N309SW

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,658 hrs · 69,525 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER PAE ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,658 hrs · 69,525 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 25L TO 26L. REMOVED AND REPLACED TIE PER PAE ER.

Part: GLOWSTRIP — DELAMINATED (CABIN) · airframe 73,658 hrs · 69,525 cycles

DURING SCHEDULED SPV CHECK, FOUND PHOTOLUMINESCENT LIGHT STRIP DELAMINATED IN CABIN. REMOVED AND REPLACED STRIP PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO BAY SHEAR TIE CORRODED AT BS 747, STR 19R TO STR 20R. REPAIRED SHEAR TIE PER ER.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 20R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,657 hrs · 69,524 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360 BETWEEN STR 27L TO STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,657 hrs · 69,524 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 25L TO 26L. REPAIRED SHEAR TIE PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,657 hrs · 69,524 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 25L TO 26L. REPAIRED SHEAR TIE PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,657 hrs · 69,524 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,524 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 16, STR 8R. REPAIRED SKIN PER ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED CHECK, FOUND FUSELAGE FRAME U-CHANNEL CORRODED AT BS 540, STR 26L. REPAIRED FRAME CHANNEL PER ACO.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,656 hrs · 6,953 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 26R CORRODED AT BS 840. REPAIRED STRINGER PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 20R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 987, STR 20R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 25R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER — CORRODED (BS 360-365 S23R) · airframe 73,656 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 23R CORRODED BETWEEN BS 360 AND BS 365. REPAIRED STRINGER PER SRM.

Part: STRINGER SPLICE — CORRODED (BS 908 S25R) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 25R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER — CORRODED (BS 350 S25R) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 25R CORRODED AT BS 350. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (BS 540 S26L) · airframe 73,656 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 26L CORRODED AT BS 540. REPAIRED STRINGER PER ACO.

Part: STRINGER — CORRODED (BS 877 S24L) · airframe 73,656 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 24L CORRODED AT BS 877. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CORRODED (BS 887 S25R) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 887, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CORRODED (BS 360-372 S22R) · airframe 73,656 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 22R CORRODED BETWEEN BS 360 AND BS 372. REPAIRED STRINGER PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 503C S16L) · airframe 73,656 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 503C, STR 16L. REPAIRED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (BS 400 S19R) · airframe 73,656 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 400, STR 19R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (BS 727E S23L) · airframe 73,656 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 23L CORRODED AT BS 727E. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (BS 520 S12L) · airframe 73,656 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 12L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (BS 440-500 S26L) · airframe 73,656 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 26L CORRODED AT BS 440 TO BS 500. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: CHARGER — INOPERATIVE (CABIN) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FWD CABIN EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND RT AFT CABIN EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT BS 968, STR 27L. REPAIRED SKIN PER SRM AND BOEING DRAWING.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 22R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 947, STR 19R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 23L CORRODED AT BS 727E. REPAIRED STRINGER PER SRM.

Part: FLOOR SKIN — CRACKED (COCKPIT) · airframe 73,656 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND COCKPIT FLOOR SKIN CRACKED AT BS 248.8, RBL 25.5. REPAIRED FLOOR SKIN PER SRM & ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,656 hrs · 69,523 cycles

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

Part: STRINGER — CORRODED (BS 302 S28R) · airframe 73,656 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 28R CORRODED AT BS 302. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,656 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 14R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 460, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: TORQUE TUBE — CRACKED (AFT CARGO DOOR) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR TORQUE TUBE CRACKED. REMOVED AND REPLACED TORQUE TUBE PER BOEING DRAWING AND SRM.

Part: DOOR FRAME — CRACKED (AFT CARGO DOOR) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR FRAME CRACKED AT PULLEY BRACKET. REPAIRED PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 460, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 27R CORRODED AT BS 1006 TO BS 1016. REPAIRED STRINGER PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 503C, STR 16L. REPAIRED SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 17R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 380, STR 17R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (BS 929 S25L) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 25L CRACKED AT BS 929. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 291 S18R) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STUB FRAME CRACKED AT BS 291, STR 18R. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: SHEAR TIE — CRACKED (BS 987 S7L) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 987, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (BS 967 S7L) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500A S16L) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (BS 520 S16L) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (BS 500B S16R) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (BS 500A S9L) · airframe 73,657 hrs · 69,523 cycles

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

Part: FRAME — CRACKED (BS 663 S1-2R) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 1 AND STR 2R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10L. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C S8L) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7L. R&R STRINGER CLIP PER SRM.

Part: FLOORBEAM — CRACKED (BS 947) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 947, LBL 54. REPAIRED CHORD PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 8L. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 685 S10L) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (BS 400 S16R) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 16R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 8L. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727B S7L) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 9L. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7L. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S10L) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 16R. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, 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 807, STR 14R. 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 15R. 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 727D, STR 14R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727E S16R) · airframe 72,391 hrs · 67,767 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, 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 500D, STR 15L. REPAIRED 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 380, STR 14L. REPAIRED 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 480, STR 15L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500D S7R) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (BS 500C S7R) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 7R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727B S7R) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (BS 500C S9L) · airframe 73,657 hrs · 69,523 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 460, STR 16R TO STR 17R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 8R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 9L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 380, STR 15R. REPAIRED STR PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 2. REPAIRED FLOORBEAM PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 480, STR 17R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 24L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 480, STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 927, STR 23L TO STR 23R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503C, STR 8L. REPAIRED SKIN PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 19L. REMOVED AND REPAIRED STRINGER CLIP PER SRM.

