N314SW

Part: FUSE — INOPERATIVE (MLG WW) · airframe 79,105 hrs · 72,869 cycles

NO L/E DEVICES DURING LANDING CONFIGURATION. REMOVED AND REPLACED BOTH L/E DEVICES HYD FUSES PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 79,013 hrs · 72,797 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 79,013 hrs · 72,797 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 78,966 hrs · 72,759 cycles

R1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED R1 WINDOW PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,620 hrs · 72,471 cycles

DURING SCHEDULED OTS CHECK, FOUND NOSE WHEEL WELL SKIN CRACKED AT BS 277. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,620 hrs · 72,471 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 948.5, STR 15L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 78,620 hrs · 72,471 cycles

DURING SCHEDULED HC1 CHECK, FOUND AFT CARGO DOOR FUSELAGE SKIN CRACKED AT BS 948.5, STR 15L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,627 hrs · 72,473 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (NLG WW) · airframe 78,092 hrs · 72,053 cycles

DURING SCHEDULED MV2 CHECK, FOUND NOSE WHEEL WELL LT FWD BULKHEAD PRESSURE DECK CRACKED. REPAIRED BULKHEAD PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,783 hrs · 71,816 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 960, STR 5R. REPAIRED SKIN PER SRM.

Part: WIRE — ARCED (COCKPIT WINDOW) · airframe 77,404 hrs · 71,541 cycles

R2 COCKPIT WINDOW INTERNAL WIRING ARCED. REMOVED AND REPLACED WINDOW PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 77,072 hrs · 71,280 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,975 hrs · 71,195 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 908.9, STR 4L. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 75,995 hrs · 70,403 cycles

R2 DOOR EVAC SLIDE PULL HANDLE OUT OF POSITION. REINSTALLED SLIDE PER MM.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 75,709 hrs · 70,210 cycles

AFTER TAKEOFF, RETRACTED GEAR, RT MLG RED LIGHT REMAINED ILLUMINATED. RECYCLED GEAR TO DOWN, ALL NORMAL WITH 3 GREEN, RETRACTED GEAR STILL WITH RT MLG RED LIGHT. GEAR DID RETRACT WITH GEAR HANDLE IN "OFF", RT MLG EXTENDED IN UP, ALL GEAR RETRACTED. REMOVED AND REPLACED RT MLG UP ACTUATOR PER MM.

Part: LENS — LOOSE (CABIN) · airframe 74,681 hrs · 69,419 cycles

DURING SCHEDULED 24Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 17. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,681 hrs · 69,419 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED BETWEEN BS 685 TO BS 706, STR 10L. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,681 hrs · 69,419 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 25. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,681 hrs · 69,419 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 24.8. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (BS 727B) · airframe 74,681 hrs · 69,419 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, AT LBL 45.5. REPAIRED BEAM PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,681 hrs · 69,419 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED BETWEEN BS 685 TO BS 706, STR 10L. REPAIRED SKIN PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 74,681 hrs · 69,419 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 3 SLAT I/B SIDE DELAMINATED. REPAIRED SLAT PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 74,681 hrs · 69,419 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING O/B LE NR 6 SLAT DELAMINATED. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,681 hrs · 69,419 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 20L. REMOVED AND REPLACED CLIP PER BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 74,681 hrs · 69,419 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CHORD CORRODED AT BS 727, STR 25L. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,681 hrs · 69,419 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 987, STR 27L. REPAIRED STRINGER PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 74,502 hrs · 69,290 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING O/B LEADING EDGE NR 5 SLAT AFT WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,502 hrs · 69,290 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 986, STR 20R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: RELAY — FAULTY (NLG) · airframe 7,194 hrs · 69,051 cycles

DECLARED EMERGENCY, NOSE GEAR UNSAFE INDICATION WHILE ON APPROACH TO HOU. RECYCLED NO CHANGE. EMERGENCY DECLARED, LANDING UNEVENTFUL. NO GEAR HORN. REMOVED AND REPLACED R374 RELAY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,140 hrs · 69,018 cycles

DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 16. REPAIRED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,140 hrs · 69,018 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 277, STR 14L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,140 hrs · 69,018 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 375, STR 15L. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,052 hrs · 68,951 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT BULL NOSE LIGHT INOP AT ROW 16. RELAMPED PER MM.

Part: SLIDE — UNSERVICEABLE (R1 DOOR) · airframe 72,832 hrs · 68,077 cycles

FOUND R1 DOOR ESCAPE SLIDE PRESSURE GAUGE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: ROD END — WORN (ELEVATOR TAB) · airframe 72,395 hrs · 67,768 cycles

DURING SCHEDULED CV CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR CONTROL ROD ENDS PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,397 hrs · 67,770 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR CUTOUT, BS 304, WL 234 TO WL 261. REPAIRED SKIN PER SRM & ER.

