N337SW

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 75,580 hrs · 66,967 cycles

DURING SCHEDULED OTS CHECK FOUND, R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,148 hrs · 66,627 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 500D, STR 11R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,148 hrs · 66,627 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 460, STR 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,963 hrs · 66,485 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 767+5, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,963 hrs · 66,485 cycles

DURING SCHEDULE SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 500A+13.5, TO BS 500A+15, STR 19L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,963 hrs · 66,485 cycles

DURING SCHEDULE SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 500+4.75, TO BS 500+5.25, STR 19L. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 74,963 hrs · 66,485 cycles

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

Part: SIGN — INOPERATIVE (CABIN) · airframe 74,963 hrs · 66,485 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED SIGN IAW MM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 74,963 hrs · 66,485 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR LOWER EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED SIGN IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,541 hrs · 66,162 cycles

DURING HC1 CHECK FOUND SKIN CRACKED AT BS 908+2, STR 19L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 74,541 hrs · 66,162 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 74,541 hrs · 66,162 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 72. REPAIRED SKIN PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 73,472 hrs · 65,335 cycles

LT OVERWING EMERGENCY EXIT SIGN LOWER FWD LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,850 hrs · 64,864 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 505D TO BS 510D, STR 13R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,605 hrs · 64,684 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 510, STR 18R. REPAIRED SKIN PER EA.

Part: LIGHT — BROKEN (COCKPIT) · airframe 72,326 hrs · 64,449 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT NOT ARMED KORRY LIGHT BROKEN. REMOVED AND REPLACED KORRY LIGHT PER MM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22YY CHECK, FOUND BULKHEAD LOWER CHORD CORROSION AT BS 227.8, BL 0. REPAIRED CHORD PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 294.5, LBL 54. REPAIRED CHORD PER AEM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CHORD CRACKED AT BS 727B, LBL 45.5. REPAIRED CHORD PER EA.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO DOOR FRAME CRACKED IN LOWER AREA. REMOVED AND REPLACED DOOR PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 707.5, LBL 24.5. REPAIRED WEB PER AEM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 711.5, LBL 24.5. REPAIRED WEB PER AEM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 706.5, LBL 24.5. REPAIRED WEB PER AEM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 807, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 957, STR 7L. REPAIRED FRAME PER AEM.

Part: CABLE — BROKEN (EVAC SLIDE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE BROKEN. REMOVED AND REPLACED CABLE PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17.0. REPAIRED WEB PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 SLAT I/B EDGE DELAMINATED. REPAIRED SLAT PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 767, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING NR 1 SLAT CRACKED. REMOVED AND REPLACED SLAT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 6 SLAT SKIN CRACKED BETWEEN STA 166 TO STR 170. REPAIRED SKIN PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 328, STR 4R. REPAIRED STRINGER PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 356, STR 27R. REMOVED AND REPLACED ANGLE PER EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM WEB CRACKED BETWEEN BS 698 TO BS 717. REPAIRED BEAM PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, BETWEEN RBL 5.7 TO RBL 17. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND WEB CRACKED AT BS 178, LBL 17.0. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, BL 0. REPAIRED WEB PER SRM.

Part: FRAME — PUNCTURED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT FRAME PUNCTURED AT BS 500A, BETWEEN STR 14R TO STR 14L. REPAIRED FRAME PER EA.

Part: COVER — DEFECTIVE (CABIN) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT EMERGENCY EXIT LIGHT COVER INOP AT ROW 4. REMOVED AND REPLACED COVER PER MM.

Part: COVER — DEFECTIVE (CABIN) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT EMERGENCY EXIT LIGHT COVER INOP AT ROW 14. REMOVED AND REPLACED COVER PER MM.

Part: COVER — DEFECTIVE (CABIN) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT EMERGENCY EXIT LIGHT COVER INOP AT ROW 2. REMOVED AND REPLACED COVER PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 SLAT O/B EDGE DELAMINATED. REPAIRED SLAT PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 380. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 6 SLAT SKIN O/B EDGE DELAMINATED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 5R. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10L. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 5R. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4L. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 8L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 10R. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5R. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 10R. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4L. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 1006, STR 2R. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 72,178 hrs · 64,327 cycles

DURING SCHEDULED 22Y CHECK, FOUND WEB CRACKED BETWEEN BS 312 TO BS 328, RBL 33. REMOVED AND REPLACED WEB PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,151 hrs · 64,302 cycles

DURING SCHEDULED CV CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP AT ROW 12. RELAMPED LIGHT PER MM.

