N671SW

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,208 hrs · 60,649 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME WEB CRACKED AT BS 500D, LBL 5. REPAIRED WEB PER EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 74,208 hrs · 60,649 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CORRODED BETWEEN BS 500C+16 TO BS 500D+5, LBL 6.50. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,208 hrs · 60,649 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 74,205 hrs · 60,648 cycles

DURING SCHEDULED CV CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT HOUSING LOOSE. SECURED LIGHT PER MM.

Part: LENS — LOOSE (CABIN) · airframe 74,205 hrs · 60,648 cycles

DURING SCHEDULED CV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,198 hrs · 60,641 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 307, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,671 hrs · 60,237 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,671 hrs · 60,237 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 793 TO BS 793.5, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,328 hrs · 59,975 cycles

DURING SCHEDULED MV1 CHECK FOUND, SKIN CRACKED AT BS 520+3, STR 15R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,328 hrs · 59,975 cycles

DURING SCHEDULED MV1 CHECK FOUND, SKIN CRACKED AT BS 500D+14.5, STR 15L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,328 hrs · 59,975 cycles

DURING SCHEDULED MV1 CHECK FOUND, SKIN CRACKED AT BS 727E+4, STR 19R. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 73,002 hrs · 59,726 cycles

FWD GALLEY OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 72,531 hrs · 59,401 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 71,512 hrs · 58,615 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,350 hrs · 58,491 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, BETWEEN STR 8L TO STR 9L. REMOVED AND REPLACED CLIP PER SRM AND EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 663.75, STR 3R. REMOVED AND REPLACED SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 663.75, STR 2L. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 663.75, STR 3L. REMOVED AND REPLACED SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 459, STR 28R. REMOVED AND REPLACED SKIN PER SRM AND EA.

Part: UPLOCK — CORRODED (LT MLG) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT MLG UPLOCK TAPERED FUSE PIN CORRODED. REMOVED AND REPLACED LT UPLOCK ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 663.75, STR 1. REMOVED AND REPLACED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD CARGO BAY FRAME CRACKED AT BS 500C, STR 20R TO STR 21R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 663.75, STR 2R. REMOVED AND REPLACED FRAME PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND OVERHEAD DOOR EMERGENCY EXIT LIGHT BROKEN. REPAIRED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

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

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR CUTOUT, AFT VERTICAL RIB CORRODED AT FS 983.5. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,606 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD CARGO FRAME CRACKED AT BS 500D, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,606 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 14R. REPAIRED FRAME PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 908, STR 20L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4L. REMOVED AND REPLACED CLIP PER ER.

Part: FLAP — DELAMINATED (LT WING) · airframe 71,060 hrs · 58,258 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 328, ABOVE L1 DOOR. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 360, BETWEEN STR 13R TO STR 14R. REMOVED AND REPLACED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: BRACKET — CRACKED (EVAC SLIDE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME WEB CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,060 hrs · 58,258 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 71,034 hrs · 58,238 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING O/B AFT FLAP T/E DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 70,513 hrs · 57,807 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,024 hrs · 57,448 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 929, STR 24L. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 70,024 hrs · 57,448 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE PER MM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 70,024 hrs · 57,448 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FWD CARGO DOOR FWD FRAME CRACKED AT RADIUS COMMON WITH FWD MOST LOWER STOP FITTING. REMOVED AND REPLACED DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,024 hrs · 57,448 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 932, STR 24L. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,733 hrs · 57,236 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP BETWEEN ROW 15 TO ROW 16. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,733 hrs · 57,236 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 68,913 hrs · 56,639 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 68,470 hrs · 56,314 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT NR 1 SLAT UPPER WEDGE SKIN DELAMINATED. REMOVED AND REPLACED NR 1 SLAT PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 68,470 hrs · 56,314 cycles

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

Part: FLAP — PUNCTURED (RT WING) · airframe 68,435 hrs · 56,292 cycles

DURING SCHEDULED MV4 CHECK, FOUND RT WING I/B AFT FLAP PUNCTURED. REMOVED AND REPLACED AFT FLAP EPR MM.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 68,332 hrs · 56,212 cycles

AIR TURNBACK, AFTER TAKEOFF B-HYDRAULIC PUMP LIGHT ILLUMINATED NOTICED "B" QYT MOVING TO 1/4 TURNED OFF BOTH "B" PUMPS RESERVOIR QTY 1/4 AT GATE. REMOVED AND REPLACED STEEL FLEX HOSE AT B-ELECTRIC HYDRAULIC PUMP PER MM.

