N699SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,331 hrs · 63,092 cycles

DURING SCHDULED CV CHECK, FOUND SKIN CRACKED AT BS 500B+12, STR 19R. REPAIRED SKIN IAW SRM.

Part: ROD END — FAULTY (LE SLAT) · airframe 75,252 hrs · 63,025 cycles

ON APPROACH FLAPS L/E TRANSIT LIGHT ON NR 2 SLAT. REMOVED AND REPLACED NR 2 SLAT ROD END IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,385 hrs · 62,377 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 339, STR 17L. REPAIRED SKIN IAW EA.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 74,355 hrs · 62,351 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: WEB — CRACKED (FUSELAGE) · airframe 74,263 hrs · 62,279 cycles

DURING SCHEDULED SPV CHECK, FOUND WEB CRACKED AT BS 430, STR 19R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 74,263 hrs · 62,279 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR FRAME CRACKED. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,263 hrs · 62,279 cycles

DURING SCHEDULED 12Y CHECK, FOUND STUB BEAM CLIP CRACKED AT BS 639, LBL 45. REMOVED AND REPLACED CLIP IAW EA.

Part: GASPER FAN — FAULTY (CARGO BAY) · airframe 74,196 hrs · 62,225 cycles

FLIGHT ATTENDANT REPORTED VERY ACRID SMELL ON CLIMBOUT AND LANDING AT ALTITUDE IT WENT AWAY. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,567 hrs · 61,759 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACK BS 500C, STR15L. REPAIRED PER DOC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,567 hrs · 61,758 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500C+4, STR 15L. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 736.5, STR 26R. REMOVED AND REPLACED STRINGER PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CORRODED BETWEEN BS 734 TO BS 740, STR 26R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 747, STR 18L. REPAIRED SKIN PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 500, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 747, STR 27R. REMOVED AND REPLACED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 727C, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 663, RBL 24.5. REPAIRED BEAM PER EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 380, BETWEEN STR 13R TO STR 14R. REPAIRED SHEAR TIE PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 211 TO BS 219, STR 17L. REPAIRED WEB PER EA.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT LOWER FWD STOP FITTING. REMOVED AND REPLACED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 520, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD ENTRY EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BULBS PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 26R. REPAIRED FRAME PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 794.3, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 400, BETWEEN STR 13R TO STR 14R. REMOVED AND REPLACED SHEAR TIE PER EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 480, BETWEEN STR 13R TO STR 14R. REMOVED AND REPLACED SHEAR TIE PER EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, BETWEEN STR 13L TO STR 14L. REMOVED AND REPLACED SHEAR TIE PER EA.

Part: LIGHT — BROKEN (EXTERIOR) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT AFT OF R2 DOOR BROKEN. REMOVED AND REPLACED LIGHT PER BAC DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 727D, STR 4R. REMOVED AND REPLACED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 480, BETWEEN STR 13L TO STR 14L. REMOVED AND REPLACED SHEAR TIE PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 400, BETWEEN STR 13R TO STR 14R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME SPLICE — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME SPLICE WEB CRACKED AT BS 440, BETWEEN STR 13R TO STR 14R. REMOVED AND REPLACED WEB PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 420, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: CONNECTOR — BROKEN (CABIN) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EXIT SIGN CONNECTOR BROKEN. REMOVED AND REPLACED CONNECTOR PER MM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONG SEAT TRACK CRACKED AT BS 727B, LBL 45.5. REMOVED AND REPLACED SEAT TRACK PER EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500C, BETWEEN STR 13L TO STR 14L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 7L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 460, BETWEEN STR 13R TO STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 259, STR 6L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND BULKHEAD VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REMOVED AND REPLACED WEB PER EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 807, BETWEEN STR 27L TO STR 27R. R&R SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 259, STR 8L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 727C, BETWEEN STR 13L TO STR 14L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 1L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 15R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, BETWEEN BBL 0 TO RBL 4. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 12R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE ANGLE CRACKED AT BS 303, STR 15L. REMOVED AND REPLACED ANGLE PER BAC DWG.

