N689SW

Part: LIGHT — CRACKED (EXIT SIGN) · airframe 78,207 hrs · 66,084 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT SIGN LIGHT CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 78,059 hrs · 65,975 cycles

L2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EEPLS PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK FOUND, STRINGER CORRODED BETWEEN BS 500A TO BS 500C, STR 26L. REPAIRED STRINGER PER SRM.

Part: HOUSING — CORRODED (HORIZ STAB) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND CORRODED RT HINGE HOUSING. REMOVED AND REPLACED PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 662, LBL 24.8. REPAIRED CHORD PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CRACKED AT BS 887, STR 1. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 965.5, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 970, STR 4L. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED AT BS 320, STR 28R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CRACKED AT BS 496, STR 23R. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FOREFLAP) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT WING I/B FORE FLAP LOWER SKIN CRACKED. REPAIRED FORE FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 14L. REPAIRED FRAME PER EA.

Part: SUPPORT FITTING — CORRODED (FLAP TRACK) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT WING NR 6 FLAP TRACK FWD SUPPORT FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME INNER CHORD CRACKED AT BS 348, BETWEEN STR 12L TO STR 13L. REPAIRED CHORD PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND CENTER WING BOX LONGITUDINAL FLOORBEAM LOWER CHORD CRACKED AT BS 663, LBL 24.8. REPAIRED CHORD PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED AT BS 767+6, RBL 14. REPAIRED SUPPORT PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEUDLED 26Y CHECK, FOUND STRINGER CRACKED AT BS 480, STR 8L. REPAIRED STRINGER PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT BS 767+6, RBL 3. REPAIRED SUPPORT PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED AT BS 767+6, LBL 8. REPAIRED SUPPORT PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT BS 767+6, RBL 8. REPAIRED SUPPORT PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT BS 727D+6, LBL 2. REPAIRED SUPPORT IAW EA.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND CORROSION IN AFT CARGO BIN FLOOR SUPPORT NUT PLATE HOLES STA 727D+6, LBL 12. REPAIRED PER DOC.

Part: SUPPORT — CORRODED (CARGO BAY) · airframe 77,443 hrs · 65,504 cycles

DURING SCHEDULED 26Y CHECK, FOUND CORROSION IN AFT CARGO BIN FLOOR SUPPORT NUT PLATE HOLES, STA 727D+6, LBL 3. REPAIRED PER DOC.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,305 hrs · 65,391 cycles

DURING SCHEDULED OTS CHECK FOUND, OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 12 TO ROW 23. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CHARGER — FAULTY (CABIN) · airframe 77,305 hrs · 65,391 cycles

DURING SCHEDULED OTS CHECK FOUND, OVERHEAD EMERGENCY EXIT BULLNOSE LIGHTS ERRATIC. REMOVED AND REPLACED CHARGER HOUSING PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 76,967 hrs · 65,143 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,955 hrs · 65,135 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 517, STR 8L. REPAIRED SKIN PER EA.

Part: WIRE — LOOSE (CABIN) · airframe 75,614 hrs · 64,154 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT AFT COCKPIT WALL. SECURED WIRE PER SWPM.

Part: AILERON — DELAMINATED (L/H WING) · airframe 75,521 hrs · 64,070 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING AILERON DELAMINATED. REMOVED AND REPLACED AILERON PER MM.

Part: GASPER FAN — FAILED (AC BAY) · airframe 75,390 hrs · 63,960 cycles

VERY STRONG ELECTRICAL SMELL ON FINAL APPROACH IN MID-CABIN APPROX BETWEEN ROW 7 TO ROW 8. FOUND GASPER FAN FAILED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,090 hrs · 63,730 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FWD EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LAMP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,090 hrs · 63,730 cycles

DURING SCHEDULED SPV CHECK, FOUND EMERGENCY EXIT LIGHT O/B L2 DOOR INOP. REMOVED AND REPLACED LAMP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,090 hrs · 63,730 cycles

DURING SCHEDULED SPV CHECK, FOUND EMERGENCY EXIT LIGHT O/B L1 DOOR INOP. REMOVED AND REPLACED LAMP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,313 hrs · 63,128 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD SERVICE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 73,589 hrs · 62,593 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 73,575 hrs · 62,584 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 73,251 hrs · 62,335 cycles

AFT I/B FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FLOOR SUPPORT — CRACKED (BS 706-713) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOOR SUPPORT WEB CRACKED BETWEEN BS 706 TO BS 713, RBL 24.5. REPAIRED WEB PER ER.

