N343SW

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,106 hrs · 64,544 cycles

DURING SCHEDULED SPV CHECK, FOUND STUB BEAM FRAME CRACKED AT RT BS 616, BOTTOM FASTENER HOLE COMMON TO INNER CHORD. REMOVED AND REPLACED FRAME IAW EA.

Part: SIGN — BROKEN (CABIN) · airframe 72,193 hrs · 63,859 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 72,086 hrs · 63,785 cycles

DURING SCHEDULED 2HC2 CHECK FOUND, LT WING NR 2 SLAT L/E SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 72,075 hrs · 63,776 cycles

DURING SCHEDULED HC2 CHECK FOUND, LT WING NR 1 SLAT L/E SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,352 hrs · 63,209 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 259.5+13, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,352 hrs · 63,209 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 259.5+13, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,352 hrs · 63,209 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 515, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,352 hrs · 63,209 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 396, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,352 hrs · 63,209 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 515D, STR 15L. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 71,165 hrs · 63,066 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR FWD WEB CRACKED AT BS 947.5, STR 10L. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,165 hrs · 63,066 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,165 hrs · 63,066 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 947, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,165 hrs · 63,066 cycles

DURING SCHEDULED 22YY CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708, BBL 0.07. REPAIRED WEB PER SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,165 hrs · 63,066 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 750, STR 14L. REPAIRED SKIN PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,165 hrs · 63,066 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 71,165 hrs · 63,066 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 1001, STR 5R. REPAIRED STRINGER PER SRM AND ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,165 hrs · 63,066 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 71,165 hrs · 63,066 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 71,165 hrs · 63,066 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 500, STR 2L. REMOVED AND REPLACED STRINGER PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 71,165 hrs · 63,066 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EXIT SIGN LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,165 hrs · 63,066 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 25. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,165 hrs · 63,066 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10R. REMOVED AND REPLACED CLIP PER SI.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,165 hrs · 63,066 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM LOWER CHORD CRACKED AT BS 714, BL 0. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,165 hrs · 63,066 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 9L. REMOVED AND REPLACED CLIP PER SI.

Part: FLAP — DELAMINATED (RT WING) · airframe 71,165 hrs · 63,066 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,165 hrs · 63,066 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 4L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,165 hrs · 63,066 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,165 hrs · 63,066 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SI.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,165 hrs · 63,066 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,162 hrs · 63,065 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,506 hrs · 62,575 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 750, STR 14L. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,409 hrs · 62,494 cycles

LT OVERHEAD EMERGENCY EXIT LIGHT INOP BETWEEN ROW 17 TO ROW 21. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,409 hrs · 62,494 cycles

RT OVERHEAD EMERGENCY EXIT LIGHT INOP AT 19. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,409 hrs · 62,494 cycles

EMERGENCY EXIT BULLNOSE LIGHT INOP. REMOVED AND REPLACED BATTERY PACK ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,227 hrs · 62,346 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 922, STR 23R. REPAIRED SKIN PER EA.

Part: SIGN — BROKEN (CABIN) · airframe 70,227 hrs · 62,346 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND RT OVERWING LOWER EMERGENCY EXIT SIDEWALL SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 68,532 hrs · 61,043 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT O/B TRAILING EDGE WEDGE CORNER DELAMINATED. REMOVED AND REPLACED NR 5 SLAT PER MM.

Part: HOOK — LOOSE (EVAC SLIDE) · airframe 68,532 hrs · 61,043 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE CONTAINER HOOK LOOSE. SECURED HOOK PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 68,532 hrs · 61,043 cycles

DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,442 hrs · 60,970 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 759 TO BS 761, STR 19L. REPAIRED SKIN PER ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,442 hrs · 60,970 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 976, STR 24L. REPAIRED STRINGER SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,442 hrs · 60,970 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 971, STR 24L. REPAIRED SKIN PER ER.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 68,449 hrs · 60,977 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,387 hrs · 60,924 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 516D, STR 15R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,387 hrs · 60,924 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 515D, STR 16R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,387 hrs · 60,924 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 515D, STR 15R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,387 hrs · 60,924 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 930, STR 21L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,894 hrs · 60,556 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B, STR 14L. REPAIRED SKIN PER SEW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,844 hrs · 60,518 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,294 hrs · 60,101 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT GALLEY LOWER EMERGENCY EXIT SIGN LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 67,179 hrs · 60,015 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER SKIN CRACKED AT STA 157.10. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 67,179 hrs · 60,015 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER SKIN CRACKED AT STA 92.70. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 67,179 hrs · 60,015 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,128 hrs · 59,975 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 520, STR 15L. REPAIRED SKIN PER ER.

