N062SW

Part: BRACKET — LOOSE (CABIN) · airframe 66,077 hrs · 73,079 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY AND FWD SVC DOOR GIRT BAR FLOOR BRACKETS LOOSE. SECURED BRACKETS PER MM.

Part: BATTERY PACK — LOOSE (CABIN) · airframe 66,077 hrs · 73,079 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT EMERGENCY LIGHT BATTERY PACK LOOSE IN MOUNT ASSY. SECURED BATTERY PACK PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 65,829 hrs · 72,820 cycles

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

Part: BATTERY — INOPERATIVE (CABIN) · airframe 65,716 hrs · 72,705 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT OUTSIDE AFT DOORS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 65,578 hrs · 72,552 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY LIGHTING INOP. REPAIRED M186 WIRE PER WDM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 65,578 hrs · 72,552 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD VERTICAL CHORD CRACKED, RBL 5.7, WL 182. REPAIRED CHORD PER SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 65,578 hrs · 72,552 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND AFT CARGO DOOR FUSELAGE SKIN CUTOUT, FWD LOWER CORNER CRACKED. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 65,578 hrs · 72,552 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKED, LBL 5.7 TO RBL 5.7. REPAIRED BULKHEAD PER SRM.

Part: WIRE — DAMAGED (ROW 11-16) · airframe 65,235 hrs · 72,206 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS DIM BETWEEN ROWS 11-16. REPAIRED WIRING PER MM.

Part: STRAP — WORN (PAX DOOR SLIDE) · airframe 65,129 hrs · 72,076 cycles

FWD ENTRY DOOR EVACUATION SLIDE GIRT BAR RETAINING STRAP PAD WORN. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP ABOVE BOTH OVERWING EXITS. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SLIDE — TORN (AFT ENTRY)

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE GIRT FABRIC TORN. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT OVERWING AND AFT END ON CABIN. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — DETACHED (SERVICE DOORWAY)

AFT SERVICE DOOR EVACUATION SLIDE SECTION FELL OUT OF CONTAINER. REPOSITIONED SLIDE ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SECTION OF EEPLS DIM. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — MISSING (CABIN)

DURING SCHEDULED C3 CHECK, FOUND EEPLS AFT END CAP MISSING. INSTALLED END CAP PER MM.

Part: WEB — CRACKED (BS 663)

DURING SCHEDULED C3 CHECK, FOUND BS 663 PRESSURE WEB CRACKED, RBL 39.5. REPAIRED WEB PER SWA RA NR 1-253-2149.

Part: SKIN — CRACKED (BS 780)

DURING SCHEDULED SERVICE CHECK, FOUND 2 INCH LONG CRACK AT FUSELAGE SKIN, BS 780, BELOW SRINGER 21L. REPAIRED SKIN PER SRM.

Part: CONNECTOR — FAILED (RT PACK)

CABIN WOULD NOT HOLD PRESSURIZATION DURING CLIMBOUT. RETURNED TO BWI AND MADE AN UNEVENTFUL LANDING. REPAIRED CANNON PLUG ON RT A/C PACK VALVE PER M/M. PRESSURIZATION AND A/C SYS OPS CHECKED OK.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED D-CHECK, FOUND RT EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BOTH BATTERY PACKS PER BOEING MM.

Part: KEELBEAM — CRACKED (BS 650)

DURING SCHEDULED D CHECK, FOUND CRACK IN LT KEEL BEAM AT BS 650. REPAIRED PER TRAMCO EWO 98-1176.

Part: SKIN — CRACKED (BS 908-947)

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FUSELAGE SKIN CRACK, AT BS 908 TO 947, STRINGER 14L. REPAIRED PER DALFORT XEA X2-53-227.

Part: KEEL BEAM — CORRODED (BS 727)

DURING SCHEDULED D-CHECK, FOUND KEEL BEAM CORRODED AT BS 727, AT S27 LT AND RT. REPLACED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 380)

DURING SCHEDULED D-CHECK, FOUND STRINGER 26L CRACKED AT UPPER FLANGE BS 380. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 760)

DURING SCHEDULED D-CHECK, FOUND STRINGER 16R FLANGE CRACKED BS 760. REPAIRED PER BOEING SRM.