Part: FRAME — CRACKED (BS 500D S26R) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 26R. REPAIRED PER SRM & ER.

Part: SHEAR TIE — CRACKED (BS 277 S16R) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 16R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 14L. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED PAE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 259, STR 11R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED PAE CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 259 S11R) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 259, STR 11R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500D S22L) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 22L. R&R STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (BS 727 S21R) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 727, STR 21R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (BS 360 S23R) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 23R CORRODED AT BS 360. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 887 S21R) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 21R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 767 S13R) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 13R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 767 S14R) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 14R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 787 S13R) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 13R. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CRACKED (BS 767 S25R) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 767, STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 13R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 847, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 727B, STR 13L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 13R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 13R. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500A, STR 13R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 13R. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 767, STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500A, STR 13R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 727B, STR 13L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 460, STR 14L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 17L DAMAGED AT BS 360 TO BS 380. REPAIRED STR PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500B, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 13R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

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

Part: FRAME — CRACKED (BS 500C S15R) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 15R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 847 S13L) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 13L. REPAIRED FRAME PER ACO & EA.

Part: FRAME — CRACKED (BS 500C S8R) · airframe 72,391 hrs · 67,767 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 21R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 21L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 22R CRACKED AT BS 496. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 927, STR 24R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 23R CRACKED AT BS 359. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259.5, STR 24R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 9L AND STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 8R CRACKED AT BS 400. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 19L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 6L AND STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8L AND STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 13R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 15L. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259, STR 24L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER CRACKED AT BS 1016, NR 19 POSITION. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER CRACKED AT BS 1016, NR 16 POSITION. REMOVED AND REPLACED STIFFENER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 13R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 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 72,391 hrs · 67,767 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 14L CRACKED AT BS 727B. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,391 hrs · 67,767 cycles

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

Part: ISOLATOR — BROKEN (THRUST REVERSER) · airframe 72,354 hrs · 67,740 cycles

ABORTED TAKEOFF, NR 1 ENGINE STARTED TO SPOOL UP SLOWLY, HUNG UP AT 51% AND WOULD NOT ADVANCE. INSPECTED AND FOUND NR 1 ENGINE OUTBOARD FWD ISOLATOR END BROKEN. REMOVED AND REPLACED FWD T/R ISOLATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,024 hrs · 67,496 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 350, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,024 hrs · 67,495 cycles

FUSELAGE SKIN CRACKED AT BS 500, STR 21R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,712 hrs · 67,271 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 375, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,712 hrs · 67,271 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515D, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 71,712 hrs · 67,271 cycles

DURING SCHEDULED MV1 CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR LBL 16. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,712 hrs · 67,271 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, STR 13R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,712 hrs · 67,271 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,009 hrs · 66,728 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,009 hrs · 66,728 cycles

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

Part: FITTING — LOOSE (GIRT BAR) · airframe 71,009 hrs · 66,728 cycles

DURING SCHEDULED BRDG CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 71,009 hrs · 66,728 cycles

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

Part: LIGHT — CRACKED (CABIN) · airframe 71,009 hrs · 66,728 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 70,737 hrs · 66,528 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (BS 740A S26L) · airframe 70,737 hrs · 66,528 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 26L CORRODED AT BS 740A. REPAIRED STRINGER PER SRM.

Part: KEELBEAM — CORRODED (BS 707-727) · airframe 70,737 hrs · 66,528 cycles

DURING SCHEDULED SPV CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 707 AND BS 727. REMOVED AND REPLACED KEEL BEAM PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 70,737 hrs · 66,528 cycles

DURING SCHEDULED SPV CHECK, FOUND RIGHT NR 5 L/E SLAT DELAMINATED AT OUTBOARD T/E. REPAIRED SLAT PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,737 hrs · 66,528 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT LOWER DOOR STOP. REMOVED AND REPLACED FRAME PER ACO.

Part: SLAT — CRACKED (LT WING) · airframe 70,737 hrs · 66,528 cycles

DURING SCHEDULED SPV CHECK, FOUND LEFT WING NR 2 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 70,602 hrs · 66,437 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,127 hrs · 66,064 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 14L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 70,127 hrs · 66,064 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 490, STR 28R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,127 hrs · 66,064 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 791, STR 14R. REPAIRED SKIN PER SWA EA.

Part: BOLT — WORN (LT ELEVATOR TAB) · airframe 69,259 hrs · 65,388 cycles

DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. R&R NR 2 HINGE BUSHING AND BOLT PER SWA EA.

Part: BOLT — WORN (LT ELEVATOR TAB) · airframe 69,259 hrs · 65,388 cycles

DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. R&R NR 1 HINGE BUSHING AND BOLT PER SWA EA.

