N698SW

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 77,221 hrs · 63,390 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 14R TO STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,218 hrs · 63,389 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 500C, STR 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,218 hrs · 63,389 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,197 hrs · 63,371 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 520, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME IAW ER.

Part: LENS — CRACKED (CABIN) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS CRACKED AT ROW 10. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,758 hrs · 63,024 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT. REMOVED AND REPLACED DOOR PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 76,718 hrs · 62,994 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT IAW MM.

Part: LIGHT — LOOSE (CABIN) · airframe 75,678 hrs · 62,201 cycles

RT OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,277 hrs · 61,910 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5L. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,277 hrs · 61,910 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CORRDED AT BS 947, STR 27R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,277 hrs · 61,910 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,277 hrs · 61,910 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,277 hrs · 61,910 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 4L. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,277 hrs · 61,910 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 486, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 75,277 hrs · 61,910 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,277 hrs · 61,910 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOORBEAM CRACKED AT BS 665, RBL 24.5. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,277 hrs · 61,910 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2L. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,277 hrs · 61,910 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 927+14, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,277 hrs · 61,910 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED BETWEEN BS 931 TO BS 932, STR 20L. REPAIRED SKIN PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 75,277 hrs · 61,910 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT OVERHEAD EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 75,277 hrs · 61,910 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT WING I/B MID FLAP T/E WEDGE LOWER SURFACE DELAMINATED. REPAIRED MID FLAP PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 75,277 hrs · 61,910 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT WING O/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,463 hrs · 61,296 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 791, STR 19L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,463 hrs · 61,296 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 350.5, STR 25R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,463 hrs · 61,296 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 405, STR 26L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,460 hrs · 61,295 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 405, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,460 hrs · 61,295 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 791, STR 19L. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 74,460 hrs · 61,295 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,460 hrs · 61,295 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,460 hrs · 61,295 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 350.5, STR 25R. REPAIRED SKIN PER SRM.

Part: LIGHT — MISSING (CABIN) · airframe 74,460 hrs · 61,295 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS MISSING AT ROW 8. INSTALLED EEPLS PER MM.

Part: COVER — MISSING (CABIN) · airframe 74,030 hrs · 60,950 cycles

L1 DOOR LOWER FWD EMERGENCY EXIT LIGHT LENS COVER MISSING. INSTALLED COVER PER MM.

Part: VSI — FAULTY (COCKPIT) · airframe 72,970 hrs · 60,142 cycles

DIVERSION - AFTER TAKEOFF FROM STL NOTICED A BURNING ACRID SMELL. CREW DONNED O2. REMOVED AND REPLACED IVSI PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 72,782 hrs · 60,003 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,728 hrs · 59,956 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787+17, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,390 hrs · 59,697 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 504D, BETWEEN STR 16L TO STR 17L. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,613 hrs · 59,120 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 21R TO STR 22R. REPAIRED FRAME PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,365 hrs · 58,931 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,365 hrs · 58,931 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 71,316 hrs · 58,887 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,170 hrs · 58,792 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 972, STR 24L. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER EA AND SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR HINGE CUTOUT FITTING CRACKED AT BS 293, BETWEEN WL 239 TO WL 240. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500D, STR 13L. REPAIRED FRAME PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 727, STR 14L. REPAIRED FRAME PER AAR EA.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GAUGE LOW PRESSURE. REMOVED AND REPLACED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR EMERGENCY EXIT SIGN LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 13L. REPAIRED FRAME PER ER.

Part: DOOR FRAME — CRACKED (AFT CARGO DOOR) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO DOOR FWD FRAME CRACKED. REMOVED AND REPLACED FRAME PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EXIT SIGN LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT L1 DOOR UPPER HINGE CUT OUT, BS 305, WL 261 - WL 258. REPAIRED SKIN PER EA & SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT UPPER L-ANGLE CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED L-ANGLE PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND L2 DOOR EMERGENCY EXIT SIGN LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 867, STR 26R. REPAIRED STRINGER PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 706, LBL 24.5. REPAIRED WEB PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN LBL 6 TO RBL 6. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME WEB CRACKED AT BS 887, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM LOWER CHORD CRACKED AT BS 662, LBL 24.8. REPAIRED BEAM PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME WEB CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 727C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 887 TO BS 907, STR 26L. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 767, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: RIB — CRACKED (RT WING) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5. REMOVED AND REPLACED RIB PER ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500D, STR 13R. REPAIRED FRAME PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 559, STR 13R. REPAIRED FRAME PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER AAR EA.