Part: COVER — MISSING (CABIN) · airframe 72,139 hrs · 64,293 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT LIGHT COVER MISSING AT ROW 2. REMOVED AND REPLACED COVER PER MM.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 72,151 hrs · 64,302 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,740 hrs · 63,981 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 402.5, BETWEEN STR 5L TO STR 15L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,202 hrs · 63,570 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 739E TO BS 727E + 14.4, STR 18R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,202 hrs · 63,570 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,206 hrs · 63,573 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 908 TO BS 1016, BETWEEN STR 20L TO STR 25L. REMOVED AND REPLACED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,206 hrs · 63,573 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 908 TO BS 1016, BETWEEN STR 20R TO STR 25R. REMOVED AND REPLACED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,202 hrs · 63,570 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 732.2 TO BS 734.5C, STR 14R. REPAIRED SKIN PER ER.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 71,030 hrs · 63,453 cycles

AFT I/B EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,477 hrs · 63,052 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 490, STR 17R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,477 hrs · 63,052 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 480, STR 17R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (BS 480 S16R) · airframe 70,477 hrs · 63,052 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 480, STR 16R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (BS 425 S16R) · airframe 70,477 hrs · 63,052 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 425, STR 16R. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CRACKED (BS 440 S15-16R) · airframe 70,477 hrs · 63,052 cycles

DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CRACKED BETWEEN BS 440, BETWEEN STR 15R TO STR 16R. REMOVED AND REPLACED SHEAR TIE PER EA.

Part: SKIN — CRACKED (BS 490 S16R) · airframe 70,477 hrs · 63,052 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 490, STR 16R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,748 hrs · 62,487 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 515B, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,748 hrs · 62,487 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 475, STR 19L. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 69,748 hrs · 62,487 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,748 hrs · 62,487 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 934, STR 22R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,748 hrs · 62,487 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 485, STR 17L. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 69,747 hrs · 62,487 cycles

DURING SCHEDULED HC2 CHECK, FOUND NOSE WHEEL WELL CEILING PANEL PRESSURE DECK WEB CRACKED AT BS 277, RBL 10.16. REPAIRED WEB PER SWA EA.

Part: ENGINE — OVERHEATED (NR 1) · airframe 69,679 hrs · 62,434 cycles

ABORTED TAKEOFF / DECLARED EMERGENCY. ON TAKEOFF NR 1 ENG OFF EGT WAS CLIMBING THRU, 800 REDUCED POWER TO MAINTAIN LIMITS AND RETURNED TO AIRPORT. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,589 hrs · 62,372 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 372, STR 15R. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,588 hrs · 62,372 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,588 hrs · 62,372 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,037 hrs · 61,943 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 799, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,037 hrs · 61,943 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 799, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,037 hrs · 61,943 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 810, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,933 hrs · 61,145 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 490, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,933 hrs · 61,145 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,933 hrs · 61,145 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737D, STR 19R. REPAIRED SKIN PER SRM.

Part: SHIELD — BROKEN (FLASHLIGHT) · airframe 67,933 hrs · 61,145 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD EMERGENCY FLASHLIGHT SHIELD BROKEN. REPLACED SHIELD PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,933 hrs · 61,145 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 470, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,933 hrs · 61,145 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 485, STR 16R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,558 hrs · 60,890 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,558 hrs · 60,890 cycles

RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,373 hrs · 60,754 cycles

DURING SCHEDULED MV4 CHECK, FOUND R2 DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 66,565 hrs · 60,138 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 13 DEF. INSTALLED LENS PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT COVER CRACKED. REMOVED AND REPLACED LIGHT COVER ASSY PER MM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR LOWER AFT CORNER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 435 S16R) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 435, STR 16R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 11R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (BS 639 S7L) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 639, STR 7L. R&R SHEAR TIE PER SRM.

Part: SKIN — BUCKLED (BS 980 S23L) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN BUCKLED AT BS 980, STR 23L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (BS 303 S16L) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 303.9, STR 16L. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (BS 559 S8L) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 787 S9L) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 510-517D) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 510 AND BS 517D, STR 16R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (BS 663 S2L-3R) · airframe 66,463 hrs · 60,065 cycles

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

Part: SHEAR TIE — CRACKED (BS 520 S22L) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 22L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 787 S8L) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 597 S8L) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500A S8L) · airframe 66,463 hrs · 60,065 cycles

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

Part: STRINGER CLIP — CRACKED (BS 747 S9L) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 907 S8L) · airframe 66,463 hrs · 60,065 cycles

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

Part: FRAME — CRACKED (BS 480 S8L) · airframe 66,463 hrs · 60,065 cycles

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

Part: SKIN — CRACKED (BS 500C S16R) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 16R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (BS 520 S8L) · airframe 66,463 hrs · 60,065 cycles

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

Part: FRAME — CRACKED (BS 727B S8L) · airframe 66,463 hrs · 60,065 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 435, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 433, RBL 3. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 15R. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BETWEEN BS 669 AND BS 665, LBL 24.75. REPAIRED FLOORBEAM PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 344, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, LBL 2.5. REPAIRED SKIN PER SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 15L CRACKED AT BS 360. REPAIRED STRINGER PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT KEEL BEAM WEB CORRODED AT BS 540, LBL 6.5. REPAIRED WEB PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT KEEL BEAM WEB CORRODED AT BS 540, RBL 6.5. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELLY SKIN TEAR STRAP CRACKED AT BS 379, LBL 4. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 380, LBL 2.5. REPAIRED SKIN PER SWA EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND CENTER CABIN LONGITUDINAL BEAM CRACKED AT BS 665, RBL 24.75. REPAIRED BEAM PER SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE STRINGER 13L CRACKED AT BS 301. REPAIRED STRINGER PER SRM & BAC DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 18L CRACKED AT BS 787. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749.5, STR 18R. REPAIRED SKIN PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 907 TO BS 927, LBL 65. REPAIRED WEB PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 414, LBL 1.5. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, LBL 2.5 TO LBL 3.5. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 433, RBL 3. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,463 hrs · 60,065 cycles