Part: BOLT — WORN (RT ELEVATOR TAB) · airframe 69,259 hrs · 65,388 cycles

DURING SCHEDULED 10Y CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. R&R NR 3 HINGE BUSHING AND BOLT PER SWA EA.

Part: BOLT — WORN (RT ELEVATOR TAB) · airframe 69,259 hrs · 65,388 cycles

DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. R&R NR 2 HINGE BUSHING AND BOLT PER SWA EA.

Part: BOLT — WORN (RT ELEVATOR TAB) · airframe 69,259 hrs · 65,388 cycles

DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. R&R NR 1 HINGE BUSHING AND BOLT PER SWA EA.

Part: BOLT — WORN (RT ELEVATOR TAB) · airframe 69,259 hrs · 65,388 cycles

DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. R&R NR 4 HINGE BUSHING AND BOLT PER SWA EA.

Part: BOLT — WORN (LT ELEVATOR TAB) · airframe 69,259 hrs · 65,388 cycles

DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. R&R NR 4 HINGE BUSHING AND BOLT PER SWA EA.

Part: SKIN — CRACKED (BS 264 S14R) · airframe 68,816 hrs · 65,053 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 264, STR 14R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 955 S24R) · airframe 68,816 hrs · 65,053 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 955, STR 24R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 767 S20L) · airframe 68,816 hrs · 65,053 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 20L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 727 S15R) · airframe 68,816 hrs · 65,053 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, STR 15R. REPAIRED SKIN PER SWA EA.

Part: HOOK — LOOSE (R2 DOOR) · airframe 68,243 hrs · 64,613 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED AFT GIRT BAR HOOK PER MM.

Part: BOLT — WORN (RT ELEVATOR) · airframe 67,911 hrs · 63,807 cycles

DURING SCHEDULED C2 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BOLT AND BUSHING PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,864 hrs · 63,561 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT BULL NOSE LIGHT INOP AT ROW 6 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,864 hrs · 63,561 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT BULL NOSE LIGHT INOP AT ROW 17 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: CONTROLLER — FAULTY (COCKPIT) · airframe 66,767 hrs · 63,491 cycles

L1 COCKPIT WINDOW SHATTERED AND ARCHED, REMOVED HEAT, ARCHING STOPPED. REMOVED AND REPLACED L1 WINDOW AND HEAT CONTROLLER PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 66,608 hrs · 63,356 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,985 hrs · 62,833 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 294, STR 11L TO STR 12L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 65,985 hrs · 62,833 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 5L TO STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER EA.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 65,827 hrs · 62,709 cycles

DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT BULL NOSE LIGHT LENS MISSING AT ROW 12 ABC. INSTALLED LIGHT LENS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,294 hrs · 62,268 cycles

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,283 hrs · 62,259 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (BS 410) · airframe 65,283 hrs · 62,259 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 410, BL 0, NR 2 RADIO ALTIMETER ANTENNA CUTOUT. MX FERRY TO DHN FOR REPAIRS. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 430) · airframe 65,283 hrs · 62,259 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 430, BL 0, NR 3 RADIO ALTIMETER ANTENNA CUTOUT. MX FERRY TO DHN FOR REPAIRS. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 912) · airframe 65,283 hrs · 62,259 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 912, STR 4R. MX FERRY TO DHN FOR REPAIRS. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 450) · airframe 65,283 hrs · 62,259 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 450, BL 0, NR 4 RADIO ALTIMETER ANTENNA CUTOUT. MX FERRY TO DHN FOR REPAIRS. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 747) · airframe 65,283 hrs · 62,259 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 19L. MX FERRY TO DHN FOR REPAIRS. REPAIRED SKIN PER SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,283 hrs · 62,259 cycles

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 8 DEF. RELAMPED LIGHT PER MM.

Part: STIFFENER — BULGED (AFT PRESS BLKHD) · airframe 65,283 hrs · 62,259 cycles

DURING SCHEDULED C4 CHECK, FOUND BS 1016 AFT PRESS BULKHEAD RADIAL STIFFENER BULGED AT STR 9R. MX FERRY TO DHN FOR REPAIRS. REPAIRED RADIAL STIFFENER PER SRM.

Part: SKIN — CRACKED (BS 390) · airframe 65,283 hrs · 62,259 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 390, BL 0, NR 1 RADIO ALTIMETER ANTENNA CUTOUT. MX FERRY TO DHN FOR REPAIRS. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 515D) · airframe 65,050 hrs · 62,092 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515D, STR 16R. MX FERRY TO DALLAS FOR REPAIRS. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 434) · airframe 64,783 hrs · 61,876 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 434, STR 16R. REPAIRED SKIN PER SWA EA.

