N303SW

Part: FLAP — DELAMINATED (LT WING) · airframe 80,077 hrs · 74,999 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING INBOARD FORE FLAP DELAMINATED AT T/E. REMOVED AND REPLACED FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,595 hrs · 74,627 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,595 hrs · 74,627 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CRACKED AT BS 500A, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 79,595 hrs · 74,627 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT AFT BULKHEAD WEB CRACKED AT BS 663, RBL 58. REPAIRED WEB PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 79,595 hrs · 74,627 cycles

DURING SCHEDULED 26Y CHECK, FOUND LONGITUDINAL FLOORBEAM LOWER WEB CRACKED AT BS 713, LBL 24.5. REPAIRED WEB PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,595 hrs · 74,627 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 706, STR 6L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,595 hrs · 74,627 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 79,595 hrs · 74,627 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO BAY FLOORBEAM CORRODED AT BS 858, BETWEEN LBL 3 TO LBL 8. REPAIRED BEAM PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,595 hrs · 74,627 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 79,595 hrs · 74,627 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO BAY BEAM CORRODED AT BS 858, BETWEEN LBL 1 TO RBL 13. REPAIRED BEAM PER EA.

Part: RIB — CRACKED (LT WING) · airframe 79,595 hrs · 74,627 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT WING RIB CRACKED AT STA 135.5, BETWEEN STR 2 TO STR 3. REPAIRED RIB PER ACO.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,104 hrs · 74,257 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED BETWEEN BS 470 TO BS 490, AT STR 27L. REMOVED AND REPLACED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,104 hrs · 74,257 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 79,104 hrs · 74,257 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CORRODED AT BS 500D, STR 27R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,104 hrs · 74,257 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,104 hrs · 74,257 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,104 hrs · 74,257 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 460, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,104 hrs · 74,257 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 514A, STR 27L. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,104 hrs · 74,257 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 475, STR 28L. REPAIRED STRINGER PER SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 79,104 hrs · 74,257 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT UPPER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,104 hrs · 74,257 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: HOOK — BROKEN (GIRT BAR) · airframe 79,104 hrs · 74,257 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR RETAINING HOOK BROKEN. REMOVED AND REPLACED HOOK ASSY PER SRM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 78,960 hrs · 74,148 cycles

DURING SCHEDULED HC2 CHECK, FOUND AFT CARGO DOOR FWD FRAME CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 78,960 hrs · 74,148 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,960 hrs · 74,148 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 564, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,960 hrs · 74,148 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 683, STR 10R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,517 hrs · 72,396 cycles

DURING SCHEDULED CV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 76,191 hrs · 72,171 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,942 hrs · 71,990 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: SPOILER — LOOSE (RT WING) · airframe 75,578 hrs · 71,753 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 GROUND SPOILER HAS LATERAL MOVEMENT. REMOVED AND REPLACED SPOILER PER MM.

Part: FITTING — LOOSE (NR 5 SPOILER) · airframe 75,578 hrs · 71,753 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 GROUND SPOILER OUTBOARD ACTUATOR FITTING LOOSE. REPAIRED FITTING PER SWA EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 75,578 hrs · 71,753 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 75,578 hrs · 71,753 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,862 hrs · 71,219 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 15 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,862 hrs · 71,219 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,860 hrs · 70,471 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20L. REPAIRED FRAME PER SRM.

