N351SW

Part: LENS — MISSING (CABIN) · airframe 71,887 hrs · 62,759 cycles

RT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,371 hrs · 62,371 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EXTERNAL OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,371 hrs · 62,371 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,074 hrs · 62,132 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 420+4, STR 16R. REPAIRED SKIN PER SRM.

Part: LINK ASSY — CRACKED (NLG) · airframe 70,855 hrs · 61,962 cycles

AIR TURNBACK - NOSE GEAR DID NOT RETRACT ON TAKEOFF, HAD RED/GREEN LIGHTS ON NOSE GREEN WITH HANDLE UP, ALL GREEN ON GEAR LOWERING. FOUND NOSE GEAR LOCK LINK ASSY AFT ATTACH SUPPORT CRACKED. REMOVED AND REPLACED LOCK LINK ASSY AND NOSE GEAR LOCK ACUTATOR PER MM.

Part: WEB — CRACKED (NLG WW) · airframe 70,555 hrs · 61,727 cycles

DURING SCHEDULED MV1 CHECK FOUND, NOSE LANDING GEAR WHEEL WELL CRACKED AT BS 259, WL 174. REPAIRED SKIN WEB PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,096 hrs · 61,382 cycles

DURING SCHEDULED SPV CHECK, FOUND CRACK FASTENER HOLE, UPPER DOOR HINGE CUTOUT. REPAIRED PER DOC.

Part: STRUCTURE — CRACKED (BS 616) · airframe 70,096 hrs · 61,382 cycles

DURING SCHEDULED SPV CHECK, FOUND PASSENGER CABIN FLOOR AREA CRACKED, BS 616, WL 200, RBL 65 INNER CHORD. REPAIRED PER DOC.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 70,097 hrs · 61,382 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: WINDOW — ARCED (COCKPIT) · airframe 69,979 hrs · 61,298 cycles

R2 COCKPIT WINDOW SPARKED AND ARCED INFLIGHT. REMOVED AND REPLACED NR 2 WINDOW AND CONTROLLER PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,480 hrs · 60,930 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FRAME CRACKED AT BS 380, 5, STR 19R. REPAIRED FRAME PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING O/B FORE FLAP I/B TRAILING EDGE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, BETWEEN RBL 6 TO RBL 15. REPAIRED BEAM PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 929, STR 24L. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND PRESSURE DECK DOME CRACKED AT BS 1016, STR 15L. REPAIRED DOME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 324, RBL 21. REPAIRED BEAM PER SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND SUPPORT ANGLE CORRODED BETWEEN BS 298 TO BS 330, RBL 58. REPAIRED ANGLE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BETWEEN RBL 18 TO RBL 47. REPAIRED BEAM PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 480, BL 0. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED BETWEEN BS 986 TO BS 1006, BETWEEN LBL 17 TO LBL 7. REPAIRED BEAM PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 6L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 5R. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BL 0. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND PRESSURE DOME CRACKED AT BS 1016, STR 15R. REPAIRED DOME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5R. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 69,341 hrs · 60,823 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 380, STR 5L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 907, STR 5L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING NR 3 SLAT SKIN LOWER SURFACED CRACKED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BBL 0. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 26R TO STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 942, STR 22L. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 1040, BETWEEN STR 23L TO STR 24L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED BETWEEN BS 750 TO BS 751, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,341 hrs · 60,823 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED BETWEEN BS 800 TO BS 802, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,608 hrs · 60,256 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 517D, STR 16L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 68,608 hrs · 60,256 cycles

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

Part: LOCK — MALFUNCTIONED (COCKPIT) · airframe 68,218 hrs · 59,936 cycles

DIVERSION - COCKPIT LOCK FAIL LIGHT SMOKED AT ALTITUDE. REMOVED AND REPLACED LOCK ASSY PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 67,748 hrs · 59,571 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,748 hrs · 59,571 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER CUTOUT. REPAIRED SKIN PER SRM.

