152 hrs · 68,192 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 268 AND BS 360, RBL 70. REPAIRED CREASE BEAM PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 72,152 hrs · 68,192 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 72,152 hrs · 68,192 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM CHORD CORRODED BETWEEN BS 947 AND BS 1006, RBL 49. REMOVED AND REPLACED CHORD PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,152 hrs · 68,192 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SLAT — CRACKED (WING) · airframe 72,152 hrs · 68,192 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING NR 2 L/E SLAT CRACKED AT T/E. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (BS 504A-500D) · airframe 71,888 hrs · 67,984 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 504A AND BS 500D, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 71,888 hrs · 67,984 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: CABLE — FRAYED (R2 DOOR SLIDE) · airframe 71,888 hrs · 67,984 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 71,888 hrs · 67,984 cycles

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

Part: SKIN — CRACKED (BS 922 S25R) · airframe 71,888 hrs · 67,984 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 922, STR 25R. REPAIRED SKIN PER SWA EA.

Part: COVER — LOOSE (EMERGENCY LIGHTS) · airframe 71,667 hrs · 67,803 cycles

FWD CABIN EMERGENCY EXIT SIGN COVER LOOSE. SECURED COVER PER MM.

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 71,657 hrs · 67,793 cycles

FWD CABIN EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,270 hrs · 67,478 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 4R. REPAIRED SKIN PER SRM.

Part: BOLT — WORN (ELEVATOR TAB) · airframe 70,957 hrs · 67,231 cycles

DURING SCHEDULED C3 CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BOLT AND BUSHING PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 70,957 hrs · 67,231 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,822 hrs · 67,120 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,822 hrs · 67,120 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R2 EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,561 hrs · 66,896 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,561 hrs · 66,896 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 14L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,561 hrs · 66,896 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 413, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 395 S19R) · airframe 70,064 hrs · 66,508 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 395, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 500) · airframe 70,064 hrs · 66,508 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 70,064 hrs · 66,508 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — CRACKED (BS 416) · airframe 70,064 hrs · 66,508 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 416, STR 16R. REPAIRED SKIN PER SWA EA.

Part: WEB — CRACKED (BS 610) · airframe 70,064 hrs · 66,508 cycles

DURING SCHEDULED C2 CHECK, FOUND WING CENTER SECTION WEB CRACKED BS 610, LBL 40.875. REPAIRED WEB PER SWA EA.

Part: SKIN — CRACKED (BS 727C S14R) · airframe 70,064 hrs · 66,508 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727C, STR 14R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 500D) · airframe 70,064 hrs · 66,508 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 8R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (NR 4 SPOILER) · airframe 70,064 hrs · 66,508 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING NR 4 SPOILER HINGE CRACKED AT OUTBOARD END. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (BS 500D) · airframe 70,064 hrs · 66,508 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 8L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 380 S8L) · airframe 70,064 hrs · 66,508 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, STR 8L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 69,626 hrs · 66,163 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,477 hrs · 66,045 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, BL 0. REPAIRED SKIN PER SB AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,477 hrs · 66,045 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,477 hrs · 66,045 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,477 hrs · 66,045 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,477 hrs · 66,045 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,475 hrs · 66,044 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 492, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,475 hrs · 66,044 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,475 hrs · 66,044 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 497, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,475 hrs · 66,044 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 348, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,475 hrs · 66,044 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,475 hrs · 66,044 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 28L CORRODED AT BS 497. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 69,475 hrs · 66,044 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME CRACKED AT BS 847, STR 18R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,475 hrs · 66,044 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,475 hrs · 66,044 cycles

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

Part: WINDOW — ARCED (COCKPIT) · airframe 69,276 hrs · 65,889 cycles

FLIGHT DECK L1 WINDOW ARCHED AT UPPER RT CORNER. REMOVED AND REPLACED L1 WINDOW PER MM.

Part: SKIN — CRACKED (BS 362 S6R) · airframe 68,699 hrs · 65,444 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 362, STR 6R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 362 S5R) · airframe 68,699 hrs · 65,444 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 362, STR 5R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 312 S18R) · airframe 68,699 hrs · 65,444 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 18R. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (RT WING SPOILER) · airframe 68,190 hrs · 65,060 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 7 SPOILER DELAMINATED ON FWD UPPER SURFACE. REMOVED AND REPLACED NR 7 SPOILER PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 68,190 hrs · 65,060 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 23 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 68,190 hrs · 65,060 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 23 ABC. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: FITTING — WORN (RT WING) · airframe 68,103 hrs · 64,976 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT MLG FWD OUTBOARD HANGER FITTING WORN. REPAIRED FITTING PER SWA EA.

Part: FITTING — WORN (LT WING) · airframe 68,103 hrs · 64,976 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT MLG FWD OUTBOARD HANGER FITTING WORN. REPAIRED FITTING PER SWA EA.

Part: SKIN — CRACKED (BS 909) · airframe 68,035 hrs · 64,917 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 909, STR 4R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 67,827 hrs · 64,761 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 67,818 hrs · 64,754 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,138 hrs · 64,216 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 67,061 hrs · 64,164 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 66,870 hrs · 64,030 cycles

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

Part: SKIN — CRACKED (BS 500) · airframe 66,131 hrs · 63,453 cycles

DURING OTS, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 452) · airframe 66,131 hrs · 63,453 cycles

DURING OTS, FOUND FUSELAGE SKIN CRACKED AT BS 452, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 800) · airframe 66,131 hrs · 63,453 cycles

FUSELAGE SKIN CRACKED AT BS 800, STR 19L. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,981 hrs · 63,335 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,750 hrs · 63,152 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 465, STR 16R. REPAIRED SKIN PER SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,595 hrs · 63,007 cycles

DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 65,265 hrs · 62,754 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 787, STR 26R. REPAIRED SKIN PER SWA EA.