Part: WEB — CRACKED (NLG WW) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND NOSE W/W UPPER CEILING PANEL CUTOUT WEB CRACKED AT INBOARD AFT CORNER. REPAIRED WEB PER ACO.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER 23R CRACKED AT BS 328. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,844 hrs · 70,456 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 721 AND BS 727, LBL 8. REMOVED AND REPLACED KEEL BEAM PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BETWEEN BS 406 AND BS 414, LBL 2 AND LBL 4. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, STR 13R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 680, STR 10L. REPAIRED SKIN PER ER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER 25L CORRODED AT BS 889. REPAIRED STRINGER PER SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED BETWEEN BS 301 AND BS 331, STR 17R. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT BS 331, STR 17R. REPAIRED SKIN PER ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER 25L CORRODED AT BS 927. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 291, STR 14R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, STR 8R. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER 17R CRACKED AT BS 638. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 278, STR 21R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (BS 887 S26L) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 887, STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 25R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 500C S27L) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 767 S27L) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 500 S26L) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500 S18R) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 18R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CORRODED (BS 500D S27L) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER 27L CORRODED AT BS 500D. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (BS 927 S26L) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 887, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 251 TO BS 277, BL 0. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: WEB — CRACKED (NLG W/W) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND NLG W/W LT CEILING PANEL CUTOUT WEB CRACKED AT LOWER INBOARD END. REPAIRED WEB PER ACO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 22R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 887, STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 907, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: WEB — CRACKED (NLG W/W) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND NLG W/W RT CEILING PANEL CUTOUT WEB CRACKED AT LOWER OUTBOARD END. REPAIRED WEB PER ACO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER 16R CRACKED AT BS 291. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 360, STR 15R. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 807, STR 18L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 74,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 22R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 74,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 23R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 20L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER 25R CORRODED AT BS 410 TO BS 420. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 634, RBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 618, RBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER 23R CORRODED AT BS 436 TO BS 439. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER 9L CRACKED AT BS 727B. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 25R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER 21R CRACKED AT BS 355. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER 8R CRACKED AT BS 727E. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER 16L CRACKED AT BS 400. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 540, STR 10L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 400 STR 14L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 887, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 597 S8R) · airframe 73,844 hrs · 71,456 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727E S7R) · airframe 73,844 hrs · 71,456 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727B S7R) · airframe 73,844 hrs · 71,456 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727E S5R) · airframe 73,844 hrs · 71,456 cycles

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

Part: STRINGER CLIP — CRACKED (BS 597 S9R) · airframe 73,844 hrs · 71,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706 S11L) · airframe 73,844 hrs · 70,456 cycles

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

Part: FRAME — CRACKED (BS 907 S8L) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 400 S8L) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 727C S22R) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727E S7R) · airframe 73,844 hrs · 70,456 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,844 hrs · 70,456 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 384, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 270 S15R) · airframe 73,714 hrs · 70,352 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 270, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 675 S26R) · airframe 73,714 hrs · 70,352 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 475, STR 26R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 73,236 hrs · 69,981 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,213 hrs · 69,957 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,213 hrs · 69,957 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 790, STR 20L. REPAIRED SKIN PER SWA EA.

Part: HOOK — LOOSE (R1 DOOR GIRT BAR) · airframe 73,115 hrs · 69,884 cycles

R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. REMOVED AND REPLACED GIRT BAR HOOK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,765 hrs · 69,594 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,765 hrs · 69,594 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 790, STR 20L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,765 hrs · 69,594 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 72,357 hrs · 69,278 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 72,257 hrs · 69,191 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 72,257 hrs · 69,191 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 72,257 hrs · 69,191 cycles

DURING SCHEDULED HC2 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: STRINGER — CRACKED (BS 337 S23R) · airframe 72,257 hrs · 69,191 cycles

DURING SCHEDULED HC2 CHECK, FOUND STRINGER 23R CRACKED AT BS 337. REPAIRED STRINGER PER SWA EA.

Part: GLOWSTRIP — WORN (CABIN) · airframe 72,257 hrs · 69,191 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 15 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: STRINGER — CRACKED (BS 365 S26R) · airframe 72,257 hrs · 69,191 cycles

DURING SCHEDULED HC2 CHECK, FOUND STRINGER 26R CRACKED AT BS 365. REPAIRED STRINGER PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 72,101 hrs · 69,057 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 72,064 hrs · 69,025 cycles

AFT CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: CABLE — OUT OF RIG (COCKPIT) · airframe 70,893 hrs · 68,879 cycles

ON APPROACH TO LAX LOWERED LANDING GEAR, 3 GREEN AND 3 RED INDICATOR LIGHTS ILLUMINATED. EXTENDED LANDING GEAR MANUALLY, GEAR INDICATED SAFE. FOUND GEAR HANDLE CABLE OUT OF RIG. RIGGED GEAR HANDLE CABLE PER MM.

Part: SKIN — CRACKED (BS 839 S17L) · airframe 71,777 hrs · 68,784 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 839, STR 17L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 772 S14L) · airframe 71,777 hrs · 68,784 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 772, STR 14L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 834 S20L) · airframe 71,777 hrs · 68,784 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 834, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 854 S17L) · airframe 71,777 hrs · 68,784 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 854, STR 17L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,496 hrs · 68,575 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 690, STR 10L. REPAIRED SKIN PER SWA EA.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 71,496 hrs · 68,575 cycles

DURING SCHEDULED MV1 CHECK, FOUND OUTBOARD TEE CHORD CORRODED AT FWD HORIZONTAL FLANGE BS 227, LBL 3. REPAIRED CHORD PER SWA EA.