Part: SKIN — PUNCTURED (LE SLAT) · airframe 68,192 hrs · 56,101 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING L/E NR 1 SLAT SKIN PUNCTURED. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,192 hrs · 56,101 cycles

DURING SCHEDULED SPV CHECK, FOUND LT CENTER CABIN EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 68,192 hrs · 56,101 cycles

DURING SCHEDULED SPV CHECK, FOUND 1016 AFT PRESSURE BULKHEAD DOME CAP WEB CRACKED AT 12:30 TO 1:00 O'CLOCK POSITION. REMOVED AND REPLACED WEB PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 68,192 hrs · 56,101 cycles

DURING SCHEDULED SPV CHECK, FOUND LT OVERWING EMERGENCY EXIT DOOR LENS COVER LOOSE. SECURED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 66,777 hrs · 55,094 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 66,777 hrs · 55,094 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,777 hrs · 55,094 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 66,305 hrs · 54,751 cycles

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

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 65,004 hrs · 53,792 cycles

DURING SCHEDULED 20Y CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, LBL 39. REPAIRED WEB PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,004 hrs · 53,792 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED SKIN PER EA.

Part: LENS — BROKEN (CABIN) · airframe 65,004 hrs · 53,792 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,004 hrs · 53,792 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,004 hrs · 53,792 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD ENTRY DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED SKIN PER EA.

Part: SIGN — CRACKED (EMERGENCY LIGHT) · airframe 65,004 hrs · 53,792 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CABIN EMERGENCY EXIT SIGN CRACKED. R&R EXIT SIGN PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,004 hrs · 53,792 cycles

DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 847 TO BS 867, LBL 70. REPAIRED WEB PER SRM AND BOEING DRAWING.

Part: BEARING — WORN (RT ELEVATOR) · airframe 65,004 hrs · 53,792 cycles

DURING SCHEDULED 20Y CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT HORN BEARING PER MM.

Part: HOUSING — BROKEN (EXIT LIGHT) · airframe 65,004 hrs · 53,792 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT HOUSING BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,004 hrs · 53,792 cycles

DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 827 AND BS 847, LBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 65,004 hrs · 53,792 cycles

DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,004 hrs · 53,792 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,004 hrs · 53,792 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,004 hrs · 53,792 cycles

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

Part: BEAM — CRACKED (FUSELAGE) · airframe 65,004 hrs · 53,792 cycles

DURING SCHEDULED 20Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17. REPAIRED WEB PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 65,004 hrs · 53,792 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING NR 4 L/E SLAT INBOARD UPPER CORNER DELAMINATED. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,004 hrs · 53,792 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,004 hrs · 53,792 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 65,004 hrs · 53,792 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR LOWER FWD FRAME CRACKED AT FWD CORNER. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,004 hrs · 53,792 cycles

DURING SCHEDULE 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,004 hrs · 53,792 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 64,962 hrs · 53,761 cycles

EEPLS LENS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 DEF. SECURED STRIP PER MM.

Part: LENS — MISSING (CABIN) · airframe 64,895 hrs · 53,714 cycles

AFT CABIN EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,283 hrs · 53,256 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,283 hrs · 53,256 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN R1 DOOR CUTOUT UPPER FWD CORNER CRACKED. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (LT FOREFLAP) · airframe 64,283 hrs · 53,256 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FLAP PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,283 hrs · 53,256 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,494 hrs · 52,696 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,494 hrs · 52,696 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,475 hrs · 52,680 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 16L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,475 hrs · 52,680 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 19R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 63,292 hrs · 52,552 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLAT — CRACKED (LT WING) · airframe 63,292 hrs · 52,552 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT INBOARD END. REPAIRED SLAT PER SWA EA.

Part: LIGHT — CRACKED (CABIN) · airframe 63,292 hrs · 52,552 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT ASSY CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 63,125 hrs · 52,428 cycles

L1 COCKPIT WINDOW ARCED IN FLIGHT. REMOVED AND REPLACED L1 COCKPIT WINDOW PER MM.

Part: SKIN — CRACKED (BS 739E S18R) · airframe 62,755 hrs · 52,116 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739E, STR 18R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 62,590 hrs · 51,988 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 62,579 hrs · 51,981 cycles

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

Part: HINGE — CRACKED (NR 5 SPOILER) · airframe 62,327 hrs · 51,764 cycles

DURING SCHEDULED C2 CHECK, FOUND RIGHT WING NR 5 GROUND SPOILER OUTBOARD HINGE CRACKED. REMOVED AND REPLACED NR 5 SPOILER PER MM.

Part: LENS — MISSING (CABIN) · airframe 61,558 hrs · 51,151 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM.

Part: STIFFENER — CRACKED (RT MLG W/W) · airframe 61,495 hrs · 51,100 cycles

DURING SCHEDULED SPV CHECK, FOUND RIGHT MLG W/W VERTICAL STIFFENER CRACKED AT BS 663, RBL 6.15. REMOVED AND REPLACED STIFFENER PER ACO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,495 hrs · 51,100 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,495 hrs · 51,100 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,495 hrs · 51,100 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 61,486 hrs · 51,092 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 61,444 hrs · 51,051 cycles

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

Part: WINDOW — ARCED (FLIGHT DECK) · airframe 61,194 hrs · 50,861 cycles

FLIGHT DECK R2 WINDOW ARCHED AND CRACKED. REMOVED AND REPLACED WINDOW AND HEAT CONTROLLER PER MM.

