N316SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,809 hrs · 73,702 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 406, STR 26L. REPAIRED SKIN IAW SWA EA.

Part: LIGHT — LOOSE (CABIN) · airframe 80,811 hrs · 73,703 cycles

DURING SCHEDULED OTS CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT BULBS LOOSE. REMOVED AND REPLACED BULBS IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,809 hrs · 73,702 cycles

DURING SCHEDULED MV1 CHECK FOUND, SKIN CRACKED TA BS 406, STR 26L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,565 hrs · 73,513 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 907, STR 7L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,565 hrs · 73,513 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 727B+6, STR 14L. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOOR STRUCTURE FLOORBEAM CORRODED AT BS 986.5, RBL 43. REPAIRED BEAM IAW EA.

Part: FITTING — CORRODED (GIRT BAR) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 947, BETWEEN STR 19R TO STR 20R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 986 TO BS 1006, STR 25L. REPAIRED STRINGER IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED AT BS 969, STR 25L. REPAIRED STRINGER IAW SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 727D+13, STR 19R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED BETWEEN BS 290 TO BS 312, BETWEEN STR 15R TO STR 18R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 927+16, STR 25R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 500A+3, STR 16L. REPAIRED SKIN PER EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND CREASE BEAM INNER CHORD CRACKED AT BS 639, STR 17L. REPAIRED CHORD IAW EO.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 767 TO BS 807, STR 26L. REPAIRED STRINGER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED BETWEEN BS 904 TO BS 907, BETWEEN STR 18L TO STR 21L. REPAIRED SKIN IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOOR STRUCTURE BEAM LOCATED AT BS 986.5, BETWEEN RBL 43 LBL 53. REPAIRED BEAM EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED BETWEEN BS 727D+13 TO BS 767, BETWEEN STR 17R TO STR 21R. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 26R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 80,083 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500B, STR 16L. REPAIRED SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,083 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 350, BETWEEN STR 12R TO STR 13R. REPAIRED SKIN IAW EA.

Part: SIGN — BROKEN (CABIN) · airframe 80,083 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CORRODED AT BS 500C, BETWEEN STR 28R TO STR 28L. REPAIRED FRAME IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 480 TO BS 500, STR 28R. REPAIRED STRINGER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 867+5, STR 17R. REPAIRED SKIN IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND FWD CEILING EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT GALLEY CEILING EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS IAW MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 500B TO BS 500C, STR 27L. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME WEB CRACKED AT BS 639.1, STR 17R. REPAIRED WEB IAW EA AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 28L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 847 TO BS 867, STR 25R. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 28L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURINGS SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 847, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CRACKED BETWEEN BS 294.5 TO BS 302.3, STR 9L. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURINGS SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 827, STR 26L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 80,053 hrs · 73,109 cycles

DURING SCHEDULED 26Y CHECK FOUND LT FWD GALLEY EMERGENCY FLASHLIGHT BROKEN. REMOVED AND REPLACED FLASHLIGHT IAW MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,065 hrs · 72,366 cycles

DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CORRODED AT BS 380, BETWEEN STR 25R TO STR 26R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,065 hrs · 72,366 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CORRODED AT BS 364, STR 25R. REMOVED AND REPLACED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,065 hrs · 72,366 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 350, STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,961 hrs · 72,292 cycles

DURING SCHEDULED CV CHECK, FOUND CRACK IN FUSELAGE STA 616 +9 ABOVE STR 8L. REPAIRED PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,966 hrs · 72,293 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 787+17, STR 18L. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,966 hrs · 72,293 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 18L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,966 hrs · 72,293 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 635, STR 8L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,966 hrs · 72,293 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 508, STR 21R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 78,966 hrs · 72,293 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,961 hrs · 72,292 cycles

DURING SCHEDULED CV CHECK, FOUND CRACK IN FUSELAGE AT STA 787 +17, ABOVE STR 18L BETWEEN TWO EXISTING REPAIRS. REPAIRED PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,029 hrs · 71,589 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 375, STR 8L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,029 hrs · 71,589 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 435, STR 16L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,029 hrs · 71,589 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 426, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,029 hrs · 71,589 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 506A, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,029 hrs · 71,589 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,029 hrs · 71,589 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 506B, STR 16L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,029 hrs · 71,589 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 16R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,029 hrs · 71,589 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 395, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,029 hrs · 71,589 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 867-3, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,029 hrs · 71,589 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 514, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,029 hrs · 71,589 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 434, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,033 hrs · 71,590 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 500C-4, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,033 hrs · 71,590 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 395, STR 16R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,033 hrs · 71,590 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 867-3, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,033 hrs · 71,590 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 506B, STR 16L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,033 hrs · 71,590 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 16L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,033 hrs · 71,590 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 16L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,033 hrs · 71,590 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 15L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,033 hrs · 71,590 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 15L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,033 hrs · 71,590 cycles

DURING SCHEDULED OTS CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP AT LOWER FWD SIDE. RELAMPED PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 78,033 hrs · 71,590 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 77,920 hrs · 71,505 cycles

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

Part: BATTERY — LOOSE (CABIN) · airframe 77,649 hrs · 71,306 cycles

AFT EMERGENCY EXIT LIGHT BATTERY LOOSE. SECURED BATTERY PER MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 77,474 hrs · 71,163 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 77,236 hrs · 70,968 cycles

L1 DOOR EMERGENCY EVAC SLIDE GAUGE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,236 hrs · 70,968 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 500C, STR 8L. REPAIRED SKIN PER MT.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 76,432 hrs · 70,366 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,432 hrs · 70,366 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 277, STR 15R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 76,401 hrs · 70,341 cycles

DURING SCHEDULED MV1 CHECK, FOUND SHEAR TIE CRACKED AT BS 400, BETWEEN STR 13L TO STR 14L. REPAIRED SHEAR TIE PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,401 hrs · 70,341 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 416, STR 16L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,401 hrs · 70,341 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 406, STR 16L. REPAIRED SKIN PER EA.

