N311SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,058 hrs · 70,824 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 503 TO BS 506, STR 22R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,058 hrs · 70,824 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 503 TO BS 506, STR 21R. REPAIRED SKIN PER EA.

Part: SIGN — MISSING (CABIN) · airframe 75,829 hrs · 7,065 cycles

DURING SCHEDULED OTS CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,866 hrs · 69,995 cycles

DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CORRODED AT BS 294, BETWEEN LBL 2 TO LBL 6. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,670 hrs · 69,845 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 390, ABOVE STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,670 hrs · 69,845 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 8L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,670 hrs · 69,845 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 570, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,670 hrs · 69,845 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 338, ABOVE STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,670 hrs · 69,845 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 350, ABOVE STR 24R. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (AFT CARGO DOOR) · airframe 74,670 hrs · 69,845 cycles

DURING SCHEDULED HC2 CHECK, FOUND AFT CARGO DOOR MAIN FRAME CRACKED AT LOWER AFT STOP FITTING. REMOVED AND REPLACED DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,670 hrs · 69,845 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 342, STR 2L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,670 hrs · 69,845 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 982, STR 5R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,670 hrs · 69,845 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 961, STR 5R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,670 hrs · 69,845 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 316, ABOVE STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,670 hrs · 69,845 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 578, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,670 hrs · 69,845 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 348, STR 2L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,670 hrs · 69,845 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 775, STR 14R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,979 hrs · 68,633 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 525, BL 0. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 72,799 hrs · 68,505 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,793 hrs · 68,502 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,116 hrs · 67,975 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503, BETWEEN STR 20R AND STR 21R. REPAIRED SKIN PER SWA EA.

Part: SPOILER — DELAMINATED (LT WING) · airframe 71,156 hrs · 67,261 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 2 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 71,156 hrs · 67,261 cycles

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

Part: PUSHROD — WORN (LT ELEVATOR) · airframe 71,156 hrs · 67,261 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 71,156 hrs · 67,261 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 6R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,156 hrs · 67,261 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 947 STR 18R AND STR 18L. REPAIRED FRAME PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 71,156 hrs · 67,261 cycles

DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 71,156 hrs · 67,261 cycles

DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,156 hrs · 67,261 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259, STR 22L. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 71,156 hrs · 67,261 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED INBOARD END. REPAIRED FLAP PER SRM.

Part: FITTING — CORRODED (EVAC SLIDE) · airframe 71,156 hrs · 67,261 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: FITTING — CORRODED (EVAC SLIDE) · airframe 71,156 hrs · 67,261 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 71,156 hrs · 67,261 cycles

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

Part: SKIN — DELAMINATED (TE FLAP) · airframe 71,156 hrs · 67,261 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND RIGHT WING INBOARD T/E FLAP DELAMINATED. REMOVED AND REPLACED RIGHT INBOARD T/E FLAP PER MM.

Part: GIRT BAR — CORRODED (L1 DOOR SLIDE) · airframe 71,156 hrs · 67,261 cycles

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

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 71,156 hrs · 67,261 cycles

DURING SCHEDULED BRDG CHECK, FOUND NLG W/W RIGHT CEILING PANEL CUTOUT WEB CRACKED AT INBOARD CORNER. REPAIRED WEB PER ACO.

Part: TAB — DELAMINATED (RT AILERON) · airframe 71,156 hrs · 67,261 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT WING AILERON TAB DELAMINATED. REPAIRED TAB PER SRM.

Part: TORQUE TUBE — WORN (TE FLAPS) · airframe 71,156 hrs · 67,261 cycles

DURING SCHEDULED BRDG CHECK, FOUND LEFT WING OUTBOARD TORQUE TUBE WORN. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: HOOK — LOOSE (R2 DOOR) · airframe 70,645 hrs · 66,726 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM.

Part: HOOK — LOOSE (L2 DOOR) · airframe 70,645 hrs · 66,726 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 70,645 hrs · 66,726 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,046 hrs · 65,622 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 6 ABC. RELAMPED PER MM.