Part: FLAP — DEBONDED (RT WING) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING INBOARD FORE FLAP DISBONDED AT OUTBOARD END. REPAIRED FLAP PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 24L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 19L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 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 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 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 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 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 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 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 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 4L. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 3L. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 968, RBL 28 TO RBL 45. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,657 hrs · 69,523 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,656 hrs · 69,523 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 7L CRACKED AT BS 1013. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,188 hrs · 69,196 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 910, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,188 hrs · 69,196 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,188 hrs · 69,196 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 400, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,188 hrs · 69,196 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 20L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,188 hrs · 69,196 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510B, STR 19R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,710 hrs · 69,183 cycles

DURING SCHEDULED MV4 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,959 hrs · 69,026 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 8L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,890 hrs · 68,697 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28R. REPAIRED SKIN PER SWA EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 72,890 hrs · 68,697 cycles

DURING SCHEDULED SPV CHECK, FOUND KEEL BEAM CORRODED AT BS 538, RBL 6.5. REPAIRED KEEL BEAM PER SRM.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 72,890 hrs · 68,697 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT DOOR HANDLE CUTOUT AFT UPPER CORNER. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,890 hrs · 68,697 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS BS 747C, STR 14L. REPAIRED SKIN PER SWA EA.

Part: SLAT — CRACKED (LT WING) · airframe 72,890 hrs · 68,697 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 3 L/E SLAT CRACKED AT LOWER OUTBOARD END. REPAIRED SLAT PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 72,890 hrs · 68,697 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT LOWER OUTBOARD END. REPAIRED SLAT PER SRM.

Part: SLAT — CRACKED (RT WING) · airframe 72,890 hrs · 68,697 cycles

DURING SCHEDULED SPV CHECK, FOUND RIGHT WING NR 4 L/E SLAT CRACKED AT LOWER OUTBOARD END. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,890 hrs · 68,697 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,890 hrs · 68,697 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 28R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 72,879 hrs · 68,959 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, STR 26L. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 72,879 hrs · 68,959 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 27L CORRODED AT BS 445. REPAIRED STRINGER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 72,879 hrs · 68,959 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 787, STR 27L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,879 hrs · 68,959 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, BL 0. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,879 hrs · 68,959 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR AFT FRAME CRACKED AT BS 847, STR 25R. REMOVED AND REPLACED FRAME PER ACO.

Part: WINDOW — ARCED (COCKPIT) · airframe 72,835 hrs · 68,931 cycles

FLIGHT DECK L1 WINDOW ARCED. REMOVED AND REPLACED WINDOW HEAT CONTROLLER AND WINDOW PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,695 hrs · 68,823 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510B, STR 15L. REPAIRED SKIN PER SWA EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 72,542 hrs · 68,702 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,494 hrs · 68,667 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733, STR 20L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,438 hrs · 68,621 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 20L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,001 hrs · 68,289 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 408, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,001 hrs · 68,289 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 416, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 750 S18L) · airframe 71,568 hrs · 67,964 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,557 hrs · 67,957 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,685 hrs · 67,263 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 395, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,685 hrs · 67,263 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, STR 16L. REPAIRED SKIN PER SWA EA.

Part: TIRE — SEPARATED (RT MLG) · airframe 70,595 hrs · 67,193 cycles

NR 4 MAIN TIRE LOST TREAD DURING TAKEOFF. REMOVED AND REPLACED NR 4 MAIN WHEEL AND TIRE ASSY PER MM. REPAIRED MID AND AFT FLAPS AND LANDING GEAR DOOR PER SRM.

Part: SKIN — CRACKED (BS 370 S17R) · airframe 42,987 hrs · 36,713 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 370, STR 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 730D S19R) · airframe 70,183 hrs · 66,870 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730D, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 514A S19R) · airframe 70,183 hrs · 66,870 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514A, STR 19R. REPAIRED SKIN PER SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 69,916 hrs · 66,654 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,477 hrs · 66,325 cycles

DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 6 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,115 hrs · 66,043 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 464, STR 26L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,115 hrs · 66,043 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,115 hrs · 66,043 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 365, STR 15R. REPAIRED SKIN PER SWA EA.

Part: CENTERING UNIT — WORN (ELEVATORS) · airframe 68,757 hrs · 65,751 cycles

WHEN MOVING YOKE FORE AND AFT ELEVATOR FEEL IS LOOSE. REMOVED AND REPLACED ELEVATOR FEEL AND CENTERING UNIT PER MM.

Part: FITTING — CORRODED (LT MLG) · airframe 68,178 hrs · 65,725 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG WALKING BEAM HANGER FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: FITTING — CORRODED (RT MLG) · airframe 68,178 hrs · 65,725 cycles

DURING SCHEDULED MV2 CHECK, FOUND RIGHT MLG WALKING BEAM HANGER FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 68,050 hrs · 65,214 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,026 hrs · 65,195 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 500C, STR 27L. REPAIRED SKIN PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 500D, STR 28L. REPAIRED SKIN PER SWA EA AND SRM.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FWD GIRT BAR FITTING PER MM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 68,024 hrs · 65,193 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506A, STR 16R. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 507B, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 372, STR 19R. REPAIRED SKIN PER SRM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT TAB NR 3 HINGE BUSHING PER MM.

Part: LENS — MISSING (CABIN) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING AT L1 DOOR. INSTALLED LIGHT LENS PER MM.

Part: HINGE — CRACKED (RT SPOILER) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 5 SPOILER, NR 3 HINGE CRACKED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 435, STR 16R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294.5, STR 11L. REPAIRED FRAME SECTION PER SRM.

Part: SHEAR TIE — CORRODED (BS 520 S27L) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (BS 300 S25R) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 25R CORRODED AT BS 380. REPAIRED STRINGER SECTION PER SRM.