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

Part: SIGN — LOOSE (CABIN) · airframe 65,865 hrs · 59,641 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 65,578 hrs · 59,454 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,578 hrs · 59,454 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 520 S13L) · airframe 64,641 hrs · 58,768 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 13L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 380 S15L) · airframe 64,641 hrs · 58,768 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,641 hrs · 58,768 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,641 hrs · 58,768 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 390 S16R) · airframe 64,583 hrs · 58,722 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 390, STR 16R. REPAIRED SKIN PER SRM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 64,583 hrs · 58,722 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CABIN EMERGENCY EXIT SIGN COVER CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — CRACKED (BS 474 S16R) · airframe 64,088 hrs · 58,336 cycles

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

Part: SKIN — CRACKED (BS 760 S18L) · airframe 64,088 hrs · 58,336 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 739D S19R) · airframe 63,263 hrs · 57,706 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739D, STR 19R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,145 hrs · 57,609 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,145 hrs · 57,609 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLAT — CRACKED (RT WING) · airframe 62,781 hrs · 57,318 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,596 hrs · 57,181 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS DIM WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED BATTERY PACKS AND BATTERY CHARGER PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,596 hrs · 57,181 cycles

DURING SCHEDULED SPV CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS DIM WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED BATTERY PACKS AND BATTERY CHARGER PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,596 hrs · 57,181 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS DIM WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED BATTERY PACKS AND BATTERY CHARGER PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,596 hrs · 57,181 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 61,969 hrs · 56,703 cycles

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

Part: SLAT — CRACKED (RT WING) · airframe 61,969 hrs · 56,703 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT OUTBOARD T/E. REPAIRED NR 6 L/E SLAT PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,982 hrs · 55,948 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 870, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 60,658 hrs · 55,693 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,124 hrs · 55,260 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,124 hrs · 55,260 cycles

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

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 60,053 hrs · 55,204 cycles

R1 DOOR EMERGENCY EVAC SLIDE INDICATED LOW PRESSURE. REMOVED AND REPLACED SLIDE PER MM.

Part: CABLE — MISROUTED (R2 DOOR SLIDE) · airframe 60,020 hrs · 55,177 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED EVAC SLIDE CABLE PER MM.

Part: SKIN — CRACKED (BS 510D) · airframe 60,020 hrs · 55,177 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510D, STR 13R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 510D) · airframe 60,020 hrs · 55,177 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510D, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 510D) · airframe 60,020 hrs · 55,177 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510D, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 517D) · airframe 60,020 hrs · 55,177 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 517D, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 500) · airframe 60,020 hrs · 55,177 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 770) · airframe 59,075 hrs · 54,420 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 770, STR 14L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 500C) · airframe 59,075 hrs · 54,420 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 777) · airframe 58,653 hrs · 54,087 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 777, STR 18L. REPAIRED SKIN PER SRM.

Part: MECHANISM — BINDING (LT AILERON) · airframe 58,510 hrs · 53,981 cycles

AILERONS BINDING. FOUND LT AILERON TOWERSHAFT BINDING. REMOVED AND REPLACED LT AILERON TOWERSHAFT FEEL & CENTERING MECHANISM PER MM.

Part: SKIN — CRACKED (BS 503C) · airframe 58,086 hrs · 53,640 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503C, STR 14R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FWD CARGO) · airframe 58,086 hrs · 53,640 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME LOWER STOP FITTING. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (LT WING) · airframe 58,086 hrs · 53,640 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT WING UPPER SKIN CRACKED AT WBL 157.00, REAR SPAR UPPER CHORD. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,086 hrs · 53,640 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SRM.

Part: BULB — INOPERATIVE (CABIN) · airframe 58,086 hrs · 53,640 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 58,086 hrs · 53,640 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: BULB — INOPERATIVE (CABIN) · airframe 58,086 hrs · 53,640 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: FRAME — CRACKED (FWD CARGO) · airframe 58,086 hrs · 53,640 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME LOWER STOP FITTING. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500B) · airframe 58,086 hrs · 53,640 cycles

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

Part: STRINGER — CRACKED (BS 300) · airframe 58,086 hrs · 53,640 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 300, STR 3L. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 312) · airframe 58,086 hrs · 53,640 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 312, STR 3L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 500C) · airframe 58,086 hrs · 53,640 cycles

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

Part: FRAME — CRACKED (BS 500B) · airframe 58,086 hrs · 53,640 cycles

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

Part: WEB — CRACKED (BS 665) · airframe 58,086 hrs · 53,640 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 665, LBL 30 TO LBL 35. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CORRODED (BS 727E) · airframe 58,086 hrs · 53,640 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727E, LBL 7 AND LBL 13. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (BS 953) · airframe 57,822 hrs · 53,432 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 953, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 927) · airframe 57,822 hrs · 53,432 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 24R. REPAIRED SKIN PER SWA EA & SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 57,621 hrs · 53,282 cycles

EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 17 ABC. SECURED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 57,381 hrs · 53,082 cycles

BULLNOSE EMERGENCY EXIT LIGHT ASSY LOOSE AT ROW 17 ABC. SECURED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,824 hrs · 52,661 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 446, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,317 hrs · 52,262 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 976, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,317 hrs · 52,262 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 920, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,317 hrs · 52,262 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 14R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,362 hrs · 51,531 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM.