Part: FRAME — CORRODED (BS 1016) · airframe 68,655 hrs · 65,329 cycles

DURING SCHEDULED OTS CHECK, FOUND BULKHEAD FRAME CORRODED AT BS 1016, BL 0. REPAIRED BULKHEAD FRAME PER SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 68,650 hrs · 65,325 cycles

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

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 68,650 hrs · 65,325 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT L2 DOOR CUTOUT LOWER FWD CORNER. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 68,650 hrs · 65,325 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (BS 578 S10R) · airframe 68,650 hrs · 65,325 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 578, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 908 S5R) · airframe 68,650 hrs · 65,325 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 908, STR 5R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 910 S4R) · airframe 68,650 hrs · 65,325 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 910, STR 4R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 500B S26R) · airframe 68,650 hrs · 65,325 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 26R. REPAIRED SKIN PER SRM.

Part: CIRCUIT CARD — FAULTY (E/E BAY) · airframe 68,227 hrs · 65,007 cycles

RIGHT MLG UNSAFE LIGHT INDICATION, CYCLED GEARS AND OPERATED NORMAL. REMOVED AND REPLACED RIGHT MLG DOWLOCK SENSOR LOGIC CARD PER MM.

Part: FITTING — LOOSE (L1 DOOR GIRT BAR) · airframe 67,702 hrs · 64,506 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED GIRT BAR FITTING PER MM.

Part: SKIN — CRACKED (BS 295 S13R) · airframe 67,702 hrs · 64,586 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT BS 295, STR 13R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 316 S18R) · airframe 67,047 hrs · 64,046 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 316, STR 18R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,026 hrs · 64,030 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 316, STR 18R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 67,018 hrs · 64,021 cycles

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

Part: SKIN — CRACKED (BS 972 S5R) · airframe 66,989 hrs · 63,998 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 972, STR 5R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,988 hrs · 63,997 cycles

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY) · airframe 66,988 hrs · 63,997 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,988 hrs · 63,997 cycles

DURING SCHEDULED SPV CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 13 DEF. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (BS 503) · airframe 66,705 hrs · 63,827 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,867 hrs · 63,090 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 374, STR 26R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,867 hrs · 63,090 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 923 TO BS 932, STR 22R TO STR 25R. REPAIRED SKIN PER SWA EA & SRM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 65,867 hrs · 63,090 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN BETWEEN ROW 14 & ROW 23. R&R STRIP PER MM.

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 64,873 hrs · 62,292 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 5 L/E SLAT UPPER WEDGE SKIN DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: CHARGER — FAILED (EMERGENCY LIGHT) · airframe 64,838 hrs · 62,261 cycles

DURING SCHEDULED A2 CHECK, R2 DOOR EMERGENCY EXIT SIGN FAILED TEST. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: PUSHROD — BROKEN (LT WING TE FLAP) · airframe 63,769 hrs · 61,407 cycles

DURING SCHEDULED RON CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DRIVE PUSHROD BROKEN. REMOVED AND REPLACED PUSHROD PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 63,730 hrs · 61,377 cycles

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

Part: GUIDE VANE — CRACKED (NR 2 ENGINE) · airframe 63,369 hrs · 61,078 cycles

DURING SCHEDULED BOROSCOPE INSP, FOUND NR 2 ENGINE LPT NOZZLE GUIDE VANES CRACKED. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND KEELBEAM CORRODED BETWEEN BS 500D + 2 TO BS 727 + 8. REMOVED AND REPLACED KEELBEAM PER SRM.

Part: SKIN — CORRODED (AFT CARGO) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 927, LBL 15. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (CABIN FLOOR) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 663, BL 0, WL 206. REPAIRED WEB PER BFG ER.

Part: FLOOR SUPPORT — CRACKED (CABIN FLOOR) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CRACKED AT BS 727A + 18, LBL 25, WL 208. REPAIRED FLOOR PER BFG ER.

Part: RIB — CRACKED (RT WING) · airframe 63,143 hrs · 60,893 cycles

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

Part: SKIN — CORRODED (FWD CARGO) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 524, RBL 7, WL 148. REPAIRED SKIN PER BFG ER.