Part: ESCAPE ROPE — OUT OF POSITION (EMERGENCY EXIT) · airframe 65,810 hrs · 59,037 cycles

RT EMERGENCY EXIT ESCAPE ROPE OUT OF DOOR. REPACKED ROPE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 65,528 hrs · 58,841 cycles

DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXT BULLNOSE LIGHT LENS LOOSE AT ROW 5. SECURED LIGHT PER MM.

Part: LENS — LOOSE (CABIN) · airframe 65,528 hrs · 58,841 cycles

DURING SCHEDULED RON CHECK, EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 5. SECURED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 17R. REPAIRED FRAME PER ER.

Part: LIGHT — DAMAGED (CABIN) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND EMERGENCY EXIT LIGHT DAMAGED AT AFT LAV. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER FLANGE CORRODED AT BS 360, BETWEEN LBL 21 TO RBL 21. REPAIRED BEAM PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 751, STR 18R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 258, WL 187. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 304, WL 259. REPAIRED SKIN PER ER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT CREASE BEAM WEB CORRODED AT BETWEEN BS 420 TO BS 440. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986 BETWEEN RBL 18 TO RBL 42, WL 208. REPAIRED BEAM PER ER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,517 hrs · 58,829 cycles

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

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 500D TO BS 540. REPAIRED BEAM PER ER.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT KEEL BEAM CORRODED BETWEEN BS 520 TO BS 525. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BETWEEN RBL 18 TO RBL 42, WL 208. REPAIRED BEAM PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 292, BETWEEN WL 232 TO WL 233. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN BUTT SPLICE CRACKED AT BS 258, WL 180 LT SIDE. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN BUTT SPLICE CRACKED AT BS 258, WL 173 LT SIDE. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN BUTT SPLICE CRACKED AT BS 258, WL 175 LT SIDE. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN BUTT SPLICE CRACKED AT BS 258, WL 186 LT SIDE. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN BUTT SPLICE CRACKED AT BS 258, WL 184 LT SIDE. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN BUTT SPLICE CRACKED AT BS 258, WL 179 LT SIDE. REPAIRED SKIN PER ER.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 360 TO BS 380, STR 17R. REMOVED AND REPLACED WEB PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 2 SLAT WEDGE I/B END DELAMINATED. REPAIRED SLAT PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 616 TO BS 639. REPAIRED WEB PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727, RBL 45. REPAIRED BEAM PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER FLANGE CRACKED AT BS 328, RBL 28. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 616 TO BS 639. REPAIRED WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND ZEE CHORD UPPER FLANGE CORRODED AT BS 270 BETWEEN LBL 7 TO RBL 7. REPAIRED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 305, STR 21R. REPAIRED SKIN PER SRM.

Part: BRACKET — CORRODED · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND ESCAPE SLIDE FLOOR BRACKET CORRODED AT BS 344, LBL 58, WL 208. REMOVED AND REPLACED BRACKET PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — PUNCTURED (MIDFLAP) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING INBD MID-FLAP T/E WEDGE SKIN PUNCTURED. REPAIRED MID FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 12L. R&R CLIP PER SRM.

Part: WEDGE — DEBONDED (MIDFLAP) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING INBD MID FLAP T/E WEDGE DISBONDED. REPAIRED WEDGE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 727, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 867 S8L) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500C S8R) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,517 hrs · 58,829 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,898 hrs · 58,386 cycles

DURING SCHEDULED C2 CHECK, FOUND SKIN CRACKED AT BS 792, STR 19L. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,427 hrs · 58,011 cycles

DURING SCHEDULED A2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 64,390 hrs · 57,978 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,917 hrs · 51,630 cycles

DURING SCHEDULED C1 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,917 hrs · 51,630 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506D, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,873 hrs · 57,598 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 19L. REPAIRED SKIN PER SRM.