Part: STRINGER — CORRODED (BS 967 S27L) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 27L CORRODED AT BS 967. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CORRODED (BS 500D S27L) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 294 S12L) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 395 S26L) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 395, STR 26L. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,024 hrs · 65,193 cycles

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

Part: SKIN — CRACKED (BS 765 S19L) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 765, STR 19L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (BS 639 S17R) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CORRODED (BS 500B S26L) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME WEB CORRODED AT BS 500B, STR 26L TO STR 26R. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S11L) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (BS 360 S10L) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED SHEAR TIE PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,024 hrs · 65,193 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,024 hrs · 65,193 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 27L. REPAIRED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD R1 DOOR SKIN CRACKED AT LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (BS 440 S16L) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 440, STR 16L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (BS 500 S27R-27L) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, STR 27R AND STR 27L. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 21L. REPAIRED FRAME PER SRM.

Part: FITTING — LOOSE (R2 GIRT BAR) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED EVAC SLIDE FITTING PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 68,024 hrs · 65,193 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED EVAC SLIDE FITTING PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 68,024 hrs · 65,193 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,493 hrs · 59,418 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: DRAG STRUT — CORRODED (LT MLG) · airframe 67,604 hrs · 64,856 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT MLG LOWER DRAG STRUT UPPER BORE CORRODED. REMOVED AND REPLACED LOWER DRAG STRUT PER MM.

Part: BOLT — CORRODED (LT MLG) · airframe 67,604 hrs · 64,856 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT MLG TRUNNION BOLT CORRODED. REMOVED AND REPLACED TRUNNION BOLT PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 67,477 hrs · 64,756 cycles

L1 DOOR EMERGENCY EXIT EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR SLIDE PER MM.

Part: SKIN — CRACKED (BS 513B) · airframe 66,616 hrs · 64,103 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513B, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 473) · airframe 66,616 hrs · 64,103 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 473, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 733D) · airframe 66,352 hrs · 63,904 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733D, STR 14L. REPAIRED SKIN PER SWA EA.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,352 hrs · 63,904 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 66,352 hrs · 63,903 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP ABOVE L1 DOOR. RESEATED LIGHT BULB. OPS CHECK GOOD PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,352 hrs · 63,903 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP ABOVE ROW 5 DEF. RESEATED LIGHT BULB. OPS CHECK GOOD PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,352 hrs · 63,903 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP ABOVE ROW 2 ABC. RESEATED LIGHT BULB. OPS CHECK GOOD PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 66,352 hrs · 63,903 cycles

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

Part: SHEAR TIE — CRACKED (BS 908) · airframe 66,352 hrs · 63,903 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 908, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (BS 780) · airframe 66,132 hrs · 63,725 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 18L. REPAIRED SKIN PER SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,132 hrs · 63,725 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (BS 727E) · airframe 66,132 hrs · 63,725 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 347) · airframe 66,132 hrs · 63,725 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 347, STR 2L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 727D) · airframe 66,132 hrs · 63,725 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 927) · airframe 66,132 hrs · 63,725 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 23R. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,721 hrs · 63,403 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY LIGHTS INOP AT FWD END. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (BS 505) · airframe 65,181 hrs · 62,975 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 492) · airframe 65,181 hrs · 62,975 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 492, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 941) · airframe 65,181 hrs · 62,975 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 21L. REPAIRED SKIN PER SWA EA.

Part: WHEEL — DEPARTED (RT MLG) · airframe 64,136 hrs · 62,132 cycles

NR 3 MLG TIRE/WHEEL ASSY DEPARTED THE AIRCRAFT ON LANDING ROLL. INSPECTED RT MLG FOR WHEEL BEARING FAILURE. NO DAMAGE NOTED. REMOVED AND REPLACED NR 3 MLG TIRE/WHEEL ASSY, BRAKE ASSY & TRANSDUCER PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 63,338 hrs · 61,493 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,338 hrs · 61,493 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 910, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,338 hrs · 61,493 cycles

DURING SCHEDULED C3 CHECK, FOUND OVERHEAD CENTER AISLE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,324 hrs · 61,486 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT R2 DOOR CUTOUT FWD LOWER CORNER, CRACKED. REPAIRED SKIN PER EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,998 hrs · 61,226 cycles

DURING SCHEDULED PM CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXTERIOR LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,358 hrs · 60,707 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 8L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,358 hrs · 60,707 cycles

DURING SCHEDULED C2 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 271, STR 15L AND STR 9L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,262 hrs · 60,623 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS AT BS 451, BS 486, BS 503, STRINGER 16R. REPAIRED SKIN SECTIONS PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,262 hrs · 60,623 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 500C + 13, BS 500D + 8, STRINGER 15L. REPAIRED SKIN SECTIONS PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,262 hrs · 60,623 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 749, STRINGER 19L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,831 hrs · 60,262 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,437 hrs · 59,928 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE FRAME AT BS 927, STRINGER 24L, CORRODED. REPAIRED FRAME SECTION PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 61,437 hrs · 59,928 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 61,196 hrs · 59,721 cycles

RIGHT R1 COCKPIT WINDOW ARCHED AT CRUISE AND DEVELOPED A CRACK, WINDOW HEAT SELECTED OFF, QRH PROCEDURE COMPLETED, WINDOW DEVELOPED MORE SMALL CRACKS ON OUTER PANE. REMOVED AND REPLACED R1 COCKPIT WINDOW PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,685 hrs · 59,315 cycles

FUSELAGE SKIN AT BS 500 D, STRINGER 15L, CRACKED. REPAIRED SKIN PER SRM.