Part: RIB — CRACKED (LT WING) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND LT WING RIB UPPER FLANGE CRACKED AT WS 453, STR 12. REMOVED AND REPLACED RIB PER SRM.

Part: FLOOR SUPPORT — CRACKED (CABIN FLOOR) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND CABIN LONGITUDINAL FLOOR SUPPORT UPPER TEE CRACKED AT BS 663, BL 0, WL 208. REPAIRED FLOOR SUPPORT PER BFG ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 500A, STR 15L TO STR 16L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND BS 727 INBOARD FUSELAGE CHORD CORRODED AT RBL 10 TO LBL 10, WL 148. REMOVED AND REPLACED CHORD SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 17R TO STR 18R. REPAIRED SKIN PER BFG ER & SWA EA.

Part: SPLICE — CORRODED (BS 360) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER SPLICE CORRODED AT BS 360 + 5, BETWEEN STR 26L & STR 27L, WL 149. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED AT BS 747 TO BS 767, RBL 65, WL 208. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: FRAME — CORRODED (AFT CARGO) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 927, RBL 7. REMOVED & REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 3L TO STR 3R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, STR 14R TO STR 15R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 520, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE SHEAR TIE AT BS 827, RBL 4 & LBL 17. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (AFT CABIN) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 13L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, RT SIDE, WL 208. REPAIRED STUB FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 847, LBL 17, WL 149. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 500D, STR 16R TO STR 17R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727B, STR 23R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 709, RBL 25. REPAIRED BEAMS PER BFG ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 312 TO BS 322, STR 27R. REPLACED STRINGER SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME ANGLE CRACKED AT BS 947, LBL 23, WL 180. REMOVED AND REPLACED ANGLE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND 4 EA FUSELAGE SHEAR TIES CRACKED AT BS 400, BS 500A, BS 500B & BS 520, STR 15R TO STR 16R. REPAIRED SHEAR TIES PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 500, STR 14R TO STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 500A, STR 16R. REPAIRED STRINGER PER SRM.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FLOOR WEB CRACKS BETWEEN BS 188 TO BS 196, LT & RT SIDE, WL 208. REPAIRED FLOOR WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, LBL 4 TO RBL 4. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE SHEAR TIES CORRODED AT BS 727C & BS 747, LBL 18. REPAIRED SHEAR TIES PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727E, BL 0 & LBL 7. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 490, STR 26R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, LT SIDE, WL 208. REPAIRED STUB FRAME PER SRM.

Part: FRAME — CRACKED (BS 727D) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

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

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB ATTACH FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

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

Part: FRAME — CRACKED (BS 787) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 767) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FAILSAFE FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.

Part: STRINGER CLIP — CRACKED (BS 727C) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727C, BETWEEN STR 6L & STR 8L. REMOVED AND REPLACED CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706) · airframe 63,143 hrs · 60,893 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 16R TO STR 17R. REPAIRED FRAME PER SRM.

Part: WEDGE — DELAMINATED (L/E SLAT) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND NR 2 L/E SLAT INBOARD T/E WEDGE DELAMINATED. REPAIRED SLAT PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FRAME CRACKS AT BS 400, STR 8L TO STR 9L & STR 15R TO STR 16R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND CABIN FLOORBEAM UPPER CHORD CRACKED AT BS 639, LBL 59, WL 206. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FRAME CRACKS AT BS 480, STR 8L TO STR 9L & STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA CRACKS AT BS 1016 PRESS BULKHEAD WEB, STR 15L & STR 23R. REPAIRED BS 1016 PRESS BULKHEAD PER BFG ER.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 63,143 hrs · 60,893 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE FLOORBEAM AT BS 344, LBL 9, WL 208. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

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

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,143 hrs · 60,893 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT MLG W/W VERTICAL STIFFENERS CRACKED AT BS 663 BULKHEAD, LBL 6 & RBL 6, WL 166. REPAIRED STIFFENERS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,993 hrs · 60,775 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,992 hrs · 60,774 cycles