Part: MOUNT — OUT OF ADJUST (R1 DOOR SLIDE) · airframe 75,641 hrs · 69,779 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 75,614 hrs · 69,758 cycles

FWD FLASHLIGHT INDICATOR INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: CONTROL ROD — CORRODED (ELEVATOR TAB) · airframe 75,315 hrs · 69,535 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT ELEVATOR TAB OUTBOARD CONTROL ROD CORRODED. REMOVED AND REPLACED ROD ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 294.5, STR 27L. REPAIRED FRAME PER ER.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 74,936 hrs · 69,234 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 669, LBL 24.5. REPAIRED BEAM PER BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 907, BETWEEN STR 23R TO STR 22R. REPAIRED FRAME PER ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 515, STR 28L. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 485 TO BS 495, STR 27L. REPAIRED STRINGER PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO BAY SKIN CORRODED AT BS 737, STR 26L. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND CENTER BOX WING FLOORBEAM LOWER CHORD CRACKED AT BS 663, RBL 24.8. REPAIRED BEAM PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 13R. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 460, STR 26L. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 21L. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, LBL 19, WL 155. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16R. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 25L TO STR 26L. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20L TO STR 21L. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

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

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO BAY RT KEEL BEAM CORRODED AT BS 500D, RBL 7. REMOVED AND REPLACED BEAM PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SECTION CORRODED AT BS 1008, STR 27L. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN RBL 8 TO RBL 15. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 663, STR 8L. REMOVED AND REPLACED SPLICE PER BAC DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND CENTER WING BOX FLOORBEAM CHORD CRACKED AT BS 663, LBL 24.8. REPAIRED BEAM PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO BAY FRAME CRACKED AT BS 500D, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME WEB CRACKED AT BS 639, LBL 65. REPAIRED FRAME PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 908, BETWEEN STR 3L TO STR 4L. REPAIRED SKIN PER ER.

Part: WIRE — BROKEN (CABIN) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND CENTER AISLE EMERGENCY EXIT LIGHT WIRE BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING I/B AFT FLAP T/E DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME WEB CRACKED AT BS 259.5, STR 11L. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

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

Part: LUG — BROKEN (SPOILER ACTUATOR) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 4 SPOILER O/B ACTUATOR LOWER LUG BROKEN. REMOVED AND REPLACED ACTUATOR PER MM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STUB BEAM WEB CRACKED AT BS 639, LBL 65. REPAIRED WEB PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 908, BETWEEN STR 4R TO STR 6R. REPAIRED SKIN PER ER.

Part: FITTING — CORRODED (GIRT BAR) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR CLIP CORRODED. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 947, BETWEEN STR 23L TO STR 24L. REPAIRED SHEAR TIE PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING O/B AFT FLAP T/E DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR SIDEWALL EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER SOPM.

Part: SIGN — BROKEN (CABIN) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND SIDEWALL EMERGENCY EXIT SIGNS BROKEN AT ROW 9. REMOVED AND REPLACED SIGNS PER SRM.

Part: RIB — CORRODED (TE FLAP) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING I/B MID FLAP RIB CORRODED. REMOVED AND REPLACED RIB PER SRM.

Part: WEDGE — PUNCTURED (TE FLAP) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING I/B MIDFLAP T/E WEDGE PUNCTURED. REPAIRED WEDGE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: RIB — CORRODED (TE FLAP) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING I/B MID FLAP RIB CORRODED. REMOVED AND REPLACED RIB ASSY PER BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 480, BETWEEN LBL 16 TO LBL 21. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 188 TO BS 196.5, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND ANGLE CRACKED AT BS 727B, LBL 46. REPAIRED ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 908, BETWEEN STR 22R TO STR 23R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STUB FRAME CHORD CRACKED AT BS 190, WL 207 LT SIDE. REPAIRED CHORD PER SRM.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT BULKHEAD SUPPORT CHANNEL CORRODED AT BS 1017, BL 0. REMOVED AND REPLACED CHANNEL PER SRM.

Part: ATTACH FITTING — CORRODED (TE FLAP) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 2 FLAP TRACK CARRIAGE FORE FLAP ATTACH FITTING CORRODED. REMOVED AND REPLACED FITTING PER OHM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 683, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 683, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,198 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,889 hrs · 69,189 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,578 hrs · 68,956 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 732B, STR 14R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,578 hrs · 68,956 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 731E, STR 14R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,578 hrs · 68,956 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,578 hrs · 68,956 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 727C, STR 14R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,578 hrs · 68,956 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 752, STR 14R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,515 hrs · 68,506 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT BULB INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,515 hrs · 68,506 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT BULB INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,515 hrs · 68,506 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 360, STR 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,145 hrs · 67,930 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,145 hrs · 67,930 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 355 TO BS 357, STR 16R. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,145 hrs · 67,930 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,145 hrs · 67,930 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,145 hrs · 67,930 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,145 hrs · 67,930 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 291, BETWEEN STR 5R TO STR 19R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,145 hrs · 67,930 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,145 hrs · 67,930 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 348, STR 16R. REPAIRED STRINGER PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,145 hrs · 67,930 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 16L. REPAIRED SKIN PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,145 hrs · 67,930 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,145 hrs · 67,930 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,145 hrs · 67,930 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 911, BELOW STR 23R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,145 hrs · 67,930 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,145 hrs · 67,930 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,145 hrs · 67,930 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,145 hrs · 67,930 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,145 hrs · 67,930 cycles