Part: ATTACH BRACKET — LOOSE (GIRT BAR) · airframe 64,741 hrs · 61,847 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR BRACKET LOOSE. SECURED BRACKET PER MM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 64,712 hrs · 61,824 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 64,290 hrs · 61,508 cycles

DURING SCHEDULED C3 CHECK, LT & RT ELEVATOR TABS FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED LT & RT ELEVATOR TABS NR 1 HINGE BUSHINGS & HARDWARE PER MM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 64,290 hrs · 61,508 cycles

DURING SCHEDULED C3 CHECK, FOUND NR 2 L/E SLAT OUTBOARD LOWER SKIN CRACKED. REPAIRED SLAT PER SWA EA.

Part: SKI — DELAMINATED (RT WING SPOILER) · airframe 64,290 hrs · 61,508 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING NR 6 SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,342 hrs · 60,717 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE CRACKS AT BS 792 AND BS 812, STR 18L. REPAIRED SKIN PER SWA EA AND SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 63,309 hrs · 60,689 cycles

LT OVERWING EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,003 hrs · 60,461 cycles

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

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 63,003 hrs · 60,461 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FWD & AFT FAILSAFE CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,003 hrs · 60,461 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE STUB FRAMES CRACKED AT BS 188, LT & RT SIDE, WL 208. REMOVED AND REPLACED STUB FRAMES PER SRM.

Part: FLOOR PANEL — CRACKED (COCKPIT FLOOR) · airframe 63,003 hrs · 60,461 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FLOOR WEB CRACKS BETWEEN BS 188 TO BS 197, LT & RT SIDE, WL 208. REPAIRED FLOOR WEB PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,003 hrs · 60,461 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 727A, STR 14R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,003 hrs · 60,461 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 400, STR 14R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO BAY) · airframe 62,991 hrs · 60,456 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, LBL 17, WL 148. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO BAY) · airframe 62,991 hrs · 60,456 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 747, LBL 5 TO RBL 5, WL 148. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO BAY) · airframe 62,991 hrs · 60,456 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE SHEAR TIES CORRODED AT BS 827 & BS 847, RBL 5 TO BL 0, WL 149. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO BAY) · airframe 62,991 hrs · 60,456 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 747, RBL 16 TO RBL 20, WL 148. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO BAY) · airframe 62,991 hrs · 60,456 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 807, RBL 5 TO BL 0, WL 149. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO BAY) · airframe 62,991 hrs · 60,456 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 967, LBL 8, WL 148. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO BAY) · airframe 62,991 hrs · 60,456 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, BL 0 TO RBL 5, WL 148. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CORRODED (AFT CARGO BAY) · airframe 62,991 hrs · 60,456 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 907 + 3, STR 25R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CORRODED (AFT CARGO BAY) · airframe 62,991 hrs · 60,456 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 62,983 hrs · 60,449 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 967, STR 7L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 727E) · airframe 62,983 hrs · 60,449 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,983 hrs · 60,449 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 9L. REPAIRED FRAME PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 62,983 hrs · 60,449 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB ATTACH FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,983 hrs · 60,449 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,983 hrs · 60,449 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 947, STR 18L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,983 hrs · 60,449 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,983 hrs · 60,449 cycles

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

Part: WEDGE — CRACKED (RT WING SLAT) · airframe 62,983 hrs · 60,449 cycles

DURING SCHEDULED D-CHECK, FOUND RT WING NR 5 L/E SLAT T/E WEDGE CRACKED. REMOVED AND REPLACED SLAT ASSY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,983 hrs · 60,449 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 62,983 hrs · 60,449 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB ATTACH FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER SRM & BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,983 hrs · 60,449 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,983 hrs · 60,449 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 827, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FRAME CRACKS AT BS 400, STR 9L & STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FRAME CRACKS AT BS 480, STR 9L & STR 9R. REPAIRED FRAME PER SRM.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR WEB CRACKED AT BS 304, STR 4L. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500D, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 62,964 hrs · 60,433 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 9L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: PLATE — CORRODED (GIRT BAR) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR ATTACH AFT PLATE CORRODED AT BS 344, LBL 58. REMOVED AND REPLACED AFT PLATE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND BS 1016 PRESSURE BULKHEAD WEB CRACKED AT STR 15R. REPAIRED BS 1016 BULKHEAD WEB PER BFG ER.

Part: CREASE BEAM — CORRODED (CABIN FLOOR) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED BETWEEN BS 767 TO BS 787, RBL 65. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME INNER CHORD CRACKED AT BS 616, LBL 64, WL 201. REPAIRED FRAME INNER CHORD PER BOEING SB.

Part: CREASE BEAM — CORRODED (CABIN FLOOR) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED BETWEEN BS 727B TO BS 727C & BETWEEN BS 807 TO BS 827, RBL 70. REMOVED AND REPLACED CREASE BEAM WEB SECTIONS PER SRM.

Part: FLOOR SUPPORT — CRACKED (CABIN FLOOR) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727A + 18, RBL 45, WL 208. REPAIRED FLOORBEAM PER BFG ER.