DURING SCHEDULED C2 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS BETWEEN BS 927 TO BS 935, STR 21R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,992 hrs · 60,774 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 450, STR 16R. REPAIRED SKIN PER SRM & SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,992 hrs · 60,774 cycles

DURING SCHEDULED C2 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS, BETWEEN BS 276 TO BS 282, STR 13L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 62,962 hrs · 60,750 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,004 hrs · 60,027 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 23R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,004 hrs · 60,027 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,606 hrs · 59,702 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 793, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 61,551 hrs · 59,653 cycles

DURING SCHEDULED RON, FOUND RT NLG WHEEL WELL WEB AT BS 259, WL 174, CRACKED. REPAIRED WEB PER EA.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 61,193 hrs · 59,359 cycles

DURING SCHEDULED C4 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT SIDEWALL LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,193 hrs · 59,359 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 8L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,251 hrs · 58,608 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 380, STRINGER 5L, AND BS 482, STRINGER 16L, CRACKED. REPAIRED FUSELAGE SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,023 hrs · 58,423 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 440, STRINGER 16R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,656 hrs · 58,135 cycles

4 LONG CRACK AT FUSELAGE SKIN AT BS 312, BETWEEN STR 17R AND STR 18R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1/R2 DOOR) · airframe 59,321 hrs · 57,857 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,150 hrs · 57,722 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACK AT BS 440 + 6, STRINGER 16R. REPAIRED SKIN CRACK PER SRM.

Part: CARRIAGE — CRACKED (RT WING TE FLAP) · airframe 59,033 hrs · 57,633 cycles

DURING SCHEDULED PM CHECK, FOUND RT WING OUTBD T/E MID FLAP INBD CARRIAGE SPINDLE CRACKED. REMOVED AND REPLACED CARRIAGE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,444 hrs · 57,156 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 416, BETWEEN STR 28L AND STR 28R. REPAIRED SKIN PER SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,389 hrs · 57,115 cycles

DURING SCHEDULED C1 CHECK, FOUND PRESS BULKHEAD CRACKED AT BS 1016, STR 6L AT THE Y-CHORD ATTACH AREA. REPAIRED BULKHEAD PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,389 hrs · 57,115 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 4, ABOVE STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,389 hrs · 57,115 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) ABOVE STR 15L, BS 374 AND BS 378. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,389 hrs · 57,115 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT BS 380, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,389 hrs · 57,115 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) BS 500 AT STR 16R, BS 500B AT STR 26R AND BS 967 AT STR 21L. REPAIRED SKIN PER SRM.

Part: STRIP — LOOSE (CABIN) · airframe 57,914 hrs · 56,762 cycles

EEPLS PHOTOLUMINICENT STRIP LOOSE AT MID CABIN. REMOVED AND REPLACED STRIP PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 57,855 hrs · 56,679 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN OPENING THE DOOR. REINSTALLED SLIDE PER MM.

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 57,653 hrs · 56,505 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,480 hrs · 56,362 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 328, STR 21R. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 56,702 hrs · 55,704 cycles

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

Part: STRIP — LOOSE (CABIN) · airframe 55,864 hrs · 55,035 cycles

PORTION OF THE EEPLS SELF ILLUMINATION STRIP NOT SECURED. SECURED THE EEPLS STRIP PER MM.

Part: BYPASS VALVE — FAULTY (LT MLG W/W) · airframe 55,765 hrs · 54,959 cycles

DIVERSION, T/E FLAPS WOULD NOT EXTEND. REMOVED AND REPLACED FLAP BYPASS VALVE PER MM.

Part: SLIDE — WORN (AFT SVC DOOR) · airframe 55,563 hrs · 54,811 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION AND GIRT ASSY WORN. REMOVED AND REPLACED SLIDE PER MM.