Part: SKIN — CRACKED (LT WING) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING SKIN CRACKED AT NR 1 SLAT I/B TRACK CUTOUT. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN LBL 17.2 TO LBL 21. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 616 TO BS 639, STR 17R. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM CRACKED AT BS 616, RBL 63.5. REPAIRED BEAM PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 1 SLAT UPPER WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (TE FLAP) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING TRAILING EDGE I/B FORE FLAP LOWER SKIN CRACKED. REPAIRED SKIN PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 13L. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 2 SLAT WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 6 SLAT T/E WEDGE, UPPER SURFACE I/B DELAMINATED. REPAIRED WEDGE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (LT WING) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING L/E SKIN DELAMINATED AT FS 364. REMOVED AND REPLACED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (BS 420 S26L) · airframe 705,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 420, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: WEDGE — DELAMINATED (LT NR 3 SLAT) · airframe 705,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 3 SLAT WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: SHEAR TIE — CRACKED (BS 616 S7L) · airframe 705,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 616, BETWEEN STR 7L TO STR 8L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,555 hrs · 58,329 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 13L. REPAIRED FRAME PER AAR EA.

Part: WIRE — EXPOSED (LAVATORY) · airframe 70,484 hrs · 58,279 cycles

DURING SCHEDULED MV3 CHECK, FOUND EXPOSED WIRE IN FWD LAV GOING TO EMERGENCY EXIT LIGHT. REPAIRED WIRE PER WDM.

Part: STRIP — WORN (CABIN) · airframe 70,021 hrs · 57,950 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP WORN AT ROW 19. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,021 hrs · 57,950 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED PER SWA EA.

Part: STRIP — WORN (CABIN) · airframe 70,021 hrs · 57,950 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP WORN AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,021 hrs · 57,950 cycles

DURING SCHEDULED HC1 CHECK, FOUND AFT CABIN RT EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,021 hrs · 57,950 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 787+17, STR 18L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,836 hrs · 57,123 cycles

FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — LOOSE (CABIN) · airframe 68,387 hrs · 56,809 cycles

R1 DOOR EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER SWA EA.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 68,366 hrs · 56,794 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED AT LOWER SURFACE. REMOVED AND REPLACED FLAP PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 68,366 hrs · 56,794 cycles

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

Part: STRINGER CLIP — CRACKED (BS 986 S18L) · airframe 67,050 hrs · 55,836 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 18L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 28R CORRODED AT BS 360. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 28R CRACKED AT BS 440. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT OUTBOARD LOWER SURFACE. REPAIRED SLAT PER SWA EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CORRODED BETWEEN BS 362 AND BS 364, STR 27L. REPAIRED SKIN PER EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, LBL 7 TO LBL 13. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BL 0 TO LBL 13. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 360, RBL 18. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 805, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, LBL 7 TO LBL 13. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 27L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 986.5, STR 20R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 336, STR 21L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, LBL 7 TO LBL 13. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM TEE CAP CORRODED AT BS 689.5, LBL 45. REMOVED AND REPLACED TEE CAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 320, STR 21L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 27L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM CHORD CORRODED BETWEEN BS 270 AND BS 360, STR 17R. REMOVED AND REPLACED CREASE BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM CHORD CORRODED BEWTEEN BS 950 AND BS 986.5, STR 17R. REMOVED AND REPLACED CEASE BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 480, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,411 hrs · 53,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA BETWEEN BS 434 AND BS 413, LBL 2 AND LBL 3. REPAIRED SKIN PER SB.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,411 hrs · 55,378 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: VALVE — FAULTY (NR 2 ENGINE) · airframe 66,163 hrs · 55,196 cycles

