N315SW

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 328, STR 26L. REPAIRED STRINGER PER SRM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT 3RD STOP FITTING CUTOUT FROM BOTTOM. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 517, STR 28L. REPAIRED STRINGER PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 1006, RBL 45. REMOVED AND REPLACED WEB PER ER AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 670, LBL 25. REPAIRED CHORD PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 25. REPAIRED CHORD PER ER AND WA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER FWD FLANGE CRACKED AT BS 947, LBL 54. REPAIRED BEAM PER ER AND WA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 662, RBL 24.8. REPAIRED WEB PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 500B, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CHORD CRACKED BETWEEN BS 709 TO BS 713, LBL 25. REPAIRED CHORD PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 456, STR 26L. REPAIRED STRINGER PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CHORD CRACKED AT BS 664, BBL 0. REPAIRED CHORD PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CHORD CRACKED AT BS 727B, RBL 45. REPAIRED CHORD PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 663, STR 3L. REPAIRED FRAME PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B-4, LBL 45. REPAIRED CHORD PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER EA.

Part: SHEAR TIE — CRACKED (BS 727D S13-14L) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 727D, BETWEEN STR 13L TO STR 14L. REPAIRED SHEAR TIE PER ER AND EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 440, BETWEEN STR 13R TO STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 315, STR 25L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CRACKED BETWEEN BS 902 TO BS 910, STR 8R. REMOVED AND REPLACED SPLICE PER SRM AND BAC DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 664, BL 0. REPAIRED WEB PER SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 908, STR 4R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 515, STR 21R. REPAIRED SKIN PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED CLIP PER EA.

Part: FLOOR SUPPORT — CRACKED (BS 664) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BS 664, RBL 25. REPAIRED WEB PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 13L. REMOVED AND REPLACED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7R. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 2R. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (BS 597 S8L) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9R. REMOVED AND REPLACED CLIP PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED BS 694, BL 0. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 7R. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 3L. REMOVED AND REPLACED CLIP PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 706 TO BS 716, BL 0. REPAIRED WEB PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 663, STR 2L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8L. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 767, STR 13L. REPAIRED FRAME PER EA.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND PRESSURE DECK CRACKED AT BS 672, RBL 41. REPAIRED DECK PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10L. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 10L. R&R CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 5R. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10L. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

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

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 639, RBL 69. REPAIRED WEB PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10L. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 3R. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, RBL 1. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, LBL 18. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED BETWEEN BS 464.5 TO BS 466, STR 16L. REPAIRED SKIN PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 507, STR 22R. REPAIRED STRINGER PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,572 hrs · 70,904 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,131 hrs · 70,547 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 731D, STR 20L. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26R TO 25R. REPAIRED FRAME PER EA.

Part: FRAME SPLICE — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND FRAME SPLICE CORRODED AT BS 747, BETWEEN STR 27L TO 26L. REPAIRED SPLICE PER EA.

Part: FRAME SPLICE — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND FRAME SPLICE CORRODED AT BS 747, BETWEEN STR 26L TO 25L. REPAIRED SPLICE PER EA.

Part: FRAME SPLICE — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND FRAME SPLICE CORRODED AT BS 747, BETWEEN STR 23L TO STR 26R. REPAIRED SPLICE PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER CORRODED BETWEEN BS 787 TO BS 807, STR 23L. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FRAME SPLICE — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND FRAME SPLICE CORRODED AT BS 747, BETWEEN STR 27R TO 23R. REPAIRED SPLICE PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND FLOORBEAM CORRODED AT BS 747, RBL 14. REMOVED AND REPLACED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CORRODED AT BS 767E, BETWEEN STR 27R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND FLOOR SUPPORT CHANNEL CORRODED AT BS 784, LBL 12. REPAIRED CHANNEL PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND FRAME SPLICE CORRODED AT BS 787, BETWEEN STR 23L TO STR 23R. REPAIRED FRAME PER EA.

Part: LIGHT — CORRODED (CABIN) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS CORRODED AT BS 943, LBL 17. REMOVED AND REPLACED EEPLS PER MM.

Part: FRAME SPLICE — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT CARGO FRAME SPLICE CORRODED AT BS 767. REPAIRED FRAME PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND FRAME CORRODED AT BS 847, BETWEEN STR 17R TO STR 27R. REMOVED AND REPLACED FRAME PER ACO.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER SPLICE CORRODED AT BS 793, STR 26R. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER SPLICE CORRODED AT BS 870, STR 26R. REMOVED AND REPLACED SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND FRAME CRACKED AT BS 827, STR 25L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER CORRODED BETWEEN BS 807 TO BS 827, STR 24L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER CORRODED BETWEEN BS 767 TO BS 787, STR 24L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER 25L CORRODED AT BS 767 TO BS 787. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 872, STR 17R. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER CORRODED BETWEEN BS 867 TO BS 887, 23L. REPAIRED STRINGER PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND FRAME CRACKED AT BS 807, STR 25L. REPAIRED FRAME PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND FLOORBEAM CORRODED AT BS 777, RBL 8. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND FLOORBEAM CORRODED AT BS 777, RBL 3. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND FLOORBEAM CORRODED AT BS 777, LBL 3. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND FLOORBEAM CORRODED AT BS 777, LBL 8. REPAIRED BEAM PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER CORRODED BETWEEN BS 948 TO BS 969, STR 27L. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CORRODED AT BS 986, STR 19R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND FRAME CRACKED AT BS 986, STR 19R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,107 hrs · 70,527 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 860, STR 17R. REPAIRED SKIN PER SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 77,025 hrs · 70,469 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 77,025 hrs · 70,469 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 76,983 hrs · 70,433 cycles

