N507SW

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,520 hrs · 65,631 cycles

EXTERIOR EMERGENCY LIGHT NEAR AFT CARGO INOP. RELAMPED PER AMM, OPS OK.

Part: CASTING — LOOSE (SPOILER) · airframe 69,406 hrs · 65,512 cycles

LEFT WING I/B NR 4 GROUND SPOILER ACTUATOR CASTING BROKEN. REMOVED AND REPLACED NR 4 GROUND SPOILER PER M/M.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,232 hrs · 65,315 cycles

RIGHT EMERGENCY EXIT LIGHT INOP BETWTEEN ROW 8 TO ROW 9. CHARGED BATTERY PACK IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,189 hrs · 64,625 cycles

FUSELAGE SKIN CRACKED AT BS 520+18 BETWEEN STR 28L & STR 28R. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,189 hrs · 64,625 cycles

SKIN CRACKED AT BS 767 +15.5, STR 23L. REPAIRED SKIN IAW ER AND EA.

Part: SIGN — LOOSE (CABIN) · airframe 66,770 hrs · 63,717 cycles

LT OVERWING EMERGENCY EXIT SIGN LOOSE. RE-INSTALLED SIGN PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,376 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 660 TO BS 673, LBL 24.5. REPAIRED CHORD IAW ER AND EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,377 hrs · 64,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 1010, STR 5R. REPAIRED STRINGER IAW ER AND EA.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND LOWER CHORD CORRODED AT BS 227, BETWEEN STR 27L TO STR 28L. REPAIRED CHORD IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 12Y CHECK, FOUND SKIN CRACKED AT BS 656, STR 4R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,376 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 870, STR 24R. REPAIRED SKIN IAW ER AND EA.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 66,376 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND BEAR STRAP IS CRACKED AT FWD GALLEY DOOR CUTOUT UPPER AFT CORNER. REPAIRED BEAR STRAP IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,376 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 761.5, BL 0. REPAIRED SKIN IAW ER AND EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 5R. REMOVED AND REPLACED SPLICE IAW ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 294, STR 7R. REPAIRED FRAME PER ER.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED SPLICE IAW ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 950, STR 23R. REPAIRED STRINGER IAW EA.

Part: WEB — CRACKED (NLG WW) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND NLG WHEEL WELL LT WEB CRACKED BETWEEN BS 246 TO BS 247, WL 168. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME INNER CHORD WEB CRACKED AT BS 807, STR 25L. REPAIRED WEB IAW ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 476, STR 26L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 943, STR 23R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 919, STR 23R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 466, STR 22L. REPAIRED SKIN IAW ER.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED SPLICE IAW ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 639, RBL 45. REPAIRED WEB IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, RBL 45. REPAIRED BEAM IAW EA.

Part: RESISTOR — BROKEN (COCKPIT) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT COCKPIT DOME LIGHT RESISTOR R340 BROKEN LEADS. REMOVED AND REPLACED RESISTOR PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 1016, WL 210. REPAIRED WEB IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 1010, STR 4L. REPAIRED STRINGER IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 639, LBL 45. REPAIRED WEB IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT FLOOR CHANNEL CORRODED AT BS 773, LBL 12.5. REPAIRED CHANNEL IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED SPLICE IAW ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 334, STR 11R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 13R. REMOVED AND REPLACED CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME O/B CHORD CRACKED AT BS 639, STR 16R. REPAIRED FRAME IAW ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 21R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 20L. REMOVED AND REPLACED CLIP IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 807, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM AND MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 20R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT STRINGER CORRODED BETWEEN BS 967 TO BS 997, STR 25L. REPAIRED STRINGER IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD GALLEY DOOR AFT FRAME CRACKED AT I/B EDGE OF CUTOUT. REPAIRED FRAME PER SRM.

Part: SUPPORT FITTING — CORRODED (GIRT BAR) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR FWD GIRT BAR FITTING SUPPORT CORRODED AT BS 312, LBL 55. REPAIRED SUPPORT IAW SRM AND DWG.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND BUTT SPLICE STRAP CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED SPLICE STRAP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 16R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER MM AND SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 807, BETWEEN STR 27L TO STR 26L. REPAIRED FRAME PER MM AND SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 16R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 16L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: TAB — DELAMINATED (AILERON) · airframe 66,377 hrs · 63,463 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING AILERON TAB O/B END DELAMINATED. REPAIRED TAB IAW SRM AND DWG.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 66,376 hrs · 63,463 cycles