Part: ATTACH FITTING — DAMAGED (R1 DOOR) · airframe 67,748 hrs · 59,571 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR AFT SLIDE ATTACH PLATE DAMAGED. REMOVED AND REPLACED PLATE PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 67,748 hrs · 59,571 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 67,748 hrs · 59,571 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 4 L/E SLAT I/B AFT CORNER DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 67,596 hrs · 59,455 cycles

FWD RT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — UNSERVICEABLE (L2 DOOR) · airframe 67,578 hrs · 59,440 cycles

L2 DOOR EMERGENCY EVAC SLIDE UNABLE TO READ PRESSURE INDICATOR. REMOVED AND REPLACED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 67,537 hrs · 59,408 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 67,321 hrs · 61,421 cycles

L2 DOOR EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 67,278 hrs · 59,219 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,278 hrs · 59,219 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 516C, STR 19R. REPAIRED SKIN PER SRM AND EA.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 67,214 hrs · 59,164 cycles

DECLARED EMERGENCY / DIVERSION. AFTER T/O RT MLG UNSAFE RED LIGHT IND. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 67,061 hrs · 59,048 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 66,719 hrs · 58,790 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: PANEL — FAULTY (COCKPIT) · airframe 66,570 hrs · 58,682 cycles

DURING CRUISE FLIGHT AT FL360 RIGHT PACK TRIPPED DURING CHECKLIST FOR THE PACK TRIP OFF, THE LEFT PACK TRIP LIGHT ILLUMINATED, THE CABIN CLIMBED RAPIDLY; DURING THE EMERGENCY DESCENT, BOTH PACKS RESET; MAINTAINED PRESSURIZATION AT 12,000 FT FOR ABOUT 25 MINUTES DID NOT DROP THE MASK IN THE CABIN. REMOVED AND REPLACED P5-10 PANEL PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 65,489 hrs · 57,864 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 65,231 hrs · 57,673 cycles

EELS LOOSE AT EXIT. SECURED EEPLS PER MM.

Part: HINGE FITTING — CRACKED (R1 DOOR) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR UPPER HINGE CUTOUT CASTING CRACKED. REMOVED AND REPLACED HINGE CASTING PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 816, STR 25R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 291.5, WL 258 RT SIDE. REPAIRED FRAME PER SWA EA.

Part: STRIP — DAMAGED (CABIN) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 22Y CHECK, FOUND MID TO AFT CABIN EEPLS STRIP DAMAGED. REMOVED AND REPLACED EEPLS PER MM.

Part: DOOR FRAME — CRACKED (AFT CARGO DOOR) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR LOWER FWD FRAME CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND RADIO ALTIMETER BELLY SKIN CUTOUT CRACKED AT BS 390, LBL 4. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME WEB CRACKED AT BS 303, STR 16L. REPAIRED WEB PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 302.2, BETWEEN WL 262 TO WL 258. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BETWEEN BS 304.55 TO BS 303, BETWEEN WL 238.3 TO WL 235. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 663, BL 0. REPAIRED BEAM PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 597, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS BS 867, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 667 AT LOWER CHORD. REPAIRED BEAM PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 727B, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BETWEEN BS 290 TO BS 293, BETWEEN WL 229.50 TO WL 259. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 727C, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT, BETWEEN BS 296.5 TO BS 307.5, BETWEEN WL 278 TO WL 285. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 727A, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 727E, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND RADIO ALTIMETER FUSELAGE BELLY SKIN CUTOUT CRACKED BETWEEN BS 394 TO BS 454, BETWEEN RBL TO LBL 4. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 767, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 807, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 907, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 14L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 14L. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM I/B UPPER CHORD CRACKED AT BS 727A+17, LBL 45. REPAIRED CHORD PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,493 hrs · 57,148 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 727E, STR 19R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 64,411 hrs · 57,089 cycles

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

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 63,903 hrs · 56,719 cycles

L2 DOOR EMERGENCY EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 62,854 hrs · 56,002 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,574 hrs · 55,792 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. R&R LIGHT BULB PER MM.

