N696SW

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 65,364 hrs · 48,795 cycles

DURING SCHEDULED C2 CHECK, FOUND RT KEEL BEAM CORRODED AT BS 500D TO BS 520. REPAIRED KEEL BEAM PER SRM.

Part: TRUNNION PIN — CORRODED (RT MLG) · airframe 65,364 hrs · 48,795 cycles

DURING SCHEDULED C2 CHECK, FOUND RIGHT MLG BEAM CLEVIS TRUNNION PIN CORRODED. REMOVED AND REPLACED CLEVIS PER MT.

Part: BUSHING — CORRODED (RT MLG) · airframe 65,364 hrs · 48,795 cycles

DURING SCHEDULED C2 CHECK, FOUND RT MLG STRUT FWD TRUNNION LINK LUG HAT BUSHINGS CORRODED. REMOVED AND REPLACED MLG OUTER CYLINDER AND COLLAR PER MT.

Part: BUSHING — CORRODED (RT MLG) · airframe 65,364 hrs · 48,795 cycles

DURING SCHEDULED C2 CHECK, FOUND RT MLG TRUNNION LINK HAT BUSHINGS CORRODED. REMOVED AND REPLACED TRUNNION LINK PER MT.

Part: COVER — BROKEN (CABIN) · airframe 65,364 hrs · 48,795 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER BROKEN FROM ROW 6 TO ROW 7. REMOVED AND REPLACED EEPLS PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 65,364 hrs · 48,795 cycles

DURING SCHEDULED C2 CHECK, FOUND RT FUSELAGE KEEL BEAM CORRODED FROM BS 500C TO BS 540. REMOVED AND REPLACED KEEL BEAM SECTION PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 65,259 hrs · 48,715 cycles

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

Part: SKIN — CRACKED (BS 970 S21L) · airframe 64,434 hrs · 48,064 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 21L. REPAIRED SKIN PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,415 hrs · 48,047 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 740E S18R) · airframe 63,961 hrs · 47,689 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740E, STR 18R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 63,297 hrs · 47,168 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,627 hrs · 46,622 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BS 516D, STR 12R. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,619 hrs · 46,613 cycles

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

Part: SKIN — CRACKED (BS 517 S12L) · airframe 62,012 hrs · 46,123 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 517, STR 12L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 61,695 hrs · 45,865 cycles

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

Part: CHARGER — INOPERATIVE (CABIN) · airframe 61,509 hrs · 45,108 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD CABIN EMERGENCY BATTERY PACK CHARGER NOT CHARGING. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,738 hrs · 45,077 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 6 L/E SLAT SKIN CRACKED AT LOWER T/E. REPAIRED L/E SLAT SKIN PER SWA EA.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 60,738 hrs · 45,077 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP LOWER INBOARD CORNER DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 60,488 hrs · 44,877 cycles

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

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 60,375 hrs · 44,790 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED LOWER SURFACE. REMOVED AND REPLACED RT WING FLAP PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 60,375 hrs · 44,790 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,375 hrs · 44,790 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 59,802 hrs · 44,331 cycles

DURING SCHEDULED C3 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT AFT SPAR, STAB STA 125. REPAIRED STAB PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 58,744 hrs · 43,538 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: SKIN — CRACKED (BS 730E) · airframe 58,657 hrs · 43,474 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730E, STR 19R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 740D) · airframe 58,657 hrs · 43,474 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740D, STR 19R. REPAIRED SKIN PER SWA EA AND SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,624 hrs · 42,663 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 991.5, STR 24R. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,623 hrs · 42,662 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME INNER CHORD CRACKED AT BS 348.2, STR 15L. REMOVED AND REPLACED INNER FRAME CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,623 hrs · 42,662 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 10L. REPAIRED FRAME PER SWA EA.

Part: VERTICAL BEAM — CRACKED (FUSELAGE) · airframe 57,623 hrs · 42,662 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE VERTICAL BEAM WEB CRACKED AT BS 183.5, RBL 5.7, WL 185. REPAIRED WEB PER SWA EA & SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 57,623 hrs · 42,662 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 57,623 hrs · 42,662 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 57,623 hrs · 42,662 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500D, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,623 hrs · 42,662 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 10L. REPAIRED SKIN PER SWA EA.