Part: ATTACH FITTING — BROKEN (ELEVATOR TAB) · airframe 60,770 hrs · 50,530 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT ELEVATOR TAB CONTROL ATTACH POINT BROKEN. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 60,597 hrs · 50,392 cycles

DURING SCHEDULED C4 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: CONTROL ROD — BROKEN (ELEVATOR) · airframe 60,597 hrs · 50,392 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT ELEVATOR TAB CONTROL ROD ATTACH POINT BROKEN. REMOVED AND REPLACED RIGHT ELEVATOR TAB PER MM.

Part: SKIN — CRACKED (BS 934 S25R) · airframe 59,669 hrs · 49,696 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 25R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (NR 1 SLAT) · airframe 59,669 hrs · 49,696 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING NR 1 L/E SLAT LOWER T/E SKIN CRACKED. REPAIRED SLAT PER SWA EA.

Part: LENS — BROKEN (EMERGENCY EXIT) · airframe 59,300 hrs · 49,409 cycles

EMERGENCY EXIT SIGN LENS BROKEN AT ROW 11 DEF. REMOVED AND REPLACED SIGN LENS PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 59,000 hrs · 49,175 cycles

EMERGENCY EXIT SIGN LENS MISSING AT FWD CABIN. INSTALLED SIGN LENS PER MM.

Part: SIGN — MISSING (EMERGENCY EXIT) · airframe 58,980 hrs · 49,163 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,665 hrs · 48,908 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,494 hrs · 48,774 cycles

DURING SCHEDULED SPV CHECK, FOUND STR 16L CRACKED AT BS 360. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 58,494 hrs · 48,774 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED T/E AFT FLAP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 58,494 hrs · 48,774 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 908 S4L) · airframe 58,494 hrs · 48,774 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (BS 360 S14R) · airframe 58,494 hrs · 48,774 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REPAIRED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (BS 178) · airframe 58,494 hrs · 48,774 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL STIFFENER WEB CRACKED AT BULKHEAD BS 178, RBL 5.7. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (BS 921 S25R) · airframe 58,316 hrs · 48,641 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 921, STR 25R. REPAIRED FUSELAGE SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 734) · airframe 58,316 hrs · 48,641 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 734, STR 19R. REPAIRED FUSELAGE SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 921 S25R) · airframe 58,305 hrs · 48,634 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 921, STR 25R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 957) · airframe 57,597 hrs · 48,099 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 957, STR 23L. REPAIRED SKIN PER SWA EA & SRM.

Part: ACTUATOR — BROKEN (LT WING SPOILERS) · airframe 57,597 hrs · 48,099 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT WING INBOARD GROUND SPOILER OUTBOARD ACTUATOR BROKEN AT FWD MOUNTING BOLT. REMOVED AND REPLACED ACTUATOR PER MM.

Part: FITTING — BROKEN (LT WING SPOILER) · airframe 57,597 hrs · 48,099 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LEFT WING INBOARD GROUND SPOILER NR 4 MOUNT SUPPORT LUG BROKEN. REPAIRED SPOILER MOUNT SUPPORT PER SWA EA.

Part: ACTUATOR — SHEARED (LT WING SPOILERS) · airframe 57,597 hrs · 48,099 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT WING INBOARD GROUND SPOILER INBOARD ACTUATOR SHEARED. REMOVED AND REPLACED ACTUATOR PER MM.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 56,945 hrs · 47,597 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT WING T/E FLAP NR 2 TRACK CORRODED AT AFT LOWER OTBD ATTACH FITTING. REMOVED AND REPLACED FLAP TRACK PER MM.

Part: FLOORBEAM — CRACKED (CABIN FLOOR) · airframe 56,945 hrs · 47,597 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,945 hrs · 47,597 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500A, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,945 hrs · 47,597 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518D, STR 12L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,945 hrs · 47,597 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 24R. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,945 hrs · 47,597 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,945 hrs · 47,597 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,945 hrs · 47,597 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 359, STR 14L. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER — CRACKED (BS 360) · airframe 56,945 hrs · 47,597 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,945 hrs · 47,597 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L TO STR 15L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,945 hrs · 47,597 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT, FWD UPPER CORNER. REPAIRED SKIN IAW SRM.

Part: SOLENOID — FAULTY (MLG) · airframe 56,094 hrs · 46,919 cycles

DECLARED EMERGENCY. MLG HANDLE WOULD NOT LOCK DOWN DURING MLG EXTENSION, 3 RED AND 3 GREEN LANDING GEAR POSITION LIGHTS ILLUMINATED. REMOVED AND REPLACED MLG LEVER HANDLE SOLENOID PER MM.

Part: SLIDE — OUT OF ADJUST (L1 & R1 DOOR) · airframe 55,901 hrs · 46,756 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 & R1 DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 55,901 hrs · 46,756 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: LENS — MISSING (CABIN) · airframe 55,163 hrs · 46,146 cycles

EMERGENCY BULLNOSE LIGHT LENS MISSING AT ROW 12DEF. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,804 hrs · 45,867 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 23L. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (EMERGNECY LIGHT) · airframe 54,765 hrs · 45,840 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,713 hrs · 45,798 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 24R. REPAIRED SKIN PER SWA EA.