LEFT EXIT SIDEWALL SIGN BROKEN AT MID CABIN. REMOVED AND REPLACED SIGN ASSY PER.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 76,827 hrs · 70,302 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT LT EXTERNAL EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 76,597 hrs · 70,124 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,322 hrs · 69,910 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 76,250 hrs · 69,853 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT LT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 76,005 hrs · 69,677 cycles

DURING SCHEDULED MV2 CHECK EMERGENCY EXIT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,908 hrs · 69,612 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,908 hrs · 69,612 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 740C, STR 14R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,843 hrs · 69,566 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR, BS 353, STR 16R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,843 hrs · 69,566 cycles

DURING SCHEDULED MV2 CHECK, FOUND FRAME CRACKED AT BS 400, STR 16R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,843 hrs · 69,566 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 393, STR 15R. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,843 hrs · 69,566 cycles

DURING SCHEDULED MV2 CHECK, FOUND FRAME CRACKED AT BS 380, STR 16R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 75,843 hrs · 69,566 cycles

DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CRACKED AT BS 400, BETWEEN STR 16R TO STR 17R. REPAIRED SHEAR TIE PER BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,843 hrs · 69,566 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 366, STR 16R. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 75,242 hrs · 69,096 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,296 hrs · 69,135 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 504B, STR 10L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 75,162 hrs · 69,038 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,740 hrs · 68,735 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 507B, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,740 hrs · 68,735 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 327, BETWEEN STR 7R TO STR 8R. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,606 hrs · 68,634 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD LT EMERGENCY EXIT BULLNOSE LIGHT INOP. RELAMPED PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 74,310 hrs · 68,424 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 73,940 hrs · 68,169 cycles

DURING SCHEDULED SPV CHECK, FOUND KEEL BEAM CORRODED BETWEEN BS 515 TO BS 520, LBL 7. REMOVED AND REPLACED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,940 hrs · 68,169 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 520, LBL 9, WL 147. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 73,940 hrs · 68,169 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT AFT SIDE FRAME CRACKED AT BS 492, RBL 67. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,940 hrs · 68,169 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED BETWEEN BS 5016C TO BS 503D, STR 27L. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,940 hrs · 68,169 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 23R CRACKED AT BS 456, RBL 45. REPAIRED STRINGER PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 73,891 hrs · 68,140 cycles

LT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 8. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,288 hrs · 67,698 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER AFT CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,261 hrs · 67,682 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 269.5, STR 6R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,261 hrs · 67,682 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 460 S16L) · airframe 73,261 hrs · 67,682 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 460, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 500A S16L) · airframe 73,261 hrs · 67,682 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, STR 16L. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,941 hrs · 67,465 cycles

DURING SCHEDULED MV3 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 72,502 hrs · 67,137 cycles

L1 COCKPIT WINDOW ARCING. REMOVED AND REPLACED L1 WINDOW AND CONTROLLER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,159 hrs · 66,895 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 780 AND BS 813, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,159 hrs · 66,895 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 764 AND BS 774, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,159 hrs · 66,895 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 25R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,156 hrs · 66,984 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,156 hrs · 66,984 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,156 hrs · 66,894 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED FWD SERVICE DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,156 hrs · 66,894 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 12R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CRACKED (BS 967) · airframe 72,156 hrs · 66,894 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 967, LBL 49. REPAIRED WEB PER SRM.

Part: FITTING — CRACKED (R2 DOOR SLIDE) · airframe 72,156 hrs · 66,894 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,156 hrs · 66,894 cycles

DURING SCHEDULE 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 8R. REPAIRED SKIN PER SRM.

Part: FITTING — WORN (RT MLG) · airframe 71,599 hrs · 66,496 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT MLG UNIVERSAL FITTING WORN. REMOVED AND REPLACED FITTING PER MM.

Part: SKIN — DELAMINATED (L/E SLAT) · airframe 71,484 hrs · 66,411 cycles

DURING SCHEDULED CV CHECK, FOUND LT WING NR 4 L/E SLAT DELAMINATED AT UPPER SURFACE. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,484 hrs · 66,411 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 910, STR 19L. REPAIRED SKIN PER SRM.

Part: FEEL UNIT — FAULTY (ELEVATOR) · airframe 70,252 hrs · 65,508 cycles

DURING ROTATION A 2 INCH DEAD BAND INDICATION IN ELEVATOR. REMOVED AND REPLACED ELEVATOR FEEL & CENTERING UNIT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,806 hrs · 65,921 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 580, STR 9R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,794 hrs · 65,912 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,794 hrs · 65,912 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,794 hrs · 65,912 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,794 hrs · 65,912 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FITTING — CORRODED (MLG W/W) · airframe 70,677 hrs · 65,821 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG SIDE SUPPORT FITTING LUG CORRODED AT BS 685. REPAIRED FITTING PER SWA EA.