R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,709 hrs · 62,996 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 360+5, STR 15R. REPAIRED SKIN PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,709 hrs · 62,996 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CRACKED AT BS 370, STR 15R. REMOVED AND REPLACED STRINGER EPR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,709 hrs · 62,996 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 400+10, STR 16R. REPAIRED SKIN PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,709 hrs · 62,996 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CRACKED AT BS 360+3.5, STR 15R. REMOVED AND REPLACED STRINGER PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,709 hrs · 62,996 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 380+15, STR 15R. REPAIRED SKIN PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,709 hrs · 62,996 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CRACKED AT BS 360+15.75, STR 15R. REMOVED AND REPLACED STRINGER PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,709 hrs · 62,996 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CRACKED AT BS 360+14.25, STR 15R. REMOVED AND REPLACED STRINGER PER EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 65,709 hrs · 62,996 cycles

DURING SCHEDULED RON CHECK, FOUND RT HORIZONTAL STABILIZER CRACKED BETWEEN STA 105.7 TO STA 180. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,709 hrs · 62,996 cycles

DURING SCHEDULED OTS CHECK FOUND, SKIN CRACKED AT BS 360+15, STR 15L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,707 hrs · 62,995 cycles

DURING SCHEDULED MV2 CHECK FOUND, SKIN CRACKED AT BS 380+10, STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,707 hrs · 62,995 cycles

DURING SCHEDULED MV2 CHECK FOUND, SKIN CRACKED AT BS 360+5, STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,707 hrs · 62,995 cycles

DURING SCHEDULED MV2 CHECK FOUND, SKIN CRACKED AT BS 360+10, STR 15L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,707 hrs · 62,995 cycles

DURING SCHEDULED MV2 CHECK FOUND, SKIN CRACKED AT BS 400+10, STR 16R. REPAIRED SKIN PER SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 65,045 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND H-STRAP CRACKED AT BS 307, STR 10L. REMOVED AND REPLACED H-STRAP PER ER AND EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,045 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND ANGLE WEB CRACKED BETWEEN BS 295 TO BS 297, STR 16L. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,045 hrs · 62,566 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,045 hrs · 62,566 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 482, BETWEEN STR 19R TO STR 22R. REPAIRED FRAME PER SRM.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 64,189 hrs · 61,954 cycles

EMERGENCY EXIT LIGHT "NOT ARMED" KORRY LIGHT INOP. RELAMPED KORRY LIGHT PER MM.

Part: LENS — BROKEN (CABIN) · airframe 64,189 hrs · 61,954 cycles

R2 DOOR EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,125 hrs · 61,908 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 15. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,125 hrs · 61,908 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 20. REPAIRED PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 64,067 hrs · 61,864 cycles

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

Part: SKIN — DELAMINATED (SPOILER) · airframe 64,067 hrs · 61,864 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING I/B GROUND SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SPINDLE — CRACKED (TE FLAP) · airframe 62,958 hrs · 61,060 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING T/O FLAP NR 2 CARRIAGE SPINDLE CRACKED. REMOVED AND REPLACED NR 2 SPINDLE PER EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 62,800 hrs · 60,941 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,543 hrs · 60,756 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 791, STR 17L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,543 hrs · 60,756 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 495, STR 15R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,539 hrs · 60,755 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 791, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,539 hrs · 60,755 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 492B, STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,539 hrs · 60,755 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 482, STR 15R. REPAIRED SKIN PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 62,514 hrs · 60,735 cycles

LOWER EMERGENCY EXIT SIGN LENS COVER LOOSE. SECURED COVER PER EA.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 62,502 hrs · 60,729 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RECONNECTED LIGHT ASSY PER MM.

Part: BRAKE ASSY — FAULTY (LT MLG) · airframe 62,107 hrs · 60,459 cycles

ABORTED TAKEOFF, A/C LURCHED LEFT ON T/O ROLL; ENGINE PARAMETERS NORMAL. ABORTED AT 85 KIAS; FELT LIKE TIRE OR BRAKE LOCKED. REMOVED AND REPLACED NR 2 MAIN WHEEL ASSY AND NR 2 MAIN BRAKE ASSY PER MM.

Part: SPAR — CRACKED (LT WING) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING UPPER SPAR CHORD CRACKED. REPAIRED CHORD PER ER.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND KEEL BEAM CORRODED AT BS 428B, STR 28R. REPAIRED BEAM PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: FITTING — CORRODED (LT MLG) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT MLG BEAM LUG FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CORRODED BETWEEN BS 727A TO BS 727B, BETWEEN RBL 3 TO LBL 3. REPAIRED SKIN PER SRM.

