N338SW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,527 hrs · 66,816 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 75,243 hrs · 66,604 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT OF CASE, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER MT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 74,971 hrs · 66,394 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,971 hrs · 66,394 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,971 hrs · 66,394 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 907, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE IAW ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,971 hrs · 66,394 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE IAW ER AND EA.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 74,971 hrs · 66,394 cycles

DURING SCHEDULED SPV CHECK, FOUND FAIL SAFE CHORD CRACKED AT BS 927, STR 23L. REPAIRED CHORD PER ER AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,971 hrs · 66,394 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 867, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE IAW ER AND EA.

Part: CONNECTOR — LOOSE (CABIN) · airframe 74,971 hrs · 66,394 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT EMERGENCY EXIT LIGHT SWITCH LOOSE. SECURED CONNECTOR PER WDM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,970 hrs · 66,397 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 360, STR 20R. REPAIRED FRAME IAW ER AND EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 74,970 hrs · 66,397 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME STRINGER SPLICE CORRODED AT BS 911, STR 18L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,971 hrs · 66,394 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 74,971 hrs · 66,394 cycles

DURING SCHEDULED SPV CHECK, FOUND RT EXTERIOR EMERGENCY EXIT LIGHTS INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 74,971 hrs · 66,394 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EXTERIOR EMERGENCY EXIT LIGHTS INOP. RELAMPED LIGHT PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,971 hrs · 66,394 cycles

DURING SCHEDULED SPV CHECK FOUND, STRINGER CRACKED AT BS 470, STR 20L. REMOVED AND REPLACED STRINGER IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,971 hrs · 66,394 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 74,971 hrs · 66,394 cycles

DURING SCHEDULED SPV CHECK, FOUND RT CREASE BEAM CHORD CRACKED AT BS 639, RBL 65. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,971 hrs · 66,394 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 911 TO BS 911.5, STR 21L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,971 hrs · 66,394 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 760 TO BS 760.5, STR 19R. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 74,866 hrs · 66,309 cycles

LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 74,866 hrs · 66,309 cycles

L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 74,774 hrs · 66,243 cycles

DURING SCHEDULED MV3 CHECK FOUND, L2 DOOR EMERGENCY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED CHARGER ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,676 hrs · 66,165 cycles

DURING SCHEDULED M1 CHECK, FOUND, RT EEPLS INOP AT ROW 16. RELAMPED PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 74,298 hrs · 66,301 cycles

FOUND L1 DOOR EMERGENCY EXIT SIGN BROKEN. SECURED LIGHT AND INSTALLED NEW LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,446 hrs · 65,983 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 3. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,330 hrs · 65,891 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 500C+15, STR 8R. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,330 hrs · 65,891 cycles

DURING SCHEDULED CV CHECK, FOUND STRINGER CRACKED AT BS 360, STR 5R. REPAIRED STRINGER PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,330 hrs · 65,891 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 365, STR 15R. REPAIRED SKIN PER EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 73,986 hrs · 65,623 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,433 hrs · 65,202 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 947+14, STR 21L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,433 hrs · 65,202 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 500B, STR 15L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,433 hrs · 65,202 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500B, STR 15L. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 73,433 hrs · 65,202 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,433 hrs · 65,202 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 967, STR 21L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (BS 967 S21L) · airframe 76,641 hrs · 67,647 cycles

SKIN CRACKED AT BS 967 + 14, S21L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,431 hrs · 65,201 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 967+14, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,431 hrs · 65,201 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 947+14, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,431 hrs · 65,201 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 500B, STR 15L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,035 hrs · 64,896 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 13L. REPAIRED FRAME PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,035 hrs · 64,896 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED BETWEEN BS 413 TO BS 416, STR 19L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,035 hrs · 64,896 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 8R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,035 hrs · 64,896 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 73,035 hrs · 64,896 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME SPLICE CRACKED AT BS 500D, STR 13L. REPAIRED SPLICE PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,035 hrs · 64,896 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 762, STR 19L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,035 hrs · 64,896 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 5L. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,035 hrs · 64,896 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 2R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 73,035 hrs · 64,896 cycles

DURING SCHEDULED 22Y CHECK, FOUND LOWER CHORD CRACKED AT BS 227.8, BL 0. REPAIRED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,035 hrs · 64,896 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,035 hrs · 64,896 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 10R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,035 hrs · 64,896 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD CARGO DOOR SKIN CUTOUT CRACKED AT LOWER AFT CORNER BEAR STRAP. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,035 hrs · 64,896 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 10R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,035 hrs · 64,896 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,035 hrs · 64,896 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,035 hrs · 64,896 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,035 hrs · 64,896 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 328, STR 20R. REPAIRED FRAME PER SRM.