Part: FRAME — DENTED (BS 807)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 807 AT LBL 28, WL 160. REPAIRED PER BOEING SRM.

Part: SPAR — CRACKED (LT WING)

DURING SCHEDULED D-CHECK, FOUND LEFT WING CENTER FUEL CELL UPPER REAR SPAR SEAL CUP CRACKED. REPAIRED PER TRAMCO EWO 98-1085.

Part: FLOORBEAM — DAMAGED (BS 727)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM TOP CHORD DAMAGED AT BS 727A, RBL 58, WL 208. REPLACED DAMAGED SECTION PER BOEING SRM.

Part: BEAM — CRACKED (BS 616)

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CRACKED AT BS 616, LBL 65, WL 208. REPLACED DAMAGED SECTION PER BOEING SRM.

Part: SPLICE — CORRODED (BS 907)

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, RBL 12. REPAIRED PER BOEING SRM.

Part: SPLICE — CORRODED (BS 359)

DURING SCHEDULED D-CHECK, FOUND FACTORY STRINGER SPLICE CORRODED AT STRINGER 27L, BS 359, WL 147. REPLACED PER BOEING SRM.

Part: SKIN — DENTED (EMER EXIT DOOR)

DURING SCHEDULED D-CHECK, FOUND RT OVERWING EXIT HATCH DENTED ON LOWER EXT SKIN. RESKINNED DOOR PER BOEING SRM.

Part: SPLICE — CORRODED (BS 927)

DURING SCHEDULED D-CHECK, FOUND STRINGER 26L CORRODED AT BS 927, LBL 12. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 328/360)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 328 BELOW S20R AND BS 360, AT S20R. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 580.5)

DURING SCHEDULED D-CHECK, FOUND CRACK IN S17R O/B CHORD, AT BS 580.5. REPAIRED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 767)

DURING SCHEDULED D-CHECK, FOUND STRINGER 20R CORRODED AT BS 767. REPLACED DAMAGED SECTION PER BOEING SRM.

Part: FRAME — CRACKED (BS 559)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559 AT RBL 66, WL 216. REPLACED DAMAGED SECTION PER BOEING SRM.

Part: SPLICE — CRACKED (BS 360)

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, AT S4L. REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 400)

DURING SCHEDULED D CHECK, FOUND CRACK IN FUSELAGE FRAME AT BS 400, 3 ABOVE S21L. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 752-758)

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 752 TO 758 BETWEEN S8-9L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (LT WING)

DURING SCHEDULED D CHECK, FOUND LT WING L/E BULLNOSE CRACKED AT LOWER EDGE OF NR 3 SLAT I/B STOP. REPAIRED PER BOEING SRM.

Part: FRAME — DENTED (BS 500)

DURING SCHEDULED D CHECK, FOUND FUSE FRAME DENTED AT BS 500, S23R. REPAIRED PER BOEING SRM.

Part: CHORD — CORRODED (BS 907)

DURING SCHEDULED D CHECK, FOUND FRAME FAIL/SAFE CHORD CORRODED AT BS 907, RBL 31, WL 173. REPAIRED PER BOEING SRM.

Part: CHORD — DAMAGED (BS 185-188)

DURING SCHEDULED D CHECK, FOUND LOWER CHORD DAMAGED AT BS 185 TO 188, AT S10L, WL 233. REPAIRED PER BOEING SRM.

Part: SKIN — DAMAGED (BS 727)

DURING SCHEDULED D CHECK, REPLACED FUSELAGE SKIN LAP REPAIR AT BS 727A+10. REPLACED PER BOEING SRM.

Part: SUPPORT — DAMAGED (BS 540)

DURING SCHEDULED D CHECK, FOUND FLOORBEAM SUPPORT DAMAGED AT BS 540. REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 911)

DURING SCHEDULED D CHECK, FOUND FUSE SKIN DENTED AT BS 911, 2 BELOW S17R. REPAIRED PER BOEING SRM.

