N328SW

Part: LATCH — DEFECTIVE (COCKPIT) · airframe 73,398 hrs · 65,763 cycles

ESCAPE ROPE DOOR INOP. REPAIRED LATCH PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,210 hrs · 65,622 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 203.8, STR 2R. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,210 hrs · 65,622 cycles

DURING SCHEDULED OTS CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP AT ROW 1 AND ROW 23. RELAMPED PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 73,213 hrs · 65,623 cycles

DURING SCHEDULED OTS CHECK, FOUND AFT OF R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 73,210 hrs · 65,622 cycles

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

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 73,210 hrs · 65,622 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR SLIDE GIRT BAR FLAP LOOSE. SECURED GIRT BAR ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,161 hrs · 65,581 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 364, STR 26L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,161 hrs · 65,581 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 405, STR 26L. REPAIRED SKIN PER EA.

Part: LATCH — OUT OF ADJUST (COCKPIT) · airframe 73,144 hrs · 65,574 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT SIDE COCKPIT EMERGENCY EXIT ROPE COMPARTMENT DOOR OUT OF ADJUST. ADJUSTED DOOR LATCH ASSY PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 73,144 hrs · 65,574 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF HOLDER, DID NOT DEPLOY. SECURED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,736 hrs · 65,261 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 385, STR 15R. REPAIRED SKIN PER EA.

Part: CONTROL ROD — CORRODED (ELEVATOR TAB) · airframe 72,420 hrs · 65,005 cycles

DURING SCHEDULED CV CHECK, FOUND RT ELEVATOR CONTROL TAB CONTROL ROD, FWD ROD END CORRODED. REMOVED AND REPLACED TAB ASSY PER EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 71,643 hrs · 6,422 cycles

DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CRACKED AT BS 807, BETWEEN STR 17L TO STR 18L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 71,643 hrs · 6,422 cycles

DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CRACKED AT BS 747, BETWEEN STR 19R TO STR 20R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,639 hrs · 64,421 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 912, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,639 hrs · 64,421 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 783, STR 19L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,639 hrs · 64,421 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 467, STR 16R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,639 hrs · 64,421 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,639 hrs · 64,421 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 731D, STR 19R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,639 hrs · 64,421 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER CUTOUT AT BS 992, STR 8L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,639 hrs · 64,421 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,639 hrs · 64,421 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 474, STR 16R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,639 hrs · 64,421 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 434, STR 16R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,643 hrs · 64,422 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 334, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,643 hrs · 64,422 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 515, STR 16L. REPAIRED SKIN PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,371 hrs · 64,223 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727A S8R) · airframe 71,230 hrs · 64,114 cycles

SUPPLEMENTAL INFORMATION - DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8R. REMOVED AND REPLACED CLIP PER SI.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,610 hrs · 63,641 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR LOWER EMERGENCY LIGHT INOP. REPLACED PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 70,013 hrs · 63,181 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 70,013 hrs · 63,181 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 291.5, STR 13R. REPAIRED FRAME PER EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 294.5, BETWEEN STR 6R TO STR 7R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 380, STR 8R. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER EO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CORRODED AT BS 500, BETWEEN STR 28L TO STR 28R. REPAIRED SKIN PER EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 380, BETWEEN STR 15R TO STR 16R. REPAIRED FRAME PER EO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CHORD CRACKED BETWEEN BS 659.0 TO BS 673.75, LBL 24.5. REPAIRED CHORD PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 947, STR 4L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SI.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 327, RBL 30. REPAIRED WEB PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 705 TO BS 715, LBL 24.5. REPAIRED WEB PER EO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4R. REMOVED AND REPLACED CLIP PER SI.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 706 TO BS 713, BBL 0. REPAIRED WEB PER SI.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 480 TO BS 500A, STR 28L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 4R. REMOVED AND REPLACED CLIP PER SI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 727E, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 927, STR 4R. REMOVED AND REPLACED SKIN PER SI.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 710 TO BS 713, BBL 0. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING NR 2 SLAT L/E SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 500A, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 705 TO BS 715, RBL 24.5. REPAIRED WEB PER SI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1121, STR 2L. REMOVED AND REPLACED CLIP PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 16R. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER FITTING CRACKED AT BS 1016, STR 7L. REMOVED AND REPLACED FITTING PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 1016 TO BS 1088, STR 24L. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 5.7. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CORRODED AT BS 1040, STR 24L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 69,902 hrs · 63,092 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 380, STR 8R. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,532 hrs · 62,816 cycles