Part: GASPER FAN — FAULTY (E&E BAY) · airframe 63,296 hrs · 57,154 cycles

CREW REPORTS ELECTRICAL SMELL IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,897 hrs · 56,878 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, LBL 2. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,897 hrs · 56,878 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,897 hrs · 56,878 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, RBL 3. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,857 hrs · 56,849 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730D, STR 19L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 62,498 hrs · 56,573 cycles

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

Part: HOOK — LOOSE (R2 DOOR) · airframe 62,255 hrs · 56,394 cycles

R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 62,181 hrs · 56,341 cycles

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

Part: STRINGER — CRACKED (BS 809 S17L) · airframe 61,768 hrs · 56,020 cycles

DURING SCHEDULED SERVICE CHECK, FOUND STRINGER 17L CRACKED AT BS 809. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (BS 933 S23R) · airframe 59,158 hrs · 53,999 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 933, STR 23R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 59,158 hrs · 53,999 cycles

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

Part: FUSE — FAULTY (NLG W/W) · airframe 59,134 hrs · 53,977 cycles

AIR TURNBACK, AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT. RED UNSAFE LIGHT ILLUMINATED, CYCLED GEAR, NO HELP. REMOVED AND REPLACED NLG HYDRAULIC FUSE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,749 hrs · 53,664 cycles

DURING SCHEDULED A1 CHECK, FOUND RT OVERWING DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LENS — MISSING (CABIN) · airframe 58,198 hrs · 53,227 cycles

DURING SCHEDULED C3 CHECK, FOUND OVERHEAD EMERGENCY EXIT SIGN LENS MISSING AT ROW 22. INSTALLED EXIT SIGN LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,308 hrs · 52,524 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 25R. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,189 hrs · 52,430 cycles

DURING SCHEDULED 1/4D CHECK, FOUND MID EMERGENCY EXIT LIGHT INOP AT BS 431, BL 0, WL 289. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK PER MM.

Part: FRAME — CRACKED (BS 303) · airframe 57,188 hrs · 52,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FRAME CUTOUT CRACKED AT FWD LOWER STOP FITTING BS 303, STR 16L. REPAIRED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (BS 378) · airframe 57,188 hrs · 52,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 378, RBL 1.5 TO RBL 3.5. REPAIRED SKIN PER SWA EA.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 57,188 hrs · 52,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 4 DEF. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,188 hrs · 52,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AFT OF RADIO ALTIMETER ANTENNA, BS 395, BL O. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (BS 294) · airframe 57,188 hrs · 52,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE LOWER FRAME ANGLE CRACKED AT BS 294, STR 10L. REMOVED AND REPLACED FRAME ANGLE PER SRM.

Part: ANGLE — CRACKED (BS 301 STRINGER) · airframe 57,188 hrs · 52,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER ANGLE CRACKED AT BS 301, STR 6L. REMOVED AND REPLACED STRINGER ANGLE PER SRM.

Part: BULKHEAD — CRACKED (BS 295) · airframe 57,188 hrs · 51,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 295, STR 16L. REPAIRED WEB SECTION PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 57,188 hrs · 52,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 15 DEF. SECURED BULLNOSE LIGHT PER MM.

Part: FRAME — CRACKED (BS 294) · airframe 57,188 hrs · 52,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE UPPER FRAME ANGLE CRACKED AT BS 294, STR 10L. REMOVED AND REPLACED FRAME ANGLE PER SRM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 57,188 hrs · 52,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR SKIN CRACKED AT LOWER HINGE CUTOUT UPPER CORNER. REMOVED AND REPLACED R1 DOOR PER MM.

