N313SW

Part: CONTROL ROD — CORRODED (ELEVATOR TAB) · airframe 79,496 hrs · 72,977 cycles

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

Part: CONTROL ROD — CORRODED (ELEVATOR TAB) · airframe 79,496 hrs · 72,977 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,957 hrs · 72,557 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 516D, STR 12L. REPAIRED SKIN PER AND ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,957 hrs · 72,557 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 19L TO STR 22L. REPAIRED FRAME PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 78,926 hrs · 72,537 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,618 hrs · 72,281 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 979.5, STR 27R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,618 hrs · 72,281 cycles

DURING SCHEDULED OTS CHECK, FOUND AFT CARGO DOOR CUTOUT CRACKED AT AFT UPPER CORNER. REPAIRED SKIN PER EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 78,621 hrs · 72,282 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CORRODED AT BS 999.5, STR 27R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,618 hrs · 72,281 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 339, STR 22R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,618 hrs · 72,281 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 507, STR 16L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 78,621 hrs · 72,282 cycles

DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CORRODED AT BS 1006, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,621 hrs · 72,282 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CORRODED AT BS 999.5, STR 27R. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 78,621 hrs · 72,282 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CORRODED BETWEEN BS 1006 TO BS 1016, STR 26L. REMOVED AND REPLACED STRINGER PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,621 hrs · 72,282 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 16L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,621 hrs · 7,282 cycles

DURING OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 340 TO BS 341, STR 22R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 78,621 hrs · 7,282 cycles

DURING OTS CHECK, FOUND AFT CARGO DOOR SKIN CRACKED. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 78,621 hrs · 72,282 cycles

DURING SCHEDULED OTS CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 78,621 hrs · 72,282 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 78,621 hrs · 72,282 cycles

FOUND CORROSION AT STA 979.5, STR 27R. REPAIRED SKIN PER SRM.

Part: SPOILER — CRACKED (LT WING) · airframe 78,618 hrs · 72,281 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT WING NR 4 GROUND SPOILER CRACKED AT I/B ATTACH POINT. REMOVED AND REPLACED SPOILER PER MM.

Part: LENS — MISSING (CABIN) · airframe 78,618 hrs · 72,281 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD EMERGENCY EXIT SIGN LENS MISSING. REMOVED AND REPLACED LENS ASSY PER MM.

Part: ACTUATOR — LEAKING (SPOILER) · airframe 78,469 hrs · 72,162 cycles

LEFT WING I/B OF NR 1 ENGINE HYDRAULIC FLUID LEAKED. REMOVED AND REPLACED NR 4 GROUND SPOILER O/B ACTUATOR ASSY PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 77,882 hrs · 71,701 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,858 hrs · 71,682 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY LIGHT INOP AT 23 DEF. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,858 hrs · 71,682 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 586 TO BS 595, STR 10R. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 77,746 hrs · 71,605 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,726 hrs · 71,587 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 420, STR 16R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,726 hrs · 71,587 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 515A, STR 16L. REPAIRED SKIN PER EA.

Part: ALTIMETER — FAULTY (COCKPIT) · airframe 77,076 hrs · 71,105 cycles

AT FLT 330, CAPTAINS ALTIMETER INDICATED 32,720, F/O ALTIMETER INDICATES 33,000, STBY ALTIMETER INDICATES 33,000. REMOVED AND REPLACED CAPTAINS ALTIMETER AND NR 1 ADC PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,792 hrs · 70,894 cycles

DURING SCHEDULED MV1 CHECK, FOUND FRAME CRACKED AT BS 374, STR 15R. REPAIRED FRAME PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,684 hrs · 70,809 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 482+14, STR 18L TO STR 19L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,400 hrs · 70,597 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 75,577 hrs · 69,961 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,577 hrs · 69,961 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 754, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,577 hrs · 69,961 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 494, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,577 hrs · 69,961 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 738E, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,577 hrs · 69,961 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 743E, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,577 hrs · 69,961 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 730E, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,577 hrs · 69,961 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 772, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,577 hrs · 69,961 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 762, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,577 hrs · 69,961 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 729E, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,446 hrs · 69,864 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,431 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT, BETWEEN BS 289.75 TO BS 290.75, BETWEEN WL 255 TO WL 257. REPAIRED SKIN PER ER.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,431 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 747, STR 26L. REPAIRED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,431 hrs · 69,852 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,431 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,431 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 27R TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,431 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,431 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 500C, BETWEEN STR 27R TO STR 28R. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,431 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND CORROSION BULGE IN FUSELAGE SKIN AT BS 203.8, STR 24L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 721, WL 265. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO DOOR SKIN CRACKED AT BS 446, STR 25R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 505, STR 16R. REPAIRED SKIN PER ER.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE LIGHT INOP. RELAMPED LIGHT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 16R. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BETWEEN BS 302 TO BS 304, BETWEEN WL 258 TO WL 263. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 472, STR 17R. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500A, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 910, STR 27L. REPAIRED SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 27R TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO BAY FRAME CRACKED AT BS 500, STR 26L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO BAY FRAME CRACKED AT BS 500C, BETWEEN STR 20R TO STR 21R. REMOVED AND REPLACED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 20R. R&R CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8R. R&R CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: WIRE — BROKEN (CABIN) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD CABIN EMERGENCY EXIT BATTERY PACK WIRE BROKEN GOING TO CONNECTOR D2956, AT BS 327R. REPAIRED WIRE PER WDM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500B, STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 757, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727C, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 864, STR 26L. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 767, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. R&R SPLICE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 827, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 27R TO STR 28R. R&R SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 15R TO STR 16R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 25L TO STR 26L. R&R SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, BETWEEN STR 25L TO STR 26L. R&R SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,432 hrs · 69,852 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 24L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,340 hrs · 69,781 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,843 hrs · 69,420 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 267, STR 15R. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,789 hrs · 69,386 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,378 hrs · 69,099 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 583, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,378 hrs · 69,099 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 583, STR 10R. REPAIRED SKIN PER SWA EA.