FUSELAGE SKIN CRACKED AT BS 500B, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,532 hrs · 62,816 cycles

DURING SCHEDULED MV4 CHECK, FOUND SKIN CRACKED AT BS 914, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,532 hrs · 62,816 cycles

DURING SCHEDULED MV4 CHECK, FOUND SKIN CRACKED AT BS 500B, STR 19R. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 69,532 hrs · 62,816 cycles

FWD CARGO DOOR FRAME CRACKED AT BS 500B, STR 19R. REPAIRED FRAME PER SRM.

Part: FAN — FAULTY (E&E BAY) · airframe 67,420 hrs · 61,302 cycles

AIR TURBACK, SMOKE SMELL IN MAIN CABIN. AFTER TURNING THE A/C RECIRC FAN OFF, SMELL BEGAN TO DISSIPATE. REMOVED AND REPLACED A/C RECIRC FAN PER MM.

Part: CIRCUIT CARD — FAULTY (E&E BAY) · airframe 69,085 hrs · 62,484 cycles

NOSE GEAR RED LIGHT REMAINED ON AFTER GEAR RETRACTION, CYCLED CIRCUIT BREAKER P6-2-C21 WITH NO EFFECT. CYCLED GEAR DOWN THEN UP AND INDICATIONS RETURNED TO NORMAL. REMOVED AND REPLACED M983 NLG RED LIGHT CARD PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,940 hrs · 62,389 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED. REPAIRED FRAME PER ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,940 hrs · 62,389 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO AFT FRAME CLOSURE WEB CRACKED AT BS 847, RBL 38. REPAIRED WEB PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,642 hrs · 62,169 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,558 hrs · 62,104 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LIGHT INOP AT R2 DOOR. RELAMPED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,488 hrs · 61,353 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 812, STR 18L. REPAIRED SKIN PER SWA EA.

Part: LENS — CRACKED (CABIN) · airframe 67,033 hrs · 61,003 cycles

DURING SCHEDULED HC2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS CRACKED AT BS 11 ABC. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,033 hrs · 61,003 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 930 AND BS 945, STR 25R AND STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,033 hrs · 61,003 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 67,033 hrs · 61,003 cycles

DURING SCHEDULED HC2 CHECK, FOUND RIGHT WING INBOARD FORE FLAP OUTBOARD UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 67,014 hrs · 60,989 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,797 hrs · 60,835 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 371, STR 26L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 68,873 hrs · 62,998 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, STR 27R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SIGN — LOOSE (CABIN) · airframe 65,284 hrs · 59,715 cycles

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

Part: SPOILER — DAMAGED (RT WING) · airframe 65,242 hrs · 59,689 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING NR 5 GROUND SPOILER ATTACH LUG BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (BS 503D S16R) · airframe 65,022 hrs · 59,537 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 513B S19R) · airframe 65,022 hrs · 59,537 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513B, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 934 S22R) · airframe 65,022 hrs · 59,537 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 22R. REPAIRED SKIN PER SRM.