Part: SKIN — CRACKED (BS 967 S22L) · airframe 71,202 hrs · 68,349 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 22L. REPAIRED SKIN PER SWA EA.

Part: LENS — MISSING (CABIN) · airframe 71,157 hrs · 68,313 cycles

OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING AT FWD CABIN. INSTALLED LIGHT LENS PER MM.

Part: MODULE — OVERHEATED (COCKPIT) · airframe 70,739 hrs · 68,015 cycles

DIVERSION, AFTER LEVEL OFF AT 30000, NOTICED STRONG ELECTRICAL ODOR BUT NO SMOKE. COMPLIED WITH QRH, SYSTEMS NORMAL. FOUND OVERHEAD SLAT INDICATION MODULE WITH BURNT SMELL AT LIGHT PLATE. REMOVED AND REPLACED INDICATION MODULE PER MM.

Part: SKIN — CRACKED (BS 502D S16L) · airframe 70,546 hrs · 67,874 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 502D, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 516C S15L) · airframe 70,546 hrs · 67,874 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 516C, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 316 S20R) · airframe 70,361 hrs · 67,739 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 316, STR 20R. REPAIRED SKIN PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,909 hrs · 66,592 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME AT FWD CARGO DOOR CUTOUT FWD WEB CRACKED, UPPER CORNER NR 5 DOOR STOP. REPAIRED FRAME WEB PER ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,909 hrs · 66,592 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CORRODED AT AFT CARGO DOOR CUTOUT LOWER AFT CORNER, BS 843, RBL 34. REPAIRED SKIN PER SRM.

Part: SUPPORT — CRACKED (L1 DOOR HINGE) · airframe 68,909 hrs · 66,592 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR UPPER HINGE SUPPORT CRACKED. REPAIRED HINGE SUPPORT PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,909 hrs · 66,592 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,909 hrs · 66,592 cycles

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

Part: STRINGER — CRACKED (BS 501 S14R) · airframe 68,909 hrs · 66,592 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 501, STR 14R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: BRACKET — CORRODED (L1 DOOR SLIDE) · airframe 68,909 hrs · 66,592 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT EVAC SLIDE CORRODED AT AFT GIRT BAR BRACKET. REMOVED AND REPLACED AFT GIRT BAR BRACKET PER MM.

Part: STRUCTURE — CRACKED (LH FORE FLAP) · airframe 68,909 hrs · 66,592 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING T/E FLAPS INBOARD FORE FLAP CRACKED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 277 S20R) · airframe 68,909 hrs · 66,592 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 20R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BRACKET — CRACKED (R2 DOOR SLIDE) · airframe 68,909 hrs · 66,592 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT EVAC SLIDE FWD MOUNTING BRACKET CRACKED. REMOVED AND REPLACED FWD BRACKET PER SRM.

Part: DOOR FRAME — CRACKED (FWD CARGO DOOR) · airframe 68,909 hrs · 66,592 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR UPPER FRAME CRACKED AT AFT HINGE UPPER BOLTS. REMOVED AND REPLACED FRAME SECTION PER SRM AND SB.

Part: SHEAR TIE — CRACKED (BS 967) · airframe 68,909 hrs · 66,592 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 967, ABOVE R2 DOOR. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: HOOK — LOOSE (R2 DOOR SLIDE) · airframe 68,909 hrs · 66,592 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT EVAC SLIDE AFT HOOK LOOSE. REMOVED AND REPLACED R2 DOOR EVAC SLIDE AFT HOOK PER MM.

Part: SKIN — CRACKED (BS 464 S17L) · airframe 68,619 hrs · 66,370 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 464, STR 17L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 500 S23R) · airframe 68,619 hrs · 66,370 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 68,619 hrs · 66,370 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,301 hrs · 66,125 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 700, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,301 hrs · 66,125 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 26L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 68,301 hrs · 66,125 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,301 hrs · 66,125 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503A, STR 16L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,301 hrs · 66,125 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN BULGED AT BS 517, STR 26R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,301 hrs · 66,125 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 932 TO BS 943, STR 22R TO STR 24R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,301 hrs · 66,125 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 396, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,301 hrs · 66,125 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 582, STR 10R. REPAIRED SKIN PER SWA EA.