Part: STRINGER — CRACKED (BS 461) · airframe 74,198 hrs · 68,974 cycles

DURING SCHEDULED MV1 CHECK, FOUND STRINGER CRACKED AT BS 461, STR 18L. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,198 hrs · 68,974 cycles

DURING SCHEDULED MV1 CHECK, FOUND STRINGER CRACKED AT BS 487 + 14, STR 18L. REPAIRED STRINGER PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,847 hrs · 68,728 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 73,839 hrs · 68,720 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 73,623 hrs · 68,568 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 EXTERIOR EMERGENCY EXIT LIGHT INOP. REPAIRED LIGHT PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 73,481 hrs · 68,455 cycles

FWD CABIN EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: CIRCUIT CARD — FAULTY (MLG) · airframe 73,416 hrs · 68,407 cycles

WHEN GEAR EXTENDED FOR LANDING, NOSE GEAR DOWNLOCK WARNING LIGHT ILLUMINATED. REMOVED AND REPLACED M125 CIRCUIT CARD PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 73,119 hrs · 68,187 cycles

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

Part: SKIN — CRACKED (SERVICE DOOR) · airframe 73,057 hrs · 68,133 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,057 hrs · 68,133 cycles

DURING SCHEDULED SPV CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. R&R LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,057 hrs · 68,133 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,912 hrs · 68,020 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 19R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,608 hrs · 67,801 cycles

DURING SCHEDULED RON CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 17R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,608 hrs · 67,801 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 395, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,347 hrs · 67,615 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 395, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,347 hrs · 67,615 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 950, STR 5R. REPAIRED SKIN PER SRM.

Part: CONTROL CABLE — OUT OF ADJUST (MLG WW) · airframe 71,314 hrs · 66,868 cycles

ON APPROACH HAD THREE GREEN LIGHTS AND THREE RED LIGHTS, CYCLED GEAR LEVER HAD THREE GREEN LIGHTS NO RED. ADJUSTED LANDING GEAR CONTROL CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,504 hrs · 66,254 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (BS 360 S28L) · airframe 70,504 hrs · 66,254 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 360, STR 28L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (BS 430) · airframe 70,504 hrs · 66,254 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, BL 1. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,504 hrs · 66,254 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 410) · airframe 70,504 hrs · 66,254 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, BL 0. REPAIRED SKIN PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,504 hrs · 66,254 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 14. REPAIRED FLOORBEAM PER SRM.

Part: TAB — DEBONDED (LT AILERON) · airframe 70,504 hrs · 66,254 cycles

DURING SCHEDULED BRDG CHECK, FOUND LEFT WING AILERON TAB DISBONDED AT AFT OUTBOARD CORNER. REPAIRED TAB PER SRM.

Part: SKIN — DELAMINATED (NR 8 SPOILER) · airframe 70,504 hrs · 66,254 cycles

DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING NR 8 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,504 hrs · 66,254 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 25R CORRODED AT BS 350. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (BS 312 S18R) · airframe 70,504 hrs · 66,254 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 70,504 hrs · 66,254 cycles

DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR CUTOUT LOWER FWD STUB FRAME CRACKED AT AFT END. REPAIRED STUB FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 294 S11L) · airframe 70,504 hrs · 66,254 cycles

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

Part: SKIN — CRACKED (BS 964 S5R) · airframe 70,504 hrs · 66,254 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 964, STR 5R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (BS 277 S16L) · airframe 70,504 hrs · 66,254 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 70,431 hrs · 66,188 cycles

DURING SCHEDULED C2 CHECK, FOUND RIGHT INBOARD FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,399 hrs · 66,161 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 376.5, STR 8L. REPAIRED SKIN PER SWA EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 69,467 hrs · 65,416 cycles

DURING SCHEDULED SPV CHECK, FOUND KEEL BEAM CORRODED AT RIGHT BS 737. REMOVED AND REPLACED KEEL BEAM PER ER.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 69,467 hrs · 65,416 cycles

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

Part: HINGE FITTING — BROKEN (NR 4 SPOILER) · airframe 69,467 hrs · 65,416 cycles

DURING SCHEDULED C1 CHECK, FOUND LEFT WING NR 4 GROUND SPOILER OUTBOARD HINGE FITTING BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (BS 584 S10L) · airframe 68,876 hrs · 64,948 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 584, STR 10L. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,547 hrs · 64,698 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 291.5, STR 15R. REPAIRED FRAME PER SWA EA.