INFLIGHT SHUTDOWN / DECLARED EMERGENCY/DIVERSION. NR 2 ENGINE ROLLED BACK AND SHUTDOWN, RESTARTED NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE SPAR VALVE PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 65,488 hrs · 54,703 cycles

L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 65,418 hrs · 54,656 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 1006, STR 27L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (BS 967 S26R) · airframe 65,418 hrs · 54,656 cycles

DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CORRODED AT BS 967, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BEAR STRAP — CRACKED (BS 957 S25R) · airframe 65,418 hrs · 54,656 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT BS 957, STR 25R. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,418 hrs · 54,656 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER 26R CORRODED AT BS 1006. REPAIRED STRINGER PER SRM.

Part: SKIN — CORRODED (BS 986 S27LR) · airframe 65,418 hrs · 54,656 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 986, STR 27L AND STR 27R. REPAIRED SKIN PER SWA EA.

Part: GLOWSTRIP — WORN (CABIN) · airframe 65,401 hrs · 54,638 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN BETWEEN ROW 14 DEF AND ROW 17 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 65,401 hrs · 54,638 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 967, STR 27L. REPAIRED SKIN PER SRM.

Part: FITTING — BROKEN (NR 4 SPOILER) · airframe 65,401 hrs · 54,638 cycles

DURING SCHEDULED C4 CHECK, FOUND LEFT WING NR 4 GROUND SPOILER OUTBOARD ACTUATOR FITTING BROKEN. REMOVED AND REPLACED ACTUATOR PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 64,490 hrs · 53,904 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,338 hrs · 53,783 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 500D S16R) · airframe 63,954 hrs · 52,480 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16R. REPAIRED SKIN PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,833 hrs · 53,390 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 420 S17R) · airframe 63,788 hrs · 53,360 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 420, STR 17R. REPAIRED SKIN PER SWA EA & SRM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 61,575 hrs · 51,680 cycles

L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 62,616 hrs · 52,458 cycles

DURING SCHEDULED C1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 12 DEF. SECURED LENS PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 61,523 hrs · 51,638 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD SIDE. REMOVED AND REPLACED INBOARD FLAP PER MM.

Part: SKIN — CRACKED (BS 760) · airframe 61,462 hrs · 51,595 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 777) · airframe 61,462 hrs · 51,595 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 777, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 749) · airframe 61,462 hrs · 51,595 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 518) · airframe 61,462 hrs · 51,595 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 780) · airframe 61,462 hrs · 51,595 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 731C) · airframe 61,462 hrs · 51,595 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 731C, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 60,530 hrs · 50,873 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,352 hrs · 50,753 cycles

DURING SCHEDULED RON CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK PER MM.

Part: SKIN — CRACKED (BS 514) · airframe 59,689 hrs · 50,252 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 947.5) · airframe 59,689 hrs · 50,252 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 941) · airframe 59,689 hrs · 50,252 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 21R. REPAIRED SKIN PER SWA EA.

Part: STRINGER — CRACKED (BS 360) · airframe 58,911 hrs · 49,660 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 360, STR 14L. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (BS 992) · airframe 58,911 hrs · 49,660 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 992, MAST DRAIN CUTOUT. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (BS 500B) · airframe 58,911 hrs · 49,660 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (BS 663) · airframe 58,911 hrs · 49,660 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 663, BL 0, WL 208. REPAIRED FLOORBEAM PER SWA EA.

Part: SHEAR TIE — CORRODED (BS 787) · airframe 58,911 hrs · 49,660 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, LBL 3. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — DELAMINATED (LT AILERON TAB) · airframe 58,911 hrs · 49,660 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT WING AILERON TAB T/E DELAMINATED. REMOVED AND REPLACED TAB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,911 hrs · 49,660 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,911 hrs · 49,660 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT, LOWER AFT CORNER. REPAIRED SKIN PER SRM.