Part: FITTING — CORRODED (MLG W/W) · airframe 70,677 hrs · 65,821 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG SIDE SUPPORT FITTING LUG CORRODED AT BS 685. REPAIRED FITTING PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,617 hrs · 65,772 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 700, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,617 hrs · 65,772 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514B, STR 18R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,170 hrs · 65,454 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 436, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 751 S14R) · airframe 69,997 hrs · 65,322 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 751, STR 14R. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,765 hrs · 65,129 cycles

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

Part: WINDOW — CRACKED (COCKPIT) · airframe 69,748 hrs · 65,114 cycles

AT FL 330 FLIGHT DECK R1 WINDOW ARCED THEN OUTER WINDOW PANE CRACKED. REMOVED AND REPLACED WINDOW PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 69,525 hrs · 64,940 cycles

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

Part: SKIN — CRACKED (BS 913 S21L) · airframe 69,002 hrs · 64,539 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 913, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 790 S18L) · airframe 69,002 hrs · 64,539 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 790, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 485 S16L) · airframe 69,002 hrs · 64,539 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 485, STR 16L. REPAIRED SKIN PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 69,002 hrs · 64,539 cycles

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

Part: SKIN — CRACKED (BS 930 S23L) · airframe 69,002 hrs · 64,539 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 23L. REPAIRED SKIN PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,155 hrs · 63,862 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 934 S20L) · airframe 68,155 hrs · 63,862 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 20L. REPAIRED SKIN PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,155 hrs · 63,862 cycles

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

Part: SKIN — CRACKED (BS 734A S21L) · airframe 68,155 hrs · 63,862 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 734A, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 740A S14L) · airframe 68,155 hrs · 63,862 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740A, STR 14L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,054 hrs · 63,785 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,054 hrs · 63,785 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 912, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,054 hrs · 63,785 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 422, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,054 hrs · 63,785 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 395, STR 14L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 986 S24L) · airframe 67,596 hrs · 63,466 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 986, STR 24L. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 67,576 hrs · 63,450 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD CABIN EMERGENCY EXIT SIGN LENS LOOSE. SECURED SIGN LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,576 hrs · 63,450 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 517D, STR 16L. REPAIRED SKIN PER SWA EA.

Part: LENS — MISSING (CABIN) · airframe 67,576 hrs · 63,450 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,576 hrs · 63,450 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 386, STR 17L. REPAIRED SKIN PER SRM.

Part: LENS — DETERIORATED (CABIN) · airframe 67,576 hrs · 63,450 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 66,815 hrs · 62,863 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,417 hrs · 62,549 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506D, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 66,021 hrs · 62,228 cycles

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

Part: TAB — CRACKED (RT ELEVATOR) · airframe 65,891 hrs · 62,128 cycles

AIRFRAME VIBRATION INCREASING IN INTENSITY FROM TAIL SECTION AT SPEEDS IN EXCESS OF 245 KNOTS. NO ATTITUDE ROLL OFF NOTED AT ANYTIME. REMOVED AND REPLACED RT ELEVATOR CONTROL TAB PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR CUTOUT, FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 65,862 hrs · 62,108 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR CUTOUT, FWD FRAME CRACKED AT NR 5 LOWER DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED EMERGENCY FLASHLIGHT PER MM.

Part: LAMP — LOOSE (EMERGENCY LIGHT) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND SIDEWALL EMERGENCY EXIT LIGHT INOP AT R1 DOOR. SECURED LIGHT BULB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17R AND STR 17L. REPAIRED FRAME SECTION PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,862 hrs · 62,108 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 8R CRACKED AT BS 344. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 13L CRACKED AT BS 300. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17L. REPAIRED FRAME SECTION PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, LBL 6 TO RBL 6. REPAIRED FRAME SECTION PER SRM.

Part: FITTING — CORRODED (L1 DOOR) · airframe 65,862 hrs · 62,108 cycles

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

Part: FITTING — CORRODED (L1 DOOR) · airframe 65,862 hrs · 62,108 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 867, LBL 6 TO RBL 6. REPAIRED FRAME SECTION PER SRM.

Part: FITTING — WORN (HORIZ STAB) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT HORIZONTAL STAB AFT UPPER SPAR FITTING LUG WORN. REMOVED AND REPLACED STAB FITTING PER MM.

Part: CABLE — FRAYED (R2 DOOR) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED EVAC SLIDE CABLE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20R. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 26L CORRODED AT BS 825. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 26R CORRODED AT BS 819. REPAIRED STRINGER SECTION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 8R CRACKED AT BS 825. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER — CORRODED (BS 825 S26L) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 26L CORRODED AT BS 825. REPAIRED STRINGER SECTION PER SRM.

Part: STRINGER — CORRODED (BS 819 S26R) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 26R CORRODED AT BS 819. REPAIRED STRINGER SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING OUTBOARD FORE FLAP DELAMINATED AT INBOARD LOWER SURFACE. REPAIRED FORE FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 500C S20L) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,862 hrs · 62,107 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 294, LBL 30 TO LBL 55. REMOVED AND REPLACED FLOORBEAM CHORD PER SRM.

Part: FRAME — CRACKED (BS 294 S4L) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294.3, STR 4L. REPAIRED FRAME SECTION PER SRM.

Part: FRAME SPLICE — CORRODED (BS 1016 S26R) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD CHORD SPLICE CORRODED AT BS 1016, STR 26R. REMOVED AND REPLACED BULKHEAD SPLICE PER SRM.

Part: FRAME — CRACKED (BS 867) · airframe 65,862 hrs · 62,102 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, LBL 6 TO RBL 6. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 520 S22L) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 520, STR 22L. REPAIRED FRAME WEB PER SRM.

