N504SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,140 hrs · 64,223 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 380+12, STR 16R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,309 hrs · 63,660 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 924, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,309 hrs · 63,660 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 924, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,309 hrs · 63,660 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 907+17, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,577 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED BETWEEN BS 767 TO BS 847, BETWEEN STR 25R TO STR 26R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,577 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT BS 867, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,577 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT BS 847, BETWEEN STR 26R TO STR 27R. REPAIRED SKIN PER SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT AFT CARGO COMPARTMENT BEAR STRAP CORRODED AT BS 787, STR 26R. REPAIRED SKIN IAW EA.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD CORRODED AT BS 1016, BETWEEN BL 0 TO RBL 8. REPAIRED BULKHEAD PER EA, SRM, DWG, AND ACO.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT BULKHEAD LOWER STIFFENER CHORD CORRODED AT BS 1016, RBL 1. REPAIRED CHORD PER SRM, ACO, AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULE 22Y CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP CRACKED AT 6 O'CLOCK POSITION. REPAIRED DOME CAP PER EA.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT CHORD CORRODED AT BS 727, BETWEEN STR 27L TO STR 27R. REPAIRED CHORD PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 747+17, STR 24L. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: LIGHT — BROKEN (CABIN) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD LAVATORY AFT WALL EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT HORIZONTAL STABILIZER HINGE HOUSING FITTING ATTACH LUGS CORRODED. REPAIRED LUGS IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR FORWARD LOWER CORNER CUTOUT. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, BETWEEN STR 10 TO STR 11L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEUDLED 22Y CHECK, FOUND SKIN CRACKED AT BS 492, STR 16L. REPAIRED SKIN PER EA AND ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK FOUND, R1 DOOR CUTOUT FWD FRAME CRACKED AT BS 294.5+6, BETWEEN STR 17R TO STR 16R. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK FOUND, SHEAR TIE CRACKED AT BS 277, BETWEEN STR 9L TO STR 10L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: MOUNT BRACKET — CRACKED (R2 DOOR) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT MOUTING BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND E&E COMPARTMENT DOOR CUTOUT, RT WEB CRACKED AT BS 351, RBL 15. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 440+15, STR 17L. REPAIRED SKIN PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 482A, STR 17L. REMOVED AND REPLACED WEB IAW BAC DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND T-CAP CORRODED AT BS 986, RBL 5. REPAIRED T-CAP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 24.8. REPAIRED CHORD PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND T-CAP CORRODED AT BS 986, RBL 14. REPAIRED T-CAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND T-CAP CORRODED AT BS 986, LBL 5. REPAIRED T-CAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND T-CAP CORRODED AT BS 986, BETWEEN LBL 5 TO RBL 14. REPAIRED T-CAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 843, STR 16L. REPAIRED SKIN PER EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING O/B AFT FLAP T/E DELAMINATED. REMOVED AND REPLACED SKIN PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK FOUND, SHEAR TIE CRACKED AT BS 294.5, STR 12L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK FOUND, BULKHEAD STIFFENER ATTACH BRACKET CRACKED AT BS 728, RBL 18. REMOVED AND REPLACED T-ANGLE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 12Y CHECK FOUND, CREASE BEAM CRACKED BETWEEN BS 616 TO BS 639, STR 17R. REMOVED AND REPLACED BEAM PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 12Y CHECK FOUND, CREASE BEAM CHORD CRACKED BETWEEN BS 663+10 TO BS 727+4, STR 17L. REMOVED AND REPLACED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 12Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 787, STR 23L. REMOVED AND REPLACED CLIP PER DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 12Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 787, STR 24L. REMOVED AND REPLACED CLIP PER DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK FOUND, R2 DOOR STA 965 TO STA 992 CREASE BEAM ATTACHED ANGLE CORRODED. REPAIRED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK FOUND, FWD CARGO DOOR EXTERIOR SKIN CRACKED AT LOWER FWD CORNER, AT EDGE OF SKIN. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 277, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK FOUND, STRINGER CLIP 15R CRACKED AT BS 277, 15R. REMOVED AND REPLACED CLIP IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK FOUND CRACKS FLIGHT DECK FLOOR WEB, BS 247 RBL 24. REPAIRED PER DOC.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED 22Y CHECK FOUND LT CARGO COMPARTMENT STRINGER CLIP CRACKED, BS 767 STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED MV1 CHECK FOUND CRACK IN FUSELAGE SKIN STA 492, STR 162. REPAIRED PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED MV1 CHECK FOUND FUSELAGE CRACK AT STA 843 JUST ABOVE STR 16L CRACK. REPAIRED PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 492, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,180 hrs · 63,576 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 843, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,440 hrs · 63,073 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 265.5, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,083 hrs · 62,811 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 413, STR 1. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,035 hrs · 62,778 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,035 hrs · 62,778 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 7R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,035 hrs · 62,778 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,035 hrs · 62,778 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,463 hrs · 62,376 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR BS 989.5, STR 7L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,463 hrs · 62,376 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR BS 948.5, STR 11R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,442 hrs · 62,361 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 948.5, STR 12R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,569 hrs · 61,747 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 384, STR 15R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,819 hrs · 61,235 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 933, STR 25R. REPAIRED SKIN PER SRM.

