N350SW

Part: SIGN — LOOSE (COCKPIT) · airframe 75,605 hrs · 65,939 cycles

EXIT SIGN OVERWING CAPT'S SIDE LOOSE. RE-SECURED SIGN CHECK GOOD PER M/M.

Part: WINDOW — ARCED (COCKPIT) · airframe 75,450 hrs · 65,837 cycles

DURING CRUISE AT FL380 CAPT LEFT WINDSHIELD L1 STARTED ARCING IN TOP LEFT AND RIGHT CONNECTIONS AND WINDOW LOST POWER 1 HEAT. WINDOW WAS SELECTED OFF AS PER QRH. REMOVED AND REPLACED L1 WINDOW AND WINDOW HEAT CONTROLLER PER MM.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 75,086 hrs · 65,572 cycles

RIGHT WING NR 7 SPOILER UPPER SURFACE DELAMINATED OUTBOARD CORNER. REMOVED AND REPLACED NR 7 FLIGHT SPOILER PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 75,086 hrs · 65,572 cycles

RIGHT WING NR 4 SLAT INBOARD TRAILING EDGE CORNER DELAMINATED. REMOVED AND REPLACED NR 4 SLAT PER AMM.

Part: COVER — LOOSE (CABIN) · airframe 74,524 hrs · 65,150 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 74,226 hrs · 64,917 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: COVER — OUT OF POSITION (CABIN) · airframe 74,144 hrs · 64,854 cycles

LEFT EEPLS COVER FELL OFF AT ROW 13. RE-INSTALLED COVER PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,112 hrs · 64,833 cycles

FRAME CRACKED AT BS 520, BETWEEN STR 20R AND STR 21R. REPAIRED FRAME PER SRM.

Part: PANEL — BROKEN (NR 4 SPOILER) · airframe 74,043 hrs · 64,782 cycles

LEFT WING NR 4 GROUND SPOILER OUTBOARD HINGE BROKEN. REMOVED AND REPLACED SPOILER PANEL IAW M/M.

Part: FLAP — DAMAGED (LT WING) · airframe 73,470 hrs · 64,342 cycles

LT WING O/B FORE FLAP DAMAGED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 72,711 hrs · 63,782 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 72,459 hrs · 63,593 cycles

L1 DOOR EMERGENCY EXIT SIGN COVER BROKEN. REPAIRED COVER PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,460 hrs · 62,822 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,295 hrs · 61,931 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 639, LBL 47. REPAIRED FRAME PER SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,295 hrs · 61,931 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 907, STR 4L. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,295 hrs · 61,931 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 14L. REPAIRED FRAME PER ER AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 70,295 hrs · 61,931 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CHORD LOWER CORRODED AT BS 227.8, BETWEEN BL 0 TO RBL 5. REPAIRED CHORD PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,295 hrs · 61,931 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 951, STR 10L. REPAIRED STRINGER PER ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,295 hrs · 61,931 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER SI AND ACO

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,295 hrs · 61,931 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 727A, STR 17L. REPAIRED FRAME PER ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,295 hrs · 61,931 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 16R. REPAIRED FRAME PER ER AND EA.

Part: HOUSING — BROKEN (EXIT SIGN) · airframe 70,295 hrs · 61,931 cycles

DURING SCHEDULED 22Y CHECK, FOUND MID CABIN EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN HOUSING PER SWPM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,295 hrs · 61,931 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 42. REMOVED AND REPLACED BEAM PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 70,295 hrs · 61,931 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,295 hrs · 61,931 cycles

DURING SCHEDULED 22Y CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHTS PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,295 hrs · 61,931 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED BETWEEN BS 375 TO BS 386, STR 2L. REPAIRED STRINGER PER ER AND EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,295 hrs · 61,931 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED BETWEEN BS 374 TO BS 386, STR 5L. REPAIRED STRINGER PER ER AND EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 70,295 hrs · 61,931 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN BULGED BETWEEN BS 954 TO BS 957, STR 20R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,295 hrs · 61,931 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 69,108 hrs · 61,026 cycles

R2 COCKPIT WINDOW ARCED AND CRACKED. REMOVED AND REPLACED WINDOW PER MM.