Part: FLAP — PUNCTURED (LT WING) · airframe 73,035 hrs · 64,896 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING I/B FORE FLAP PUNCTURED. REPAIRED FORE FLAP PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 73,035 hrs · 64,896 cycles

DURING SCHEDULED 22Y CHECK, FOUND EMERGENCY EXIT LIGHT AFT OF G1 GALLEY BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,035 hrs · 64,896 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, BETWEEN STR 11L TO STR 12L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,677 hrs · 64,616 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 731B, STR 14L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,677 hrs · 64,616 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 504B, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,631 hrs · 64,578 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 504B, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,631 hrs · 64,578 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 731B, STR 14L. REPAIRED SKIN PER SRM.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 71,922 hrs · 64,017 cycles

DIVERSION / DECLARED EMERGENCY. CABIN ALTITUDE WARNING HORN ACTIVATED AT FL 340 WHOLE IN CRUISE. CABIN ALTITUDE REACHED 10,000 FEET. OXYGEN MASKS NEVER DROPPED DUE TO AN IMMEDIATE EMERGENCY DESCENT DOWN TO 10,000 FEET MSL. REMOVED AND REPLACED OUTFLOW VALVE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,737 hrs · 64,418 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT BULB INOP. RELAMPED PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 71,737 hrs · 64,418 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,737 hrs · 64,418 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT BULB INOP. RELAMPED PER MM.

Part: LENS — LOOSE (CABIN) · airframe 71,737 hrs · 64,418 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND EMERGENCY EXIT LIGHT LENS ABOVE FLT DECK THRESHOLD LOOSE. SECURED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,737 hrs · 64,418 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT BULB INOP. RELAMPED PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,595 hrs · 63,028 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500B, STR 20L. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,595 hrs · 63,028 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500B, STR 20R. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,595 hrs · 63,028 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,595 hrs · 63,028 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500B, STR 20R. REPAIRED FRAME PER ER.

Part: WIRE — BROKEN (CABIN) · airframe 70,427 hrs · 62,912 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT F/A'S EGRESS LIGHT TEST SWITCH INOP. REPAIRED LIGHT TEST SWITCH WIRE PER WDM & MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 70,417 hrs · 62,906 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR ASSY LOOSE. SECURED SLIDE PER MM.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 70,256 hrs · 62,781 cycles

L2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,256 hrs · 62,781 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 503, STR 16R. REPAIRED SKIN PER EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 70,254 hrs · 62,780 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,254 hrs · 62,780 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 475, STR 16R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,254 hrs · 62,780 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 468, STR 16R. REPAIRED SKIN PER EA.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 69,765 hrs · 62,406 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,341 hrs · 61,388 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED BETWEEN BS 344 TO BS 360. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,267 hrs · 61,337 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 23. REMOVED AND REPLACED BULB PER MM.

Part: WIRE — DAMAGED (RT WING) · airframe 67,636 hrs · 60,893 cycles

IN FLT SHUTDOWN / DIVERSION / DECLARED EMERGENCY. NR 2 ENG FLAMED OUT, UNABLE TO RESTART. FOUND NR 2 ENG FUEL SHUT-OFF VALVE WIRING DAMAGED AT BUNDLE W804. REPAIRED WIRING PER WPM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 667, LBL 24.8. REPAIRED BEAM PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT OVERWING EXIT. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 673, LBL 24.8. REPAIRED BEAM PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND R1 EMERGENCY EXIT OVERHEAD DOOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND NLG WHEEL WEB CRACKED AT LBL 7.75. REPAIRED WEB PER SWA ACO.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT KEEL BEAM CORRODED AT STA 663 TO 727. REMOVED AND REPLACED BEAM PER SWA EA.