Part: FLOOR SUPPORT — CRACKED (BS 727B) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 45.5. REPAIRED CHORD PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 20R TO STR 21R. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 420, STR 28L. REMOVED AND REPLACED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515B, STR 8R. REPAIRED SKIN PER EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME STRAP CRACKED AT BS 492, STR 18R TO STR 19R. REPAIRED FRAME PER SRM AND ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20R TO STR 21R. REPAIRED FRAME PER SRM AND ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 859, STR 25L TO STR 26L. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20R TO STR 21R. REPAIRED FRAME PER SRM AND ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 440, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 525, STR 8R. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20R TO STR 21R. REPAIRED FRAME PER SRM AND ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663.75, STR 2R. REPAIRED FRAME PER SRM AND ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED GROUND AIR CONDITIONING DOOR CUTOUT. REPAIRED SKIN PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 907, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 440, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 598, STR 15R. REMOVED AND REPLACED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20L TO STR 21L. REPAIRED FRAME PER SRM AND ER.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY PACKS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 460, STR 28R. REPAIRED STRINGER PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE LONGITUDINAL FLOORBEAM CRACKED AT BS 710 TO BS 714, BL 0. REPAIRED FLOORBEAM PER ER.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 793, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO BAY BILGE WEB CORRODED AT BS 940, STR 26R. REMOVED AND REPLACED WEB PER DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SHEAR TIE FRAME CRACKED AT BS 867, STR 25L TO STR 26L. REPAIRED FRAME PER SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB ATTACH ANGLE CRACKED AT BS 559, STR 17R. REPAIRED ANGLE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 728,848 hrs · 62,053 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 277, BETWEEN STR 11R TO STR 10R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FAME CRACKED AT BS 847, RBL 25. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 728,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 1006 TO BS 1010, STR 26R. REPAIRED STRINGER PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 708, LBL 24.8. REPAIRED WEB PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME WEB ANGLE CRACKED AT BS 640, STR 15L. REMOVED AND REPLACED ANGLE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 28R TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 728,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 360, STR 5L. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 728,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 728,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED BS 1010, STR 27L. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 27R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 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 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, BETWEEN STR 27L TO 27R. REPAIRED SHEAR TIE PER BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 728,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 728,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 728,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 27L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 27L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 728,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

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

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND FAIL-SAFE CHORD ANGLE CRACKED AT BS 460, STR 28R. REMOVED AND REPLACED CHORD PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SHEAR TIE FRAME CORRODED AT BS 747, STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. REMOVED AND REPLACED HOOK PER MM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND BULKHEAD CHORD CORRODED AT BS 1016, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 14R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,884 hrs · 62,053 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 1008, STR 26R. REMOVED AND REPLACED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,246 hrs · 61,593 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 291.5, RT 6 HOLES DOWN FROM THE TOP. REPAIRED FRAME PER EA.

Part: LENS — BROKEN (CABIN) · airframe 72,047 hrs · 61,436 cycles

EMERGENCY BULLNOSE LIGHT LENS BROKEN AT 17 ABC. REMOVED AND REPLACED LENS PER MM.

Part: DOWNLOCK SENSOR — FAULTY (NLG) · airframe 71,628 hrs · 61,123 cycles

DECLARED EMERGENCY / DIVERSION,14,000FT STEADY RED LIGHT ON NOSE GEAR. PUT GEAR DOWN, GREEN LIGHT ON MAINS NO GREEN ON NOSE GEAR. GEAR CHECK DOWN THRU VIEW PORT. LANDED NORMALLY. REMOVED AND REPLACED NOSE GEAR DOWNLOCK SENSOR PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,528 hrs · 60,319 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT OVERWING EMERGNECY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,528 hrs · 60,319 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 270, STR 16R. REPAIRED SKIN PER SWA EA.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 70,528 hrs · 60,319 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT T/E WEDGE DELAMINATED. REPAIRED SLAT PER SRM.

Part: STRIP — LOOSE (CABIN) · airframe 70,528 hrs · 60,319 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS STRIP LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: HOOK — LOOSE (L1 DOOR) · airframe 70,528 hrs · 60,319 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVACUATION SLIDE FWD GIRT BAR STOW HOOK ON CASE LOOSE. SECURED HOOK PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 70,528 hrs · 60,319 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVACUATION SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: LENS — MISSING (CABIN) · airframe 69,207 hrs · 59,357 cycles

DURING SCHEDULED MV3 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 23 DEF. INSTALLED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,921 hrs · 59,152 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 344, STR 22L. REPAIRED FRAME PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,920 hrs · 59,152 cycles

DURING SCHEDULE 22Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. R&R LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,920 hrs · 59,152 cycles

DURING SCHEDULED 22Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 23 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,920 hrs · 59,152 cycles

DURING SCHEDULED 22Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 12 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,920 hrs · 59,152 cycles

DURING SCHEDULED 22Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 21 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FLASHLIGHT — CRACKED (CABIN) · airframe 68,920 hrs · 59,152 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CABIN EMERGENCY FLASHLIGHT LENS CRACKED. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: CREASE BEAM — CORRODED (BS 314-343) · airframe 68,921 hrs · 59,152 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 314 AND BS 343, LBL 58 TO LBL 65. REMOVED AND REPLACED WEB PER SRM.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 68,921 hrs · 59,152 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. FOUND BROKEN WIRE. REPAIRED WIRE PER WDM.