Part: FITTING — CORRODED (RT MLG) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT MLG BEAM LUG FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: RIB — CRACKED (HORIZ STAB) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT HORIZONTAL STABILIZER RIB CHORD CRACKED AT STA 149.12. REMOVED AND REPLACED CHORD PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 265, STR 10L. REPAIRED SKIN PER ER.

Part: FLAP — DELAMINATED (LT WING) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING I/B FORE FLAP SKIN DELAMINATED. REPAIRED SKIN PER SRM.

Part: LUG — CORRODED (LT MLG) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT MLG BEAM STABILIZER BAR LUG FACES CORRODED. REMOVED AND REPLACED LUG PER MM.

Part: LUG — CORRODED (RT MLG) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT MLG BEAM STABILIZER BAR LUG FACES CORRODED. REMOVED AND REPLACED LUG PER MM.

Part: LUG — CORRODED (RT MLG) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT MLG BEAM STABILIZER BAR LUG FACES CORRODED. REMOVED AND REPLACED LUG PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: LUG — CORRODED (LT MLG) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT MLG BEAM STABILIZER BAR LUG FACES CORRODED. REMOVED AND REPLACED LUG PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 947, RBL 23. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 947) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 947, RBL 23. REPAIRED FRAME PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 3 SLAT I/B END T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 482B, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 932, STR 23R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 942, STR 24R. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED BETWEEN BS 821 TO BS 823, BETWEEN STR 1R TO STR 2R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CRACKED AT BS 400, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO BAY FRAME CORRODED AT BS 482A, BL 0. REPAIRED FRAME PER SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT BS 685 FRAME LOWER FITTING CORRODED. REPAIRED FITTING PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,857 hrs · 59,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,506 hrs · 59,427 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 916, STR 24L. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,506 hrs · 59,427 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 943, STR 23L. REPAIRED SKIN PER AAR EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 60,506 hrs · 59,427 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO PIT FLOORBEAM VERTICAL SUPPORT WEB CORRODED BETWEEN BS 927 TO BS 947, STR 26R. REMOVED AND REPLACED WEB PER BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,506 hrs · 59,427 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,506 hrs · 59,427 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,505 hrs · 59,426 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 914, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,505 hrs · 59,426 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 913, STR 24L. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 59,632 hrs · 58,861 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,632 hrs · 58,861 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 911, STR 23R. REPAIRED SKIN PER SRM.

Part: STRIP — LOOSE (CABIN) · airframe 59,605 hrs · 58,843 cycles

EEPLS CLEAR STRIP LOOSE. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 59,368 hrs · 58,694 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,184 hrs · 58,568 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 291, WL 254, RT SIDE. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,184 hrs · 58,568 cycles

DURING SCHEDULED SPV CHECK, FOUND GALLEY DOOR SKIN CUTOUT CRACKED AT BS 291, WL 254. REPAIRED SKIN PER ER.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 59,184 hrs · 58,568 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 58,391 hrs · 57,854 cycles

FOUND AFT EMERGENCY FLASHLIGHT INOP. R&R BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,057 hrs · 57,567 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 434, STR 1. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,869 hrs · 57,424 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT FWD FUSE BS 400, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,869 hrs · 57,424 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 344, STR 22R TO 23R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,773 hrs · 57,359 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,544 hrs · 57,188 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 265 AND BS 271, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,304 hrs · 56,202 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 920, STR 24L AND STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,304 hrs · 56,202 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 831, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,131 hrs · 56,076 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 395, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,100 hrs · 56,051 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 395, STR 16R. REPAIRED SKIN PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,126 hrs · 55,230 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 5 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,126 hrs · 55,230 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 3 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: TORQUE TUBE — WORN (LT WING TE FLAP) · airframe 55,030 hrs · 55,142 cycles

DURING SCHEDULED SERVICE CHECK, NR 4 FLAP TRANSMISSION TO 90 DEGREE GEARBOX TORQUE TUBE WORN. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: TORQUE TUBE — WORN (TE FLAP) · airframe 55,030 hrs · 55,142 cycles

DURING SCHEDULED SERVICE CHECK, NR 4 FLAP TRANSMISSION TO 120 DEGREE GEARBOX TORQUE TUBE WORN. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 54,573 hrs · 54,727 cycles