Part: SHEAR TIE — CORRODED (BS 827 S26-27R) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 13R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND SPLICE CHANNEL CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED CHANNEL PER SRM AND BAC DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND WEB SUPPORT CORRODED BETWEEN BS 440 TO BS 500, RBL 22. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND VERTICAL FRAME ANGLE CRACKED AT BS 727B, LBL 45.5. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 787, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 1L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 1L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: ATTACH BRACKET — LOOSE (GIRT BAR) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH BRACKETS LOOSE. REMOVED AND REPLACED BRACKETS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 4L. REPAIRED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 4R. REPAIRED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 15L. REPAIRED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 14L. REMOVED AND REPLACED CLIP PER BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 887, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 10L. REPAIRED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 727C, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 847, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 360, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 15L. REMOVED AND REPLACED CLIP PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 20L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 767, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 707, STR 11L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 16L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 1L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 28L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 787, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 1L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 10R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 23R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,117 hrs · 60,640 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 72,083 hrs · 60,609 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MM AND MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,424 hrs · 60,096 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 913, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,424 hrs · 60,096 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 943, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,424 hrs · 60,096 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 309.5, STR 23R. REPAIRED SKIN PER SRM.

Part: UPLOCK SENSOR — OUT OF ADJUST (RT MLG) · airframe 71,303 hrs · 60,004 cycles

AIR TURNBACK, UNSAFE GEAR INDICATION RT MLG AFTER TAKEOFF WITH GEAR HANDLE OFF. WITH GEAR HANDLE DOWN NORMAL INDICATIONS AND NORMAL LANDING WEIGHT. ADJUSTED RT UPLOCK SENSOR, TARGET AND GAP PER MM.

Part: CIRCUIT CARD — FAULTY (E&E BAY) · airframe 71,248 hrs · 59,961 cycles

AIR TURNBACK - UNSAFE GEAR INDICATION RIGHT SIDE RIGHT AFTER TAKEOFF. ALL OTHER INDICATIONS NORMAL. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED M982 PC CARD PER MM.

Part: OUTFLOW VALVE — FAULTY (E&E BAY) · airframe 70,938 hrs · 59,720 cycles

DIVERSION / DECLARED EMERGENCY. EN ROUTE FL 320 CABIN PRESSURIZATION FAILURE. CABIN ALT 10,500 MANUAL FOCC CLOSED DC STABILIZED CABIN ALT 10,300. NO FURTHER DECREASE. REMOVED AND REPLACED OUTFLOW VALVE AND CABIN PRESSURE CONTROLLER PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,122 hrs · 59,114 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 314 TO BS 317, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,822 hrs · 58,895 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 305, STR 18R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,822 hrs · 58,895 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 931, STR 21R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,822 hrs · 58,895 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 970, STR 21L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,822 hrs · 58,895 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 586, STR 10L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,825 hrs · 58,896 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 305, STR 18R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,825 hrs · 58,896 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 586, STR 10L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,825 hrs · 58,896 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 931, STR 21R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,825 hrs · 58,896 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 970, STR 21L. REPAIRED SKIN PER EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 69,722 hrs · 58,822 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM CRACKED AT BS 312, LBL 60. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,722 hrs · 58,822 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CRACKED AT BS 312, LBL 60. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,722 hrs · 58,822 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,104 hrs · 56,409 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED PER MM.

Part: SIGN — MISSING (CABIN) · airframe 69,169 hrs · 58,407 cycles

RIGHT FWD OVERWING EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,733 hrs · 58,068 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514D TO BS 518D, STR 12L. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,733 hrs · 58,068 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515B TO BS 514D, STR 15L TO STR 16L. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,733 hrs · 58,068 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 770 TO BS 780, STR 18L TO STR 19L. REPAIRED SKIN PER SRM AND EA.

Part: LENS — MISSING (CABIN) · airframe 68,612 hrs · 57,977 cycles

RT EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 68,638 hrs · 57,997 cycles

RT EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,323 hrs · 57,773 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 931, STR 25R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 68,323 hrs · 57,773 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: FLAP — DELAMINATED (RT WING) · airframe 68,030 hrs · 57,571 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 67,840 hrs · 57,450 cycles

L1 DOOR EMERGENCY EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,411 hrs · 57,158 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 500D, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,411 hrs · 57,158 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 460, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,411 hrs · 57,158 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 907, STR 24R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 66,870 hrs · 56,760 cycles

FOUND L1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,141 hrs · 56,256 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT AIR STAIR CUTOUT LOWER FWD CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,137 hrs · 56,253 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 765, STR 19R. REPAIRED SKIN PER EA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,137 hrs · 56,253 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: STRINGER — CORRODED (BS 324 S24R) · airframe 66,137 hrs · 56,253 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 24R CORRODED AT BS 324. REPAIRED STRINGER PER SRM.