Part: MOUNT — BROKEN (EMERGENCY LIGHT) · airframe 67,950 hrs · 65,857 cycles

DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHT BASE BATTERY MOUNT BROKEN. REMOVED AND REPLACED BATTERY BASE PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,950 hrs · 65,857 cycles

DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT DOOR LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,720 hrs · 65,675 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 24L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,720 hrs · 65,675 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 368, STR 25L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,720 hrs · 65,675 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 21L. REPAIRED SKIN PER SWA EA & SRM.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 67,443 hrs · 65,468 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NLG W/W LEFT FWD PRESSURE SIDE WEB CRACKED AT BS 251.625, WL 177. REPAIRED WEB PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,336 hrs · 65,385 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 700, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,336 hrs · 65,385 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,336 hrs · 65,385 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 446, STR 26L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 450) · airframe 67,067 hrs · 65,155 cycles

DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 450, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 324) · airframe 66,844 hrs · 64,966 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 324, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 863) · airframe 66,844 hrs · 64,966 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 863, STR 16L. REPAIRED SKIN PER SWA EA & SRM.

Part: DOOR FRAME — CRACKED (AFT CARGO) · airframe 66,844 hrs · 64,966 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR FWD FRAME CRACKED AT BALANCE CABLE PULLEY MOUNT BRACKET. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,888 hrs · 64,180 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 861 TO BS 864, ABOVE STR 16L. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (LT OVERWING EXIT) · airframe 65,494 hrs · 63,858 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,934 hrs · 63,418 cycles

FOUND FUSELAGE SKIN AT BS 450, STRINGER 16R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,947 hrs · 62,644 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STRINGER 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,947 hrs · 62,644 cycles

DURING SCHEDULED C1 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS BETWEEN 937 & BS 947, STRINGER 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,947 hrs · 62,644 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 908, STRINGER 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,947 hrs · 62,644 cycles

DURING SCHEDULED C1 CHECK, FOUND 3 EA FUSELAGE SKIN CRACKS BETWEEN BS 450 & BS 500A, STRINGER 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,947 hrs · 62,644 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 271, STRINGER 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,106 hrs · 61,967 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 517, STRINGER 12R, BS 520, STRINGER 12R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,117 hrs · 61,976 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 510, STRINGER 15R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,597 hrs · 61,542 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 813, STRINGER18L, CRACKED. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,597 hrs · 61,542 cycles

DURING SCHEDULED SERVICE CHECK, FOUND STRINGER TIE CLIP AT BS 807, STRINGER 18L, CRACKED. REMOVED AND REPLACED STRINGER TIE PER SRM.

Part: STRUCTURE — DELAMINATED (T/E FLAP) · airframe 62,572 hrs · 61,519 cycles

DURING SCHEDULED A1 CHECK, FOUND RIGHT WING T/E OUTBOARD AFT FLAP, DELAMINATED. REMOVED AND REPLACED RIGHT OUTBOARD AFT FLAP PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 62,393 hrs · 61,387 cycles

L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,163 hrs · 61,193 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 1000, STRINGER 20L, CRACKED. REPAIRED SKIN PER SRM.

Part: MOUNT — CORRODED (HORIZONTAL STAB) · airframe 61,202 hrs · 60,444 cycles

DURING SCHEDULED D CHECK, FOUND CORROSION AT HORIZONTAL STABILIZER RIGHT CENTER SECTION HINGE HOUSING UPPER MOUNT LUG. REPAIRED MOUNT LUG PER ER.

Part: CREASE BEAM — CORRODED (AFT PAX CABIN) · airframe 61,202 hrs · 60,444 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 776, LBL 68, WL 208. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,202 hrs · 60,444 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 270, BETWEEN STRINGERS 15L AND 14L. REPAIRED SKIN CRACK PER SRM.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 61,202 hrs · 60,444 cycles

DURING SCHEDULED D CHECK, FOUND AFT CARGO DOOR EXTERNAL SKIN CRACKED AT UPPER AFT CORNER OF HANDLE CUTOUT. REPAIRED PER SRM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 61,201 hrs · 60,444 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT BS 847, WL 148, RBL10. REPAIRED STRAP PER BFG ER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 61,201 hrs · 60,444 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER 26L CRACKED AT BS 1020. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,201 hrs · 60,444 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, WL 202, RT SIDE. REPAIRED FRAME BFG ER.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 61,202 hrs · 60,444 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL STAB ATTACH FITTING FRONT SPAR LEFT AND RIGHT AFT BODY CLEVICES CORRODED. REPAIRED FITTING PER BFG ER.