Part: STRINGER CLIP — CRACKED (BS 500D) · airframe 57,188 hrs · 52,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 24R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500C) · airframe 57,188 hrs · 52,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 744 S19L) · airframe 57,188 hrs · 52,429 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 744, STR 19L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 56,396 hrs · 51,811 cycles

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

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 56,315 hrs · 51,740 cycles

LT WING NR 3 L/E SLAT UPPER SKIN, OUTBD AFT EDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 56,315 hrs · 51,740 cycles

LT WING NR 3 L/E SLAT UPPER SKIN, OUTBOARD AFT EDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — CRACKED (BS 929-931) · airframe 52,528 hrs · 48,743 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 929.75 TO BS 931.50, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 780) · airframe 52,528 hrs · 48,743 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780.50, BETWEEN STR 18L TO STR 19L. REPAIRED SKIN IAW EA AND SRM.

Part: SKIN — CRACKED (BS 739D) · airframe 55,409 hrs · 51,041 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739D, STR 19L. REPAIRED SKIN PER SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,857 hrs · 50,596 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT EXTERIOR FUSELAGE LIGHTS INOP. RELAMPED LIGHTS PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 52,543 hrs · 48,758 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,528 hrs · 48,743 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 950, ABOVE STRINGER 19R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,379 hrs · 48,631 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 978, STRINGER 21L, CRACKED. REPAIRED SKIN SECTION PER EA.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 52,123 hrs · 48,466 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SHAFT — INOPERATIVE (NR 1 ENGINE) · airframe 51,853 hrs · 48,232 cycles

AIR TURNBACK, UNABLE TO STAY BELOW MAX CONTINUOUS EGT DURING CLIMBOUT TO FL 26, NR 1 EGT WAS 900 DEGREES TO 910 DEGREES AT CLIMB N1. REMOVED AND REPLACED NR 1 ENGINE VBV MOTOR SHAFT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,739 hrs · 48,141 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 18L, CRACKED. REPAIRED SKIN PER EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,558 hrs · 47,998 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR CUTOUT UPPER AFT RADIUS CRACKED. REPAIRED DOOR SKIN CUTOUT PER SRM.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 50,647 hrs · 47,256 cycles

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

Part: SLIDE — LOOSE (R2 DOOR) · airframe 50,588 hrs · 47,213 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE LOOSE. SECURED R2 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,588 hrs · 47,213 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 790, STRINGER 17L, CRACKED. REPAIRED SKIN PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,801 hrs · 45,793 cycles

DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 48,791 hrs · 45,782 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT NR 2 PAX WINDOW FRAME CRACKED. REMOVED AND REPLACED RT NR 2 PAX WINDOW FRAME PER SRM AND ERO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,791 hrs · 45,782 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: RIB — CRACKED (LT WING) · airframe 48,791 hrs · 45,782 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT WING RIB LOWER CHORD CRACKED AT WBL 135.5 BETWEEN STRINGERS 2 AND 3. REPAIRED RIB PER SRM AND T1-257-008.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,791 hrs · 45,782 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, ABOVE STR 14L. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 48,791 hrs · 45,782 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 360 STRINGER SPLICE CRACKED AT STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,791 hrs · 45,782 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 987, RBL 45. REPAIRED FLOORBEAM PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 48,791 hrs · 45,782 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 BULKHEAD CRACKED AT STR 7L. REPAIRED BULKHEAD WEB PER SRM AND ERO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,791 hrs · 45,782 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 48,791 hrs · 45,782 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM CORRODED AT BS 947 TO BS 967 RT SIDE. REPAIRED CREASE BEAM PER SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 48,791 hrs · 45,782 cycles

DURING SCHEDULED 1/2D CHECK, FOUND NR 1 AND NR 2 LT SIDE PAX WINDOW FRAMES CRACKED AT FASTENER HOLE. REMOVED AND REPLACED WINDOW FRAMES PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 48,791 hrs · 45,782 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 540 FUSELAGE STRINGER SPLICE CRACKED AT 10R. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 48,791 hrs · 45,782 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT CREASE BEAM CORRODED AT BS 947 AND BS 967. REPAIRED CREASE BEAM SECTION PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 48,791 hrs · 45,782 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 540, STR 10L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,791 hrs · 45,782 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 291.5, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 48,791 hrs · 45,782 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 3 EA STRINGER CLIPS CRACKED AT BS 737, STR 19R, BS 727B, STR 21R, AND BS 727A, STR 21R. REMOVED AND REPLACED CLIPS PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 48,791 hrs · 45,782 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TO FRAME ANGLE CRACKED AT BS 294.5 STR 23L. REPAIRED PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,791 hrs · 45,782 cycles