Part: MEC — ERRATIC (NR 2 ENGINE) · airframe 63,622 hrs · 58,448 cycles

DIVERSION / DECLARED EMERGENCY, NR 2 ENG N1 ROLLBACK IND. REMOVED AND REPLACED NR 2 ENG MEC.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND LEFT NLG W/W PRESSURE WEB CRACKED AT BS 246, WL 170. REPAIRED PRESSURE WEB PER SWA EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 727, LBL 19. REMOVED AND REPLACED VERTICAL STIFFENER PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM UPPER TEE CAP CORRODED AT BS 986.5, RBL 14 TO LBL 44. R&R FLOORBEAM UPPER TEE CAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5, LBL 53 TO RBL 52. REPAIRED FLOOR BEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOOR BEAM CORRODED AT BS 328, LBL 56 TO RBL 56. REPAIRED FLOOR BEAM PER SWA EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. R&R STRINGER SPLICE PER SRM.

Part: FLOORBEAM — CORRODED (BS 1016) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS BS 1016, RBL 40 TO LBL 40. REPAIRED FLOORBEAM PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 336 S21L) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 336, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 600 S13L) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 600, STR 13L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 344 S21L) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 277 S16L) · airframe 63,554 hrs · 58,391 cycles

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

Part: STRINGER CLIP — CRACKED (BS 312 S21L) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 312, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 328 S21L) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (BS 360 S7L) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 7L CRACKED AT BS 360. REPAIRED STRINGER PER SRM.

Part: STRUCTURE — CRACKED (AILERON TAB) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND LEFT WING AILERON TAB DELAMINATED ON OUTBOARD T/E. REMOVED AND REPLACED AILERON TAB PER MM.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP CRACKED AT BS 1016, STR 23R, RBL 1. REPAIRED DOME CAP PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND NLG RIGHT PRESSURE WEB CRACKED AT BS 246, WL 170. REPAIRED PRESSURE WEB PER SWA EA.

Part: BELTFRAME — CRACKED (BS 360) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 360, STR 14L. REPAIRED BELTFRAME PER SRM.

Part: FRAME — CRACKED (BS 500B) · airframe 63,554 hrs · 58,391 cycles

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

Part: TAB — CRACKED (RT ELEVATOR) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT ELEVATOR TAB CRACKED AT LOWER HINGE CUTOUT. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: STRINGER CLIP — CRACKED (BS 294) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND NLG LEFT PRESSURE WEB CRACKED AT BS 246, WL 170. REPAIRED PRESSURE WEB PER SWA EA.

Part: FRAME — CRACKED (BS 500C) · airframe 63,554 hrs · 58,391 cycles

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

Part: FRAME — CRACKED (BS 500A) · airframe 63,554 hrs · 59,391 cycles

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

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 63,554 hrs · 59,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND FWD CARGO DOOR CRACKED AT LOWER DOOR STOP FITTING NEAR TEE BEAM. REPAIRED DOOR PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,554 hrs · 58,391 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 27L CORRODED AT BS 950. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 270 , BL 0. REMOVED AND REPLACED FLOORBEAM CHORD PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 927, STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 907 AND BS 927, STR 17L. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: FRAME — CRACKED (BS 639) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT RIGHT BS 639, ATTACH FITTING AT NR 4 SEAT TRACK. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,554 hrs · 58,391 cycles

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

Part: FRAME — CRACKED (BS 616) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT LT BS 616, AT LOWER FASTENER ABOVE FUEL TANK. REPAIRED FRAME PER TYPICAL REPAIR MANUAL.

Part: SKIN — CRACKED (NR 2 SLAT) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND LEFT WING NR 2 L/E SLAT CRACKED AT OUTBOARD AUX TRACK. REPAIRED SLAT PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT RIGHT BS 616, AT LOWER FASTENER ABOVE FUEL TANK. REPAIRED FRAME PER TYPICAL REPAIR MANUAL.

Part: FRAME — CRACKED (BS 500C S20L) · airframe 63,554 hrs · 58,391 cycles

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

Part: FRAME — CRACKED (BS 616) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT RT BS 616, WL 202. REPAIRED FRAME PER TYPICAL REPAIR MANAUL.