Part: BEAM — WORN (RT WING) · airframe 68,920 hrs · 59,152 cycles

DURING SCHEDULED 22Y CHECK, FOUND RIGHT MLG FWD STABILIZER LUG WORN. REMOVED AND REPLACED RIGHT MLG STABILIZER BEAM PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,920 hrs · 59,152 cycles

DURING SCHEDULED HC1 CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 293.5, RBL 5. REMOVED AND REPLACED UPPER CHORD PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,920 hrs · 59,152 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 978 AND BS 992, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: FITTING — CRACKED (GIRT BAR) · airframe 68,920 hrs · 59,152 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CRACKED. REMOVED AND REPLACED FITTING PER SRM.

Part: LENS — MISSING (CABIN) · airframe 68,688 hrs · 58,974 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 19 DEF. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,498 hrs · 58,833 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 16R. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,267 hrs · 58,657 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,998 hrs · 58,440 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,890 hrs · 58,357 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 67,532 hrs · 58,093 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 66,803 hrs · 57,516 cycles

DURING SCHEDULED MV4 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 19 DEF. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,398 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 16R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (BS 867 S20L) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 867, STR 20L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 639) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT LEFT BS 639, WL 208. REMOVED AND REPLACED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (BS 520 S8L) · airframe 66,368 hrs · 57,177 cycles

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

Part: STRINGER CLIP — CRACKED (BS 597 S7L) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616 S5L) · airframe 66,368 hrs · 57,177 cycles

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

Part: STRINGER — CRACKED (BS 727C S8R) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 8R CRACKED AT BS 727C. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 987, STR 23R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 13R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 10L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,368 hrs · 57,177 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,161 hrs · 57,012 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16L. REPAIRED SKIN PER SRM & EA.

Part: FRAME — CORRODED (BS 807 S25L) · airframe 66,161 hrs · 57,012 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, STR 25L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (BS 827 S25L) · airframe 66,161 hrs · 57,012 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 827, STR 25L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (BS 847 S25L) · airframe 66,161 hrs · 57,012 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, STR 25L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,161 hrs · 57,012 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 763, STR 25L. REPAIRED SKIN PER SWA EA.

Part: LIGHT — LOOSE (CABIN) · airframe 65,865 hrs · 56,793 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 ABC. SECURED STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,728 hrs · 56,692 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 290, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,527 hrs · 56,546 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737E, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,527 hrs · 56,546 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 485, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 743E S25R) · airframe 65,010 hrs · 56,133 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 743E, STR 25R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 751 S25R) · airframe 65,010 hrs · 56,133 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 751, STR 25R. REPAIRED SKIN PER SWA EA.

Part: KEELBEAM — CORRODED (BS 510D-540) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND KEEL BEAM CHORD CORRODED AT BS 510D TO BS 540, RBL 6. REMOVED AND REPLACED KEEL BEAM CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME WEB CRACKED AT LOWER DOOR STOP. REMOVED AND REPLACED FRAME WEB PER SRM.

Part: SKIN — CRACKED (BS 791) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 791, STR 14R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 135.70. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR CUTOUT, FWD FRAME CRACKED FROM NR 2 DOOR STOP TO NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (BS 797) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT BS 797, STR 24R. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (BS 847) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, BL 3 TO LBL 3. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: RIB — CRACKED (LT WING) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING FUEL CELL INTERIOR MAIN BOX UPPER RIB CRACKED AT WBL 114, STR 1. REPAIRED RIB PER ER.