Part: FLOORBEAM — CORRODED (BS 1016) · airframe 66,137 hrs · 56,253 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, LBL 12. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 1016) · airframe 66,137 hrs · 56,253 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, LBL 12. REPAIRED FLOORBEAM PER SRM.

Part: FITTING — CORRODED (LT WING) · airframe 66,137 hrs · 56,253 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING STABILIZER LINK LUG CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 66,137 hrs · 56,253 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.

Part: BULKHEAD — CRACKED (BS 178) · airframe 66,137 hrs · 56,253 cycles

DURING SCHEDULED 22Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (BS 277 S9R) · airframe 66,137 hrs · 56,253 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,974 hrs · 56,134 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 65,932 hrs · 56,106 cycles

DURING SCHEDULED MV3 CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 65,653 hrs · 55,893 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,050 hrs · 55,468 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,050 hrs · 55,468 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 18R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,528 hrs · 55,101 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 410 AND BS 430, BL 0. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 64,365 hrs · 54,978 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 65,354 hrs · 54,970 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — DELAMINATED (NR 9 SPOILER) · airframe 63,532 hrs · 54,360 cycles

RIGHT WING NR 9 GROUND SPOILER DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED SPOILER PER MM.

Part: LAMP — INOPERATIVE (CABIN) · airframe 63,431 hrs · 54,282 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 806 S19L) · airframe 63,304 hrs · 54,185 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 806, STR 19L. REPAIRED SKIN PER SWA EA.

Part: STRIP — WORN (EMERGENCY LIGHTS) · airframe 63,304 hrs · 54,185 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT FWD CABIN. REMOVED AND REPLACED STRIP PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 63,304 hrs · 54,185 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,419 hrs · 53,496 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730B, STR 14R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,595 hrs · 52,855 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504C, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,595 hrs · 52,855 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513D, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 520 S16L) · airframe 60,888 hrs · 52,321 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 16L. REPAIRED SKIN PER SWA EA.

Part: TORQUE TUBE — DISCONNECTED (T/E FLAP) · airframe 60,284 hrs · 51,854 cycles

DECLARED EMERGENCY, ON APPROACH FLAPS WOULD NOT EXTEND BEYOND 2. FOUND LEFT WING INBOARD 90 DEGREE ANGLE GEAR BOX TORQUE TUBE DISCONNECTED, RECONNECTED TORQUE TUBE PER MM.

Part: SKIN — CRACKED (BS 970 S21L) · airframe 60,200 hrs · 51,783 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 21L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (BS 500C S20R) · airframe 59,738 hrs · 51,487 cycles

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

Part: WIRE — FAULTY (EMERGENCY LIGHT) · airframe 59,738 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, WHEN PLACING EMERGENCY EXIT LIGHT SWITCH TO OFF POSITION, ALL OF THE MAIN CABIN LOWER EXIT LIGHTS REMAIN ILLUMINATED. REMOVED AND REPLACED WIRE W132-022-22 PER WDM.

Part: FRAME — CRACKED (R1 DOOR) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT NR 3 DOOR STOP. REPAIRED DOOR FRAME SECTION PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 968 TO BS 979, STR 24L TO STR 26L. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 1006, STR 27R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 987, STR 27L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 27L CRACKED AT BS 987. REPAIRED STRINGER SECTION PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 971, STR 26L. REPAIRED SKIN PER SWA EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND KEEL BEAM CHORD CORRODED AT LT BS 540. REPAIRED KEEL BEAM CHORD PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 360, STR 28R. REPAIRED SKIN PER SRM.

Part: BELTFRAME — CORRODED (FUSELAGE) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND BELT FRAME CORRODED AT BS 360, STR 28L AND 28R. REPAIRED BELT FRAME PER SRM.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND BELT FRAME CRACKED AT BS 1006, STR 27L AND 27R. REPAIRED BELT FRAME PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 989, STR 27L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727E S18L) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 18L. REMOVED AND REPLACED STRINGER CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 948 S25R) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 948, STR 25R. REMOVED AND REPLACED STRINGER CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 948 S22L) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 948, STR 22L. REMOVED AND REPLACED STRINGER CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 948 S25R) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 948, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CRACKED (BS 669) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER TEE CHORD CRACKED AT BS 669, LBL 24.5. REPAIRED FLOORBEAM PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 787 S22L) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 787 S23L) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CRACKED (BS 662) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER TEE CHORD CRACKED AT BS 662, LBL 24.5. REPAIRED FLOORBEAM PER SWA EA.