Part: PANEL — DELAMINATED (RT WING FLAP) · airframe 55,362 hrs · 51,531 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD MIDFLAP WEDGE PANEL DELAMINATED. REPAIRED MIDFLAP WEDGE PANEL PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 & R2 DOORS) · airframe 54,528 hrs · 50,896 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L1 AND R2 DOOR EVAC SLIDES PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,528 hrs · 50,896 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SERVICE DOOR, LT OVERWING EXIT, AFT ENTRY DOOR, SIDE MOUNTED EMERGENCY EXIT LIGHTS INOP. RELAMPED LIGHTS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 53,298 hrs · 49,917 cycles

DURING SCHEDULED RON, FOUND RT AFT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,286 hrs · 49,908 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 520, STRINGER 15L, CRACKED. REPAIRED SKIN PER SRM AND EA.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 52,641 hrs · 49,415 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT LOWER FLASHLIGHT IND LIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 52,114 hrs · 48,995 cycles

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

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 51,316 hrs · 48,371 cycles

R1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: SLIDE — LOOSE (ENTRY DOOR) · airframe 50,556 hrs · 47,741 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: FITTING — CORRODED (LT AND RT MLG) · airframe 50,434 hrs · 47,647 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT AND RT MLG WALKING BEAM FITTINGS CORRODED. REMOVED AND REPLACED BOTH LT AND RT MLG WALKING BEAM FITTINGS PER SWA SI AND MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,312 hrs · 47,550 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT CREASE BEAM CORRODED AT BS 1011. REPAIRED CREASE BEAM PER SRM.

Part: SKIN — CRACKED (NR 6 L/E SLAT) · airframe 50,312 hrs · 47,550 cycles

DURING SCHEDULED 1/2D CHECK, FOUND NR 6 L/E SLAT CRACKED IN LOWER SKIN OUTBD EDGE. REMOVED AND REPLACED NR 6 L/E SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,312 hrs · 47,550 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 971, JUST BELOW STR 21L. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,312 hrs · 47,550 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 44. REPAIRED FLOORBEAM PER T1-453-037.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,312 hrs · 47,550 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 812, STR 17L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,312 hrs · 47,550 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BRACKET — CORRODED (ESCAPE SLIDE) · airframe 50,312 hrs · 47,588 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINING BRACKETS CORRODED. REMOVED AND REPLACED GIRT BAR RETAINING BRACKETS PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 50,252 hrs · 47,502 cycles

DURING SCHEDULED RON, FOUND OVERHEAD BIN BULL MOSE EMERGENCY EXIT LIGHT SOCKET DAMAGED AT ROW 18 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 49,745 hrs · 47,116 cycles

DURING SCHEDULED C4 CHECK, SWA SI 11139-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 ELEVATOR TAB HINGE FITTING PER MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 49,520 hrs · 46,918 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW FRAMES CRACKED AT RT WINDOWS NR 12 & 30. REMOVED AND REPLACED WINDOW FRAMES PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,520 hrs · 46,918 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BELOW STR 14R. REPAIRED SHEAR TIE PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 49,520 hrs · 46,918 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICES CRACKED (4 EA) AT BS 360, STR 4R, BS 360, STR 14R, BS 540, STR 14R & BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICES PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 49,520 hrs · 46,918 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 727, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: LINK — CORRODED (RT MLG) · airframe 49,323 hrs · 46,763 cycles

DURING SCHEDULED RON, FOUND RT MLG FWD TRUNNION LINK TRUNNION LUGS CORRODED. REMOVED AND REPLACED RT MLG TRUNNION LINK, BEARING AND BEARING BOLT PER MM.

Part: STRUT — CORRODED (RT MLG) · airframe 49,323 hrs · 46,763 cycles

DURING SCHEDULED RON, FOUND RT MLG UPPER STRUT CYLINDER CORRODED. REMOVED AND REPLACED RT MLG UPPER STRUT CYLINDER PER MM.