Part: KEELBEAM — CORRODED (BS 727) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND KEELBEAM CHORD CORRODED AT BS 727, LBL 6. REMOVED AND REPLACED KEELBEAM CHORD PER BOEING DRAWING AND ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME WEB CRACKED AT LOWER DOOR STOP. REMOVED AND REPLACED FRAME WEB PER BOEING DRAWING AND SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, STR 24R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND KEEL BEAM CHORD CORRODED AT BS 727, LBL 7. REMOVED AND REPLACED KEEL BEAM CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 15L. REPAIRED FRAME SECTION PER ER.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 348, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SKIN — DEBONDED (MIDFLAP) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING MID FLAP INBOARD T/E LOWER SURFACE DISBONDED. REPAIRED MID FLAP PER SRM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 5 L/E SLAT LOWER SKIN CRACKED AT INBOARD RIB ATTACHMENT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 751, STR 14R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (ELEVATOR TAB) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT ELEVATOR TAB LOWER SKIN CRACKED AT CENTER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: ARM — CORRODED (MIDFLAP CARRIAGE) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD MID FLAP INBOARD CARRIAGE OUTBOARD ARM CORRODED. REMOVED AND REPLACED OUTBOARD ARM PER CMM.

Part: SKIN — CRACKED (ELEVATOR TAB) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT ELEVATOR TAB LOWER SKIN CRACKED AT INBOARD CENTER HINGE CUTOUT OUTBOARD CORNER. REPAIRED SKIN PER SRM.

Part: ARM — CORRODED (MIDFLAP CARRIAGE) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD MID FLAP OUTBOARD CARRIAGE INBOARD ARM CORRODED. REMOVED AND REPLACED INBOARD ARM PER CMM.

Part: SKIN — DEBONDED (MIDFLAP) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING MID FLAP INBOARD T/E LOWER SURFACE DISBONDED. REPAIRED MID FLAP PER SRM.

Part: BRACKET — LOOSE (CABIN) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD BRACKET LOOSE. REMOVED AND REPLACED BRACKET PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING FORE FLAP INBOARD T/E SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: SKIN — DELAMINATED (EELVATOR TAB) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT ELEVATOR TAB LOWER SKIN DELAMINATED AT OUTBOARD END. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT BS 492, STR 24R. REMOVED AND REPLACED FRAME SECTION PER BOEING DRAWING AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,892 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD CARGO DOOR CUTOUT BEAR STRAP LOWER FWD CORNER. REPAIRED SKIN PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,862 hrs · 55,239 cycles

DURING SCHEDULED 20Y CHECK, FOUND STUB FRAME ANGLE CRACKED IN RADIUS AT BS 348, STR 16L. REMOVED AND REPLACED ANGLE PER SRM.

Part: LIGHT — WORN (CABIN) · airframe 63,672 hrs · 55,086 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS STRIP WORN AT ROW 17 ABC. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: SKIN — CRACKED (BS 739 S24R) · airframe 63,672 hrs · 55,086 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739, STR 24R. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (BS 385 S26L) · airframe 63,672 hrs · 55,086 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 385, STR 26L. REPAIRED SKIN PER SWA EA SRM.

Part: SKIN — CRACKED (BS 787 S20L) · airframe 63,672 hrs · 55,086 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 20L. REPAIRED SKIN PER SWA EA AND SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,234 hrs · 54,756 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD GALLEY LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 62,673 hrs · 54,336 cycles

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

Part: SKIN — CRACKED (BS 833) · airframe 62,664 hrs · 54,329 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 833, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 917-919) · airframe 62,664 hrs · 54,329 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 914 TO BS 919, STR 24R TO STR 25R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 860) · airframe 62,664 hrs · 54,329 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 860, STR 25L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 800) · airframe 62,664 hrs · 54,329 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 261) · airframe 62,377 hrs · 54,090 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 261, STR 9L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 905) · airframe 62,307 hrs · 54,038 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 905, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 883) · airframe 62,173 hrs · 53,935 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 883, STR 23R. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (BS 727D) · airframe 61,697 hrs · 53,552 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 14R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 767) · airframe 61,618 hrs · 53,492 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 907) · airframe 61,618 hrs · 53,492 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 907, STR 25L. REPAIRED SKIN PER SRM.

Part: COVER — MISSING (CABIN) · airframe 61,290 hrs · 53,226 cycles

LEFT OVERWING EMERGENCY EXIT SIGN COVER MISSING. INSTALLED COVER PER MM.

Part: CIRCUIT CARD — ARCED (E/E BAY) · airframe 60,919 hrs · 52,914 cycles

AIR TURNBACK/DECLARED EMERGENCY. RED NOSE GEAR LIGHT ILLUMINATED, ACFT DID NOT PRESSURIZE ABOVE 10,000 FT, LOW IDLE LIGHT ILLUMINATED DURING DESCENT. FOUND ARCING ON M1112, M990 & M991 CIRCUIT CARDS. REMOVED AND REPLACED CIRCUIT CARDS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,874 hrs · 52,870 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 810, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,874 hrs · 52,870 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 781, STR 18L. REPAIRED SKIN PER SRM.

