N318SW

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 80,629 hrs · 73,246 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SLIDE IAW MT.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK FOUND, SHEAR TIE CORRODED AT BS 380, STR 28L. REPAIRED SHEAR TIE IAW ER AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK FOUND, SHEAR TIE CORRODED AT BS 440, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK FOUND, FRAME CRACKED AT BS 400, STR 26L. REPAIRED FRAME PER ER AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK FOUND, SHEAR TIE CORRODED AT BS 360, STR 28R. REPAIRED SHEAR TIE IAW ER AND EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK FOUND, STRINGER CORRODED BETWEEN BS 767 TO BS 787, STR 22L. REPAIRED STRINGER PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK FOUND, SKIN CORRODED AT BS 532, STR 27R. REPAIRED SKIN IAW ER AND EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULE 26Y CHECK FOUND, STRINGER CORRODED AT BS 897, STR 21L. REMOVED AND REPLACED STRINGER PER ER AND EA.

Part: LENS — MISSING (CABIN) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK FOUND, LT OVERWING OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK FOUIND, SHEAR TIE CORRODED AT BS 500B, BL 0L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 480, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN LBL 6 TO RBL 6. REPAIRED ER AND EA.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND FWD CARGO BEAR STRAP CORRODED AT BS 441, RBL 11. REPAIRED STRAP IAW EA AND ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 747 TO BS 787, STR 26R. REPAIRED STRINGER IAW SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND FWD CARGO BAY FITTING CORRODED AT BS 540, STR 27L. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT KEEL BEAM CORRODED AT BS 500D+2. REPAIRED BEAM PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND FWD CARGO BAY SKIN CORRODED AT BS 500C+16, STR 26L. REPAIRED SKIN IAW MT.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 747, STR 26R. REMOVED AND REPLACED CLIP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 27R TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 27R TO STR 26R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 460, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED AT BS 500C+19, STR 27L. REMOVED AND REPLACED STRINGER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986, BETWEEN STR 19R TO STR 20R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED AT BS 807, STR 26L. REMOVED AND REPLACED STRINGER IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CORRODED AT BS 747, BETWEEN STR 23L TO STR 24L. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED AT BS 500D, STR 27R. REMOVED AND REPLACED STRINGER PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 50. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, LBL 6. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 27L TO STR 28L. REPAIRED SHEAR TIE IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 747 TO BS 787, STR 26L. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727C, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE IAW SRM.

Part: BEAR STRAP — CORRODED (BS 411) · airframe 50,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND BEAR STRAP CORRODED AT BS 411, RBL 11. REPAIRED BEAR STRAP PER SRM.

Part: SHEAR TIE — CORRODED (BS 500) · airframe 80,537 hrs · 73,174 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, RBL 6. REMOVED AND REPLACED SHEAR TIE PER SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,294 hrs · 72,986 cycles

DURING SCHEDULED MV1 CHECK FOUND, STRINGER CORRODED BETWEEN BS 945 TO BS 944, STR 27L. REPAIRED STRINGER IAW EO.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,294 hrs · 72,986 cycles

DURING SCHEDULED OTS CHECK FOUND, STRINGER CORRODED AT BS 827+12, STR 27R. REPAIRED STRINGER IAW SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 80,294 hrs · 72,986 cycles

DURING SCHEDULED OTS CHECK FOUND, BEAR STRAP CRACKED AT BS 847, BETWEEN STR 26R TO STR 27R. REPAIRED SKIN IAW EA.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 80,294 hrs · 72,986 cycles

DURING SCHEDULED OTS CHECK FOUND, BEAR STRAP CORRODED AT BS 847, STR 27R. REPAIRED SKIN IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,294 hrs · 72,986 cycles

DURING SCHEDULED MV1 CHECK FOUND, STRINGER CORRODED BETWEEN BS 945 TO BS 954, STR 27L. REPAIRED STRINGER IAW EO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,294 hrs · 72,986 cycles

DURING SCHEDULED OTS CHECK FOUND, SHEAR TIE CORRODED AT BS 967, BETWEEN STR 27R TO STR 26R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 80,294 hrs · 72,986 cycles

DURING SCHEDULED SPV CHECK FOUND, FRAME CORRODED AT BS 947, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 80,294 hrs · 72,986 cycles

DURING SCHEDULED SPV CHECK FOUND, SKIN CORRODED AT BS 948, STR 27L. REPAIRED SKIN IAW AAR EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,296 hrs · 72,987 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CORRODED AT BS 827+8, STR 26L. REPAIRED STRINGER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,268 hrs · 72,967 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE CROWN SKIN CRACKED AT BS 480+15, STR 2L. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 79,694 hrs · 72,513 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,330 hrs · 72,234 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 867, STR 17L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,330 hrs · 72,234 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,323 hrs · 72,232 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 867, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,330 hrs · 72,234 cycles

DURING SCHEDULED OTS CHECK, FOUND FSLG SKIN CRACK AT STA 422, BELOW STR 2R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,330 hrs · 72,234 cycles

DURING SCHEDULED OTS CHECK, FOUND FSLG SKIN CRACK AT STA 887, ABOVE STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,330 hrs · 72,234 cycles

DURING SCHEDULED OTS CHECK, FOUND FSLG SKIN CRACK AT STA 395, ABOVE STR 2R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,323 hrs · 72,232 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 395, STR 2R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,323 hrs · 72,232 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 442, STR 2R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,330 hrs · 72,234 cycles

DURING SCHEDULED OTS CHECK, FOUND FSLG SURFACE CRACK AT STA 867, 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,323 hrs · 72,232 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 887, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,323 hrs · 72,232 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 412, STR 2R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,330 hrs · 72,234 cycles

DURING SCHEDULED OTS CHECK, FOUND FSLG SKIN CRACK AT STA 412, BELOW STR 2R. REPAIRED SKIN PER SRM.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 79,286 hrs · 72,208 cycles

AIRTURN BACK, SMOKE ALARM IN AFT LAV WENT OFF IN FLIGHT. RETURNED TO PHL. NO SIGN OF SMOKE. REMOVED AND REPLACED AFT LAV SMOKE DETECTOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,157 hrs · 72,103 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 378, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,809 hrs · 71,842 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 271, STR 16R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,809 hrs · 71,842 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 348, STR 19R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,806 hrs · 71,841 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 348, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,809 hrs · 71,842 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 348, STR 18R. REPAIRED SKIN PER EA.