Part: TRUNNION PIN — CORRODED (LT & RT MLG) · airframe 49,323 hrs · 46,763 cycles

DURING SCHEDULED RON, FOUND BOTH LT AND RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED LT AND RT MLG TRUNNION PINS PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 48,756 hrs · 46,327 cycles

RT OVERWING EXIT SIGN LOOSE. SECURED EXIT SIGN PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 48,732 hrs · 46,306 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 48,125 hrs · 45,832 cycles

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

Part: CABLE — MISROUTED (AFT SVC DOOR) · airframe 47,815 hrs · 45,569 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,815 hrs · 45,569 cycles

DURING SCHEDULED C2 CHECK, FOUND BS 1016 AFT PRESS BULKHEAD CRACKED (2 EA) AT 6 0' CLOCK AND 9 0' CLOCK POSITION. REPAIRED BULKHEAD PER SWA EA.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 47,742 hrs · 45,505 cycles

DURING SCHEDULED RON, FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,659 hrs · 45,440 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 26R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,659 hrs · 45,440 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 26R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 47,429 hrs · 45,250 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER WHILE OPENING DOOR. REINSTALLED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,142 hrs · 45,003 cycles

DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT LIGHTS INOP AT ROW'S 3 ABC AND 20 DEF. RELAMPED EXIT LIGHTS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 46,108 hrs · 44,148 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,106 hrs · 44,148 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 935, STR 25R. REPAIRED SKIN PER SRM.

Part: GATE — CRACKED (SERVICE DOOR) · airframe 46,106 hrs · 44,148 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR LOWER GATE CRACKED .500 INCH AT AFT EDGE. REPAIRED LOWER GATE ASSY PER SWA RA.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 43,409 hrs · 41,896 cycles

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

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 43,244 hrs · 41,750 cycles

DURING SCHEDULED BC1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED EMERGENCY EVAC SLIDE PER MM.

Part: SPAR — CRACKED (HORIZ STAB) · airframe 43,244 hrs · 41,750 cycles

DURING SCHEDULED C1 CHECK, FOUND RT HORIZ STABILIZER AFT SPAR LWR SURFACE CRACKED, APPROX 60 INCHES OTBD OF ROOT. REPAIRED SPAR PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,062 hrs · 41,589 cycles

FUSELAGE SKIN CRACKED AT BS 967, STR 21L AND BS 927, STR 23L. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 42,438 hrs · 41,048 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT INBD T/E AFT FLAP DELAMINATED AT OUTBD T/E. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: FRAME — CRACKED (R1 DOOR) · airframe 42,438 hrs · 41,048 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED AT AFT LOWER CORNER. REPAIRED FRAME PER BAC DRAWING.

Part: SLAT — CRACKED (RT WING) · airframe 42,438 hrs · 41,048 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 5 L/E SLAT CRACKED AT LOWER SKIN, 7 INBD OF ACTUATOR. REPAIRED SLAT PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 42,438 hrs · 41,048 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS LOOSE AT ROWS 18 ABC & 21 ABC. SECURED LIGHTS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 42,438 hrs · 41,048 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 2 DEF. SECURED LIGHT ASSY PER MM.

Part: RETAINER — CORRODED (SERVICE DOOR) · airframe 42,438 hrs · 41,048 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER CORRODED. REMOVED AND REPLACED GIRT RETAINER PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 42,438 hrs · 41,048 cycles

DURING SCHEDULED 1/4D CHECK, FOUND TRANSVERSE BEAM WEB CRACKED AT BS 663, BL 0. REPAIRED BEAM WEB PER SWA RA & SB.

Part: FLAP — DELAMINATED (RT WING) · airframe 42,488 hrs · 41,048 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RIGHT T/E OUTBOARD AFT FLAP INBOARD EDGE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SLAT — CRACKED (LT WING) · airframe 42,438 hrs · 41,048 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 2 L/E SLAT T/E SKIN CRACKED AT RIVETS HEADS, 3 INBD OF T-DUCT. REPAIRED SLAT PER SRM.

Part: DOOR FRAME — CRACKED (ENTRY DOOR) · airframe 42,438 hrs · 41,048 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FRAME UPPER HINGE CUTOUT CRACKED AT FWD CORNER. REPAIRED FRAME PER SWA RA.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 41,571 hrs · 40,378 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: LIGHT — LOOSE (FUSELAGE) · airframe 40,699 hrs · 39,593 cycles

DURING SCHEDULED C2 CHECK, FOUND RT AFT FUSELAGE EMERGENCY LIGHT ASSY LOOSE. SECURED LIGHT ASSY PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 40,201 hrs · 39,136 cycles

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

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 40,163 hrs · 39,108 cycles

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

Part: SLIDE — DISCHARGED (SERVICE DOOR) · airframe 39,581 hrs · 38,589 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (BS 945)

DURING SCHEDULED C4 CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED, BS 945, STRINGER 23L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOP (LT EMER EXIT)

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

Part: EGT IND — MALFUNCTIONED (NR 1 ENGINE)

ABORTED TAKEOFF, NR 1 ENG EGT OVERTEMP LIGHT ILLUMINATED AT 95 KNOTS, REDUCED ENG THRUST AND LIGHT WENT OUT. INSPECTED NR 1 ENG PER MM 72-00-00-6. PERFORMED ENG RUN TO TAKEOFF LIMITS AND OPS CHECK GOOD. LATER AT PHX ADJUSTED VSV'S DUE TO NR 1 ENG SLOW TO START .

Part: SLIDE — DEPLOYED (SERVICE DOOR)

DURING SCHEDULED A1 CHECK, FWD SERVICE DOOR EVACUATION SLIDE ACCIDENTALLY DEPLOYED. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SLIDE — DETACHED (PASSENGER DOOR)

AFT ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. RESTOWED SLIDE ASSY PER MM.