Part: STRINGER — CRACKED (BS 500 S16R) · airframe 68,532 hrs · 64,684 cycles

DURING SCHEDULED C4 CHECK, FOUND STRINGER 16R CRACKED AT BS 500. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (BS 937 S4R) · airframe 68,409 hrs · 64,739 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 937, STR 4R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 380 S16R) · airframe 68,532 hrs · 64,684 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 500 S17R) · airframe 68,532 hrs · 64,684 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 17R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (R1 DOOR) · airframe 68,532 hrs · 64,684 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (L2 DOOR) · airframe 68,532 hrs · 64,684 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER AFT RADIUS CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 466 S16R) · airframe 68,044 hrs · 64,324 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 466, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 428 S16R) · airframe 68,044 hrs · 64,324 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 428, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 474 S16R) · airframe 68,044 hrs · 64,324 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 474, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 67,960 hrs · 64,264 cycles

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

Part: LINE — LEAKING (B-HYD SYSTEM) · airframe 67,903 hrs · 64,216 cycles

DIVERSION / DECLARED EMERGENCY. HYD B-SYS QTY IND DECREASED TO 1/4 FULL. FOUND HYD B-SYS LINE LEAKING BETWEEN ACOUSTIC FILTER & MODULE. REMOVED AND REPLACED HYD LINE PER MM.

Part: ACTUATOR — LEAKING (TE FLAPS) · airframe 67,505 hrs · 63,896 cycles

AIR TURNBACK, AFTER FLAP RETRACTION LOST A-HYDRAULIC PRESSURE AND QUANTITY. REMOVED AND REPLACED RIGHT WING NR 6 SPOILER ACTUATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,287 hrs · 63,717 cycles

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

Part: SKIN — CRACKED (BS 450) · airframe 67,287 hrs · 63,717 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, BL 0. REPAIRED SKIN PER ER.

Part: STRINGER SPLICE — CRACKED (BS 360 S15L) · airframe 67,284 hrs · 63,714 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,717 hrs · 63,272 cycles

DURING SCHEDULED MV1 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,515 hrs · 63,157 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 484, STR 16R. REPAIRED SKIN PER SRM.

Part: CROSSBEAM — WORN (NR 1 PYLON) · airframe 66,559 hrs · 63,138 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NR 1 ENGINE FWD MOUNT CROSS BEAM FREEPLAY OUT OF LIMITS. REMOVED AND REPLACED FWD MOUNT CROSSBEAM PER MM.

Part: PACKING — FAILED (MLG WW) · airframe 66,436 hrs · 63,032 cycles

AIR TURNBACK, DECLARED EMERGENCY -LOST ALL -A- SYSTEM HYDRAULIC QUANTITY INFLIGHT. REMOVED AND REPLACED -A- SYSTEM MODULE PACKING PER MM.

Part: CABLE ASSY — MISROUTED (L2 DOOR SLIDE) · airframe 65,663 hrs · 62,465 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM.

Part: SKIN — CRACKED (BS 731E) · airframe 65,653 hrs · 62,455 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 731E, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 403) · airframe 65,653 hrs · 62,455 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 403, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 361) · airframe 65,653 hrs · 62,455 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 361, STR 15L. REPAIRED SKIN PER SWA EA.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,448 hrs · 62,302 cycles

DURING SCHEDULED A1 CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SWITCH — FAULTY (MLG) · airframe 65,313 hrs · 62,204 cycles

WITH GEAR HANDLE IN DOWN POSITION - 3 RED & 3 GREEN LIGHTS ILLUMINATED. RECYCLED GEAR HANDLE - 3 RED & 3 GREEN LIGHTS STILL ILLUMINATED. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER POSITION SWITCH PER MM. OPS CHECKED GOOD.

Part: SKIN — CRACKED (BS 454-456) · airframe 64,924 hrs · 61,887 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 454 TO BS 456, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (LH WING TE FLAP) · airframe 64,801 hrs · 61,794 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING OTBD T/E AFT FLAP DELAMINATED. REPAIRED FLAP PER SWA EA.