Part: FLOOR SUPPORT — CRACKED (BS 706-707) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CRACKED AT BS 706 TO BS 707, LBL 25, WL 204. REPAIRED FLOOR SUPPORT PER BFG ER.

Part: STRINGER CLIP — CRACKED (BS 706) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2L, STR 9L & STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM UPPER CHORD CORRODED AT BS 294.5, BETWEEN LBL 7.5 & RBL 7.5. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (CABIN FLOOR) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM UPPER CHORD CORRODED AT BS 328, BETWEEN LBL 28 & RBL 49. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (BS 597) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, BETWEEN STR 8R & STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 578) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 9R, STR 7R & STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (CABIN FLOOR) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED AT BS 332 TO BS 344, RBL 63. REPAIRED WEB PER SRM.

Part: FLOORBEAM — CORRODED (CABIN FLOOR) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM UPPER CHORD CORRODED AT BS 312, BETWEEN RBL 8 & RBL 35. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (BS 639) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R & STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: PLATE — CORRODED (GIRT BAR) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR ATTACH AFT PLATE CORRODED AT BS 344, LBL 58. REMOVED AND REPLACED GIRT BAR ATTACH AFT PLATE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER BFG ER.

Part: FLOOR SUPPORT — CORRODED (COCKPIT FLOOR) · airframe 62,964 hrs · 60,433 cycles

DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOOR ZEE FITTING CORRODED AT BS 270, RBL 11 TO LBL 11, WL 208. REPAIRED ZEE FITTING PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 62,837 hrs · 60,335 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,446 hrs · 59,239 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 440, STRINGER 26L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,446 hrs · 59,239 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 17L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,808 hrs · 58,732 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 463 TO BS 466, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,808 hrs · 58,732 cycles

DURING SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 922, STRINGER 25L, CRACKED. REPAIRED SKIN PER EA, SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 60,538 hrs · 58,941 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT WING OUTBOARD AFT T/E FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,538 hrs · 58,491 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 484, STRINGER 26L, CRACKED. REPAIRED SKIN PER SRM.

Part: CABLE — DISCONNECTED (L2 DOOR GIRT BAR) · airframe 60,538 hrs · 58,491 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE DISCONNECTED. SECURED CABLE PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 60,149 hrs · 58,164 cycles

FWD SERVICE DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 60,017 hrs · 58,052 cycles

DURING SPV, FOUND BULKHEAD WEB AT BS 1016, BL 0, CORRODED. REPAIRED BULKHEAD WEB PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,008 hrs · 58,042 cycles

DURING SPV CHECK, FOUND FUSELAGE SKIN AT BS 790 TO BS 796, STRINGER 19L, CRACKED. REMOVED AND REPLACED SKIN SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,008 hrs · 58,042 cycles

DURING SPV, FOUND CHORD AT RT BS 178 ABOVE AND BELOW FLOOR, CRACKED. REMOVED AND REPLACED CHORD AT RT BS 178 PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,627 hrs · 57,753 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 980, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 59,627 hrs · 57,753 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: BEARING — BROKEN (RT MLG WHEEL) · airframe 59,343 hrs · 57,517 cycles

DURING TAXI, FELT MLG WHEEL VIBRATION AND NR 4 MLG TIRE/WHEEL ASSY WAS CANTED AT AN ANGLE. FOUND NR 4 MLG WHEEL RIM ASSY AND INNER BEARING RACE BROKEN APART. REMOVED AND REPLACED NR 3 AND NR 4 MLG TIRE/WHEEL ASSY'S AND NR 4 BRAKE ASSY PER MM.

Part: LIGHT — LOOSE (ROW 10 ABC) · airframe 59,289 hrs · 57,473 cycles

BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 10 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,020 hrs · 57,260 cycles

FUSELAGE SKIN CRACKED UNDER R1 DOOR BS 319, STRINGER 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,008 hrs · 57,250 cycles

DURING SCHEDULED PM CHECK, FOUND SKIN CRACKED AT BS 980, STRINGER 23 L. REPAIRED SKIN PER SRM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 58,067 hrs · 56,516 cycles

R1 DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,626 hrs · 56,174 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800, ABOVE STR 18L. REPAIRED SKIN PER SRM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 57,626 hrs · 56,174 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR ATTACH FITTINGS LOOSE. SECURED ATTACH FITTINGS PER MM.

Part: TIRE — FAILED (NLG) · airframe 56,878 hrs · 55,540 cycles

AIR TURNBACK, AT ROTATION FELT NOSE VIBRATION, HEARD MATERIAL IMPACTING FUSELAGE. FOUND, TREAD LOSS AT NR 1 NLG TIRE. REMOVED AND REPLACED BOTH NOSE TIRE AND WHEEL ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,728 hrs · 55,427 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 761, BELOW STR 18R. REPAIRED SKIN PER SRM.