Part: STRINGER CLIP — CRACKED (BS 294 S13L) · airframe 65,862 hrs · 62,108 cycles

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

Part: CABLE — FRAYED (R2 DOOR SLIDE) · airframe 65,862 hrs · 62,108 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED EVAC SLIDE CABLE PER MM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 64,940 hrs · 61,389 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND RT WING NR 5 L/E SLAT UPPER WEDGE DELAMINATED. REPAIRED SLAT PER SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 64,939 hrs · 61,387 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND LT WING INBD T/E AFT FLAP DELAMINATED AT BOTH SURFACES. REPAIRED FLAP PER SRM.

Part: SKIN — CRACKED (BS 442) · airframe 64,939 hrs · 61,387 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 442, STR 16R. REPAIRED SKIN PER EA & SRM.

Part: DOUBLER — CRACKED (BS 380) · airframe 64,939 hrs · 61,387 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE INTERNAL DOUBLER CRACKED AT E&E COOLING EXHAUST FAN CUTOUT, BS 380, STR 28L. REMOVED AND REPLACED DOUBLER PER SRM.

Part: SKIN — CRACKED (BS 732D) · airframe 64,939 hrs · 61,387 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 732D, STR 14R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (BS 750) · airframe 64,939 hrs · 61,387 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 20R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 578) · airframe 64,939 hrs · 61,387 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 578, STR 10L. REPAIRED SKIN PER SWA EA.

Part: FRAME — CORRODED (BS 960) · airframe 64,939 hrs · 61,387 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CORRODED AT BS 960, BETWEEN STR 27L & STR 27R. REPAIRED FRAME PER SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,939 hrs · 61,387 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (BS 410) · airframe 64,939 hrs · 61,387 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 410, BL 0, NR 2 RADIO ALTIMETER ANTENNA CUTOUT. MX FERRY TO DHN FOR REPAIRS. REPAIRED SKIN PER SWA EA.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,939 hrs · 61,387 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (BS 450) · airframe 64,939 hrs · 61,387 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 450, BL 0, NR 4 RADIO ALTIMETER ANTENNA CUTOUT. MX FERRY TO DHN FOR REPAIRS. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,939 hrs · 61,387 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (BS 430) · airframe 64,939 hrs · 61,387 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 430, BL 0, NR 3 RADIO ALTIMETER ANTENNA CUTOUT. MX FERRY TO DHN FOR REPAIRS. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 390) · airframe 64,939 hrs · 61,387 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 390, BL 0, NR 1 RADIO ALTIMETER ANTENNA CUTOUT. MX FERRY TO DHN FOR REPAIRS. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CRACKED (BS 521) · airframe 64,903 hrs · 61,360 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 520, BETWEEN STR 15L TO STR 16L. REPAIRED SHEAR TIE PER SWA EA.

Part: SKIN — CRACKED (BS 470) · airframe 64,903 hrs · 61,360 cycles

DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 470, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 510) · airframe 64,903 hrs · 61,360 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 514D) · airframe 64,903 hrs · 61,360 cycles

DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 514D, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 64,544 hrs · 61,090 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR PROTRUDING THRU VIEWING WINDOW. REMOVED AND REPLACED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,916 hrs · 60,606 cycles

DURING SCHEDULED C3 CHECK, FOUND BULLNOSE EMERGENCY LIGHTS INOP AT ROW 19 DEF. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SEAL — LEAKING (NR 2 ENG OIL SYS) · airframe 63,749 hrs · 60,466 cycles

ELECTRICAL ODOR IN CABIN FOR APROX 5 MINUTES DURING CLIMB. FOUND NR 2 ENGINE OIL LEAK AT NR 3 OIL BEARING SEAL. MX FERRY TO MDW AND REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: ENGINE — OVERTEMP (NR 2) · airframe 63,570 hrs · 60,310 cycles

AIR TURNBACK, NR 2 ENGINE OVERTEMP AT 990 DEGREES FOR 15 SECONDS. RED OVERTEMP LIGHT ILLUMINATED FOR MORE THAN 1 MINUTE. MX FERRY TO PHX. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 63,250 hrs · 60,051 cycles

EMERGENCY BULLNOSE LIGHT LOOSE AT ROW 8 DEF. SECURED LIGHT PER MM.

Part: SENSOR — FAULTY (NLG) · airframe 63,115 hrs · 59,945 cycles

AIR TURNBACK/DECLARED EMERGENCY. LG POSITION INDICATING LIGHTS ILLUMINATED AFTER GEAR RETRACTION. RECYCLED GEARS, NO HELP. REMOVED AND REPLACED NLG PRIMARY DOWN PROX SENSOR PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 63,115 hrs · 59,945 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,000 hrs · 59,855 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 361, BETWEEN STR 6R & STR 7R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,000 hrs · 59,855 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 359, BETWEEN STR 5R & STR 6R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,000 hrs · 59,855 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 63,000 hrs · 59,855 cycles

DURING SCHEDULED C2 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT INBOARD AFT SPAR. REPAIRED HORIZONTAL STAB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,897 hrs · 59,768 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS BETWEEN BS 740 AND BS 750, STR 18L. REPAIRED SKIN PER SWA EA.