Part: SPLICE — DAMAGED (CABIN) · airframe 62,251 hrs · 60,854 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED SPLICE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,114 hrs · 60,140 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 873, STR 23R. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD GALLEY EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT RADIO ALTIMETER CUTOUT, BETWEEN BS 410 TO BS 450. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,114 hrs · 60,140 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: LENS — MISSING (CABIN) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT ASSY PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT KEEL BEAM LOWER CHORD CORRODED AT BS 482. REPAIRED BEAM PER SRM.

Part: MODULE — FAULTY (A/C SYSTEM) · airframe 61,106 hrs · 60,130 cycles

DECLARED EMERGENCY, SMOKE AND FUMES FILLED AIRCRAFT WHEN INITIATING DESCENT FROM FL 350. SMOKE DISSIPATED AFTER RUNNING SMOKE AND FUMES CHECKLIST. REMOVED AND REPLACED HYDRAULIC SYS PRESSURE MODULE, CHECK VALVES, AND COALESCER BAGS.

Part: TAB — DELAMINATED (AILERON) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING AILERON TAB AFT I/B CORNER DELAMINATED. REMOVED AND REPLACED TAB PER MM.

Part: FLAP — PUNCTURED (LT WING) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING O/B FORE FLAP L/E PUNCTURED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 767, STR 13L TO STR 14L. REPAIRED FRAME PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 819, BETWEEN STR 22L TO STR 23L. REPAIRED SKIN PER SRM.

Part: RIB — CRACKED (LT WING) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING LOWER RIB CHORD CRACKED, WBL 135.5, BETWEEN S2 TO S3. REPAIRED CHORD PER ACO.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SURFACE SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,104 hrs · 60,128 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,696 hrs · 59,867 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 436, STR 17R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,696 hrs · 59,867 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 413, STR 17L. REPAIRED SKIN PER SWA EA.

Part: HOUSING — BROKEN (CABIN) · airframe 59,781 hrs · 59,218 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EMERGENCY LIGHT BATTERY PACK HOUSING BROKEN. REMOVED AND REPLACED HOUSING PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 59,578 hrs · 59,011 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,488 hrs · 58,926 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 827, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,488 hrs · 58,926 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 482A, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 59,481 hrs · 58,919 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 2 SLAT L/E SKIN CRACKED AT THE INBOARD AUXILIARY TRACK. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,481 hrs · 58,919 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR SKIN CUTOUT CRACKED AT LOWER FWD CORNER. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (NR 6 SLAT) · airframe 59,481 hrs · 58,919 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING NR 6 SLAT L/E LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,971 hrs · 58,440 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 435, STR 1. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,853 hrs · 58,356 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 58,319 hrs · 57,957 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,312 hrs · 57,948 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 460 S17L) · airframe 58,074 hrs · 57,760 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 460, STR 17L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 390 S15L) · airframe 58,074 hrs · 57,760 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 390, STR 15L. REPAIRED SKIN PER SWA EA.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,471 hrs · 57,310 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 56,610 hrs · 56,637 cycles

DURING SCHEDULED HC1 CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 664, RBL 40. REPAIRED WEB PER SRM.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 55,816 hrs · 55,893 cycles

RIGHT MLG WOULD NOT REMAIN UP ON INITIAL RETRACTION. SECOND ATTEMPT GEAR STAYED UP. REMOVED AND REPLACED RIGHT MLG UPLOCK ACTUATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,408 hrs · 55,509 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 55,327 hrs · 55,423 cycles

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

Part: FRAME — CORRODED (BS 992) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 992, RBL 46. REPAIRED FRAME PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED RON, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986.5, RBL 44. REPAIRED FLOORBEAM PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,961 hrs · 55,050 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 406, RBL 1. REPAIRED SKIN PER ER.