Part: ROD END — WORN (LT ELEVATOR) · airframe 56,728 hrs · 55,427 cycles

DURING SCHEDULED C3 CHECK, SWA SI 11139-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB ROD END ASSY'S PER MM.

Part: SLIDE — DEPLOYED (SERVICE DOOR) · airframe 56,516 hrs · 55,248 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED WHEN OPENING DOOR. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,473 hrs · 55,211 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 1.75 INCH LONG FUSELAGE SKIN CRACK, BETWEEN BS 768 & BS 778, STRINGER 20R. REPAIRED SKIN PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 30,672 hrs · 27,119 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 663, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,182 hrs · 54,974 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (3 EA) BS 360 AT STR 5L, BS 616 AT STR 4L AND BS 639 AT STR 4L. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,182 hrs · 54,974 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,182 hrs · 54,974 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED AT BS 727B PLUS 19, STR 10R. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,182 hrs · 54,974 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT BS 663 AT STR 10R & BS 908 AT 4L. REMOVED AND REPLACED STR TIE CLIPS PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,182 hrs · 54,974 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICES CRACKED (2 EA) AT BS 908, STR 4R AND STR 10R. REMOVED AND REPLACED STRINGER SPLICES PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,182 hrs · 54,974 cycles

DURING SCHEDULED C3 CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BELOW STR 14R. REPAIRED SHEAR TIE PER SRM.

Part: TORQUE TUBE — BROKEN (LT WING T/E) · airframe 55,878 hrs · 54,738 cycles

DURING APPROACH, RT T/E FLAP POS IND WOULD NOT GO PAST 25 DEG'S. REMOVED AND REPLACED LEFT INBD T/E FLAP TORQUE TUBE PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 55,779 hrs · 54,661 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,747 hrs · 54,635 cycles

DURING SCHEDULED BC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,730 hrs · 54,621 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED 1 INCH LONG AT BS 500D, STRINGER 10L. REPAIRED SKIN PER SRM.

Part: ACTUATOR — CRACKED (RT WING) · airframe 54,984 hrs · 54,041 cycles

AFTER LANDING, DURING TAXIING, HYD A-SYS PRESS AND QTY IND WENT TO ZERO. REMOVED AND REPLACED NR 8 SPOILER ACTUATOR PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,816 hrs · 53,909 cycles

DURING SCHEDULED RON, FOUND AFT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 54,784 hrs · 53,885 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 54,784 hrs · 53,885 cycles

DURING SCHEDULED C1 CHECK, FOUND NLG UPPER SUPPORT ANGLE CRACKED JUST FWD OF A FRAME. REMOVED AND REPLACED SUPPORT ANGLE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,704 hrs · 53,818 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 14R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,704 hrs · 53,818 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 4R, BS 626, BS 578 AND BS 626. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,704 hrs · 53,818 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIPS CRACKED (2 EA) AT STR 4R, BS 597 AND BS 685. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 54,648 hrs · 53,767 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BELT FRAME CRACKED AT BS 500B, BETWEEN STR 20L AND STR 21L. REPAIRED BELT FRAME PER SRM.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 54,648 hrs · 53,766 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BELT FRAME CRACKED AT BS 500C, BETWEEN STR 20L AND STR 21L. REPAIRED BELT FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,648 hrs · 53,766 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT FUSELAGE SKIN CRACKED AT BS 520, UPPER WINDOW CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,648 hrs · 53,766 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 592, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,648 hrs · 53,766 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727 PLUS 14, ABOVE STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,648 hrs · 53,766 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C PLUS 5, STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,648 hrs · 53,766 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727 PLUS 14, ABOVE STR 4R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,648 hrs · 53,766 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,648 hrs · 53,766 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 494, STR 14L. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 54,648 hrs · 53,766 cycles

DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 20 DEF. SECURED LENS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 54,476 hrs · 53,623 cycles

RT OVERWING EMERGENCY EXIT LIGHT BROKEN. REPAIRED WIRING AND REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,112 hrs · 53,313 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,858 hrs · 53,095 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,858 hrs · 53,095 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 370, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,858 hrs · 53,095 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,858 hrs · 53,095 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 322, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,858 hrs · 53,095 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,967 hrs · 52,362 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 10R, BS 727C, BS 727B AND BS 500B. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,967 hrs · 52,362 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 10R, BS 500B AND BS 727. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,761 hrs · 52,186 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED .125 INCH LONG AT BS 178, WL 234 AND RBL 10. REPAIRED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,761 hrs · 52,186 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND HORIZONTAL WEBS CRACKED (2 EA) AT BS 180, WL 207, LBL 26.0 AND RBL 26.0. REMOVED AND REPLACED WEBS PER SRM.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 52,761 hrs · 52,186 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND LT ELEVATOR TAB HINGE CUTOUTS DELAMINATED. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,761 hrs · 52,186 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED 1.0 INCH LONG AT BS 180, WL 184 AND RBL 17.1. REPAIRED PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,758 hrs · 52,182 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED 1.0 INCH LONG AT BS 180, WL 184 AND RBL 17.1. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,758 hrs · 52,182 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED .3 INCH LONG AT BS 470, WL 190 RT. REPAIRED SKIN PER SRM..