Part: LENS — MISSING (LT PAX DOOR)

PLASTIC COVER LENS MISSING FOR LH AFT ESCAPE SLIDE ASSY. REMOVED AND REPLACED PLASTIC LENS PER MM.

Part: BULB — FAILED (RT SERVICE DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND RH AFT SERVICE DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LAMP ASSY PER MM.

Part: LIGHT — INOPERATIVE (ROW 23)

DURING SCHEDULED C3 CHECK, FOUND FLOOR PROX LIGHT BULB INOPERATIVE AT SEAT ROW 23 DEF. REMOVED AND REPLACED FLOOR PROX LAMP AT SEAT ROW ROW 23 DEF PER BOEING MM.

Part: SKIN — DENTED (BS 343)

DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 343 BETWEEN STR 19 AND 20R. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACK INDICATIONS OF BS 178 BULKHEAD, UNDER STRAP AT RBL 4.7, WL 197.5 TO 198.5. REPAIRED PER BOEING SRM.

Part: FLOOR — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACKED FLOOR WEB AT BS 178, LBL 25-29 WL 207. REPAIRED PER BOEING SRM.

Part: BULKHEAD ANGLE — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND ANGLE TO BS 178 BULKHEAD CRACKED, LBL 26-29 AT STR 17 LT AND RBL 26-29, AT STR 17 RT. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 1015)

DURING SCHEDULED D-CHECK, FOUND CORRODED SUPPORT AT BS 1015, LBL 39, WL 207. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 315.5 & 324)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 315.5 AND 324, RBL 10, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 400 & 500)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 8 AND 9 RT AT BS 500A AND BS 400. REMOVED AND REPLACED PER BOEING SRM.

Part: STRAP — CRACKED (BS 326)

DURING SCHEDULED D-CHECK, FOUND STABILIZER STRAP CRACKED AT BS 326, RBL 32, WL 200. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 181)

DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 181, LBL 6, WL 187. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACKED BS 178 BULKHEAD AT WL 200, LBL 5, FWD SIDE. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 340)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 340, RBL 11, WL 208. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM UPPER CHORD AT BS 986.5, RBL 5, 22, 23, 26, 43.5, LBL 4.5, 14, 43.5, WL 208 AND WL 207. REPAIRED PER BOEING SRM.

Part: SHEAR WEB — CRACKED (BS 386)

DURING SCHEDULED D-CHECK, FOUND CRACKED SHEAR WEB AT BS 386, BL 0, WL 207. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 182)

DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 182, RBL 17, WL 181. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACK INDICATIONS OF BS 178 BULKHEAD, UNDER STRAP AT LBL 6.7, WL 212-213. REPAIRED PER BOEING SRM.

Part: FLOOR — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACKED FLOOR WEB AT BS 178, RBL 25-29 WL 207. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 827)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT RACK ATTACH BRACKET BETWEEN STRINGER 8 AND 9 RIGHT AT BS 827. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM AT BS 312, LBL 39, 33, 20, 14 RBL 8, WL 208 AND WL 207. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACK INDICATIONS OF BS 178 BULKHEAD, UNDER STRAP AT RBL 4.7, WL 200.5 TO 201.5. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 305.5)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 305.5 AND RBL 10, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 500)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 8 AND 9 LT AT BS 500C. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 867)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 8 AND 9 LT, BS 867; STR 8 & 9 LT, BS 827 & STR 8 AND 9 LT, BS 787. REMOVED AND REPLACED PER BOEING SRM.

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACKED SIDE CHORD AT BS 178, RBL 29, WL 207 AND BS 178, LBL 29 WL 207. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 349)

DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT BS 349, WL 217, LBL 64. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 747)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 8 AND 9 LT, BS 747. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — DENTED (BS 787)

DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 787, RBL 24-25, WL 158. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — DAMAGED (CARGO DOORWAY)

DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CLOSEOUT PANEL DAMAGED AT BS 794, RBL 25. REMOVED AND REPLACED PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 360)

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED BELOW STRINGER AT BS 360, STR 13 LT. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727-947)

DURING SCHEDULED D-CHECK, FOUND CARGO FLOORBEAM CORRODED AROUND NUT PLATE AT BS 727-947, LBL 12.5, WL 159; BS 727-947, LBL 8, WL 159; BS 727-947, LBL 3, WL 159 AND BS 727-947, RBL 8, WL 159. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DENTED (LT HORIZ STAB)

DURING SCHEDULED D-CHECK, FOUND LEFT HORIZ STAB L/E DENTED BETWEEN STABILIZER AT BS 0 AND STABILIZER AT BS 57.93. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727-947)

DURING SCHEDULED D-CHECK, FOUND CARGO FLOORBEAM CORRODED AROUND NUT PLATE AT BS 727-947, RBL 3, WL 159. REMOVED AND REPLACED PER BOEING SRM.

Part: FASTENERS — OVERSIZE (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE ABOVE STRINGER 23 RT HAS OVERSIZED FASTENER HOLES AT BS 727D AND BS 727D-727D+10. PERFORMED MODIFICATION PER BOEING SRM.