Part: FITTING — CORRODED (VERTICAL FIN) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND VERTICAL FIN PRIMARY FITTING CLEVIS LUGS CORRODED. REPAIRED FITTING CLEVIS LUGS PER ER.

Part: CABLE — BROKEN (EVAC SLIDE) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE BROKEN. R&R EVAC SLIDE CABLE PER MM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM.

Part: HOOK — LOOSE (L1 DOOR) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 304, STR 16L. REPAIRED FRAME PER SB.

Part: FLAP — DEBONDED (RT WING) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DISBONDED. REPAIRED FLAP PER SRM.

Part: HINGE — CRACKED (R1 DOOR) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR LOWER GATE HINGE CRACKED. R&R LOWER GATE HINGE PER SRM.

Part: FRAME — CRACKED (BS 616) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT LT BS 616, LOWER ATTACH FASTENERS WL 201. REPAIRED FRAME PER SB.

Part: STRINGER CLIP — CRACKED (BS 597 S16L) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (BS 420-440) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 420 AND BS 440, LBL 69. REPAIRED CREASE BEAM WEB PER SRM.

Part: FRAME — CRACKED (BS 616) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT RT BS 616, LOWER ATTACH FASTENERS WL 201. REPAIRED FRAME PER SB.

Part: FLOORBEAM — CORRODED (BS 294) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 294, RBL 38. REPAIRED FLOORBEAM CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (BS 927 S11R) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — DEBONDED (T/E FLAP) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP UPPER SKIN DISBONDED AT INBOARD END. REPAIRED FLAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5, LBL 5. REPAIRED FLOORBEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 967, STR 8R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SLAT — WORN (LT WING) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND LEFT WING NR 5 L/E SLAT WORN AT INBOARD T/E. REPAIRED SLAT PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — DEBONDED (FORE FLAP) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND RIGHT WING INBOARD FORE FLAP LOWER SURFACE DISBONDED. REPAIRED FORE FLAP PER SRM.

Part: FRAME — CRACKED (BS 440) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 380) · airframe 54,961 hrs · 55,050 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,838 hrs · 54,946 cycles

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

Part: SKIN — CRACKED (BS 259 S23L) · airframe 54,765 hrs · 54,866 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 259 S21L) · airframe 54,765 hrs · 54,866 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,765 hrs · 54,866 cycles

FUSELAGE SKIN CRACKED AT BS 374, STR 15L. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,748 hrs · 54,844 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,748 hrs · 54,844 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,097 hrs · 54,186 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,097 hrs · 54,186 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 777, STR 18L. REPAIRED SKIN PER SWA EA.

Part: MOTOR — SEIZED (TE FLAPS) · airframe 53,265 hrs · 53,339 cycles

FLAPS WOULD NOT EXTEND PAST POSITION 5, ALTERNATE FLAPS NO HELP. REMOVED AND REPLACED FLAP ALT HYDRAULIC MOTOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,645 hrs · 52,690 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 902, STR 25R. REPAIRED SKIN PER SRM.

Part: SPOILER — LOOSE (LT WING) · airframe 52,298 hrs · 52,290 cycles

LEFT WING NR 4 GROUND SPOILER OUTBOARD HINGE LOOSE. REMOVED AND REPLACED NR 4 SPOILER PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 52,230 hrs · 52,214 cycles

DURING SCHEDULED A2 CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING AT AFT SERVICE DOOR. INSTALLED LIGHT LENS PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 51,529 hrs · 51,467 cycles

DURING SCHEDULED C2 CHECK, FOUND LH WING OUTBD T/E AFT FLAP DELAMINATED. R&R FLAP PER MM.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 51,529 hrs · 51,467 cycles

DURING SCHEDULED C2 CHECK, FOUND NLG W/W CEILING PANEL CUTOUT CRACKED AT BS 251.625, LBL 7.75 & RBL 7.75. REPAIRED PANELS PER SWA EA.

Part: SKIN — CRACKED (BS 930) · airframe 51,470 hrs · 51,402 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 21R. REPAIRED SKIN PER SWA EA & SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 51,395 hrs · 51,316 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: CABLE — MISROUTED (R2 DOOR SLIDE) · airframe 50,732 hrs · 50,607 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM.