Part: LIGHT — BROKEN (CABIN) · airframe 53,275 hrs · 44,681 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT FWD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,272 hrs · 43,049 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT EXTERNAL A/C DOOR CUTOUT, FWD RT CORNER. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,272 hrs · 43,049 cycles

DURING SCHEDULED C2 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 983, STR 21L, AND BS 947, STR 24L. REPAIRED SKIN PER SRM.

Part: BLOWER — FAULTY (E/E BAY) · airframe 51,132 hrs · 42,945 cycles

F/A REPORTED ELECTRICAL ODOR IN CABIN. TURNING OFF RECIRC FAN ODOR ELIMINATED. REMOVED AND REPLACED RECIRC FAN BLOWER PER MM.

Part: SPINDLE — CRACKED (RT WING TE FLAP) · airframe 50,571 hrs · 42,500 cycles

DURING SCHEDULED PMC, FOUND NR 8 T/E FLAP SPINDLE WITH CRACK INDICATION. REMOVED AND REPLACED NR 8 FLAP SPINDLE PER MM.

Part: SLIDE — DEPLOYED (L1 DOOR) · airframe 50,523 hrs · 42,475 cycles

UPON OPENING L1 DOOR, EVACUATION SLIDE DEPLOYED. REMOVED AND REPLACED L1 DOOR EVACUATION SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,352 hrs · 42,342 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACK AT BS 927, STRINGER 23L. REPAIRED SKIN PER SRM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 49,410 hrs · 41,578 cycles

DURING SCHEDULED C4 CHECK, SWA SI 11138-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 HINGE HARDWARE AND BUSHING PER MM.

Part: SLIDE — OUT OF ADJUST (SERVICE DOOR) · airframe 49,002 hrs · 41,237 cycles

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

Part: SLIDE — LOOSE (SERVICE DOOR) · airframe 48,982 hrs · 41,218 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 48,823 hrs · 41,107 cycles

DURING SCHEDULED 1/2D CHECK, FOUND KEEL BEAM CORRODED AT BS 520-540. REPAIRED KEEL BEAM PER SWA EA.

Part: DOOR FRAME — CRACKED (AFT CARGO DOOR) · airframe 48,823 hrs · 41,107 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR AFT FRAME T-CHORD CRACKED AT NR 3 STOP FITTING. REM0VED AND REPLACED AFT CARGO DOOR PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 48,823 hrs · 41,107 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED AT BS 706, LBL 57. REPAIRED FLOORBEAM PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,823 hrs · 41,107 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIPS CRACKED (2 EA) BS 663 AT STR 10R, AND BS 633 AT STR 10L. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 48,823 hrs · 41,107 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT LENS CLOUDED. REMOVED AND REPLACED EXIT LIGHT LENS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,823 hrs · 41,107 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 48,823 hrs · 41,107 cycles

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

Part: SLIDE — OUT OF ADJUST (AFT CABIN DOORS) · airframe 48,497 hrs · 40,844 cycles

DURING SCHEDULED C3 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED BOTH AFT CABIN DOOR SLIDES PER MM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 48,497 hrs · 40,844 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT ADJUST. ADJUSTED SLIDE PER MM.

Part: CABLE — MISROUTED (ESCAPE SLIDE) · airframe 48,497 hrs · 40,844 cycles

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

Part: LINE — LEAKING (HYD SYSTEM) · airframe 48,306 hrs · 40,693 cycles

AIR TURNBACK. LOST A-SYSTEM HYDRAULICS. FOUND, HYD LINE LEAKING AT RT MLG ACTUATOR UPSIDE. REMOVED AND REPLACED HYD LINE FOR RT MLG ACTUATOR PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 48,008 hrs · 40,450 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (7 EA) AT BS 178, BETWEEN LBL 6 & RBL 12. REPAIRED BULKHEAD WEB PER SRM.

Part: SKIN — BULGED (FUSELAGE) · airframe 47,600 hrs · 40,136 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN BULGED BETWEEN BS 727 AND BS 727A, ABOVE STR 8L. REPAIRED SKIN PER SWA EA.

Part: SENSOR — MALFUNCTIONED (NLG) · airframe 45,019 hrs · 38,047 cycles

DURING FLT, BOTH NLG RED AND GREEN LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. REMOVED AND REPLACED S845 SWITCH PER MM.

Part: BYPASS VALVE — ERRATIC (T/E FLAP) · airframe 43,568 hrs · 36,867 cycles

T/E FLAPS WOULD NOT STOP AT 35 DEGS WHEN FLAP HANDLE WAS MOVED FROM 30 TO 40 DEGS. WORKS OK ON THE GROUND. REMOVED AND REPLACED T/E FLAP BYPASS VALVE AND FLAP DRIVE MOTOR PER MM.

Part: SLIDE — LOOSE (AFT ENTRY DOOR) · airframe 42,765 hrs · 36,226 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PARTIALLY PULLED FROM CONTAINER. REINSTALLED EVAC SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 14,236 hrs · 12,138 cycles

DURING SCHEDULED C4 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED BETWEEN ROW 12 & ROW 18. R&R COVERS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,315 hrs · 35,850 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR LOWER HINGE CUTOUT, CRACK IS .025 LONG. REPAIRED SKIN PER SWA RA.