Part: BELTFRAME — CORRODED (BS 1006) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BELTFRAME CORRODED AT BS 1006 BETWEEN STR 27L AND 27R. REPAIRED BELTFRAME PER SWA EA.

Part: SHEAR TIE — CORRODED (BS 827 S27R-27L) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827 BETWEEN STR 27R AND 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500A S22R) · airframe 59,793 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 747 S18L) · airframe 59,798 hrs · 51,487 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN TEAR STRAP CRACKED AT BS 747, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SIGN — BROKEN (CABIN) · airframe 59,461 hrs · 51,208 cycles

EMERGENCY EXIT SIGN BROKEN AT R1 DOOR. REMOVED AND REPLACED EMERGENCY EXIT SIGN IAW MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 59,101 hrs · 50,919 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 DEF. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 59,068 hrs · 50,895 cycles

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

Part: SKIN — CRACKED (BS 777 S18L) · airframe 58,768 hrs · 50,653 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 777, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 757 S19L) · airframe 58,768 hrs · 50,653 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 19L. REPAIRED SKIN PER SWA EA.

Part: CABLE — MISROUTED (R2 DOOR SLIDE) · airframe 58,148 hrs · 50,197 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 58,148 hrs · 50,197 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,406 hrs · 49,637 cycles

DURING SCHEDULED A2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. RELAMPED LIGHTS PER MM.

Part: SKIN — DELAMINATED (LT WING SPOILER) · airframe 57,406 hrs · 49,637 cycles

DURING SCHEDULED A2 CHECK, FOUND LEFT WING NR 2 SPOILER DELAMINATED. REMOVED AND REPLACED NR 2 SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,236 hrs · 48,688 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 23L. REPAIRED SKIN PER SRM.

Part: ROLLER — MISSING (RT WING FOREFLAP) · airframe 56,236 hrs · 48,688 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD T/E FOREFLAP MID-TRACK ROLLER MISSING. INSTALLED ROLLER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,236 hrs · 48,688 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 21R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,236 hrs · 48,688 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,259 hrs · 47,890 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12R. REPAIRED SKIN PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,183 hrs · 47,828 cycles

DURING SCHEDULED A2 CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,289 hrs · 47,152 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM.

Part: BULKHEAD — PUNCTURED (RT MLG WW) · airframe 54,012 hrs · 46,931 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT MLG BULKHEAD WEB PUNCTURED AT BS 727, RBL 24, WL 178. REPAIRED WEB PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 53,684 hrs · 46,829 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 53,597 hrs · 46,616 cycles

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

Part: MODULE — LEAKING (MLG WW) · airframe 53,578 hrs · 46,600 cycles

AIR TURNBACK, DECLARED EMERGENCY. HYDRAULIC B-SYSTEM FAILURE. REMOVED AND REPLACED B-SYSTEM HYDRAULIC MODULE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,323 hrs · 46,388 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 727E + 5, BELOW STRINGER 19R, CRACKED. REPAIRED SKIN PER EA.

Part: SLIDE — WORN (R1 DOOR) · airframe 53,323 hrs · 46,388 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE GIRT WORN. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM.

Part: BRACKET — CRACKED (ESCAPE SLIDE) · airframe 53,323 hrs · 46,388 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE FWD MOUNTING BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: GIRT BAR — DISLODGED (R1 DOOR) · airframe 52,337 hrs · 45,604 cycles

R1 DOOR EVAC SLIDE GIRT BAR FELL OUT. INSTALLED R1 DOOR EVAC SLIDE GIRT BAR PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DDOR) · airframe 52,198 hrs · 45,492 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,047 hrs · 45,376 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 944, STRINGER 25R, CRACKED. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 827, STRINGER 9L AND BS 867, STRINGER 9R, CRACKED. REPAIRED FRAMES PER ER AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 500A + 5, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 284, BETWEEN STRINGERS 23R AND 24R, CREASED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES AT STRINGER 9L, BS 360, BS 400, BS 440, BS 480, BS 727E, BS 747, BS 807, BS 907, CRACKED. REPAIRED FRAME SECTIONS PER ER.

Part: RIB — CRACKED (RT WING) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D CHECK, FOUND RT WING AT WBL 114, S2, UPPER RIB CRACKED. REPAIRED RT WING RIB PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES AT STRINGER 9R, BS 380, BS 480, BS 747, BS 807, BS 827, BS 887, BS 907, CRACKED. REPAIRED FRAME SECTIONS PER ER.