Part: ANGLE — BROKEN (RT WING) · airframe 77,745 hrs · 71,010 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING STRUT PANEL 585R UPPER SUPPORT ANGLE FWD FASTENER BROKEN. REMOVED AND REPLACED ANGLE PER SRM AND EA.

Part: SLAT — DELAMINATED (RT WING) · airframe 77,696 hrs · 70,968 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 4 SLAT DELAMINATED. REMOVED AND REPLACED NR 4 SLAT PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 77,696 hrs · 70,968 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,630 hrs · 70,910 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 760, STR 18L. REPAIRED SKIN PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,630 hrs · 70,910 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,630 hrs · 70,910 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 513.1B TO BS 514.2B, STR 16L. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,630 hrs · 70,910 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 495, STR 3R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,630 hrs · 70,910 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 506C, STR 26R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,630 hrs · 70,910 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 505, STR 16L. REPAIRED SKIN PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,630 hrs · 70,910 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,630 hrs · 70,910 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 749, STR 18L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,069 hrs · 70,476 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,819 hrs · 70,287 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 522, STR 2R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,819 hrs · 70,287 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 910, STR 3L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,819 hrs · 70,287 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 362, STR 6R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,822 hrs · 70,288 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 522, STR 2R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,822 hrs · 70,288 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 908, STR 3L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,822 hrs · 70,288 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 362, STR 6R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,822 hrs · 70,288 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 494, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,822 hrs · 70,288 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 526, STR 2R. REPAIRED SKIN PER SRM.

Part: LIGHT — WORN (CABIN) · airframe 76,819 hrs · 70,287 cycles

DURING SCHEDULED CV CHECK, FOUND RT EEPLS STRIPS WORN AT ROW 12. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,096 hrs · 69,754 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 752, STR 14R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,096 hrs · 69,754 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 969.5, STR 5R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,099 hrs · 69,755 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 969, STR 5R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,096 hrs · 69,754 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 376, STR 15L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,096 hrs · 69,754 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 525, STR 2L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,099 hrs · 69,755 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 525, STR 2L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,099 hrs · 69,755 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 376, STR 15L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,099 hrs · 69,755 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BS 752, STR 14R. REPAIRED SKIN PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,099 hrs · 69,755 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,099 hrs · 69,755 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: SIGN — LOOSE (CABIN) · airframe 76,096 hrs · 69,754 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND RT OVERWING EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED SIGN PER MM.

Part: ATTACH FITTING — CRACKED (SPOILER) · airframe 76,096 hrs · 69,754 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND LT WING INBOARD NR 4 GROUND SPOILER O/B ATTACH FITTING CRACKED. REMOVED AND REPLACED SPOILER PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 76,096 hrs · 69,754 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 907 BETWEEN STR 13R & STR 14R. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 328, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN PANEL CRACKED AT BS 178, AT 12 O'CLOCK POSITION. REMOVED AND REPLACED PANEL PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 328, STR 19R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 20R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 907, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500D, STR 20R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 20R. REPAIRED FRAME PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CORRODED AT BS 917, STR 26R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 767, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 14L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 952, STR 24R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 13L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 390, STR 26R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10L. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10L. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 13R. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23R. REMOVED AND REPLACED CLIP PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 9L. REMOVED AND REPLACED CLIP PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8R. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 24R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 887, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,383 hrs · 69,227 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,340 hrs · 69,198 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 810, STR 19L. REPAIRED SKIN PER SWA EA.

Part: BATTERY — FAULTY (CABIN) · airframe 74,669 hrs · 68,712 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT FLICKERING. REMOVED AND REPLACED LIGHT BATTERY ASSY.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,669 hrs · 68,712 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 736C, STR 14L. REPAIRED SKIN PER SRM AND EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 74,669 hrs · 68,712 cycles

DURING SCHEDULED HC2 CHECK, FOUND AFT GALLEY OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BATTERY ASSY.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,097 hrs · 68,315 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 74,097 hrs · 68,315 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 440, STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,039 hrs · 68,278 cycles

DURING SCHEDULED MV4 CHECK, FOUND SKIN CRACKED BETWEEN BS 515A TO BS 505B, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,039 hrs · 68,278 cycles

DURING SCHEDULED MV4 CHECK, FOUND SKIN CRACKED AT BS 792, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,039 hrs · 68,278 cycles

DURING SCHEDULED MV4 CHECK, FOUND SKIN CRACKED AT BS 514, STR 16L. REPAIRED SWA SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,039 hrs · 68,278 cycles

DURING SCHEDULED MV4 CHECK, FOUND SKIN CRACKED BETWEEN BS 784.4 TO BS 785, BETWEEN STR 20L TO STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,039 hrs · 68,278 cycles

DURING SCHEDULED MV4 CHECK, FOUND SKIN CRACKED AT BS 406, STR 16L. REPAIRED SWA SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,039 hrs · 68,278 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT R2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 73,168 hrs · 67,677 cycles

R1 DOOR EMERGENCY EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 72,193 hrs · 66,930 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS STAY ILLUMINATED. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 71,709 hrs · 66,582 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG 685 FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: FITTING — CORRODED (FUSELAGE) · airframe 71,709 hrs · 66,582 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG 685 FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,599 hrs · 66,496 cycles

DURING SCHEDULED BRDG CHECK, FOUND FWD LAV AFT WALL EXIT LIGHT BULBS INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (BS 303) · airframe 71,599 hrs · 66,496 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR FUSELAGE SKIN CUTOUT CRACKED AT BS 303.90, WL 236.68. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (BS 616 S17L) · airframe 71,599 hrs · 66,496 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, STR 17L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 947 S11L) · airframe 71,599 hrs · 66,496 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 947, STR 11L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (BS 291) · airframe 71,599 hrs · 66,496 cycles

DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR FUSELAGE SKIN CUTOUT CRACKED AT BS 291.50, WL 233.50. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,599 hrs · 66,496 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS BS 616, STR 17L. REPAIRED FRAME PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 71,599 hrs · 66,496 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING OUTBOARD FORE FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,599 hrs · 66,496 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 71,599 hrs · 66,496 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 950 TO BS 955, RBL 50. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,599 hrs · 66,496 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,599 hrs · 66,496 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 330, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,599 hrs · 66,496 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 330, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,318 hrs · 66,281 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 370, STR 2L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 71,318 hrs · 66,281 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,318 hrs · 66,281 cycles

DURING SCHEDULED C2 CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 26R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,318 hrs · 66,281 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,318 hrs · 66,281 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 26R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,318 hrs · 66,281 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 908, BETWEEN STR 2L AND STR 3L. REPAIRED SKIN PER SWA EA.