Part: LIGHT — DISLODGED (EMERGENCY EXIT) · airframe 60,446 hrs · 59,115 cycles

EMERGENCY EXIT NOT ARMED LENS FELL OUT. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: ACTUATOR — INOPERATIVE (TE FLAPS) · airframe 60,404 hrs · 59,076 cycles

DIVERSION, ON FINAL APPROACH TO BUR T/E FLAPS WOULD NOT EXTEND PAST 5 DEGREES. T/E FLAPS WOULD NOT RETRACT, T/E FLAPS WOULD NOT RETRACT/EXTEND WITH ALT FLAP. REMOVED AND REPLACED HYDRAULIC FLAP DRIVE MOTOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,365 hrs · 59,043 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 807, STRINGER 15L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,347 hrs · 59,028 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 516, STRINGER 16L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — BULGED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN BULGED AT BS 727 + 13, STRINGER 27R. REPAIRED SKIN PER ER.

Part: FITTING — CORRODED (LT MLG) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND LT MLG STABILIZER FORWARD FITTING CORRODED. REMOVED AND REPLACED LT MLG FORWARD FITTING PER BAC DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES CRACKED AT BS 480, BS 827, BETWEEN STRINGER 8R AND STRINGER 9R, AND BS 807, BETWEEN STRINGER 8L AND STRINGER 9L. REPAIRED FRAME SECTIONS PER ER.

Part: WEB — CRACKED (LT WING) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND LT WING FSS 223, INBOARD OF FITTING (D) CRACKED AT WEB CHORD. REMOVED AND REPLACED WEB CHORD PER SRM AND ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 480, BETWEEN STRINGER 8L AND STRINGER 9L. REPAIRED FRAME SECTION PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT UPPER OUTBOARD CORNER OF THE NR 1 WINDOW. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED IN AFT CARGO COMPARTMENT AT BS 767, RBL 8. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAMS CRACKED AT BS 727B, RBL 25, WL 208 AND BS 727B, LBL 45, WL 208. REPAIRED BEAMS PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND INBOARD FRAME CHORD CRACKED AT BS 616, RBL 65, WL 204. REPAIRED FRAME CHORD PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND FRAMES CRACKED AT BS 867, BETWEEN STRINGERS 8L AND 9L, AND BS 907, BS 887, BS 867, BETWEEN STRINGERS 8R AND 9R. REPAIRED FRAMES PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 188, STRINGER 17R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND CORROSION ON WEB AT BS 1016, FWD SIDE OF BULKHEAD. REPAIRED WEB ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,060 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 277, RBL 55, WL 250 AND BS 277, RBL 55, WL 254. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER TIE CLIP AT BS 807 STRINGER 26 R, CORRODED. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 887 BETWEEN STRINGERS 20R AND STRINGER 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIES CORRODED AT AFT CARGO COMPT BS 767, BL 0, BS 807, LBL 17. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 616, STRINGER 5R AND BS 907, STRINGER 4R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 188, STRINGER 17L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND STIFFENER CORRODED IN MAIN WHEEL WELL, BS 663 TO BS 676, RBL 27. REMOVED AND REPLACED STIFFENER SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 328, BETWEEN STRINGERS 20R AND 21R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (E/E DOOR) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND E&E DOOR SKIN CRACKED NEAR AFT EDGE. REPAIRED DOOR SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT THE FOLLOWING BS 500D, STRINGER 8R, BS 520, STRINGER 8R, BS 578, STRINGER 8R, BS 597, STRINGERS 8R AND 7R, BS 616, STRINGERS 8R AND 8L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 277, STRINGER 16 L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 320, LBL 53, WL 181. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER END TIE CORRODED AT BS 365, STRINGER 28L. REPAIRED END TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STRINGER 5L. REMOVED AND REPLACED CRACKED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 5L CRACKED AT BS 380. REMOVED AND REPLACED CRACKED STRINGER PER SRM.

Part: PANEL — DAMAGED (ESCAPE ROPE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D-CHECK, FOUND FIRST OFFICERS EMERGENCY ESCAPE ROPE PANEL NOT OPENING. FOUND ROPE CAUGHT IN DOOR, REMOVED AND REPLACED ROPE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,066 hrs · 58,804 cycles

DURING SCHEDULED D-CHECK, FOUND CRACK IN EXTERNAL SKIN L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: CLIP — LOOSE (R1 DOOR) · airframe 59,623 hrs · 58,471 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVACUATION SLIDE GIRT BAR RESTRAIN CLIP LOOSE. SECURED CLIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,623 hrs · 58,471 cycles

DURING SCHEDULED C3 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS, BS 797, STR 7L AND BS 500A, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,869 hrs · 57,024 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 520, BETWEEN STR 15R AND STR 16R, STR 16L BETWEEN BS 474 AND BS 477. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,869 hrs · 57,024 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW CUTOUTS CRACKED AT RT WINDOWS NR 1, NR 4 AND NR 6. REPAIRED CUTOUT SKINS PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,869 hrs · 57,024 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED (2 EA) AT STR 11R, BS 390 AND BS 500A. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,939 hrs · 56,925 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACK (2 EA ) AT STR 15R, BS 500C & BS 500D. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,869 hrs · 57,024 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT STR 8L, BS 380 & BS 400. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,869 hrs · 57,024 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER TIE CLIP CRACKED AT BS 787, STR 9R. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 57,781 hrs · 56,958 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,496 hrs · 56,729 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 500A, BETWEEN STR 16R AND STR 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,963 hrs · 56,314 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,514 hrs · 55,961 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 420, STR 10L. REPAIRED SKIN PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,514 hrs · 55,961 cycles

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

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,514 hrs · 55,961 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,514 hrs · 55,961 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIPS CRACKED (3 EA) AT STR 4L AT BS 597 AND BS 616, STR 4R AT BS 559. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,066 hrs · 55,610 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,066 hrs · 55,610 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 10L, BS 383, BS 494 AND BS 500 PLUS 15. REPAIRED SKIN PER SRM AND SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,057 hrs · 55,604 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,001 hrs · 55,565 cycles

DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,897 hrs · 55,486 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 484, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,014 hrs · 54,766 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 395, STR 15L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,014 hrs · 54,766 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 16R, BS'S 444 AND 466. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,004 hrs · 54,757 cycles

DURING SCHEDULED C2 CHECK, FOUND FRAME CRACKED AT FWD SVC DOOR UPPER HINGE CUTOUT. REPAIRED FRAME PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,553 hrs · 54,387 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED 3 INCHES AT BS 545, STR 16R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 54,106 hrs · 54,045 cycles

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

Part: WINDOW — CRACKED (FWD SVC DOOR) · airframe 54,106 hrs · 54,045 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND VIEWING WINDOW CRACKED. REMOVED AND REPLACED WINDOW PER MM.