Part: LENS — OUT OF POSITION (EMERGENCY LIGHT) · airframe 62,547 hrs · 59,493 cycles

EMERGENCY EXIT BULLNOSE LIGHT LENS OUT OF POSITION AT ROW 8 DEF. REINSTALLED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 62,049 hrs · 59,080 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,049 hrs · 59,080 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,049 hrs · 59,080 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 350, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,049 hrs · 59,080 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 490, STR 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,049 hrs · 59,080 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, GROUND A/C RECEPTICLE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: BOLT — WORN (LT ELEVATOR) · airframe 61,196 hrs · 58,406 cycles

DURING SCHEDULED C4 CHECK, LT ELEVATOR CONTROL TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR CONTROL TAB BOLT PER MM.

Part: SLIDE — OUT OF ADJUST (L1 & R1 DOORS) · airframe 61,196 hrs · 58,406 cycles

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

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 60,410 hrs · 57,822 cycles

R2 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. INSTALLED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,293 hrs · 57,725 cycles

DURING THRU CHECK FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 466 AND BS 470, ABOVE STRINGER 16R. REPAIRED SKIN SECTIONS PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,203 hrs · 57,643 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 270, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA.

Part: FITTING — WORN (ELEVATOR TAB) · airframe 60,203 hrs · 57,643 cycles

DURING SCHEDULED C3 CHECK, FOUND LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT AND RT NR 1 ELEVATOR TABS HINGE HARDWARE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,203 hrs · 57,643 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 22R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,194 hrs · 57,632 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 22R, CRACKED. REPAIRED SKIN PER EA AND SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 59,943 hrs · 57,424 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 59,901 hrs · 57,388 cycles

R1 AND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENSES, MISSING. REMOVED AND REPLACED LIGHT LENSES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,273 hrs · 56,883 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 500C + 16, BETWEEN STRINGER 15R AND STRINGER 14R, CRACKED. REPAIRED SKIN PER EA.

Part: WEDGE — DELAMINATED (LT WING SLAT) · airframe 59,267 hrs · 56,877 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT T/E WEDGE DELAMINATED. REPAIRED NR 2 L/E SLAT WEDGE PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,940 hrs · 56,617 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 504, STRINGER 21R, CRACKED. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,921 hrs · 56,603 cycles

DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROWS 5 DEF, 2 ABC, INOP. RELAMPED LIGHTS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 58,921 hrs · 56,603 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,446 hrs · 56,197 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 752, STRINGER 20L CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,446 hrs · 56,197 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 917, STRINGER 25L, CRACKED. REPAIRED SKIN PER SRM.

Part: ENGINE — FAULTY (RIGHT) · airframe 58,379 hrs · 56,140 cycles

INFLIGHT SHUTDOWN/AIRTURN BACK, NR 2 ENG OIL PRESSURE WENT TO ZERO AND OIL QUANTITY ALSO WENT TO ZERO. PERFORMED LOW OIL PRESSURE TEST AND ZONE A INSPECTION PER MM. ENGINE IS ON 50 CYCLE REINSPECT PER MX NOTE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,144 hrs · 55,962 cycles

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 2 ABC. RELAMPED EMERGENCY EXIT LIGHT PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 57,901 hrs · 55,787 cycles

EMERGENCY EXIT LIGHT AT ROW 13 DEF SIDE LOOSE. SECURED LIGHT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,567 hrs · 55,516 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD R1 DOOR UPPER HINGE CUTOUT SHOWS CRACK INDICATION. REPAIRED R1 DOOR PER SB.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 57,439 hrs · 55,414 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING INBD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,439 hrs · 55,414 cycles

DURING SCHEDULED C4 CHECK, FOUND 5 EA FUSELAGE SKIN CRACKS AT BS 727E+6, STR 18L, BS 931, STR 21L, BS 919, STR 24L, BS 727E+14, STR 19L, AND BS 931, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 55,029 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A + 6, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,798 hrs · 54,911 cycles

FUSELAGE SKIN CRACKED AT BS 516D, STRINGER 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,428 hrs · 54,609 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) BS 947 AT STR 23R, BS 967 AT STR 21L AND BS 787 AT STR 19L. REPAIRED SKIN PER SRM.

Part: INDICATOR — DAMAGED (SLIDE BOTTLE) · airframe 55,953 hrs · 54,207 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 54,600 hrs · 53,119 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING INBD T/E FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,742 hrs · 52,441 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (4 EA) AT STR 14L, BS 476, BS 510, BS 510B AND BS 518B. MX FERRY TO CYXX, C/W SKIN LAP JOINT MOD PER SWA ACO.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 53,742 hrs · 52,441 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICES CRACKED (2 EA) AT BS 360, STR 14L AND STR 15L. REPAIRED STR SPLICES PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,742 hrs · 52,441 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 4L, BS 510C AND BS 510D. MX FERRY TO CYXX, C/W SKIN LAP JOINT MOD PER SWA ACO.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,742 hrs · 52,441 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CRACKED AT BS 500C, STR 10L. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,742 hrs · 52,441 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (4 EA) AT STR 4R, BS 639, BS 688, BS 700 AND BS 712. MX FERRY TO CYXX, C/W SKIN LAP JOINT MOD PER SWA ACO.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,742 hrs · 52,441 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,741 hrs · 52,439 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIES CRACKED (3 EA) BETWEEN STR 13L AND STR 14L, BS 460, BS 727E AND BS 727B. REPAIRED SHEAR TIES PER SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 53,741 hrs · 52,439 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND AFT UPPER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,741 hrs · 52,439 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT BS 360, STR 4R AND BS 908, STR 10R. REMOVED AND REPLACED TIE CLIPS PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 53,741 hrs · 52,439 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT BS 727E AT STR 9R AND BS 597 AT STR 9L. REMOVED AND REPLACED TIE CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,741 hrs · 52,439 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 12L. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,741 hrs · 52,439 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED AT BS 440, STR 4R. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (MID CABIN) · airframe 53,741 hrs · 52,439 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIES CRACKED (2 EA) AT BS 616, STR 7L AND STR 8L AND STR 7R AND STR 8R. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 53,741 hrs · 52,439 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT STR 4L, BS 616 AND BS 639. REMOVED AND REPLACED STR TIE CLIPS PER SRM.