Part: WEB — CORRODED (FUSELAGE) · airframe 61,202 hrs · 60,444 cycles

DURING SCHEDULED D CHECK, FOUND FLOOR WEB CORRODED AT BS 1016, LBL 5, WL 208. REPAIRED FLOOR WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,202 hrs · 60,404 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 847, LBL 17, WL 148. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,202 hrs · 60,444 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 44, WL 208, BS 986.5, LBL 12, WL 208, BS 986.5, LBL 13.5, BS 986, LBL 14, WL 209, BS 986, LBL 44, WL 209, BS 986.5 LBL 16, WL 210, BS 947.5, RBL 11, WL 208, BS 947.5, RBL 15 WL 208, BS 947, RBL 8, WL 208. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,202 hrs · 60,444 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CORRODED AT BS 986.5, RBL 46, WL 208. REPAIRED FRAME PER SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 61,202 hrs · 60,444 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM SPLICE CORRODED AT BS 290, RBL 53. REMOVED AND REPLACED CREASE BEAM SPLICE SECTION PER SRM.

Part: WEDGE — DELAMINATED (RT WING SLAT) · airframe 61,202 hrs · 60,444 cycles

DURING SCHEDULED D CHECK, FOUND NR 5 L/E SLAT T/E WEDGE INBOARD END DELAMINATED. REPAIRED WEDGE PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 61,202 hrs · 60,444 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON STRINGER CLIP BS 847, RBL 13.8. REPAIRED STRINGER CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,202 hrs · 60,444 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CORRODED AT BS 807, RBL 4. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,202 hrs · 60,444 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 847 LBL 3. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,202 hrs · 60,444 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 727, BS 767, BS 787 AND LBL 9, LBL 18, LBL 4 THROUGH RBL 4. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,202 hrs · 60,444 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 859, RBL 3 AND LBL 17. REPAIRED CORROSION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 61,202 hrs · 60,444 cycles

DURING SCHEDULED D CHECK, FOUND CRACK IN STRINGER 7L BS 1012. REPAIRED STRINGER PER SRM.

Part: WEDGE — DELAMINATED (RT WING TE FLAP) · airframe 61,202 hrs · 60,444 cycles

DURING SCHEDULED D CHECK, FOUND NR 5 T/E FLAP WEDGE OUTBOARD END DELAMINATED. REPAIRED WEDGE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,197 hrs · 60,443 cycles

DURING SCHEDULED C2 CHECK, FOUND 8 EA FUSELAGE SKIN CRACKS AT BS 487, STR 26L, AT BS 803, STR 20L, AT BS 970, STR 24L, AT BS 910, STR 23R, AT BS 759, STR 18R, AT BS 933, STR 23R, AT BS 685, STR 10R, AND AT BS 580, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,669 hrs · 60,021 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 847 AT STR 16L AND BS 945 AT STR 21L. REPAIRED SKIN PER SRM.

Part: STRIP — LOOSE (CABIN) · airframe 60,599 hrs · 59,960 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE IN CABIN. SECURED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,999 hrs · 59,481 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 6, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,999 hrs · 59,481 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 360, STR 26R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,353 hrs · 58,968 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED ( 3 EA ) AT STR 26L, BS 395, BS 430 & BS 455. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 58,811 hrs · 58,547 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,474 hrs · 58,252 cycles

DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 848 STR 16L AND BS 972 STR 21L. REPAIRED FUSELAGE SKIN CRACKS PER SRM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 57,722 hrs · 57,667 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11139-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHINGS AT NR 1 ELEV TAB HINGE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,572 hrs · 57,543 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 18L, BS 485 AND BS 492. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,067 hrs · 57,111 cycles

AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,929 hrs · 56,997 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 375, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,502 hrs · 56,646 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 500D PLUS 4, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,502 hrs · 56,646 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 4, ABOVE STR 16R. REPAIRED SKIN PER SRM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 56,111 hrs · 56,315 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NR 4 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED NR 4 GROUND SPOILER PER MM.