Part: BULKHEAD — CRACKED (BS 178) · airframe 57,623 hrs · 42,662 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE VERTICAL BEAM WEB CRACKED AT BS 178 BULKHEAD, BETWEEN LBL 17.1 TO RBL 17.1, BETWEEN WL 212 TO WL 227. REPAIRED WEB PER SRM.

Part: FITTING — BROKEN (GIRT BAR) · airframe 57,623 hrs · 42,662 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT FLOOR FITTING BROKEN. REMOVED AND REPLACED FITTING PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,623 hrs · 42,662 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,623 hrs · 42,662 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: VERTICAL BEAM — CRACKED (FUSELAGE) · airframe 57,623 hrs · 42,662 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 181, RBL 17.1, WL 181. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,623 hrs · 42,662 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE WEB CRACKS AT BS 178 BULKHEAD, RBL 5 & LBL 5, WL 200. REPAIRED WEB PER SRM.

Part: LIGHT — BROKEN (MID CABIN) · airframe 56,908 hrs · 42,080 cycles

DURING SCHEDULED RON CHECK, FOUND RT OVERWING EMERGENCY WALL LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 56,836 hrs · 42,022 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 56,830 hrs · 42,016 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,919 hrs · 41,300 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 927 + 6, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 55,199 hrs · 41,300 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,454 hrs · 40,946 cycles

DURING SPV, FOUND FUSELAGE SKIN AT BS 727F + 15 BETWEEN STRINGER 18R AND STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 54,294 hrs · 39,994 cycles

L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,798 hrs · 38,801 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STRINGER 23L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,051 hrs · 38,209 cycles

MID CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 52,041 hrs · 38,202 cycles

DURING SCHEDULED C3 CHECK, FOUND BULLNOSE EMERGENCY LIGHT INOP AT RT SIDE, SECOND FROM AFT END. REMOVED AND REPLACED POWER SUPPLY ASSY PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 50,133 hrs · 36,708 cycles

DURING SCHEDULED C1 CHECK, FOUND RT OUTBOARD AFT T/E FLAP DELAMINATED AT NR 7 FAIRING. REMOVED AND REPLACED RT OUTBOARD AFT T/E FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,512 hrs · 36,206 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, BETWEEN STRINGERS 11R AND 13R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,512 hrs · 36,206 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD CARGO DOOR AFT CUT OUT FRAME CRACKED NEXT TO LOWEST STOP FITTING CASTING. REPAIRED FRAME PER SWA T1-653-044

Part: DOOR FRAME — CRACKED (FWD ENTRY DOOR) · airframe 49,512 hrs · 36,206 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR FRAME CRACKED AT 6TH FROM TOP STOP PIN CASTING ASSY. REPAIRED FRAME PER SRM.

Part: DOOR FRAME — CRACKED (FWD SVC DOOR) · airframe 49,512 hrs · 36,206 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR FRAME CRACKED AT CUTOUT AT 3RD FROM TOP STOP PIN CASTING. REPAIRED FRAME PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 49,512 hrs · 36,206 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BEADED WEB CRACKED AT BS 663, LBL 30. REPAIRED BEADED WEB PER SRM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 49,248 hrs · 35,985 cycles

FWD ENTRY DOOR EVACUATION SLIDE LOOSE. REINSTALLED SLIDE ASSY PER MM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 49,026 hrs · 35,808 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 5 GROUND SPOILER DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED NR 5 GROUND SPOILER PER MM.

Part: COVER — BROKEN (MID CABIN) · airframe 49,017 hrs · 35,802 cycles

RT OVERWING EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: FLAP — DELAMINATED (RH WING) · airframe 44,658 hrs · 32,190 cycles

DURING SCHEDULED C3 CHECK, FOUND RH WING OTBD AFT FLAP DELAMINATED. R&R AFT FLAP PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 44,412 hrs · 31,976 cycles

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

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 43,748 hrs · 31,407 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF ADJ (FWD SERVICE DOOR) · airframe 41,767 hrs · 29,801 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR GIRT ASSY OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.