Part: BELTFRAME — CORRODED (BS 500A) · airframe 58,911 hrs · 49,660 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BELTFRAME CORRODED AT BS 500A, RBL 1. REPAIRED BELTFRAME PER SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 58,711 hrs · 49,493 cycles

DURING SCHEDULED C1 CHECK, FOUND LT MLG STABILIZER BEAM OTBD ATTACH ANGLE CRACKED. REMOVED AND REPLACED ATTACH ANGLE PER SRM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 58,711 hrs · 49,493 cycles

DURING SCHEDULED C1 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 2 HINGE BUSHING AND HARDWARE PER MM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 58,474 hrs · 49,281 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 847, LBL 4. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,172 hrs · 49,052 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED FROM BS 517 TO BS 519, STR 12R. REPAIRED SKIN PER SWA EA & SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 58,172 hrs · 49,052 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NLG W/W PRESSURE WEB CRACKED AT RT FWD PANEL CUTOUT, BS 246, WL 168.5. REPAIRED WEB PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 57,736 hrs · 48,708 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,778 hrs · 47,966 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 752, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,794 hrs · 47,192 cycles

DURING SCHEDULED C2 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 500A + 2, STRINGER 10R, BS 500A + 10, STRINGER 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,794 hrs · 47,192 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 777, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,371 hrs · 46,840 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 791, STRINGER 20L, CRACKED. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (ROW 16 & 17) · airframe 53,968 hrs · 45,748 cycles

DURING SCHEDULED C4 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 16 AND 17 DEF. SECURED LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,733 hrs · 45,572 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 486 AND BS 500D, STRINGER 10R. REPAIRED SKIN PER SRM.

Part: GLARE SHIELD — MALFUNCTIONED (COCKPIT) · airframe 53,169 hrs · 45,121 cycles

SMOKE APPEARED IN FRONT OF CAPT'S INSTRUMENT PANEL FOR ABOUT 5 SECONDS. SMOKE AND ODOR DISSIPATED. COMPLIED WITH COCKPIT INSPECTION NO DEFECTS FOUND. REMOVED AND REPLACED GLARESHIELD ASSY, RADAR IND, FMC CDU, AND RADIO CONTROL PANELS PER MM.

Part: LENS — LOOSE (EXTERIOR) · airframe 52,123 hrs · 44,278 cycles

DURING SCHEDULED C2 CHECK, FOUND RT AFT EXTERIOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED EXIT LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,807 hrs · 44,013 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (6 EA) AT STR 4L, BS'S 591, 592, 644, 698, 702 AND 590. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,807 hrs · 44,013 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 689, STR 4R. REPAIRED SKIN PER SRM.

Part: WIRE — CHAFED (RT WING ROOT) · airframe 51,274 hrs · 43,594 cycles

ABORTED TAKEOFF, WITH 80 PERCENT N2, NR 2 ENG WENT BACK TO IDLE. REPAIRED WIRING AT BUNDLE NR W804 PER WDM. OPS CK GOOD PER MM.

Part: FITTING — CRACKED (LT WING) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND LT MLG FITTING UPPER REAR SPAR D-HOLE CRACKED. REMOVED AND REPLACED LT MLG ATTACK FITTING PER ER, SRM, & BAC DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727, WL 148 & RBL 4. REPAIRED FUSELAGE FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CORRODED (2 EA) AT BS 794, WL 157 AT RBL 21 & BS 786, WL 153 AT RBL 14. REPAIRED FUSELAGE FRAMES PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, WL 208 & LBL 5. REPAIRED FLOORBEAM PER BFG ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727C, WL 148 RBL 5 TO LBL 5. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED (12 EA) AT STRINGER 9L, BS 406, 827, 867, 901, 440, 480, 500, 747, 767, 887, 847 & 807. REPAIRED FRAMES PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) AT STRINGER 9R, BS 440 & BS 867. REPAIRED FUSELAGE FRAMES PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AND CRACKED AT BS 639, BETWEEN WL 208 & WL 212 RT SIDE. REPAIRED FRAME PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND KEELBEAM WEB CORRODED, BS 663 TO BS 727A RT SIDE. REPAIRED KEELBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED AT BS 277 AT STR 15R & BS 360 AT STR 4L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FLOORBEAM — CORRODED (AFT CABIN) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 1006, WL 208 & LBL 9. REPAIRED FLOORBEAM PER SRM.