Part: MODULE — ERRATIC (NLG W/W) · airframe 53,987 hrs · 53,495 cycles

LOWERED GEAR HANDLE AND NOSE GEAR DID NOT DROP. CYCLED HANDLE AND NOSE GEAR DROPPED. REMOVED AND REPLACED NOSE GEAR MODULE PER MM.

Part: ACTUATOR — FAULTY (NLG W/W) · airframe 53,755 hrs · 53,757 cycles

DURING GEAR EXTENSION, NOSE GEAR LIGHT REMAINED RED, WARNING HORN SOUNDED. PLACED LEVER UP AND GEAR RETRACTED. PLACED LEVER DOWN, THREE GREEN LIGHTS AND NORMAL LANDING. REMOVED AND REPLACED NOSE GEAR UPLOCK ACTUATOR AND ADJUSTED RT NLG DOOR PER MM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 53,648 hrs · 53,680 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR EXTERNAL SKIN CRACKED ON AFT EDGE, 8 INCHES FROM TOP. REPAIRED SKIN PER SWA RA.

Part: SKIN — CRACKED (R1 DOOR) · airframe 53,648 hrs · 53,680 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SKIN CRACKED AT FWD SERVICE DOOR AROUND LOWER HINGE. REPAIRED SKIN PER SRM.

Part: ANGLE — CRACKED (FWD FUSELAGE) · airframe 53,648 hrs · 53,680 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL CHORD ANGLE CRACKED, LBL 5.7, WL 190. REPAIRED VERTICAL CHORD ANGLE SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 53,648 hrs · 53,680 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 28R CORRODED, BS 480. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 53,648 hrs · 53,680 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 26L CORRODED, BS 500A. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,648 hrs · 53,680 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CORRODED, BS 480, BETWEEN STRINGERS 27L AND 26L. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,648 hrs · 53,680 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED, BS 938, STRINGER 23R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,648 hrs · 53,680 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD RT SIDE CHORD CRACKED, WL 207. REMOVED AND REPLACED SIDE CHORD PER SWA ACO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,648 hrs · 53,680 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 860 AND BS 859, LBL 3, LONGITUDINAL BEAM CORRODED AT NUT PLATE HOLES. REPAIRED FLOORBEAM PER SWA RA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 53,648 hrs · 53,680 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT SIDE STRINGER 18A SHEAR BEAM CRACKED AT BS 706. REPAIRED SHEAR BEAM PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,648 hrs · 53,680 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS INOP AT ROWS 10 ABC AND 7 ABC. REMOVED AND REPLACED LIGHT ASSY'S PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 53,648 hrs · 53,680 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 180 VERTICAL WEB CRACKED, WL 183, LBL 17. REPAIRED WEB PER SRM.

Part: SLIDE — TORN (L2 DOOR) · airframe 53,648 hrs · 53,680 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE GIRT ASSY TORN. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,648 hrs · 53,680 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED, BS 933 TO BS 935, STRINGER 24R. REPAIRED SKIN PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 53,648 hrs · 53,680 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CORRODED AT VERTICAL LEG, BETWEEN BS 514-BS 520, STRINGER 28R. REPAIRED PER SWA RA.

Part: SKIN — CRACKED (MLG W/W) · airframe 53,189 hrs · 53,304 cycles

DURING SCHEDULED C4 CHECK, FOUND KEEL BEAM SKIN CRACKED 2 INCHES BETWEEN MLG W/W CUT OUTS RH SIDE. REPAIRED SKIN PER SWA T1-153-009.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,189 hrs · 53,304 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, ABOVE STR 11L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,189 hrs · 53,304 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED 2 INCHES AT BS 727E + 12, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,954 hrs · 53,101 cycles

DURING WALK AROUND INSPECTION FOUND FUSELAGE SKIN CRACKED 2.5 INCHES LONG AT BS 470, BETWEEN STR 15L & 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,641 hrs · 52,830 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED ( 5 LONG ) AT BS 947.6, STR 26L. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 52,470 hrs · 52,682 cycles

EEPLS LENS LOOSE IN FWD CABIN. SECURED EEPLS LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,373 hrs · 52,561 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED APPROX 3.35 LONG, BS 380, STR 10L. REPAIRED SKIN PER SWA RA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,159 hrs · 52,400 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (L/E FLAP) · airframe 51,431 hrs · 51,787 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING INBD FOREFLAP DELAMINATED ON UPPER SURFACE. R&R FOREFLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,431 hrs · 51,787 cycles

DURING SCHEDULED C2 CHECK, FOUND 5 LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 500D, ABOVE STR 10L. REPAIRED SKIN PER SRM.