Part: FITTING — CRACKED (LT WING) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND LT MLG BEAM FITTING AT D-HOLE CRACKED. REMOVED AND REPLACED LT MLG FITTING PER ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D CHECK, FOUND BULKHEAD AT BS 1016, STRINGER 23L, CRACKED. REPAIRED BULKHEAD PER ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D CHECK, FOUND AFT CARGO DOOR FRAME CUTOUT AT BS 794, STRINGER 20R TO STRINGER 25R, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM AT BS 960 TO BS 986, LBL 60 TO LBL 65, WL 208, CORRODED. REPAIRED CREASE BEAM PER SRM.

Part: FITTING — CRACKED (RT MLG) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D CHECK, FOUND RT MLG BEAM FITTING AT 5 O'CLOCK POSITION CRACKED. REMOVED AND REPLACED BEAM FITTING PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

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

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 616, RBL 71, WL 208. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 616, STRINGER 4 R. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 967, LBL 1. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 520, STRINGER 4R AND BS 867, STRINGER 9R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 911, BETWEEN STR 27L & STR 24L. REPAIRED SKIN PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND 3 EA STRINGER CLIPS CRACKED AT BS 727C, STR 22R, STR 21R, & BS 727D, STR 23R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CORRODED AT BS 947 TO BS 986, RT SIDE. REPAIRED CREASE BEAM PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND 2 CRACKS AT FUSELAGE BULKHEAD, BS 1016, STR 7R, AND OUTBOARD OF DOME CAP. REPAIRED BULKHEAD WEB PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 970, STR 7L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FWD CARGO) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, STR 24R. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CHORD CRACKED AT BS 616 TO BS 639, RBL 63, WL 208. REMOVED AND REPLACED CREASE BEAM CHORD PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEBS CRACKED AT BS 576, LBL 71, WL 208 AND BS 637, LBL 71, WL 208. REMOVED AND REPLACED CREASE BEAM WEBS PER SRM.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON RIGHT HORIZONTAL STAB CENTER SECTION FWD AND AFT SPAR, UPPER AND LOWER CLEVIS, FWD AND AFT LUG FACES. REPAIRED HORIZONTAL STAB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STRINGER 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 639, STRINGER 8L, BS 706, STRINGER 2L AND BS 616, STRINGER 4R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 867, STRINGER 9L. REPAIRED FRAME SECTION PER SRM.

Part: SPLICE — CRACKED (STRINGER) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED A BS 907, STRINGER 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 51,496 hrs · 44,938 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIPS CRACKED AT STRINGER 4L AND BS 706, BS 639, BS 616. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,489 hrs · 44,936 cycles

DURING SCHEDULED SPV, FOUND FUSELAGE SKIN CRACKED AT BS 727 + 3, STRINGER 18R AND AT BS 766, STRINGER 22R. REPAIRED SKIN CRACKS PER SRM.

Part: STRAP — BROKEN (CABIN) · airframe 50,646 hrs · 44,251 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD OB EMERGENCY LIGHT LOWER STRAP BROKEN. REMOVED AND REPLACED STRAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,415 hrs · 44,062 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED 3.5 LONG AT BS 501D, STR 12R. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 50,068 hrs · 43,777 cycles

FWD ENTRY DOOR EMERGENCY OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,778 hrs · 43,541 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT BS 520 AT STR 10L, BS 727D AT STR 22L AND BS 767 AT STR 18R. REPAIRED SKIN PER SRM.

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 48,886 hrs · 42,810 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLAT — CRACKED (RT WING) · airframe 47,931 hrs · 42,059 cycles

DURING SCHEDULED BC3 CHECK, FOUND NR 5 L/E SLAT CRACKED AT RIVETS ON LOWER SURFACE. REPAIRED SLAT PER SWA EA.

Part: SLAT — CRACKED (RT WING) · airframe 47,928 hrs · 42,057 cycles

DURING SCHEDULED C3 CHECK, FOUND NR 6 L/E SLAT T/E SKIN CRACKED AT AFT ROW OF RIVETS. REMOVED AND REPLACED NR 6 L/E SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,997 hrs · 41,305 cycles

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

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 46,997 hrs · 41,305 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,919 hrs · 41,239 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E PLUS 10, STR 22R. REPAIRED SKIN PER SRM.