Part: FRAME — CRACKED (CARGO DOOR) · airframe 41,256 hrs · 29,369 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 41,256 hrs · 29,369 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD T-CHORD CRACKED AT LBL 5, WL 184. REPAIRED T-CHORD PER TR T1-253-022.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 41,256 hrs · 29,369 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 178 BULKHEAD VERT WEB CRACKED AT WL 168, LBL 18. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (BULKHEAD) · airframe 41,256 hrs · 29,369 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 LT AND RT CHORD ANGLES CRACKED AT WL 207. REMOVED AND REPLACED LT AND RT CHORDS PER SRM.

Part: COVER — LOOSE (ROW 18) · airframe 41,256 hrs · 29,369 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EEPLS TRACK COVER LOOSE AT ROW 18. SECURED TRACK COVER PER MM.

Part: FRAME — CRACKED (SERVICE DOOR) · airframe 41,256 hrs · 29,369 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT FRAME CRACKED NEAR NR 3 STOP. REPAIRED FRAME PER TI-152-003.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 39,867 hrs · 2,821 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD EEPLS INOPERATIVE. R&R BATTERY PACK PER MM.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROW 6 AND FWD. REMOVED AND REPLACED POWER SUPPLY UNIT PER MM.

Part: SWITCH — INOPERATIVE (LE FLAP)

AIR TURNBACK, NR 2 L/E SLAT TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 2 L/E SLAT ROD END SWITCH PER MM.

Part: SLIDE — LOW PRESS (SERVICE DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESS LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: WEB — CRACKED (BS 1032-1034)

DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 1034, LBL 2 WL 209, BS 1033 LBL 9.5 WL 209 AND BS 1032 LBL 18 WL 209. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 887/827/887)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET AT BS 887, STR 9 LT BS 827 STR 9 LT AND BS 887 STR 9 RT. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 1032)

DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 1032 RBL 16 WL 209. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 519)

DURING SCHEDULED D-CHECK, FOUND CRACKED SHEAR WEB AT BS 519, RBL 25, WL 206. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 316/996/1007)

DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 316, 2 BELOW STR 2 LT AND BS 996 AND 1007, 4 ABOVE STR 14 LT. REPAIRED PER BOEING SRM.

Part: STIFFENER — DAMAGED (BS 520)

DURING SCHEDULED D-CHECK, FOUND CRACKED MECHANICAL DAMAGE IN STIFFENER ANGLE AT BS 520, RBL 25, WL 200. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 847/400/360)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET AT BS 847 STR 9 RT, BS 400 STR 9 LT AND BS 360 STR 9 RT. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 964-978)

DURING SCHEDULED D-CHECK, FOUND CORRODED THRESHOLD Z-SUPPORT ANGLES AFT SERVICE DOOR AT BS 964 TO 978 RBL 55 WL 209. REMOVED AND REPLACED PER BOEING SRM, DAMAGE OUT OF LIMITS.

Part: INTERCOSTAL — CORRODED (BS 747-767)

DURING SCHEDULED D-CHECK, FOUND CORRODED INTERCOSTAL AT BS 747 TO 767 RBL 20, WL 155. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 294)

DURING SCHEDULED D-CHECK, FOUND CRACKED L-ANGLE AT BS 294, WL 208.5, RBL 55. REPAIRED PER BOEING SRM.

Part: FRAME — DENTED (BS 500)

DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 500, LBL 63 WL 215. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 519-500 380)

DURING SCHEDULED D-CHECK, FOUND CRACKED SHEAR WEB AT BS 519 LBL 25 WL 205, BS 500 D+11 BL 0 WL 208 AND BS 380 TO 400 WL 207 BL 0. REPAIRED PER BOEING SRM.

Part: SUPPORT — CRACKED (BS 540)

DURING SCHEDULED D-CHECK, FOUND CRACKED FLOOR SUPPORT AT BS 540 LBL 28 WL 207. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 328)

DURING SCHEDULED D-CHECK, FOUND CRACKED FLOORBEAM L-ANGLE AT BS 328 LBL 45 WL 207. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 328)

DURING SCHEDULED D-CHECK, FOUND CRACKED FLOORBEAM STIFFENER AT BS 328, RBL 33, WL 200. REPAIRED PER BOEING SRM.