Part: STRINGER — CORRODED (AFT CARGO) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 795, STR 26R. REPAIRED STRINGER PER SWA EA.

Part: VERTICAL BEAM — CORRODED (AFT CARGO) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CORRODED BETWEEN BS 767 TO BS 787, STR 25R TO STR 26R. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 301.2, STR 17R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, L1 DOOR LOWER FWD STOP FITTING CUTOUT. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 EACH LONGITUDINAL FLOORBEAMS CORRODED AT BS 847 + 10, LBL 7 & LBL 12. REPAIRED FLOORBEAMS PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSLEAGE) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 867, LBL 7. REPAIRED FLOORBEAM PER SWA EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 907, BETWEEN STR 25L TO STR 25R. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 330, STR 11R. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,677 hrs · 62,272 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 847, BETWEEN STR 27R AND STR 27L. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 805, STR 26L. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (RT NR 5 SLAT) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING NR 5 L/E SLAT INBD UPPER SKIN CRACKED. REPAIRED SLAT PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 807, STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (BS 794) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 794, BETWEEN LBL 8 & LBL 12. REPAIRED FLOORBEAM PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKS AT BS 500B, BETWEEN STR 20R AND STR 20L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT, UPPER AFT CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 847, BETWEEN STR 27L TO STR 27R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 968 TO BS 971, STR 21L. REPAIRED SKIN PER SWA EA.

Part: BELTFRAME — CORRODED (FUSELAGE) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BELTFRAME CORRODED AT BS 847, BETWEEN STR 27L TO STR 27R. REPAIRED BELTFRAME PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 727D + 5, LBL 13. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 767 + 5, RBL 3 & RBL 8. REPAIRED FLOORBEAMS PER SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,677 hrs · 62,272 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: STRINGER CLIP — CRACKED (BS 727A) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED AT BS 727A, STR 25L & STR 25R. REMOVED AND REPLACED CLIPS PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 25L & STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (BS 767) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE LONGITUDINAL FLOORBEAM CORRODED AT BS 767 + 5, LBL 3 & LBL 12. REPAIRED FLOORBEAM PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 947.5, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26L & STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 967, BETWEEN STR 27L AND STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 807, STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 64,677 hrs · 62,272 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 907, STR 24L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,677 hrs · 62,272 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 64,600 hrs · 62,215 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 64,559 hrs · 62,175 cycles

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

Part: HOOK — LOOSE (L1 DOOR GIRT BAR) · airframe 64,382 hrs · 62,022 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 64,382 hrs · 62,022 cycles

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 17. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,382 hrs · 62,022 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 935, STR 25L. REPAIRED SKIN PER SWA EA & SRM.

Part: TRIM TAB — DELAMINATED (LT ELEVATOR) · airframe 64,121 hrs · 61,811 cycles

LT ELEVATOR TRIM TAB LOWER T/E DELAMINATED. REPAIRED TAB PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 63,771 hrs · 61,534 cycles

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

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 63,534 hrs · 61,348 cycles

L2 DOOR EMERGENCY EVAC SLIDE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,645 hrs · 60,660 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 933, STRINGER 22L, CRACKED. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 62,465 hrs · 60,529 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,285 hrs · 60,394 cycles

DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY AND AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. RELAMPED LIGHTS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,132 hrs · 60,269 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 410, STRINGER 26L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,132 hrs · 60,269 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 23R, CRACKED. REPAIRED SKIN PER EA.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 61,968 hrs · 60,135 cycles

DURING SPV, FOUND STRINGER SPLICE AT BS 360, STRINGER 22R, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 61,968 hrs · 60,135 cycles

DURING SPV, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,656 hrs · 59,879 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 440, STRINGER 26L, CRACKED. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 61,666 hrs · 59,879 cycles

DURING SCHEDULED C1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS AT ROW 17 ABC, LOOSE. SECURED BULL NOSE EMERGENCY EXIT LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,620 hrs · 59,846 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 797, STRINGER 18L, BS 767, 18L, BS 797, STRINGER 19L, CRACKED. REPAIRED SKIN PER EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,620 hrs · 59,846 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 475, STRINGER 16R, CRACKED. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 61,546 hrs · 59,786 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,499 hrs · 59,747 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 500D + 16, STRINGER 16R AND STRINGER 16L, CRACKED. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 60,977 hrs · 59,314 cycles

DURING SCHEDULED RON, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 60,822 hrs · 59,197 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,371 hrs · 58,830 cycles

DURING SCHEDULED A1 CHECK, FOUND 3 EA FUSELAGE SKIN CRACKS AT BS 913, STR 10L, BS 783, STR 20L, AND BS 740, STR 19R. REPAIRED SKIN PER SRM AND SWA EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 59,349 hrs · 57,978 cycles

R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,847 hrs · 57,567 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 823, STR 18L. REPAIRED SKIN PER SRM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 58,841 hrs · 57,562 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,841 hrs · 57,562 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR CRACKED ON OUTER SKIN AT UPPER HINGE CUT OUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,677 hrs · 57,425 cycles

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

Part: INDICATOR — OUT OF LIMITS (ESCAPE SLIDE) · airframe 58,300 hrs · 57,119 cycles

DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,970 hrs · 56,863 cycles

DURING SCHEDULED RON, FOUND BS 1016 BULKHEAD WEB CRACKED (2 EA) BETWEEN STR 7L AND STR 8L. REPAIRED BULKHEAD WEB PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,931 hrs · 56,824 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED JUST OF BS 440, ABOVE STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,015 hrs · 56,128 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED ( 3 EA ) AT BS 312 ABOVE STR 18R, BS 400 ABOVE STR 17L & BS 747 BELOW STR 19R. REPAIRED SKIN PER SRM.