Part: ACTUATOR — LEAKING (RT WING) · airframe 55,329 hrs · 54,616 cycles

ON TAXI OUT, LOSS OF HYDRAULIC 'A' SYSTEM, ZERO QUANITY AND ZERO PRESS. REMOVED AND REPLACED NR 6 SPOILER ACTUATOR AND CASE DRAIN FILTER PER MM.

Part: SKIN — CRACKED (FWD CARGO DOOR) · airframe 54,891 hrs · 54,262 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR FWD LOWER FRAME CRACKED ABOVE LOWER STOP FITTING. REMOVED AND REPLACED LOWER FRAME SECTION PER CCO.

Part: TEE CHORD — CRACKED (CARGO DOOR) · airframe 54,891 hrs · 54,262 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR LOWER T-CHORD CRACKED AT AFT END. REMOVED AND REPLACED T-CHORD PER CCO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,586 hrs · 54,000 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT RT FWD EDGE OF GROUND AIR CONDITIONING CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,586 hrs · 54,000 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,586 hrs · 54,000 cycles

DURING SCHEDULED C1 CHECK, FOUND SKIN CRACKED AT BOTH UPPER AND LOWER HINGE ATTACH POINTS ON FWD ENTRY DOOR. REPAIRED SKIN PER SRM.

Part: BATTERY — FAULTY (CABIN) · airframe 54,586 hrs · 54,000 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH AFT CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS INTERMITENT. REMOVED AND REPLACED BATTERIES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,320 hrs · 53,792 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,164 hrs · 53,659 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, ABOVE STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,164 hrs · 53,659 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D PLUS 5, ABOVE STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,166 hrs · 53,660 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 18R, BS'S 727E AND 747. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 53,689 hrs · 53,264 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 53,689 hrs · 53,264 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: TAB — WORN (LT ELEVATOR) · airframe 53,648 hrs · 53,234 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 53,462 hrs · 53,083 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND WEB CRACKED AT BS 182, WL 190 AT RBL 5.7. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,462 hrs · 53,083 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LT AND RT OUTBOARD CHORDS CRACKED AT BS 178, WL 207. REMOVED AND REPLACED CHORDS PER SWA ACO.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 53,462 hrs · 53,083 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL CHORD CRACKED AT BS 178, WL 184 AT LBL 5.7. REPAIRED CHORD PER SWA T1.

Part: WEB — CRACKED (FUSELAGE) · airframe 53,462 hrs · 53,083 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL WEB CRACKED AT BS 178, WL 220 AT RBL 17.1. REMOVED AND REPLACED VERTICAL WEB PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,462 hrs · 53,083 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE'S CRACKED (2 EA) AT BS 360, ABOVE AND BELOW STR 14L. REMOVED AND REPLACED SHEAR TIE'S PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 53,462 hrs · 53,083 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 53,462 hrs · 53,083 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICES CRACKED (2 EA) AT BS 908, STR 4R AND 10R. REMOVED AND REPLACED STR SPLICES PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,462 hrs · 53,083 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 440, BETWEEN STR 4R AND 12R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,462 hrs · 53,083 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 52,895 hrs · 52,627 cycles

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

Part: SLAT — CRACKED (LT WING) · airframe 52,771 hrs · 52,529 cycles

DURING SCHEDULED C3 CHECK, FOUND NR 4 L/E SLAT CRACKED (2 EA) ON LOWER T/E RIVET ROW ADJACENT TO OTBD AUX TRACK. REPAIRED SLAT PER SRM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 52,096 hrs · 51,978 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,940 hrs · 50,988 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 428, STRINGER 16R. REPAIRED SKIN PER SRM.

Part: RETAINER — LOOSE (ENTRY DOOR) · airframe 49,985 hrs · 50,176 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMEGENCY EVAC SLIDE GIRT RETAINER RIVETS LOOSE. SECURED GIRT RETAINER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 49,985 hrs · 50,176 cycles

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHT LENS LOOSE AT LT OVERWING EXIT. SECURED LENS PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 49,985 hrs · 50,176 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC AND FWD ENTRY DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY''S PER MM.