Part: SKIN — WORN (FORE FLAP) · airframe 71,318 hrs · 66,281 cycles

DURING SCHEDULED C2 CHECK, FOUND RIGHT WING OUTBOARD FORE FLAP UPPER SURFACE WORN. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,318 hrs · 66,281 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 400, STR 2R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,318 hrs · 66,281 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 810, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,318 hrs · 66,281 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 832, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,889 hrs · 65,943 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 263, STR 9L. REPAIRED SKIN PER SWA EA.

Part: GLOWSTRIP — BROKEN (CABIN) · airframe 70,462 hrs · 65,632 cycles

EEPLS PHOTOLUMINESCENT STRIP BROKEN AT LT OVERWING EMERGENCY EXIT ROW. REMOVED AND REPLACED STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,118 hrs · 65,382 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727C, STR 14R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,118 hrs · 65,382 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,118 hrs · 65,382 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,118 hrs · 65,382 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 317, STR 18R. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (BS 779-792) · airframe 69,486 hrs · 64,895 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 779 AND BS 792, STR 18L AND STR 19L. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 69,187 hrs · 64,601 cycles

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

Part: CONNECTOR — FAULTY (MLG W/W) · airframe 69,041 hrs · 64,548 cycles

RIGHT MLG RED LIGHT ILLUMINATED INTERMITTENTLY DURING FLIGHT. REMOVED AND REPLACED UPLOCK SENSOR AND CONNECTOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,911 hrs · 64,453 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 415, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,911 hrs · 64,453 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 474, STR 16L. REPAIRED SKIN PER SRM.

Part: LIGHT — DISLODGED (EMERGENCY EXIT) · airframe 68,784 hrs · 64,352 cycles

L2 DOOR EMERGENCY EXIT LIGHT ASSY FELL OFF. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 68,210 hrs · 63,882 cycles

DURING SCHEDULED SPV CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 68,197 hrs · 63,872 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,197 hrs · 63,872 cycles

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

Part: SKIN — CRACKED (BS 410) · airframe 67,554 hrs · 63,388 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT NR 2 RADIO ALTIMETER ANTENNA CUTOUT BS 410, BL 0. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 520 S28R) · airframe 67,554 hrs · 63,388 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28R. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,554 hrs · 63,388 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,554 hrs · 63,388 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 378, STR 26L. REPAIRED SKIN PER SWA EA.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 67,078 hrs · 63,049 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT NOSE WHEEL WELL PRESSURE WEB CRACKED AT BS 259, WL 174. REPAIRED WEB PER SWA EA.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 67,078 hrs · 63,049 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT NOSE WHEEL WELL PRESSURE WEB CRACKED AT BS 247, WL 168.6. REPAIRED WEB PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,571 hrs · 62,657 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 812, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,571 hrs · 62,657 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 840, STR 17L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,571 hrs · 62,657 cycles

DURING SCHEDULED C1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT IINOP AT ROW 19 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,931 hrs · 61,388 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 732, STR 14L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — LOW (R2 DOOR) · airframe 63,669 hrs · 60,408 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM.

Part: CABLE — MISROUTED (R2 DOOR SLIDE) · airframe 63,653 hrs · 60,396 cycles

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

Part: SKIN — CRACKED (L1 DOOR) · airframe 63,325 hrs · 60,154 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR SKIN CRACKED AT LOWER AFT CORNER. REPAIRED SKIN PER SWA EA & SRM.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 63,217 hrs · 60,066 cycles

DURING SCHEDULED D CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REPAIRED GROUND WIRES L3 & L4 PER WDM. OPS CHECK OK PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 500C TO BS 740. REMOVED AND REPLACED LT KEEL BEAM PER SRM.

Part: SKIN — CRACKED (BS 454) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 454, STR 16R. REMOVED AND REPLACED SIDE SKIN PANEL BETWEEN BS 360 TO BS 540, STR 14R TO STR 19R PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 741, STR 27L. REPAIRED SKIN PER BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED/CRACKED BETWEEN BS 259 TO BS 360, STR 19R TO STR 24R. REPAIRED SKIN PER BFG ER.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT BS 442, RBL 8, FWD CARGO DOOR CUTOUT. REPAIRED SKIN PER BFG ER & SRM.

Part: FRAME — CRACKED (BS 440) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 24R. REPAIRED FRAME PER BFG ER.

Part: STIFFENER — CORRODED (BS 1017) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER CORRODED AT BS 1017, LBL 10. REPAIRED RADIAL STIFFENER PER BFG ER.

Part: BULKHEAD — CRACKED (BS 178) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE BS 178 BLKHD LT SIDE WEB CRACKED. REPAIRED BS 178 BLKHD WEB PER SRM.

Part: STRINGER CLIP — CRACKED (BS 827) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 827, RBL 23. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 188) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, STR 17R. REPAIRED STUB FRAME PER SRM.

Part: FRAME — CRACKED (BS 663) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 2L. REPAIRED FRAME PER BFG ER.

Part: CHANNEL — CORRODED (COCKPIT FLOOR) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR Z-CHORD CORRODED AT BS 270, BETWEEN LBL 54 TO RBL 54, WL 208. REMOVED AND REPLACED Z-CHORD PER SRM.

Part: FLOORBEAM — CORRODED (BS 259) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 259, BETWEEN LBL 11 TO RBL 11, WL 208. REPAIRED FLOORBEAM PER BFG ER.

Part: FLOORBEAM — CRACKED (BS 947) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CRACKED AT BS 947.5, LBL 55, WL 208. REPAIRED FLOORBEAM PER BFG ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 277, STR 11R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 277) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER BFG ER.

Part: FRAME — CRACKED (BS 188) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, RT SIDE, WL 207. REPAIRED STUB FRAME PER SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND CABIN FLOORBEAM CORRODED AT BS 986.5, RBL 45. REPAIRED FLOORBEAM PER BFG ER AND SRM.