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

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 73,044 hrs · 67,855 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD O/B FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,024 hrs · 67,840 cycles

DURING SCHEDULED CV CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 3 TO ROW 4. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 72,181 hrs · 67,232 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,839 hrs · 66,990 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 779, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,674 hrs · 66,876 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,272 hrs · 66,576 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 502D AND BS 514D, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,272 hrs · 66,576 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 373, STR 26L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,272 hrs · 66,576 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505C, STR 17R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,272 hrs · 66,576 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 512D, STR 21R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,272 hrs · 66,576 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 443, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,750 hrs · 66,195 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 512A, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,750 hrs · 66,195 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505B, STR 15R. REPAIRED SKIN PER SWA EA.

Part: PIN — NOT SEATED (UPLOCK SENSOR) · airframe 70,458 hrs · 66,051 cycles

AIR TURNBACK, RT MLG RED LIGHT DID NOT EXTINGUISH AFTER RAISING LANDING GEAR. RESEATED PIN 3 ON RT MLG UPLOCK SENSOR PER MM.

Part: FITTING — CRACKED (NR 4 SPOILER) · airframe 70,458 hrs · 66,051 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 4 GROUND SPOILER INBOARD FITTING LUG CRACKED. REPAIRED FITTING PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,418 hrs · 65,945 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,418 hrs · 65,945 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,418 hrs · 65,945 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,418 hrs · 65,945 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 390, BL 0. REPAIRED SKIN PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,418 hrs · 65,945 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 11R CRACKED AT BS 947. REPAIRED STRINGER PER SRM.

Part: ROD — WORN (LT ELEVATOR) · airframe 70,418 hrs · 65,945 cycles

DURING SCHEDULED BRDG CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED INPUT ROD PER MM.

Part: ROD — WORN (RT AILERON) · airframe 70,418 hrs · 65,945 cycles

DURING SCHEDULED BRDG CHECK, RT WING AILERON FAILED FREE PLAY CHECK. REMOVED AND REPLACED AILERON OUT PUT ROD PER MM.

Part: SKIN — CRACKED (BS 347 S15R) · airframe 69,489 hrs · 65,250 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT 347, STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 350 S15R) · airframe 69,489 hrs · 65,250 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 350, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 272 S15L) · airframe 69,167 hrs · 64,993 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 272.5, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SLAT — CRACKED (LT WING) · airframe 68,981 hrs · 64,838 cycles

DURING SCHEDULED C4 CHECK, FOUND LEFT WING NR 2 L/E SLAT CRACKED AT FWD INBOARD END. REPAIRED SLAT PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,973 hrs · 64,831 cycles

FUSELAGE SKIN CRACKED AT BS 520, STR 8L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,661 hrs · 64,579 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 751, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,661 hrs · 64,579 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,661 hrs · 64,579 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 764, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,661 hrs · 64,579 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 20L. REPAIRED SKIN PER SRM.

Part: SPOILER — BROKEN (LT WING) · airframe 68,626 hrs · 64,554 cycles

DURING SCHEDULED A2 CHECK, FOUND LEFT WING NR 4 GROUND SPOILER OUTBOARD HINGE LUG BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 68,511 hrs · 64,467 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,193 hrs · 64,234 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 363, STR 8L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,193 hrs · 64,234 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749.5, STR 18L. REPAIRED SKIN PER SWA EA.

Part: KEELBEAM — CORRODED (BS 500D) · airframe 67,180 hrs · 63,461 cycles

DURING SCHEDULED C2 CHECK, FOUND KEELBEAM CORRODED AT BS 500D LT SIDE. REPAIRED KEEL BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,124 hrs · 63,413 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 14R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,080 hrs · 63,379 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 460, STR 16L. REPAIRED SKIN PER SWA EA.

Part: LINK — WORN (RT MLG) · airframe 66,744 hrs · 63,104 cycles

VIBRATION FELT DURING TAKEOFF AND LANDING. REMOVED AND REPLACED RT MLG UPPER AND LOWER TORSION LINKS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 66,430 hrs · 62,854 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,264 hrs · 62,733 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 21R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — DEPLOYED (L1 DOOR) · airframe 66,161 hrs · 62,654 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 66,041 hrs · 62,556 cycles

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

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 65,647 hrs · 62,245 cycles

R2 DOOR EMERGENCY EVAC SLIDE INDICATED LOW PRESSURE. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 65,287 hrs · 61,973 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: ACTUATOR — BROKEN (NR 4 SPOILER) · airframe 65,231 hrs · 61,926 cycles

DURING SCHEDULED A2 CHECK, FOUND LT WING NR 4 SPOILER, OUTBOARD ACTUATOR ROD BROKEN. REMOVED AND REPLACED SPOILER ACTUATOR PER MM.

Part: SKIN — CRACKED (BS 810 S8L) · airframe 64,877 hrs · 61,651 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 810, STR 18L. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 64,677 hrs · 61,503 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SKIN — CRACKED (BS 948) · airframe 64,328 hrs · 61,234 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 948, STR 23R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 500D-512D) · airframe 64,265 hrs · 61,189 cycles

DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 500D TO BS 512D, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 63,843 hrs · 60,861 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: FRAME — CRACKED (BS 440) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 23R. REPAIRED FRAME PER SRM.