Part: GUSSET — CRACKED (NLG) · airframe 50,629 hrs · 51,135 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NOSE LANDING GEAR MAIN ACTUATOR UPPER ATTACH POINT GUSSET CRACKED. REMOVED AND REPLACED GUSSET BRACKET PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,428 hrs · 50,960 cycles

DURING SCHEDULED C1 CHECK, FOUND .75 INCH EXTERNAL FUSELAGE SKIN CRACK AT AFT SVC DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,428 hrs · 50,960 cycles

DURING SCHEDULED C1 CHECK, FOUND 1 EXTERNAL FUSELAGE SKIN CRACK AT AFT ENTRY DOOR CUTOUT, UPPER AFT CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,428 hrs · 50,960 cycles

DURING SCHEDULED C1 CHECK, FOUND 3.0 EXTERNAL FUSELAGE SKIN CRACK AT BS 270, STR 16L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (AFT SVC DOOR) · airframe 50,420 hrs · 50,952 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR SIDEWALL EMERGENCY EXIT LIGHT BULBS INOP. REMOVED AND REPLACED BULBS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,428 hrs · 50,960 cycles

DURING SCHEDULED C1 CHECK, FOUND 2.0 EXTERNAL FUSELAGE SKIN CRACK AT BS 727E, BELOW STR 18R. REPAIRED SKIN PER SRM.

Part: SLIDE — DETACHED (SERVICE DOOR) · airframe 50,357 hrs · 50,890 cycles

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

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 49,879 hrs · 50,499 cycles

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

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 49,496 hrs · 50,145 cycles

DURING SCHEDULED C4 CHECK, FOUND .75 INCH CRACK ON RT HORIZONTAL STAB LWR SKIN SURFACE, 2 FWD OF BAL PNL 9208R. REPAIRED SKIN PER SRM.

Part: FAN — FAILED (A/C BAY) · airframe 48,885 hrs · 49,630 cycles

AIR TURNBACK, AFTER TAKEOFF MODERATE TO SEVERE VIBRATION NOTED. C/W ACFT VIBRATION CONDITION INSP, FOUND RT A/C PACK TURBO FAN FAILURE. REMOVED AND REPLACED SAME PER MM.

Part: SLIDE — DEPLOYED (PASSENGER DOOR)

FWD ENTRY DOOR EVACUATION SLIDE ACCIDENTALLY DEPLOYED. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: CHORD — CRACKED (CARGO DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND FWD CARGO DOOR NR 3 LOWER T-CHORD CRACKED. REMOVED AND REPLACED T-CHORD PER SRM.

Part: CHORD — CRACKED (CARGO DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR NR 2 LOWER T-CHORD CRACKED. REMOVED AND REPLACED T-CHORD PER SRM.

Part: SHEAR TIE — CRACKED (BS 400-440)

DURING SCHEDULED 1/2D CHECK, FOUND 4 EA SHEAR TIES CRACKED, BS 400 AND 440, STRINGER 14R, BS 460, STRINGER 14L, AND BS 360, STRINGER 13L. REPAIRED SHEAR TIES PER SRM.

Part: FLOORBEAM — CORRODED (FWD GALLEY)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM, BS 294.5, BL 0 - LBL 17. REPAIRED BEAM PER SRM.

Part: STRINGER — CORRODED (BS 785)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT STRINGER 26L, BS 785. REPAIRED STRINGER PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED BULKHEAD, BS 178, LBL 6.5. REPAIRED BULKHEAD PER SRM.

Part: KEEL BEAM — CORRODED (BS 520)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT KEEL BEAM, BS 520. REPAIRED BEAM PER SWA RA NR 1-353-2107 AND SRM.

Part: FRAME — CRACKED (BS 294)

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED STUB FRAME, BS 294, RBL 53. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM, BS 986 RBL 10-43. REPAIRED BEAM PER SWA RA NR 1-353-2103.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM, BS 312, AFT AND FWD FLANGES. REPAIRED BEAM PER SWA RA NR 1-353-2109.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT BS 328 FLOORBEAM, LBL 34. REPAIRED BEAM PER SWA RA NR 1-353-2108.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND 2 EA CRACKS, BS 178 BULKHEAD RBL 1 AND LBL1. REPAIRED BULKHEAD PER SRM.

Part: WEB — CRACKED (BS 663)

DURING SCHEDULED 1/2D CHECK, FOUND LT WHEEL WELL CEILING CRACKED, BS 663, LBL 30. REPAIRED WEB PER SWA RA NR1 -353-2104.

Part: PRESSURE BLKHD — CRACKED (NLG WW)

DURING SCHEDULED 1/2D CHECK, FOUND CRACK AT NOSE WHEEL WELL CEILING PRESSURE BULKHEAD AROUND AFT INBD ACCESS PANEL. REPAIRED PRESSURE BULKHEAD PER SWA RA NR 1-353-2106.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT BS 986 FLOORBEAM, LBL 29. REPAIRED BEAM PER SWA RA NR 1-353-2103.

Part: BRACKET — CORRODED (BS 312)

DURING SCHEDULED 1/2D CHECK, FOUND BS 312 FWD ENTRY DOOR FLOOR GIRT BAR BRACKET CORRODED. REMOVED AND REPLACED GIRT BAR FLOOR BRACKET.

Part: KEEL BEAM — CRACKED (BS 706)

DURING SCHEDULED 1/2D CHECK, FOUND KEEL BEAM LOWER SKIN CRACKED AT LT SIDE, BS 706. REPAIRED KEEL BEAM PER SRM.

Part: SKIN — CRACKED (BS 750)

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED, BS 750, STR 18R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY ESCAPE FLOOR TRACK LIGHT AT FRONT OF PAX CABIN INOP. REMOVED AND REPLACED BATTERY PACK AND GROUND WIRE SECTION PER MM.

Part: GIRT BAR — DETACHED (L1 DOOR)

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR AFT GIRT BAR HOOK NOT SECURED. RESECURED GIRT BAR HOOK PER MM.