DURING SCHEDULED BRDG CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FRAME — CRACKED (BS 482 S20L) · airframe 54,573 hrs · 54,727 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 20L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,553 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 20L. REPAIRED FRAME PER SWA EA.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,553 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND FWD CABIN EMERGENCY EXIT FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,553 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16R. REPAIRED FRAME PER SWA EA.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 54,533 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT BS 303.9, STR 10L TO STR 13L. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,533 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 54,553 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT BS 847, STR 16R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (BS 440 S8L) · airframe 54,553 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CORRODED (BS 277 S11L) · airframe 54,553 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 277, STR 11L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,553 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,553 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 1010, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 328 S4R) · airframe 54,553 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 328 S8R) · airframe 54,553 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 827 S8R) · airframe 54,553 hrs · 54,711 cycles

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

Part: FRAME — CRACKED (BS 827 S9R) · airframe 54,553 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 9R. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CRACKED (BS 277 S9L) · airframe 54,553 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 277, STR 9L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 294 S12L) · airframe 54,553 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727B S7L) · airframe 54,553 hrs · 54,711 cycles

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

Part: STRINGER CLIP — CRACKED (BS 294 S11L) · airframe 54,553 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 867 S10L) · airframe 54,553 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,553 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 54,553 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND LEFT KEEL BEAM CORRODED AT BS 488B, LBL 6.50. REPAIRED KEEL BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,553 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,553 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,553 hrs · 54,711 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,553 hrs · 54,711 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,188 hrs · 54,354 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT LOWER LT SIDE. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,188 hrs · 54,354 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,188 hrs · 54,354 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT LOWER END. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,095 hrs · 53,329 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 20 DEF. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 53,071 hrs · 53,304 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,462 hrs · 52,662 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,462 hrs · 52,662 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,462 hrs · 52,662 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, BL 0. REPAIRED SKIN PER BOEING SB.

Part: CONNECTOR — LOOSE (CABIN) · airframe 51,462 hrs · 52,662 cycles

DURING SCHEDULED SPV CHECK, FOUND MID CABIN EMERGENCY EXIT OVERHEAD LIGHTS INOP. SECURED BATTERY PACK CONNECTOR PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,462 hrs · 52,662 cycles

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

Part: BATTERY — LOOSE (EMERGENCY LIGHT) · airframe 52,215 hrs · 52,456 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. RECONNECTED CONNECTOR AT BATTERY PACK PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,210 hrs · 52,383 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (BS 812 S19L) · airframe 51,866 hrs · 52,022 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 812, STR 19L. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (BS 797 S19L) · airframe 51,866 hrs · 52,022 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 797, STR 19L. REPAIRED SKIN IAW SWA EA.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,764 hrs · 51,915 cycles

DURING SCHEDULED C2 CHECK, FOUND RIGHT AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,998 hrs · 51,091 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 486, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 50,960 hrs · 51,048 cycles

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

Part: SKIN — CRACKED (BS 766 S23L) · airframe 50,862 hrs · 50,930 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 766, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 312) · airframe 50,246 hrs · 50,244 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 6R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 797) · airframe 50,175 hrs · 50,169 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 797, STR 18L. REPAIRED SKIN PER SWA EA AND SRM.

Part: BEAR STRAP — CORRODED (BS 867) · airframe 50,049 hrs · 50,020 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT BS 867, STR 25R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 881-893) · airframe 50,049 hrs · 50,020 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 881 TO BS 893, STR 24R TO STR 25R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (AFT CARGO) · airframe 49,496 hrs · 49,458 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT AFT CARGO DOOR CUTOUT, FWD FRAME NR 5 STOP FITTING. REPAIRED FRAME PER SRM.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 49,496 hrs · 49,458 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REPAIRED WIRE NR W1150-559-20 PER WDM AND MM.

Part: FRAME — CRACKED (FWD CARGO) · airframe 49,496 hrs · 49,458 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME LOWER CORNER. REPAIRED FRAME PER BFG ER.

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 49,496 hrs · 49,458 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AFT FRAME NR 5 STOP FITTING. REPAIRED FRAME PER BFG ER.

Part: SKIN — CRACKED (BS 361.5) · airframe 49,496 hrs · 49,458 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 361.5, STR 17L. REPAIRED SKIN PER BFG ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,496 hrs · 49,458 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: BULKHEAD — CRACKED (BS 178) · airframe 49,496 hrs · 49,458 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BLKHD WEB CRACKED AT RBL 17.1 & LBL 17.1, WL 227. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (BS 807) · airframe 49,484 hrs · 49,447 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 807, STR 24L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 49,326 hrs · 49,294 cycles