Part: SLIDE — DISCHARGED (R2 DOOR) · airframe 49,399 hrs · 49,688 cycles

DURING SCHEDULED A2 CHECK, FOUND AFT ENTRY DOOR EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,997 hrs · 49,344 cycles

DURING SCHEDULED C3 CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACK AT BS 767, STR 20L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 48,997 hrs · 49,344 cycles

DURING SCHEDULED C3 CHECK, FOUND BOTH AFT DOOR EMERGENCY EVAC SLIDE GIRT BAR ASSYS OUT OF ADJUSTMENT. READJUSTED SLIDE ASSYS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,997 hrs · 49,344 cycles

DURING SCHEDULED C3 CHECK, FOUND 2.5 EXTERNAL FUSELAGE SKIN CRACK AT BS 259 -277, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,997 hrs · 49,344 cycles

DURING SCHEDULED C3 CHECK, FOUND 3.0 EXTERNAL FUSELAGE SKIN CRACK AT BS 947, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 47,238 hrs · 47,801 cycles

DURING SCHEDULED C1 CHECK, FOUND NR 5 AND NR 6 L/E SLAT LOWER SKINS CRACKED AROUND IDLER TRACK CUTOUTS. REPAIRED SLATS PER SWA RA 1-A57-0691.

Part: LENS — LOOSE (FAIRING) · airframe 47,030 hrs · 47,614 cycles

DURING SCHEDULED 1/2D CHECK, FOUND OUTER EGRESS LIGHT LENS AFT OF LT WING TO BODY FAIRING LOOSE. RESECURED LENS PER MM.

Part: BRACKET — CORRODED (CABIN FLOOR) · airframe 47,030 hrs · 47,614 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKETS CORRODED. REMOVED AND REPLACED BOTH BRACKETS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,030 hrs · 47,614 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 500D, STRINGER 10L. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (GALLEY) · airframe 47,030 hrs · 47,614 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOOR BEAM UPPER SURFACE CORRODED, BS 294, LBL 11. REPAIRED BEAM PER RA NR T1-253-006.

Part: FLOORBEAM — CRACKED (GALLEY) · airframe 47,030 hrs · 47,614 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 947 FLOORBEAM CRACKED ON UPPER SURFACE, LBL 54. REPAIRED BEAM PER SWA RA NR 1-353-1834.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,030 hrs · 47,614 cycles

DURING SCHEDULED 1/2 D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 10. WL 234. REPAIRED BULKHEAD PER SRM.

Part: MOUNT — LOOSE (ESCAPE SLIDE)

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE MOUNTING HARDWARE LOOSE. SECURED MOUNTING HARDWARE PER MM.

Part: SKIN — CRACKED (BS 947)

DURING SCHEDULED C4 CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED, BS 947, STRINGER 24L. REPAIRED SKIN PER SRM.

Part: MEC — MALFUNCTIONED (NR 1 ENGINE)

ENGINE SHUTDOWN, AT 26,000 FEET, NR 1 ENG SPOOLED DOWN. C/W ENG SHUTDOWN AND NORMAL ENG RESTART. REMOVED AND REPLACED NR 1 ENG MEC, FUEL PUMP, AND REINSTALLED LT AFT FUEL BOOST PUMP CHECK VALVE CORRECTLY PER MM.

Part: SKIN — CRACKED (BS 747)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 747, WL 208. REPAIRED SKIN PER SRM.

Part: KEEL BEAM — CRACKED (FUSELAGE)

DURING SCHEDULED C3 CHECK, FOUND KEEL BEAM CRACKED AT 2 EACH PLACES, 1.5 FEET FROM FWD END AND 3 FEET FROM FWD END AT LT SIDE. REPAIRED BEAM PER TI-153-009.

Part: FRAME — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR UPPER FUSELAGE CUT OUT CENTER FWD FRAME CRACKED. REPAIRED FRAME PER SWA RA NR 1-353-2170.

Part: BATTERY — DISCHARGED (SERVICE DOORWAY)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY ASSY PER MM.

