N329SW

Part: LENS — BROKEN (CABIN) · airframe 76,790 hrs · 68,422 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: TAB — DELAMINATED (RT AILERON) · airframe 76,522 hrs · 68,222 cycles

DURING SCHEDULED 2HC1 CHECK FOUND, RT WING AILERON TAB DELAMINATED AT T/E. REMOVED AND REPLACED TAB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 947, BETWEEN STR 24R TO STR 25R. REPAIRED FRAME IAW ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 344, BETWEEN STR 23L TO STR 24L. REPAIRED FRAME IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CUTOUT CRACKED AT R1 DOOR LOWER FWD CORNER. REPAIRED SKIN IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM UPPER AFT FLANGE CORRODED AT BS 344, LBL 11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 328, STR 20R. REPAIRED FRAME IAW ER AND EA.

Part: BRACKET — CRACKED (EVAC SLIDE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE UPPER FWD ATTACHMENT BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER SRM, MM, AND DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT KEEL BEAM CHORD CORRODED BETWEEN BS 551 TO BS 565. REPAIRED CHORD PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT SKIN CORRODED AT BS 803, STR 26R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 951, STR 14R. REPAIRED SKIN IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEUDLED 24Y CHECK, FOUND STRINGER CORRODED AT BS 438, STR 28R. REPAIRED STRINGER IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND I-BEAM O/B ATTACH FITTING CRACKED AT BS 727, LBL 45. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 706 TO BS 710, LBL 24.8. REPAIRED WEB IAW ER AND EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 400 TO BS 420, RBL 67. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 460 TO BS 480, LBL 67. REMOVED AND REPLACED WEB PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO BAY KEEL BEAM CORRODED AT BS 500D+5, STR 28R. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 16R. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK FOUND, CREASE BEAM WEB CORRODED BETWEEN BS 400 TO BS 420, LBL 67. REPAIRED WEB IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 27L TO STR 28L. REPAIRED SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 1 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 21R. REPAIRED CLIP IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 20R. REPAIRED SPLICE PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 887, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 27L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 16R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 18R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 19R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 10R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 19R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 9R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 25L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 23L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,358 hrs · 68,093 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,026 hrs · 67,846 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT IAW MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 75,317 hrs · 67,302 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOKS PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 75,301 hrs · 67,289 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT WING NR 5 SLAT UPPER LT CORNER DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: SPOILER — CRACKED (RT WING) · airframe 75,133 hrs · 67,171 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING I/B GROUND SPOILER CRACKED. REMOVED AND REPLACED SPOILER PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,892 hrs · 66,982 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,892 hrs · 66,982 cycles

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

Part: SKIN — DELAMINATED (TE FLAP) · airframe 73,492 hrs · 65,899 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING O/B AFT FLAP LOWER SKIN DELAMINATED. REMOVED AND REPLACED AFT FLAP PER SRM.

Part: LIGHT — MISSING (CABIN) · airframe 73,429 hrs · 65,852 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT EEPLS MISSING AT ROW 1. INSTALLED EEPLS PER MM.

Part: LENS — MISSING (CABIN) · airframe 72,654 hrs · 65,204 cycles

RT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 23. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 726,544 hrs · 65,204 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 72,218 hrs · 64,870 cycles

RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 23. RE-INSTALLED LENS PER MM.

Part: SLAT — CRACKED (LT WING) · airframe 71,704 hrs · 64,497 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING L/E NR 2 SLAT CRACKED. REPAIRED SLAT PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 500D, STR 25L TO STR 26L. REPAIRED SHEAR TIE PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16L. REPAIRED FRAME PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727A TO BS 727A+13, STR 14R. REPAIRED SKIN PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACE STR CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 227, BL 0. REPAIRED FRAME PER ER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 400, STR 21L. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 616, STR 1R. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 470, STR 15L. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 378, STR 23L. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, BETWEEN STR 15R & STR 16R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 425, STR 27L. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 520, STR 23R TO STR 24R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 70,996 hrs · 63,992 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 22L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 15L. REPAIRED FRAME PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 420, STR 22R. REPAIRED STRINGER PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FWD EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED SIGN PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 793, BETWEEN STR 19L TO STR 20L. REMOVED AND REPLACED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 410, STR 15L. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND STUB FRAME CORRODED AT BS 467, UPPER CARGO DOOR SILL WEB. REPAIRED FRAME PER SRM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 70,996 hrs · 63,992 cycles