Part: LIGHT — NOT SECURED (GALLEY)

DURING SCHEDULED C2 CHECK, FOUND EGRESS LIGHT NOT SECURED AT FWD GALLEY. SECURED EGRESS LIGHT PER MM.

Part: INDICATOR — OUT OF POSITION (R1 DOOR)

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVACUATION SLIDE PRESS INDICATOR NOT VISIBLE IN WINDOW. REPOSITIONED PRESS INDICATOR PER MM.

Part: SKIN — CRACKED (BS 867)

DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 867 AT S19R, 3 FT FWD OF CARGO DOOR UPPER SIDE, 3.25 LONG. REPAIRED PER BOEING SRM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED SC CHECK, AFT ENTRY EMERGENCY LIGHT INOP. RELAMPED PER BOEING M/M.

Part: FLOORBEAM — CRACKED (BS 660)

DURING SCHEDULED SPECIAL VISIT TO DLF, FOUND CENTER FLOORBEAM IN PAX CABIN CRACKED AT BS 660. REPAIRED PER SWA RA NR 1-357-0579.

Part: WIRE — BROKEN (NR 1 LE FLAP)

AIR TURNBACK DUE TO NR 1 KREUGER FLAP TRANSIT LIGHT LE FLAPS TRANSIT LIGHT ON WHEN FLAPS SELECTED UP RE-CYCLED, NO HELP. ALL INDICATIONS OK WHEN SELECTED DOWN. AIRCRAFT MADE AN UNEVENTFUL LANDING. FOUND GROUND WIRE TO NR 1 KREUGER FLAP BROKEN. INSTALLED NEW GROUND TERMINAL END PER BOEING MM. NO DEFECTS NOTED.

Part: SKIN — CRACKED (BS 911-913)

DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 911 TO 913 JUST BELOW S23L. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 235)

DURING SCHEDULED SERVICE CHECK, FOUND WEB CRACKED AT BS 235 AT TWO RIVETS JUST BEHIND CREW CALL HORN. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (ENTRY DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR UPPER FRAME CUTOUT CRACKED ON TOP SIDE. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR UPPER FRAME CUTOUT CRACKED ON TOP SIDE. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (ENTRY DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR LOWER FRAME CUTOUT CRACKED .25, RUNNING UNDER PRODUCTION SPLICE. REPAIRED PER SWA RA 1-353-1692.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND A PRESSURE BULKHEAD BS 178 CRACKED AT LBL 4.7, AT RBL 10.75 TO 11.75, AT RBL 6.7, RBL 4.7, RBL 1.5 TO 2.0, AND AT RBL 11.25 TO 11.75. REPAIRED PER TRAMCO EWO 97-007.

Part: HINGE SEAL — LEAKING (FWD ENTRY DOOR)

DURING CLIMBOUT, NOTED LOUD AIR SQUEAL FROM FWD ENTRY DOOR, LEVELED OFF AIRCRAFT AT 10,000 WITH CABIN PRESSURE CONTINUOUSLY CLIMBING. AIRCRAFT RETURNED TO RNO AND MADE AN UNEVETFUL LANDING. INSPECTED DOOR, RE-ADJUSTED UPPER HINGE SEAL PER BOEING M/M.

Part: WINDSHIELD — CRACKED (RT COCKPIT)

EN ROUTE FROM TUS TO SAN, FIRST OFFICER'S WINDSHIELD BEGAN ARCING, THEN CRACKED. AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING. REPLACED WINDOW ASSEMBLY AND HEAT CONTROLLER PER BOEING M/M.

Part: BEARING — FAILED (NR 3 MLG WHEEL)

ON TAKEOFF FROM LBB, NUMBER 3 MAIN GEAR WHEEL ASSEMBLY SEPARATED FROM BRAKE ASSEMBLY. AIRCRAFT MADE AN UNEVENTFUL LANDING AT ABQ. INSPECTED AND FOUND THE REASON FOR SEPARATION WAS DUE TO FAILED WHEEL BEARING. REPLACED NUMBER 3 AND 4 MAIN GEAR WHEEL ASSEMBLIES, NUMBER 3 BRAKE ASSEMBLY AND ANTI-SKID TRANSDUCER PER BOEING M/M.

Part: VERTICAL SUPPORT — DENTED (BS 500)

DURING SCHEDULED D CHECK, FOUND FORWARD FOUND VERTICAL SUPPORT WEB DENTED AT SIDEWALL SUPPORT PLATE ATTACH LOCATION BS 500+3, RBL 22.5, WL 156. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: CLIP — CRACKED (FUSELAGE)

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 927, S27R, AT BS 500A, S9R, AT BS 663, S10L, AT BS 663, S10R, AND AT BS 947, S25R. REPLACED ALL PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DENTED (FUSELAGE)

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTS AT: BS 916.5, 2 INCH ABOVE S25L, BS 807 TO 812, S27L TO 27R, AT BS 307, BETWEEN 21 AND 22R, AT BS 500A +6, BETWEEN S24 AND 24R, AT BS 311, BETWEEN S20 AND 21R, AT BS 1064, BETWEEN S20 AND 21R, AND FROM BS 849 TO 854, BL 0 TO RBL 15, WL 159. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: CLIP — BENT (BS 727B)

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP BENT AND GOUGED AT BS 727B, S26R. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CRACKED (NR 2 SLAT)

DURING SCHEDULED D CHECK, FOUND NUMBER 2 SLAT SKIN CRACKED ADJACENT TO EXISTING REPAIR. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND DRAWING 65C30133.