Part: BRACKET — LOOSE (CABIN) · airframe 42,315 hrs · 35,850 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD STOW HOOK ATTACH BRACKET RIVETS LOOSE. SECURED RIVETS PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 40,929 hrs · 34,716 cycles

FWD OUTBD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 40,644 hrs · 34,474 cycles

DURING SCHEDULED 1/4D CHECK, FOUND PRESSURE BEADED WEB CRACKED AT BS 665, RBL 40. REPAIRED BEADED WEB PER SRM & T1-353-032.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 40,644 hrs · 34,474 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CAPTS WINDOW POST CRACKED ON UPPER SECTION, BETWEEN NR 1 & NR 2 WINDOWS. REPAIRED WINDOW POST PER SRM.

Part: SKIN — DAMAGED (LT WING LE FLAP) · airframe 40,644 hrs · 34,474 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT WING L/E INBOARD FORE FLAP HAS 10 INCH CREASE ON UPPER SURFACE. REMOVED AND REPLACED INBOARD FORE FLAP PER MM.

Part: FLOORBEAM — CORRODED (CARGO BAY) · airframe 40,644 hrs · 34,474 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 727A, RBL 3. REPAIRED FLOORBEAM PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 40,644 hrs · 34,474 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY LIGHT LOOSE AT BULLNOSE ROW 10 ABC. SECURED LIGHT ASSY PER MM.

Part: SKIN — DELAMINATED (LT WING LE FLAP) · airframe 40,644 hrs · 34,474 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LEFT WING L/E OUTBOARD FORE FLAP T/E DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: FLOORBEAM — CORRODED (CARGO BAY) · airframe 40,644 hrs · 34,474 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 773, LBL 13 TO RBL 8. REPAIRED FLOORBEAM PER RA.

Part: FLOORBEAM — CORRODED (CARGO BAY) · airframe 40,644 hrs · 34,474 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 814, RBL 3 & RBL 8. REPAIRED FLOORBEAM PER SRM & RA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 40,644 hrs · 34,474 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR AFT FRAME CRACKED AT 3RD FROM TOP DOOR PIN FITTING. REPAIRED DOOR FRAME PER T1-152-003 & SRM.

Part: WEB — CRACKED (CENTER SECTION) · airframe 40,644 hrs · 34,474 cycles

DURING SCHEDULED 1/4D CHECK, FOUND PRESSURE BEADED WEB CRACKED AT BS 665, LBL 33. REPAIRED BEADED WEB PER TI-353-046.

Part: LIGHT — LOOSE (GALLEY) · airframe 40,420 hrs · 34,281 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS LOOSE AT FWD GALLEY. SECURED EEPLS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 40,358 hrs · 34,229 cycles

LT SIDE OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT ASSY PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 39,499 hrs · 33,474 cycles

DURING SCHEDULED C1 CHECK, FOUND LEFT WING OUTBOARD T/E FLAP DELAMINATION. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 39,499 hrs · 33,474 cycles

DURING SCHEDULED C1 CHECK, FOUND LT HORIZ STAB AFT SPAR HAS 2 INCH CRACK APPROX 4 FROM ROOT. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 39,327 hrs · 33,350 cycles

EEPLS TRACK LOOSE AT FWD SECTION. SECURED TRACK PER MM.

Part: ENGINE — LEAKING (NR 2) · airframe 39,245 hrs · 33,289 cycles

AIR TURNBACK, IN FLIGHT ENG SHUT-DOWN. NR 2 ENG LOST OIL PRESS AND QTY. INSP NR 2 RNG MAGNETIC CHIP DETECTORS, OIL SUPPLY AND SCAVANGE FILTERS, REINSTALLED GREAR BOX ACCESS PLATE, C/W POWER ASSURANCE. OPS AND LEAK CHECK GOOD PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 38,854 hrs · 32,956 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOPERATIVE. R&R BOTH FWD AND AFT BATTERY PACKS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 38,600 hrs · 32,735 cycles

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY LIGHT ON BULLNOSE PANEL LOOSE AT ROW 20 DEF. RESECURED LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (PAX DOOR) · airframe 38,419 hrs · 32,561 cycles

FWD ENTRY DOOR EVACUATION SLIDE MOVED OUT OF POSITION WHEN DOOR WAS OPENED. REPOSITIONED SLIDE ASSY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 38,279 hrs · 32,450 cycles

FWD EMERGENCY EXIT LIGHT HOUSING INOP. REMOVED AND REPLACED LIGHT HOUSING ASSY PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 38,279 hrs · 32,450 cycles

FWD ENTRY DOOR EVACUATION SLIDE MOVED OUT OF POSITION WHEN DOOR WAS OPENED. REINSTALLED SLIDE ASSY PER MM.