Part: DOUBLER — CRACKED (BS 678)

DURING SCHEDULED D CHECK, FOUND CRACK IN AILERON QUADRANT DOUBLER AT BS 678, LBL AND RBL 25, WL 206. REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND CRACK AT WL 218, LBL 11 TO 12, BS 178. REPAIRED PER BOEING SRM.

Part: STRINGER — GOUGED (BS 341)

DURING SCHEDULED D-CHECK, FOUND GOUGES AND DRILL START ON STRINGER AT BS 341, 8R. REMOVED AND REPLACED STRINGER AND SPLICE PER BOEING SRM.

Part: SKIN — DENTED (BS 188)

DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 188, STR 14L. REMOVED AND REPLACED SKIN PER BOEING SRM.

Part: SKIN — DENTED (BS 1051)

DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 1051 BETWEEN STR 27R AND 37L. REPAIRED DOUBLER PER BOEING SRM.

Part: BULKHEAD ANGLE — CORRODED (BS 520)

DURING SCHEDULED D-CHECK, FOUND CORRODED LT BULKHEAD SUPPORT ANGLE AT BS 520, LBL 26, WL 157. REMOVED AND REPLACED BULKHEAD SUPPORT ANGLE PER BOEING SRM.

Part: BULKHEAD ANGLE — CORRODED (BS 520)

DURING SCHEDULED D-CHECK, FOUND CORRODED ON RT BULKHEAD SUPPORT ANGLE AT BS 520, RBL 26, WL 157. REPAIRED PER BOEING SRM.

Part: SKIN — MISREPAIRED (BS 489.5-499.5)

DURING SCHEDULED D-CHECK, FOUND BLIND FASTENER IN SKIN REPAIR AT BS 489.5 TO BS 499.5, STR 7R. REMOVED EXISTING BLIND FASTENER AND REPAIR CUT OUT DAMAGE PER BOEING SRM.

Part: SKIN — CRACKED (GALLEY DOORWAY)

DURING SCHEDULED D-CHECK, FOUND FWD GALLEY DOOR HINGE CUTOUT CRACKED ON THE FWD LWR CORNER. REPAIRED CUTOUT PER BOEING SRM.

Part: SKIN — CHAFED (RT WING)

DURING SCHEDULED D-CHECK, FOUND LEADING EDGE SKIN ABOVE NR 2 ENGINE PYLON IS CHAFED. REMOVED AND REPLACED SKIN PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 294)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT LBL 12, WL 208, BS 294. REMOVED AND REPLACED FLOOR SUPPORT PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 767-787)

DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 767 TO 787 CRACKED, RT STRINGER 25, WL 149. REMOVED AND REPLACED INTERCOSTAL PER BOEING SRM.

Part: DOUBLER — CRACKED (BS 332.1)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME DOUBLER AT BS 332.1, RBL 63, WL 216. REMOVED AND REPLACED FRAME DOUBLER PER BOEING SRM.

Part: ANGLE — CRACKED (BS 993)

DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL SUPPORT ANGLE CRACKED AT BS 933, BL 0, WL 208. REMOVED AND FABRICATED INTERCOSTAL SUPPORT ANGLE PER BOEING SRM.

Part: INTERCOSTAL — DENTED (BS 400-420)

DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL DENTED AT BS 400 TO 420, LBL 21, WL 156. REMOVED AND REPLACED INTERCOSTAL PER BOEING SRM.

Part: SKIN — DENTED (BS 500-517)

DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 500+17, 2 ABOVE STR 18 RT. REPAIRED SKIN PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 277-294.5)

DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL AT BS 277 TO 294.5, BL 0, WL 208. REMOVED AND REPLACED INTERCOSTAL PER BOEING SRM.

Part: FLOORBEAM — CHAFING (BS 767)

DURING SCHEDULED D-CHECK, FOUND CHAFING AROUND FASTENER HOLES IN FLOORBEAM AT BS 767, RBL 10 TO LBL 11, WL 208. CUT OUT DAMAGE AREA AND REPAIRED PARTS PER BOEING SRM.