Part: STRINGER — CRACKED (BS 767)

DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 767, S11L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: STRINGER — CORRODED (BS 501)

DURING SCHEDULED D CHECK, FOUND STRINGER CORRODED AT BS 501, S28R. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: PRESSURE DECK — CRACKED (BS 665.75-672.75)

DURING SCHEDULED D CHECK, FOUND WING CENTER SECTION PRESSURE DECK WEB CRACKS AT BS 665.75, RBL 39.25, WL 202.5 AND AT BS 672.75, RBL 42.5, WL 202.5. REPAIRED PER TRAMCO EWO 95-0065.

Part: SPLICE — CRACKED (BS 360)

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, S4L. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SUPPORT — CRACKED (BS 540)

DURING SCHEDULED D CHECK, FOUND FLOOR BEAM SUPPORT CRACKED AT BS 540, WL 208, BL 0 TO LBL 25. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SPLICE — CRACKED (BS 360)

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, S14L. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — GOUGED (BS 957)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 957, AT S19R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOOR BEAM — CORRODED (BS 947)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM FASTENER HOLE CORRODED AT BS 947, WL 208, RBL 5. REPAIRED PER SWA EWO 95-0086.

Part: SUPPORT — CRACKED (BS 540)

DURING SCHEDULED D CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 540, BL 0 TO RBL 25. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOOR BEAM — CORRODED (BS 312)

DURING SCHEDULED D CHECK, FOUND FLOOR BEAM NUTPLATE HOLES CORRODED AT BS 312, LBL 11 TO RBL 11, WL 208. REPLACED DAMAGED SECTION PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FRAME — CRACKED (FWD CARGO DOOR)

DURING SCHEDULED D CHECK, FOUND FORWARD CARGO AFT DOOR FRAME CRACKED IN FORWARD TOP RADIUS ABOVE NUMBER 5 STOP FITTING. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FRAME — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED D CHECK, FOUND AFT SERVICE DOORWAY UPPER FORWARD FRAME CRACKED ON INBOARD RADIUS AT LATCH FITTING. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: ANGLE — CRACKED (BS 663)

DURING SCHEDULED D CHECK, FOUND PRESSURE WEB ANGLE CRACKED AT BS 663, RBL 65, WL 203. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DAMAGED (FUSELAGE)

DURING SCHEDULED D CHECK, FOUND LIGHTNING STRIKE DAMAGE AT THE FOLLOWING AREAS: BS 777, S9R, AT BS 727A+16 TO 18, S8R, AT BS 500D+1.5, S3R, AT BS 727E+10, S9R, AT BS 607.75, S5R, AT BS 441, S9L, AT 278.5, 3.75 INCH ABOVE S12L, AT BS 500A+11.25 AND +13.75, S6R, AT BS 748, S9R, AT BS 727E+1.25, S9R, AT BS 727C+7 TO 8, S9R, AT BS 749.5, S9R, AT BS 727A+2, S8R, AT BS 656, S5R, AT BS 582.5, S5R, AT BS 727C+1.25, S9R, AT BS 546.5, S5R, AT BS 500A+8, S8L, AT BS 540.5, S5R, AND AT BS 523.5, S5R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: STRINGER — CRACKED (BS 360)

DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 360, S15L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: VERTICAL BEAM — CRACKED (BS 747)

DURING SCHEDULED D-CHECK, FOUND VERTICAL BEAM STANCHION CRACKED AT BS 747+4, RBL 11, WL 161. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: ANGLE — CRACKED (BS 616)

DURING SCHEDULED D CHECK, FOUND 'L' ANGLE CRACKED AT BS 616, WL 200. REPAIRED PER TRAMCO EWO 95-0066.

Part: MOP SILL — CORRODED (BS 985)

DURING SCHEDULED D CHECK, FOUND AFT SERVICE DOOR MOP SILL CORRODED AT BS 985, WL 208, S17R. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FRAME — CRACKED (AFT PAX DOOR)

DURING SCHEDULED D CHECK, FOUND AFT ENTRY DOOR UPPER FORWARD FRAME CRACKED. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: KEEL BEAM — CORRODED (BS 500)

DURING SCHEDULED D CHECK, FOUND AC DISTRIBUTION BAY LEFT KEEL BEAM OUTBOARD FLANGE CORRODED AT BS 500D, WL 149, LBL 7. REPAIRED PER TRAMCO EWO 95-0073.

Part: FRAME — DENTED (BS 500)

DURING SCHEDULED D CHECK, FOUND FORWARD CARGO AFT DOOR FRAME DENTED IN TOP FLANGE OF FRAME, BS 500, RBL 45, WL 165.75. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DAMAGED (E/E DOOR)

DURING SCHEDULED D CHECK, FOUND E/E DOOR OUTER SKIN GOUGED AND NICKED. REPAIRED DAMGED AREAS PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CRACKED (BS 727-907)

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKS FROM BS 727 TO 907, S20 TO 25L AND R. REPLACED SKINS PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CRACKED (BS 327)

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 327, RBL 65, WL 210. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: VERTICAL BEAM — CRACKED (BS 727)

DURING SCHEDULED D CHECK, FOUND WEB BETWEEN VERTICAL STANCHION BEAMS CRACKED AT BS 727, LBL 12-15, WL 170. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: MOP SILL — CORRODED (SERVICE DOOR)

DURING SCHEDULED D CHECK, FOUND AFT SERVICE DOOR MOPSILL CORRODED. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — GOUGED (SERVICE DOOR)

DURING SCHEDULED D CHECK, FOUND FORWARD SERVICE DOOR OUTER SKIN GOUGED ON FORWARD EDGE ABOVE LOWER HINGE. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: STRESS PANEL — DAMAGED (BS 663-727)

DURING SCHEDULED D CHECK, FOUND KEEL BEAM STRESS PANEL DAMAGED AT BS 663-727, BL 0, WL 148. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.