Part: O-RING — LEAKING (LTWING)

AIR TURNBACK, PASSENGER REPORTED FLUID LEAKING (APPARENTLY FUEL) FROM LT WING UPPER SURFACE AROUND FUEL CAP. INSPECTED LT UPPER WING. NO LEAK FOUND. REMOVED AND REPLACED LT WING UPPER FUELING CAP O-RING AS A PRECAUTION.

Part: BATTERY — DISCHARGED (AFT CABIN)

DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS BATTERY ASSY INOP. RECHARGED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD END OF EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: PIN — BROKEN (RT MLG)

AIR TURNBACK DUE TO AN UNSAFE LIGHT, REMAINED ON AT RIGHT MAIN LANDING GEAR AFTER TAKEOFF. GEAR WAS LOWERED AND 3 GREEN LIGHTS WERE NORMAL. FOUND BROKEN PIN LOCK AT DISCONNECT D4536, PIN NR 3, WIRE 424-A-R. REMOVED AND REPLACED PIN PER MM GEAR RETRACTION GOOD.

Part: LINE — LEAKING (MLG WW)

ON PUSH BACK GROUND CREW NOTICED SMOKE COMING FROM WHEEL WELL. TIGHTENED B NUT ABOVE SHUTTLE VALVE, ABOVE FLAP ACTUATOR. THEN SECOND PUSHBACK WITH B PUMPS ON AND BRAKE SET, THE SMOKE REAPPEARED. REPLACED LINE BETWEEN BRAKE MEETING VALVE AND BRAKE SHUTTLE VALVE PER MM.

Part: SKIN — CRACKED (BS 515)

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515, S12R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 950)

DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 950 AT S22R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 747)

DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, BELOW S15R. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (ROW 1-5)

DURING WALKAROUND CHECK, FOUND EGRESS LIGHTS ROWS 1 TO 5 INOPERATIVE. REMOVED AND REPLACED FWD EMERGENCY LIGHTS BATTERY ASSY PER BOEING MM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED ABOVE LT WING ILLUMINATION LIGHT. REPAIRED PER BOEING SRM.

Part: HINGE — CRACKED (SERVICE DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR HINGE CRACKED. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 967)

DURING SERVICE CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 967 APROX 27 BELOW AFT ENTRY DOOR CUT OUT. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (R2 DOORWAY)

DURING SCHEDULED C1 CHECK, FOUND CRACKED R2 LOWER HINGE CUTOUT ON FUSELAGE SIDE (.850 LONG). REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (L2 DOORWAY)

DURING SCHEDULED C1 CHECK, FOUND CRACKED L2 LOWER HINGE CUTOUT ON FUSELAGE SIDE (.875 LONG). REPAIRED PER BOEING SRM.

Part: SLIDE — LOW PRESSURE (FWD ENTRY)

DURING WALKAROUND CHECK, FOUND FWD ENTRY DOOR SLIDE PRESS LOW. REPLACED PER BOEING M/M.

Part: FUEL SYST — VENTING (LT WING)

DURING TAKEOFF, TOWER INFORMED CREW OF FLUID VENTING FROM LEFT WING, APPROX 5 FT FROM WINGTIP. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. PERFORMED INSPECTION OF WING AND FUEL DUMP SYSTEM PER BOEING M/M WITH NO DEFECTS NOTED.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP AND RT OVERWING EXIT SIGN INOP. REPLACED M1135 POWER SUPPLY UNIT PER BOEING M/M.

Part: GENERATOR — INOPERATIVE (NR 1)

EN ROUTE, NR 1 TRANSFER BUSS C/B TRIPPED TWICE, LOST PRESSURIZATION. DIVERTED TO ABQ AND MADE AN UNEVENTFUL LANDING. INSPECTED NR 1 MAIN AND NR 1 TRANSFER BUSS USING APU GENERATOR, ALL OK. DEFERRED NR 1 GENERATOR PER MEL AND CONTINUED.