Part: BUSHING — WORN (LT ELEVATOR TAB) · airframe 60,762 hrs · 52,774 cycles

DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 & 2 HINGE BUSHINGS & HARDWARE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,623 hrs · 52,661 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 391, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,623 hrs · 52,661 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 443, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,566 hrs · 52,599 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, STR 14R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,566 hrs · 52,599 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 750 TO BS 752, STR 21L & STR 24L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,566 hrs · 52,599 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 3 EA FUSELAGE SKIN CRACKS AT BS 500C + 5, STR 15R, BS 500D + 3, STR 16R & BS 520, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,526 hrs · 52,563 cycles

DURING PREFLIGHT CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 18L TO STR 19L. TEMP REPAIRED SKIN & MX FERRY TO PHX. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,023 hrs · 52,171 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, BETWEEN STR 23R TO STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,887 hrs · 51,261 cycles

DURING SCHEDULED C3 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS BETWEEN BS 747 AND BS 867, BETWEEN STRINGERS 21L AND 24L. REPAIRED SKIN SECTIONS PER EA AND SRM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 58,032 hrs · 50,606 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR NR 1 WEB BEAM CRACKED AT RIGHT CORNER. REMOVED AND REPLACED R1 DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,148 hrs · 49,898 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 727D + 5, STRINGER 21L AND BS 767, STRINGER 22L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,148 hrs · 49,898 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 727D + 5, STRINGER 19R AND BS 732, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM.

Part: TIE — CRACKED (FUSELAGE) · airframe 56,921 hrs · 49,714 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIES AT BS 706, STRINGER 1R, BS 787, STRINGER 10L, BS 847, STRINGER 14L, CRACKED. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,921 hrs · 49,714 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 663, BL 0, CRACKED. REPAIRED FLOORBEAM SECTION PER ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,916 hrs · 49,709 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME AT BS 727D, STRINGER 26R AND STRINGER 27R, CORRODED. REPAIRED FRAME PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 56,916 hrs · 49,709 cycles

DURING SCHEDULED 1/4D CHECK, FOUND MLG W/W BEADED PRESSURE WEB AT BS 663, LBL 40, CRACKED. REPAIRED WEB PER ER.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,916 hrs · 49,709 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICES AT STRINGER 4R, BS 360, AND BS 908, CRACKED. REMOVED AND REPLACED STRINGER SPLICES PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,916 hrs · 49,709 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB AT BS 1016, FROM STRINGER 6R TO STRINGER 6L, STRINGER 23R, CRACKED. REPAIRED WEB PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,916 hrs · 49,709 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BUTT STRAP AT BS 908, STRINGER 4R, CRACKED. REPAIRED STRAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,905 hrs · 49,700 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FRAME WEB AT BS 639, RT OVERWING EXIT DOOR, CRACKED. REPAIRED FRAME WEB PER ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,905 hrs · 49,700 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT BS 867, STRINGER 26 R, CORRODED. REPAIRED STRINGER PER SRM.

Part: TIE — CRACKED (FUSELAGE) · airframe 56,905 hrs · 49,700 cycles

DURING SPV, FOUND SHEAR TIES AT BS 360, STRINGER 14L AND STRINGER 14R, CRACKED. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,905 hrs · 49,700 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICE AT BS, 908, STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,761 hrs · 49,591 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STRINGER 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,761 hrs · 49,591 cycles

DURING SCHEDULED SERVICE CHECK, FOUND KEEL BEAM SKIN CRACKED AT LT WHEEL WELL. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,761 hrs · 49,591 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKS AT FOLLOWING LOCATIONS, BS 740, STRINGER 18R, BS 740, STRINGER 24L, BS 920, STRINGER 23R AND BS 930, STRINGER 25L. REPAIRED SKIN PER SRM.

Part: ACTUATOR — LEAKING (RT WING) · airframe 56,752 hrs · 49,581 cycles

DECLARED EMERGENCY, A SYSTEM HYDRAULIC FAILURE, COMPLETE LOSS OF A SYSTEM HYDRAULIC FLUID AT FL 280, COMPLIED WITH QRH. REMOVED AND REPLACED NR 3 FLIGHT SPOILER ACTUATOR PER MM.

Part: FLAP TRACK — WORN (LT WING) · airframe 56,645 hrs · 49,495 cycles

AIRFRAME VIBRATION WHEN FLAPS SELECTED TO 5 DEGREES. REPAIRED LT WING T/E INBOARD MIDFLAP TRACK PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,211 hrs · 49,164 cycles

DURING SCHEDULED C4 CHECK, FOUND 3 INCH LONG FUSELAGE SKIN CRACK AT BS 747, STR 18R. REPAIRED SKIN PER SRM.