Part: BEARING — WORN (RH ELEVATOR) · airframe 57,015 hrs · 56,128 cycles

DURING SCHEDULED C4 CHECK, SWA SI 11139-55, RH ELEVATOR TAB FAILED FREE PLAY INSPECTION. R&R RH ELEVATOR PUSH ROD CRANK ASSY BEARING PER MM.

Part: BRACKET — MISINSTALLED (SERVICE DOOR) · airframe 56,887 hrs · 56,038 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR HOLD DOWN BRACKET INSTALLED BACKWARD. INSTALLED FLOOR BRACKET CORRECTLY PER MM.

Part: WIRE — BROKEN (COCKPIT) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND COCKPIT OVERHEAD EMERGENCY EXIT LIGHT INOP. REPAIRED BROKEN WIRE L-4 TO M1219 MODULE PER MM.

Part: CONNECTOR — DIRTY (AFT ENTRY DOOR) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE LIGHT INOP. CLEANED SLIDE LIGHT CONNECTOR AND OPS CK GOOD PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR 19R AND STR 20R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 927, WL 168 AND BL 0. REPAIRED SHEAR TIE PER SRM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 56,870 hrs · 56,029 cycles

DURING SCHEDULED D CHECK, FOUND LOWER CHORD DOUBLER CORRODED AT BS 1016, WL 191 AND LBL 5. REPAIRED DOUBLER PER SRM.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 56,870 hrs · 56,029 cycles

DURING SCHEDULED D CHECK, FOUND BULKHEAD SKIN CORRODED AT BS 1016, WL 192 AND BL 0. REPAIRED BULKHEAD SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,029 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (6 EA) BETWEEN STR 8L AND 9L, AT BS'S 480, 727C, 767, 807, 847 AND 867. REPAIRED FRAMES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,029 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (6 EA) BETWEEN STR 8L AND 9L, AT BS'S 480, 727C, 767, 807, 847 AND 867. REPAIRED FRAMES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,029 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (6 EA) BETWEEN STR 8R AND STR 9R, AT BS'S 440, 480, 727D, 767, 827 AND 867.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,029 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (6 EA) BETWEEN STR 8L AND 9L, AT BS'S 480, 727C, 767, 807, 847 AND 867. REPAIRED FRAMES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,029 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (6 EA) BETWEEN STR 8L AND 9L, AT BS'S 480, 727C, 767, 807, 847 AND 867. REPAIRED FRAMES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,029 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (6 EA) BETWEEN STR 8L AND 9L, AT BS'S 480, 727C, 767, 807, 847 AND 867. REPAIRED FRAMES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,029 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (6 EA) BETWEEN STR 8L AND 9L, AT BS'S 480, 727C, 767, 807, 847 AND 867. REPAIRED FRAMES PER SRM.

Part: FLOORBEAM — CRACKED (MID CABIN) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAMS CRACKED (2 EA) AT BS 662, WL 206 AND RBL 25 AND BS 727A + 18, WL 208 AND RBL 27. REPAIRED FLOORBEAMS PER SRM.

Part: BEAM — CRACKED (CABIN FLOOR) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL BEAM CRACKED AT BS 727A, RBL 43, WL 208. REPAIRED BEAM PER BFG ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CRACKED AT BS 947.5, WL 208 AND LBL 54. REPAIRED FLOORBEAM PER BFG ER.

Part: TRUNNION PIN — CORRODED (RT MLG) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND RT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED RT MLG TRUNNION PIN PER MM.

Part: ARM — CORRODED (LT/RT MLG) · airframe 56,870 hrs · 56,024 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 410 AFT OF LRRA ANTENNA. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STUB FRAME CRACKED, BS 294, RBL 55, WL 208 -211. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, BETWEEN STR 2L AND STR 3R. REPAIRED FRAME PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 STOP FITTING. REPAIRED DOOR FRAME PER SWA T1.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 362, STR 10L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED, BS 867, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (COCKPIT) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND BS 188 FRAME CRACKED AT STR 17L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED, BS 907, STR 10R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED, BS 727D, STR 13R. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND 7 EA STRINGER CLIPS CRACKED, BS 559, STR 10RL, BS 597, STR 7R, BS 907, STR 7R, BS 706, STR 7R, BS 616, STR 5L, BS 727D, STR 1, AND BS 400, STR 4L. REMOVED AND REPLACED CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND 6 EA STRINGER CLIPS CRACKED, BS 500D, STR 19R AND 19L, BS 727A, STR 10L, BS 727B, STR 10L, BS 867, STR 9L, AND BS 727B, STR 13R. REMOVED AND REPLACED CLIPS PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STRINGERS 14R AND 15R. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND CORROSION ON FLOORBEAMS UPPER SURFACE AT BS 312, LBL 10, AND UPPER AND LOWER SURFACE AT BS 328, RBL 9 - RBL 58. REPAIRED CORRODED SECTION OF FLOORBEAMS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED AT BS 597, STR 7L, BS 616, STR 5R, AND BS 727B, STR 7L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND CRACKED FUSELAGE FRAME AT BS 188 STR 17R. REMOVED AND REPLACED CRACKED FUSELAGE FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 578 STR 11L, BS 663 STR 10R, BS 706 STR 10L, BS 727A STR 7R, BS 727B STR 8R, 767 STR 10L, BS 787 STR 10L AND STR 10R AND BS 807 STR 10L. REMOVED AND REPLACED CRACKED STRINGER CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 500A STR 4L, BS 520 STR 7R, STR 8R AND STR 12L, BS 597 STR 3L, BS 616 STR 3R, BS 727A STR 8L, 727B STR 8L, BS 727D STR 3R & STR 4L AND BS 727E STR 7L. REMOVED AND REPLACED CRACKED STRINGER CLIPS PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 400 BETWEEN STR 13R AND STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727B STR 2L AND 727C STR 6R AND STR 7L AND BS 727D STR 6R AND STR 7R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND SWAY STRAP CRACKED AT BS 312 RBL 45 AND LBL 45 AND BS 328 BBL 0 WL 200. REMOVED AND REPLACED SWAY STRAPS PER SRM.