Part: LENS — LOOSE (CABIN) · airframe 62,070 hrs · 55,429 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 62,070 hrs · 55,429 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 61,570 hrs · 55,058 cycles

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

Part: SIGN — LOOSE (CABIN) · airframe 61,499 hrs · 55,009 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 61,313 hrs · 54,879 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 61,274 hrs · 54,846 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: HINGE — WORN (LT SPOILER) · airframe 61,274 hrs · 54,846 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 4 SPOILER INBOARD HINGE WORN. REMOVED AND REPLACED SPOILER PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 61,274 hrs · 54,846 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: LENS — LOOSE (CABIN) · airframe 61,217 hrs · 54,803 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,911 hrs · 54,565 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 462 AND BS 466, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,346 hrs · 65,551 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 263.5, STR 9L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 60,357 hrs · 54,155 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,357 hrs · 54,155 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505D, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 59,928 hrs · 53,824 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 59,766 hrs · 53,672 cycles

FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 57,568 hrs · 53,534 cycles

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

Part: GLOWSTRIP — WORN (CABIN) · airframe 59,492 hrs · 53,478 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 3 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHTS) · airframe 59,492 hrs · 53,478 cycles

DURING SCHEDULED HC1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 2 ABC. SECURED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 59,482 hrs · 53,472 cycles

DURING SCHEDULED HC1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 2 ABC. SECURED LENS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,367 hrs · 52,627 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — LOOSE (CABIN) · airframe 58,317 hrs · 52,582 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 58,317 hrs · 52,582 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (BS 310 S18R) · airframe 57,735 hrs · 52,153 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 310, STR 18R. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,735 hrs · 52,153 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED BRDG CHECK, FOUND STR FUSELAGE FRAME CRACKED AT BS 380, STR 15R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 907 S8L) · airframe 57,731 hrs · 52,149 cycles

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

Part: FRAME — CRACKED (BS 400 S8L) · airframe 57,731 hrs · 52,149 cycles

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

Part: STRINGER CLIP — CRACKED (BS 400 S8L) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED BRDG CHECK, FOUND STR CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FRAME — CRACKED (BS 727D S8L) · airframe 57,731 hrs · 52,149 cycles

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

Part: FRAME — CRACKED (BS 787 S8L) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787 STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 440 S8R) · airframe 57,731 hrs · 52,149 cycles

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

Part: FRAME — CRACKED (BS 706 S8L) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706 STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 747 S8L) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747 STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 867 S8R) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 827 S8R) · airframe 57,731 hrs · 52,149 cycles

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

Part: FRAME — CRACKED (BS 727B S8R) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 520 S8L) · airframe 57,731 hrs · 52,149 cycles

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

Part: FRAME — CRACKED (BS 827 S8R) · airframe 57,731 hrs · 52,149 cycles

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

Part: FRAME — CRACKED (BS 500C S8L) · airframe 57,731 hrs · 52,149 cycles

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

Part: FRAME — CRACKED (BS 727D S8R) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 727B S8L) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 520 S8R) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500A S8L) · airframe 57,731 hrs · 52,149 cycles

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

Part: FRAME — CRACKED (BS 480 S8L) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 787 S8R) · airframe 57,731 hrs · 52,149 cycles

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

Part: FRAME — CRACKED (BS 500A S8R) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 480 S8R) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 380 S9R) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 380 S15R) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 500C S8R) · airframe 57,731 hrs · 52,149 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER 4L CRACKED AT BS 1010. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER 8L CRACKED AT BS 1010. REMOVED AND REPLACED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,791 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, LBL 14. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,791 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 10L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,791 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,791 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,791 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,791 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 1 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 17L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING NR 5 L/E SLAT SKIN CRACKED INBOARD OF ACTUATOR. REPAIRED SLAT SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,791 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 665, RBL 38. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,791 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,791 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 336, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CRACKED AT BS 665, LBL 24. REPAIRED FLOORBEAM PER SWA EA.

Part: KEELBEAM — CORRODED (BS 520) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED BRDG CHECK, FOUND KEEL BEAM CHORD CORRODED AT BS 520, LBL 6.5. REPAIRED KEEL BEAM CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT WING NR 6 L/E SLAT SKIN LOWER SURFACE CRACKED. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (BS 731D S19L) · airframe 57,731 hrs · 52,149 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 731D, STR 19L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 56,999 hrs · 51,558 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,843 hrs · 51,436 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 8 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 56,680 hrs · 51,314 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,394 hrs · 51,101 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 24R. REPAIRED SKIN PER SWA EA.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 56,278 hrs · 51,011 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. SECURED LIGHT LENS PER MM.