Part: WEB — CORRODED (BS 986-1016)

DURING SCHEDULED D-CHECK, FOUND CORRODED WEB AT BS 986 TO 1016M RBL 39 TO 46, WL 208. REMOVED AND REPLACED WEB PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 1010)

DURING SCHEDULED D-CHECK, FOUND CORRODED TOP FLANGE OF FLOORBEAM AT BS 947, LBL 24 TO LBL 26 WL 208.

Part: INTERCOSTAL — BROKEN (BS 500-520)

DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL BROKEN AT BS 500B TO 520, LBL 21, WL 156. REMOVED AND REPLACED INTERCOSTAL PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 995-1004)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT NUT CLIP BS 995 TO 1004, LBL 14, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED D-CHECK, FOUND CORRODED AT BS 328 FLOORBEAM UPPER T-CHORD, RBL 35, WL 208. REMOVED AND REPLACED UPPER CHORD AND ANGLES PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 500-520)

DURING SCHEDULED D-CHECK, FOUND CORRODED RIGHT HAND INTERCOSTAL AT BS 500B TO BS 520, STR 26R. REMOVED AND REPLACED INTERCOSTAL PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 1010)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 1010, LBL 8, WL 208 AROUND NUT CLIP HOLES. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 500)

DURING SCHEDULED D-CHECK, FOUND CORRODED RIGHT HAND INTERCOSTAL AT BS 500A TO BS 500B, STR 26R. REMOVED AND REPLACED INTERCOSTAL PER BOEING SRM.

Part: TRACK — CORRODED (BS 993)

DURING SCHEDULED D-CHECK, FOUND CORRODED HAT TRACK AT NUT CLIP BS 993, LBL 18 TO LBL 41, WL 208. REMOVED AND REPLACED HAT TRACK PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 987)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM AT NUT CLIP BS 987, RBL 45, LBL 45, WL 208. REMOVED AND REPLACED TOP CHORD AND ANGLES PER TI-A53-055.

Part: SUPPORT — CORRODED (BS 992-1010)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 992 TO 1010, LBL 40, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — MISDRILLED (BS 907-927)

DURING SCHEDULED D-CHECK, FOUND WEB AT BS 907 TO 927, LBL 59 TO 63, WL 208 HAS MISDRILLED HOLE AT BS 920, LBL 59. REMOVED AND REPLACED PER BOEING SRM.

Part: SPLICE — DAMAGED (BS 500)

DURING SCHEDULED D-CHECK, FOUND DAMAGE FASTENER HEAD ON FWD CARGO PIT FRAME SPLICE AT BS 500A, STR 25R. REMOVED AND REPLACED FASTENER PER BOEING SRM.

Part: ANGLE — MISDRILLED (BS 920)

DURING SCHEDULED D-CHECK, FOUND L-ANGLE AT BS 920, LBL 59 TO 63, WL 207 HAS MISDRILLED HOLE AT BS 920, LBL 59, WL 207. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — PUNCTURED (BS 992-1016)

DURING SCHEDULED D-CHECK, FOUND WEB PUNCTURED AT BS 992 TO 1016, LBL 40 TO 45, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CHAFED (BS 727)

DURING SCHEDULED D-CHECK, FOUND CHAFING AROUND FASTENER HOLES IN FLOORBEAM AT BS 727B, LBL 35 TO LBL 58, WL 208. REMOVED AND REPLACED FLOORBEAM PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 420)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON TOP FLANGE OF FLOORBEAM AT NUTCLIP LOCATION AT BS 420, RBL 20, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: CLIP — DAMAGED (BS 420)

DURING SCHEDULED D-CHECK, FOUND MECHANICAL DAMAGE ON STRINGER CLIP (14L) AT BS 420. REMOVED AND REPLACED STRINGER CLIP PER BOEING SRM.

Part: FLOORBEAM — CHAFED (BS 787)

DURING SCHEDULED D-CHECK, FOUND CHAFING AROUND FASTENER HOLES IN FLOORBEAM AT BS 787, RBL 10 TO LBL 11, WL 208. REMOVED AND REPLACED FLOORBEAM PER BOEING SRM AND INSTALLED REPAIR STRAP PER SWA TI-A53-014.