Part: WIRE — CHAFED (COCKPIT) · airframe 46,761 hrs · 41,099 cycles

BURN SMELL IN COCKPIT, SMELL IMMEDIATELY DISSIPATED. C/W INSPECTION IN MCI NO DEFECTS NOTED. LATER AT LAS, DID FOLLOW UP AND FOUND CHAFFED WIRE AT L1 WINDOW HEAT UNDER GLARE SHIELD. REPAIRED WIRE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 45,662 hrs · 40,178 cycles

OVERHEAD BIN BULL NOSE EMERGENCY LIGHT LENS LOOSE AT ROW NR 23 DEF. SECURED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,349 hrs · 39,914 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, BETWEEN STR 19L AND 20L. REPAIRED FRAME PER SRM.

Part: LIGHT — LOOSE (COCKPIT) · airframe 45,349 hrs · 39,914 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT NOT ARMED LIGHT ASSY LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,349 hrs · 39,914 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 179, WL 227 AT LBL 17.1. REMOVED AND REPLACED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,349 hrs · 39,914 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 183, WL 233 AT RBL 17.1. REMOVED AND REPLACED WEB PER SRM.

Part: DOOR FRAME — CRACKED (FWD ENTRY DOOR) · airframe 45,349 hrs · 39,914 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR AFT FRAME CRACKED (3 EA) AT NR 3, NR 4 AND NR 5 STOP FITTINGS FROM BOTTOM. REPAIRED FRAME PER SRM.

Part: WEB — CRACKED (LT MLG W/W) · airframe 45,349 hrs · 39,914 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 663, LBL 33. REPAIRED WEB PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,349 hrs · 39,914 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED 4 INCHES AT BS 769, STR 18L. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 45,349 hrs · 39,914 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 845, LBL 12. REPAIRED FLOORBEAM PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,233 hrs · 39,800 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED 3 INCHES AT BS 520D PLUS 13, ABOVE STR 10R. REPAIRED SKIN PER SRM.

Part: HOSE — FAILED (NLG W/W) · airframe 44,893 hrs · 39,536 cycles

DIVERSION, AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT. F0UND LOCKING ACTUATOR FLEX HOSE FAILURE AT SWEDGE AREA. REMOVED AND REPLACED HOSE. OPS CK OK PER MM.

Part: LENS — LOOSE (CABIN) · airframe 44,687 hrs · 39,376 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 44,300 hrs · 39,057 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS LOOSE IN FWD CABIN. SECURED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,125 hrs · 38,910 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C PLUS 4, STR 10R. REPAIRED SKIN PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,125 hrs · 38,910 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED(6 EA) BETWEEN BS 727D AND BS 887, STR 19R TO STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,125 hrs · 38,910 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED(2 EA) AT BS 752 AND BS 763, STR 24L. REPAIRED SKIN PER SRM.

Part: TAB — WORN (RH ELEVATOR) · airframe 43,514 hrs · 38,389 cycles

DURING SCHEDULED C2 CHECK, RH ELEVATOR TAB FAILED FREE PLAY CHECK. R&R RH ELEVATOR TAB PER MM.

Part: BEARING — WORN (RH ELEVATOR) · airframe 43,514 hrs · 38,389 cycles

DURING SCHEDULED C2 CHECK, RH ELEVATOR FAILED FREE PLAY CHECK. R&R RH ELEVATOR CONTROL BEARING PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 41,579 hrs · 36,734 cycles

DURING SCHEDULED BC4 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 41,154 hrs · 36,382 cycles

LANDING GEAR HANDLE WOULD NOT GO UP PAST OFF POSITION. FOUND LANDING GEAR LATCH PRESS WARN C/B TRIPPED. RESET C/B AND RAISED LAND GEAR AND CONTINUED. SYSTEM TEST OF LAND GEAR CONTROL LEVER LOCK GOOD AND C/B REMAINS CLOSED, NO FAULTS NOTED PER MM.

Part: SLIDE — DEPLOYED (ENTRY DOOR) · airframe 41,032 hrs · 36,286 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED AT JETWAY. R&R EVAC SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,606 hrs · 35,933 cycles

DURING SCHEDULED C3 CHECK, FOUND APPROX 2 INCH LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 727E, BELOW STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT WING LE FLAP) · airframe 40,606 hrs · 35,933 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD T/E FOREFLAP DELAMINATED ON UPPER SURFACE. REPAIRED FOREFLAP PER SRM.