Part: WEB — CRACKED (COCKPIT FLOOR) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR WEB CRACKED BETWEEN BS 188 TO BS 196.5, RBL 29, WL 207. REPAIRED FLOOR WEB PER SRM.

Part: SHEAR TIE — CRACKED (BS 967) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 967, STR 4L TO STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 827) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 1R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 188) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, LT SIDE, WL 208. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: WEB — CRACKED (COCKPIT FLOOR) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR WEB CRACKED BETWEEN BS 188 TO BS 196.5, LBL 29, WL 207. REPAIRED FLOOR WEB PER SRM.

Part: STRINGER — CRACKED (BS 344) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 344, STR 8R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FRAME — CRACKED (BS 360) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (BS 967) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 967, STR 26L. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (BS 400) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 400, STR 2L. REPAIRED STRINGER PER SRM.

Part: DOOR FRAME — CRACKED (AFT CARGO) · airframe 63,215 hrs · 60,065 cycles

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

Part: SHEAR TIE — CORRODED (BS 787) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 578) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (AFT CARGO) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND AFT CARGO DOOR CUTOUT, FWD FRAME CORRODED BETWEEN STR 24R TO STR 25R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 303) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME ANGLE CRACKED AT BS 303, STR 4L. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 400) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 400, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 400) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (BS 597) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 597, BETWEEN STR 13R TO STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 727E) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 360) · airframe 63,215 hrs · 60,065 cycles

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

Part: STRINGER CLIP — CRACKED (BS 827) · airframe 63,215 hrs · 60,065 cycles

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

Part: FRAME — CRACKED (BS 907) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 440) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 767) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (BS 639) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 639, BETWEEN STR 7R TO STR 8R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 867) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360) · airframe 63,215 hrs · 60,065 cycles

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

Part: SPACER — WORN (L2 DOOR SLIDE) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CONTAINER FWD BRACKET GUIDE SPACER WORN. REMOVED AND REPLACED SPACER PER MM.

Part: STRINGER CLIP — CRACKED (BS 277) · airframe 63,215 hrs · 60,065 cycles

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

Part: SHEAR TIE — CORRODED (BS 967) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 967, BETWEEN BL 0 TO BL 3, LT SIDE. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 2R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 947.5) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 947.5, BETWEEN STR 10R TO STR 13R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 277) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 277, STR 10L. REMOVED AND REPLADED CLIP PER SRM.

Part: FRAME — CRACKED (BS 328) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME TO SKIN ATTACH ANGLE CRACKED AT BS 328, LBL 45, WL 206. REPAIRED ATTACH ANGLE PER SRM.

Part: FLOORBEAM — CORRODED (BS 295) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND CABIN FLOORBEAM CORRODED AT BS 295, BETWEEN LBL 20 TO RBL 59, WL 208. REPAIRED FLOORBEAM PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 5R. REPAIRED WEB PER SRM.

Part: FLOORBEAM — CORRODED (CABIN FLOOR) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM UPPER CHORD CORRODED AT BS 312, BETWEEN LBL 10 TO RBL 32, WL 208. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (AFT CARGO) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 927, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (AFT CARGO) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 927, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 500D TO BS 727. REMOVED AND REPLACED KEEL BEAM PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 277, STR 11L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 1006, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (CABIN FLOOR) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 360 TO BS 380, WL 208. REPAIRED CREASE BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (AFT CARGO) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 927, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (AFT CARGO) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 986, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (AFT CARGO) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 927, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (AFT CARGO) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (CABIN FLOOR) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED BETWEEN BS 540 TO BS 727, RBL 25. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 704, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: FITTING — CORRODED (TAIL) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND LT AND RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (HORIZONTAL STAB) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STAB OTBD T/E UPPER SKIN DELAMINATED. REPAIRED STAB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — BROKEN (BS 867) · airframe 63,215 hrs · 60,065 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP BROKEN AT BS 867, STR 23R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 63,215 hrs · 30,065 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 62,738 hrs · 59,700 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (BS 460) · airframe 62,738 hrs · 59,700 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 460, STR 17R. MX FERRY TO DALLAS. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 810) · airframe 62,738 hrs · 59,700 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 810, STR 14R. MX FERRY TO DALLAS. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 400) · airframe 62,738 hrs · 59,700 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 400, STR 26R. MX FERRY TO DALLAS. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 920) · airframe 62,738 hrs · 59,700 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 920, STR 25R. MX FERRY TO DALLAS. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 424) · airframe 62,738 hrs · 59,700 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 424, STR 26L. MX FERRY TO DALLAS. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,454 hrs · 59,477 cycles

DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 480, STR 16L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,150 hrs · 59,249 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,761 hrs · 58,918 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 972, STR 21L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,761 hrs · 58,918 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 468, STR 16R. REPAIRED SKIN PER SWA EA & SRM.

Part: ENGINE — MAKING METAL (NR 1) · airframe 61,761 hrs · 58,918 cycles

DURING SCHEDULED C4 CHECK, NR 1 ENGINE FWD SUMP CHIP DETECTOR HAD EXCESSIVE METAL DEBRIS. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: HINGE — BROKEN (RT WING SPOILER) · airframe 60,762 hrs · 58,145 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING NR 5 GROUND SPOILER HINGE BROKEN. REMOVED AND REPLACED RT WING NR 5 GROUND SPOILER PER MM.

Part: STRUCTURE — CRACKED (BULKHEAD) · airframe 59,774 hrs · 57,370 cycles

DURING SCHEDULED C2 CHECK, FOUND 2 EACH CRACKS AT AFT PRESSURE BULKHEAD Y-CHORD AT BS 1016, STRINGER 6L AND STRINGER 6R. REPAIRED Y-CHORD SECTIONS PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,774 hrs · 57,370 cycles

DURING SCHEDULED C2 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS AT BS 312, STRINGER 25R, BS 386, STRINGER 17R, BS 390, STRINGER 17R. REPAIRED SKIN SECTIONS PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,774 hrs · 57,370 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 273, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 59,774 hrs · 57,370 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT OUTBOARD AFT T/E FLAP PER MM.

Part: WEDGE — DELAMINATED (RT WING SLAT) · airframe 59,774 hrs · 57,370 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING NR 4 L/E SLAT WEDGE DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,774 hrs · 57,370 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 19R, CRACKED. REPAIRED SKIN PER EA.