Part: ANGLE — CORRODED (BS 986-999)

DURING SCHEDULED D-CHECK, FOUND DRILL START AND CORRODED FLOOR SUPPORT ANGLE AT BS 986 TO 999, RBL 45, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — DAMAGED (BS 380)

DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIP AT BS 380, STR 2 RT HAS MECHANICAL DAMAGE. REMOVED AND REPLACED STRINGER TIE CLIP PER BOEING SRM.

Part: CHORD — CORRODED (BS 294)

DURING SCHEDULED D-CHECK, FOUND CORRODED UPPER T-CHORD OF 294 FLOORBEAM, AT WL 208. REMOVED AND REPLACED T-CHORD PER BOEING SRM.

Part: FLOORBEAM — CHAFED (BS 344)

DURING SCHEDULED D-CHECK, FOUND AREAS OF BARE METAL AND CHAFING ON FLOORBEAM AT BS 344, LBL 57 TO RBL 57, WL 208.1. REMOVED AND REPLACED UPPER CHORD PER BOEING SRM.

Part: SKIN — DENTED (BS 409)

DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 409 BETWEEN STR 21R AND 22R. CUT OUT DAMAGED AREA, REMOVED AND REPLACED DOUBLER PER BOEING SRM.

Part: ANGLE — MISDRILLED (BS 920)

DURING SCHEDULED D-CHECK, FOUND L-ANGLE AT BS 920, RBL 59 TO 63, WL 208 HAS MISDRILLED HOLE. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 302)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 302, LBL 12, WL 208. REMOVED AND REPLACED FLOOR SUPPORT PER BOEING SRM.

Part: CLIP — DAMAGED (BS 440)

DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIP AT BS 440, STR 7 RT HAS MECHANICAL DAMAGE. REMOVED AND REPLACED STRINGER TIE CLIP PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 947)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON TOP FLANGE OF FLOORBEAM AT BS 947, RBL 44 TO RBL 53, WL 208. REMOVED AND REPLACED FLOORBEAM PER BOEING SRM.

Part: INTERCOSTAL — CHAFED (BS 500-520)

DURING SCHEDULED D-CHECK, FOUND 5 CHAFED AREAS ON INTERCOSTAL AT NUTCLIP LOCATIONS BS 500B-520, BL 0, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — DAMAGED (BS 500)

DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIP MECHANICAL DAMAGE AT BS 500 RT, STR 7R. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (LT MLG)

DURING SCHEDULED D-CHECK, FOUND LT MAIN LANDING GEAR STABILIZER BAR FAIRING L-ANGLES PITTED AND CORRODED AROUND BOLT HOLES. REMOVED AND REPLACED L-ANGLES PER BOEING SRM.

Part: WEB — MISDRILLED (BS 907-927)

DURING SCHEDULED D-CHECK, FOUND MISDRILLED HOLE IN WEB AT BS 907 TO 927, RBL 59-63, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 1138)

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE BELOW STR 5A RT, BS 1138 CRACKED AT FASTENER HOLE. REMOVED AND REPLACED SHEAR TIE PER BOEING SRM.

Part: ANGLE — CORRODED (BS 1011)

DURING SCHEDULED D-CHECK, FOUND CORRODED ANGLES AT BS 1011, RBL 42, WL 208.5. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — DAMAGED (BS 328)

DURING SCHEDULED D-CHECK, FOUND ELONGATED HOLES AT RBL 14, LBL 12, LBL 22.5, WL 207 AT BS 328. REPAIRED DAMAGED WEB PER BOEING SRM.

Part: WEB — DAMAGED (BS 328)

DURING SCHEDULED D-CHECK, FOUND ELONGATED HOLES FROM RBL 25 TO RBL 30, WL 207 AT BS 328. WHILE WORKING CUSTOMER CARD NR A617871. REPAIRED DAMAGED TO WEB BS 328 PER BOEING SRM.