Part: VALVE — INOPERATIVE (NR 1 ENGINE)

DURING TAKEOFF, CONTROL TOWER NOTED A STREAM OF VAPOR COMING FROM LEFT WING TIP, SUSPECTED FUEL VENTING. TRANSFERRED FUEL FROM NUMBER 1 TANK TO CENTER. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. PERFORMED OVERWEIGHT LANDING INSPECTION, DEFERRED NUMBER 1 REFUELING VALVE PER MEL.

Part: SKIN — CRACKED (BS 800)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800, AT S20L. REPAIRED PER BOEING SRM.

Part: HYD LINE — RUPTURED (LT MLG WW)

AFTER TAKEOFF AT 3,000 FT, A-SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED WITH ASSOCIATED FLUID LEVEL DROP. RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND LEFT MAIN GEAR RETRACT LINE RUPTURED. REPLACED LINE, ASSOCIATED FILTERS AND OP CHECKED PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING WALKAROUND CHECK, FOUND AFT CABIN UPPER FLASHLIGHT INOPERATIVE. REPLACED BATTERY PER BOEING M/M.

Part: FLOOR BEAM — CORRODED (BS 986.5)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 986.5, RBL 27 AND 31.5. REPLACED PER SWA RA 1-353-542.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUTOUT AT LOWER I/B CORNER. REPAIRED PER BOEING BOEING STRUCTURAL REPAIR MANUAL.

Part: STRINGER — CRACKED (BS 360)

DURING SCHEDULED D-CHECK, FOUND STRINGER 15L CHANNEL CRACKED AT BS 360. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DAMAGED (FWD SERV DOOR)

DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR OUTER SKIN DAMAGED 6 INCHES ABOVE LOWER HINGE CUTOUT OUTER EDGE AND CRACKED AT RIVET HEAD 1 INCH ABOVE LOWER CORNER. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — GOUGED (FWD SERV DOOR)

DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR OUTER SKIN GOUGED AT LOWER HINGE CUTOUT LOWER EDGE. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FRAME — CRACKED (BS 867/907)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT LOWER HAT SECTION SUPPORT AT BS 867, S9L AND AT BS 907, S9L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: CLIPS — CRACKED (BS 663/1138)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 663, S10L AND S10R, AND AT BS 1138, S13L. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: TE SKIN — CRACKED (NR 3/4 LE SLAT)

DURING SCHEDULED D-CHECK, FOUND NR 3 SLAT CRACKED AT T/E SKIN O/B OF ACTUATOR AND NR 4 SLAT CRACKED AT LOWER T/E SKIN, I/B OF ACTUATOR. REPAIRED PER BOEING DRAWING 65C30133 AND BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DAMAGED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN AT BS 727E PLUS 13 BETWEEN S2 AND 3L, AT BS 796, S3L, AT BS 278, BETWEEN S2 AND 3L, AT BS 488, S3L, AT BS 847 AND 858, S3L, AND AT BS 727D PLUS 3.75, ABOVE S3L. REPAIRED ALL PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SPLICE — CRACKED (BS 908)

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, S4L. REPLACED PER BOEING BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DAMAGE (BS 860-887)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DAMAGE FROM BS 860 TO BS 887, BETWEEN S2L AND S2R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FRAME — GOUGED (BS 344)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME GOUGED AT BS 344, S8R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — GOUGED (FWD SERVICE DOOR)

DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR OUTER SKIN GOUGED AT LOWER HINGE CUTOUT AT LOWER OUTER SKIN. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DENTED (BS 1054)

DURING SCHEDULED D-CHECK, FOUND FUSLAGE SKIN DENTED AT BS 1054, S17-18R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: BLKHD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE WEB CRACKED AT WL 219, LBL 11.4 AND AT WL 212, LBL 4.7. REPAIRED PER BOEING BOEING STRUCTURAL REPAIR MANUAL.

Part: FRAME — CRACKED (BS 807-887)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 807 AND BS 887, AT S9L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — GOUGED (FWD SERV DOOR)

DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR OUTER SKIN GOUGED AT LOWER HINGE CUTOUT LOWER EDGE. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOOR BEAM — CRACKED (BS 709)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM WEB CRACKED AT BS 709, BL 0 WL 204. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.