Part: SKIN — BULGED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN BULGED AT BS 380, BETWEEN STR 16L & STR 17L. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500C, BETWEEN STR 27R & STR 28R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500C, BETWEEN STR 27L & STR 28L. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 1121, STR 3L. REPAIRED STR PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED ( 7 EA ) AT BS 380 AT STR 8L, BS 616 AT STR 4L, BS 727D AT STR 6L, BS 767 AT STR 3L, BS 867 AT STR 3L, BS 500D AT STR 8L & BS 500D AT STR 7L. R&R STRINGER CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED ( 4 EA ) AT BS 616 AT STR 4R, BS 727D AT STR 8R, BS 500B AT STR 4R & BS 520 AT STR 8R. R&R STRINGER CLIPS PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

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

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 663.75, LBL 6.75. R&R VERTICAL STIFFENER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIPS CRACKED (6 EA) AT BS 639 AT STR 4L, BS 727D AT STR 7L, BS 727D AT STR 3L, BS 727E AT STR 3L, BS 500D AT STR 5L & BS 520 AT STR 7L. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIPS CRACKED (7 EA) AT BS 597 AT STR 3R, BS 639 AT STR 4R, BS 727 AT STR 6R, BS 867 AT STR 4R, BS 867 AT STR 5R, BS 500D AT STR 8R & BS 520 AT 6R. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED ( 4 EA ) AT BS 500C AT STR 7R, BS 520 AT STR 7R, BS 663 AT STR 10R & BS 663 AT STR 10L. R&R STRINGER CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIPS CRACKED AT BS 500D, STR 7R & STR 6L. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME OUTER CHORD CRACKED AT BS 188, WL 207 & RBL 30. REMOVED AND REPLACED FUSELAGE FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 13L & 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,237 hrs · 43,566 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,398 hrs · 42,923 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 6, STR 24L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 50,398 hrs · 42,923 cycles

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

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 49,858 hrs · 42,499 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 49,566 hrs · 42,301 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD RT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — FAULTY (CABIN) · airframe 49,101 hrs · 41,888 cycles

DURING SCHEDULED PM CHECK, FWD CABIN EMERGENCY EXIT LIGHTS NOT TURNING OFF. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,773 hrs · 45,556 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKS (2 EA) AT STR 22L, BS 767 AND BS 787. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,692 hrs · 41,565 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 10R. REPAIRED SKIN PER SRM.

Part: LENS — BROKEN (FWD ENTRY DOOR) · airframe 48,692 hrs · 41,565 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 48,166 hrs · 41,135 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 48,166 hrs · 41,135 cycles

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

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 47,820 hrs · 40,837 cycles

EMERGENCY FLASHLIGHT INOP IN AFT CABIN TOP POSITION. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (FWD CABIN DOORS) · airframe 47,812 hrs · 40,829 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 47,715 hrs · 40,750 cycles

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

Part: PUMP — FAILED (FUEL TANK) · airframe 47,333 hrs · 40,424 cycles

NR 2 FUEL TANK FWD FUEL BOOST PUMP LOW PRESS LIGHT ILLUMINATED. REMOVED AND REPLACED NR 2 FUEL TANK FWD BOOST PUMP AND LOW PRESS SWITCH PER MM.