Part: SPLICE — CRACKED (BS 1106-1154)

DURING SCHEDULED D-CHECK, FOUND SPLICE STRAP AT BS 1106-11 TO 4, STR 5AR CRACKED. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CORRODED (BS 771)

DURING SCHEDULED D-CHECK, FOUND BULGING SKIN AT BS 771, BL 0, WL 149. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DAMAGED (BS 1137-1156)

DURING SCHEDULED D-CHECK, FOUND BLIND FASTENER IN SKIN DOUBLER AT BS 1137 TO 1156 STR 3L. REMOVED AND REPLACED PER BOEING SRM.

Part: FASTENER — MISINSTALLED (FRAME CHORD)

DURING SCHEDULED D-CHECK, FOUND AT BS 639 RT, FASTENER GOING THROUGH I/B FRAME CHORD NOT INSTALLED AS PER BOEING SRM. REMOVED AND REPLACED NEW FASTENER IN FRAME CHORD PER BOEING SRM.

Part: SKIN — DENTED (BS 1051)

DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 1051 BETWEEN STR 20 AND 21 RT. CUT OUT DAMAGED AREA PER BOEING SRM AND FABRICATED DOUBLER.

Part: BULKHEAD STRIP — CORRODED (BS 1030)

DURING SCHEDULED D-CHECK, FOUND CORRODED BULKHEAD SEAL RETAINING STRIP AT BS 1030, RBL 19, WL 209.5. REMOVED AND REPLACED PER BOEING SRM.

Part: HINGE — BROKEN (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND BROKEN HINGE ON EXTERNAL POWER RECEPTACLE DOOR. REMOVED AND REPLACED BROKEN HINGE PER BOEING SRM.

Part: SKIN — CRACKED (NR 4 LE SLAT)

DURING SCHEDULED D-CHECK, FOUND FIXED L/E AT NR 4 SLAT O/B AUX TRACK, CUTOUT HAS A STOP DRILLED CRACK. REMOVED CRACK AREA, FABRICATED DOUBLER AND FILLER PER SWA TR T1-251-008.

Part: SKIN — DAMAGED (BS 1137-1156)

DURING SCHEDULED D-CHECK, FOUND BLIND FASTENER IN SKIN DOUBLER AT BS 1137 TO 1156 STR 3R. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD STRIP — CORRODED (BS 1032)

DURING SCHEDULED D-CHECK, FOUND CORRODED BULKHEAD SEAL RETAINING STRIP AT BS 1032, LBL 12, WL 209.5. REMOVED ADH REPLACED PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 400)

DURING SCHEDULED SERVICE VISIT CHECK, FOUND SHEAR TIE AT STR 14R, BS 400 CRACKED. REPAIRED PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 480)

DURING SCHEDULED SERVICE VISIT CHECK, FOUND SHEAR TIE AT STR 14R, BS 480 CRACKED. REPAIRED PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 360)

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

Part: SHEAR TIE — MISDRILLED (BS 967, 986,1006)

DURING SCHEDULED SERVICE VISIT CHECK, FOUND 3 SHEAR TIES AT BS 967-986.5 AND 1006, STR 4R HAVE MISDRILLED HOLES. REPAIRED PER BOEING SRM.

Part: SPLICE — CRACKED (BS 908)

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND CRACKED 14L STRINGER SPLICE AT BS 908. REPLACED CRACKED STRINGER SPLICE PER BOEING SRM.

Part: STRINGER — CRACKED (BS 927-247)

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND HFEC INDICATES 6 FASTENER HOLES CRACKED STR 14R, AT BS 927-947. REPAIRED PER XEA X2-53-224.

Part: STRINGER — CRACKED (BS 927-947)

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND HFEC INDICATES 7 FASTENER HOLES CRACKED STR 14L, AT BS 927-947. REPAIRED PER XEA X2-53-224 REV 1.

Part: STRINGER — CRACKED (BS 927-247)

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND HFEC INDICATES 3 FASTENER HOLES CRACKED STR 10R, AT BS 927-947. REPAIRED PER XEA X2-53-224.

Part: STRINGER — CRACKED (BS 908-947)

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND HFEC INDICATES 15 FASTENER HOLES CRACKED STR 10L, AT BS 908-947. REMOVED AND REPLACED DAMAGED FASTENER HOLES PER XEA X2-53-223.