Part: SKIN — CRACKED (BS 757) · airframe 56,059 hrs · 50,838 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,050 hrs · 50,833 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 56,050 hrs · 50,833 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,050 hrs · 50,833 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 24R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (AFT CARGO DOOR) · airframe 55,037 hrs · 50,058 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR FRAME CRACKED AT FWD LOWER STOP FITTING. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,851 hrs · 49,914 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 731D, STR 19R. REPAIRED SKIN PER SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,317 hrs · 49,513 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT SLIDE LIGHT INOP. RELAMPED LIGHT PER MM.

Part: FRAME — CRACKED (BS 440) · airframe 54,314 hrs · 49,512 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME NR 5 STOP FITTING, BS 440, RBL 25. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,314 hrs · 49,512 cycles

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

Part: BULKHEAD — CRACKED (BS 178) · airframe 54,314 hrs · 49,512 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 178 BULKHEAD, RBL 5.7, WL 184. REPAIRED WEB PER BFG ER.

Part: SPLICE — CRACKED (BS 359) · airframe 54,314 hrs · 49,512 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 359, STR 16L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SPLICE — CRACKED (BS 359) · airframe 54,314 hrs · 49,512 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 359, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER — CRACKED (BS 807) · airframe 54,314 hrs · 49,512 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CRACKED AT BS 807, STR 14R. REPAIRED STRINGER PER SRM.

Part: SPLICE — CRACKED (BS 360) · airframe 54,314 hrs · 49,512 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: WEB — CRACKED (COCKPIT FLOOR) · airframe 54,314 hrs · 49,512 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND COCKPIT FLOOR WEB CRACKED BETWEEN BS 188 TO BS 196, RH SIDE, WL 207. REPAIRED FLOOR WEB PER SRM.

Part: STRINGER — CRACKED (BS 380) · airframe 54,314 hrs · 49,512 cycles

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

Part: FRAME — CRACKED (COCKPIT FLOOR) · airframe 54,314 hrs · 49,512 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, RT SIDE, WL 207. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 867) · airframe 54,314 hrs · 49,512 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 867, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 54,075 hrs · 49,329 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 54,075 hrs · 49,329 cycles

DURING SCHEDULED C3 CHECK, FOUND NLG W/W UPPER CEILING WEB CRACKED AT BS 251.625, RBL 7.75 & LBL 7.75. REPAIRED WEB PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 54,075 hrs · 49,329 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: MODULE — BURNED (COCKPIT DOOR) · airframe 54,039 hrs · 49,302 cycles

BURNING ODOR IN CABIN ALONG WITH SEVERAL MASTER CAUTION LIGHTS ILLUMINATED. FOUND LOCK FAIL LIGHT ASSY BURNT ON COCKPIT DOOR LOCK MODULE ASSY. REMOVED AND REPLACED COCKPIT DOOR LOCK MODULE ASSY PER MM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 52,985 hrs · 48,482 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD SECTION EEPLS PHOTO LUMINESCENT STRIP DAMAGED. REMOVED AND REPLACED STRIP PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 52,319 hrs · 47,953 cycles

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

Part: HOOK — LOOSE (L1 DOOR GIRT BAR) · airframe 52,120 hrs · 47,797 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,203 hrs · 47,053 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 935, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,191 hrs · 47,050 cycles

DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN AT BS 935, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM.

Part: FITTING — CORRODED (RT & LT WING) · airframe 50,171 hrs · 46,257 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH RT AND LT FWD OUTBOARD MLG HANGER FITTINGS CORRODED. REMOVED AND REPLACED BOTH RT AND LT HANGER FITTINGS PER EA.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 50,162 hrs · 46,253 cycles

DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BUSHING PER MM.