Part: ATTACH FITTING — CORRODED (CABIN) · airframe 56,870 hrs · 56,024 cycles

DURING SCHEDULED D CHECK, FOUND CORROSION ON THE L1 GIRT BAR ATTACH FITTINGS BS 312 AND BS 344. REMOVED AND REPLACED THE L1 GIRT BAR ATTACHED FITTINGS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,129 hrs · 55,722 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 4L, BS 807, BS 797 AND BS 908. REPAIRED SKIN PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,129 hrs · 55,422 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICES CRACKED (2 EA) AT BS 360, STR 3L AND STR 6L. REMOVED AND REPLACED STR SPLICES PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,129 hrs · 55,422 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICES CRACKED (2 EA) AT BS 908, STR 4R AND STR 5L. REMOVED AND REPLACED STR SPLICES PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,129 hrs · 55,422 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED (17 EA) AT STR 4R, BS 716, BS 685, BS 577, BS 694, BS 706, BS 700, BS 837, BS 818, BS 727A, BS 797, BS 777, BS 757, BS 440, BS 727E + 10, BS 727E AND BS 727B. MX FERRY TO CYXX, C/W SKIN LAP JOINT MOD PER SWA ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,129 hrs · 55,422 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED (19 EA) AT STR 4L, BS 563, BS 628, BS 578, BS 606, BS 570, BS 696, BS 685, BS 639, BS 609, BS 600, BS 588, BS 595, BS 787, BS 727E + 10, BS 727B, BS 500C + 10, BS 500, BS 450 AND BS 757. MX FERRY TO CYXX, C/W SKIN LAP JOINT MOD PER SWA ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,129 hrs · 55,422 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (4 EA) AT STR 4R, BS 727D, BS 727C, BS 847 AND BS 827. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,129 hrs · 55,422 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 14L, BS500 + 10, BS 500C + 10 AND BS 380. MX FERRY TO CYXX, C/W SKIN LAP JOINT MOD PER SWA ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,129 hrs · 55,422 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 14R, BS 380 AND BS 500D. MX FERRY TO CYXX, C/W SKIN LAP JOINT MOD PER SWA ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,129 hrs · 55,422 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (4 EA) AT STR 5R, BS 727E, BS 727E, BS 727B AND BS 667. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,059 hrs · 55,366 cycles

DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 4L, BS 300 AND BS 420. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 55,518 hrs · 54,915 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,857 hrs · 54,348 cycles

DURING SCHEDULED RON, FOUND OVERHEAD BIN EMERGENCY EXIT BULL NOSE LIGHTS INOP AT ROW 9 DEF, ROW'S 18 AND 21 ABC. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,791 hrs · 54,292 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 355, STR 14L AND BETWEEN BS'S 450 AND 470, RT SIDE OF FUSELAGE CROWN. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 54,791 hrs · 54,292 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND OVERHEAD EMERGENCY EXIT BULL NOSE LIGHT LOOSE AT ROW 7 ABC. SECURED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,791 hrs · 54,292 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 733E, STR 20L AND BS 729E, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,121 hrs · 53,758 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED 5 INCHES LONG AT BS 927, STR 25R. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 54,111 hrs · 53,750 cycles

DURING SCHEDULED BC1 CHECK, FOUND EMERGENCY EXIT LIGHT LENS LOOSE AT LT OVERWING EXIT. SECURED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 54,111 hrs · 53,750 cycles

DURING SCHEDULED BC1 CHECK, FOUND EMERGENCY EXIT LIGHT LENS LOOSE IN AFT CABIN. SECURED LENS PER MM.

Part: HYDRAULIC LINE — LEAKING (RT MLG) · airframe 53,890 hrs · 53,577 cycles

AIR TURNBACK, AFTER DEPARTURE LOSS A-SYSTEM HYD, ENG DRIVEN LOW PRESS LIGHT ILLUMINATED FOLLOWED BY SLOW DEPLETION OF B-SYSTEM TO BELOW 3/4 MARK. REMOVED AND REPLACED RT MLG ACTUATOR PRESS LINES AND CASE DRAIN FILTERS PER MM.

Part: COVER — MISSING (CABIN) · airframe 53,584 hrs · 53,322 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,203 hrs · 53,016 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA), BS 500A, STR 10R, BS 500B, STR 4L AND BS 500D, STR 10R.. REPAIREDSKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,203 hrs · 53,016 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 20L, BS 767 AND 787. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,372 hrs · 52,307 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED ( 3 EA ) AT BS 500C, STR 15L, BS 520, STR 8R, BS 787, STR 20R. REPAIRED SKIN PER SRM.