Part: FRAME — CORRODED (AFT CARGO) · airframe 49,052 hrs · 43,320 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 1006, RBL 34 & WL 200. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,920 hrs · 39,270 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 19R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF TOLERANCE (ENTRY DOOR) · airframe 41,037 hrs · 35,686 cycles

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

Part: PLATE — DELAMINATED (L/E FLAP) · airframe 44,163 hrs · 37,795 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING L/E INBD FORE FLAP REPAIR PLATE DISBONDED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,839 hrs · 37,548 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 4 BS 178 BULKHEAD WEB CRACKS BETWEEN RBL 26 TO LBL 12.5, WL 207 TO WL 232. REPAIRED BULKHEAD WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,839 hrs · 37,548 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL CHORD CRACKED AT LBL 5.7, AFT SIDE, INBOARD RADIUS, WL 182.5 TO WL 184. REPAIRED VERTICAL CHORD PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,839 hrs · 37,548 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT BS 178, WL 240 RT. REPAIRED SKIN PER ER 01-0045.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,657 hrs · 37,400 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHTING INOP IN FWD SECTION. R&R BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,522 hrs · 37,290 cycles

DURING SCHEDULED A2 CHECK, FOUND .5 EXTERNAL FUSELAGE SKIN CRACK BETWEEN BS 727D & BS 727E AT STR 21L. REPAIRED SKIN PER SRM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 43,316 hrs · 37,112 cycles

EEPLS IN AFT CABIN LOOSE. REPAIRED EEPLS TRACK COVER PER MM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 43,163 hrs · 36,977 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT, 6 CRACK, AT LOWER T/E SKIN, O/B OF THE O/B ACTUATOR STOP. REPAIRED SKIN PER SRM.

Part: LENS — CRAZED (FUSELAGE) · airframe 43,163 hrs · 36,977 cycles

DURING SCHEDULED C4 CHECK, FOUND LT HATCH EXTERNAL EMERGENCY EVAC LIGHT LENS CRAZED. REMOVED AND REPLACED LENS PER MM.

Part: LINE — LEAKING (NLG ACTUATOR) · airframe 42,160 hrs · 36,123 cycles

AIR TURNBACK, NLG EXTENDED WHEN HANDLE PLACED IN OFF POSITION. REMOVED AND REPLACED UPPER NLG ACTUATOR UPLOCK HYD LINE PER MM. OPS CHECK GOOD.

Part: ROD END — OUT OF ADJ (NR 6 SLAT) · airframe 41,935 hrs · 35,926 cycles

AIR TURNBACK, NR 6 L/E SLAT WOULD FULLY EXTEND AND WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED NR 6 L/E SLAT ROD END ACTUATOR PER MM.

Part: VALVE — FAILED (HYDRAULIC SYS) · airframe 41,903 hrs · 35,896 cycles

AIR TURNBACK. DURING CLIMB, NR 1 ENG HYD PUMP FAILED FOLLOWED BY ELEC A-SYS HYD PUMP FAILURE. REMOVED AND REPLACED A-SYS HYD MANUAL SHUT-OFF VALVE IN TAIL COMPARTMENT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,365 hrs · 35,437 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED AT 4 PLACES, STRINGER 23R, BS 747, BS 730, BS 870, AND BS 747, STRINGER 24R. REPAIRED SKIN PER SRM.

Part: CONTROL PANEL — INOPERATIVE (COCKPIT) · airframe 41,213 hrs · 35,305 cycles

AIR TURNBACK - UNABLE TO CONTROL CABIN PRESSURE AFTER BECOMING AIRBORNE. R&R PRESS CONTROL PANEL, OUTFLOW VALVE, REPLACED LOOSE CLAMP AT RH A/C PACK WATER SEPARATOR, AND R&R MIXING CHAMBER DUCT PER MM.

Part: LENS — LOOSE (FUSELAGE)

RT AFT WING TO FUSELAGE OUTER EMERGENCY LIGHT LENS LOOSE. RESECURED LENS ASSY PER MM.

Part: MODULE — INOP (E&E COMPT)

AIR TURNBACK, LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED RELAY R276, AND M991 MODULE PER MM.

Part: SOLENOID — INOP (COCKPIT)

AIR TURNBACK, DURING TAKEOFF, LANDING GEAR HANDLE WOULD NOT RAISE PAST OFF POSITION. LANDING GEARS WOULD NOT RETRACT. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER SOLENOID PER MM.

Part: SKIN — CRACKED (BS 727)

DURING WALK ARROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED, BS 727D, STRINGER 18L AND STRINGER 18R. REPAIRED CRACKS PER SRM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED, BS 727E, STRINGER 24R. REPAIRED SKIN PER SRM.