Part: SKIN — CRACKED (BS 405) · airframe 50,500 hrs · 50,375 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 405, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — WORN (BS 865) · airframe 50,054 hrs · 49,892 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN WORN AT BS 865, UNDER DORSAL FIN BLADE SEAL. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 947) · airframe 49,888 hrs · 49,731 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — DISCHARGED (R2 DOOR) · airframe 49,563 hrs · 49,362 cycles

DURING SCHEDULED RON CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM.

Part: WEDGE — DELAMINATED (T/E FLAP) · airframe 48,991 hrs · 48,726 cycles

DURING SCHEDULED RON CHECK, FOUND RT WING INBOARD MIDFLAP T/E WEDGE DELAMINATED. REMOVED AND REPLACED MIDFLAP T/E WEDGE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,975 hrs · 48,704 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 882, STR 26R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 48,965 hrs · 48,691 cycles

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

Part: BOLT — WORN (LT ELEVATOR) · airframe 48,196 hrs · 47,878 cycles

DURING SCHEDULED C2 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BOLT PER MM.

Part: FRAME — CRACKED (SERVICE DOOR) · airframe 48,196 hrs · 47,878 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR LOWER FRAME AT AFT LOWER STOP, CRACKED. REMOVED AND REPLACED FWD SERVICE DOOR MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,196 hrs · 47,878 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 23R, CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 47,774 hrs · 47,479 cycles

L1 DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT WINDOW CUTOUT, BS 482A + 10, STRINGER 13R, CRACKED. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND R1 DOOR CUTOUT LOWER AFT CORNER SKIN CRACKED. REPAIRED SKIN PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 380, STRINGER 20L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 10R AT BS 908, CRACKED. REPAIRED STRINGER SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 797 AND BS 817, STRINGER 13L. REPAIRED SKIN SECTIONS PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BUTT STRAP AT BS 907, STRINGER 4R, CRACKED. REPAIRED BUTT STRAP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT PRESSURE BULKHEAD AT BS 1016, BL 0, 4 INCHES ABOVE CENTER WEB, CRACKED. REPAIRED AFT BULKHEAD PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 482, STRINGER 14R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH CRACKS ON FLOORBEAM WEB AND FLOORBEAM UPPER CAP AT CENTER FLOORBEAM, BS 663.75. REPAIRED FLOORBEAM CHORD AND UPPER CAP PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH SHEAR TIES CRACKED AT BS 360, BETWEEN STRINGERS 13L AND 15L. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 445, STRINGER 10R, CRACKED. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS BETWEEN BS 767 AND BS 787, STRINGER 14R. REPAIRED SKIN SECTIONS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BUTT STRAP AT BS 908, STRINGER 11L, CRACKED. REPAIRED BUTT STRAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER FWD CUTOUT. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT LBL 6, WL 208. REPAIRED WEB PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS STR 4R CRACKED AT BS 908. REPAIRED STRINGER ASSY PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 482A FRAME CRACKED BETWEEN STR 20L & STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 20L TO STR 20 R. REPAIRED FRAME PER SRM.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BOTH L1 DOOR EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 380, STRINGER 22L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 846, STRINGER 25R CORRODED. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER BETWEEN BS 695 AND BS 706, STRINGER 17L, CRACKED. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,736 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 480, BETWEEN STRINGER 20R AND STRINGER 21R, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,636 hrs · 47,321 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STRINGER 21L REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,331 hrs · 47,007 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 482, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,331 hrs · 47,007 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 790, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,847 hrs · 46,493 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN AT BS 516, STRINGER 16R, CRACKED. REPAIRED SKIN PER EA.

Part: WEB — CRACKED (AFT CARGO DOOR) · airframe 46,514 hrs · 46,180 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR FWD LOWER CORNER WEB, CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: LENS — LOOSE (CABIN) · airframe 46,198 hrs · 45,870 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT BULLNOSE LENS BETWEEN ROWS 16 DEF AND 17 DEF, LOOSE. SECURED BULLNOSE LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,074 hrs · 45,730 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 428 + 13, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 45,814 hrs · 45,470 cycles

R2 DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. ADJUSTED SLIDE ASSY PER MM.