Part: SOLENOID — FAULTY (MLG) · airframe 63,966 hrs · 61,122 cycles

MOVING LANDING GEAR LEVER TO DOWN POSITION, ALL RED AND GREEN WARNING LIGHTS ILLUMINATED. CYCLED LANDING GEAR LEVER SEVERAL TIMES BEFORE RED WARNING LIGHTS EXTINGUISHED. REMMOVED AND REPLACED LANDING GEAR LEVER SOLENOID PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,869 hrs · 61,052 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 835, STR 20L. REPAIRED SKIN PER SWA EA & SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,868 hrs · 61,051 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 986.5, STR 27L. MX FERRY TO DAL FOR REPAIRS. REPAIRED STRINGER PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,868 hrs · 61,051 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 986.5, BETWEEN STR 26L TO STR 27L. MX FERRY TO DAL FOR REPAIRS. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,868 hrs · 61,051 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 865 TO BS 872, STR 16L. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 63,797 hrs · 60,995 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NLG W/W RT FWD UPPER ACCESS CUTOUT, AFT INBD CORNER CRACKED AT BS 251.6, LBL 2.0. REPAIRED WEB PER SWA EA.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 63,717 hrs · 60,932 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR FWD BRACKET LOOSE. SECURED BRACKET PER MM.

Part: FLOORBEAM — CRACKED (CABIN FLOOR) · airframe 62,846 hrs · 60,209 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA LONGITUDINAL FLOORBEAMS CRACKED AT BS 727A + 18, LBL 45 & RBL 45, WL 208. REPAIRED BEAMS PER PAE ER.

Part: FLOOR SUPPORT — CRACKED (CABIN FLOOR) · airframe 62,846 hrs · 60,209 cycles

DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CRACKED AT BS 727B - 2, RBL 25, WL 208. REPAIRED BEAM PER PAE ER.

Part: SKIN — CRACKED (RT WING) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND RIGHT WING UPPER SKIN CRACKED AT RSS 238. REPAIRED SKIN PER PAE ER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 1006, STR 12R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA CRACKS AT FUSELAGE FRAME, BS 727, BETWEEN STR 14L & STR 16L. REPAIRED FRAME PER PAE ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE SKIN AT BS 1006, BETWEEN STR 2L & STR 3L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER PAE ER.

Part: FRAME — CRACKED (BS 747) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 847) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 9R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 787, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME SHEAR TIE CRACKED AT BS 500D, STR 16L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727E) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727 E, STR 5R & STR 3L. REMOVED AND REPLACED CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727A, STR 14R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 520) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 520, BETWEEN STR 6L & STR 8R. REMOVED AND REPLACED CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727D) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727D, BETWEEN STR 3R & STR 5R. REMOVED AND REPLACED CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500D) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500D, BETWEEN STR 6L & STR 8R. REMOVED AND REPLACED CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727B) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727B, STR 5L & STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED AT BS 727C, STR 5L & STR 7L. REMOVED AND REPLACED CLIPS PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 727B, BETWEEN STR 13L & STR 14L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500C) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500C, BETWEEN STR 5L & STR 7L. REMOVED AND REPLACED CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME SHEAR TIE CRACKED AT BS 500B, BETWEEN STR 15R & STR 16R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 685) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 685, STR 4R TO STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 705, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727A, STR 3L & STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 639) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 639, STR 3R & STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727A, STR 6R & STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 8L & STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOOR SUPPORT — CRACKED (CABIN FLOOR) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 660, BL 0. REPAIRED BEAM PER PAE ER & SB.

Part: FLOORBEAM — CRACKED (BS 715) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 715, BL 0, WL 204. REPAIRED BEAM PER SRM & EO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500C, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, BETWEEN STR 8L & STR 9L. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 380, STR 5L. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, BETWEEN STR 8R & STR 9R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 616, STR 4L & STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FITTING — CRACKED (RT MLG WW) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND RIGHT MLG W/W FITTING CRACKED AT BS 715, RBL 68, WL 198. REMOVED AND REPLACED MLG FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (BS 597) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 597, STR 1R TO STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME U-CHANNEL CRACKED AT BS 360, STR 14L. REPAIRED U-CHANNEL PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

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

Part: STRINGER CLIP — CRACKED (BS 578) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 578, STR 5R TO STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 662, RBL 25, WL 207. REPAIRED BEAM PER SB & PAE ER.

Part: STRINGER CLIP — CRACKED (BS 277) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 277, STR 10R & STR 14R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 65, WL 202. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE STRINGER CLIPS CRACKED AT BS 597, STR 8L & STR 9L. REMOVED AND REPLACED CLIPS PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON CABIN FLOORBEAM UPPER CHORD AT BS 344, BETWEEN RBL 8 TO LBL 35. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON CABIN FLOORBEAM UPPER CHORD AT BS 328, LBL 16. REPAIRED FLOORBEAM PER SRM.

Part: FITTING — CORRODED (L1 DOOR SLIDE) · airframe 62,845 hrs · 60,208 cycles

DURING SCHEDULED D-CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE, FWD & AFT GIRT BAR FLOOR FITTINGS CORRODED. REMOVED AND REPLACED FLOOR FITTINGS PER SRM.