Part: RIB — CRACKED (RT WING) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND RIGHT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 & STR 3. REPAIRED RIB PER BFG ER.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 7L. REPAIRED WEB PER BFG ER & SRM.

Part: FRAME — CRACKED (BS 847) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847 AND AFT CARGO DOOR CUT OUT NR 5 STOP FITTING. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (BS 492) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, FWD CARGO DOOR CUTOUT. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (BS 515) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515, STR 16L. REPAIRED SKIN PER BFG ER.

Part: FLOOR SUPPORT — CRACKED (BS 706) · airframe 63,632 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CRACKED AT BS 706, RBL 25, WL 203. REPAIRED FLOOR SUPPORT PER BFG ER.

Part: STRINGER — CORRODED (BS 515) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STR CORRODED AT BS 515, STR 26L. REPAIRED STR PER SRM.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL STAB ATTACH FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.

Part: STRINGER CLIP — CRACKED (BS 294.5) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (BS 309-349) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED BETWEEN BS 309 TO BS 349, LBL 55 TO LBL 61, WL. 208. REPAIRED WEB PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 63,362 hrs · 60,464 cycles

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

Part: BULKHEAD — CRACKED (BS 1016) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT AFT SIDE, LBL 40, WL 209. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (BS 597) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (BS 500D) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (BS 967) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 967, BETWEEN STR 6L TO STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (COCKPIT FLOOR) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOOR Z-CHORD CORRODED AT BS 270, BETWEEN LBL 11 TO RBL 11. REPAIRED Z-CHORD PER SRM.

Part: FRAME — CRACKED (BS 360) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 400) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 827) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 807) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 9R. REPAIRED FRAME PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 63,362 hrs · 60,464 cycles

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

Part: FRAME — CRACKED (BS 787) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 887) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 578, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 727E) · airframe 63,362 hrs · 60,464 cycles

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

Part: FRAME — CRACKED (BS 867) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 480) · airframe 63,362 hrs · 60,464 cycles

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

Part: SHEAR TIE — CORRODED (BS 787) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, RBL 7. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 639) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-HECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 7R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 294) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED AT BS 294.5, BETWEEN STR 11L & STR 12L. REMOVED AND REPLACED CLIPS PER SRM.

Part: STRINGER — CORRODED (BS 787-807) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CORRODED BETWEEN BS 787 TO BS 807, STR 26R. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (BS 787) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 787, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706) · airframe 63,362 hrs · 60,464 cycles

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

Part: FLOORBEAM — CORRODED (BS 294.5) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM UPPER CHORD CORRODED AT BS 294.5, BETWEEN LBL 12 TO RBL 12. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED AT BS 663, STR 10L & STR 10R. REMOVED AND REPLACED CLIPS PER SRM.

Part: STRINGER — CORRODED (BS 438) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 438, STR 27L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (BS 685) · airframe 63,362 hrs · 60,464 cycles

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

Part: SHEAR TIE — CRACKED (BS 639) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 639, BETWEEN STR 7L TO STR 8L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 882) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 882, STR 19L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (BS 827) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 827, BETWEEN LBL 4 TO RBL 4. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 907) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 1. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 328) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (BS 500) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500, LBL 18. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (BS 616) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 616, BETWEEN STR 7R TO STR 8R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 827) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 827, LBL 17. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 663) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 2L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A) · airframe 63,362 hrs · 60,464 cycles

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

Part: STRINGER — CORRODED (BS 447) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 447, STR 26L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (BS 597) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 597. REMOVED AND REPLACED CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (BS 747) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 747, LBL 9. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (BS 787 - 807) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 787 TO BS 807, WL 208. REPAIRED CREASE BEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 328, LBL 39. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 312) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM UPPER CHORD CORRODED AT BS 312, BETWEEN LBL 12 TO RBL 12. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706) · airframe 63,362 hrs · 60,464 cycles

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

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 63,362 hrs · 60,464 cycles

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

Part: SHEAR TIE — CORRODED (BS 787) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, LBL 16. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 597) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED AT BS 597, BETWEEN STR 7R TO STR 9R. REMOVED AND REPLACED CLIPS PER SRM.

Part: CREASE BEAM — CRACKED (BS 578.5) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE CREASE BEAM WEB CRACKED AT BS 578.5, RBL 66. REPAIRED CREASE BEAM WEB PER SRM.

Part: STRINGER — CORRODED (BS 867) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 867, STR 26R. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (BS 500) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500, RBL 12. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 500A) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500A, LBL 18. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616) · airframe 63,362 hrs · 60,464 cycles

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

Part: STRINGER CLIP — CORRODED (BS 947) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CORRODED AT BS 947, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 827) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 20L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (BS 500) · airframe 63,362 hrs · 60,464 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500, RBL 12. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,495 hrs · 58,990 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 450, BETWEEN STRINGERS 28R AND 28L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,495 hrs · 58,990 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR CUTOUT LOWER FWD CORNER CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,495 hrs · 58,990 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 946.5, STRINGER 11R, CRACKED. REPAIRED SKIN PER EA.

Part: WEDGE — DELAMINATED (NR 4 SLAT) · airframe 61,485 hrs · 58,983 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 L/E SLAT WEDGE DELAMINATED. REPAIRED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,485 hrs · 58,983 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 270, STRINGER 10L, CRACKED. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 60,539 hrs · 58,269 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,539 hrs · 58,269 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 272, STRINGER 15R, CRACKED. REPAIRED SKIN PER EA.