Part: PIN — SHEARED (RT MLG) · airframe 50,074 hrs · 46,177 cycles

DIVERSION, RT MLG UNSAFE LIGHT ILLUMINATED, AFTER LANDING GEAR RETRACTION ON TAKEOFF. CYCLED GEAR DOWN NORMAL INDICATION, LANDING GEAR TO UP POSITION RT MLG UNSAFE LIGHT ILLUMINATED. REMOVED AND REPLACED RT MLG TRUNNION ANTI ROTATION PIN PER MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 49,701 hrs · 45,865 cycles

DURING SCHEDULED 1/2D CHECK, FOUND COCKPIT L1 WINDOW POST UPPER OUTBOARD CORNER CRACKED. REPAIRED WINDOW POST PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,701 hrs · 45,865 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 3 ABC, INOP. RELAMPED LIGHT PER MM.

Part: RIB — CRACKED (LT WING) · airframe 49,701 hrs · 45,865 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LEFT WING RIB LOWER CHORD CRACKED AT WBL 135.5. REPAIRED RIB PER SWA EA.

Part: SKIN — CRACKED (STABILIZER) · airframe 49,701 hrs · 45,865 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN AT STATION 144, RT STATION 117, AFT SPAR CRACKED. REPAIRED STAB SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 49,701 hrs · 45,865 cycles

DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,701 hrs · 45,865 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727B) · airframe 49,701 hrs · 45,865 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 727B, STRINGER 22L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BRACKET — CRACKED (ESCAPE SLIDE) · airframe 49,701 hrs · 45,865 cycles

DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR EVAC SLIDE FWD UPPER MOUNT BRACKET CRACKED. REMOVED AND REPLACED FWD UPPER BRACKET PER MM.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 49,620 hrs · 45,796 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY AND BATTERY PER MM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 49,218 hrs · 45,468 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT UPPER T/E CORNER DELAMINATED. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,656 hrs · 45,037 cycles

DURING SPV, FOUND AFT CARGO DOOR FRAME CUTOUT AT BS 847, STRINGER 25R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 48,653 hrs · 45,036 cycles

DURING SPV, FOUND STRINGER 25R, AT BS 896, CRACKED. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,345 hrs · 44,799 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT COOLING DUCT CUT OUT. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 47,400 hrs · 44,057 cycles

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

Part: BRACKET — CORRODED (R1 ENTRY) · airframe 47,038 hrs · 43,777 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND R1 DOOR EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,038 hrs · 43,777 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED, WL 199, RBL 6.5. REPAIRED WEB PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 47,038 hrs · 43,777 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED, WL 177, LBL 5.7. REPAIRED WEB PER SRM.

Part: INDICATOR — OUT OF POSITION (SLIDE) · airframe 46,830 hrs · 43,602 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 46,469 hrs · 43,319 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 45,893 hrs · 42,869 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR ASSY OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 45,862 hrs · 42,838 cycles

DURING SCHEDULED RON, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 45,579 hrs · 42,589 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR EMERGENCY EVACUATION SLIDE GIRT BAR AFT HOOK LOOSE. SECURED GIRT BAR HOOK PER MM.

Part: TEE FITTING — CRACKED (CARGO DOOR) · airframe 43,749 hrs · 41,134 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR LOWER LONGITUDINAL T-CHORD CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: CABLE — MISROUTED (AFT ENTRY DOOR) · airframe 43,753 hrs · 41,137 cycles

DURING SCHEDULED CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 43,456 hrs · 40,887 cycles

DURING SCHEDULED RON, FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SLIDE — UNSERVICEABLE (AFT ENTRY DOOR) · airframe 43,362 hrs · 40,804 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 42,568 hrs · 40,149 cycles

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

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 42,151 hrs · 39,805 cycles

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

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 41,507 hrs · 39,262 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EEPLS INOP IN FWD CABIN. RECONNECTED CONNECTORS AT BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,507 hrs · 39,262 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 41,507 hrs · 39,262 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: FRAME — CRACKED (FWD SVC DOOR) · airframe 41,507 hrs · 39,262 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR AFT FRAME CRACKED (2 EA) AT NR 3 STOP FITTING CUTOUT AND LOWER END. REPAIRED FRAME PER SWA T1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,507 hrs · 39,262 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR, UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (LT MLG W/W) · airframe 41,507 hrs · 39,262 cycles

DURING SCHEDULED 1/4D CHECK, FOUND WHEEL WELL CEILING PRESS WEB CRACKED AT BS 665, LBL 31. REPAIRED WEB PER SWA T1.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 41,507 hrs · 39,262 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 770, LBL 7 AND LBL 17. REPAIRED FLOORBEAM PER SWA RA.