Part: FRAME — CRACKED (BS 616) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT LT BS 616, WL 202. REPAIRED FRAME PER TYPICAL REPAIR MANAUL.

Part: FLOORBEAM — CORRODED (BS 312) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM UPPER TEE CAP CORRODED AT BS 312, BETWEEN LBL 56 AND RBL 56. REMOVED AND REPLACED FLOORBEAM TEE CAP PER SRM.

Part: HOOK — LOOSE (R1 DOOR SLIDE) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM.

Part: FLOORBEAM — CORRODED (BS 967) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 967, LBL 27. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 967) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 967, RBL 5. REPAIRED FLOORBEAM PER SWA EA.

Part: SKIN — CRACKED (BS 427-447) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BETWEEN BS 427 AND BS 447, LBL 1. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19L. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 294, BL 0. REPAIRED FLOORBEAM PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800, STR 18L. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,554 hrs · 58,391 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 294, LBL 36 TO RBL 53. REPAIRED FLOORBEAM PER SWA EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 63,494 hrs · 58,347 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,162 hrs · 58,103 cycles

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

Part: SKIN — CRACKED (LT WING SLAT) · airframe 63,013 hrs · 57,985 cycles

DURING SCHEDULED C3 CHECK, FOUND LEFT WING NR 2 L/E SLAT CRACKED AT INBOARD ACTUATOR. REPAIRED SLAT PER SWA EA.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 63,002 hrs · 57,976 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 62,879 hrs · 57,887 cycles

DURING SCHEDULED A2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP MISSING AT ROW 8 ABC TO ROW 10 ABC. INSTALLED STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,012 hrs · 57,251 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 771, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,012 hrs · 57,251 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 804, STR 18L. REPAIRED SKIN PER SWA EA.

Part: BOLT — WORN (RT ELEVATOR) · airframe 61,104 hrs · 56,556 cycles

DURING SCHEDULED C1 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT TAB NR 1 HINGE BOLT AND BUSHING PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 60,872 hrs · 56,387 cycles

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

Part: STRUCTURE — WORN (RT FOREFLAP) · airframe 60,154 hrs · 55,835 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING T/E OUTBOARD FORE FLAP WORN AT INBOARD END. REMOVED AND REPLACED FORE FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,141 hrs · 55,823 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,141 hrs · 55,823 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AT UPPER NR 1 DOOR STOP FITTING. REPAIRED FRAME PER EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 60,141 hrs · 55,823 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT UPPER INBOARD CORNER OF NR 5 STOP. REPAIRED FRAME SECTION PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,141 hrs · 55,823 cycles

DURING SCHEDULED SPV CHECK, FOUND MID CABIN LT OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,141 hrs · 55,823 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,141 hrs · 55,823 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 58,424 hrs · 54,479 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (BS 762.25) · airframe 57,946 hrs · 54,092 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 762.25, STR 19L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 750.5) · airframe 57,946 hrs · 54,092 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750.5, STR 19L. REPAIRED SKIN PER SWA EA.

Part: WIRE — CHAFED (CONTROL PANEL) · airframe 57,679 hrs · 53,867 cycles

DIVERSION/DECLARED EMERGENCY, A LARGE ELECTRIC SPARK OCCURRED IN COCKPIT OVERHEAD PANEL AND SHOWERED CENTER CONSOLE WITH SPARKLER LIKE FRAGMENTS. FOUND CHAFFED WIRE BUNDLE IN OVERHEAD PANEL, REPAIRED WIRE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,506 hrs · 53,737 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 15, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,506 hrs · 53,737 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 15, STR 18L. REPAIRED SKIN PER SWA EA & SRM.

Part: DOOR FRAME — CRACKED (AFT CARGO DOOR) · airframe 57,506 hrs · 53,737 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT CARGO DOOR FWD FRAME CRACKED BETWEEN 2ND & 3RD STOP FITTING CUTOUT. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,506 hrs · 53,737 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 15, STR 19R. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (R1 DOOR) · airframe 56,554 hrs · 52,972 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EXIT LOWER LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY.