Part: GIRT BAR — LOOSE (L1 DOOR SLIDE) · airframe 59,774 hrs · 57,370 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FWD FLOOR ANCHOR LOOSE. REMOVED AND REPLACED FLOOR ANCHOR PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 59,774 hrs · 57,370 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 59,774 hrs · 57,370 cycles

DURING SCHEDULED C2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 59,774 hrs · 57,370 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,697 hrs · 57,304 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,697 hrs · 57,304 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 727D, BS 727B, STRINGER 14R. REPAIRED SKIN PER RA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,375 hrs · 57,036 cycles

DURING SCHEDULED A1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 17 ABC, INOP. RELAMPED LIGHT PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,327 hrs · 56,993 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT RT AND LT EMERGENCY EXIT LIGHTS INOP. RELAMPED EMERGENCY LIGHTS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,854 hrs · 56,612 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 380, STRINGER 16R, BS 400, STRINGER 17R, CRACKED. REPAIRED SKIN PER EA AND SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 58,854 hrs · 56,612 cycles

DURING SCHEDULED C1 CHECK, FOUND SHEAR TIE AT BS 380, STRINGER 15R, CRACKED. REPAIRED SHEAR TIE PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 58,608 hrs · 56,412 cycles

OVERHEAD EMERGENCY EXIT LIGHT LENS AT ROW 2 ABC, LOOSE. SECURED OVERHEAD LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,033 hrs · 55,941 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 917, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 58,033 hrs · 55,941 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD GALLEY OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED EMERGENCY EXIT LENS PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 57,361 hrs · 55,418 cycles

L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,540 hrs · 54,779 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 431, STR 26L, AND BS 512B, STR 26R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,429 hrs · 54,696 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 390, STR 16R. REPAIRED SKIN PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 55,292 hrs · 53,747 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT KEEL BEAM CORRODED AT BS 727, LBL 7. REPAIRED KEEL BEAM PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 55,292 hrs · 53,747 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 665, RBL 36. REPAIRED PRESSURE WEB PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 55,292 hrs · 53,747 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NLG W/W CRACKED (2 EA) AT RT UPPER WEB TIRE BRAKE ATTACH HOLES. REPAIRED UPPER WEB PER SWA EA.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 55,292 hrs · 53,747 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS PANEL CRACKED AT BS 664, LBL 36. REPAIRED PRESS WEB PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,292 hrs · 53,747 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 668, RBL 24. REPAIRED FLOORBEAM PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,292 hrs · 53,747 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STUB FRAME CRACKED AT BS 360, STR 14R. REPAIRED FRAME PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 55,292 hrs · 53,747 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED AT BS 672, RBL 36. REPAIRED PRESS WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,239 hrs · 53,701 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND OUTER FRAME CRACKED AT BS 639, STR 17R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,249 hrs · 53,709 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA SHEAR TIES CRACKED AT BS 360, STRINGERS 14L & 14R. REPAIRED SHEAR TIES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,249 hrs · 53,709 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW FRAME CRACKED AT BS 470 LT SIDE. REMOVED AND REPLACED WINDOW FRAME PER ERO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,249 hrs · 53,709 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED 7 INCH LONG AT BS 639 STRINGER 16L. REPAIRED FRAME PER ERO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,239 hrs · 53,701 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED, BS 360, STRINGER 10R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,239 hrs · 53,701 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SHEAR TIE CRACKED, BS 500C STRINGER 15R. REPAIRED SHEAR TIE PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 55,239 hrs · 53,701 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,212 hrs · 53,683 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,208 hrs · 53,679 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT BS 480 AT STR 16R, BS 520 AT STR 4L AND BS 727B AT STR 10R. REPAIRED SKIN PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 54,820 hrs · 53,375 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,820 hrs · 53,375 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 792, ABOVE STR 19L. REPAIRED SKIN PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 54,352 hrs · 53,007 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 1 L/E SLAT CRACKED AT T/E EDGE. REMOVED AND REPLACED NR 1 L/E SLAT PER MM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 54,352 hrs · 53,007 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,352 hrs · 53,007 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,352 hrs · 53,007 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, STR 4L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,343 hrs · 52,999 cycles

DURING SCHEDULED A2 CHECK, FOUND AFT LT EXTERIOR EMERGENCY EXIT LIGHT AND 3 EA INTERIOR OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED MID CABIN BATTERY PACK AND BATTERY CHARGER BASE ASSY PER MM.

Part: SKIN — CRACKED (SKIN) · airframe 53,761 hrs · 52,538 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 11, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,761 hrs · 52,538 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW CUTOUTS CRACKED AT LT WINDOWS NR 1, NR 2, NR 32, NR 3 AND NR 6. REPAIRED FRAMES PER BFG ER AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,761 hrs · 52,538 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 11, STR 14L. REPAIRED SKIN PER BFG ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,761 hrs · 52,538 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 12, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,761 hrs · 52,538 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 14L, BS 370 AND BS 380. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,761 hrs · 52,538 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L AND STR 4L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,761 hrs · 52,538 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (3 EA) AT BS 500A PLUS 11 AT STR 14L, BS 380 AT STR 10L AND BS 495 AT STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,761 hrs · 52,538 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 511 AT STR 4R AND BS 430 AT STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,761 hrs · 52,538 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 392 AT STR 10R AND BS 460 AT STR 14R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,761 hrs · 52,538 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 440 AND BS 448, STR 4R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,761 hrs · 52,538 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,761 hrs · 52,538 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500A PLUS 11, STR 14R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,761 hrs · 52,538 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,761 hrs · 52,538 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,761 hrs · 52,538 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 53,625 hrs · 52,432 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,354 hrs · 51,390 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,344 hrs · 51,378 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,787 hrs · 50,096 cycles

DURING WALK AROUND ON SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 328, STR 21R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,420 hrs · 49,777 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED 1.0 INCH LONG AT BS 486, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,420 hrs · 49,777 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED 4.0 INCHES AT BS 440, FWD UPPER CORNER CUTOUT FOR FWD CARGO DOOR. REPAIRED SKIN PER SRM.