Part: BEAM — CORRODED (FUSELAGE) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT BEAM WEB CORRODED AT STA 500C TO 500D. REPAIRED WEB BEAM PER SRM.

Part: SKIN — CRACKED (FWD CARGO DOOR) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FWD CARGO DOOR SKIN CRACKED AT HANDLE CUTOUT. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (AFT CARGO DOOR) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT CARGO DOOR LOWER AFT FRAME CRACKED. REPAIRED FRAME PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FWD DOOR CUTOUT AFT FRAME CRACKED AT LOWER STOP. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (BS 747 S8R) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500C S8R) · airframe 67,043 hrs · 60,473 cycles

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

Part: FRAME — CRACKED (BS 727B S8L) · airframe 67,043 hrs · 60,473 cycles

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

Part: FRAME — CRACKED (BS 787 S8R) · airframe 67,043 hrs · 60,473 cycles

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

Part: FRAME — CRACKED (BS 907 S8L) · airframe 67,043 hrs · 60,473 cycles

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

Part: STRINGER — CRACKED (BS 1010 S4L) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 4L CRACKED AT BS 1010. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 303 S10L) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 303, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 520 S8R) · airframe 67,043 hrs · 60,473 cycles

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

Part: STRINGER CLIP — CRACKED (BS 400 S27L) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 27L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S9L) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S15L) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 291.5 S11L) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 291.5, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S11L) · airframe 67,043 hrs · 60,473 cycles

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

Part: STRINGER CLIP — CRACKED (BS 277 S15R) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 294.5 S13R) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294.5, STR 13R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 663 S10L) · airframe 67,043 hrs · 473 cycles

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

Part: ANGLE — CRACKED (BS 178 BULKHEAD) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FWD BULKHEAD ANGLE CRACKED AT BS 178, LBL 28. REMOVED AND REPLACED ANGLE PER SRM.

Part: FRAME — CRACKED (BS 663 S2L) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663.75, STR 2L, STR 2R AND STR 3R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663 S4R) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (BS 440-500A) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 440 TO BS 500A, LBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: SKIN — CRACKED (BS 291) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT FWD SERVICE DOOR BS 291.5, WL 232.5. REPAIRED SKIN PER SWA EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOOR WEB CRACKED AT BS 247, RBL 24. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 400 AND BS 420, STR 17L. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,043 hrs · 60,473 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 291.5, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 66,191 hrs · 59,861 cycles

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

Part: SIGN — OUT OF POSITION (CABIN) · airframe 66,105 hrs · 59,797 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN FELL OFF. INSTALLED SIGN PER MM.

Part: FUSE — FAILED (MLG W/W) · airframe 65,465 hrs · 59,342 cycles

AIR TURNBACK, AFTER TAKEOFF LEADING EDGE FLAPS TRANSIT LIGHT ILLUMINATED, TRANSIT LIGHT INDICATED ON APPROACH. REMOVED AND REPLACED LEADING EDGE RETRACT FUSE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,261 hrs · 59,175 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 424, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,261 hrs · 59,175 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 512D, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SLAT — CRACKED (LT WING) · airframe 65,261 hrs · 59,175 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,813 hrs · 58,831 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 480, STR 16R. REPAIRED SKIN PER SRM.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 64,307 hrs · 58,440 cycles

DURING SCHEDULED RON CHECK, L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 64,307 hrs · 58,440 cycles

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

Part: ROD END — SEIZED (ELEVATOR TAB) · airframe 64,307 hrs · 58,440 cycles

DURING SCHEDULED C3 CHECK, FOUND RIGHT OUTBOARD ELEVATOR TAB PUSHROD AFT ROD END SEIZED. REMOVED AND REPLACED PUSHROD ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 64,307 hrs · 58,440 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,307 hrs · 58,440 cycles

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

Part: WINDOW — ARCED (COCKPIT) · airframe 64,048 hrs · 58,243 cycles

AT FL 350 FLIGHT DECK L1 WINDOW ARCING. REMOVED AND REPLACED WINDOW PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,379 hrs · 57,708 cycles

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

Part: SLAT — DELAMINATED (RT WING) · airframe 63,379 hrs · 57,708 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT UPPER OUTBOARD END. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,379 hrs · 57,708 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 20R. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,339 hrs · 57,677 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT BS 792, STR 24R. REPAIRED FRAME PER ACO.