Part: CLIP — LOOSE (GIRT BAR) · airframe 55,350 hrs · 52,054 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR STOW HOOK CLIPS LOOSE. SECURED STOW HOOK CLIPS PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 55,350 hrs · 52,054 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED AT MID SPAR AREA. REMOVED FORE FLAP ASSY PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 55,350 hrs · 52,054 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE KEELBEAM CORRODED AT STR 28L, BETWEEN BS 500D AND BS 520. REPAIRED KEEL BEAM SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,350 hrs · 52,054 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR FWD LOWER CUTOUT. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (L1 DOOR) · airframe 55,350 hrs · 52,054 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,350 hrs · 52,054 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT DOME CAP, 2 O'CLOCK POSITION. REPAIRED WEB PER SWA EA.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 55,350 hrs · 52,054 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR AFT FRAME CRACKED AROUND 4TH STOP FITTING. REPAIRED FRAME PER SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 55,350 hrs · 52,054 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 665 BEADED WEB CRACKED AT RBL 40. REPAIRED WEB PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 55,350 hrs · 52,054 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 665, LBL 39.5, CRACKED. REPAIRED PRESSURE WEB PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,350 hrs · 52,054 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 665, BL 0, CRACKED. REPAIRED CHORD PER EA.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 55,350 hrs · 52,054 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CAPT'S NR 1 WINDOW UPPER OUTBOARD POST CRACKED. REPAIRED NR 1 WINDOW POST PER SRM.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 55,350 hrs · 52,054 cycles

DURING SCHEDULED 1/4D CHECK, FOUND F/O'S NR 1 WINDOW UPPER OUTBOARD POST CRACKED. REPAIRED NR 1 WINDOW POST PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,350 hrs · 52,054 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 663, BL 0, CRACKED. REPAIRED CHORD PER EA.

Part: SKIN — CRACKED (PAX DOOR) · airframe 55,350 hrs · 52,054 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,350 hrs · 52,054 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,350 hrs · 52,054 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT FRAME WEB CRACKED AT BS 303, FWD LOWER STOP FITTING. REMOVED AND REPLACED FRAME WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,350 hrs · 52,054 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 771, LBL 13, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,299 hrs · 52,017 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 933, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,848 hrs · 51,627 cycles

DURING SCHEDULED A1 CHECK, FOUND 2 EACH SERVICE DOORS EGRESS LIGHTS INOP. RELAMPED EGRESS LIGHTS PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 54,633 hrs · 51,442 cycles

DURING SPINDLE INSPECTION, FOUND AREA OF DELAMINATION ON OUTBOARD T/E FLAPS. REPAIRED OUTBOARD T/E FLAPS PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,528 hrs · 51,347 cycles

R2 & L2 DOOR EMERGENCY EXIT LIGHTS STAY ON IN ARMED POSITION. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 59,832 hrs · 50,890 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT LOWER LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 53,799 hrs · 50,744 cycles

DURING SCHEDULED C1 CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RIGHT ELEVATOR HINGE BUSHING PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 53,794 hrs · 50,740 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT CARGO DOOR, FWD FRAME AT SPRING TENSION PLATE, CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 53,775 hrs · 50,726 cycles

LEFT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED T/E AFT FLAP PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 52,891 hrs · 50,011 cycles

DURING SCHEDULED C4 CHECK, FOUND OVERWING OVERHEAD EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,891 hrs · 50,011 cycles

DURING SCHEDULED C4 CHECK, FOUND STRINGER 18L CRACKED AT BS 750. REPAIRED STRINGER PER SRM.

Part: SKIN — DELAMINATED (LT SPOILER) · airframe 52,771 hrs · 49,922 cycles

NR 2 FLIGHT SPOILER DEVELOPS BULGE ON TOP OF SPOILER DURING FLIGHT. REMOVED AND REPLACED NR 2 FLIGHT SPOILER PER MM.