DURING SCHEDULED C2 CHECK, FOUND SKIN CRACKED AT AFT EDGE OF COOLING FAN EXHAUST. REPAIRED PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,791 hrs · 45,782 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,791 hrs · 45,782 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 13R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,791 hrs · 45,782 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 348.5, STR 6L. REPAIRED FRAME PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 48,039 hrs · 45,162 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 207, RBL 14 AND WL 203, RBL7. REPAIRED BULKHEAD WEB PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 48,004 hrs · 45,132 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,004 hrs · 45,132 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT 2 EA BULBS INOP. RELAMPED EXIT LIGHT PER MM.

Part: SLIDE — LOOSE (SERVICE DOOR) · airframe 47,629 hrs · 44,829 cycles

FWD SERVICE DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: TRIM TAB — CRACKED (RT ELEVATOR) · airframe 46,352 hrs · 43,842 cycles

DURING SCHEDULED A1 CHECK, SWA SI 11139-55, RT ELEVATOR TAB CRACKED AT NR 3 HINGE CUTOUT. REMOVED AND REPLACED RT ELEVATOR TAB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,028 hrs · 43,574 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER FWD CORNER OF AFT ENTRY DOOR. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 46,028 hrs · 43,574 cycles

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

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 45,268 hrs · 42,967 cycles

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

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 45,173 hrs · 42,880 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 44,271 hrs · 42,144 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 4 L/E SLAT T/E WEDGE DELAMINATED ON INBD EDGE. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.

Part: FAN — OVERTEMP (A/C DIST. BAY) · airframe 43,790 hrs · 41,746 cycles

FLIGHT ATTENDANTS REPORTED BURNING ODOR IN CABIN, SMELL ALSO NOTED IN COCKPIT. REMOVED AND REPLACED AIR CONDITIONING RECIRCULATION FAN PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 43,381 hrs · 41,415 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,381 hrs · 41,415 cycles

DURING SCHEDULED C3 CHECK, FOUND KEEL BEAM LOWER SKIN CRACKED 1.25 INCHES BETWEEN MLG W/W. REPAIRED SKIN PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 42,458 hrs · 40,642 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY LIGHT LENS CRACKED. R&R LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,458 hrs · 40,642 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED .562 INCH AT AFT SVC DOOR LOWER HINGE CUT OUT. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 42,370 hrs · 40,563 cycles

FWD OVERHEAD AISLE EXIT LENS COVER FELL OFF. REINSTALLED LENS COVER PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,487 hrs · 39,793 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK INOP. REMOVED AND REPLACED OVERWING BATTERY PACK.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 41,509 hrs · 39,811 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD CRACKED AT BS 178, RBL 0.5 & WL 207. REPAIRED BULKHEAD PER SRM.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 41,487 hrs · 39,793 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY LIGHT BATTERY PACK AT LT OVERWING NOT CHARGING. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,912 hrs · 38,449 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER MM.

Part: TEE CHORD — CRACKED (FUSELAGE) · airframe 39,707 hrs · 38,266 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD T-CHORD CRACKED, LBL 5.7, WL 184. REPAIRED CHORD PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 39,707 hrs · 38,266 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 663 VERTICAL STIFFNER CRACKED AT RBL 3. R&R STIFFNER PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,707 hrs · 38,266 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BOTH AFT GALLEY EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 39,707 hrs · 38,266 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS INOP AFT OF ROW 19. R&R BATTERY CHARGER PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 38,545 hrs · 37,287 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT FWD SECTION. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 37,992 hrs · 36,813 cycles

DURING SCHEDULED A2 CHECK, FOUND FWD AISLE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 37,816 hrs · 36,649 cycles

DURING SCHEDULED C1 CHECK, FOUND 2 INCH LONG CRACK AT NOSE WHEEL WELL UPPER WEB PANEL WHERE LT BRAKE SNUBBER ATTACHES. REPAIRED WEB PER SWA RA NR 1-353-2287.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 37,808 hrs · 36,638 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CSD — LACK OF LUBE (NR 1 ENGINE)

AIR TURNBACK, NR 1 ENG CSD LOW OIL PRESSURE LIGHT ILLUMINATED. DEFERRED PER MEL.