Part: FLASHLIGHT — INGESTED (CABIN) · airframe 62,084 hrs · 59,617 cycles

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

Part: BOLT — WORN (ELEVATOR TAB) · airframe 62,068 hrs · 59,605 cycles

DURING SCHEDULED C1 CHECK, LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT AND LT INBOARD NR 1 TAB BOLTS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,068 hrs · 59,605 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 375, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 61,542 hrs · 59,210 cycles

R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. REINSTALLED R1 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,352 hrs · 59,061 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 940, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA.

Part: ACTUATOR — LEAKING (FLT SPOILER) · airframe 61,187 hrs · 58,924 cycles

AIR TURNBACK, AIR RETURN TO DAL DUE TO LOSS OF A-SYSTEM HYDRAULIC FLUID AND PRESSURE. REMOVED AND REPLACED NR 6 INBOARD FLIGHT SPOILER ACTUATOR PER MM.

Part: BEAM — CRACKED (L1 DOOR) · airframe 61,124 hrs · 58,862 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR WEB BEAM AT DOOR STOP, CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 61,124 hrs · 58,862 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 & R1 DOOR EVAC SLIDES GIRT BAR HOOKS LOOSE. SECURED L1 & R1 DOOR EVAC SLIDES GIRT BAR HOOKS PER MM.

Part: ACTUATOR — LEAKING (RT WING) · airframe 61,031 hrs · 58,784 cycles

AIR TURNBACK. CLIMBING THRU 8500, HYDRAULIC -A- SYSTEM FAILURE. REMOVED AND REPLACED NR 6 SPOILER ACTUATOR O-RING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,186 hrs · 58,102 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,186 hrs · 58,102 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 285, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 59,469 hrs · 57,544 cycles

F/O'S AIR SPEED IND C/B TRIPPED AND ACRID ODOR FOLLOWED. REMOVED AND REPLACED F/O'S MACH AIR SPEED IND PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,282 hrs · 57,393 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 920, STRINGER 22L. REPAIRED SKIN PER SRM.

Part: STRAP — CRACKED (DOOR FRAME) · airframe 59,282 hrs · 57,393 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR CUTOUT AT UPPER AND LOWER HINGE STRAPS CRACKED. REMOVED AND REPLACED STRAPS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,282 hrs · 57,393 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 270, STRINGER 9L. REPAIRED SKIN PER SRM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 29,282 hrs · 57,393 cycles

DURING SCHEDULED C2 CHECK, FOUND FORWARD CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 59,225 hrs · 57,342 cycles

EMERGENCY EXIT LIGHT ON LT BULLNOSE MISSING LENS AT ROW 6 ABC. INSTALLED EMERGENCY EXIT LIGHT LENS PER MM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 59,049 hrs · 57,195 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BULKHEAD WEB CORRODED AT BS 1016, BL 0. REPAIRED WEB PER ACO.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 59,049 hrs · 57,195 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RADIAL STIFFENER CORRODED AT BS 1016, BL 0. REPAIRED RADIAL STIFFENER PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,899 hrs · 57,069 cycles

DURING SCHEDULED CHECK, FOUND SKIN CRACKED AT BS 852, STRINGER 20 L. REPAIRED PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,386 hrs · 56,655 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, BETWEEN STR'S 21L AND 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,069 hrs · 56,401 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 14, STR 16L. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (AFT CABIN DOORS) · airframe 57,924 hrs · 56,284 cycles

DURING SCHEDULED A2 CHECK, FOUND BOTH AFT CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. RELAMPED EXIT LIGHTS PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 57,552 hrs · 55,966 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 57,552 hrs · 55,966 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 57,308 hrs · 55,756 cycles

NR 1 ENGINE QUIT ON LANDING ROLLOUT AFTER COMING OUT OF REVERSER THRUST. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: LIGHT — INOPERATIVE (FWD ENTRY DOOR) · airframe 57,086 hrs · 55,572 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM.

Part: INDICATOR — OUT OF POSITION (SLIDE) · airframe 56,954 hrs · 55,477 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,954 hrs · 55,477 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED AT BS 500C + 14, STR 16R. REPAIRED STR PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,954 hrs · 55,477 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED (2 EA) AT BS 540, STR 4R AND STR 10R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,954 hrs · 55,477 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED (2 EA) AT BS 663, STR 1R AND STR 2R. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,954 hrs · 55,477 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 3 EA STRINGER SPLICES CRACKED AT BS 908, STRINGERS 10R AND 4L, AND BS 817 TO BS 847, STRINGER 4L. REPAIRED STRINGER SPLICES PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,800 hrs · 55,346 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH AFT ENTRY & AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,639 hrs · 55,227 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 937 AT STR 23R AND BS 975 AT STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,276 hrs · 54,920 cycles

DURING OTS, FOUND FUSELAGE SKIN CRACKED 4 LONG AT BS 476, STRINGER 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,276 hrs · 54,920 cycles

DURING OTS, FOUND FUSELAGE SKIN CRACKED 2.5 LONG AT BS 311, BELOW STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,689 hrs · 54,471 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 753, ABOVE STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,689 hrs · 54,471 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 464, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,689 hrs · 54,471 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, ABOVE STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,689 hrs · 54,471 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 743, STR 18R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 55,661 hrs · 54,449 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,476 hrs · 54,300 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500B + 13, STR 4R. REPAIRED SKIN PER BFG ER.