Part: ROD END — WORN (ELEVATOR TAB) · airframe 56,008 hrs · 56,226 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH LT AND RT ELEVATOR TAB PUSH ROD ENDS WORN. REMOVED AND REPLACED TAB ROD ENDS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,126 hrs · 55,562 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (1.9 INCHES LONG), BS 727E, STRINGER 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,126 hrs · 55,562 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (3 INCHES LONG), BS 500C, STRINGER 15R. REPAIRED SKIN PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,139 hrs · 54,721 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 270, BETWEEN STR 9L & 10L. REPAIRED SKIN PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 54,139 hrs · 54,721 cycles

DURING SCHEDULED 1/4D CHECK, FOUND TIE CLIP CRACKED AT BS 663, STR 4R. REMOVED AND REPLACED TIE CLIP PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 54,139 hrs · 54,721 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIPS CRACKED ( 2 EA ) AT BS 400, STR 4R, BS 767, STR 11L. R&R TIE CLIP PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 54,139 hrs · 54,721 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: FRAME — CRACKED (AFT CARGO) · airframe 54,139 hrs · 54,721 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 927, BBL 0. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,139 hrs · 54,721 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAMES CRACKED ( 2 EA ) AT BS 500A & BS 500B, STR 14R. REPAIRED FRAMES PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 53,968 hrs · 54,582 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REINSTALLED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,507 hrs · 54,202 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT STRINGER 10L, BS 500A & BS 400. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,507 hrs · 54,202 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT STRINGER 10R, BS 500C & BS 727B. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,507 hrs · 54,202 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 19L. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 53,507 hrs · 54,202 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING AT FWD CABIN CEILING. INSTALLED LENS PER MM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 53,319 hrs · 54,042 cycles

DURING SCHEDULED RON CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM.

Part: STIFFENER — CRACKED (WING) · airframe 52,745 hrs · 53,554 cycles

DURING SCHEDULED RON CHECK, FOUND WING CENTER SECTION REAR SPAR ZEE STIFFENER CRACKED AT LBL 6.15. REPAIRED STIFFENER PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,588 hrs · 53,419 cycles

DURING SCHEDULED C4 CHECK, FOUND 4 INCH EXTERNAL FUSELAGE SKIN CRACK AT BS 927, STR 21R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,588 hrs · 53,419 cycles

DURING SCHEDULED C4 CHECK, FOUND 1.25 EXTERNAL FUSELAGE SKIN CRACK AT BS 927, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,588 hrs · 53,419 cycles

DURING SCHEDULED C4 CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACKS AT BS 500B, STR 10R, 1 IN LENGTH & BS 500C, STR 10R, 3 IN LENGTH. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,588 hrs · 53,419 cycles

DURING SCHEDULED C4 CHECK, FOUND 6 EXTERNAL FUSELAGE SKIN CRACK AT BS 420, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,588 hrs · 53,419 cycles

DURING SCHEDULED CHECK, FOUND 3.25 EXTERNAL FUSELAGE SKIN CRACK AT BS 787, STR 18L. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 52,588 hrs · 53,419 cycles

DURING SCHEDULED C4 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 52,588 hrs · 53,419 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 1 L/E SLAT LOWER SKIN CRACKED AT 2 FASTENER HOLES, AFT ROW, OUTBD MAIN TRACK. REPAIRED SLAT SKIN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,588 hrs · 53,419 cycles

DURING SCHEDULED C4 CHECK, FOUND 2.5 EXTERNAL FUSELAGE SKIN CRACK AT BS 727B, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,588 hrs · 53,419 cycles

DURING SCHEDULED C4 CHECK, FOUND 5 EXTERNAL FUSELAGE SKIN CRACK AT BS 500, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,784 hrs · 52,756 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 1.5 EXTERNAL FUSELAGE SKIN CRACK, LT SIDE, AT BS 518, WL 250. REPAIRED SKIN PER SRM.

Part: RETAINER — LOOSE (SERVICE DOOR) · airframe 57,606 hrs · 52,597 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY RETAINER LOOSE. SECURED RETAINER PER MM.

Part: SLIDE — OUT OF ADJ (AFT SERVICE DOOR) · airframe 51,454 hrs · 52,463 cycles

AFT SVC EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. REINSTALLED SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (AFT SERVICE DOOR) · airframe 51,419 hrs · 52,435 cycles

AFT SVC EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 51,389 hrs · 52,410 cycles

LOWER AFT EMERGENCY FLASHLIGHT DOES NOT SHOW CHARGE. REMOVED AND REPLACED BATTERY PER MM.

Part: FRAME — CRACKED (BULKHEAD) · airframe 50,888 hrs · 51,991 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND CRACKED BS 178 VERT CHORD, WL 184, LBL 5.7. REPAIRED CHORD PER SRM.