Part: INDICATOR — MALFUNCTIONED (NR 1 EGT) · airframe 39,518 hrs · 35,012 cycles

AIR TURNBACK, NR 1 ENG EGT INDICATOR INOP. REMOVED AND REPLACED NR 1 ENG EGT IND PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED RON, FOUND EEPLS INOP AT FWD END. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: RIB — CRACKED (BS 616)

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE CENTER SECTION, BS 616, RBL 60 RIB ASSY CRACKED. REPAIRED RIB SECTION PER TI-153-018.

Part: CLIP — CRACKED (BS 294)

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED, BS 294, STRINGERS 13L AND 11L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOOR BEAM, BS 986.5, LBL 16 - LBL 60. REPAIRED BEAM PER TI-453-037.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 11- RBL 7. REMOVED AND REPLACED BULKHEAD WEB PER ACO 7154-53.

Part: SKIN — CORRODED (WS 345&475)

DURING SCHEDULED 1/2D CHECK, FOUND RT WING UPPER SURFACE SKIN CORRODED AROUND IN SPAR, WS 345 AND WS 475. REPAIRED SKIN PER SWA RA NR 1-357-0754, REVISION 1.

Part: FLOOR BEAM — CORRODED (BS 947)

DURING SCHEDULED 1/2D CHECK, FOUND BS 947 FLOORBEAM UPPER SECTION CORRODED AT LBL 9. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (BS 294)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FUSELAGE FRAME, BS 294, RBL 54 AT FWD GALLEY DOOR CUT OUT. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (BS 787)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FUSELAGE SHEAR TIE, BS 787, STRINGER 27R. REPAIRED SHEARTIE PER SRM.

Part: FLOORBEAM — CORRODED (BS 1006)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM, BS 1006, LBL 19. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED 1/2D CHECK, FOUND BS 328 FLOORBEAM UPPER SURFACE CORRODED BETWEEN LBL 15 - RBL 58. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 294.5)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM UPPER FACE, BS 294.5, LBL 10.5. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (SERVICE DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR, AFT FRAME CRACKED AT TWO PLACES. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (BS 727 & 747)

DURING SCHEDULED BC2 CHECK, FOUND 4 EA FUSELAGE SKIN CRACKS APPROX 1.5 INCHES LONG, BS 727E AND 727D, STRINGER 23R, BS 727E, STRINGER 21L, AND BS 747, STRINGER 22L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (PASSENGER DOOR)

LT FWD EMERGENCY ESCAPE SLIDE CAME OUT OF THE HOLDER. INSPECTED AND RESTOWED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED SC CHECK, FOUND 2 FUSE SKIN CRACKS BETWEEN BS 727D AND E AT S22R, 1.5 LONG AND 3 APART. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 747)

DURING SCHEDULED SC CHECK, FOUND A FUSE SKIN CRACK AT BS 747, S21R, 2.25 LONG. REPAIRED PER BOEING SRM.

Part: CONTROLLER — MALFUNCTIONED (NR 1)

AT FL 350, PRESS MODE SELECTOR IN AUTO, THE ALTITUDE 'CABIN' WARNING HORN SOUNDED. EMERGENCY DECLARED. EMERGENCY DESCENT ACCOMPLISHED. PASSENGER MASK DID NOT DROP. CABIN ALT INCREASED TO APPROX 12,500 FT, MAN PRESS OK. REPLACED CABIN PRESSURIZATION CONTROLLER, OPS CK OK PER M/M.

Part: SKIN — CRACKED (BS 887)

DURING SCHEDULED A2 CHECK, FOUND SKIN CRACKED AT BS 887, STR 21R. REPAIRED PER BOEING SRM.

Part: UPLOCK SWITCH — MALFUNCTIONED (LT MLG)

AIR RETURN AFTER TAKEOFF AND GEAR RETRACTION. LEFT MAIN GEAR GREEN LIGHT REMAINED ILLUMINATED, LEFT RED GEAR LIGHT DID NOT EVER ILLUMINATE. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED LT MLG UP AND LOCK SWITCH, DOWN AND LOCK SWITCH AND LT GREEN LIGHT BASE. OPS CHECKED OK PER BOEING MM.

Part: HYD LINE — RUPTURE (NLG)

RETURN TO LAS DUE TO NOSE LANDING GEAR FAILING TO RETRACT AND MADE UNEVENTFUL LANDING. INSPECTED AND FOUND NOSE GEAR ACTUATOR UPLOCK HYD LINE RUPTURE. REMOVED AND REPLACED PER BOEING MM.