Part: BATTERY — FAULTY (CABIN) · airframe 55,476 hrs · 54,300 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CABIN EMERGENCY EXIT LIGHTS M1132 BATTERY DISCHARGED. RECHARGED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,476 hrs · 54,300 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FWD ENTRY DOOR BOTTOM HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,476 hrs · 54,300 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 480, STR 4R. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,476 hrs · 54,300 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED AT BS 500C + 16, STR 16L. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,476 hrs · 54,300 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED, BS 440.5, STRINGER 14R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,476 hrs · 54,300 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CORRODED AT BS 767, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,476 hrs · 54,300 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CORRODED AT BS 827, BETWEEN STR 27L AND 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,476 hrs · 54,300 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CORRODED AT BS 827, WL 156 AND RBL 3. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,476 hrs · 54,300 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 4R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,525 hrs · 53,488 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 323, STR 18R. REPAIRED SKIN PER SRM.

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

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 AND RBL 10.5. REPAIRED WEB PER SRM.

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

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 445, STR 16R. REPAIRED SKIN PER SRM.

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

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 22R. REPAIRED SKIN PER SRM.

Part: CONTROL UNIT — ERRATIC (E&E COMP) · airframe 54,169 hrs · 53,175 cycles

LT BRAKE FLUCTUATES AND RELEASES DURING BRAKING. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,018 hrs · 53,052 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 485, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,018 hrs · 53,052 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 6, ABOVE STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,018 hrs · 53,052 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 10L, BS'S 484, 520 AND 500D + 15. REPAIRED SKIN PER SRM AND SWA RA.

Part: ROD END — LOOSE (ELEVATOR TAB) · airframe 54,016 hrs · 53,049 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, LT ELEVATOR TAB INBOARD PUSH ROD, AFT ROD END HAS LOOSE DUST SEAL. REMOVED AND REPLACED LT ELEVATOR TAB PUSH ROD END PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,142 hrs · 52,363 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR CUTOUT CRACKED BELOW UPPER HINGE ON FWD CENTER STUB FRAME. REPAIRED FRAME PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,100 hrs · 52,325 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 890, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,245 hrs · 51,597 cycles

DURING SCHEDULED C2 CHECK, FOUND 1 INCH FUSELAGE SKIN CRACK AT BS 500B, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,247 hrs · 51,599 cycles

DURING SCHEDULED C2 CHECK, FOUND 2 INCH FUSELAGE SKIN CRACK AT BS 927, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,165 hrs · 52,042 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXT SKIN CRACKED, BS 500D, STRINGER 15L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 51,903 hrs · 51,314 cycles

DURING SCHEDULED A2 CHECK, FOUND COCKPIT OVERHEAD EMERGENCY LIGHT INOP. RELAMPED OVERHEAD EMERGENCY LIGHT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,398 hrs · 50,900 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515, STR 12L & BS 505, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,737 hrs · 50,310 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 805, STR 19. REPAIRED SKIN PER SRM.

Part: STIFFENER — CRACKED (MLG W/W) · airframe 49,962 hrs · 49,654 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BS 663 BULKHEAD STIFFENER CRACKED AT LBL 6.5. REPAIRED STIFFENER PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,962 hrs · 49,645 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 3 EXTERNAL FUSELAGE SKIN CRACK AT BS 940, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,803 hrs · 49,517 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACK AT BS 500C, STR 15L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJ (PAX DOOR) · airframe 49,429 hrs · 49,223 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SVC AND ENTRY DOORS EMERGENCY EVAC SLIDE GIRT ASSY''S OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY''S PER MM.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 48,241 hrs · 48,234 cycles

FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER AS DOOR WAS CLOSED. REINSTALLED SLIDE ASSY PER MM.