Part: COVER — BROKEN (CABIN) · airframe 41,071 hrs · 38,880 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER BROKEN AT ROW NR 4. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: COMBUSTION LINER — DAMAGED (NR 1 ENGINE) · airframe 40,838 hrs · 38,683 cycles

DURING SCHEDULED A2 CHECK, FOUND HOLE BURNED AT PANEL NR 3, AT NR 1 ENG COMBUSTION CHAMBER OUTER LINER, 12 O'CLOCK POS. (SIZE OF HOLE IS APPROX 3 TIMES THE SIZE OF THE NEAREST DILUTION HOLE). REMOVED AND REPLACED NR 1 ENG PER MM.

Part: SOCKET — DEFECTIVE (CABIN) · airframe 40,061 hrs · 38,047 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS LIGHT INOP (1 EA) AT AFT CABIN. REMOVED AND REPLACED LIGHT SOCKET PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,061 hrs · 38,047 cycles

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT LT OVERWING EXIT. RELAMPED LIGHT PER MM.

Part: CAP — MISSING (CABIN) · airframe 40,061 hrs · 38,047 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS END CAP MISSING IN AFT CABIN. INSTALLED END CAP PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 39,837 hrs · 37,853 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178 UPPER CORNER. R&R WEB PER SWA ACO.

Part: WEB — CRACKED (FUSELAGE) · airframe 39,837 hrs · 37,853 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED ( 2 EA ) 1 INCH LONG, AT BS 178, WL 188, BLO. REPAIRED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 39,837 hrs · 37,853 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEBS CRACKED ( 2 EA ) AT BS 178, WL 232, RBL 17.1 & LBL 17.1. R&R WEBS PER SRM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 39,208 hrs · 37,305 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED EMERGENCY EVAC SLIDE GIRT ASSY PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 38,365 hrs · 36,567 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE ASSY OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 38,262 hrs · 36,475 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBD T/E AFT FLAP DELAMINATED AT INBD AFT CORNER. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 38,262 hrs · 36,475 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY AND SVC DOOR EMERGENCY EVAC SLIDE ASSY''S OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY''S PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,853 hrs · 36,151 cycles

DURING WALK-AROUND INSPECTION, FOUND 1.5 INCH EXTERNAL FUSELAGE SKIN CRACK BETWEEN BS 500C & BS 520, STR 10L. REPAIRED SKIN PER SRM.

Part: PANEL — CRACKED (MLG W/W) · airframe 37,295 hrs · 35,663 cycles

DURING SCHEDULED C1 CHECK, FOUND 1.5 CRACK AT LOWER KEEL BEAM STRESS PANEL, BETWEEN MLG W/W CUTOUT, RT AFT SIDE. REPAIRED PANEL PER TI-153-009.

Part: SKIN — CRACKED (L/E SLAT) · airframe 37,295 hrs · 35,663 cycles

DURING SCHEDULED C1 CHECK, FOUND NR 6 L/E SLAT SKIN CRACKED AT TWO LOCATIONS; ONE EXTENDS ACROSS THREE FASTENERS AT OTBD AUX TRACK, THE SECOND EXTENDS ACROSS TWO FASTENERS AT OTBD END OF SLAT. REPAIRED SLAT PER SRM.

Part: TRANSMITTER — INOPERATIVE (RT WING) · airframe 37,193 hrs · 35,569 cycles

DECLARED EMERGENCY. DURING APPROACH, SELECTED FLAPS 5 DEGREES; FLAPS SHOWED SPLIT ON IND; RT = 0 DEGREES, LT = 1 DEGREE, WITH FLAP SELECTOR IN 5 DEGREE POSITION. REMOVED AND REPLACED RT WING FLAP POSITION TRANSMITTER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,392 hrs · 34,871 cycles

DURING SCHEDULED C4 CHECK, FOUND LT EMERGENCY EXIT LOWER LIGHT INOP. RELAMPED PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 36,392 hrs · 34,871 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.