Part: TAB — CRACKED (RT AILERON)

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND RT AILERON TAB LOWER SURFACE CRACKED AND DELAMINATED. REMOVED AND REPLACED AILERON TAB PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED 1/2 D CHECK, FOUND RIGHT HAND CENTER EMERGENCY LIGHTS BATTERY PACK WILL NOT CHARGE. REMOVED AND REPLACED BATTERY PACK PER BOEING MM.

Part: FLOORBEAM — CRACKED (BS 787)

DURING SCHEDULED 1/2 D CHECK, FOUND CRACKED FLOORBEAM AT TIE DOWN BS 787 RBL 14. REPAIRED PER BOEING MM.

Part: LIGHT — LOOSE (CABIN)

DURING SCHEDULED 1/2 D CHECK, FOUND 7 ABC BULLNOSE EGRESS LIGHT LOOSE. REPAIRED PER BOEING MM.

Part: SKIN — CRACKED (NR 2 PYLON)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM AT RBL 13 BETWEEN BS 794 AND BS 847 AROUND MANY FASTENER LOCATIONS. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 794-847)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM AT RBL 13 BETWEEN BS 794 AND BS 847 AROUND MANY FASTENER LOCATIONS. REPAIRED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 500)

DURING SCHEDULED 1/2 D CHECK, FOUND STRINGER 27L CORRODED BETWEEN BS 500C + 500D. REPAIRED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 844)

DURING SCHEDULED 1/2 D CHECK, FOUND STRINGER 26R AT BS 844 CORRODED AROUND HI-LOK. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED BS 178 LT BULKHEAD CHORD ANGLE WL 207. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — BUCKLED (BS 500)

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN BUCKLED/WARPED AROUND FASTENERS ON LOWER LOBE AT BS 500C, STR 28L. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 440)

DURING SCHEDULED 1/2D CHECK, FOUND WEB CRACKED AT DOOR OPENING BS 440, STR 25R. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED FLOORBEAM AT BS 986, RBL 32; BS 986, RBL 36; AND BS 986, RBL 40. REPAIRED PER BOEING SRM.

Part: CHANNEL — CRACKED (LT WING)

DURING SCHEDULED 1/2D CHECK, FOUND U CHANNEL SUPPORT FOR I/B PYLON PANEL CRACKED. REPAIRED PER BOEING MM.

Part: ANGLE — CORRODED (BS 727-767)

DURING SCHEDULED 1/2D CHECK, FOUND LT TRANSITION ANGLE CORRODED AT BS 727D-727E.; BS 727E-747; BS 747-767; AND 727-727B. REPAIRED PER BOEING MM.

Part: STRAP — CRACKED (LT WING)

DURING SCHEDULED 1/2D CHECK, FOUND STRAP FOR I/B PYLON PANEL CRACKED. REPAIRED PER BOEING MM.

Part: ANGLE — WORN (LT WING)

DURING SCHEDULED 1/2D CHECK, FOUND PYLON SUPPORT ANGLE FOR PANEL WORN JUST BELOW HYD LINES NR 3 JACKSCREW CANOE FAIRING. REMOVED AND REPLACED PER BOEING MM.

Part: WEB — CRACKED (BS 360-380)

DURING SCHEDULED 1/2 D-CHECK, FOUND O/B WEB AT BS 360 TO 380, STR 17L IS BENT AND CRACKED. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED SKIN AT BS 178 WL 188 LBL .5, WL 188 RBL .5 AND WL 198 RBL 5. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED FWD SIDE OF BULKHD, RBL 5 WL 201 AND WL 201 LBL 5. REPAIRED PER BOEING SRM.

Part: ANGLE — MISSING (BS 294.5)

DURING SCHEDULED 1/2 D-CHECK, FOUND ANGLE MISSING AT FWD SERV DOOR POST FWD LOWER CORNER ATTACHED TO Z-ANGLE AT BS 294.5, RBL 56. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM AT BS 986 LBL 10.5. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 380-400)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED C/L INTERCOSTAL AT SCREW HOLES BS 380 TO 400. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED SKIN AT BS 178, WL 198, RBL 5. REPAIRED PER BOEING SRM.