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

Part: MOTOR — FAULTY (TE FLAPS) · airframe 49,056 hrs · 49,006 cycles

LOUD NOISE HEARD WHEN FLAPS ARE EXTENDED & RETRACTED. REMOVED AND REPLACED FLAP HYDRAULIC DRIVE MOTOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,019 hrs · 48,965 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 784, STR 19L. REPAIRED SKIN PER SWA EA & SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 48,940 hrs · 48,901 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,879 hrs · 48,845 cycles

DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 19L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 48,752 hrs · 48,718 cycles

R2 DOOR EVACUATION SLIDE OUT OF POSITITON. REPOSITIONED SLIDE ASSY PER MM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 47,594 hrs · 47,527 cycles

DURING SCHEDULED 1/2D CHECK, R1 DOOR EMERGENCY EXIT LIGHT COVER FELL OFF. REINSTALLED COVER PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,594 hrs · 47,527 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 907, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: WEB — CRACKED (NLG WW) · airframe 47,594 hrs · 47,527 cycles

DURING SCHEDULED 1/2D CHECK, FOUND NOSE W/W CEILING CRACKS ON LT & RT SIDE AT BRAKE PAD ATTACH POINT, BS 251.6. REPAIRED NOSE W/W CEILING PER SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,594 hrs · 47,527 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CRACK AT BS 178 BULKHEAD, WL 198, RBL 5.7. REPAIRED BULKHEAD PER SRM.

Part: FLOOR SUPPORT — CRACKED (MID CABIN) · airframe 47,594 hrs · 47,527 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CENTER CABIN LONGITUDINAL FLOOR SUPPORT CRACKED AT BS 664, BL 0. REPAIRED FLOOR SUPPORT PER SWA EA.

Part: SKIN — CRACKED (R1 DOOR) · airframe 47,594 hrs · 47,527 cycles

DURING SCHEDULED 1/2D CHECK, FOUND R1 DOOR SKIN CRACKED AT LOWER HINGE CUTOUT. REPAIRED R1 DOOR SKIN PER SRM.

Part: SKIN — WORN (FUSELAGE) · airframe 47,594 hrs · 47,527 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN, UPPER LOBE, WORN BETWEEN BS 870 & BS 887, RT SIDE & BETWEEN BS 878 & BS 880, LT SIDE. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 47,594 hrs · 47,527 cycles

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

Part: FLOOR SUPPORT — CRACKED (CENTER WING BOX) · airframe 47,594 hrs · 47,527 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 3 EA CRACKS AT NR 2 LONGITUDINAL FLOOR SUPPORT AT BS 656, BS 665, & BS 669. REPAIRED BEAM PER SWA EA.

Part: FLOOR SUPPORT — CRACKED (CENTER WING BOX) · airframe 47,594 hrs · 47,527 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 3 EA CRACKS AT NR 3 LONGITUDINAL FLOOR SUPPORT AT BS 665, BS 662.5, & BS 669. REPAIRED BEAM PER SWA EA.

Part: FITTING — CORRODED (GIRT BAR) · airframe 47,594 hrs · 47,527 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON L1 DOOR EVAC SLIDE, AFT GIRT BAR FITTING AT BS 344. REMOVED AND REPLACED GIRT BAR FITTING PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 47,594 hrs · 47,527 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON SHEAR TIE AT BS 787, BETWEEN STR 26R & 27R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 47,594 hrs · 47,527 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED STRINGER CLIP AT BS 663, STR 10L AND STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,594 hrs · 47,527 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON CREASE BEAM Z-ANGLE, RT SIDE, BETWEEN BS 927 AND BS 1006. REMOVED AND REPLACED RT CREASE BEAM Z-ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,594 hrs · 47,527 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FRAME AT LT FWD LOWER CORNER EMERGENCY EXIT AT BS 616. REPAIRED FRAME PER TYPICAL REPAIR MANUAL.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 47,594 hrs · 47,527 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT SHEAR WEB, BS 956, RBL 21. REMOVED AND REPLACED SHEAR WEB ANGLE PER SRM.