Part: SLIDE — DISCHARGED (PAX DOOR)

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: LENS — CRACKED (ROW 1 & 2)

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK AND LENS CRACKED, ROWS 1 AND 2. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED RON, FOUND EEPLS INOP AT FWD END. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF POSITION (GALLEY DOOR)

AFT GALLEY DOOR EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM.

Part: BULB — FAILED (ROW 16 DEF)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHT LENS COVER ON OVERHEAD AT 16 DEF WILL NOT SECURE. INSTALLED BULB AND LENS COVER PER BOEING MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED D-CHECK, FOUND FWD END OF FLOOR TRACK LIGHTS OFF. RESECURED FWD END FLOOR TRACK LIGHTS PER BOEING MM.

Part: BULKHEAD PANEL — DENTED (BS 380)

DURING SCHEDULED D-CHECK, FOUND FWD RT STATIONARY BULKHEAD PANEL DENTED AT BS 380 RBL 14 WL 159. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 328)

DURING SCHEDULED D-CHECK, FOUND CRACKED ANGLE AT BS 328 RBL 35 WL 200-207. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 328)

DURING SCHEDULED D-CHECK, FOUND CRACKED ANGLE AT BS 328 LBL 47 WL 200-207 (AFT SIDE OF FLOORBEAM). REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — GOUGED (BS 227.8)

DURING SCHEDULED D-CHECK, FOUND GOUGED INTERCOSTAL AT BS 227.8 LBL 22 WL 2655. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 312-328)

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

Part: FLOORBEAM — CORRODED (BS 294.5)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM AT BS 294.5 LBL 12 RBL 15 AND RBL 44 WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 312-328)

DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL AT BS 312-328 RBL 35 WL 208. REPAIRED PER BOEING SRM.

Part: FRAME — DENTED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 787 RBL 29 WL 160, BS 727B LBL 32 WL 158, BS 747 LBL 27 WL 156, BS 767 LBL 28 WL 157, BS 807 LBL 26 WL 157 AND BS 500 RBL 32 WL 159. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — DENTED (BS 847-867)

DURING SCHEDULED D-CHECK, FOUND DENTED INTERCOSTAL AT BS 847 TO 867 LBL 30 WL 163. REMOVED AND REPLACED PER BOEING SRM.

Part: TRACK — GOUGED (BS 851)

DURING SCHEDULED D-CHECK, FOUND GOUGED CARGO TRACK AT ANCHORD POINT AT BS 851 LBL 17 WL 116. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 1114-1124)

DURING SCHEDULED D-CHECK, FOUND CORRODED APU AIR INLET OPENING UPPER STRINGER AT BS 1114 TO 1124 WL 252 RBL 12. REMOVED AND REPLACED PER BOEING SRM.

Part: BEAM — CRACKED (BS 178)

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

Part: FRAME — DAMAGED (CARGO DOORWAY)

DURING SCHEDULED D-CHECK, FOUND AFT CARGO BAY FWD DOOR FRAME COVER WEB DAMAGED AT BS 794 WL 154. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 178)

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

Part: KEELBEAM — DENTED (BS 854)

DURING SCHEDULED D-CHECK, FOUND WORKING FASTENER DAMAGED BS 720 RBL 7 OF HORIZONTAL FLANGE ON KEEL BEAM. REPAIRED PER TRAMCO ER NR 980626.

Part: WEB — DAMAGED (BS 178)

DURING SCHEDULED D-CHECK, FOUND ACCESS HOLE AT BS 178 WL 198.7 LBL 21. REPAIRED PER BOEING SRM.

Part: BULKHEAD WEB — DAMAGED (BS 178)

DURING SCHEDULED D-CHECK, FOUND ELONGATED FASTENER HOLE IN WEB AT BS 178 BULKHEAD WL 184 TO 240 RBL 1736. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 854)

DURING SCHEDULED D-CHECK, FOUND DENTED AT BS 854 STR 21R. REMOVED AND REPLACED PER BOEING SRM.

Part: CLIP — DAMAGED (BS 400)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP DAMAGED AT BS 400 RBL 65 AND BS 500D STR 19 RT. REPAIRED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 1118)

DURING SCHEDULED D-CHECK, FOUND APU INLET AIR DUCT AT LOWER TORQUE BOX CORRODED AT BS 1118 RBL 19 WL 238 ON STRINGER. REMOVED AND REPLACED PER BOEING SRM.

Part: PLATE — CRACKED (BS 791)

DURING SCHEDULED D-CHECK, FOUND CRACK ON ANCHORD PLATE AT BS 791 LBL 40 WL 167 AND LBL 48 WL 172. REPAIRED PER BOEING SRM.

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACK ON RT SIDE CHORD AT BS 178 WL 207 AND LT SIDE CHORD AT BS 178 WL 207. REPAIRED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACKED INDICATIONS AT BS 178 BULKHEAD WEB RBL 5.0 WL 197-198 AND 200-201 AND WL 198-198.5 RBL 67. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 9432)

DURING SCHEDULED D-CHECK, FOUND DENTED FUSELAGE SKIN AT BS 943, 2 INCHES BELOW STR 22R. REPAIRED PER BOEING SRM.