Part: STRINGER CLIP — CRACKED (BS 500 S16R) · airframe 63,339 hrs · 57,677 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,339 hrs · 57,677 cycles

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

Part: SKIN — CRACKED (BS 500B S15R) · airframe 62,627 hrs · 57,141 cycles

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

Part: SKIN — CRACKED (BS 434 S16R) · airframe 62,477 hrs · 57,032 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 434, STR 16R. REPAIRED SKIN PER SRM & EA.

Part: SKIN — CRACKED (BS 727E S18R) · airframe 62,477 hrs · 57,032 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18R. REPAIRED SKIN PER SRM & EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 62,207 hrs · 56,807 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,197 hrs · 56,801 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 450, STR 17R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 62,197 hrs · 56,801 cycles

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

Part: SKIN — CRACKED (BS 450 S17R) · airframe 62,175 hrs · 56,785 cycles

FOUND FUSELAGE SKIN CRACKED AT BS 450, STR 17R. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 62,082 hrs · 56,712 cycles

AFT CABIN EMERGENCY FLASHLIGHT HAS LOW BATTERY. REMOVED AND REPLACED BATTERY PER MM.

Part: BOLT — WORN (ELEVATOR TAB) · airframe 61,579 hrs · 56,331 cycles

DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT TAB NR 1 HINGE BOLT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,614 hrs · 55,574 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,614 hrs · 55,574 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 59,737 hrs · 54,892 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CABIN EMERGENCY EXIT SIGN LENS MISSING. INSTALLED SIGN LENS PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 59,683 hrs · 54,847 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,873 hrs · 54,252 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CABIN CENTER EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 58,873 hrs · 54,252 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RIGHT WING OUTBD T/E AFT FLAP INBOARD T/E DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: CREASE BEAM — CORRODED (BS 360-380) · airframe 58,873 hrs · 54,252 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 360 TO BS 380, STR 17R. REPAIRED CREASE BEAM PER SRM.

Part: SKIN — CRACKED (BS 747) · airframe 58,873 hrs · 54,252 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 14L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 727B-727E) · airframe 58,873 hrs · 54,252 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN INTERNAL BONDED DOUBLER CRACKED BETWEEN BS 727B TO BS 727E, STR 14L. REPAIRED SKIN PER SWA EA.

Part: LENS — MISSING (CABIN) · airframe 58,873 hrs · 54,252 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FWD CABIN EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 58,726 hrs · 54,139 cycles

DURING SCHEDULED C1 CHECK, FOUND RT HORIZONTAL STAB AFT SPAR CRACKED BETWEEN STAB STA 157.10 AND STAB STA 166.30. REPAIRED HORIZONTAL STAB PER SRM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 58,726 hrs · 54,139 cycles

DURING SCHEDULED C1 CHECK, CABIN EMERGENCY EXIT LIGHT BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,665 hrs · 54,084 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,665 hrs · 54,084 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (EMERGENCY EXIT) · airframe 58,637 hrs · 54,058 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD GALLEY EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 58,620 hrs · 54,045 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,610 hrs · 54,034 cycles

LT OVERWING EEPLS STRIP INOP. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (BS 747) · airframe 58,220 hrs · 53,722 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 727E) · airframe 58,220 hrs · 53,722 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 747) · airframe 58,220 hrs · 53,722 cycles

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

Part: SKIN — CRACKED (BS 770) · airframe 58,220 hrs · 53,722 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 770, STR 18L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (BS 500C) · airframe 57,354 hrs · 53,011 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 15L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,643 hrs · 52,464 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 17, STR 12R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,961 hrs · 51,930 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 55,953 hrs · 51,920 cycles

DURING SCHEDULED C2 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 135. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,510 hrs · 50,775 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 927, STRINGER 23R, CRACKED. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,397 hrs · 50,674 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY, FWD SERVICE, AFT ENTRY, AFT SERVICE DOORS AND OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: GATE — CRACKED (L2 DOOR) · airframe 54,118 hrs · 50,431 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR LOWER GATE CRACKED. REMOVED AND REPLACED LOWER GATE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,118 hrs · 50,431 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 53,528 hrs · 49,941 cycles

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

Part: SKIN — DELAMINATED (RT WING SPOILER) · airframe 53,410 hrs · 49,844 cycles

DURING SCHEDULED A1 CHECK, FOUND RT WING NR 5 SPOILER DELAMINATED. REMOVED AND REPLACED RT WING NR 5 SPOILER PER MM.