Part: RIB — CRACKED (LT WING) · airframe 47,594 hrs · 47,527 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BOTH LT & RT WING LOWER T-CHORDS CRACKED AT WBL 135.5, BETWEEN STR 2 & 3. REPAIRED T-CHORDS PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,529 hrs · 47,446 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT FWD LT CORNER OF AIR CONDITIONER CUTOUT, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,529 hrs · 47,446 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR UPPER HINGE CUTOUT, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 47,464 hrs · 47,392 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT WING NR 4 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,085 hrs · 47,056 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 930, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 46,776 hrs · 46,766 cycles

EEPLS STRIP COVER FROM ROW 17 DEF TO ROW 19 DEF, LOOSE. REMOVED AND REPLACED EEPLS STRIP COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,620 hrs · 46,610 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 971, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,488 hrs · 46,463 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 877, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,958 hrs · 44,900 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN BEHIND LT WING TO BODY FAIRING AT BS 767, CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 43,990 hrs · 43,994 cycles

R2 DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF POSITION. READJUSTED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,056 hrs · 43,117 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767 + 3, STR 18L. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 42,360 hrs · 42,446 cycles

DURING SCHEDULED RON, FOUND RT FWD CABIN OVERHEAD BIN EMERGENCY EXIT BULL NOSE LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — WORN (CABIN) · airframe 42,218 hrs · 42,317 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINSCENT STRIP WORN AND CHIPPED IN SEVERAL AREAS. REMOVED AND REPLACED WORN AREAS OF EEPLS STRIP.

Part: TRACK — DEBONDED (CABIN) · airframe 40,422 hrs · 40,646 cycles

DURING SCHEDULED C1 CHECK, FOUND SEVERAL PHOTO LUMINESCENT FLOOR STRIPS DEBONDED. REMOVED AND REPLACED STRIPS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,790 hrs · 40,018 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,782 hrs · 40,009 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 24L. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 39,782 hrs · 40,009 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 663, LBL 33 AND LBL 39. REPAIRED BEADED WEB PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,782 hrs · 40,009 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 328, STR 17R AT FWD SVC DOOR AFT LOWER CORNER CUTOUT. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 39,782 hrs · 40,009 cycles

DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW NR 13 DEF. SECURED LENS PER MM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 39,782 hrs · 40,009 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 1 L/E SLAT LOWER SKIN CRACKED AT AFT FASTENERS NEAR OTBD END. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 39,436 hrs · 39,677 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: TAB — WORN (RT ELEVATOR) · airframe 38,947 hrs · 39,228 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 38,398 hrs · 38,718 cycles

FWD ENTRY DOOR EVACUATION SLIDE PRESS IND OUT OF LIMIT. REMOVED AND REPLACED EVACUATION SLIDE ASSY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 37,922 hrs · 38,248 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 21. REMOVED AND REPLACED COVER PER MM.

Part: FLAP — DELAMINATED (LH WING) · airframe 37,124 hrs · 37,480 cycles

DURING WALK AROUND INSPECTION, FOUND # 1 T/E FLAP DELAMINATED 1 1/2 INCHES FROM AFT T/E. REPAIRED FLAP PER SRM..

Part: COVER — LOOSE (CABIN FLOOR) · airframe 36,187 hrs · 36,544 cycles

EEPLS COVER LOOSE AT ROW 21. SECURED EEPLS COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,790 hrs · 36,137 cycles

DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 847, STR 24L. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 35,429 hrs · 35,772 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING OUTBD T/E AFT FLAP DISBONDED AT INBD END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,716 hrs · 34,063 cycles

EEPLS TRACK INOP AT MID CABIN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 33,618 hrs · 33,971 cycles

EEPLS WIRES WERE DAMAGED AT ROW 9. REPAIRED EEPLS PER MM.

Part: COVER — MISSING (CABIN) · airframe 33,193 hrs · 33,515 cycles

EEPLS MISSING TRACK COVER AT ROW 9. INSTALLED TRACK COVER PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,098 hrs · 32,420 cycles

DURING SCHEDULED D CHECK, FOUND BS 986.5 UPPER SURFACE OF FLOORBEAM CORRODED, LBL 10 TO LBL 44. REPAIRED FLOORBEAM PER ER 00-245P2 AND SRM.

Part: MOUNT — CORRODED (VERTICAL STAB) · airframe 32,098 hrs · 32,420 cycles

DURING SCHEDULED D CHECK, FOUND CORROSION DAMAGE IN VERTICAL STABILIZER RT FWD MOUNT LUG BORE. REPAIRED LUG PER ER 00-0278.

Part: SKIN — CRACKED (BS 856)

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CORRODED AND CRACKED, BS 856, JUST BELOW STRINGER 18R. REPAIRED SKIN PER SRM AND ER NR 00-0289.

Part: FRAME — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD RT AND LT SIDE CHORDS CRACKED, WL 208. REPAIRED CHORD SECTIONS PER SRM.

Part: BRACKET — CORRODED (GIRT BAR)

DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT BAR FLOOR BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER SRM.

Part: SPLICE — CRACKED (BS 907)

DURING SCHEDULED D-CHECK, FOUND 2 STRINGER SPLICES CRACKED, BS 907, STRINGERS 4R AND 4L. REMOVED AND REPLACED STRINGER SPLICES PER SRM.