Part: ACTUATOR — LEAKING (# 3 SPOILER) · airframe 50,024 hrs · 49,435 cycles

( DIVERSION, DECLARED EMERGENCY )…………………………LOSS OF A SYSTEM HYDRAULIC FLUID. FOUND # 3 SPOILER ACTUATOR LEAKING, R&R 'O' RINGS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,964 hrs · 49,383 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 4 INCH CRACK AT AFT SVC DOOR LWR FWD CORNER OF FUSELAGE SKIN CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,927 hrs · 49,353 cycles

DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN CRACKED 3 INCHES LONG AT BS 747, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,927 hrs · 49,353 cycles

DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN CRACKED 3.750 INCHES LONG AT BS 935, STR 26R REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,927 hrs · 49,353 cycles

DURING SCHEDULED BC3 CHECK, FOUND ( 3 EA ) FUSELAGE SKIN CRACKS AT STR 4R, BS 410, BS 520 & BS 482. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,605 hrs · 48,249 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2.25 INCH LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 500+4, STR 10L. REPAIRED SKIN PER BAC SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,605 hrs · 48,249 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 1.5 INCH LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 944, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,605 hrs · 48,249 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 1.25 INCH LONG EXTERNAL FUSELAGE SKIN CRACK AT 758, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,605 hrs · 48,249 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2.25 EXTERNAL FUSLEAGE SKIN CRACK AT BS 524, ABOVE STR 10R. REPAIRED SKIN PER BAC SB & SWA RA.

Part: LENS — LOOSE (CABIN) · airframe 48,355 hrs · 48,033 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 3 ABC. SECURED LENS PER MM.

Part: DOOR FRAME — CRACKED (ENTRY DOOR) · airframe 47,476 hrs · 47,285 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR LOWER FWD CORNER FRAME CRACKED. R&R LOWER FRAME SECTION PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 47,476 hrs · 47,285 cycles

1/2D CHECK, FOUND BS 663 BULKHEAD STIFFNERS CRACKED AT LBL 6.15 & RBL 6.25. R&R STIFFNERS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,476 hrs · 47,285 cycles

DURING SCHEDULED 1/2D CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 420, STR 16R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (COCKPIT) · airframe 47,476 hrs · 47,285 cycles

DURING SCHEDULED 1/2D CHECK, FOUND F/O NR 1 WINDOW FRAME POST CRACKED AT UPPER OUTBOARD CORNER. REPAIRED FRAME POST PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,476 hrs · 47,285 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 4 EGRESS BULLNOSE LIGHTS INOP IN CABIN. REMOVED AND REPLACED 1 BATTERY PACK AND 2 BULBS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 47,476 hrs · 47,285 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BULLNOSE EGRESS LIGHTS LOOSE AT ROW 3 ABC & ROW 16 DEF. SECURED LIGHTS PER SRM.

Part: LIGHT — DAMAGED (CABIN) · airframe 47,476 hrs · 47,285 cycles

DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY EXIT LIGHT IN BULLNOSE PUSHED IN AT ROW 7. REPOSITIONED LIGHT ASSY PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 47,476 hrs · 47,285 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 797, STR 27R. REPAIRED SKIN PER RA 1-353-2391.

Part: STRINGER CLIP — CRACKED (CABIN) · airframe 47,476 hrs · 47,285 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STR CLIPS CRACKED AT BS 344 STR 11R, BS 294 STR 12L & BS 294 STR 11L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: SHEAR TIE — CRACKED (CABIN) · airframe 47,476 hrs · 47,285 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 663 BELT FRAME SHEAR TIE CRACKED AT STR 10L. REPAIRED FRAME PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,476 hrs · 47,285 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 221, RBL 17. REPAIRED WEB PER ACO 7342-53.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 47,476 hrs · 47,285 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 24 TO LBL 64. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FWD SERVICE DOOR) · airframe 47,476 hrs · 47,285 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR FRAME CRACKED AT STOP FITTING ABOVE AND BELOW DOOR CENTERLINE. REPAIRED DOOR PER TI-152-003.

Part: BRACKET — CRACKED (ESCAPE SLIDE) · airframe 47,476 hrs · 47,285 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE MOUNT BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 47,476 hrs · 47,285 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 987, LBL 43. REPAIRED FLOORBEAM PER TI-453-037.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,476 hrs · 47,285 cycles

DURING SCHEDULED 1/2D CHECK, FOUND .125 INCH CRACK AT BS 178 BULKHEAD WEB, WL 234, LBL 11. REPAIRED BULKHEAD PER SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 47,476 hrs · 47,285 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 11 - RBL 56. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (CABIN) · airframe 47,476 hrs · 47,285 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME CRACKED AT PREVIOUS REPAIR, BS 294.5, FLOOR LINE, FWD SVC DOOR. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,476 hrs · 47,285 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STR CLIP CRACKED AT BS 500A, STR 21R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,403 hrs · 47,225 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2.5 EXTERNAL FUSELAGE SKIN CRACKED AT BS 500C, WL 223, RT SIDE. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,403 hrs · 47,225 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2.75 EXTERNAL FUSELAGE SKIN CRACK AT BS 767, WL 191. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,101 hrs · 46,982 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR FRAME LOWER HINGE CUTOUT SKIN CRACK. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,089 hrs · 46,970 cycles

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

Part: GIRT BAR — OUT OF ADJ (PAX DOOR SLIDE) · airframe 47,089 hrs · 46,970 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT PLAY LENGTH OUT OF LIMITS. REPOSITIONED SLIDE PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 46,686 hrs · 46,616 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER WHEN F/A OPENED DOOR. REINSTALLED SLIDE ASSY PER MM.

Part: SLIDE — DEPLOYED (SERVICE DOOR) · airframe 46,465 hrs · 46,408 cycles

FWD SERVICE DOOR EVACUATION SLIDE DEPLOYED INADVERTENTLY, (STILL CONNECTED TO GIRT BAR FLOOR BRACKETS WHEN DOOR WAS OPENED). REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,220 hrs · 46,197 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 519, STRINGER 12L. REPAIRED SKIN PER SRM.

Part: GATE — OUT OF ADJ (PAX DOOR) · airframe 46,220 hrs · 46,197 cycles

AIR TURNBACK, FWD ENTRY DOOR HAS PRESS LEAK AROUND LOWER AREA. MX FERRY TO DAL AND ADJUSTED LOWER GATE ASSY PER MM.