Part: SLIDE — DEPLOYED (L1 DOOR) · airframe 45,524 hrs · 45,210 cycles

L1 DOOR EVAC SLIDE DEPLOYED AT GATE. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,208 hrs · 44,910 cycles

DURING SCHEDULED SPV, FOUND SKIN CRACKED AT BS 432, STRINGER 16L, BS 777, STRINGER 18L, BS 933, STRINGER 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,877 hrs · 43,668 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 764, STR 22L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 42,560 hrs · 42,436 cycles

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

Part: SLIDE — LOOSE (FWD ENTRY DOOR) · airframe 40,964 hrs · 40,954 cycles

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

Part: GATE — OUT OF ADJUST (FWD SVC DOOR) · airframe 40,465 hrs · 40,477 cycles

AIR TURNBACK, DURING CLIMB ABRUPTLY EXTREMELY LOUD NOISE COMING FROM FWD SVC DOOR. ADJUSTED LOWER GATE ON DOOR PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 40,418 hrs · 40,432 cycles

EEPLS LOOSE BETWEEN ROW'S NR 5 TO NR 8. SECURED EEPLS PER MM.

Part: BATTERY — INTERMITTENT (CABIN) · airframe 39,925 hrs · 39,978 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD EMERGENCY LIGHTS INTERMITTENT. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 39,925 hrs · 39,978 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LOWER CARGO DOOR BEAR STRAP CORRODED AT BS 794.30, STR 26R TO 27R. REPAIRED BEAR STRAP PER SWA RA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,925 hrs · 39,978 cycles

DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY LIGHT INOP AT ROW NR 3 DEF. REMOVED AND REPLACED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,925 hrs · 39,978 cycles

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

Part: FLOORBEAM — CRACKED (AFT CARGO) · airframe 39,925 hrs · 39,978 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 747, RBL 14. REPAIRED FLOORBEAM PER SWA RA.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 39,925 hrs · 39,978 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAMS CORRODED AT BS 770, BETWEEN LBL 12 TO RBL 8. REPAIRED FLOORBEAMS PER SWA RA.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 39,925 hrs · 39,978 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 754, RBL 3. REPAIRED FLOORBEAM PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,023 hrs · 38,182 cycles

DURING SCHEDULED A1 CHECK, FOUND CAPT'S FWD WINDOW POST SKIN CRACKED .5 INCHES. REPAIRED WINDOW POST SKIN PER SRM.

Part: WINDOW — MISSING (AFT SVC DOOR) · airframe 38,006 hrs · 38,159 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND VIEWING WINDOW MISSING. INSTALLED VIEWING WINDOW PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 37,750 hrs · 37,909 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL WEBS CRACKED ( 2 EA ) AT BS 183, WL 233, LBL 17.1 & RBL 17.1. R&R WEBS PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 37,750 hrs · 37,909 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL WEB CRACKED AT BS 179, WL 227 & LBL 17.1. R&R WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 37,750 hrs · 37,909 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND HORIZONTAL WEBS CRACKED ( 2 EA ) AT BS 180, WL 207, LBL 26.5 & RBL 26.5. R&R WEBS PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 37,550 hrs · 37,702 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED AT FWD CABIN. R&R EEPLS COVERS PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 37,550 hrs · 37,702 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AND COVER BROKEN AT ROWS NR 1 & 2. REPAIRED EEPLS WIRES AND REMOVED AND REPLACED COVER PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 36,965 hrs · 37,104 cycles

AFT SVC DOOR EMERGENCY EXIT SIGN LOOSE. SECURED EXIT SIGN PER MM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 36,735 hrs · 36,874 cycles

DURING SCHEDULED C1 CHECK, FOUND NR 1 L/E SLAT LWR SKIN CRACKED AT AFT ROW OF RIVETS, IN 4 PLACES. REMOVED AND REPLACED NR 1 L/E SLAT PER MM.

Part: STRUCTURE — CRACKED (AFT CARGO DOOR) · airframe 35,787 hrs · 35,969 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR CRACKED INSIDE AT LOWER FWD CORNER ANGLE BRACKET, WEB SKIN AND FWD SIDE OF DOOR, INSIDE, LOWER SIDE STOP FITTING FASTENER. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: SLIDE — OUT OF ADJ (FWD SERVICE DOOR) · airframe 35,425 hrs · 35,600 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE SLIDE ASSY OUT OF ADJUST. REPOSITIONED EVAC SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,175 hrs · 35,355 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE EXT SKIN CRACKED, BS 748-751, STR 18L. REPAIRED SKIN PER SRM.