Part: LENS — MISSING (CABIN) · airframe 53,234 hrs · 49,700 cycles

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT LENS AT ROW 20 ABC, MISSING. INSTALLED EMERGENCY EXIT LIGHT LENS PER MM.

Part: SKIN — CRACKED (LT WING) · airframe 53,234 hrs · 49,700 cycles

DURING SCHEDULED C3 CHECK, FOUND LOWER WING SKIN OUTBOARD NR 1 ENGINE, CRACKED. REPAIRED SKIN PER EA.

Part: FASTENER — MISSING (R2 DOOR) · airframe 52,909 hrs · 48,455 cycles

L2 DOOR EVAC SLIDE DOOR GIRT BAR HOOK MISSING FASTENER. INSTALLED FASTENER IN R2 DOOR EVAC SLIDE HOOK PER MM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 51,590 hrs · 48,399 cycles

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

Part: SPLICE — CRACKED (FUSELAGE) · airframe 51,580 hrs · 48,390 cycles

CYXX - DURING SPECIAL VISIT CRACKED STRINGER SPLICE AT BS 360 STRINGER 4L, 4R AND 14R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. (M)

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,580 hrs · 48,390 cycles

CYXX - DURING SPECIAL VISIT FOUND SKIN CRACKED AT BS 787 BELOW STRINGER 13R. REPAIRED SKIN PER ERO. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

DURING SPECIAL VISIT FOUND SHEAR TIES CRACKED AT BS 807 STRINGER 14L, BS 767 STRINGER 14L, BS 360 STRINGER 14L. REPAIRED PER SRM. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

CYXX - DURING SPECIAL VISIT CRACK INDICATION AT WINDOW 12 BS 530. REMOVED AND REPLACED WINDOW FRAME PER MM. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 51,580 hrs · 48,390 cycles

CYXX - DURING SPECIAL VISIT, FOUND CRACK INDICATION AT WINDOWS 28 AND 29, BS 777 AND BS 787. REPAIRED CRACK PER ERO. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,573 hrs · 48,385 cycles

DURING SPECIAL VISIT FOUND SHEAR TIE CRACKED BETWEEN STR L 13 AND L 14, BS 787. REPAIRED DAMAGE PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 51,433 hrs · 48,264 cycles

LT OVERWING EMERGENCY EXIT LIGHT COVER LOOSE. SECURED LENS COVER PER MM.

Part: SKIN — CRACKED (LT WING) · airframe 50,952 hrs · 47,861 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT WING UPPER SKIN CRACKED AT WBL 181. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,952 hrs · 47,861 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED AT BS 714, BL 0. REPAIRED FLOORBEAM PER SWA EA.

Part: ATTACH FITTING — CORRODED (FWD ENTRY) · airframe 50,952 hrs · 47,861 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE FWD AND AFT GIRT BAR ATTACHMENT FITTINGS CORRODED. REMOVED AND REPLACED ATTACHMENT FITTINGS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,952 hrs · 47,861 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 972, BELOW STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,952 hrs · 47,861 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 727D + 4 AT STR 19R AND BS 944 AT STR 23L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,952 hrs · 47,861 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 727A, STR 19L AND STR 25L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: CABLE — MISROUTED (AFT ENTRY DOOR) · airframe 49,498 hrs · 46,704 cycles

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

Part: SLIDE — LOOSE (AFT SVC DOOR) · airframe 48,537 hrs · 45,940 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: CABLE — MISROUTED (AFT ENTRY DOOR) · airframe 48,537 hrs · 45,940 cycles

DURING SCHEDULED CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY CABLE MISROUTED. REROUTED CABLE PER MM.