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

Part: TEE FITTING — CRACKED (CARGO DOOR) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR, NR 2 O/B TEE CHORD CRACKED. REMOVED AND REPLACED CHORD PER BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 400, BETWEEN STR 15R TO STR 16R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING I/B FORE FLAP LOWER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 980, BETWEEN LBL 16 TO RBL 30. REPAIRED BEAM PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 16L TO STR 17L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — DAMAGED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE DAMAGED AT BS 495, STR 22R. REMOVED AND REPLACED SPLICE PER ESR.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND CENTER BOX WING LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727, LBL 24.8. REMOVED AND REPLACED BEAM PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 503D, STR 9L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 504B S9L) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 504B, STR 9L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 503D S9L) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 503D, STR 9L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 504B, STR 9L. REPAIRED SKIN PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,996 hrs · 63,992 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,995 hrs · 63,992 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 70,827 hrs · 63,863 cycles

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

Part: ACM — FAULTY (A/C BAY) · airframe 70,284 hrs · 63,445 cycles

SMELLED MODERATE PUNGENT ODOR IN COCKPIT AND FWD PART OF AIRCRAFT. NO VISIBLE SMOKE. TURNED OFF GALLEY & LAV POWER AND SMELL CONTINUED. SUSPECT SMELL FROM PACK OR FAN. FOUND SOURCE TO BE LT PACK. REMOVED AND REPLACED LT PACK AIR CYCLE MACHINE AND SOCK PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 69,997 hrs · 63,228 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND NOSE WHEEL WELL RT UPPER AFT CEILING SKIN CRACKED AT BS 277. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,960 hrs · 63,201 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,960 hrs · 63,201 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT AT BS 291, BETWEEN WL 259 TO WL 260. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,960 hrs · 63,201 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT AT BS 291, BETWEEN WL 241 TO WL 244. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,960 hrs · 63,201 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT BETWEEN BS 303 TO BS 304, BETWEEN WL 258 TO WL 259. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,960 hrs · 63,201 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 277, BETWEEN STR 10R TO STR 11R. REMOVED AND REPLACED SHEAR TIE PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,960 hrs · 63,201 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 291.5, BETWEEN WL 232 TO WL 234 RT SIDE. REPAIRED FRAME PER ER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,847 hrs · 62,409 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (BS 510 S15R) · airframe 67,454 hrs · 61,401 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,511 hrs · 60,727 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503B, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,511 hrs · 60,727 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739E, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,429 hrs · 60,664 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 939 AND BS 943, STR 25R AND STR 24R. REPAIRED SKIN PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 64,817 hrs · 59,479 cycles

DURING SCHEDULED BRDG CHECK, FOUND VERTICAL STABILIZER FITTING CLEVIS LUG FACES CORRODED. REPAIRED FITTING PER SWA EA.

Part: FRAME — CRACKED (BS 706 S8R) · airframe 64,817 hrs · 59,479 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,817 hrs · 59,479 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,817 hrs · 59,479 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,817 hrs · 59,479 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, BL 0. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,817 hrs · 59,479 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,817 hrs · 59,479 cycles

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

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 64,817 hrs · 59,479 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD LOWER STIFFENER CRACKED AT BS 1016, 5 O'CLOCK POSITION. REPAIRED STIFFENER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,817 hrs · 59,479 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 1121, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,817 hrs · 59,479 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,817 hrs · 59,479 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 22L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,817 hrs · 59,479 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,817 hrs · 59,479 cycles

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

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 64,817 hrs · 59,479 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 188 AND BS 196.5, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,817 hrs · 59,479 cycles

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

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 64,817 hrs · 59,479 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 188 AND BS 196.5, STR 17R. REMOVED AND REPLACED WEB PER SRM.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 64,817 hrs · 59,479 cycles

DURING SCHEDULED BRDG CHECK, FOUND LEFT WING NR 2 FLAP TRACK CORRODED AT REAR SPAR. REPAIRED FLAP TRACK PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,817 hrs · 59,479 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,685 hrs · 59,373 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 64,306 hrs · 59,068 cycles

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

Part: LIGHT — FAULTY (CABIN) · airframe 64,179 hrs · 58,968 cycles

F/A REPORTED BURNING SMELL FROM OVERHEAD CABIN LIGHT AT ROW 19 DEF. REMOVED AND REPLACED LIGHT BALLAST AND LIGHT ASSY PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 63,062 hrs · 58,127 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED EXIT SIGN PER MM.