Part: COVER — BROKEN (CABIN FLOOR) · airframe 34,784 hrs · 34,967 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK BROKEN AT ROW 8. REMOVED AND REPLACED TRACK COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 34,560 hrs · 34,734 cycles

FWD SECTION EEPLS TRACK ASSY LOOSE. INSTALLED EEPLS END-CAP ASSY PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 34,158 hrs · 34,341 cycles

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

Part: SENSOR — ERRATIC (LE FLAP)

ABORTED TAKEOFF, TAKEOFF WARNING SOUNDED. FLAPS, SPEED BRAKE, AND TRIM SET PROPERLY. CLEANED NR 1 AND NR 4 L/E FLAP EXTEND PROX SENSORS. OPS CK GOOD PER MM.

Part: FRAME — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD LT AND RT SIDE CHORDS CRACKED, WL 207. REPAIRED PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD 3 EACH CRACKS, RBL1- LBL 6. REPAIRED BULKHEAD PER SRM.

Part: STRINGER — CRACKED (BS 907)

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

Part: FRAME — CRACKED (BS 291)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED, BS 291, BETWEEN STRINGERS 12R-13R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER SURFACE CORRODED, BS 986, LBL 45 TO RBL 45. REPAIRED FLOORBEAM PER RE NR 99-6451.

Part: CLIP — CRACKED (E/E BAY)

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED, BS 312, STRINGER 18R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: ANGLE — CRACKED (BS 291)

DURING SCHEDULED D CHECK, FOUND FUSELAGE INNER SKIN WEB ANGLES CRACKED, BS 291, BETWEEN STRINGERS 10R-12R. REMOVED AND REPLACED ANGLES PER SRM.

Part: SHEAR TIE — CRACKED (BS 967)

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED, BS 967, STRINGER 6L. REPAIRED SHEAR TIE PER SRM.

Part: SLIDES — OUT OF ADJUST (PAX DOORWAY)

DURING SCHEDULED SERVICE CHECK, FOUND BOTH ENTRY DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. ADJUSTED SLIDE ASSY'S PER MM.

Part: LIGHT — OUT OF TRACK (CABIN)

EEPLS LIGHTS PULLED OUT OF TRACK. RE-INSTALLED LIGHTS PER MM.

Part: COVER — BROKEN (PASSENGER DOOR)

FWD ENTRY DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — LOW PRESSURE (PASSENGER DOOR)

L2 DOOR SLIDE PRESSURE GAUGE IN RED. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: FRAME — CRACKED (CARGO DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND FORWARD CARGO AFT DOORWAY FRAME AT UPPER CORNER CRACKED 1 INCH LONG. REPAIRED PER SWA RA 1-553-1949.

Part: FRAME — CRACKED (CARGO DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND FORWARD CARGO DOORWAY AFT FRAME UPPER CORNER CRACKED 1.5 INCH LONG. REPAIRED PER SWA RA 1-553-1949.

Part: FRAME — CRACKED (EMER EXIT DRWAY)

DURING SCHEDULED CHECK, FOUND A 1 INCH CRACK IN AFT DOORWAY FRAME AT LOWER CORNER MOST I/B STOP. REPAIRED PER SWA RA 1-553-1949.

Part: LIGHT — BROKEN (CABIN)

DURING WALKAROUND CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED FWD ENTRY EMERGENCY EXIT LIGHT, OPS CKS OK PER BOEING MM.

Part: SLIDE — DETACHED (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY ESCAPE SLIDE FELL OUT OF FIBERGLASS SHELL. F/A WAS UNABLE TO ATTACH GIRT BAR. REINSTALLED SLIDE PER BOEING MM.

Part: LIGHTS — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND TWO EMERGENCY LIGHTS INOP IN FLOOR TRACK ROW 10. REPAIRED PER BOEING SRM.

Part: SLIDE — OUT OF CASE (EMER EXIT DOOR)

DURING WALKAROUND CHECK, FOUND LEFT FWD EMERGENCY SLIDE CAME OUT OF CONTAINER WHEN DOOR WAS SHUT FOR PUSH BACK. REINSTALLED SLIDE IN HARD CASE PER BOEING MM.

Part: SKIN — DAMAGED (FUSELAGE)

DURING SCHEDULED A2 CHECK, FOUND NUMEROUS AREA OF LIGHTNING STRIKE DAMAGE AT LEFT FUSELAGE SKIN ALONG WINDOWS 4, 5 AND 7. REPAIRED PER BOEING SRM.