Part: BULKHEAD WEB — DAMAGED (BS 178)

DURING SCHEDULED D-CHECK, FOUND DAMAGED AT BS 178 BULKHEAD WEB LBL 50 WL 200-201 AND 197-198. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 794--847)

DURING SCHEDULED D-CHECK, FOUND CORRODED THRESHOLD WEB AT BS 794-847 RBL 25 WL 157. REPAIRED PER BOEING SRM.

Part: STRAP — CORRODED (BS 790-847)

DURING SCHEDULED D-CHECK, FOUND CORRODED STRAP AT BS 790 TO 847 RBL 20 WL 157. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DENTED (HORIZ STAB)

DURING SCHEDULED D-CHECK, FOUND DENTED RIGHT HORIZONTAL REMOVABLE L/E AT BS 124.5. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 328)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 328 RBL 58 WL 184. REPAIRED PER BOEING SRM.

Part: ANGLE — DAMAGE (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND AFT FUSELAGE TO VERTICAL FIN SKATE ANGLE HAS CHAFING DAMAGE ON LT SIDE. REPAIRED PER BOEING SRM.

Part: ANGLE — DAMAGE (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND AFT FUSELAGE TO VERTICAL FIN SKATE ANGLE HAS CHAFING DAMAGE ON RT SIDE. REPAIRED PER BOEING SRM.

Part: ANGLE — DAMAGE (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND FWD FUSELAGE TO VERTICAL FIN SKATE ANGLE HAS CHAFING DAMAGE ON RT SIDE. REPAIRED PER BOEING SRM.

Part: ANGLE — DAMAGE (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND FWD FUSELAGE TO VERTICAL FIN SKATE ANGLE HAS CHAFING DAMAGE ON LT SIDE. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 312328)

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

Part: INTERCOSTAL — CRACKED (BS 344-360)

DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL AT BS 344 TO 360 LBL 1 WL 208. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 207-208)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM AT BS 344 LBL 25 RBL 11 WL 207-208. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 330)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 330 BETWEEN STR 21R AND 22R. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 294.5)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM STIFFENER AT BS 294.5 RBL 4653 WL 207. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 887/807/727)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 887 STR 9R, BS 807 STR 9R AND BS 727E STR 9R. REPAIRED PER BOEING SRM.

Part: SKIN — LIGHTNING STRIKE (BS 757)

DURING SCHEDULED D-CHECK, FOUND LIGHTNING STRIKE FUSELAGE SKIN AT BS 757 AT STR 10R AND AT BS ON LOWER ROW OF FASTENERS OF STR 4R LAP. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 940-949)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN IS GOUGED AND DENTED FROM BS 995 TO 1005 BETWEEN STRINGER 3L AND 4L AND BS 940 TO 949, 2 INCHES BELOW STR 13L. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 887 STR 9L, BS 847 STR 9L AND BS 827 STR 9L. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 973)

DURING SCHEDULED D-CHECK, FOUND CORRODED WEB AT BS 973 RBL 50 WL 208. REPAIRED PER BOEING SRM.

Part: SKIN — LIGHTNING STRIKE (BS 904)

DURING SCHEDULED D-CHECK, FOUND LIGHTNING STRIKE ON FUSELAGE SKIN AT BS 904 STR 15L. REPAIRED PER BOEING SRM.

Part: BEAM — CRACKED (WINGS)

DURING SCHEDULED D-CHECK, FOUND CRACKED RT MAIN LANDING GEAR BEAM FITTING. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 1016-1033)

DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL AND HAVE ELONGATED FASTENER HOLES AT BS 1016 TO 1033 RBL 940 WL 210. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (GALLEY DOORWAY)

DURING SCHEDULED D-CHECK, FOUND FWD GALLEY SERVICE DOORWAY UPPER FWD STUB FRAME CRACKED AT NR 1 STOP FITTING. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (APU DOORWAY)

DURING SCHEDULED D-CHECK, FOUND APU DOOR FWD HINGE CUTOUT CRACKED. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 1016)

DURING SCHEDULED D-CHECK, FOUND CORRODED TOP OF SHEAR WEB AT BS 1016 RBL 526 WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 328-344)

DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL AT BS 328 TO 344 LBL 47 WL 208. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED D-CHECK, FOUND CORROSION AROUND NUT PLATE HOLE AT BS 986 FLOORBEAM UPPER CHORD LBL 22 WL 208 AND BS 986.5 LBL 22 WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: BRACKET — CRACKED (NR 1 PYLON)

DURING SCHEDULED D CHECK, FOUND CRACKED NR 1 PYLON UPR AFT END, L BRACKET ON I/B SIDE OF SUPPORT BETWEEN ACCESS PANELS 5735L AND 5736L AND AFT SIDE PANEL SUPPORT AT THE AFT END OF ACCESS PANEL 5736L. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 381)

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT BS 381 BELOW STR 15L. REPAIRED PER BOEING SRM.