Part: SKIN — CRACKED (CARGO DOOR)

DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR EXTERNAL SKIN CRACKED AROUND UPPER LT CORNER OF HANDLE CUT-OUT. REPAIRED SKIN PER RA NR 1-A52-020.

Part: LENS — MISSING (CABIN)

DURING SCHEDULED C2 CHECK, FOUND EEPLS LENS MISSING ON AFT END. INSTALLED LENS ASSY PER MM.

Part: SKIN — CRACKED (BS 435)

DURING SCHEDULED RON CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED, BS 435, STRINGER 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 940)

DURING SCHEDULED RON CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED, BS 940, STRINGER 21L. REPAIRED SKIN PER SRM.

Part: SLIDE — LOOSE (PAX DOOR)

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

Part: SKIN — CRACKED (FUSELAGE)

EXTERNAL FUSELAGE SKIN CRACKED APPROX 8 INCHES AFT OF LT WING ILLUMINATION LIGHT. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (BS 665)

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND MLG WHEEL WELL CEILING WEB CRACKED, BS 665, LBL 30.5-33.6. REPAIRED WEB PER ER NR 99-5820.

Part: PLACARD — TORN (OVERWING)

DURING SCHEDULED C2 CHECK, FOUND RT OVERWING EXTERIOR EMERGENCY PLACARD TORN. REPLACED PLACARD PER BOEING M/M.

Part: STOP — CRACKED (LT, RT EMER EXIT)

DURING SCHEDULED C2 CHECK, FOUND RT AND LT OVERWING EMERGENCY EXIT FWD STOP PADS CRACKED. REMOVED AND REPLACED STOP PADS PER BOEING M/M.

Part: WEB — CRACKED (BS 234)

DURING SCHEDULED C-CHECK, ROUTINE INSPECTION OF AIRCRAFT AFTER C-CHECK WASH, FOUND A 3.5 INCH LONG CRACK ON NOSE GEAR ACTUATOR SUPPORT FITTING FORWARD WEB. CRACK IS LOCATED AT BS 234.0 AND IS 7 INCHES AFT OF FORWARD BULKHEAD IN NOSE WHEEL WELL. REPAIRED NOSE GEAR ACTUATOR SUPPORT BRACKET PER SRM.

Part: BATTERY — DISCHARGED (ROW 19-23)

DURING SCHEDULED CHECK, FOUND FLOOR EGRESS LIGHTS BETWEEN ROWS 19 THRU 23 FAILED TO ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY, OPS CHK GOOD PER MM.

Part: LIGHT — DISCONNECTED (ROW 5)

DURING SCHEDULED SC CHECK, FOUND CABIN EMERGENCY EXIT LIGHT AT BULLNOSE AT ROW 5R INOP. REATTACHED LIGHT ASSEMBLY AND OP CHECKED PER BOEING MM.

Part: KEELBEAM — CORRODED (BS 727)

DURING SCHEDULED 1/4D CHECK, FOUND CORRODED KEEL BEAM CHORD AT BS 727 LBL 6. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 367)

DURING SCHEDULED 1/4D CHECK, FOUND CRACKED FUSELAGE SKIN FWD OF EQUIPMENT COOLING DUCT AT BS 367. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 367)

DURING SCHEDULED 1/4 D CHECK, FOUND CRACKED 2 1/4 FUSELAGE SKIN FWD OF EQUIPMENT COOLING DUCT AT BS 367. REPAIRED PER BOEING SRM.

Part: KEEL BEAM — CRACKED (BS 663)

DURING SCHEDULED 1/4 D CHECK, FOUND CRACKED KEELBEAM SKIN AT BS 663. REPAIRED PER BOEING SRM.

Part: WEB — CHAFED (PAX DOOR)

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR UPPER TORQUE TUBE BOLT IS CHAFFING WEB. REMOVED AND REPLACED PER BOEING SRM.

Part: PANEL — CRACKED (RT WING)

DURING SCHEDULED 1/4D CHECK, FOUND CRACKED PANEL UPPER WING SURFACE AT END OF ENG PYLON PANELS. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — LOOSE (BAGGAGE COMPT)

DURING SCHEDULED 1/4D CHECK, FOUND UPLATCH HOLDER FOR REAR B/BIN DOOR LOOSE WITH INTERCOSTAL MOVING. REMOVED AND REPLACED INTERCOSTAL PER BOEING SRM.

Part: LIGHT — LOOSE (CABIN)

DURING SCHEDULED 1/4D CHECK, FOUND EGRESS EMERGENCY LIGHT IN BULLNOSE AT 5 DEF COMING LOOSE AND IMPROPERLY INSTALLED. REINSTALLED LIGHT AND LENS AS PER BOEING MM.

Part: FLOORBEAM — CRACKED (BS 747/757-870)

DURING SCHEDULED 1/4D CHECK, FOUND CRACKED FLOORBEAM UNDER CARGO NET TIEDOWN LUG AT BS 747, RBL 14; AND BS 757 TO 870, RBL 14. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 847)

DURING SCHEDULED 1/4D CHECK, FOUND CRACKED AT BS 847 STRINGER 24R-25R BELTFRAME WEB AFT OF CARGO DOOR. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — BULGING (BS 797)

DURING SCHEDULED 1/4D CHECK, FOUND SKIN BULGING AND WRINKLED LAP SPLICE FUSELAGE AT BS 797, LT SIDE OF FUSELAGE. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 727)

DURING SCHEDULED 1/4D CHECK, FOUND CRACKED STRINGER CLIP AT BS 727C, STR 21L. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (RT MLG WW)

DURING SCHEDULED 1/4D CHECK, FOUND CRACKED FRAME FWD SIDE OF W/W OPENING LBL60. REMOVED AND REPLACED PER BOEING SRM.

Part: OIL PRESS IND — LOST (NR 1 ENGINE)

DIVERTED TO STL, DUE TO NUMBER 1 ENGINE LOSS OF OIL PRESSURE INDICATION. LANDED WITHOUT INCIDENT. INSPECTED ENGINE, OIL FILTERS, NO DEFECTS NOTED. REMOVED AND REPLACED LUBE UNIT, SERVICED OIL, AND PERFORMED ENGINE RUN PER BOEING M/M.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED BC1 CHECK, FOUND AFT SERVICE DOOR UPPER HINGE CUTOUT CRACKED .25 ON OUTER SKIN. REPAIRED PER SWA RA 1-353-1735.