Part: FRAME — DENTED (BS 827)

DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 827, LBL 46, WL 173. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD — CORRODED (BS 947)

DURING SCHEDULED D-CHECK, FOUND FLOOR TO BULKHEAD SUPPORT ANGLE CORRODED AT BS 947, LBL 21, RBL 21, WL 180. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CHAFED (BS 1126.56)

DURING SCHEDULED D-CHECK, FOUND LEFT SKATE ANGLE CHAFED AT BS 1126.56. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — GOUGED (BS 989-1016)

DURING SCHEDULED D-CHECK, FOUND NUMEROUS SCRATCHES AND GOUGES IN SKIN AT BS 989 TO BS 1016, WL 233 - WL 241 LEFT SIDE. REMOVED AND REPLACED PER TRAMCO EWO NR 98-0676.

Part: SKIN — DENTED (BS 337)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 337 DENTED 3 BELOW STR 17 LT FWD ENTRY DOOR LOWER THRESHOLD. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — DENTED (CARGO DOORWAY)

DURING SCHEDULED D-CHECK, FOUND FWD CARGO BAY DOOR FRAME COVER PLATE DENTED AT BS 492 TO 495, RBL 25 TO 30, WL 169. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 568)

DURING SCHEDULED D-CHECK, FOUND RAM AIR INLET DUCT SKATE ANGLE CRACKED AT BS 568 WL 166, LBL 47. REPAIRED PER BOEING SRM.

Part: CLIP — CRACKED (BS 500)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 19R, WL 192. REMOVED AND REPLACED PER BOEING MM.

Part: FLOORBEAM — DENTED (BS 430)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM TIE STRAP DENTED AT BS 430, RBL 10, WL 156. REMOVED AND REPLACED PER BOEING MM.

Part: STRAP — CORRODED (BS 780-847)

DURING SCHEDULED D-CHECK, FOUND CORRODED SILL WEB TIE STRAP AT BS 780 TO 847, RBL 20, WL 160. REMOVED AND REPLACED PER BOEING SRM.

Part: STRAP — CORRODED (BS 787-800)

DURING SCHEDULED D-CHECK, FOUND CORRODED SILL WEB LOWER TIE STRAP AT BS 787 TO 800, RBL 20, WL 157. REMOVED AND REPLACED PER BOEING SRM.

Part: CREASE BEAM — CRACKED (BS 179)

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM AT BS 179 CRACKED AT 17 RT, RBL 29. REPAIRED PER BOEING SRM.

Part: STRAP — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND STABILIZER STRAP CRACKED AT BS 344, LBL 45.5 WL 200. REPAIRED PER BOEING SRM.

Part: STRAP — CORRODED (BS 842-852)

DURING SCHEDULED D-CHECK, FOUND CORRODED SILL WEB LOWER TIE STRAP AT BS 842 TO 852, RBL 20, WL 162. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — DAMAGED (CARGO DOORWAY)

DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR CUTOUT, AFT FRAME CLOSEOUT PANEL IS DAMAGED AT BS 847, RBL 25. REPAIRED PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 1104)

DURING SCHEDULED D-CHECK, FOUND CRACKED SHEAR TIE AT BS 1104 BETWEEN STR 17R AND 18R. REPAIRED PER BOEING SRM.

Part: CREASE BEAM — CRACKED (BS 179)

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM AT BS 179 CRACKED AT 17 RT RBL 29. REPAIRED PER BOEING SRM.

Part: STRAP — CORRODED (BS 772)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM TIE STRAP AT BS 772, RBL 21 LBL 21 WL 162. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 291)

DURING SCHEDULED D-CHECK, FOUND CRACKED ANGLE STIFFENER AT BS 291, WL 248, RBL 60. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — MISDRILLED (BS 986.5)

DURING SCHEDULED D-CHECK, FOUND MISDRILLED HOLE AT BS 986.5 FLOORBEAM RBL 2 WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — GOUGED (BS 1124)

DURING SCHEDULED D-CHECK, FOUND GOUGED SKIN AT BS 1124, 1 INBOARD OF STR 2 LT. REPAIRED PER TRAMCO EWO NR 980696.

Part: FLOORBEAM — CRACKED (BS 947)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT FLOORBOARD FASTENER HOLE AT BS 947, LBL 53.5 WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CHAFED (BS 720)

DURING SCHEDULED D-CHECK, FOUND WHEEL WELL ATTACH ANGLE CHAFED FASTENER HOLES AT BS 720, RBL 15, WL 152. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 616)

DURING SCHEDULED D-CHECK, FOUND BS 616 FRAME INBOARD CHORD CRACKED AT LBL 64 WL 201. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 1124)

DURING SCHEDULED D-CHECK, FOUND GOUGED SKIN AT BS 1124, 1 INBOARD OF STR 2 RT. REPAIRED PER TRAMCO EWO NR 980696.