Part: SIGN — CRACKED (EMERGENCY LIGHT) · airframe 60,539 hrs · 58,269 cycles

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT SIGN ABOVE FWD SERVICE DOOR CRACKED. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 60,539 hrs · 58,269 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: ACTUATOR — LEAKING (LT WING SPOILER) · airframe 60,346 hrs · 58,111 cycles

AIR TURNBACK, B-HYDRAULIC SYSTEM QUANTITY WENT TO ZERO AND LOW PRESSURE LIGHTS ILLUMINATED. REMOVED AND REPLACED CAP AND O-RING ON NR 2 SPOILER ACTUATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,704 hrs · 57,573 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT EXTERNAL AIR CONDITION HOOK UP CUTOUT FWD RT CORNER, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,704 hrs · 57,573 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 735, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,704 hrs · 57,573 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 953, STRINGER 24L, BS 967, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA.

Part: SIGN — CRACKED (EMERGENCY LIGHT) · airframe 59,309 hrs · 57,238 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD AISLE CABIN OVERHEAD EMERGENY EXIT SIGN CRACKED. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 58,827 hrs · 56,866 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING NR 2 L/E SLAT SKIN AT INBOARD EDGE CRACKED. REPAIRED SLAT SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,745 hrs · 56,799 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 927, STRINGER 24, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,745 hrs · 56,799 cycles

FUSELAGE SKIN AT BS 780, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM.

Part: PROXIMITY SENSOR — FAULTY (LT MLG) · airframe 58,513 hrs · 56,612 cycles

LT MLG UNSAFE LIGHT ILLUMINATED. RECYCLED GEARS, NO HELP. REMOVED AND REPLACED LT MLG UPLOCK PROX SWITCH. OPS CK GOOD PER MM.

Part: SLIDE — OUT OF ADJUST (SERVICE DOOR) · airframe 56,919 hrs · 55,311 cycles

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

Part: STRAP — CRACKED (FUSELAGE) · airframe 56,098 hrs · 54,657 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BLKHD STRAP CRACKED AT BL 0, WL 175 TO WL 242. REPAIRED STRAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,095 hrs · 54,655 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 13R. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,095 hrs · 54,655 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 10R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 56,095 hrs · 54,655 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED RT OVERWING EMERGENCY EXIT LIGHT LENS PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,095 hrs · 54,655 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 12R AND 13R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,095 hrs · 54,655 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 11R AND STR 12R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,095 hrs · 54,655 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGERS CRACKED (2 EA) AT BS 395 AT STR 16L AND BS 364 AT STR 15L. REPAIRED STRINGERS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,095 hrs · 54,655 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 12L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,095 hrs · 54,655 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 12L AND STR 13L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,095 hrs · 54,655 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,095 hrs · 54,655 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 56,030 hrs · 54,604 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 55,384 hrs · 54,140 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CAPT'S UPPER WINDOW POST CRACKED. REPAIRED WINDOW POST PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,375 hrs · 54,133 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,375 hrs · 54,133 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 505 AND BS 508, ABOVE STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,375 hrs · 54,133 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,375 hrs · 54,133 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727A + 16, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,375 hrs · 54,133 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED ( 8 EA ) AT STR 4R, BS 727D + 19, BS 727E + 1, BS 727E + 13, BS 727E + 14, BS 727E + 15, BS 758, BS 761.5 & BS 777. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,375 hrs · 54,133 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 810, STR 10R. REPAIRED SKIN PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,375 hrs · 54,133 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED ( 4 EA ) AT STR 14L, BS 430, BS 460, BS 471 & BS 500. REPAIRED SKIN PER SRM.

Part: FITTING — LOOSE (FWD SVC DOOR) · airframe 55,375 hrs · 54,133 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD ATTACH FITTING LOOSE. R&R FASTENERS PER SRM.

Part: SLIDE — CRACKED (FUSELAGE) · airframe 55,375 hrs · 54,133 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,153 hrs · 53,949 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED (4 EA) ABOVE STR 4R, AT BS 747, BS 755, BS 767 AND BS 775. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 54,460 hrs · 53,395 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,440 hrs · 53,381 cycles

DURING SCHEDULED RON, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 54,281 hrs · 53,246 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 54,157 hrs · 53,146 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 54,157 hrs · 53,146 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING INBD T/E FORE FLAP DELAMINATED AT UPPER SURFACE. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELGE) · airframe 54,157 hrs · 53,146 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED 2 LONG, BS 360, STRINGER 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,053 hrs · 53,056 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW CUTOUT CRACKED AT RT WINDOW NR 11. REPAIRED FRAME PER BFG ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,053 hrs · 53,056 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 489, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,761 hrs · 52,538 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 14R, BS 500A AND BETWEEN BS 373 AND BS 374. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,053 hrs · 53,056 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 439, STR 14R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,053 hrs · 53,056 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C PLUS 15, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,052 hrs · 53,055 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 809, ABOVE STR 10R. REPAIRED SKIN PER SRM.