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,701 hrs · 51,294 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 533B, STR 10L. REPAIRED STR PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 51,215 hrs · 50,857 cycles

DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BULLNOSE EMERGENCY LIGHT LENS LOOSE AT ROW 22 ABC. SECURED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,052 hrs · 50,687 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 300, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,025 hrs · 50,687 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, BETWEEN STR'S 14L &15L REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,025 hrs · 50,687 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,053 hrs · 47,205 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 EA CRACKS AT FUSELAGE SKIN, BS 500 & 500D, STR 12L REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 50,275 hrs · 50,041 cycles

DURING SCHEDULED C4 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL EXIT SIGN MISSING LENS. INSTALLED EMERGENCY EXIT SIGN LENS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,275 hrs · 50,041 cycles

DURING SCHEDULED BC4 CHECK, FOUND FUSELAGE SKIN CRACKED AT STR 10R, BS 727B AND BS 510. REPAIRED SKIN PER SRM.

Part: ACM — FAILED (A/C BAY) · airframe 49,787 hrs · 49,616 cycles

AIR TURNBACK, DECLARED EMERGENCY. SMOKE AND FUMES NOTICED IN CABIN AFTER TAKEOFF. REMOVED AND REPLACED LT AIR CYC MACHINE, RECIRC FAN (P/N 64505-1), COALESCER BAGS, AND HEPA FILTER PER MM. PERFORMED 5 MIN ENG POWER RUN AND PRESSURIZED ACFT, ALL SYS OPS CHECK GOOD PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,166 hrs · 49,079 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 4 EXTERNAL FUSELAGE SKIN CRACK AT BS 727A-B, STR 10R. REPAIRED SKIN PER RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,912 hrs · 48,847 cycles

DURING WALKAROUND INSPECTION, FOUND 4 EXTERNAL FUSELAGE SKIN CRACK AT BS 727D, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,342 hrs · 48,393 cycles

DURING SCHEDULED C2 CHECK, FOUND 2 EXTERNAL FUSLEAGE SKIN CRACK AT BS 727E, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,342 hrs · 48,393 cycles

DURING SCHEDULED C2 CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACK AT BS 967, STR 23R. REPAIRED SKIN PER SRM.

Part: WIRE — FAILED (BS 945)

ELECTRICAL SMELL IN CABIN. REPAIRED SHORTED WIRE AT BS 945 LEFT FOR THE PASSENGER WARNING SIGN INSIDE AFT WIND SCREEN. REMOVED AND REPLACED RECIRCULATION FILTER PER MM.

Part: WEB — CRACKED (BS 663)

DURING SCHEDULED 1/2D CHECK, FOUND BEADED PRESSURE WEB CRACKED, BS 663, RBL 38. REPAIRED WEB PER T-1-353-032.

Part: STRINGER — CORRODED (BS 320)

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 28L LOWER LEG CORRODED, BS 320. REPAIRED STRINGER PER SWA RA NR 1-353-2230.

Part: WEB — CRACKED (BS 230)

DURING SCHEDULED 1/2D CHECK, FOUND NOSE WHEEL WELL UPPER WEB CRACKED, BS 230, BL 0. REPAIRED WEB PER SRM.

Part: FRAME — CORRODED (BS 320)

DURING SCHEDULED 1/2D CHECK, FOUND BS 320 FRAME CORRODED, STRINGER 28L. REPAIRED FRAME PER RA NR 1-353-2230.

Part: SKIN — CRACKED (BS 940)

DURING SCHEDULED 1/2D CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED, BS 940, STRINGER 23R. REPAIRED FUSELAGE SKIN PER SRM.

Part: FRAME — CRACKED (SERVICE DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR 3RD LOWER FRAME CRACKED. REMOVED AND REPLACED DOOR ASSY PER MM.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED, BS 344, LBL 22 TO RBL 9. REPAIRED BEAM PER TI.

Part: BRACKET — CORRODED (GIRT BAR)

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT BAR FLOOR MOUNT BRACKET PADS CORRODED. REMOVED AND REPLACED PADS PER SRM.