Part: ACTUATOR (LH WING) · airframe 52,180 hrs · 52,143 cycles

DURING SCHEDULED A1 CHECK, FOUND # 4 GROUND SPOILER ACTUATOR UPPER ATTACH LOBE BROKEN. R&R # 4 GROUND SPOILER ACTUATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,089 hrs · 52,058 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 22L, & BS 931, STR 21L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — ERRATIC (FWD SVC DOOR) · airframe 51,987 hrs · 51,974 cycles

FWD SVC DOOR EMERGENCY EXIT LIGHT WOULD NOT EXTINGUISH. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,987 hrs · 51,974 cycles

OVERHEAD BULL NOSE EXIT LIGHT INOP AT ROW 1 & 2 DEF. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,344 hrs · 51,415 cycles

DURING WALK AROUND INSPECTION, FOUND 4 INCH LONG FUSELAGE SKIN CRACK AT BS 528, BELOW STR 6R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,278 hrs · 51,358 cycles

FUSELAGE SKIN CRACKED BS 380, STR 4L AND BS 460 STR 4L. MX FERRY TO PHX AND REPAIRED SKIN PER SRM.

Part: BRACKET — OUT OF ADJ (ENTRY DOOR) · airframe 50,745 hrs · 50,895 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE ASSY WOULD NOT ARM. ADJUSTED GIRT BRACKET ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT AFT SVC DOOR, FWD LOWER CORNER CUTOUT. REPAIRED SKIN PER SWA RA.

Part: DOOR FRAME — CRACKED (ENTRY DOOR) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FRAME CRACKED AT UPPER FWD LATCH ATTACHMENT POINT. REMOVED AND REPLACED FWD ENTRY DOOR PER MM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR FWD FRAME CRACKED AT ASSIST CABLE PULLEY LOWER ATTACH BOLT. REMOVED AND REPLACED CARGO DOOR PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 17 TO LBL 29. REPAIRED BULKHEAD PER SWA ACO.

Part: SKIN — CRACKED (RT SLAT) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 6 L/E SLAT SKIN CRACKED AT OUTBOARD TRACK CUTOUT, AFT ROW OF RIVETS. REMOVED AND REPLACED NR 6 SLAT PER PER MM.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 5 SPOILER DELAMINATED ON BOTTOM CORNER. REMOVED AND REPLACED NR 5 SPOILER PER MM.

Part: SKIN — DELAMINATED (FLAP) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBD AFT FLAP INBD CORNER DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL T-CHORD CRACKED AT LBL 5.7, WL 184. REPAIRED T-CHORD PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAMS CORRODED AT BS 727D+4, RBL 2.5, BS 867, LBL 7.5, BS 858 TO 861, LBL 7.5 TO LBL 12. REPAIRED BEAMS PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 3 EXTERNAL FUSELAGE SKIN CRACK AT BS 907, STR 4L. REPAIRED SKIN PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 5 FUSELAGE SKIN CRACKS AT FASTENER HOLES, BS 907, STR 4L (AT DOUBLER). REPAIRED SKIN PER SWA RA.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STR SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: SKIN — CRACKED (LT SLAT) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 SKIN CRACKS AT NR 1 L/E SLAT FASTENER HOLES. REPAIRED SLAT PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STR 26L CORRODED AT BS 827, 847 & 867. REPAIRED STRINGER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 907, STR 27L TO STR 27R, FWD SIDE. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (LT T/E FLAP) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT WING INBD T/E AFT FLAP DELAMINATED AT OUTBD AFT EDGE. REPAIRED AFT FLAP PER SRM.

Part: BEAM — CRACKED (BULKHEAD) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT LBL 17.1, WL 227. REPAIRED VERTICAL BEAM WEB PER SWA ACO.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STR 26R CORRODED BETWEEN BS 827 TO BS 870. REPAIRED STR PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME ANGLE CORRODED AT BS 500D, STR 27R. REMOVED AND REPLACED FRAME ANGLE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 400, RBL 14. REPAIRED FLOORBEAM PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 BS 178 BULKHEAD WEB CRACK, BEHIND DOUBLER, AT RBL 5.9, WL 201. REPAIRED BULKHEAD WEB PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STR 27R CORRODED AT BS 500D. REPAIRED STR PER SRM.

Part: BEAM — DAMAGED (BULKHEAD) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM LOWER WEB DAMAGED AT RBL 5.7, WL 187. REPAIRED VERTICAL BEAM WEB PER SWA RA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM LOWER LT CHORD CORRODED AT BS 500D + 4. REPAIRED KEEL BEAM PER SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 50,745 hrs · 50,895 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 1.5 BS 178 BULKHEAD VERTICAL BEAM CRACK AT RBL 17.1, WL 227. REMOVED AND REPLACED VERTICAL BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,709 hrs · 50,860 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 932, STR 22L. REPAIRED SKIN PER SRM.

Part: RETAINER — LOOSE (GIRT BAR) · airframe 50,453 hrs · 50,646 cycles

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

Part: TAB — DELAMINATED (AILERON) · airframe 50,120 hrs · 50,372 cycles

DURING SCHEDULED A1 CHECK, FOUND RT WING AILERON TAB AFT EDGE DELAMINATED. R&R TAB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,120 hrs · 50,372 cycles

DURING SCHEDULED A1 CHECK, FOUND 1.25 EXTERNAL FUSELAGE SKIN CRACK AT BS 500C, STR 10R. REPAIRED SKIN PER SRM.

Part: RETAINER — LOOSE (SERVICE DOOR) · airframe 50,120 hrs · 50,372 cycles

FWD SVC DOOR GIRT ASSY RETAINER HOOKS LOOSE. SECURED RETAINER HOOKS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,120 hrs · 50,372 cycles

DURING SCHEDULED A1 CHECK, FOUND APPROX 4 EXTERNAL FUSELAGE SKIN CRACK AT BS 780 ABOVE STR 19R. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 50,058 hrs · 50,323 cycles

RED EEPLS LENS MISSING AT OVERWING EXIT. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 49,984 hrs · 50,273 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 49,555 hrs · 49,921 cycles

DURING SCHEDULED C4 CHECK, FOUND 1.5 INCH CRACK ON LT HORIZ STAB LOWER SKIN, FWD OF AFT SPAR. REPAIRED SKIN PER SRM.