Part: OUTFLOW VALVE — INOPERATIVE (A/C BAY) · airframe 35,732 hrs · 34,306 cycles

AIR TURNBACK. UNABLE TO MAINTAIN CABIN PRESSURE. R&R LH A/C PACK VALVE AND 450 DEG MUSCLE LINE PER MM.

Part: INDICATOR — DISLODGED (ESCAPE SLIDE) · airframe 35,397 hrs · 34,026 cycles

AFT ENTRY AND SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATORS OUT OF VIEW. REPOSITIONED SLIDES PER MM.

Part: INDICATOR — DISLODGED (ESCAPE SLIDE)

DURING SCHEDULED C2 CHECK, FOUND BOTH AFT ENTRY AND SERVICE DOOR EVACUATION SLIDE PRESS INDS OUT OF VIEW. REPOSITIONED BOTH SLIDE ASSY'S PER MM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AROUND AIR CONDITIONING GROUND SERVICE CONNECTION CUT OUT. REPAIRED SKIN PER SRM AND ER NR 99-6051A.

Part: CONNECTOR — BROKEN (SERVICE DOORWAY)

DURING SCHEDULED D CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE EXTERIOR LIGHT CONNECTOR CAP BROKEN. REMOVED AND REPLACED LIGHT HOUSING PER MM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED D CHECK, FOUND BS 328 FLOORBEAM UPPER CHORD CORRODED, RBL 20-RBL 40. REPAIRED BEAM PER SRM.

Part: SHEAR TIES — CRACKED (BS 360)

DURING SCHEDULED D CHECK, FOUND 2 EACH FUSELAGE SHEAR TIES CRACKED, BS 360 BETWEEN STRINGERS 14L-15L AND 14R-15R. REPAIRED SHEAR TIES PER SRM.

Part: FRAME — CRACKED (BS 907)

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 907, LBL 2, WL 303. REPAIRED FRAME PER ER NR 99-6081.

Part: SPLICE — CRACKED (BS 907)

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

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED D CHECK, FOUND BS 986 FLOORBEAM UPPER CHORD CORRODED, LBL 45 - RBL 45. REPAIRED FLOORBEAM PER ER 99-6052.

Part: FRAME — CRACKED (FUSELAGE)

DURING SCHEDULED D CHECK, FOUND 3 EACH FUSELAGE FRAMES CRACKED, BS 827, BS 867 AND BS 907, WL 266, LBL 65. REPAIRED FRAMES PER ER 99-6050A.

Part: CLIP — CRACKED (BS 767&807)

DURING SCHEDULED D CHECK, FOUND 2 EACH FUSELAGE STRINGER CLIPS CRACKED, BS 767 AND BS 807, STRINGER 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE)

DURING SCHEDULED D CHECK, FOUND 3 EACH FUSELAGE FRAMES CRACKED, BS 380 AND BS 440, WL 283, LBL 55, AND BS 440, WL 283, RBL 55. REPAIRED FRAMES PER ER 99-6050A.

Part: SHEAR TIE — CRACKED (BS 500)

DURING SCHEDULED D CHECK, FOUND BS 500C SHEAR TIE CRACKED BETWEEN STRINGERS 13L - 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: COVER — DAMAGED (DOOR SLIDE)

DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE SHROUD COVER DAMAGED. REPAIRED SHROUD COVER PER MM.

Part: FRAME — CORRODED (BS 794)

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED, BS 794, RBL 8, WL 150. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (BS 420)

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED, BS 420, RBL 74. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FITTING — CORRODED (RT TE FLAP)

DURING SCHEDULED D CHECK, FOUND CORROSION ON RT WING NR 8 T/E AFT FLAP TRACK ATTACH FITTING. REMOVED AND REPLACED NR 8 AFT FLAP TRACK ATTACH FITTING PER SRM.

Part: CLIP — CRACKED (BS 706)

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP 11L CRACKED, BS 706. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND 2 EACH CRACKS, BS 178 BULKHEAD, BL 0 - RBL 7. REPAIRED BULKHEAD PER SRM.