Part: SENSOR — ERRATIC (APU BAY) · airframe 47,494 hrs · 47,634 cycles

AIR TURNBACK. APU FIRE WARNING LIGHT ILLUMINATED AND BELL SOUNDED. APU FIRE EXTINGUISHER DISCHARGED. APU WAS NOT OPERATING. INSPECTED APU COMPARTMENT, NO EVIDENCE OF FIRE NOTED. FOUND APU TAIL PIPE OVERHEAT SENSOR FAULTY. DEFERRED APU PER MEL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,407 hrs · 47,568 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT ENTRY DOOR FUSELAGE STUB FRAME CRACKED AT FWD UPPER CORNER. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,407 hrs · 47,568 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR FWD LOWER CORNER FUSELAGE CUTOUT DOUBLER CRACKED. REPAIRED SKIN PER SWA RA NR 1-353-2299.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 47,407 hrs · 47,568 cycles

DURING SCHEDULED 1/2D CHECK, FOUND PRESS WEB CRACKED, BS 663, RBL 39, AND BS 665, RBL 34. REPAIRED WEB PER TI-353-032.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,406 hrs · 47,567 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 328 FLOORBEAM UPPER SURFACE CORRODED, LBL 28 TO RBL 28. REMOVED AND REPLACED BEAM UPPER CHORD SECTION PER SWA RA NR 1-353-424.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,406 hrs · 47,567 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD RT SIDE CHORD CRACKED, WL 207. REPLACED CHORD SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,406 hrs · 47,567 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 987 FLOORBEAM UPPER SURFACE CORRODED, LBL 45 TO RBL 45. REPAIRED BEAM PER SRM.

Part: RIB — CRACKED (LT WING) · airframe 47,406 hrs · 47,567 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT WING LOWER RIB CHORD CRACKED, STA 135.5, STRINGER 2. REPAIRED RIB PER SWA RA NR 1-357-0847.

Part: FRAME — CRACKED (SERVICE DOOR) · airframe 47,406 hrs · 47,567 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR AFT FRAME CRACKED IN TWO PLACES. REPAIRED FRAME PER SRM AND BAC DRAWING.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,406 hrs · 47,567 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED ON UPPER SURFACE, BS 947, LBL 53. REPAIRED BEAM PER SWA RA NR 1-353-2292.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 47,406 hrs · 47,567 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 294.5 FLOORBEAM UPPER SURFACE CORRODED AROUND NUT CLIP HOLES. REPAIRED BEAM PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,406 hrs · 47,567 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 1.5 INCH LONG CRACK BS 1016 BULKHEAD STRINGER 6L. REPAIRED BULKHEAD PER SWA RA NR 1-353-2291.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,406 hrs · 47,567 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 312 FLOORBEAM UPPER SURFACE AFT FLANGE CORRODED, LBL 10. REPAIRED BEAM PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 47,406 hrs · 47,567 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 663 - 665 PRESSURE WEB HAS 2 CRACKS, LBL 28 AND LBL 32. REPAIRED WEB PER SRM AND T1-353-046.

Part: SKIN — CRACKED (BS 500D)

DURING WALKAROUND INSPECTION, FOUND EXTERNAL FUSELAGE SKIN CRACK, BS 500D, STRINGER JUST BELOW STRINGER 15R. REPAIRED SKIN PER SRM.

Part: BRACKET — LOOSE (GIRT BAR)

DURING SCHEDULED BC2 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT BAR ATTACH BRACKETS LOOSE. TIGHTENED HOLDING BRACKETS PER MM.

Part: BATTERY — DISCHARGED (CABIN)

LOWER AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: LIGHT — LOOSE (CABIN)

FWD EEPLS LIGHT PULLED UP FROM TRACK. REINSTALLED FWD EEPLS LIGHT SECTION PER MM.

Part: COVER — CRACKED (PAX DOORWAY)

AFT ENTRY DOOR EVACUATION SLIDE PRESS GAUGE VIEW LENS CRACKED. REMOVED AND REPLACED SLIDE COVER ASSY PER MM.

Part: SKIN — CRACKED (UPPER FUSELAGE)

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED APPROX BS 500 TO 500A, STRINGER 11R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (NR 1 LE SLAT)

DURING SCHEDULED C1 CHECK, FOUND NR 1 L/E SLAT AUX TRACK SKIN CUTOUT CRACKED. REPAIRED SKIN PER SWA RA NR 1-A57-0691.

Part: BATTERY PACKS — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT LT AND RT DOORS EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BOTH BATTERY PACKS PER MM.

Part: SKIN — CRACKED (BS 500)

DURING SCHEDULED SERVICE CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 500C-500D, STRINGER 10L. REPAIRED SKIN PER SRM.

Part: MODULE — INOPERATIVE (A HYD SYSTEM)

LOSS OF 'A' SYSTEM HYDRAULICS AFTER TAKEOFF. REMOVED AND REPLACED 'A' SYS HYD MODULE AND BOTH CASE DRAIN FILTERS, SYSTEM OPS CHECKED GOOD PER MM.

Part: SLIDE — DEPLOYED (PASSENGER DOOR)

FWD ENTRY DOOR SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (BS 927-395)

DURING SCHEDULED C4 CHECK, FOUND 2 CRACKS ON FUSELAGE SKIN APPROX 3 INCHES LONG, BS 927 STR 25L AND BS 935, STR 24L. REPAIRED SKIN PER SRM.