Part: SLIDE — LOOSE (PAX DOOR) · airframe 50,785 hrs · 51,888 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL A FEW INCHES OUT OF CONTAINER AS DOOR WAS OPENING. REINSTALLED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,402 hrs · 51,540 cycles

DURING WALK AROUND CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 505, STRINGER 10R, BS 734, STRINGER 20R AND BS 525, STRINGER 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,272 hrs · 51,426 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2, 3 INCH LONG CRACKS AT FUSELAGE EXTERNAL SKIN, BS 500 AND BS 887, ABOVE STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 500)

DURING SCHEDULED C4 CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED, BS 520, STRINGER 10R AND BS 500, STRINGER 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, AFT ENTRY DOOR UPPER AFT CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 727 & 913)

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE EXTERNAL SKIN 2 EACH CRACKS, BS 727+7, STRINGER 20L, AND BS 913, STRINGER 19R.. REPAIRED SKIN PER SRM.

Part: BRACKET — LOOSE (SERVICE DOOR)

DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKETS LOOSE. TIGHTENED AND SECURED BRAKETS PER MM.

Part: SKIN — CRACKED (BS 747&727)

DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS, BS 747 AND BS 727D, AT STRINGER 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 500)

DURING SCHEDULED RON, FOUND 4 EACH CRACKS ON FUSELAGE SKIN, BS 500A +4, AND BS 500C +6, STRINGER 10L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR UPPER CENTER CUT OUT STUB FRAME CRACKED. REPAIRED STUB FRAME PER SWA RA NR 1-353-2133.

Part: ANGLE — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND 2 EA CHORDS CRACKED AT LBL AND RLB 28.5, BS 178. REPAIRED PER SRM.

Part: TEE — CRACKED (CARGO DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND LOWER T-CHORD CRACKED THIRD FROM AFT END, FWD CARGO DOOR. REMOVED DOOR, REPAIRED AND REINSTALLED DOOR PER SRM AND MM.

Part: SKIN — CRACKED (BS 272-274)

DURING SCHEDULED 1/2D CHECK, FOUND A 2 INCH LONG CRACK ON FUSELAGE OUTER SKIN, BS 272 TO 274 STR 16L. REPAIRED SKIN PER SRM.

Part: KEEL BEAM — CORRODED (BS 545.9)

DURING SCHEDULED 1/2D CHECK, FOUND INTERGRANULAR CORROSION ON KEEL BEAM, RT O/B SIDE BS 545.9. REPAIRED BEAM PER SWA RA NR 1-353-2044.

Part: WEB — CRACKED (BS 665)

DURING SCHEDULED 1/2D CHECK, FOUND THRU EDDY CURRENT INSPECTION A CRACK ON BEADED WEB AT BS 665, RBL 42 AT CABIN FLOOR. REPAIRED WEB PER SWA RA NR 1-353-2034.

Part: FRAME — CRACKED (PAX DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND THRU EDDY CURRENT INSPECTION, CRACKED UPPER FRAME ON AFT ENTRY DOOR CUTOUT FOR DOOR ASSIST HANDLE. REMOVED AND REPLACED FRAME PER SRM.

Part: FRAME — CRACKED (BS 616)

DURING SCHEDULED 1/2D CHECK, FOUND BELTFRAME CRACKED AT BS 616 LT SIDE CABIN FLOOR. REPAIRED PER SWA RA NR1-353-2042.

Part: FRAME — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND AFT SERVICE DOOR UPPER FWD FRAME CRACKED AT ASSIST HANDLE. REPAIRED PER SRM.

Part: STRINGER — CRACKED (BS 360)

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 14L CHANNEL CRACKED AT STUB FRAME BS 360. REPAIRED PER SRM.

Part: CHANNEL — CRACKED (BS 360)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED U-CHANNEL AT STR 15L, BS 360. REPAIRED CHANNEL PER SRM.

Part: CLIP — CRACKED (BS 663)

DURING SCHEDULED 1/2D CHECK, FOUND 4 STRINGER CLIPS CRACKED AT BS 663, STR 12R AND 10L, BS 767, STR 13R, AND BS 787, STR 11L. REMOVED AND REPLACED CLIPS PER SRM.

Part: SKIN — CRACKED (BS 780-787)

DURING SCHEDULED 1/2D CHECK, FOUND 2 CRACKS ON EXTERNAL FUSELAGE SKIN BS 787 STR 19L AND ON BS 780 STR 18L. REPAIRED CRACKS PER SRM.

Part: SKIN — CRACKED (BS 326)

DURING SCHEDULED 1/2D CHECK, FOUND A 1.5 INCH VERTICAL CRACK ON EXTERNAL FUSELAGE SKIN, BS 312 STR 19R. REPAIRED PER SRM.