Part: TEE CHORD — CRACKED (FUSELAGE) · airframe 54,052 hrs · 53,055 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BOTH INBOARD AND OUTBOARD T-CHORDS CRACKED AT BS 178 WL 184 AND LBL 5.7. REPAIRED T-CHORDS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,052 hrs · 53,055 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 789, ABOVE STR 10R. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 54,052 hrs · 53,055 cycles

DURING SCHEDULED D CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 213 AND RBL 5.7 AND WL 200 AND LBL 5.7. REPAIRED BULKHEAD WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,052 hrs · 53,055 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIPS CRACKED (2 EA) AT STR 4R, BS 616 AND BS 639. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,164 hrs · 52,334 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,164 hrs · 52,334 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 4R, BS 727D AND 727E. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,111 hrs · 52,282 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500D PLUS 16, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,800 hrs · 52,009 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT STR 10R, BETWEEN BS 496 AND BS 505 AND STR 15R, BS 505. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,356 hrs · 51,639 cycles

DURING SCHEDULED BC2 CHECK, FOUND FUSELAGE SKIN CRACKS (2 EA) AT STR 10R, BS'S 430 AND 450. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,185 hrs · 51,507 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, BETWEEN STR'S 11L AND 13L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,185 hrs · 51,507 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 10L, BS 360 AND BETWEEN BS 727A AND BS 727 B. REPAIRED SKIN PER SRM.

Part: SENSE LINE — OUT OF ADJ (RT MLG) · airframe 37,939 hrs · 24,111 cycles

AIR TURNBACK, AFTER T/O, LANDING GEAR HANDLE WOULD NOT GO THE UP POSITION. ADJUSTED GROUND SENSE CABLE, OPS CK GOOD PER MM.

Part: ACTUATOR — WORN (NLG) · airframe 51,279 hrs · 50,762 cycles

NOSE GEAR MAKES A GRINDING NOISE DURING EXTENSION. REMOVED AND REPLACED NLG RETRACT ACTUATOR AND NLG DOOR RT CRANK ARM ASSY.

Part: FLAP — DEBONDED (LT WING) · airframe 50,619 hrs · 50,216 cycles

DURING SCHEDULED C4 CHECK, FOUND LT OUTBOARD T/E FORE FLAP DISBONDED AT UPPER INBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: FLAP — DELAMINATED (LH WING) · airframe 50,619 hrs · 50,216 cycles

DURING SCHEDULED C4 CHECK, FOUND LH OTBD AFT T/E FLAP DELAMINATED AT INBD END. R&R FLAP PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,537 hrs · 50,146 cycles

DURING SCHEDULED PM CHECK, FOUND STRINGER CRACKED AT BS 747,STR 19L. REPAIRED STR PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,841 hrs · 49,576 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FRAME CRACKED AT BS 727E, STR 18R, WL 208. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,739 hrs · 49,493 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKINS CRACKED AT BS 520, STR 12R & BS 482, STR 10R. REPAIRED SKINS PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,739 hrs · 49,493 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 10R. REPAIRED SKIN PER SWA RA.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 49,145 hrs · 48,981 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 48,848 hrs · 48,723 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 47,872 hrs · 47,911 cycles

DURING SCHEDULED C1 CHECK, FOUND NR 2 L/E SLAT LOWER SKIN CRACKED NEAR OUTBD MID TRACK CUT OUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,872 hrs · 47,911 cycles

DURING SCHEDULED C1 CHECK, FOUND 2 EA FUSELAGE EXT SKIN CRACKS, BS 520, STR 10R AND BS 747, STR 18R. REPAIRED SKIN SECTIONS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,632 hrs · 47,711 cycles

DURING WALKAROUND INSPECTION FOUND 2 INCH LONG EXTERNAL FUSELAGE SKIN CRACK, STR 15L, BETWEEN BS 500C & 500D. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (RT/LT WING) · airframe 47,389 hrs · 47,508 cycles

DURING SCHEDULED 1/2D CHECK, FOUND EXTERNAL EMERGENCY LIGHTS INOP AFT OF RT AND LT WINGS. REPAIRED EVAC LIGHT SYSTEM PER MM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 47,389 hrs · 47,508 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, RBL 37 TO LBL 37, WL 208. REPAIRED FLOORBEAM PER ER 00-1103 & SRM.

Part: RIB — CRACKED (LT WING) · airframe 47,389 hrs · 47,508 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT WING INTERNAL RIB CRACKED AT WBL 135.5, BETWEEN STR S-2 & S-3. REPAIRED RIB PER ER 00-1051A.

Part: ATTACH ANGLE — CRACKED (BULKHEAD) · airframe 47,389 hrs · 47,508 cycles

DURING SCHEDULED D-CHECK, FOUND BS 663 BULKHEAD WEB ATTACH ANGLE CRACKED AT RBL 6 TO LBL 6, WL 171.5.

Part: FITTING — CRACKED (LT MLG) · airframe 47,389 hrs · 47,508 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT MLG FITTING CRACK EXTENDING FROM UPPER HOLE TO THE EDGE OF THE REAR SPAR CHORD. REPLACED UPPER REAR SPAR CHORD FROM RSS 285 TO THE INBD END PER ER 00-1071.

Part: STIFFENER — CRACKED (MLG WW) · airframe 47,389 hrs · 47,508 cycles

DURING SCHEDULED D-CHECK, FOUND 2 CRACKED STIFFENERS AT BS 663 BULKHEAD, LBL 6.15 & RBL 6.15. REMOVED AND REPLACED STIFFENERS PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 47,389 hrs · 47,508 cycles

DURING SCHEDULED D-CHECK, FOUND ATTACH ANGLES CRACKED BS 658 TO BS 663, LBL 8 & RBL 8, WL 170.