Part: VALVE — LEAKING (HYD SYSTEM) · airframe 56,141 hrs · 49,110 cycles

AFTER TAKEOFF LOST A SYSTEM HYDRAULIC PRESSURE. RETURNED TO BNA FOR LANDING. REMOVED AND REPLACED MANUAL SHUTOFF VALVE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,315 hrs · 48,448 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 10R. REPAIRED SKIN PER SRM.

Part: FLASHLIGHT — WEAK (FWD CABIN) · airframe 55,297 hrs · 48,431 cycles

EMERGENCY FLASHLIGHT IN FWD CABIN WEAK. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,005 hrs · 48,193 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (3 EA) AT LOWER AFT CORNER OF AIRSTAIR CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,979 hrs · 48,172 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,979 hrs · 48,172 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 874, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,415 hrs · 47,697 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 10R, BS 460, BS 500C AND BS 500D. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,415 hrs · 47,697 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (4 EA) BS 294 AT STR 14L, BS 520 AT STR 12R, BS 787 AT STR 23L AND BS 807 AT STR 22L. REPAIRED SKIN PER SRM.

Part: SENSOR — FAILED (L/E FLAP) · airframe 53,644 hrs · 47,081 cycles

AIR TURNBACK, AFTER FLAP RETRACTION, NR 4 L/E FLAP TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 4 L/E FLAP RETRACT SENSOR PER MM. OPS CK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,497 hrs · 46,982 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 789, STR 25L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 53,497 hrs · 46,982 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,497 hrs · 46,982 cycles

DURING SCHEDULED BC1 CHECK, FOUND ONE LIGHT BULB INOP AT EACH CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHT. RELAMPED EACH CABIN DOOR EXIT LIGHT PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,429 hrs · 46,925 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED ( 2 EA ) AT BS 178, WL 235 AND BL 11, LT AND RT. REPAIRED BULKHEAD PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,429 hrs · 46,925 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 727D + 14 AT STR 22L AND BS 770 AT STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,316 hrs · 46,828 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 10R, BS 504 AND BS 500D + 8. REPAIRED SKIN PER SRM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 52,164 hrs · 45,886 cycles

DIVERSION, DURING FLIGHT R-1 COCKPIT WINDOW CRACKED. REMOVED AND REPLACED R-1 COCKPIT WINDOW AND CONTROLLER PER MM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 51,773 hrs · 45,556 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

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

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12L. REPAIRED SKIN PER SRM.

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

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACK AT BS 500D, STR 10L. REPAIRED SKIN PER SRM.

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

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKS (2 EA) AT STR 23L, BS 727E AND BS 747. REPAIRED SKIN PER SRM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 46,447 hrs · 40,832 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,002 hrs · 44,112 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED 1.5 INCHES LONG AT BS 727D+10, STR 19R. REPAIRED SKIN PER SRM..

Part: CABLE — MISROUTED (AFT ENTRY DOOR) · airframe 50,002 hrs · 44,112 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,988 hrs · 44,098 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 745, ABOVE STR 21L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,049 hrs · 43,364 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LENS — LOOSE (CABIN) · airframe 49,049 hrs · 43,364 cycles

DURING SCHEDULED C4 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,052 hrs · 43,320 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 360, BETWEEN STR'S 28L & 28R. REPAIRED SHEAR TIE PER SRM & BFG ER 01-0911.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,052 hrs · 43,320 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, BETWEEN STR 8R & 9R. REPAIRED FRAME PER BFG ER 01-0885.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,052 hrs · 43,320 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 987, RBL 21 TO RBL 44, WL 208. REPAIRED FLOORBEAM PER BFG ER 01-0891.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,052 hrs · 43,320 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 8L. R&R SHEAR TIE PER BFG ER 01-0908.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 49,052 hrs · 43,320 cycles

DURING SCHEDULED D-CHECK, FOUND RT KEEL BEAM CORRODED AT BS 540. REPAIRED KEEL BEAM PER BFG ER 01-0905.

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

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 1018, RBL 1 & WL 191. REPAIRED FRAME PER SRM.

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

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 847, RBL 2 & WL156. R&R SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,052 hrs · 43,320 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED ( 4 EA ) BETWEEN STR 8R & 9R, BS 440, 480, 827 & 887. REPAIRED FRAMES PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,052 hrs · 43,320 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED ( 7 EA ) BETWEEN STR 8L & 9L, BS 807, 827, 847, 867, 907, 887 & 480. REPAIRED FRAMES PER BFG ER.