Part: FRAME — CRACKED (CARGO DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR FWD, LOWER FRAME CRACKED BELOW UPLATCH. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (PAX DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND AFT ENTRY DOOR UPPER HINGE CUTOUT CRACKED AT LOWER CORNER (VERIFIED WITH EDDY CURRENT INSPECTION). REPAIRED SKIN CUT OUT PER SWA RA NR 1-352-0323.

Part: FLOORBEAM — CRACKED (BS 663)

DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER T CHORD CRACKED AT BS 663 BL 0. REPAIRED PER SWA RA NR 1-357-0648.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND 4 CRACKS AT BS 178 BULKHEAD WEB BETWEEN LBL 9-RBL 7. REPAIRED PER SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND 5 CRACKS AT BS 178 BULKHEAD WEB BETWEEN LBL 32 AND RBL 5. REPAIRED PER SRM.

Part: WEB — CRACKED (BS 664)

DURING SCHEDULED 1/2D CHECK, FOUND THRU EDDY CURRENT INSPECTION A CRACK IN BEADED WEB AT BS 664 LBL 32. REPAIRED PER SWA RA NR 1-353-2033.

Part: FLOORBEAM — CRACKED (BS 787)

DURING SCHEDULED 1/2D CHECK, FOUND CRACK ON FLOORBEAM AROUND NET TIE DOWN HOLE, BS 787 RBL 14. REPAIRED PER SRM.

Part: FLOORBEAM — CORRODED (BS 727)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM AROUND SCREW HOLE, BS 727 RBL 8. REPAIRED PER SRM.

Part: STRINGER — CORRODED (BS 868)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON STRINGER 25L UPPER FLANGE, BS 868. REPAIRED PER SRM.

Part: CHORD — CRACKED (BS 180)

DURING SCHEDULED 1/2D CHECK, FOUND T-CHORD CRACKED AT BS 180, RBL 25, WL 207. REPAIRED CHORD PER SRM.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND APPROXIMATE A 2.5 INCH CRACK IN FUSELAGE SKIN ON AFT LOWER CORNER OF FWD SERVICE DOOR CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 753)

DURING SCHEDULED SP VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 753 ABOVE S20L. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (CARGO COMPT)

DURING SCHEDULED BC4 CHECK, FOUND CRACKED FWD CARGO INTERCOSTAL. REMOVED AND REPLACED PER BOEING MM.

Part: SKIN — CRACKED (R2 DOORWAY)

DURING SCHEDULED BC1 CHECK, FOUND R2 DOOR UPPER FUSELAGE HINGE CUT-OUT HAS .250 LONG CRACK IN RADIUS. REPAIRED PER SWA RA NR 1-353-1807.

Part: SKIN — CORRODED (BS 1013)

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN BLENDED BEYOND LIMITS AT BS 1013 RT, 1 BELOW SKIN LAP. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 482)

DURING SCHEDULED BC2 CHECK, FOUND FUSELAGE SKIN CRACKED 2 PLACES JUST ABOVE UPPER LAP JOINT AT BS 482. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 785)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 785, ABOVE S20R. REPAIRED PER BOEING SRM.

Part: FUSE — FAILED (CABIN)

DURING SCHEDULED BC3 CHECK, FOUND CABIN BULLNOSE EMERGENCY EXIT LIGHTS ABOVE ROWS 22 AND 18 INOP. REPLACED BULB SOCKET AND BATTERY PACK FUSE PER BOEING M/M.

Part: BULB — FAILED (COCKPIT)

DURING SCHEDULED BC3 CHECK, FOUND COCKPIT EMERGENCY LIGHTING VERY DIM. RELAMPED PER BOEING M/M.

Part: LAMP — INOPERATIVE (CABIN)

DURING SCHEDULED BC3 CHECK, FOUND CABIN AFT RED EMERGENCY FLOOR TRACK LIGHT INOP. REPLACED 2 LAMPS PER BOEING M/M.

Part: AIR DISTR — ODOR (CABIN)

NOTED ELECTRICAL ODOR IN MID CABIN AREA. INSPECTED ELECTRICAL WIRING AND NOTED NO DEFECTS PER BOEING M/M.

Part: SKIN — DAMAGED (BS 259.5)

DURING SCHEDULED SC-CHECK, FOUND SKIN DAMAGED AT BS 259.5 UNDER GUSSET FITTING IN UPPER NOSE GEAR AREA. INSTALLED WEB REPAIR PER BOEING SRM.

Part: SKIN — CRACKED (BS 800)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800 WL 205. REPAIRED PER BOEING SRM.