Part: SHEAR TIE — CRACKED (BS 360)

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED, BS 360, BETWEEN STRINGERS 13L-14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BY ULTRASONIC INSP BS 178 BULKHEAD CRACKED, WL 209-213, LBL 5-LBL 6. REPAIRED BULKHEAD PER SRM.

Part: STRINGER CLIP — CRACKED (BS 597 - 847)

DURING SCHEDULED D-CHECK, FOUND 12 STRINGER CLIPS CRACKED, STRINGER 11L, BS 706, BS 597, STRINGER 4L, BS 663, BS 616, BS 578, BS 847, STRINGER 5R, BS 727C, STRINGER 5L, BS 578, STRINGER 11R, BS 707, STRINGER 7L, BS 727C, BS 727A, AND STRINGER 8L, BS 727A. REMOVED AND REPLACED CLIPS PER SRM.

Part: GUIDE ARM — OUT OF ADJUST (PAX DOOR)

AIR TURNBACK, LOUD PRESSURIZATION LEAK AROUND FWD ENTRY DOOR. ADJUSTED FWD ENTRY DOOR UPPER GUIDE ARM PER MM.

Part: INDICATOR — LOOSE (EVAC SLIDE)

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE PRESS IND VIEWING WINDOW LOOSE. SECURED VIEWING WINDOW PER MM.

Part: LENS — MISSING (CABIN)

DURING SCHEDULED C3 CHECK, FOUND EEPLS LENS MISSING AT ROW 21. REPLACED LENS ASSY PER MM.

Part: TRIM ACTUATOR — INOPERATIVE (HORIZONTAL STAB)

DUAL CHANNEL TRIM FAIL LIGHT ILLUMINATED AND AUTOPILOT INOP. DIVERTED TO LAS. REMOVED AND REPLACED MACH TRIM ACTUATOR PER MM. C/W BITE CK AND OPS CK GOOD.

Part: LIGHT — INOP (CABIN)

3 EACH MOST FWD EEPLS LIGHTS INOP. REMOVED AND REPLACED LIGHT ASSY'S PER MM.

Part: LENS — BROKEN (EXIT LIGHT)

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

Part: SLIDE — DETACHED (SERVICE DOOR)

FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY INTO CONTAINER PER MM.

Part: WIRE — EXPOSED (CABIN)

DURING SCHEDULED C1 CHECK, FOUND EEPLS WIRING EXPOSED AND LENS COVER MISSING. REROUTED WIRES AND REPLACED LENS COVER PER MM.

Part: LENS — LOOSE (CABIN)

SEVERAL EEPLS LIGHT LENS CAME OUT OF TRACK DURING LANDING. RE-INSTALLED LENS PER MM.

Part: WIRE — EXPOSED (CABIN)

EEPLS LIGHT HAS EXPOSED WIRES AND MISSING LENS. REPAIRED WIRES AND REPLACED LENS PER MM.

Part: LIGHT — DAMAGED (ROW 8)

EMERGENCY ESCAPE FLOOR LIGHT PULLED OUT OF TRACK AT ROW 8. REPLACED WITH NEW TRACK LIGHT ASSY PER MM.

Part: CONTROLLER — ERRATIC (E & E COMP)

AIR TURNBACK, PRESSURIZATION CONTROLLER FAILED TO RETURN TO FIELD (EVEN WITH BOTH PACKS OFF). UPON RETURN TO LAS, MANUAL A/C WAS REQUIRED TO DUMP THE CABIN. REMOVED AND REPLACED PRESSURE CONTROLLER PER MM.

Part: BATTERY — DISCHARGED (CABIN)

FWD AND AFT EMERGENCY FLASHLIGHTS INOP. REMOVED AND REPLACED BATTERIES PER MM.

Part: SLIDE — LOW PRESSURE (PAX DOOR)

DURING SCHEDULED CHECK, FOUND AFT ENTRY EVACUATION SLIDE INDICATOR IS IN THE RED BAND. REPLACED SLIDE ASSY PER MM.

Part: LAMPS — FAILED (CABIN)

DURING SCHEDULED SC CHECK, FOUND 3 FLOOR EMERGENCY EXIT LIGHTS INOP. RELAMPED PER BOEING M/M.

Part: BULB — FAILED (EMER EXIT)

DURING PREFLIGHT CHECK, FOUND RED EMERGENCY EXIT FLOOR TRACK LIGHTS AT OVERWING EXIT INOP. RELAMPED PER BOEING M/M.