Part: SLAT — CRACKED (RT WING) · airframe 62,862 hrs · 57,956 cycles

DURING SCHEDULED C2 CHECK, FOUND RIGHT WING NR 6 L/E SLAT CRACKED AT LOWER INBOARD T/E END. REPAIRED SLAT PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,750 hrs · 57,867 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,750 hrs · 57,867 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 62,889 hrs · 57,200 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 13 DEF TO ROW 15 DEF. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 62,889 hrs · 57,200 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 19 ABC TO ROW 21 ABC. REMOVED AND REPLACED COVER PER MM.

Part: FITTING — CRACKED (LT WING) · airframe 61,889 hrs · 57,200 cycles

DURING SCHEDULED C1 CHECK, FOUND LT MLG ACTUATOR BEAM HANGER FWD SPAR FITTING CRACKED. REMOVED AND REPLACED FITTING PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,795 hrs · 57,119 cycles

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

Part: SKIN — CRACKED (BS 407) · airframe 61,795 hrs · 57,119 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER CUTOUT, BS 407, LBL 1. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 447) · airframe 61,795 hrs · 57,119 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER CUTOUT, BS 447, LBL 1. REPAIRED SKIN PER ER.

Part: STRINGER CLIP — CRACKED (BS 294 S12L) · airframe 61,789 hrs · 57,116 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 360 S15L) · airframe 61,789 hrs · 57,116 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 61,748 hrs · 57,080 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 21 ABC. INSTALLED LENS IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,756 hrs · 56,284 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 923, STR 25L. REPAIRED SKIN PER SRM.

Part: O-RING — FAILED (SPOILER ACTUATOR) · airframe 60,437 hrs · 56,039 cycles

DECLARED EMERGENCY. DURING FLIGHT, A SYSTEM FLUID LOSS, ACCOMPLISHED QRH, YOKE DISPLACEMENT TO THE LEFT TO MAINTAIN LEVEL ATTITUDE. REPLACED O-RING PACKING ON NR 3 FLIGHT SPOILER ACTUATOR PER MM.

Part: SKIN — CRACKED (BS 767) · airframe 59,270 hrs · 55,171 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 780) · airframe 59,270 hrs · 55,171 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 730-739) · airframe 59,270 hrs · 55,171 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 730 TO BS 739, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,045 hrs · 54,154 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16R. REPAIRED SKIN PER SWA EA & SRM.

Part: LIGHT — LOOSE (EMERGENCY EXIT) · airframe 57,757 hrs · 53,889 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING LOWER EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,832 hrs · 53,149 cycles

EMERGENCY BULLNOSE LIGHT LENS MISSING AT ROW 19 DEF. INSTALLED LENS PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,562 hrs · 52,935 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE WEB CRACK AT DOME CAP, BS 1016, AFT PRESSURE BULKHEAD. REPAIRED WEB PER SWA EA.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 56,562 hrs · 52,935 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT 3RD STOP FITTING. REPAIRED R1 DOOR FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 52,935 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR, LOWER HINGE. REPAIRED FUSELAGE SKIN PER SRM.

Part: FITTING — CORRODED (LT WING) · airframe 56,562 hrs · 52,935 cycles

DURING SCHEDULED QD CHECK, FOUND CORROSION ON LT MLG STABILIZER BEAM ATTACH FITTING. REMOVED AND REPLACED LT MLG STABILIZER BEAM ATTACH FITTING PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 56,562 hrs · 52,935 cycles

DURING SCHEDULED QD CHECK, FOUND FUSELAGE BEADED PRESSURE WEB CRACKED AT BS 665, LBL 30. REPAIRED FUSELAGE WEB PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,179 hrs · 52,646 cycles

DURING SCHEDULED C3 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 21 ABC, INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 55,945 hrs · 52,446 cycles

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

Part: SLIDE — OUT OF LIMITS (R1 DOOR) · airframe 55,432 hrs · 52,056 cycles

DURING SCHEDULED A1 CHECK, FOUND R1 DOOR EVAC SLIDE IND OUT OF LIMITS. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,237 hrs · 51,899 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 957, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,237 hrs · 51,899 cycles

DURING SCHEDULED C2 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 767, BS 750, STRINGER 18L. REPAIRED SKIN SECTIONS PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 54,309 hrs · 51,127 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 54,205 hrs · 51,047 cycles

L1 DOOR EVAC SLIDE FELL OUT. INSTALLED AND SECURED L1 DOOR EVAC SLIDE PER MM.

Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 53,425 hrs · 50,426 cycles

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHT AT LT OVERWING HATCH LOOSE. SECURED SIGN PER MM.

Part: SPLICE — CRACKED (STRINGER) · airframe 51,261 hrs · 48,757 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SKIN — DELAMINATED (OUTBD FORE FLAP) · airframe 51,261 hrs · 48,757 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND LT OUTBD T/E FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED LT OUTBD T/E FORE FLAP PER MM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 51,261 hrs · 48,757 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REPAIRED STRINGER SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,505 hrs · 48,138 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 540, STR 10R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,234 hrs · 47,146 cycles

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

Part: SKIN — CRACKED (WINDOW POST) · airframe 48,370 hrs · 46,452 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED ON BOTH CAPTAIN'S AND F/O WINDOW POSTS. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,370 hrs · 46,452 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 12R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,370 hrs · 46,451 cycles

DURING SCHEDULED 1/2D CHECK, FOUND WINDOW CUTOUTS CRACKED AT BS RT 777 LT, BS 837 LT, BS 500A + 10 RT AND BS 857 RT. REPAIRED FRAMES PER SWA EA.

Part: FLOORBEAM — CORRODED (AFT CABIN) · airframe 48,370 hrs · 46,451 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 40 TO RBL 40. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: FLOORBEAM — CRACKED (MID CABIN) · airframe 48,370 hrs · 46,451 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED AT BS 663, BL 0. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,370 hrs · 46,451 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 294.5, LBL 11. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,353 hrs · 46,432 cycles

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

Part: SLIDE — DEPLOYED (FWD ENTRY DOOR) · airframe 47,653 hrs · 45,818 cycles

DURING SCHEDULED RON, FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,568 hrs · 43,225 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,603 hrs · 42,409 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL EGRESS LIGHT INOP AT AFT SVC DOOR. RELAMPED LIGHT ASSY PER MM.

Part: SKIN — DEBONDED (LT WING LE FLAP) · airframe 43,067 hrs · 41,979 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD FORE FLAP DISBONDED AT T/E, INBOARD SECTION. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,458 hrs · 41,442 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2.5 INCH EXTERNAL FUSELAGE SKIN CRACK AT BS 970, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 42,162 hrs · 41,194 cycles

DURING SCHEDULED C4 CHECK, FOUND 1.75 INCH CRACK ON LT HORIZ STAB LOWER SKIN AFT SPAR 5 FT O/B OF ROOT. REPAIRED SKIN PER SRM.

Part: CHECK VALVE — FAILED (LT WING) · airframe 41,850 hrs · 40,917 cycles

DIVERSION, UNABLE TO TRANSFER FUEL TO NR 1 TANK. REMOVED AND REPLACED NR 1 FUEL TANK CHECK VALVE PER MM.

Part: SUPPORT BRACKET — CRACKED (LT ELEVATOR) · airframe 40,240 hrs · 39,561 cycles

DURING SCHEDULED QUARTER D CHECK, FOUND LT ELEVATOR INBD LOWER CORNER PANEL SUPPORT CHANNEL CRACKED. R&R ELEVATOR ASSY PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 40,240 hrs · 39,561 cycles

DURING SCHEDULED QUARTER D CHECK, FOUND NR 5 LE SLAT LOWER SURFACE CRACKED INBD OF OUTBD AUX TRACK CUT-OUT. REPAIRED SKIN PER TI-657-012.

Part: SLIDE — DISLODGED (PAX DOOR)

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

Part: BRACKET — CRACKED (EVAC SLIDE)

DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR FWD SLIDE SUPPORT BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: SKIN — DELAMINATED (LT TE AFT FLAP)

DURING SCHEDULED C4 CHECK, FOUND LT OUTBOARD AFT FLAP DELAMINATED BETWEEN 2ND AND 3RD TRACKS. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: LIGHT — INOPERATIVE (AFT SRVC DOOR)

DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 980)

DURING SCHEDULED SERVICE CHECK, FOUND CRACKED FUSELAGE SKIN, BS 980 STRINGER 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT LE SLAT)

DURING SCHEDULED C2 CHECK, FOUND NR 2 LE SLAT INBD AUX TRACK CUT OUT CRACKED AT BOTH CORNERS. REPAIRED PER SWA RA NR 1357-0423.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SC CHECK, FOUND SEVERAL EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM, CKS GOOD.