Part: BLADE — DAMAGED (NR 1 ENGINE)

AT FL 310, FELT AND HEARD A LOUD THUMP, NOTED CHANGE IN NR 1 ENG N2 AND FUEL FLOW INCREASE. ENG VIBRATION MON ROSE TO PLUS 4. PERFORMED CHECKLIST, RAN ON REDUCED POWER. VIBRATION CONTINUED TO SHUTDOWN AT GATE. INSPECTED AND FOUND ICE DAMAGE TO C1 FAN. REPLACED FAN ASSY PER MM. NO OTHER DAMAGE NOTICED.

Part: SKIN — CRACKED (LT WING)

DURING SCHEDULED C2 CHECK, FOUND NR 3 CRACK ON UPPER SURFACE OF FIXED L/E NEAR OUTBD END OF NR 2 SLAT. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED RON CHECK, FOUND 4 IN SKIN CRACK, RT SIDE ABOVE AND BETWEEN CABIN WINDOWS 12-13. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — DOUBLE DRILLED (BS 420-440)

DURING SCHEDULED 1/4 D CHECK, FOUND FLOORBEAM HAS 12 DOUBLE DRILLED HOLES FROM BS 420-440 RBL 13. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 480)

DURING SCHEDULED 1/4 D CHECK, FOUND FLOORBEAM CRACKED UPPER SIDE AT BS 480 RBL 13. REPAIRED PER BOEING SRM.

Part: LAMP — INOPERATIVE (CABIN)

DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR EMERGENCY LIGHT INOP. RELAMPED PER BOEING M/M.

Part: BULKHEAD — DENTED (BS 178)

DURING SCHEDULED C4 CHECK, FOUND PRESSURE BULKHEAD BS 178 DENTED FLOOR LEVEL. REPAIRED PER BOEING SRM.

Part: BULKHEAD — DENTED (BS 1016)

DURING SCHEDULED C4 CHECK, FOUND AFT PRESSURE BULKHEAD DENTED AT FLOOR LEVEL, BS 1016. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 270)

DURING SCHEDULED SERVICE CHECK, FOUND UPPER FUSELAGE SKIN SCRATCHED WITH A DEEP DENT BETWEEN STRINGERS 4 AND 5L, 42 FWD OF FWD ENTRY DOOR. REPAIRED PER BOEING SRM.

Part: ENGINE — FAILED (NR 1)

EXPERIENCED NR 1 ENGINE VIBRATION, FOLLOWED BY A/C YAWING TO THE LEFT. N2 RED WARNING LIGHT ILLUMINATED. ENGINE THROTTLE WAS RETARDED TO IDLE, BUT VIBRATION CONTINUED. CREW PERFORMED ENGINE SHUT-DOWN PROCEDURES. AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING. REPLACED ENGINE ASSEMBLY PER BOEING M/M.

Part: WINDOW — CRACKED (RT COCKPIT)

DURING CLIMBOUT AT 31,000 FEET, NOTED FIRST OFFICER'S SLIDING WINDOW CRACKED. AIRCRAFT RETURNED TO BOI AND MADE AN UNEVENTFUL LANDING. INSPECTED WINDOW AND CONFIRMED TO BE OUTER PANE. REMOVED AND REPLACED WINDOW ASSEMBLY PER BOEING M.M.

Part: FLOORBEAM — CORRODED (BS 294/1016)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 1016 LBL 5 WL 208 AND AT BS 294 AT LBL12 WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: CLIP — CRACKED (BS 500)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 500D, S19R. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: TE SKIN — CRACKED (NR 3 SLAT)

DURING SCHEDULED D-CHECK, FOUND NUMBER 3 SLAT LOWER T/E SKIN CRACKED AT I/B END. REPAIRED PER BOEING DRAWING 65C30133 AND BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DENTED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 500 PLUS 6, STRINGER 23R AT BS 860 STRINGER 26L BETWEEN BS 909 AND 916 STRINGER 24R AND AT BS 330 STRINGER 25L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: DOOR FRAME — CRACKED (BS 492)

DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR AFT FRAME CRACKED AT BS 492 RBL 39 WL 162. REPAIRED PER TRAMCO EWO 95-0497 AND BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DAMAGE (BS 867-887)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CHAFING DAMAGE FROM BS 867 TO 887 BETWEEN S2 LT AND RT. REPAIRED PER TRAMCO EWO 95-0497 AND BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — GOUGED (BS 316)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 316 BELOW S17L AND AT BS 332 BETWEEN S19 AND 20L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 178 WL 189 BL 0. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND TRAMCO EWO 95-0494.

Part: PUMP — INOP (HYD SYST)

DURING CLIMBOUT, EXPERIENCED SYSTEM A HYDRAULIC PRESSURE LOSS. AIRCRAFT RETURNED TO ELP AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND A SYSTEM HYDRAULIC PUMP INOP. REPLACED AND SERVICED SYSTEM PER BOEING M/M.