Part: SKIN — GOUGED (BS 296)

DURING SCHEDULED D-CHECK, FOUND SKIN DENTED AND GOUGED AT BS 296 ABOVE STR 19L. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 294)

DURING SCHEDULED D-CHECK, FOUND LOWER STUB FRAME CRACKED AT BS 294, WL 208 RBL 54. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 727 & 440)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STRINGER 8 AND 9 LT AT BS 727D AND STRINGERS 8 AND 9 RT AT BS 440. REPAIRED PER BOEING SRM.

Part: CHORD — CORRODED (BS 270)

DURING SCHEDULED D-CHECK, FOUND CORRODED AT BS 270 Z-CHORD, RBL 11, WL 208. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 178, LBL 5.7 WL 202. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED D-CHECK, FOUND CRACKED SKIN AFT SERVICE DOOR HINGE CUTOUT LOWER RADIUS. REPAIRED PER BOEING SRM.

Part: SKIN — CREASE (BS 807)

DURING SCHEDULED D-CHECK, FOUND CREASE IN SKIN AT BS 807 BETWEEN STR 27L AND 27R. REPAIRED PER BOEING SRM.

Part: FRAME — DENTED (BS 727)

DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 727, RBL 34, WL 158. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 400)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 8R AND 9R AT BS 400. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 907)

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

Part: STRAP — CORRODED (BS 440-492)

DURING SCHEDULED D-CHECK, FOUND CORRODED SILL WEB TIE STRAP AT BS 440 TO 492 RBL 22 WL 157. REMOVED AND REPLACED PER BOEING SRM.

Part: STRAP — CORRODED (BS 589)

DURING SCHEDULED D-CHECK, FOUND FLOOR PANEL TIE STRAP CORRODED AT BS 589, RBL 18 LBL 21 WL 165. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 440)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 8R AND 9R AT BS 440. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 867)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 8R AND 9R AT BS 867. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — DENTED (BS 727)

DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 727E, LBL 25.5, WL 157. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 500)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 8R AND 9R AT BS 500C. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 386)

DURING SCHEDULED D-CHECK, FOUND SHEAR WEB UPPER ATTACH L-ANGLE CRACKED BS 386 WL 207 BL 0. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 907)

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

Part: FRAME — CRACKED (BS 727)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 8R AND 9R AT BS 727B. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — DENTED (BS 767)

DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 767, RBL 35, WL 160. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (LEFT)

DURING SCHEDULED D-CHECK, FOUND CORRODED LEFT HAND STABILIZER BEAM PANEL L-ANGLES ARE CHAFED. REPAIRED PER BOEING MM.

Part: BEAM — CORRODED (LEFT)

DURING SCHEDULED D-CHECK, FOUND CORRODED LEFT HAND STABILIZER BEAM. REPAIRED PER BOEING MM.

Part: SKIN — DENTED (BS 953)

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN DENTED 15 BELOW AFT GALLEY DOOR FWD LOWER CORNER BS 953 WL 196 RBL 53. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM UPPER CHORD BS 328, RBL 29, 33, 35.5 AND RBL 42.5 WL 208 AND WL 207. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CORRODED (BS 1015)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR WEB AT BS 1015 LBL 38 WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — GOUGED (BS 848)

DURING SCHEDULED RON CHECK, FOUND GOUGE AND DENTED FUSELAGE SKIN AT BS 848 STR 18L. REPAIRED CUT OUT DAMAGED SKIN PER BOEING SRM.

Part: STIFFENER — CRACKED (BS 328)

DURING SCHEDULED D-CHECK, FOUND FLOOR STIFFENER CRACKED AT BS 328, LBL 45.5, WL 204 AFT SIDE OF FLOORBEAM. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 344, LBL 9, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: STIFFENER — CRACKED (BS 328)

DURING SCHEDULED D-CHECK, FOUND FLOOR STIFFENER CRACKED AT BS 328, RBL 32, WL 201. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 345)

DURING SCHEDULED D-CHECK, FOUND CORRODED INTERCOSTAL AT BS 345, BL 0 WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 540)

DURING SCHEDULED C2 CHECK, FOUND CRACKED INTERCOSTAL AT BS 540 FLOOR RT 1.5 FROM CENTER, AND AT BS 540 FLOOR LT 1.5 FROM CENTER. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 380)

DURING SCHEDULED BC3 CHECK, FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT E AND E COOLIING DUCT AT BS 380. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (CARGO DOOR)

DURING SCHEDULED BC3 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT LOWER AFT CORNER. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED SERV CHECK, FOUND A 2 INCH FUSELAGE SKIN CRACK APPROXIMATELY 10 INCHES FORWARD OF WATER SERV PANEL. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING WALKAROUND CHECK, FOUND FUSELAGE SKIN CRACKED NEAR WATER SERVICE PANEL. REPAIRED PER BOEING SRM.

Part: UPLOCK SWITCH — FAILED (LT MLG)

LEFT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. CYCLED GEAR, NO HELP. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. REPLACED LEFT GEAR UPLOCK SWITCH PER BOEING M/M.

Part: FLOOR BEAM — CRACKED (E/E COMPT)

DURING SCHEDULED C1 CHECK, FOUND FLOOR BEAM CRACKED IN E/E COMPARTMENT. REPAIRED PER BOEING STRUCTURAL REPAIR MANAUL.