Part: SHEAR TIE — CRACKED (FWD CABIN) · airframe 53,741 hrs · 52,439 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,729 hrs · 52,431 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR FUSELAGE SKIN AND BEARSTRAP CRACKED AT BOTH UPPER AND LOWER DOOR HINGE CUTOUTS. REPAIRED SKIN AND BEARSTRAP PER SRM AND SWA EA.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 53,729 hrs · 52,431 cycles

DURING SCHEDULED BC4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,729 hrs · 52,431 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 360, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,729 hrs · 52,431 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,729 hrs · 52,431 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 10R. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 53,065 hrs · 51,876 cycles

OVERHEAD BIN BULL NOSE EMERGENCY EXIT LENS MISSING AT ROW NR 22 DEF. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,880 hrs · 51,737 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKS (5 EA) AT BS 500A AT STR 10R, BS 500D AT STR 15R, BS 737 AT STR 18R, BS 757 AT STR 10R AND BS 937 AT STR 24R. REPAIRED SKIN PER SRM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 52,694 hrs · 51,585 cycles

DURING SCHEDULED A2 CHECK,SWA SI 11111-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED TAB NR 1 HINGE BUSHINGS PER MM.

Part: ROD END — CORRODED (ELEVATOR TAB) · airframe 52,694 hrs · 51,585 cycles

DURING SCHEDULED A2 CHECK, FOUND BOTH LT AND RT ELEVATOR TAB ROD ENDS CORRODED INBOARD AND OUTBOARD. REMOVED AND REPLACED ALL ELEVATOR TAB ROD ENDS PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 52,327 hrs · 51,280 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,018 hrs · 51,042 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED 4.5 INCHES LONG AT BS 927, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,018 hrs · 51,042 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 10R, BS'S 500 AND 727B. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LH WING) · airframe 51,102 hrs · 50,304 cycles

DURING SCHEDULED BC1 CHECK, FOUND LH OTBD AFT FLAP DELAMINATED ON INBD END. R&R FLAP PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 51,102 hrs · 50,304 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,646 hrs · 49,936 cycles

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

Part: SOCKET — CORRODED (EXTERIOR) · airframe 50,132 hrs · 49,498 cycles

DURING SCHEDULED PMC CHECK, FOUND FWD ENTRY DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT SOCKET DUE TO CORROSION PER MM.

Part: WEB — CRACKED (AFT BULKHEAD) · airframe 49,920 hrs · 49,310 cycles

DURING SCHEDULED 1/2D CHECK, FOUND WEB CRACKED AT PRESS BULKHEAD BS 1016, RBL 39. R&R WEB SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,920 hrs · 49,310 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED UNDER FLOOR SUPPORT AT BS 859, RBL 8.0. REPAIRED FLOORBEAM PER SWA RA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,920 hrs · 49,310 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 295, LBL 6. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,920 hrs · 49,310 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 727D+6, LBL 12 TO RBL 2.5. REPAIRED PER SWA RA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,920 hrs · 49,310 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 587, STR 10R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: LENS — BROKEN (FUSELAGE) · airframe 49,920 hrs · 49,310 cycles

DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY OVER WING EXIT LIGHT LENS BROKEN. R&R EXIT LIGHT LENS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,920 hrs · 49,310 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 794, LBL 2.5. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,920 hrs · 49,310 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 773, RBL 7.5 TO LBL 2.5. REPAIRED FLOORBEAM PER SWA RA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,920 hrs · 49,310 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 500C, LBL 18 TO RBL 13. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,920 hrs · 49,310 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 9 TO RBL 8. REPAIRED FLOORBEAM PER SWA TI.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,920 hrs · 49,310 cycles

DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL WEBS CRACKED AT BS 180, WL 236, LBL 17.1 & WL 183 RBL 5.7. REPAIRED WEBS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,884 hrs · 49,276 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, ABOVE LAP SEAM BETWEEN WINDOWS # 5 & # 6.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,771 hrs · 49,187 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504.5C, ABOVE STR15L. REPAIRED PER SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 49,350 hrs · 48,825 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD CARGO DOOR .25 INCH SKIN CRACK AT DOOR HANDLE CUTOUT, AFT UPPER CORNER. REPAIRED DOOR SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 49,350 hrs · 48,825 cycles

DURING SCHEDULED C3 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 12 DEF. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,702 hrs · 48,295 cycles

DURING SCHEDULED RON CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACKS AT BS 500C, BETWEEN STR 9R & STR 10R, BS 525, BETWEEN STR 9R & STR 10R. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 48,383 hrs · 48,023 cycles

DURING SCHEDULED C2 CHECK, FOUND LT INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD CORNER. REPAIRED AFT FLAP ASSY PER SRM.