Part: LIGHT — INOPERATIVE (ROW 6, 20 &16)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 6, 10 AND 16 ARE INOPERATIVE. RELAMPED FLOOR TRACK LIGHTS PER BOEING MM.

Part: RETRACT MECH — FAILED (NR 4 LE SLAT)

AIR TURNBACK TO PHX, DUE TO NR 4 SLAT FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT MADE AN UNEVENTFUL LANDING (LGPAGE 99546). REMOVED AND REPLACED FLAP/SLAT MODULE AND FULL EXT SENSOR AS REQ PER BOEING MM. OPS CHECK GOOD.

Part: LIGHT — DAMAGED (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT NEAR SEAT 12C IS RIPPED OUT. ALL OTHER LIGHTS WORK NORMALLY. INSTALLED TRACK LIGHTING ASSY PER BOEING MM, OPS CHECK GOOD.

Part: WIRE — BROKEN (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT LIGHTS INOP IN LEFT HAND EMERGENCY EXIT LOCATION. RECONNECTED BROKEN WIRE PER BOEING MM. OPS CK GOOD.

Part: SOCKET — BROKEN (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT INOP. REPLACED LIGHT SOCKET PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING WALKAROUND INSPECTION, FOUND WHITE FLOOR TRACK LIGHTING INOP IN AFT CABIN AREA. REMOVED AND REPLACED LIGHT ASSEMBLY AND LENS PER BOEING M/M.

Part: LIGHTS — INOPERATIVE (CABIN)

DURING WALKAROUND, FOUND A SECTION OF CABIN EMERGENCY TRACK LIGHTING INOP. RECONNECTED 2 LIGHT ASSEMBLIES AND OP CHECKED PER BOEING M/M.

Part: LIGHTS — INOPERATIVE (CABIN)

DURING SCHEDULED C3 CHECK, FOUND CABIN FLOOR TRACK LIGHTING HAD CRACKED COVERS, INOP LAMPS THROUGHOUT CABIN. REPAIRED AND REPLACED AS REQUIRED PER BOEING M/M.

Part: SKIN — GOUGED (BS 986.5)

DURING SCHEDULED BC2 CHECK, FOUND FUSELAGE SKIN GOUGED 3 PLACES AT 986.5, 16 INCHES BELOW AFT ENTRY DOOR. REPLACED PER BOEING SRM AND TYPICAL REPAIR T1-A53-042.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SC-CHECK, FOUND CABIN FLOOR TRACK LIGHTING INOPERATIVE AT ROWS 7 AND 8. SECURED WIRING PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED C1 CHECK, FOUND 2 FLOOR TRACK LIGHTS INOPERATIVE AT EMERGENCY EXIT ROW. RELAMPED PER BOEING M/M.

Part: EEL — INOP (CABIN)

FOUND FLOOR TRACK LIGHTING TORN UP AT ROW 6 AND SEVERAL LIGHTS INOP. REPAIRED TRACK LIGHTING AND REPLACED LIGHTS PER BOEING M/M.

Part: EEL — INOP (CABIN)

FOUND 2 EMERGENCY FLOOR TRACK LIGHTS INOP. RELAMPED AND RECONNECTED LIGHTS PER BOEING M/M.

Part: FLOORBEAM — CORRODED (BS 947)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947, LBL 5.0. REPAIRED PER SWA RA 1-553-1282.

Part: FLOORBEAM — CORRODED (BS 947)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947, RBL 15. REPAIRED PER SWA RA 1-553-1280.

Part: FLOORBEAM — CORRODED (BS 947)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947, RBL 48 TO RBL 53. REPAIRED PER SWA RA 1-553-1283.

Part: FLOORBEAM — CORRODED (BS 947)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947, LBL 4 TO RBL 2. REPAIRED PER SWA RA 1-553-1277.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 312, RBL 8 TO LBL 10. REPAIRED PER SWA RA 1-553-1275.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 312, RBL 8. REPAIRED PER SWA RA 1-553-1274.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5, LBL 25.75 TO 43. REPAIRED PER SWA RA 1-553-1284.

Part: FLOORBEAM — CORRODED (BS 947)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947, RBL 5.0. REPAIRED PER SWA RA 1-553-1279.

Part: WEB — CRACKED (BS 726)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACK IN WEB AT BS 726, STRINGER 18A RIGHT SIDE. REPAIRED PER SWA RA 1-553-1286.

Part: FLOORBEAM — CORRODED (BS 947)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947, LBL 21.0. REPAIRED PER SWA RA 1-553-1278.