Part: SKIN — CRACKED (BS 510)

DURING SCHEDULED C3 CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED, BS 510, ABOVE STRINGER 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 757)

DURING SCHEDULED C3 CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED, BS 757, ABOVE STRINGER 21R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 24 INCHES BELOW AFT ENTRY DOOR. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 929/943)

DURING SCHEDULED SC CHECK, FOUND AFT FUSELAGE SKIN CRACKED AT STA 929 AND 943, AT STRINGER 23L. CRACK MEASURES 2.70 AND 1.7 LONG. INSTALLED REPAIR PER SRM.

Part: SKIN — CRACKED (BS 500)

DURING SCHEDULED RON CHECK, FOUND 4 IN SKIN CRACKED AT RT SIDE ABOVE CABIN WINDOWS 11 AND 12 BS STA 500C STR 10R. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (CARGO DOOR)

DURING SCHEDULED C2 CHECK, FOUND AFT CARGO PIT DOOR INTERCOSTAL CRACKED. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING WALKAROUND CHECK, FOUND CRACKED SKIN APPROX 3 RT SIDE FWD OF REAR BAG BELOW OTHER PATCH. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C2 CHECK, FOUND A FUSELAGE SKIN CRACK AFT OF EQUIPMENT COOLING DUCT MEASURING 1.3 INCH LONG. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SV CHECK, FOUND 3 BULKHEAD EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: VALVE — MALFUNCTIONED (MLG WW)

ON GEAR EXTENSION, ANTI-SKID INOP LIGHT ILLUMINATED. AIRCRAFT RETURNED TO STL AND MADE AN UNEVENTFUL LANDING. REMOVED PARKING BRAKE VALVE AND OP CHECKED PER BOEING M/M.

Part: PCU — FAILED (RUDDER)

EXPERIENCED UNCOMMANDED YAW INPUT TO THE RIGHT DURING FLIGHT. DISENGAGING YAW DAMPER, NO HELP. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. REPLACED RUDDER PCU, YAW DAMPER COUPLER AND TEST FLEW PER BOEING M/M.

Part: BATTERY — DISCHARGED (BS 756)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT BS 756. REPLACED BATTERY PACK PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHT AT LEFT OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK PER BOEING M/M.

Part: STRINGER — CRACKED (BS 747)

DURING SCHEDULED CHECK, FOUND A 3 INCH CRACK AT S18R AT BS 747. REPAIRED PER BOEING SRM.

Part: FRAME — DENTED (BS 500)

DURING SCHEDULED D-CHECK, FOUND FWD CARGO COMPT FRAME DENTED AT BS 500 RBL 46 WL 169, BETWEEN S22 AND 23R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: DOORWAY FRAME — CRACKED (BS 294.5)

DURING SCHEDULED D-CHECK, FOUND FWD GALLEY DOORWAY LOWER FWD FRAME SECTION CRACKED AT LOWER I/B CORNER, BS 294.5 WL 208 RBL 55. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SPLICE — CRACKED (BS 908)

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908 S4R. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — GOUGED (BS 969)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 969, 2 INCHES ABOVE S19L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CRACKED (GALLEY DOOR)

DURING SCHEDULED D-CHECK, FOUND FWD GALLEY DOOR OUTER SKIN CRACKED ABOVE LOWER HINGE CUTOUT FWD CORNER, BS 300 WL 228 RBL 65. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: WEB — CRACKED (BS 360)

DURING SCHEDULED D-CHECK, FOUND HORIZONTAL WEB TIES CRACKED AT BS 360 LBL 61 WL 274 AND AT WL 253.5. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CRACKED (BS 344)

DURING SCHEDULED D-CHECK, FOUND FWD GALLEY DOORWAY LOWER AFT CORNER SKIN CRACKED AT BS 344 RBL 65 WL 211. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND BOEING DRAWING 65C27287-11.

Part: STRINGER — DAMAGED (BS 727)

DURING SCHEDULED D-CHECK, FOUND STRINGER DAMAGED AT BS 727 PLUS 11, S7R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: DOOR SILL — CORRODED (BS 277-360)

DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR MOPSILL CORRODED FROM BS 277 TO 360 WL 208. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FRAME — CRACKED (BS 277)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277 S16L WL 217. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: CLIP — CRACKED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 639 S1 S2L AND S2R, BS 616 S6L, BS 480 S8R, BS 727A S26L AND S25R, BS 500D S19R, BS 616 S2L, BS 616 S1 AND S5R, BS 887 S25R, BS 277 S15R, BS 663 S10L AND R, AND AT BS 520 S16L. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: ANGLE — CRACKED (BS 328)

DURING SCHEDULED D-CHECK, FOUND ATTACH ANGLE CRACKED AT BS 328 WL 174, BETWEEN S20 AMD 21L. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — GOUGED (BS 360-368)

DURING SCHEDULED D-CHECK, FOUND NUMEROUS SKIN GOUGES AT BS 360 TO 368, S4L TO 5L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DENTED (BS 998-1003)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED FROM BS 998 TO 1003, BETWEEN S13 AND 14L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.