Part: MODULE — MALFUNCTIONED (E/E BAY)

AIR TURNBACK, DURING TAKEOFF, NR 4 L/E FLAP TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED FLAP/SLAT MODULE PER MM.

Part: SWITCH — OUT FO ADJUST (LE FLAP)

AIR TURNBACK, RT WING L/E FLAP INDICATED PARTIALLY EXTENDED AFTER FLAP RETRACTION. QRH PROCEDURED C/W WITH NO CHANGE. ADJUSTED RT L/E FLAP TARGET RETRACT SWITCH PER MM. OPS CHECK GOOD.

Part: KEEL BEAM — CRACKED (BS 714)

DURING SCHEDULED BC1 CHECK, FOUND KEEL BEAM PANEL CRACKED APPROX 1 INCH LONG AT LT SIDE OF BS 714. REPAIRED PER SRM.

Part: CONTROLLER — MALFUNCTIONED (COCKPIT)

WHILE CRUISING AT FL 330 CABIN ALT ROSE ABOVE 10,000 FT, HORN SOUNDED. DESCENDED TO FL 200 AND WENT TO PACKS ON HIGH, CABIN CAME BACK UNDER CONTROL. REMOVED AND REPLACED PRESSURIZATION CONTROLLER AND CONTROL PANEL OPS CHECKS GOOD PER M/M.

Part: CONTROL CABLE — OUT OF ADJ (LANDING GEAR)

AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT TO UP POSITION, APPEARED TO BE SOLENOID. AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING. ADJUSTED GROUND SHIFT CABLE PER M/M, OPS CK GOOD.

Part: SKIN — DENTED (CARGO DOOR)

DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR DENTED 5 INCHES FROM AFT EDGE, 12 INCHES FROM TOP. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: SKIN — DENTED (CARGO DOOR)

DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR DENTED CENTER OF DOOR 11 INCHES FROM TOP. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: FRAME — DENTED (BS 807)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 807 AT LBL 31, WL 161. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: FRAME — DENTED (BS 767)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 767 AT RBL 27, WL 157. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: FRAME — CRACKED (BS 907)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907 AT LBL 2 FROM S1. REPAIRED PER TRAMCO EWO 98-1050.

Part: SKIN — DENTED (CARGO DOOR)

DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR DENTED 1 INCH FROM AFT EDGE, 12 INCHES FROM TOP. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: SKIN — DENTED (R2 DOORWAY)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AFT OF R2 DOOR BELOW EMERG LIGHT. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: SKIN — DENTED (BS 912)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 912, BELOW S16L. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: FRAME — CRACKED (BS 440, 480, 747)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 440, 480, 747 AND 827. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 360)

DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT BS 360, ABOVE S15R. REPAIRED PER BOEING SRM.

Part: CHANNEL — CRACKED (BS 359)

DURING SCHEDULED D-CHECK, FOUND STRINGER CHANNEL CRACKED AT BS 359, S14L. REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 380)

DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT BS 380, ABOVE S16R. REPAIRED PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 360)

DURING SCHEDULED D-CHECK, FOUND FUSE FRAME SHEAR TIES CRACKED AT BS 360, BETWEEN S13 AND 15L. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 500)

DURING SCHEDULED D-CHECK, FOUND STRINGER 16L CRACKED AT BS 500B+2.5. REPLACED DAMAGED SECTION PER BOEING SRM.

Part: WEB — CORRODED (BS 616)

DURING SCHEDULED D CHECK, FOUND LOWER SIDE OF CREASE BEAM WEB CORRODED AT BS 616, LBL 67. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (SERVICE DOOR)

DURING SCHEDULED D CHECK, FOUND FWD SERVICE DOORWAY UPPER FWD FRAME CRACKED AT BS 296, RBL 48, WL 269. REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 1006)

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1006, S20R. REPAIRED PER BOEING SRM.