Part: FRAME — CRACKED (AFT CARGO DOOR) · airframe 46,484 hrs · 44,233 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR FWD OUTER FRAME CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: BRACKET — CRACKED (AFT SVC DOOR) · airframe 43,709 hrs · 41,920 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE FWD ATTACH BRACKET CRACKED. R&R EMERGENCY EVAC SLIDE ATTACH BRACKET PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,709 hrs · 41,920 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 11R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 43,445 hrs · 41,698 cycles

FWD ENTRY & FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BARS CONTACT DOOR FRAME WHEN DOORS ARE OPENED. REMOVED AND REPLACED EMERGENCY EVAC SLIDES AND CONTAINERS PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 43,096 hrs · 41,417 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. R&R EVAC SLIDE ASSY PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 42,821 hrs · 41,167 cycles

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

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 42,782 hrs · 41,129 cycles

DURING SCHEDULED 1/4D CHECK, FOUND WINDOW POST CRACKED AT LT SIDE, BETWEEN CAPT''S NR 1 & NR 2 WINDOWS. REPAIRED WINDOW POST PER SRM.

Part: SLIDE — FRAYED (SERVICE DOOR) · airframe 42,782 hrs · 41,129 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY FRAYED AT INBD EDGES. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 42,782 hrs · 41,129 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 6 BS 178 BULKHEAD WEB CRACKS AT RBL 5.0 TO LBL 7.0, WL 199 TO WL 207. REPAIRED BULKHEAD WEB PER SWA RA.

Part: SLIDE — FRAYED (ENTRY DOOR) · airframe 42,782 hrs · 41,129 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY FRAYED & STRAPS UNGLUED. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 42,782 hrs · 41,129 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STR 28L CLIP CRACKED AT BS 867. REMOVED AND REPLACED STR CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 42,782 hrs · 41,129 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD SHEAR TIE CRACKED AT FWD FASTENER HOLE, LT SIDE, WL 208. REPAIRED SHEAR TIE ANGLE PER SWA RA.

Part: LIGHT — LOOSE (CABIN) · airframe 42,594 hrs · 40,975 cycles

EEPLS LOOSE IN FWD SECTION. SECURED EEPLS PER MM.

Part: STIFFENER — CRACKED (WING BOX) · airframe 41,262 hrs · 39,867 cycles

TWO STIFFENERS FOUND CRACKED AT FWD BULKHEAD BS 663, MLG W/W. REMOVED AND REPLACED STIFFENERS PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 41,262 hrs · 39,867 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CRACKED STIFFENER AT BS 663, LBL 6 & RBL 6. REMOVED AND REPLACED STIFFENERS PER SRM.

Part: CABLE — MISROUTED (GIRT BAR) · airframe 40,898 hrs · 39,545 cycles

DURING SCHEDULED RON CHECK, FOUND AFT DOOR EVACUATION SLIDE GIRT CABLE ASSY MISROUTED. REPOSITIONED CABLE PER MM.

Part: SLIDE — DISCHARGED (SERVICE DOOR) · airframe 40,364 hrs · 39,081 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR READING LOW. R & R SLIDE ASSY PER MM.

Part: FLOORBEAM — GOUGED (BS 986.5)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD, UPPER SURFACE FWD EDGE GOUGED AT BS 986.5, WL 208, LBL 49. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 342)

DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 342, WL 205 BETWEEN STRINGER 17 AND 18 RT. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 295)

DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT STR 16L, BS 295 FWD OF FWD ENTRY DOORWAY. REMOVED AND REPLACED PER BOEING SRM.

Part: BRACKET — CRACKED (BS 344)

DURING SCHEDULED D-CHECK, FOUND CRACKED L-BRACKET AT BS 344, STR 12R. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — DENTED (BS 428)

DURING SCHEDULED D-CHECK, FOUND DENTED INTERCOSTAL AT BS 428, LBL 45, WL 166. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 348 & 346)

DURING SCHEDULED D-CHECK, FOUND TWO DENTS IN SKIN AT BS 348 AND 346, WL 200 BETWEEN STRINGERS 17 AND 18 RT. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 468 & 474)

DURING SCHEDULED D-CHECK, FOUND TWO DENTS IN FUSELAGE SKIN AT BS 468 AND 474 BETWEEN STRINGER 22 AND 23 LT. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 241)

DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 241, WL 170, LBL 59. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGE (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOORWAY FUSELAGE TORQUE TUBE CAVITY GOUGE ON INSIDE OF SKIN. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CORRODED (BS 429)

DURING SCHEDULED D-CHECK, FOUND CORRODED UPPER SURFACE OF WEB AT BS 429, WL 208, RBL 70. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 727)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME BETWEEN STR 8L AND STR 9L AT BS 727D. REPAIRED PER TRAMCO EWO NR 98-0751. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 867 & 827)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME BETWEEN STR 8R AND STR 9R AT BS 867 AND BS 827. REPAIRED PER TRAMCO EWO NR 98-0751. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 747)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME BETWEEN STR 8L AND STR 9L AT BS 747. REPAIRED PER TRAMCO EWO NR 98-0751. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 314)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 294.5, RBL 47, WL 208 CORRODED ON UPPER FLANGES. REPAIRED PER BOEING SRM.

Part: STABILIZER — CRACKED (BS 314)

DURING SCHEDULED D-CHECK, FOUND FLOOR STABILIZER CRACKED AT BS 314, LBL 12, WL 198.5. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 727)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME BETWEEN STR 8R AND STR 9R AT BS 727D AND BS 727B. REPAIRED PER TRAMCO EWO NR 98-0751.

Part: FRAME — CRACKED (BS 827)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME BETWEEN STR 8L AND STR 9L AT BS 827. REPAIRED PER TRAMCO EWO NR 98-0751.

Part: FRAME — CRACKED (BS 500)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 500A BELOW STR 8 LT. REPAIRED PER TRAMCO EWO NR 98-0751. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 480)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 480 BELOW STR 8 LT. REPAIRED PER TRAMCO EWO NR 98-0751. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 440)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 440 BELOW STR 8 LT. REPAIRED PER TRAMCO EWO NR 98-0751. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 400)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 400 BELOW STR 8 LT. REPAIRED PER TRAMCO EWO NR 98-0751. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 380)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 380 BELOW STR 8 RT. REPAIRED PER TRAMCO EWO NR 98-0751. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 500)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 500A BELOW STR 8 RT. REPAIRED PER TRAMCO EWO NR 98-0751. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 440)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 440 BELOW STR 8 RT. REPAIRED PER TRAMCO EWO NR 98-0751. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 500)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 500C BELOW STR 8 RT. REPAIRED PER TRAMCO EWO NR 98-0751. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (SERVICE DOORWAY)

DURING SCHEDULED D-CHECK, FOUND AFT GALLEY SERVICE DOORWAY THRESHOLD Z ANGLES CORRODED. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 500)

DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL AT BS 500B TO 500C, RBL 26, WL 159. REPAIRED PER BOEING SRM.

Part: STRINGER — DAMAGED (BS 787)

DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIP MECHANICALLY DAMAGED AT BS 787, STR 21 RT. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD — CORRODED (BS 500)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD SUPPORT ANGLE AT BS 500D, RBL 24 TO LBL 24, WL 156 CORRODED SURFACE AROUND NUT PLATE . REPAIRED PER BOEING SRM.

Part: ANGLE — DAMAGED (NR 1 PYLON)

DURING SCHEDULED D-CHECK, FOUND NR 1 PYLON ANGLE LOWER EDGE OF I/B FLAP CUTOUT DAMAGED. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 294-312)

DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AT BS 294-312, LBL 12, WL 208 CORRODED. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 867)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME BETWEEN STR 8L AND 9L AT BS 867. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 295)

DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT STR 7L, BS 295 FWD OF FWD ENTRY DOOR. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 367)

DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 367, 1 BELOW STR 5L. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 344)

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER 8R AT BS 344. REPAIRED PER BOEING SRM.

Part: CLIP — CRACKED (BS 867)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED IN AFT CARGO BAY AT BS 867, STR 24R. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 390)

DURING SCHEDULED D-CHECK, FOUND CORRODED UPPER SURFACE OF WEB AT WL 208, BS 390, RBL 70. REMOVED AND REPLACED PER BOEING SRM.