Part: LENS — MISSING (CABIN)

DURING SCHEDULED BC3 CHECK, FOUND MAIN ENTRY AISLE EMERGENCY EXIT LIGHT MISSING LENS. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (ROW 3 & 6)

DURING SCHEDULED BC3 CHECK, FOUND 2 EA EMERGENCY ESCAPE LIGHT TRACKS OUT AT ROWS 6 AND 3. RELAMPED LIGHTS PER MM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED C2 CHECK, FOUND A 1.25 INCH CRACK IN FUSELAGE SKIN AT BS 727E, AT S24L. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, PERFORM C1 TASK 2041, REPLACE EMERGENCY LIGHT BATTERY PACKS BY USING SERVICEABLE BATTERIES. IF SERVICEABLE BATTERIES ARE NOT AVAILABLE ACCOMPLISH TEST AS OUTLINE ON TASK CARD 2041. REMOVED AND REPLACED NINE EMERGENCY LIGHT BATTERY PACKS PER BOEING MM.

Part: WEB — CRACKED (BS 767)

DURING SCHEDULED A2 CHECK, FOUND 2 INCH CRACK IN WEB AT BS 767, STR 22. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 767)

DURING SCHEDULED A2 CHECK, FOUND CRACKED 2 AT BS 767 STR 22. REPAIRED PER BOEING SRM.

Part: SIGN — BROKEN (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT SIGN RT SIDE BROKEN AT OVERWING EXIT DOOR. REMOVED AND REPLACED EXIT SIGN, OPS CHECKED PER BOEING MM.

Part: SLIDE — LOW PRESSURE (FWD ENTRY)

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

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACK INDICATION AT BS 178 BULKHEAD, WL 198 TO RBL 4.7. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD BS 178 CRACKED, AT WL 212 TO 212.5, LBL 6.7. REPAIRED PER T1-353-046.

Part: STRAP — CORRODED (BS 797-857)

DURING SCHEDULED D-CHECK, FOUND TEAR STRAP CORRODED FROM BS 797 TO 857, RBL 18. REPLACED PER BOEING SRM.

Part: STRAP — CRACKED (BS 314)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM STABILIZER STRAPS CRACKED AT BS 314, BL 0, WL 200, AND AT BS 314, RBL 31, WL 200. REPLACED PER BOEING SRM.

Part: BULKHEAD SUPPORT — CORRODED (BS 500)

DURING SCHEDULED D-CHECK, FOUND FLOOR TO BULKHEAD SUPPORT AT BS 500D CORRODED FROM RBL 17 TO LBL 5. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED TERMINAL CHECK, FOUND FWD SERVICE DOORWAY UPPER STUB FRAME CRACKED. REPLACED PER BOEING SRM.

Part: SLIDE — DEPLOYED (FWD GALLEY DOOR)

DURING SCHEDULED RON, GALLEY DOOR SLIDE DEPLOYED. REPLACED SLIDE PER BOEING M/M.

Part: SENSOR — OUT OF ADJUST (LANDING GEAR)

ON CLIMBOUT, CREW HAD TO USE OVERRIDE TRIGGER TO RAISE GEAR HANDLE, GEAR EXTENDED NORMALLY. AIRCRAFT RETURNED TO SLC AND MADE AN UNEVENTFUL LANDING. AIRCRAFT MX FERRIED TO PHX, ADJUSTED GROUND SHIFT SENSOR PER BOEING M/M.

Part: INDICATOR — INOP (TE FLAPS)

AFTER TAKEOFF, FLAPS WOULD NOT RETRACT PAST 5 DEGREES, EXTENDED FLAPS NORMALLY. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. REPLACED FLAP POSITION INDICATOR PER BOEING MAINTENANCE MANUAL.

Part: CONNECTOR — CORRODED (RRT TE FLAP)

DURING CLIMBOUT, FLAPS REMAINED AT FIVE DEGREES. AIRCRAFT RETURNED TO SLC AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND RIGHT FLAP POSITION TRANSMITTER CANNON PLUG CORRODED. CLEANED PLUG AND OPERATED FLAPS THROUGH ALL SETTINGS, OK PER BOEING MAINTENANCE MANUAL.