Part: SPLICE — CORRODED (BS 490)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED SPLICE AT BS 490, STR 27L. REPAIRED PER BOEING SRM.

Part: SPLICE — CORRODED (BS 490)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED SPLICE AT BS 470 TO 480, STR 27L. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 927-947)

DURING SCHEDULED 1/2 D-CHECK, FOUND C/L INTERCOSTAL HAS CRACKS AT SCREW HOLES BS 927 TO 947. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM AT BS 344 PANEL HOLE, LBL 28. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 787)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED TRANSITION ANGLE AT BS 787 RBL 23. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (LT PYLON)

DURING SCHEDULED C2 CHECK, FOUND PANEL ATTACH ANGLE ON TOP OF PYLON CRACKED, INBD SIDE. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 520)

DURING SCHEDULED BC2 CHECK, FOUND SHEAR WEB AND ANGLE CRACKED AT BS 520, LBL 24.75. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 520)

DURING SCHEDULED C2 CHECK, FOUND WEB BETWEEN FLOORBEAMS CRACKED AT BS 520 LBL 24.75 AND BS 520 ALONG LBL 45.50 (CRACK IS 1.5 LONG, LOCATED AT THE UPPER AFT CORNER). REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 520)

DURING SCHEDULED C2 CHECK, FOUND FLOORBEAM AT BS 520 CRACKED. REPAIRED PER BOEING SRM.

Part: B-NUT — LEAK (AC BAY)

AFTER PUSH BACK FROM GATE, SMOKE FILLED CABIN AND COCKPIT IMMEDIATELY AFTER TURNING PACKS ON. RETURNED TO GATE, CLEARED CABIN AIR, INSPECTED AND CONTINUED PER MEL. AFTER TAKEOFF, CREW EXPERIENCED SMOKE IN THE CABIN AGAIN AIRCRAFT RETURN TO TUL AND MADE AN UNEVENFUL LANDING. RETORQUED B-NUT ON HYD FUSE ABOVE AFT HEAT EXCHANGER. REMOVED AND REPLACED WATER SEPARATOR AND BAGS. LEAK AND OPS CHECKED ALL PER BOEING MM.

Part: WINDOW — NOT SEALED (LT COCKPIT)

DURING CLIMBOUT, NOTED VERY LARGE AIR LEAK AT CAPT NR 1 WINDOW. AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED WINDOW ASSEMBLY PER BOEING M/M.

Part: HARNESS — SHORTED (NR 2 ENGINE)

DURING CLIMBOUT, CREW WAS UNABLE TO CONTROL CABIN PRESSURE USING AUTO AND STANDBY MODES. AIRCRAFT RETURNED TO SLC AND MADE AN UNEVENTFUL LANDING. PERFORMED PRESSURE CONTROL SYSTEM TEST, NO DEFECTS NOTED. FOUND NR 2 ENGINE BLEED CONTROL C/B CONTINUALLY TRIPPING. REPAIRED WIRING AT NR 2 ENGINE PRSOV WIRING HARNESS PER BOEING M/M.

Part: TARGET — FAILED (RT MLG)

AFTER TAKEOFF, RT MAIN GEAR RED UNSAFE WARNING LIGHT WOULD NOT EXTINGUISH. CYCLED GEAR, NO HELP. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED UPLOCK BRACKET AND TARGET ASSEMBLY PER BOEING M/M.

Part: SKIN — CORRODED (BS 727)

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CORROSION BULGING BETWEEN FASTENERS AT BS 727 TO 727A AT STRINGER 27R. REPAIRED PER SWA RA 1-353-1544.

Part: SKIN — CORRODED (BS 727)

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE LOWER SKIN CORROSION BULGING BETWEEN BS 727 TO 727A, S28L. REPAIRED PER SWA RA 1-353-1465.