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

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 1018, LBL 1 & WL 191. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,052 hrs · 43,320 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (4 EA) AT BS 597, STR 7L & STR 8R, BS 767, STR 10L, BS 706, STR 10L. REMOVED AND REPLACED STR CLIPS PER SRM.

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

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 987, RBL 51 & WL 199. R&R SHEAR TIE PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,052 hrs · 43,320 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 637, STR 17R. R&R WEB SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,052 hrs · 43,320 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

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

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 967, LBL 2 & WL 171. REPAIRED FRAME PER SRM.

Part: WEB — CORRODED (CORRODED) · airframe 46,387 hrs · 41,011 cycles

DURING SCHEDULED D CHECK, FOUND WEB CORRODED AT BS 296, RBL 50 & WL 208. REPAIRED WEB PER MM.

Part: WEB — CRACKED (MID CABIN) · airframe 49,052 hrs · 43,320 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 637, STR 17L. R&R WEB PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 49,052 hrs · 43,320 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,052 hrs · 43,320 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,079 hrs · 42,504 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 22R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 47,903 hrs · 42,360 cycles

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

Part: SKIN — DELAMINATED (L/E SLAT) · airframe 47,277 hrs · 41,855 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT SKIN DISBONDED. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,277 hrs · 41,855 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AND DOUBLER CRACKED AT FWD ENTRY DOOR LOWER AFT CUTOUT CORNER. REPAIRED SKIN AND DOUBLER PER SWA RA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 47,277 hrs · 41,855 cycles

DURING SCHEDULED C2 CHECK, FOUND 2.5 INCH LONG CRACK AT RT HORIZ STAB SKIN, BS 147.90, REAR SPAR. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,474 hrs · 41,223 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 4.5 EXTERNAL FUSELAGE SKIN CRACK AT BS 897, STR 24L. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,474 hrs · 41,223 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA. BS 178 BULKHEAD WEB CRACKS AT WL 230, LBL 17.1 & RBL 17.1. REPAIRED BULKHEAD PER SRM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 46,310 hrs · 41,077 cycles

DURING SCHEDULED C1 CHECK, FOUND NR 5 L/E SLAT SKIN CRACKED AT LOWER SURFACE, AFT RIVET ROW, OTBD DETENT CUTOUT. REPAIRED SLAT PER SRM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 46,310 hrs · 41,077 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 46,310 hrs · 41,077 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY WORN. R&R EVAC SLIDE ASSY PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 45,744 hrs · 40,619 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT WING OTBD T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,368 hrs · 40,296 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 727E, STR 25R, BS 727D, STR 25L AND BS 747, STR 26L. REPAIRED SKIN PER SRM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 44,950 hrs · 39,959 cycles

AIRFRAME VIBRATION FELT ABOVE 250 KNOTS. MX FERRY TO HOU AND FOUND LT ELEV I/B TAB HINGE BOLTS AND BUSHINGS WORN. REMOVED AND REPLACED LT ELEV TAB AND I/B ATTACH FITTING BUSHINGS AND BOLT PER MM.

Part: ACTUATOR — INOPERATIVE (RT MLG) · airframe 44,338 hrs · 39,435 cycles

RIGHT MLG HAD AN UNCOMMANDED EXTENSION DURING CLIMB. GEAR HANDLE PLACED IN UP POS AND GEAR REMAINED RETRACTED THROUGH OUT THE FLIGHT. REMOVED AND REPLACED RIGHT MLG UPLOCK ACTUATOR PER MM.

Part: SKIN — CRACKED (BS 747 & 757)

DURING SCHEDULED RON, FOUND FUSELAGE EXTERNAL SKIN HAS 2 EACH CRACKS, STRINGER 19R, BS 747 AND BS 757. REPAIRED SKIN PER SRM.

Part: LINE — RUPTURED (NLG)

AIR TURNBACK, NLG FAILED TO RETRACT DURING TAKEOFF. FOUND RUPTURED NLG DOWNLOCK ACTUATOR HYDRAULIC PRESS LINE. REMOVED AND REPLACED LINE PER MM.

Part: WEB — CRACKED (NLG)

DURING SCHEDULED RON, NLG WEB CRACKED INBD AFT RADIUS OF LT SIDE ACCESS PANEL. REMOVED AND REPLACED WEB ASSY PER TR NR T1-253-001.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, UT INSPECTION INDICATES 5 EACH CRACKS ON BS 178 BULK HEAD, RBL 5 - LBL 57. REPAIRED BULKHEAD PER SRM.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR UPPER HINGE FUSELGE SKIN CUT OUT CRACKED (VERIFIED WITH HFEC INSP). REPAIRED SKIN PER SRM.