Part: DUCT — BROKEN (RT A/C BAY) · airframe 48,216 hrs · 48,767 cycles

DIVERSION, RT WING BODY OVERHEAT LIGHT ILLUMINATED. FOUND RT A/C PRIMARY HEAT EXCHANGER DUCT, LOWER ATTACH FLANGE BROKEN. REPAIRED DUCT PER MM.

Part: LENS — CRACKED (PRESS INDICATOR) · airframe 47,795 hrs · 48,411 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR GLASS CRACKED. R&R SLIDE ASSY PER MM.

Part: SCREW — MISSING (FUSELAGE) · airframe 47,795 hrs · 48,411 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD LT EXTERIOR EMERGENCY EXIT LIGHT LENS SCREW MISSING. INSTALLED SCREW PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,670 hrs · 48,306 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED 2 INCHES LONG, BS 747, STRINGER 18 RT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 518)

DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED, BS 518, STRINGER 12L. REPAIRED PER SRM.

Part: COVER — FAILED (PASSENGER DOOR)

AIR TURNBACK, VERY LOUD NOISE AT FWD ENTRY DOOR DURING FLIGHT. REMOVED AND REPLACED UPPER HINGE COVER ON FWD ENTRY DOOR.

Part: COVER — MISSING (ROW 13-14)

COVER MISSING ON EMERGENCY EXIT LIGHT BY OVERHEAD BIN BETWEEN ROWS 13-14. INSTALLED LENS COVER PER MM.

Part: SKIN — DELAMINATED (RT TE FOREFLAP)

DURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD FOREFLAP DELAMINATED AT 3 PLACES JUST INBOARD OF OUTBOARD END. REMOVED AND REPLACED FOREFLAP ASSY PER MM.

Part: INDICATOR — FLUCTUATES (NR 1 FUEL FLOW)

NR 1 ENG FUEL FLOW INDICATOR NEEDLE FLUCTUATES RAPIDILY AND INDICATES 7-800 PPH HIGHER THAN DIGITAL INDICATOR. REMOVED AND REPLACED FUEL FLOW INDICATOR PER MM.

Part: INDICATOR — INOP (C/P)

ON TAKEOFF FLAPS WOULD NOT COME UP, RETRACTION STOPPED BETWEEN 0 AND 1 POSITION. ELECTRIC FLAPS LOWERED FLAPS TO 10 DEG FOR LANDING. AIRCRAFT RETURNED TO LBB. FLAPS WERE SYMMETRICAL AND RETRACTED NORMAL ON THE GROUND UNDER HYD POWER. REMOVED AND REPLACED POSITION INDICATOR PER MM, OPS CK NORMAL. CLEANED CANNON PLUGS TO BOTH TRANSMITTERS.

Part: MODULE — INOP (PRESSURE SYST)

AFTER TAKEOFF, PRESSURIZATION SYSTEM FAILED. RETURNED TO BWI AND MADE AN UNVENTFUL LANDING. REMOVED AND REPLACED PRESSURIZATION CONTROL MODULE PER BOEING M/M.

Part: BULKHEAD WEB — CRACKED (BS 1016)

DURING SCHEDULED SC CHECK, FOUND 2 CRACK INDICATIONS BETWEEN STR 7R AND 5L ON AFT ROW OF FASTENERS OF BS 1016 AFT PRESSURE BULKHEAD. REMOVED DAMAGED WEB, FABRICATED, FIT, DRILLED AND INSTALLED REPAIR PARTS PER TRAMCO EWO 99-0138.

Part: SKIN — CRACKED (L-1 DOORWAY)

DURING SCHEDULED A1 CHECK, FOUND L-1 DOOR FUSELAGE LOWER CUTOUT CRACKED APPROX 10. REPAIRED PER SWA RA 1-353-1910.

Part: ANGLE — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 LT CHORD ANGLE CRACKED AT WL 207. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (CARGO DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND FWD CARGO DOOR WEB CRACKED AT AFT LOWER CORNER SIDE. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 663)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED PRESSURE DECK (FLOORBEAM) AT BS 663, RBL 41.0. REPAIRED PER BOEING SRM.

Part: RIB — CRACKED (RT WING)

DURING SCHEDULED 1/2D CHECK, FOUND UPPER I/B, T/E PANEL RIB CRACKED. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 270)

DURING SCHEDULED 1/2D CHECK, FOUND ANGLE AT BS 270 CORRODED BENEATH NUT PLATES LBL 10 TO RBL 10. REPAIRED PER TI-A53-02.

Part: ANGLE — CRACKED (RT WING)

DURING SCHEDULED 1/2D CHECK, FOUND BOTTOM WEB ANGLE CRACKED JUST FWD FROM O/B SIDE AILERON. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 433)

DURING SCHEDULED 1/2D CHECK, FOUND SKIN CUTOUT FOR NR 2 LRR XMIT ANTENNA CRACKED AT AFT END OF ANTENNA AT BS 433. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 986-1006)

DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CLIP NUT HOLES CORRODED AT BS 986-1006, LBL 14. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 927-947)

DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CRACKED AT BS 927 TO 947, BL0. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (E/E COMPT)

DURING SCHEDULED 1/2D CHECK, FOUND LEFT FWD E1-2 RACK MOUNT CRACKED AT SCREW HOLE. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 250)

DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL FOR NLG VIEWER CRACKED AT FWD LT SIDE BELOW COCKPIT FLOOR AT BS 250 LBL5. REPAIRED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 837)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED STR 25L AT BS 837. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED 1/2 D-CHECK, FOUND SKIN CRACKED AT BS 727, STR 19R. REPAIRED PER BOEING SRM.