Part: SUPPORT — CRACKED (BS 328)

DURING SCHEDULED D-CHECK, FOUND CRACKED CHANNEL SUPPORT AT BS 328, LBL 44.5, WL 208. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 519)

DURING SCHEDULED D-CHECK, FOUND CRACKED ANGLE STIFFENER AT BS 519 RBL 25 WL 206, BS 519 LBL 25 WL 205 AND BS 519 LBL 45 WL 206. REPAIRED PER BOEING SRM.

Part: CHORD — CORRODED (BS 270)

DURING SCHEDULED D-CHECK, FOUND CORRODED Z-CHORD AT BS 270, WL 207, RBL 9 TO LBL 9. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 301.9)

DURING SCHEDULED D-CHECK, FOUND MECHANICAL DAMAGE ON FRAME AT BS 294, LBL 50, WL 267. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM AT BS 312, WL 207, LBL 14. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 277)

DURING SCHEDULED D-CHECK, FOUND CRACKED WEB INTERCOSTAL AT BS 277, RBL 56, WL 231. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 290)

DURING SCHEDULED D-CHECK, FOUND CRACKED ANGLE STIFFENER AT BS 290, RBL 54, WL 240 AND BS 290, RBL 25, WL 254. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 500)

DURING SCHEDULED D-CHECK, FOUND CORRODED WEB AT BS 500+11 AND 18, RBL 70 WL 208, BS 500 A+7 RBL 70 WL 208 AND BS 500 C+10 TO 18 RBL 70 WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 301.9)

DURING SCHEDULED D-CHECK, FOUND CRACKED L-ANGLE AT BS 301.9, LBL 54, WL 257.5. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CORRODED (BS 390/424/454)

DURING SCHEDULED D-CHECK, FOUND CORRODED WEB AT BS 390 RBL 70 WL 208, BS 424 TO 438 RBL 70 WL 208 AND BS 454 RBL 70 WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CORRODED (BS 381-389)

DURING SCHEDULED D-CHECK, FOUND CORRODED WEB AT BS 381 TO 389, LBL 70, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 179)

DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL CRACKED AT BS 179, RBL 25 AND LBL 25. REPLACED BOTH PER BOEING SRM.

Part: WEB — CORROSION (BS 704-885)

DURING SCHEDULED D CHECK, FOUND CORROSION ON WEB AT BS 828 TO 830, WL 208, LBL 70; BS 704, WL 208, RBL 65; BS 878 TO 885, RBL 70, WL 208;BS 901, WL 208, RBL 65. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORROSION (BS 986)

DURING SCHEDULED D CHECK, FOUND CORROSION ON FLOORBEAM UPPER AND LOWER AT BS 986, RBL 44, WL 208. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORROSION (BS 993)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOOR SUPPORT FITTING AT NAT 993, WL 208, LBL 34. REPAIRED PER BOEING SRM.

Part: STUB FRAME — CRACKED (BS 299)

DURING SCHEDULED D CHECK, FOUND CRACKED STUB FRAME AT BS 299, WL 210, RBL 55. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 727)

DURING SCHEDULED D-CHECK, FOUND CRACKED SUPPORT ANGLE BS 727+2 LBL 1, WL 169. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND WEB CRACK AT BS 178 BL 0 WL 188. REMOVED AND REPLACED PER SWA T1-353-057.

Part: SKIN — DENTED (BS 940.5)

DURING SCHEDULED D-CHECK, FOUND DENT IN SKIN AT BS 940.5, BELOW STR 23 RT, BS 348, 1 BELOW STR 22 RT, BS 362 TO 374 2-6 ABOVE STR 19 RT. REPAIRED PER BOEING SRM.

Part: LATCH — OUT OF ADJUST (SERV DOOR)

RETURNED TO PHC, DUE TO AFT SERVICE DOOR OPEN WARNING LIGHT ILLUMINATING. RIGGED DOOR LATCH ADJUSTMENT AND REMOVED AND REPLACED LOCK CAM PLATE PER BOEING M/M.