Part: SLIDE — DAMAGED (PAX DOOR)

FWD ENTRY DOOR GIRT VELCRO TORN ON ESCAPE SLIDE ASSY. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: TAB — DELAMINATED (LT AILERON)

DURING SCHEDULED SERVICE CHECK, FOUND LEFT AILERON TAB DELAMINATED. REMOVED AND REPLACED TAB PER MM.

Part: SEAL — OUT OF POSITION (PAX DOOR)

FWD ENTRY DOOR DEVELOPED AN EXTREMELY LOUD AIR LEAK IN THE VICINITY OF UPPER HINGE. PRESSURIZATION REMAINED NORMAL. REPOSITIONED FWD ENTRY DOOR UPPER HINGE SEAL COVER (INTERIOR COVER) PER M/M, OPS CK'D OK.

Part: CONTROLLER — MALFUNCTIONED (CABIN)

LOSS OF PRESSURIZATION ON ARRIVAL INTO SEA AT 4000 AGL AFTER SLOW DESCENT. DESCENT INTO SEA WAS NORMAL WITH NORMAL CABIN INDICATIONS UNTIL 4000 AGL. REMOVED AND REPLACED CABIN PRESS CONTROLLER PER M/M.

Part: SKIN — CRACKED (BS 727-747)

DURING SCHEDULED SC CHECK, FOUND A 3 INCH CRACK IN FUSELAGE SKIN LOCATED SEC 46 BETWEEN BS 727E AND 747 AT STRINGER 18R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED SC CHECK, FOUND A 2 INCH LONGITUDINAL FUSELAGE SKIN CRACK, AT BS 727D, STRINGER 23R. REPAIRED PER BOEING SRM.

Part: CARD — FAILED (E/E BAY)

RETURNED TO TPA DUE TO AFTER GEAR RETRACTION NOSE WHEEL RED AND GREEN LIGHTS REMAINED ON WITH HANDLE UP. WITH HANDLE OFF NOSE WHEEL WAS GREEN, MAIN GEAR WENT NORMALLY UP AND LOCKED. REMOVED AND REPLACED M983 CARD, JACKED NOSE OF AIRCRAFT, CYCLED NOSE GEAR SEVERAL TIMES AND OPS CHECKED GOOD PER M/M.

Part: OIL SYST — REQD SERVICE (NR 1 ENGINE)

DIVERSION DUE TO NR 1 ENGINE OIL QUANTITY IS LOW, NEEDS SERVICING. AIRCRAFT MADE AN UNEVENTFUL LANDING. RAN NR 1 ENG. INSPECTED FOR OIL LEAKS, NO LEAKS NOTED. (LP 187371)

Part: WEB — DAMAGED (BS 950)

DURING SCHEDULED C3 CHECK, FOUND WEB DAMAGE JUST FWD OF AFT SERVICE DOOR FRAME AT BS 950. REPAIRED PER BOEING SRM.

Part: SEAL — FAILED (CARGO DOOR)

FLT LEVEL 350, CABIN ALT WARNING HORN SOUNDED WOULD NOT HOLD PRESSURE IN AUTO/STBY OR MANUAL WITH OUTFLOW VALVE SULL CLOSE, DESCENDED TO FLT LEVEL 240 AND STILL WOULD NOT HOLD CABIN PRESSURE. WENT TO HIGH ON PACKS, REGAINED PRESSURIZATION, PRESSURE WOULD HOLD WITH EITHER OR BOTH PACKS IN HIGH. MADE AN UNEVENTFUL LANDING. REPAIRED AFT CARGO DOOR SEAL PER BOEING SRM.

Part: SKIN — CRACKED (BS 727B)

DURING SCHEDULED SERVICE CHECK, FOUND A CRACK IN FUSELAGE SKIN AT BS 727B+16 BETWEEN S21 AND 22R. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED BC3 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT ROWS 7, 8 AND 9. REMOVED AND REPLACED BATTERY PACK PER BOEING M/M.

Part: FLOORBEAM — CRACKED (BS 1006)

DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM CRACKED ON UPPER FLANGE OF WEB .5 INCH AFT OF BS 1006, LBL 2.5. REPAIRED PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 295)

DURING SCHEDULED 1/2 D CHECK, FOUND STRINGER 22L SHEAR TIE CRACKED BS 295. REPLACED PER BOEING SRM.

Part: KEEL BEAM — CRACKED (LWR FUSELAGE)

DURING SCHEDULED BC4 CHECK, FOUND LOWER FUSELAGE KEEL BEAM FIXED PANEL CRACKED AT I/B RT ROW OF FASTENERS. REPAIRED PER SWA RA 1-A53-1273.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED A2 CHECK, FOUND OVERWING EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.