Part: LIGHT — CORRODED (PAX DOOR)

DURING SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY ESCAPE SLIDE LIGHT CORRODED AND INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/M.

Part: SKIN — CRACKED (BS 727)

DURING SERVICE CHECK, FOUND A 3 INCH FUSELAGE SKIN CRACK AT BS 727E, S24L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 747)

DURING SCHEDULED 1/4 D CHECK, FOUND A 4 FUSELAGE SKIN CRACK AT BS 747, S25R. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (DOOR STOP)

DURING SCHEDULED C3 CHECK, FOUND UPPER FWD DOOR STOP CRACKED IN WEB. REPAIRED PER SWA RA 1-353-1558.

Part: CHORD — CRACKED (BS 727)

DURING SCHEDULED TRANSITION CHECK, FOUND COMPRESSION CHORD CRACKED AT BS 727, WL 199, RBL 13 TO 15. REPAIRED PER TRAMCO EWO 95-0076.

Part: SKIN — OIL CANNING (BS 727-747)

DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN OIL CANNING FROM BS 727D TO 747, STRINGER 22L TO 24L. REPAIRED PER TRAMCO EWO 95-0082.

Part: STRINGER — CORRODED (BS 727)

DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CORROSION AROUND FASTENERS AT BS 727D TO 767, S26R, AND AT BS 767 TO 807, S26R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: STRINGER — CORRODED (BS 1116-1127)

DURING SCHEDULED TRANSITION CHECK, FOUND APU COMPARTMENT BULKHEAD AIR INLET CUTOUT WITH CORROSION ON UPPER AND LOWER STRINGERS AND STIFFENERS FROM BS 1116 TO 1127. REPLACED PARTS PER BOEING STRUCTURAL REPAIR MANUAL.

Part: STIFFENER — CORRODED (BS 294.5)

DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM STIFFENER CORRODED AT BS 294.5 AND 312, WL 208. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: ANGLE — CORRODED (BS 832)

DURING SCHEDULED TRANSITION CHECK, FOUND AFT CARGO DOOR L ANGLE CORRODED AT BS 832 RBL 32 WL 158. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DENTED (BS 767)

DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED, AND A PREVIOUS REPAIR AT BS 767, BETWEEN S20 AND 21R. REPAIRED BOTH PER BOEING STRUCTURAL REPAIR MANUAL.

Part: INTERCOSTAL — CORRODED (BS 767-787)

DURING SCHEDULED TRANSITION CHECK, FOUND INTERCOSTAL CORROSION AT BS 767-787, RBL 22, WL 150 AND AT BS 344, BL 0, WL 208. FABRICATED AND REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: WEB — CRACKED (BS 726)

DURING SCHEDULED MAINTENANCE CHECK, FOUND CRACK IN WEB AT BS 726, S18A, LEFT SIDE. REPAIRED PER SWA RA 1-553-1222.

Part: FLOOR BEAM — CORRODED (BS 294.5)

DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORROSION AT BS 294.5, LBL 11 TO RBL 45. REPAIRED PER SWA RA 1-353-418.

Part: SPAR — CORRODED (WS 500)

DURING SCHEDULED TRANSITION CHECK, FOUND RIGHT WING SPAR UPPER SURFACE AT WS 500 JUST AFT OF FRONT SPAR CORRODED. REPAIRED PER TRAMCO EWO 95-0051.

Part: CLIP — CORRODED (BS 727D)

DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CLIP CORRODED AT BS 727D, RBL 16, WL 150. REPLACED PER BOEING STRUCTURAL REPAIR MANAUL.

Part: SKIN — DENTED (BS 885)

DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 885, BETWEEN S19 AND 20R. REPAIRED PER BOEING STRUCTURAL REPAIR MANAUL.

Part: ANGLE — CRACKED (BS 570)

DURING SCHEDULED TRANSITION CHECK, FOUND SKATE ANGLE CRACKED AT BS 570, WL 158, LBL 50. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: CLIP — CORRODED (BS 727D)

DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CLIP CORRODED AT BS 727D, RBL 8, WL 147. REPLACED STRINGER CLIP PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DENTED (BS 368/867)

DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 368, WL 205, LEFT SIDE AND A LONGITUDINAL CREASE AFT OF CARGO DOOR, BS 867, BETWEEN S22R AND 23R. REPAIRED BOTH PER BOEING STRUCTURAL REPAIR MANUAL.