Part: CREASE BEAM — CRACKED (CABIN) · airframe 47,389 hrs · 47,508 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM SHEAR WEB CRACKED AT BS 927 - 951, RBL 57, WL 208. REPAIRED CREASE BEAM PER SRM.

Part: SHEAR TIE — CRACKED (CABIN) · airframe 47,389 hrs · 47,508 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED SHEAR TIE AT BS BS 400, STR 13R - 14R. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 47,389 hrs · 47,508 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 947, RBL 54 - LBL 54. REPAIRED FLOORBEAM PER SWA T1-453-037.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 47,389 hrs · 47,508 cycles

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM AT BS 312, LBL 10 - RBL 10. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 47,389 hrs · 47,508 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 54 - LBL 54, WL 208. REPAIRED FLOORBEAM PER SRM, T1-453-037 AND ESR034.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 47,389 hrs · 47,508 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORROSION AT BS 344, RBL 10 - LBL 55, WL 208. REPAIRED FLOORBEAM PER MM.

Part: FRAME — CORRODED (AFT CARGO BAY) · airframe 47,389 hrs · 47,508 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME CORRODED AT BS 794, RBL 10, WL 152. REPAIRED FRAME PER SRM.

Part: BRACKET — LOOSE (AFT ENTRY DOOR) · airframe 47,389 hrs · 47,508 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EVAC SLIDE GIRT BAR AFT FLOOR BRACKET LOOSE. REMOVED AND REPLACED BRACKET PER MM.

Part: WEB — CRACKED (CENTER BOX) · airframe 47,389 hrs · 47,508 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED BULKHEAD WEB, BS 663, WL 163, RBL 13. REPAIRED CRACKED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (CABIN) · airframe 47,389 hrs · 47,508 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED, BS 597, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,389 hrs · 47,508 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD LT AND RT SIDE CHORDS CRACKED, WL 205 - 208. REPAIRED CHORD SECTIONS PER ACO.

Part: FITTING — WORN (LT ELEVATOR) · airframe 46,934 hrs · 47,118 cycles

DURING SCHEDULED BC4 CHECK, FOUND LT ELEV TAB I/B HINGE HAS EXCESSIVE PLAY. REMOVED AND REPLACED ELEV TAB HINGE FITTING ASSY PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 46,649 hrs · 46,881 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER DURING DOOR CLOSING. REINSTALLED SLIDE ASSY PER MM.

Part: CABLE — OUT OF POSITION (ESCAPE SLIDE) · airframe 46,008 hrs · 46,345 cycles

DURING SCHEDULED -C3- CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE RELEASE CABLE OUT OF POSITION. REPOSITIONED RELEASE ASSY PER MM.

Part: SKIN — CRACKED (BS 500D)

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED 4 INCHES LONG, BS 500D, STRINGER 10R. REPAIRED SKIN PER SRM..

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED SEVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 727C, STRINGER 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 927)

DURING SCHEDULED SEVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 927, STRINGER 24R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP ON AFT END. REMOVED AND REPLACED COVER PLUG ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE)

DURING WALK AROUND CHECK, FOUND A 4 INCH LONG CRACK ON FUSELAGE SKIN RT SIDE, JUST FWD OF REAR BAG BIN. REPAIRED SKIN PER SRM.

Part: CONNECTOR — LOOSE (CABIN)

DURING SCHEDULED C2 CHECK, FOUND RT EMERG EXIT LIGHT INOP. REINSTALLED CANNON PLUG AND OP CHECKED PER BOEING M/M.

Part: BUSHING — WORN (LT ELEV)

VIBRATION IN CRUISE FLIGHT. STRUCTURE, FELT IN YOKE AND FLOOR OF AIRCRAFT. FLIGHT ATTENDANTS REPORTED REAR OF AIRCRAFT WAS VERY BAD. FOUND WORN BUSING O/B LT ELEV TAB. REMOVED AND REPLACED BUSHING PER M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED C1 CHECK, FOUND R-1 DOOR LOWER EMERGENCY EXIT SIGN IS UNSECURED. REMOVED AND REPLACED LIGHT PER BOEING MM.

Part: FLOORBEAM — CORRODED (BS 767-787)

DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED FLOORBEAM UPPER AND LOWER SURFACE AT BS 770 LBL 17, FLOORBEAM AT BS 767 TO 787 RBL 13 UPPER SRFC, BS 770 RBL 3 AND BS 787 TO 847 LBL 12. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 520)

DURING SCHEDULED SERVICE CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 520 LT SIDE BETWEEN NR 11 AND 12 WINDOW BELOW STR 15. REPAIRED PER BOEING SRM.

Part: SKIN — DAMAGED (BS 460)

DURING SCHEDULED SERVICE CHECK, FOUND LIGHTNING STRIKE DAMAGED AT BS 460 UPPER LEFT CROWN AREA. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING WALKAROUND CHECK, FOUND APPROX 4 SKIN CRACK RT SIDE OF FUSELAGE ABOVE NR 9 CABIN WINDOW. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 515)

DURING SCHEDULED A2 CHECK, FOUND CRACKED APPROX 4 FEET LONG AT BS 515, STR 14, ABOVE NR 9 WINDOW RT SIDE OF A/C. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 770)

DURING SCHEDULED 1/4 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 770, AT RBL 3. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 770)

DURING SCHEDULED 1/4 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 770, AT RBL 3. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 727)

DURING SCHEDULED RON CHECK, FOUND STRINGER 18A AT S 727, 1 INCH CRACK PASSING THROUGH FASTENER HOLE TO AFT EDGE OF WEB. REPAIRED PER SWA ACO 6580-53.