Part: STRUCTURE — CRACKED (ENTRY DOOR) · airframe 52,007 hrs · 49,315 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR FWD LOWER CORNER CUTOUT CRACKED 2.0 IN. REPAIRED PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,000 hrs · 49,310 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER FWD CUTOUT. REPAIRED SKIN PER SWA EA.

Part: HANDLE — LOOSE (SERVICE DOOR) · airframe 38,143 hrs · 34,952 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PULL HANDLE LOOSE. REMOVED AND REPLACED SLIDE PER MM.

Part: SLAT — OUT OF RIG (LT WING) · airframe 50,561 hrs · 48,133 cycles

NR 4 L/E SLAT VISUALLY NOT ALIGNED WITH OTHER SLATS. REMOVED AND REPLACED NR 4 L/E SLAT AND OUTBD GUIDE STOP.

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 50,222 hrs · 47,872 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,222 hrs · 47,872 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH AFT ENTRY & AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. RELAMPED BOTH AFT ENTRY AND AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHTS PER MM.

Part: CABLE — MISROUTED (ESCAPE SLIDE) · airframe 50,222 hrs · 47,872 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 50,222 hrs · 47,872 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH FWD ENTRY AND FWD SERVICE DOOR EMERGENCY EVACUATION SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 50,222 hrs · 47,872 cycles

DURING SCHEDULED C1 CHECK, FOUND OVERHEAD CEILING EMERGENCY EXIT LIGHT LOOSE AT OVERWING EXITS. SECURED CEILING EMERGENCY EXIT LIGHT PER MM.

Part: COVER — MISSING (FWD CABIN) · airframe 49,952 hrs · 47,654 cycles

DURING SCHEDULED RON, FOUND EEPLS COVER MISSING IN FWD CABIN. REMOVED AND REPLACED EEPLS LIGHT ASSY SECTION PER MM.

Part: FITTING — CORRODED (LT MLG W/W) · airframe 49,318 hrs · 47,145 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT MLG FWD WALKING BEAM SUPPORT FITTING CORRODED. REMOVED AND REPLACED LT MLG FWD WALKING BEAM SUPPORT FITTING PER MM.

Part: SKIN — CRACKED (A/C COMPT) · airframe 49,220 hrs · 47,059 cycles

DURING SCHEDULED C4 CHECK, FOUND LT/RT EXTERNAL A/C COMPT DOOR CUTOUTS CRACKED AT FWD OUTBD EDGES. REPAIRED SKIN CUTOUTS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,373 hrs · 46,337 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 748, STR 18L. REPAIRED SKIN PER SRM.

Part: TAB — WORN (LT ELEVATOR) · airframe 47,225 hrs · 45,389 cycles

DURING SCHEDULED A1 CHECK, SWA SI 11111-55, LEFT ELEVATOR NR 1, 2 AND 4 TAB HINGE BEARINGS WORN. REMOVED AND REPLACED LT ELEVATOR TAB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,225 hrs · 45,389 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 14R. REPAIRED FRAME PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 47,225 hrs · 45,389 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT BS 787, STR 21R AND BS 727E, STR 25R. REMOVED AND REPLACED TIE CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,225 hrs · 45,389 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, BETWEEN STR'S 20R AND 21R. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 47,225 hrs · 45,389 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE AND TIE CLIP CRACKED AT BS 663.75, STR 10. REPAIRED STR SPLICE AND REMOVED AND REPLACED TIE CLIP PER SRM.

Part: WEB — CRACKED (NLG W/W) · airframe 46,503 hrs · 44,784 cycles

DURING SCHEDULED C1 CHECK, FOUND NLG ACTUATOR SUPPORT BEAM WEB CRACKED AT FWD END. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,046 hrs · 44,732 cycles

DURING WALKAROUND INSPECTION, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 500D, STRINGER 16R. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,771 hrs · 44,197 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEBS CRACKED (2 EA) AT BS 178, WL 183, RBL 17.1 AND LBL 17.1. REPAIRED WEBS PERSWA RA.