Part: CLIP — CORRODED (BS 986)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED AT CLIP NUT HOLE AT BS 986, RBL 44. REMOVED AND REPLACED PER TYPICAL REPAIR TI-A53-014.

Part: DOUBLER — CRACKED (BS 663)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED DOUBLER BS 663, LBL 65. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 927-1016)

DURING SCHEDULED 1/2 D-CHECK, FOUND RT Z-ANGLE CORRODED ON SURFACE FROM BS 927-1016. REPAIRED PER BOEING SRM.

Part: WEB — BENT (BS 360 - 380)

DURING SCHEDULED 1/2 D-CHECK, FOUND WEB BENT AT STR 17L BETWEEN BS 360 AND 380. REPAIRED PER BOEING SRM.

Part: DOUBLER — CRACKED (BS 663)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED DOUBLER AT BS 663, RBL 65. REMOVED AND REPLACED PER BOEING SRM.

Part: CLIP — CRACKED (BS 667)

DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 667 STR 10R. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CORRODED (FUSELAGE)

DURING SCHEDULED 1/2 D-CHECK, FOUND SKIN CORRODED AT DME ANT FWD CARGO LOWER SKIN. REMOVED AND REPLACED PER BOEING SRM.

Part: CLIP — CRACKED (BS 706)

DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER CLIP CRACKED AT BELTFRAME BS 706, STR 11R AND BS 727A, STR 15R. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 375)

DURING SCHEDULED 1/2 D-CHECK, FOUND WEB ATTACH T-ANGLE CRACKED AT BS 375, STR 17L. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 360.)

DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 16L CRACKED AT BS 360. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 294.5)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED RAMER ANGLE AT BS 294.5 STR 5-7R IN TOP CORNER. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 773)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM AT BS 773, LBL 5 CORRODED AT NUT PLATE HOLES. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 773)

DURING SCHEDULED 1/2 D-CHECK, FOUND AFT CARGO FLOOR SUPPORT BEAM AT BS 773, RBL 5 CORRODED AT NUT PLATE HOLES. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 663)

DURING SCHEDULED 1/2 D-CHECK, FOUND CENTER SECTION FLOOR WEB CRACKED AT BS 663, LBL 22. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 639)

DURING SCHEDULED 1/2 D-CHECK, FOUND FRAME TO STRINGER WEB CRACKED ON BOTTOM SIDE AT BS 639, STR 15L. REMOVED AND REPLACED PER BOEING SRM.

Part: CLIP — CRACKED (BS 663)

DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 305-344)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED Z ANGLE AT BS 305 TO 344, LBL 64. REMOVED AND REPLACED PER BOEING SRM.

Part: BELTFRAME — CRACKED (BS 639)

DURING SCHEDULED 1/2 D-CHECK, FOUND BS 639 BELTFRAME WEB CRACKED IN TWO LOCATIONS AT STR 17R. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 639)

DURING SCHEDULED 1/2 D-CHECK, FOUND BS 639 BELTFRAME I/B L-ANGLE CRACKED AT STR 17R. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED 1/2 D-CHECK, FOUND BS 178 SKIN CRACKED AT LBL 5.7, WL 197 - 205 AND RBL 5.7, WL 201. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — BROKEN (AFT CARGO)

DURING SCHEDULED SERVICE CHECK, FOUND AFT CARGO DOOR INTERCOSTAL BROKEN. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED 1/2 D-CHECK, FOUND BS 178 SKIN CRACKED AT RBL 5.7. WL 198.5. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 291.5)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED ANGLE AT BS 291.5, STR 12R. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CANNED (BS 178)

DURING SCHEDULED 1/2 D-CHECK, FOUND BS 178 SKIN OIL CANNED AT BL 0 WL 201 TO WL 195. REPAIRED PER BOEING SRM.

Part: CLIP — DAMAGED (BS 460)

DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER CLIP AT BS 460, STR 23L DAMAGED. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 294-312)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED IN AND AROUND HOLES IN ANGLE AT BS 294 TO 312, RBL 16. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — DAMAGED (BS 328 & 344)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL BETWEEN BS 328 AND 344 RBL 11. REMOVED AND REPLACED PER BOEING SRM.

Part: CLIP — DAMAGED (BS 460)

DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER CLIP AT BS 460, STR 24L DAMAGED. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 500)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED T-ANGLE AT BS 500A TO 500D. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD ANGLE — CORRODED (BS 500)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED L-ANGLE FOR FLOORBOARD AND CENTER BULKHEAD PANEL AT BS 500D, STR 25L TO 25R. REMOVED AND REPLACED PER BOEING SRM. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 440-500)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED LT TRANSITION ANGLE NUT PLATE HOLES AT BS 440-500. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 328-344)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORROSION IN AND AROUND HOLES IN INTERCOSTAL AT BS 328 - 344, LBL 11. REMOVED AND REPLACED PER BOEING SRM.

Part: FASTENER — CORRODED (BS 967)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORROSION AROUND FASTENER AT BS 967, RBL 17. REPAIRED PER BOEING TI-A53-14. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 294-312)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED IN AND AROUND HOLES IN INTERCOSTAL AT BS 294 TO 312, LBL 11. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED 1/2 D-CHECK, FOUND BS 178 SKIN CRACKED AT FASTENER HOLE WL 234, RBL 10; WL 234, RBL 11 AND WL 234, LBL 9. REMOVED AND REPLACED PER BOEING SRM. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 847)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED AND DENTED WEB AT BS 847, STR S24 AND S25R. REPAIRED PER BOEING SRM. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED 1/2 D-CHECK, FOUND BS 178 SKIN CRACKED AT FASTENER HOLE WL 234, RBL 8. REPAIRED PER BOEING TI-A53-015.