Part: SKIN — CRACKED (BS 930)

DURING SCHEDULED TERMINAL CHECK, FOUND A 2 INCH FUSELAGE SKIN CRACK AT BS 930, AT S23L. REPAIRED SKIN PER BOEING SRM.

Part: SKIN — CRACKED (BS 958)

DURING SCHEDULED TERMINAL CHECK, FOUND A 4 INCH FUSELAGE SKIN CRACK AT BS 958, AT S20L. REPAIRED SKIN PER BOEING SRM.

Part: FAIRING — DAMAGED (LT WING/FUS)

LT WING TO BODY FAIRING DAMAGED FROM LT FLAP AND MID FLAP. FAIRING REMOVED AND REPAIRED, D-VELCO WORK ORDER SSR 336, REPAIR STATION DIRR408N, REINSTALLED FAIRING.

Part: SKIN — CRACKED (BS 970)

DURING SCHEDULED C4 CHECK, FOUND AFT FUSELAGE SKIN CRACKED AT BS 970, S21L AND AT BS 944 AT S24L. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 312)

DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL CRACKED AT BS 312, S4L. REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (HORZ STAB)

DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB CENTER SECTION RT THRUST BEAM UPPER I/B ATTACH ANGLE CRACKED AT BS 1113. REPLACED PER BOEING SRM.

Part: CLIP — CRACKED (BS 616/277)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED BS 616, S5L, S8R AND AT BS 277, S10 AND 11R. REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND FUSE SKIN CRACKS AT BS 178 WL 217 LBL 11 TO 12, AT WL 218 RBL 10 TO 12, AT WL 212 TO 213 RBL 5, AT WL 200 TO 201 RBL 5, AT WL 197 TO 199 LBL 5 AND WL 201 TO 202.5 LBL 5. REPAIRED PER BOEING SRM.

Part: SPLICE — CRACKED (BS 360)

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, S15L. REPLACED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 333)

DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AND STRINGER AT BS 333, S8R. REPLACED PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 360)

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED BETWEEN S15L AND 14L, BS 360, WL 228. REPLACED PER BOEING SRM.

Part: DOOR FRAME — CRACKED (BS 294.5)

DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED, BS 294.5, WL 208, RBL 54. REPAIRED PER BOEING SRM.

Part: CLIPS — CRACKED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND THE FOLLOWING STRINGER CLIPS CRACKED: S10 AND 11R AT BS 277, S8L AT BS 685, S10L AT BS 663, S5L AND S8R AT BS 616, S8L AT BS 639, S19R AT BS 500D, S22L AT BS 380, S19 TO 20L AT BS 938, S8L AT BS 616. REPLACED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 475)

DURING SCHEDULED D-CHECK, FOUND STRINGER FLANGE CRACKED AT BS 475, S22R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178 WL 200 TO 201 RBL 5. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 570)

DURING SCHEDULED D-CHECK, FOUND SKATE ANGLE CRACKED AT BS 570 LBL 46 TO 51, WL 170. REPLACED PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 616)

DURING SCHEDULED D-CHECK, FOUND SHEAR TIES CRACKED AT BS 616 BETWEEN S7 AND 8L, BETWEEN S15 AND 14L, BS 360, WL 228. REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 380)

DURING SCHEDULED D-CHECK, FOUND CRACK IN SKIN AT AFT EDGE OF EQUIPMENT COOLING EXHAUST, BS 380 LBL 5 WL 148. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 328)

DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOORWAY LOWER AFT CORNER SKIN CRACKED AT BS 328 RBL 64 WL 210. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 328 RBL 10 WL 208. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5 LBL 5 TO RBL 32 WL 208 AND 207. REPAIRED PER TRAMCO EWO 95-0727.

Part: SKIN — DAMAGED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 318 BETWEEN 18 AND 19, BS 356 BETWEEN S23 TO 24R, BS 818 LBL 7 RBL 12 WL 151, BS 767 BETWEEN S19 AND 20L AND AT BS 203.8 LBL 21 WL 172. REPAIRED PER BOEING SRM.

Part: SKIN — DAMAGED (BS 360-971)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AND DENTED FROM BS 360 TO 375 BETWEEN S4 AND 6L AND AT BS 962 TO 971 BETWEEN S19 TO 20L. REPAIRED PER BOEING SRM.

Part: FRAME — GOUGED (BS 294.5)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME GOUGED AT BS 294.5, RIGHT SIDE AT S4R. REPAIRED PER BOEING SRM.

Part: FRAMES — CRACKED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 294 S7R, BS 616 S9L, BS 787 S9L, BS 907 S9L, BS 827 S9L, BS 867 S9L, BS 847 S9L, AND BS 887 S9L. REPAIRED ALL PER BOEING SRM.

Part: FRAME — CRACKED (BS 616)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE LEFT FRAME I/B CHORD CRACKED AT LOWER FASTENER HOLE, BS 616 WL 200. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 333)

DURING SCHEDULED D-CHECK, FOUND WEB AND STRINGER CRACKED AT BS 333, S8R. REPAIRED STRINGER AND REPLACED WEB PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178 WL 218 RBL 10 TO 12 AND AT WL 217 LBL 11 TO 12, BS 178 WL 212 TO 213 RBL 5. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 294.5)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE LEFT FRAME CRACKED AT BS 294.5 WL 208 RBL 54. REPAIRED PER BOEING SRM.

Part: SPLICE — CRACKED (BS 907)

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, S4R. REPLACED PER BOEING SRM.