Part: FLAP — DELAMINATED (LT WING) · airframe 43,803 hrs · 42,510 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING INBD AFT FLAP DELAMINATED AT INBD END. R&R AFT FLAP PER MM.

Part: STIFFENER — CRACKED (MLG W/W) · airframe 42,824 hrs · 41,678 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 663 BULKHEAD VERTICAL STIFFENER CRACKED AT LWR GROUND STUD, FWD OF INBOARD END OF A SYS ELEC HYD PUMP. REMOVED AND REPLACED VERTICAL STIFFENER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,824 hrs · 41,678 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACK AT BS 944, STR 22L. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 40,914 hrs · 39,989 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER DUE TO GIRT BAR NOT PROPERLY STOWED TO CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: FRAME — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD LEFT AND RIGHT OUTBOARD CHORDS CRACKED AT WL 207. REMOVED AND REPLACED BOTH CHORD SECTIONS PER SRM.

Part: FRAME — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD HORIZONTAL CHORD CRACKED, LBL 28. REPAIRED CHORD PER SWA RA NR 1-353-2184.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 12. REPAIRED BULKHEAD PER SRM.

Part: FLOORBEAM — CORRODED (BS 794)

DURING SCHEDULED 1/4D CHECK, FOUND BS 794 FLOORBEAM CORRODED, RBL 8. REPAIRED BEAM PER SWA RA NR 1-353-2182.

Part: FRAME — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 HORIZONTAL CHORD CRACKED, RBL 28. REMOVED AND REPLACED CHORD SECTION PER SRM.

Part: SLIDE — DETACHED (PAX DOOR)

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT DURING DOOR OPENING. (DID NOT DEPLOYED). REINSTALLED SLIDE ASSY PER MM.

Part: BATTERY — DISCHARGED (CABIN)

FWD UPPER EMERGENCY FLASHLIGHT BATTERY WEAK. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY PER MM.

Part: SKIN — GOUGED (BS 516)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 516, ABOVE S22R. REPAIRED PER BOEING SRM.

Part: LONGERON — CRACKED (NR 2 PYLON)

DURING SCHEDULED D-CHECK, FOUND LONGERON ON LOWER I/B SIDE OF NR 2 PYLON CRACKED. REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 498)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 498, AT S23L. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 500)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 500A+4, BELOW S16L. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 351)

DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 351, RBL 1, WL 153. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 360)

DURING SCHEDULED D-CHECK, FOUND STRINGER CHANNEL CRACKED AT BS 360, AT S4L. REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 328)

DURING SCHEDULED D-CHECK, FOUND ANGLE CRACKED AT BS 328, LBL 54, WL 182. REPLACED PER BOEING SRM.

Part: STRAP — CRACKED (BS 314)

DURING SCHEDULED D-CHECK, FOUND STABILIZER STRAP CRACKED AT BS 314, AND RBL 32. REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 279)

DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 279, AT RBL 54. REPLACED PER BOEING SRM.

Part: LONGERON — CRACKED (NR 1 PYLON)

DURING SCHEDULED D-CHECK, FOUND LONGERON ON LOWER I/B SIDE OF NR 1 PYLON CRACKED. REPLACED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 1140)

DURING SCHEDULED D CHECK, FOUND STRINGER 5R CRACKED AT BS 1140. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 947)

DURING SCHEDULED D CHECK, FOUND FLOOR TO SIDEWALL SUPPORT ANGLE CORRODED AT BS 947, RBL 21-LBL21. REPLACED PER BOEING SRM

Part: FRAME — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED D CHECK, FOUND STUB FRAME AT BS 294, WL 209, FWD SERVICE DOORWAY FWD FRAME CRACKED. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (FUSELAGE)

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT HAT RACK ATTACH BRACKET BETWEEN S8 AND 9R OF BS 747, 727D, 787 AND 827. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 398)

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT BS 398, ABOVE S16L, AND AT BS 827 BETWEEN S16 AND 17L, AT BS 303, BETWEEN S22 AND 23R, AT BS 316, BETWEEN S19 AND 20R, BS 269, ABOVE S25R, AT BS 328 TO 348, BETWEEN S22 AND 23R. REPAIRED PER BOEING SRM.