Part: PCU — FAILED (RUDDER)

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

Part: AIR DISTR — ODOR (CABIN)

IN-FLIGHT, EXPERIENCED A STRONG SMELL OF HYDRAULIC FLUID IN CABIN AND COCKPIT DURING TAKEOFF AND AGAIN WHEN LOWERING FLAPS COMING INTO LAX. INSPECTED A/C BAYS, PERFORMED ENGINE RUN WITH BLEEDS ON PER BOEING M/M, NO DEFECTS NOTED.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED SERVICE CHECK, FOUND A 3 INCH FUSELGE SKIN CRACK FORWARD OF WATER SERV PANEL. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND 3 CRACKS ON BS 178 BULKHEAD ADJACENT TO 2 FASTENERS AT WL 234 RBL 10. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 987)

DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 987, S20R. REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORTS CORRODED AT BS 957.5 WL 208 RBL 49, BS 1006 TO 1016 WL 208 LBL 6 TO 8 AND AT BS 540 LBL 2 WL 208. REPLACED PER BOEING SRM.

Part: CHORD — CRACKED (BS 1138/1156)

DURING SCHEDULED D-CHECK, FOUND CRACKED LOWER CHORDS AT S5L AND S5R, BS 1138 AND AT BS 1156, LBL 23 AND RBL 23. REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 328/986)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAMS CORRODED AT BS 986 LBL 30 TO RBL 51, BS 328 RBL 14 AND 15 WL 208 AND BS 986 WL 208 RBL 5, 24, 32, 43 AND LBL 43. REPAIRED PER BOEING SRM.

Part: CLIPS — CRACKED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 787 S11L, BS 947 S25R AND S21L AND AT BS 663 S10R AND S10L. REPLACED PER BOEING SRM.

Part: DOOR FRAME — CRACKED (BS 296)

DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR FRAME CRACKED AT BS 296 RBL 40 WL 274. REPAIRED PER BOEING SRM.

Part: DOOR FRAME — CRACKED (FWD CARGO)

DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT BS 492 RBL 37 WL 161. REPAIRED PER BOEING SRM.

Part: SPLICE — CRACKED (BS 907)

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

Part: SHEAR TIE — CRACKED (BS 1121)

DURING SCHEDULED D-CHECK, FOUND SHEAR TIES CRACKED AT BS 1121 BETWEEN S12 AND 13L AND AT BS 360, S13L AND S15L. REPLACED PER BOEING SRM.

Part: CHORD — CRACKED (BS 663)

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CRACKED AT BS 663 RBL 65 WL 208. REPLACED CREASE BEAM CHORD PER BOEING SRM.

Part: WEB — CRACKED (BS 526)

DURING SCHEDULED D-CHECK, FOUND WEB CRACKED IN RADIUS AT BS 526 LBL 44 WL 160. REPAIRED PER BOEING SRM.

Part: BRACKET — CRACKED (BS 887)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME HAT SECTION ATTACH BRACKET AT BS 887 S9R, BS 847 S9R, BS 827 S9R, BS 787 S9R, BS 787 S9R, BS 767 S9R. REPAIRED PER BOEING SRM.

Part: BLKHD ANGLE — DAMAGED (BS 727)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE BULKHEAD SUPPORT ANGLE CRUSHED AND DENTED AT BS 727, BBL 0. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD AT BS 178 CRACKED 2 PLACES WL 210 TO 213, RBL 5.7. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 327)

DURING SCHEDULED D-CHECK, FOUND FORWARD GALLEY DOORWAY LOWER AFT CORNER SKIN CRACKED 1 INCH AT BS 327 WL 206 RBL 65. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD AT BS 178 CRACKED 2 PLACES WL 219, LBL 5 TO 12. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 727)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE BULKHEAD CRACKED AT BS 727 BBL 0. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 986 WL 208 RBL 5, 24, 32 AND 43. REPAIRED PER BOEING SRM.

Part: SPLICE — CRACKED (BS 360/907)

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AND SHEAR TIE AT S15 CRACKED AT BS 360 AND BS 907 S4R. REPLACED PER BOEING SRM.

Part: SKIN — GOUGED (BS 258/875-883)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 875 TO 883, BETWEEN S1 AND 2L, BETWEEN S1 AND 2R, AT BS 258, S21L. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD CRACKED 2 PLACES AT BS 178, LBL 5 TO 12 AT WL 201 TO 205, LBL 5.7. REPAIRED PER BOEING SRM.

Part: CHORD — CRACKED (BS 1156)

DURING SCHEDULED D-CHECK, FOUND O/B CHORD CRACKED AT BS 1156 RBL 23 S4R. REPLACED PER BOEING SRM.

Part: STIFFENER — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 178 LBL 5 WL 184. REPAIRED PER BOEING SRM.

Part: BLKHD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178 BBL 0 WL 185. REPAIRED PER BOEING SRM.

Part: DOOR FRAME — CRACKED (BS 492)

DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT BS 492 RBL 37 WL 161. REPAIRED PER TRAMCO EWO 95-0789.

Part: SKIN — DENTED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1019, BS 340 BETWEEN S17 AND 18L, BS 256 BETWEEN S22 TO 23R AND AT BS 310, S21R. REPAIRED PER BOEING SRM.

Part: CLIP — CRACKED (BS 787)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 787, S1L. REPLACED PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 1121)

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 1121, BETWEEN S12 AND 13L. REPLACED PER BOEING SRM.

Part: PUMP — OVERHEATED (W/W)

DURING CLIMBOUT, EXPERIENCED A-SYSTEM HYDRAULIC PUMP OVERHEAT LIGHT ILLUMINATED. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. REPLACED PUMP, FILTERS AND FLUSHED SYSTEM PER BOEING M/M.

Part: SKIN — CRACKED (BS 812)

DURING SCHEDULED SERVICE CHECK, FOUND 2 INCH FUSELAGE SKIN CRACK AT BS 812, AT STRINGER 23R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CRACKED (AFT OF CARGO DR)

DURING SCHEDULED SERVICE CHECK, FOUND 4 INCH FUSELAGE SKIN CRACK 24 INCHES AFT OF AFT CARGO DOOR. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.