Part: SHEAR TIE — DAMAGED (BS 907)

DURING SCHEDULED D-CHECK, FOUND DAMAGED SHEAR TIE BETWEEN STR 21R AND 22R AT BS 907. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 1142)

DURING SCHEDULED D-CHECK, FOUND STRINGER 5 RT LOWER CHORD CRACKED AT BS 1142. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — GOUGED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND AFT CARGO BAY FWD DOOR FRAME NR 5 STOP PAD FITTING WITH DEEP GOUGES. REMOVED AND REPLACED PER BOEING SRM.

Part: SHEAR TIE — DAMAGED (BS 907)

DURING SCHEDULED D-CHECK, FOUND DAMAGED SHEAR TIE BETWEEN STR 22R AND 23R AT BS 907 AND STR 23R AND 24R AT BS 907. REMOVED AND REPLACED PER BOEING SRM.

Part: KEEL BEAM — CHAFED (BS 712.5-725)

DURING SCHEDULED D-CHECK, FOUND KEEL BEAM FLANGE RT OUT BOARD CHAFED AROUND FASTENER HOLES AT BS 712.5 TO 725, RBL 6. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 984)

DURING SCHEDULED D-CHECK, FOUND CORRODED SUPPORT ANGLE AT BS 984, LTBL 53, WL 207. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED LBL 1, WL 186. REPAIRED PER BOEING SRM.

Part: BRACKET — CORRODED (BS 344)

DURING SCHEDULED D-CHECK, FOUND CORRODED AT BS 344, LBL 60, WL 208 ON GIRT BAR BRACKET MOUNT PAD. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD CHORD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND VERTICAL CHORD CRACKED ON AFT SIDE OF 178 BULKHEAD, LBL 5.7, WL 184. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 890)

DURING SCHEDULED D-CHECK, FOUND SKIN DENTED AT BS 890 BETWEEN STRINGERS 25-26 RT. REPAIRED PER BOEING SRM. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 270)

DURING SCHEDULED D-CHECK, FOUND CORRODED AT BS 270 Z ANGLE, LBL 12 TO RBL 12. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD UPPER SURFACE CORRODED AT BS 986.5, WL 208, LBL 4.75, LBL 13.5 & LBL 30.5. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 727)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB AT BS 727A-727B, WL 208. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 986.5 - 1016)

DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 986.5 - 1016, LBL 35-45, WL 208. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 727)

DURING SCHEDULED D-CHECK, FOUND CORRODED ON CREASE BEAM WEB AT BS 727B-727C, WL 208, LBL 60. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 992)

DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 992, WL 208, LBL 24. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 1008 & 1014)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD UPPER SURFACE CORRODED AT BS 1008 & 1014, WL 208, LBL 30.5 & LBL 6.0. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — GOUGED (BS 986)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD UPPER SURFACE FWD EDGE GOUGED AT BS 986, WL 208, RBL 44. REPAIRED PER BOEING SRM.

Part: SUPPORT — CRACKED (BS 312-328)

DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AT BS 312-328, LBL 12, WL 208 CRACKED. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — DENTED (BS 907)

DURING SCHEDULED D-CHECK, FOUND FRAME DENTED AT BS 907, WL 172, LBL 24. REMOVED AND REPLACED PER TRAMCO EWO NR 98-0774.

Part: FRAME — CRACKED (BS 616)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 616, WL 201, LBL 65. REMOVED AND REPLACED PER TRAMCO EWO NR 98-0743.

Part: INTERCOSTAL — CORRODED (BS 787-791)

DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL CORRODED AT BS 787-791, STR 25R IN AFT CARGO BAY. REMOVED AND REPLACED PER BOEING SRM.

Part: STIFFENER — CRACKED (BS 538)

DURING SCHEDULED D-CHECK, FOUND FLOOR STIFFENER CRACKED AT BS 538, RBL 2, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 870)

DURING SCHEDULED BC1 CHECK, FOUND A 2.5 INCH FUSELAGE SKIN CRACK AT BS 870, AT S24R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 880)

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 880, ABOVE S25R. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 772)

DURING SCHEDULED MAINT CHECK, FOUND FLOORBEAM CORROSION AT BS 772 LBL 12.25 RBL 3, RBL 7.5, RBL 8.25 AND RBL 13.25. REPAIRED PER BOEING SRM.