Part: ACTUATOR — FAILED (NLG) · airframe 48,276 hrs · 47,929 cycles

UPON ARRIVAL, NOSE GEAR WOULD NOT EXTEND. MANUALLY EXTENDED GEAR. R&R NLG LOCK ACTUATOR & ACCOMPLISHED GEAR SWING PER MM.

Part: BULB — INOPERATIVE (CABIN) · airframe 47,609 hrs · 47,372 cycles

DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND EEPLS TRACK FWD ENTRY RED LIGHTS INOP. REMOVED AND REPLACED EEPLS BULB PER MM.

Part: LAMP — MISSING (SERVICE DOOR) · airframe 47,609 hrs · 47,372 cycles

DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND FWD SVC DOOR LWR EMERGENCY EXIT SIGN MISSING BULBS. REPLACED BULBS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,482 hrs · 47,269 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR LOWER CUTOUT CRACKED EXTENDING BELOW SKIN DOUBLER. REPAIRED SKIN DOUBLER PER RA 1-353-2368.

Part: LEVER — LACK OF LUBE (COCKPIT) · airframe 47,491 hrs · 47,277 cycles

DURING LANDING, GEAR SELECTED TO DOWN AND BOTH RED AND GREEN LIGHTS ILLUMINATED. CYCLED GEAR AND ONLY GREEN LIGHTS ILLUMINATED. LUBRICATED GEAR LEVER ASSY AND PERFORMED M986 CIRCUIT CARD TEST PER MM.

Part: FRAME — CRACKED (BULKHEAD) · airframe 47,366 hrs · 47,173 cycles

DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND BS 178 BULKHEAD RT SIDE CHORD CRACKED. REMOVED AND REPLACED RT SIDE CHORD PER ACO 7342-53.

Part: BULB — FAILED (CABIN) · airframe 47,366 hrs · 47,173 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS FWD SECTION INOP. REMOVED AND REPLACED BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,098 hrs · 46,945 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 4 CRACK AT FUSELAGE EXTERNAL SKIN, BS 480 - 520, ABOVE STRINGER 10R, AND 1 CRACK, BS 500C - 500D, ABOVE STRINGER 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,723 hrs · 46,636 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACK 3 INCHES LONG, BS 967, WL 184. REPAIRED SKIN PER SRM.

Part: COVER — LOOSE (ESCAPE SLIDE) · airframe 46,553 hrs · 46,472 cycles

FWD SERVICE DOOR EVACUATION SLIDE COVER CASE LOOSE. SECURED CASE PER MM.

Part: SKIN — CRACKED (BS 942)

DURING SCHEDULED SPECIAL VISIT, FOUND EXTERNAL FUSELAGE SKIN CRACKED, BS 942, STRINGER 20R, BS 940, STRINGER 21L, AND BS 930, STRINGER 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 505A - 517B)

DURING SCHEDULED SPECIAL VISIT, FOUND EXTERNAL FUSELAGE SKIN CRACKED, BS 505A, 506B, 517B, STRINGER 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 769)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 769, ABOVE STRINGER 19R. REPAIRED SKIN PER SRM.

Part: SLIDE — LOOSE (PAX DOOR)

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. INSTALLED SLIDE ASSY PER MM.

Part: LIGHT — INOP (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EXTERIOR EMERGENCY EGRESS LIGHT INOP. RELAMPED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (BS 515)

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED, BS 515, STRINGER 12R. REPAIRED SKIN PER SRM.

Part: SLIDE — DETACHED (SERVICE DOOR)

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

Part: SKIN — CRACKED (NR 1 LE SLAT)

DURING SCHEDULED C4 CHECK, FOUND NR 1 LE SLAT HAS A 6 INCH LONG CRACK ON AFT RIVET ROW, 27 INCHES FROM INBD END. REPAIRED SKIN PER SWA RA 1-A57-0691.

Part: LIGHT — INOPERATIVE (ROW 3 & 23)

EMERGENCY EXIT FLOOR LIGHTS INOP AT ROWS 3 AND 23. REMOVED AND REPLACED LIGHT BULBS PER MM.

Part: BLADE — DENTED (NR 2 ENGINE)

DURING SCHEDULED C3 CHECK, FOUND RT ENGINE NR 31 FAN BLADE HAS DENT AT MIDSPAN FILLET RADIUS. REMOVED AND REPLACED NR 31 FAN BLADE PER MM.

Part: SLIDE — LOW PRESSURE (SERVICE DOOR)

FWD SERVICE DOOR SLIDE PRESSURE IS LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: BULKHEAD TEE — CRACKED (BS 178)

DURING SCHEDULED 1/4 CHECK, FOUND BS 178 T CHORD CRACKED AT WL 184, LBL 5.5. REPAIRED PER BOEING SRM.

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 LT O/B CHORD CRACKED AT WL 207. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED 1/4 CHECK, FOUND BS 178 SKIN CRACKED AT WL 188. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 520)

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED ON LT SIDE OF A/C BETWEEN NR 11 AND NR 12 PASSENGER WINDOWS AT BS 520. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING WALKAROUND CHECK, FOUND FWD ENTRY DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING M/M.

Part: SKIN — CRACKED (FUSELAGE)

DURING WALKAROUND CHECK, FOUND APPROX 5 INCH SKIN CRACK LEFT SIDE BETWEEN CABIN WINDOWS 11 AND 12. REPAIRED PER BOEING SRM.

Part: PCU — FAILED (RUDDER)

ON LANDING, LOST B-SYSTEM HYDRAULIC QUANTITY. REPLACED RUDDER PCU PER BOEING M/M.