Part: STRINGER — CRACKED (BS 986-1006)

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND HFEC INDICATES 3 FASTENER HOLES CRACKED STR 14L, AT BS 986-1006. INSTALLED REPAIRED DOUBLERS PER BOEING SRM.

Part: SKIN — CRACKED (BS 540-727)

DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 540 TO 727 AT S4L PER SWA ACO 6717-53 REV 5.

Part: SKIN — CRACKED (BS 727-908)

DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 727 TO 908 AT S10L PER SWA ACO 6717-53 REV 5.

Part: SKIN — CRACKED (BS 727-908)

DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 727 TO 908 AT S4L PER SWA ACO 6717-53 REV 5.

Part: SKIN — CRACKED (BS 360-540)

DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 360 TO 540 AT S4L PER SWA ACO 6717-53 REV 5.

Part: SKIN — CRACKED (BS 908-1016)

DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 908 TO 1016 AT S4R PER SWA ACO 6717-53 REV 5.

Part: SKIN — CRACKED (BS 908-951)

DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 908 TO 951 AT S10L PER DALFORT XEA X2-53-223.

Part: SKIN — CRACKED (BS 727-908)

DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 727 TO 908 AT S4R PER SWA ACO 6717-53 REV 5.

Part: SKIN — CRACKED (BS 908-951)

DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 908 TO 951 AT S10R PER DALFORT XEA X2-53-223.

Part: SKIN — CRACKED (BS 360-540)

DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 360 TO 540 AT S10R PER SWA ACO 6717-53 REV 5.

Part: SKIN — CRACKED (BS 290)

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND CRACK INDICATION AT BS 290, S4R. REPAIRED PER SWA ACO 6717-53 REV 5.

Part: SKIN — CRACKED (BS 727-908)

DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 727 TO 908 AT S1OR PER SWA ACO 6717-53 REV 5.

Part: SKIN — CRACKED (BS 908-1016)

DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 908 TO 1016 AT S4L PER SWA ACO 6717-53 REV 5.

Part: SKIN — CRACKED (BS 360-540)

DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 360 TO 540 AT S4R PER SWA ACO 6717-53 REV 5.

Part: SKIN — CRACKED (BS 908-951)

DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 908 TO 951 AT S14R PER DALFORT XEA X2-53-224.

Part: SKIN — CRACKED (BS 360-540)

DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 360 TO 540 AT S10L PER SWA ACO 6717-53 REV 5.

Part: SKIN — CRACKED (BS 540-727)

DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 540 TO 727 AT S4R PER SWA ACO 6717-53 REV 5.

Part: SKIN — CRACKED (BS 908-951)

DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 908 TO 951 AT S14L PER DALFORT XEA X2-53-224 REV 1.

Part: SKIN — CRACKED (BS 360-540)

DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 360 TO 540 AT S14L PER SWA ACO 6717-53 REV 5.

Part: SKIN — CRACKED (BS 360-540)

DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 360 TO 540 AT S14R PER SWA ACO 6717-53 REV 5.

Part: INTERCOSTAL — CRACKED (CARGO COMPT)

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR UPLATCH MECHANISM INTERCOSTAL CRACKED. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 520)

DURING SCHEDULED SERVICE CHECK, FOUND CRACKED SKIN 0.15 INCH LONG AT BS 520 RBL 1. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 480)

DURING SCHEDULED SERVICE CHECK, FOUND CRACKED SKIN 0.15 INCH LONG AT BS 480 RBL 2. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 420)

DURING SCHEDULED SERVICE CHECK, FOUND CRACKED SKIN .25 INCH LONG AT BS 420 RBL 3. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 790)

DURING SCHEDULED SERVICE CHECK, FOUND CRACKED SKIN 0.15 INCH LONG AT BS 790 LBL 2. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED RON CHECK, FOUND CRACKED SKIN ON LT FUSELAGE AT 48 AFT OF FLAP AND 10 BELOW SKIN LAP JOINT. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727)

DURING SERVICE CHECK, FOUND SKIN HAS A 2 DEGREE INCH CRACK AT FS 727A JUST BELOW STR 18L. REPAIRED PER BOEING SRM.