Part: SWITCH — FAILED (NR 2 LE FLAP)

NR 2 L/E FLAP REMAINED FULL EXTEND AFTER RETRACTION ON DEPARTURE. RETURNED TO BURBANK. REMOVED AND REPLACED NR 2 LEADING EDGE FLAP PROX SWITCH PER MM, OPS CHECK GOOD.

Part: SKIN — CRACKED (LT WING)

DURING SCHEDULED C2 CHECK, FOUND NR 1 SLAT I/B AUX TRACK CUTOUT CRACKED IN 2 PLACES AT AFT EDGE. REPAIRED PER SWA RA NR 1-357-0545.

Part: FRAME — CRACKED (BS 907)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 907, S1R. REPAIRED PER BOEING SRM.

Part: BEAM — CRACKED (BS 213.32)

DURING SCHEDULED D-CHECK, FOUND RT HORZ STAB T/E BEAM CRACKED AT FS 213.32. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (SERVICE DOOR)

DURING SCHEDULED D-CHECK, FWD FUSELAGE SKIN CRACKED AT LOWER AFT CORNER OF FWD SERVICE DOOR CUTOUT. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 274)

DURING SCHEDULED D-CHECK, FWD FUSELAGE SKIN GOUGED AND DENTED AT 274 BELOW S4L. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 992/997)

DURING SCHEDULED D-CHECK, FWD FUSELAGE SKIN DENTED AT BS 992 AND 997. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 328/727-947)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 328 AND FROM 727 TO 947. REPAIRED PER BOEING SRM.

Part: SKIN — OIL CANNING (BS 380-387)

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN OIL CANNING AT BS 380-387, 5 BELOW S18R. REPAIRED PER BOEING SRM.

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND RT CHORD CRACKED IN RADIUS AT BS 178, WL 207. REPLACED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 188, WL 197 TO 201.75, 197.25 TO 201.25, 208.25 TO 208.75, AND AT 211.25 TO 210.75. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 727)

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT BS 727C, 803, AND 500. REPAIRED PER BOEING SRM.

Part: CREASE BEAM — CRACKED (BS 179)

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CRACKED AT BS 179 LEFT AND RIGHT, WL 207. REPAIRED PER BOEING SRM.

Part: CLIP — CRACKED (BS 500)

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, S19L. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 978)

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 978, JUST BELOW S19L. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 363-375)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AND GOUGED AT BS 363 TO 375, S4L TO 6L. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 500)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE DENTED AT BS 500B, ABOVE S25R AND AT BS 500D+12 AND +18, AT BS 300, S18R, AT BS 338.5, S18R, AND BS 344. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 933)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 933, 2 BELOW S19L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR FRAME TOP CUTOUT CRACK TOP CORNER. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR FRAME LOWER CUTOUT CRACKED APPROX .5 INCH. REPAIRED PER BOEING SRM AND SWA RA 1-353-1672.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR FRAME TOP CUTOUT CRACKED APPROX 1 INCH IN TOP CORNER. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED BC2 CHECK, FOUND FUSELAGE SKIN CRACKED JUST AFT OF WATER SERVICE PANEL. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 951)

DURING SCHEDULED BC2 CHECK, FOUND FUSELAGE SKIN CRACKED 2.25 INCHES, 4 FWD OF BS 951, AT S24L. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (WS 208)

DURING SCHEDULED BC2 CHECK, FOUND WING FIXED L/E RIB GOUGED AFT OF NR 4 KREUGER FLAP. REPAIRED PER SWA RA 1-357-0430.

Part: SKIN — CRACKED (LT WING)

DURING SCHEDULED BC2 CHECK, FOUND NR 1 SLAT CRACKED ACTUATOR CUTOUT. REPAIRED PER SWA RA 1-A57-0377.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED C2 CHECK, FOUND A RED FLOOR TRACK LIGHT INOP. REPLACED PER BOEING M/M.

Part: SKIN — DENTED (BS 988)

DURING SCHEDULED C4 CHECK, FOUND SHARP DENT ON FUSELAGE SKIN BS 988 AT STRINGER 16L. REPAIRED PER SWA RA 1-353-1519.

Part: SKIN — CRACKED (BS 877)

DURING SCHEDULED TERM CHECK, FOUND A 2 INCH FUSELAGE SKIN CRACK AT BS 877, JUST AFT OF EMERGENCY LIGHT. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACK AT BS 727D BELOW STRINGER 20L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.