Part: CLIP — CRACKED (BS 500D)

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT S19R, BS 500D. REPAIRED PER BOEING SRM.

Part: FRAME — DENTED (BS 500)

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME DENTED AT BS 500, RBL 35 AND 39, WL 162. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 263/1058)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 263, BETWEEN S15 AND 16L, AT BS 298, BETWEEN S17 AND 18R, AND AT BS 1058, 1.5 ABOVE S15L. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 295)

DURING SCHEDULED D CHECK, FOUND WEB CRACKED AT BS 295, LBL 56, WL 217. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 296)

DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 296, LBL 54. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 390)

DURING SCHEDULED D CHECK, FOUND CRACKED SHEAR WEB UPPER ATTACH L ANGLE AT BS 390. REPLACED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BS 178 WEB CRACKED AT WL 212 TO 212.5, WL 201 TO 202, 197.5 TO 199, 209.75 TO 210.25, 211.75 TO 213, 200.25 TO 201.25, 198.75 TO 199.25. REPAIRED PER BOEING SRM.

Part: STRAP — CRACKED (BS 314/328)

DURING SCHEDULED D CHECK, FOUND STABILIZER STRAP CRACKED AT BS 328 RBL46, AND AT BS 314, RBL 32. REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 336)

DURING SCHEDULED D CHECK, FOUND MULTIPLE FUSELAGE SKIN DENTS AT BS 336, ABOVE S12R. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5, LBL 25, BL 0 RBL 5, 9, 31.5 AND 35.5, AND 39.5, AT BS 727-947, RBL 25, AND LBL 8, 25, AND 12. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 270)

DURING SCHEDULED D CHECK, FOUND Z ANGLE CHORD BODY CORRODED AT BS 270, LBL 9. REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 328)

DURING SCHEDULED D CHECK, FOUND 1.5 FUSELAGE SKIN CRACKED AT BS 328, AT WL 209 AT FWD SERVICE DOORWAY AFT LOWER CORNER. REPAIRED PER BOEING SRM.

Part: KEELBEAM — CORRODED (BS 712-727)

DURING SCHEDULED D CHECK, FOUND KEEL BEAM CORROSION AT BS 712 TO 727. REPAIRED PER TRAMCO EWO 97-0544.

Part: ANGLE — CRACKED (BS 294)

DURING SCHEDULED D CHECK, FOUND CRACKED L ANGLE AT BS 294, RBL 55, WL 208. REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (SERV DR CUTOUT)

DURING SCHEDULED C1 CHECK, FOUND FORWARD SERVICE DOOR UPPER CUTOUT LOWER CORNER CRACKED. REPAIRED PER SWA RA 1-352-0260.

Part: SKIN — CRACKED (PAX DOOR CUTOUT)

DURING SCHEDULED C1 CHECK, FOUND FORWARD ENTRY DOOR UPPER HINGE CUTOUT UPPER CORNER CRACKED. REPAIRED PER SWA RA 1-352-0261.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED A1 CHECK, FOUND CRACK FORWARD OF SHEAR WEB BEAM STRINGER 18A. REPAIRED PER ACO 6580-56 AND RA 1-353-1518.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND FWD CABIN EMERGENCY LIGHTS ERRATIC. REPLACED BATTERY PACK AND CHARGER PER BOEING M/M.

Part: SKIN — CRACKED (FWD SERV DOOR)

DURING SCHEDULED B/C2 CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUTOUT CRACKED .25 INCHES AT UPPER CORNER. REPAIRED PER SWA RA 1-352-242.