Part: ANGLE — CORRODED (BS 420-440)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED TRANSITION ANGLE RT AT BS 420-440. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 967-986)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL CLIP NUT HOLES AT BS 967-986, LBL 18. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 1006-1016)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL AT BS 1006-1016, LBL 7. REMOVED AND REPLACED PER BOEING SRM. REPAIRED PER BOEING SRM.

Part: CLIP — CRACKED (BS 947)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED STR CLIP AT BS 947 STR 24L. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 986-1006)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL CLIP NUT HOLES AT BS 986-1006, BL 0. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 947-967)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL CLIP NUT HOLES AT BS 947-967, LBL 18 AND 947-967, RBL 18. REPAIRED PER BOEING SRM. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 947)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED CLIP NUT HOLE AT BS 947, LBL 15 AND BS 947, RBL 15. REPAIRED PER TI-A53-04. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (FUSELAGE)

DURING SCHEDULED 1/2 D-CHECK, FOUND SKIN PLATE I/B OF LT HORIZ STAB GOUGED/WORN. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — GOUGED (FUSELAGE)

DURING SCHEDULED 1/2 D-CHECK, FOUND SKIN PLATE I/B OF RT HORIZ STAB GOUGED/WORN. REMOVED AND REPLACED PER BOEING SRM.\N\N\N\N\N\N\N\N\N\N\N\N\N\N\NREPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 950)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL CLIP NUT HOLES AT BS 950, RBL 40. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 500)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED RT AFT TRANSITION ANGLE AT BS 500A TO 500D. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 380)

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 380, STR 22L, WL 170. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 300.9)

DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT BS 300.9 WL 257 LBL 53. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 327)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SERVICE DOORWAY AFT LOWER SKIN CUTOUT AT BS 327, WL 210. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 294)

DURING SCHEDULED D-CHECK, FOUND WEB INTERCOSTAL CRACKED AT BS 294, WL 216, LBL 57. REPAIRED PER BOEING SRM.

Part: SLIDE — OUT OF DATE (CABIN)

DURING SCHEDULED C2 CHECK, FOUND L-2 EMERGENCY EVACUATION SLIDE OUT OF DATE. REMOVED AND REPLACED PER BOEING MM.

Part: SKIN — CRACKED (RT LE FLAP)

DURING SCHEDULED C2 CHECK, FOUND CRACK ON L/E SKIN AT KRUEGER FLAP SEAL DOOR CUTOUT. REPAIRED PER SWA RA 1-357-0538.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED TERM CHECK, FOUND 6 IN FUSE SKIN CRACK RT SIDE ABOVE AND AFT OF NR 12 CABIN WINDOW. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 943)

DURING SCHEDULED TERM CHECK, FOUND 1.5 CRACK IN FUSELAGE EXTERIOR SKIN BS 943 STR 24L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 213)

DURING SCHEDULED C1 CHECK, FOUND RIGHT AFT SERVICE DOOR FRAME LOWER HINGE CUTOUT CRACKED FROM RADIUS UNDER EXISTING DOUBLER. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (WS 213.0)

DURING SCHEDULED C1 CHECK, FOUND RIGHT AFT SERVICE DOOR FRAME LOWER HINGE CUTOUT CRACKED FROM RADIUS UNDER EXISTING DOUBLER. REPAIRED PER BOEING SRM.

Part: SWITCH — INOPERATIVE (COCKPIT)

DURING SCHEDULED RON CHECK, FOUND E TRACK LIGHTS INOP. REPLACED OVERHEAD SWITCH IN COCKPIT PER BOEING M/M.

Part: START VALVE — MALFUNCTIONED (NR 2 ENGINE)

AT FL330, NR 2 ENGINE START VALVE OPEN LIGHT ILLUMINATED, UNABLE TO MAINTAIN CABIN PRESSURE. DESCENDED TO 8,000 FT, START VALVE LIGHT EXTINGUISHED. ON ANOTHER ATTEMPT TO USE NR 2 BLEED AT FL 290, SAME SCENARIO OCCURED. DESCENDED TO FL 250, ALL OPERATED OK FOR REMAINDER OF FLIGHT. INSPECTED AND REPLACED NR 2 ENGINE START VALVE AND PRESSURE CHECKED PER BOEING M/M.

Part: FLOORBEAM — CRACKED (E/E BAY)

DURING SCHEDULED C1 CHECK, FOUND FLOORBEAM STRAP CRACKED IN RIGHT FWD E AND E BAY COMPARTMENT. REPAIRED PER SWA RA 1-353-1136.

Part: CONTROLLER — FAILED (E/E BAY)

RETURNED DUE TO RT WING/BODY OVERHEAT ILLUMINATING. AFTER ISOLATING SYSTEM, AIRCRAFT WOULD NOT HOLD PRESSURIZATION. REMOVED AND REPLACED PRESSURE CONTROLLER AND CONTROL PANEL PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT ROW 3DEF INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/M.

Part: STRAP — CRACKED (ENTRY DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND FLOORBEAM STRAP UNDERNEATH FWD ENTRY DOOR CRACKED. REPAIRED PER BOEING SRM.

Part: SPLICE — LOOSE (NLG)

IN FLIGHT, RED NOSE GEAR LIGHT ILLUMINATED, NO AIR NOISE NOTED. CYCLED GEAR HANDLE, NO HELP. ON GEAR EXTENSION HAD ALL GREEN INDICATION. INSPECTED AND FOUND A WIRE PULLED FROM SPLICE IN NOSE W/W. REPAIRED PER BOEING M/M.

Part: EEL BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRYWAY EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK AND HOUSING PER BOEING M/M.