Part: ENGINE — FAILED (NR 2)

IN FLIGHT, EXPERIENCED NR 2 ENGINE VIBRATION ALONG WITH NR 2 GENERATOR DROPPING OFF LINE. REDUCED ENGINE TO IDLE, NO HELP. CREW PERFORMED ENGINE SHUTDOWN PROCEDURES AND DIVERTED TO OAK. LANDED WITHOUT INCIDENT. REPLACED NR 2 ENGINE PER BOEING M/M.

Part: SKIN — CRACKED (BS 930)

DURING SCHEDULED TERMINAL CHECK, FOUND FUSELAGE SKIN CRACK AT BS 930, S23R. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 995)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 995, RBL 611, WL 226. REPAIRED PER BOEING SRM.

Part: DOUBLER — GOUGED (VERT STAB)

DURING SCHEDULED D-CHECK, FOUND DOUBLER ON LT VERTICAL STAB AFT T-BEAM HAS A DEEP GOUGE, 10 INCHES FROM TOP OF BODY. REPLACED DOUBLER PER BOEING SRM.

Part: SKIN — DENTED (BS 470)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 470, BETWEEN S23 AND 22L. INSTALLED DOUBLER REPAIR PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED IN RADIUS CHORD ON LEFT SIDE AT WL 195 TO 196. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 847-947.5)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM TO SIDEWALL SUPPORT PLATE CORRODED AT BS 847 TO 947.5, RBL 21. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 470)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 470 BETWEEN S23 AND 22L. REPAIRED PER BOEING SRM.

Part: TIE — CRACKED (BS 344)

DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CRACKED AT BS 344, S10R. REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 639)

DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 639, S15L. REPLACED PER BOEING SRM.

Part: SUPPORT — CRACKED (BS 813)

DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT LOWER FLANGE CRACKED AT BS 813, LBL 17, WL 156. REPAIRED PER BOEING SRM.

Part: SKIN — CREASED (BS 480)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CREASE AT BS 480, S28L TO 29L, WL 264. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: KEEL BEAM — CORRODED (BS 500+2)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON KEEL BEAM AT BS 500 PLUS 2, LBL 8, WL 149. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 318)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 318, RBL 43, WL 173. REPAIRED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE BULKHEAD WEB CRACKED AT WL 200, LBL 4.7. REPAIRED PER BOEING SRM.

Part: FLOOR BEAM — CORRODED (BS 312)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 312, BL 0, WL 208. REPAIRED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE BULKHEAD WEB CRACKED AT WL 199.5. REPAIRED PER BOEING SRM.

Part: SPLICE — CRACKED (BS 907)

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICES CRACKED AT BS 907, S4L AND S4R. REPLACED BOTH PER BOEING SRM.

Part: FLOOR BEAM — CORRODED (BS 328)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 328, LBL 11, WL 208. REPAIRED PER BOEING SRM.

Part: FLOOR BEAM — CORRODED (BS 967)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 967, RBL 28, WL 208. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 807/847)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 807 AND 847, AT STRINGER 9L. REPAIRED PER BOEING SRM.

Part: FLOOR BEAM — CORRODED (BS 294)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 294, LBL 10 AND AT RBL 35, WL 208. REPLACED FLOOR BEAM CHORD PER BOEING SRM.

Part: SKIN — DENTED (BS 995)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 995, RBL 11, WL 226. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 747/727)

DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, AT BS 727B, AND AT BS 747 RT SIDE. REPAIRED ALL PER BOEING SRM.

Part: SKIN — CRACKED (BS 727/747/500)

DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 747 LEFT SIDE, AT 727B, 747 AND 500 RIGHT SIDE. REPAIRED PER BOEING SRM.

Part: ENGINE — DAMAGED (NR 2)

ON LANDING ROLL, AIRCRAFT LEFT GEAR LEFT RUNWAY. AIRCRAFT RETURNED TO RUNWAY AND CONTINUED TO GATE. PERFORMED GEAR SIDELOAD INSPECTION, REPLACED NR 2 ENGINE DUE TO FOD DAMAGE, REPAIRED 3 SKIN AREAS FOR GOUGES, AND RT I/B AFT FLAP. REPLACED ONE AND REPAIRED ANOTHER NR 2 ENGINE REVERSER CASCADES. TEST HOPPED AIRCRAFT. REPLACED ALL GEAR WHEEL/TIRE ASSEMBLIES. ALL WORK PER BOEING M/M AND SRM.

Part: SKIN — CRACKED (PAX DOOR AREA)

DURING SCHEDULED B2 CHECK, FOUND A .3750 INCH CRACK AT UPPER RADIUS OF HINGE CUTOUT ON FUSELAGE AFT ENTRY DOOR CUTOUT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CRACKED (AFT ENTRY DOOR)

DURING SCHEDULED B2 CHECK, FOUND AFT ENTRY DOOR UPPER RADIUS HINGE CUTOUT CRACKED .3750 INCH. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CRACKED (SERV DOOR CUTOUT)

DURING SCHEDULED B2 CHECK, FOUND FORWARD SERVICE DOOR CUTOUT CRACKED 1 INCH AT AFT LOWER RADIUS. REPAIRED PER SWA RA 1-353-1252.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED MAINT CHECK, FOUND A 2 INCH CRACK IN LOWER LEFT FUSELAGE SECTION 46, BS 727E, AFT OF LOWER EMERGENCY EXIT LIGHT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.