Part: SUPPORT — CRACKED (NR 1 PYLON)

DURING SCHEDULED D CHECK, FOUND CRACKED NR 1 PYLON LWR AFT END L SUPPORT ON I/B SIDE OF PYLON. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CRACKED (NR 1 PYLON)

DURING SCHEDULED D CHECK, FOUND CRACKED NR1 PYLON 'L' ANGLE SUPPORT ON I/B AFT SIDE ON LWR SIDE OF FLAP CUTOUT IS GOUGED BEYOND LIMITS. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 294.5-303.9)

DURING SCHEDULED D CHECK, FOUND INTERCOSTAL WEB CRACKED AT STRINGER 12, WL 244, LBL 62, BETWEEN BS 294.5-303.9. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 344)

DURING SCHEDULED D CHECK, FOUND UPPER FLANGE OF FLOORBEAM CORRODED AT FASTENER HOLES AT BS 344 RBL 12 TO LBL 12 TOP AND BOTTOM SIDES; AND BS 344 LBL 12 - LBL 58. REPAIRED PER BOEING SRM.

Part: CHORD — CORRODED (BS 270)

DURING SCHEDULED D CHECK, FOUND CORRODED Z CHORD AT BS 270, LBL 11 RBL 11, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 294.5-303.9)

DURING SCHEDULED D CHECK, FOUND CRACKED INTERCOSTAL WEB AT LBL 62, STR 16, WL 216, BETWEEN BS 294.5-303.9; AND BS 277+1, RBL 54 STR 14. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOORBEAM AT BS 312, LBL 45, RBL 12, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 291.5-295.5)

DURING SCHEDULED D CHECK, FOUND CRACKED ATTACH ANGLE AT BS 291.5- 295.5, WL208, RBL 54 THAT ATTACHED FLOORBEAM TO MOPSILL. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 277-291)

DURING SCHEDULED D CHECK, FOUND CRACKED WEB AT BS 277-291, RBL 59-63, WL 253. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 290)

DURING SCHEDULED D CHECK, FOUND CRACKED ANGLE AT BS 290, RBL 63, WL 253. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 294.5-312)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 294.5-312, RBL 12, WL 208. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (SERVICE DOOR)

DURING SCHEDULED D CHECK, FOUND CRACKED EXTERNAL SKIN FWD SERVICE DOOR, AFT CORNER, RBL 66.5 WL 210. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 312-328)

DURING SCHEDULED D CHECK, FOUND CRACKED INTERCOSTAL AT BS 312-328, LBL 47, WL 208. REPAIRED PER BOEING SRM.

Part: SHEAR WEB — CORRODED (BS 1016)

DURING SCHEDULED D CHECK, FOUND CORRODED SHEAR WEB AT BS 1016, LBL 27 WL 208; AND 500A-500B, LBL 65, WL 208. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 991)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR WEB AT BS 991, RBL 45, WL 208. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 967)

DURING SCHEDULED D CHECK, FOUND CORRODED AROUND NUTPLATE HOLES UPPER CHORD FLOORBEAM AT BS 967, RBL 5, 28 + 37, WL 208; AND DOUBLE HOLE AT BS 947, WL 208, LBL 42. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED C4 CHECK, FOUND EXFOLIATED CORROSION FLOORBEAM SUPPORT AT BS 986.5 FAR RIGHT SIDE. REPAIRED PER SWA RA NR 1-353-1808.

Part: SKIN — CRACKED (NR 1/2 LE SLATS)

DURING SCHEDULED C4 CHECK, FOUND CRACKED SKIN NR 1 SLAT LWR T/E O/B OF AND NR 2 SLAT LWR T/E OF ACTUATOR. REPAIRED PER BOEING RA T1-A57-018.

Part: ROD END — OUT OF ADJUST (NR 3 LE SLAT)

AFTER TAKEOFF, NR 3 L/E SLAT WOULD NOT RETRACT PER INDICATION. AIRCRAFT RETUNED TO PHX AND MADE AN UNEVENTFUL LANDING. ADJUSTED NR 3 SLAT ROD END AND REPAIRED ROD END WIRING PER BOEING M/M.

Part: STRINGER — TORN (BS 397)

DURING SCHEDULED B/C4 CHECK, FOUND STRINGERS TORN AT BS 397, S18L. REPAIRED PER BOEING SRM.

Part: SKIN — DAMAGED (BS 378)

DURING SCHEDULED B/C4 CHECK, FOUND FUSELAGE SKIN DAMAGE AT BS 378 AND 403 AT S19L. REPAIRED PER BOEING SRM.

Part: SLIDE — LOW PRESS (AFT SERVICE DR)

DURING SCHEDULED TERMINAL CHECK, FOUND AFT SERVICE DOOR ESCAPE SLIDE PRESSURE LOW. REPLACED PER BOEING M/M.

Part: ENGINE — FAILED (NR 2)

AT 37,000, EXPERIENCED NUMBER 2 ENGINE OIL PRESSURE DROP, THEN ENGINE STOPPAGE. CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. AIRCRAFT DIVERTED TO TUS AND MADE AN UNEVENTFUL LANDING. REPLACED NUMBER 2 ENGINE PER BOEING M/M.