Part: CHORD — CRACKED (BS 616)

DURING SCHEDULED D CHECK, FOUND I/B CHORD CRACKED AT BS 616, LBL 64.5. REPAIRED PER BOEING SRM.

Part: BULKHEAD CHORD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND SIDE CHORDS CRACKED IN RADIUS OF CHORD AT BS 178, LBL 29 AND RBL 29, WL 207. REPLACED PER BOEING SRM.

Part: SKIN — CREASED (BS 266)

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CREASED AT BS 266, AT S4 TO 6L. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5, LBL 25, 40, 43, WL 208. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORROSION AT BS 328, RBL 14, WL 208. REPAIRED PER BOEING SRM.

Part: BEAM — CORRODED (BS 500-516)

DURING SCHEDULED D CHECK, FOUND FLOOR SUPPORT BEAM CORRODED AT BS 500C+16. REPLACED DAMAGED SECTION PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD CRACK AT WL 197-201, LBL 4.7, WL 210-212, LBL 6.7, WL 200-201, RBL 4.7. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (APU DOOR)

DURING SCHEDULED D CHECK, FOUND APU DOOR SKIN DENTED 2 PLACES. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: RIB — CRACKED (LT HORIZ STAB)

DURING SCHEDULED D-CHECK, FOUND LT HORIZONTAL STAB LEADING EDGE PANEL RIB CRACKED AT L/E BS 164.04. REMOVED AND REPLACED RIB PER BOEING SRM.

Part: RIB — CRACKED (LT HORIZ STAB)

DURING SCHEDULED D-CHECK, FOUND LT HORIZONTAL STAB LEADING EDGE PANEL RIB CRACKED AT L/E BS 170.34. REMOVED AND REPLACED RIB PER BOEING SRM.

Part: ANGLE — DAMAGED (BS 640)

DURING SCHEDULED D-CHECK, FOUND ANGLE, UPPER FASTENER HOLE IS ELONGATED AT BS 640, LBL 39, WL 166. REMOVED AND REPLACED DAMAGED AREA AND REPAIR ANGLE PER BOEING SRM.

Part: TIE STRAP — CORRODED (BS 727)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR PANEL TIE STRAP AT BS 727, RBL 21, LBL 21, WL 159. REMOVED AND REPLACED TIE STRAP PER BOEING SRM.

Part: TIE STRAP — CORRODED (BS 727)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR PANEL TIE STRAP AT BS 727+5, RBL 21, LBL 21, WL 156. REMOVED AND REPLACED TIE STRAP PER BOEING SRM.

Part: BRACKET — CRACKED (BS 727)

DURING SCHEDULED D-CHECK, FOUND APU SHROUD SUPPORT BRACKET IS CRACKED AT BS 727+2, BL 0, WL 163. REPAIRED APU SUPPORT BRACKET PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C4 CHECK, FOUND AFT GALLEY DOOR HINGE CUTOUT CRACKED .25 AT UPPER CORNER. REPAIRED PER BOEING SRM.

Part: ACM — OVERSERVICED (AC BAY)

DURING CLIMBOUT, EXPERIENCED AN OIL TYPE SMELL IN IN COCKPIT. SMELL DISSAPATED AT CRUISE. FLIGHT CONTINUED AND LANDED NORMALLY. INSPECTED AND FOUND BOTH AIR CYCLE MACHINES OVERSERVICED. DRAINED OIL TO PROPER LEVEL, REPLACED BOTH COALESCER FILTERS, AND RAN ENGINES OK PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SECTION OF FLOOR TRACK LIGHTING OPERATES INTERMITTENTLY. REPLACED BATTERY AND CHARGER PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND FORWARD CABIN EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REPLACED BATTERY PACK AND CHARGER PER BOEING M/M.

Part: SKIN — DENTED (BS 847)

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN DENTED 6 INCHES AFT OF AFT CARGO DOOR AT BS 847, AT S19R. REPAIRED PER BOEING SRM.