Part: LENS — BROKEN (CABIN) · airframe 69,079 hrs · 61,003 cycles

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

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 68,747 hrs · 60,750 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 68,556 hrs · 60,595 cycles

L1 DOOR EMERGENCY EXIT LIGHT LOWER LENS LOOSE. SECURED LENS PER MM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 68,297 hrs · 60,382 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING O/B FLIGHT SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,297 hrs · 60,382 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,297 hrs · 60,382 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 66,985 hrs · 59,413 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,006 hrs · 58,695 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL BUTT STRAP SKIN CRACKED BETWEEN BS 361 TO BS 362.2, STR 14R. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED BETWEEN BS 986 TO BS 1016, STR 23L. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 2R. REMOVED AND REPLACED SPLICE PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND BULKHEAD LOWER SUPPORT ANGLE CRACKED AT BS 947, STR 22L. REMOVED AND REPLACED ANGLE PER BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 400 TO BS 420. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 867, BETWEEN STR 8R TO STR 9R. REMOVED AND REPLACED FRAME SPLICE PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 400, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SECTION CORRODED BETWEEN BS 956 TO BS 1016, STR 22L. REPAIRED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 967, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — TORN (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE TORN AT BS 500D, BETWEEN STR 22R TO STR 23R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 887, STR 13L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 19L. REMOVE AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED BETWEEN BS 467 TO BS 471, STR 16R. REMOVED AND REPLACED STRINGER PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,908 hrs · 58,620 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CRACKED AT BS 986, STR 27R. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND RADIO ALTIMETER BELLY SKIN CUTOUT CRACKED AT BS 430. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND RADIO ALTIMETER BELLY SKIN CUTOUT CRACKED AT BS 410. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND RADIO ALTIMETER BELLY SKIN CUTOUT CRACKED AT BS 450. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 301.4, WL 238. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 28L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CORRODED BETWEEN BS 892 TO BS 902, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR THRESHOLD CORRODED BETWEEN BS 807 TO BS 847. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CHORD CORRODED AT BS 727B, BETWEEN STR 26L TO STR 27L. REPAIRED CHORD PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CRACKED AT BS 296, STR 10L. REPAIRED STRINGER PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 19L. REPAIRED FRAME PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BETWEEN BS 301 TO BS 304, BETWEEN WL 256.5 TO WL 262. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BETWEEN BS 290 TO BS 291, BETWEEN WL 230.5 TO WL 232.75. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BETWEEN BS 303 TO BS 304, WL 234. REPAIRED SKIN PER ER.

Part: RIB — CRACKED (RT WING) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING LOWER RIB CHORD CRACKED AT 135.5, BETWEEN STR 2 TO STR 3. REPAIRED RIB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT, BETWEEN BS 288 TO BS 289, BETWEEN WL 253 TO WL 259. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 28R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 25R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 887, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986, BETWEEN STR 24R TO STR 25R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,285 hrs · 58,175 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 727D +2, STR 19R. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (BS 747 S26-27L) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (BS 727B S26-27L) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND FAIL SAFE FRAME CHORD CORRODED AT BS 727B, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING I/B AFT FLAP UPPER SKIN DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: WEDGE — CORRODED (TE FLAP) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING I/B MID FLAP T/E WEDGE CORRODED ON LWR SKIN. REPAIRED WEDGE PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING O/B AFT FLAP T/E SKIN DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: RIB — CORRODED (FOREFLAP) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING I/B FORE FLAP O/B RIB CORRODED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING I/B FORE FLAP UPPER SKIN DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 21R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,251 hrs · 58,154 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 14R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,992 hrs · 57,971 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 473, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,112 hrs · 57,363 cycles

DURING SCHEDULED MV4 CHECK, FOUND SKIN CRACKED AT BS 438, STR 31L. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 63,928 hrs · 57,235 cycles

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

Part: HOUSING — DEFECTIVE (CABIN) · airframe 63,928 hrs · 57,235 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT AFT EMERGENCY EXIT LIGHT BATTERY PACK HOUSING INOP. REMOVED AND REPLACED HOUSING PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,670 hrs · 57,058 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD LAV EMERGENCY EXIT LIGHT INOP. REPLAMPED LIGHT PER WDM.

Part: LIGHT — BROKEN (CABIN) · airframe 63,196 hrs · 56,709 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,077 hrs · 56,619 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 526, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,077 hrs · 56,619 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 933, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 750 S18L) · airframe 62,877 hrs · 56,468 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,719 hrs · 56,342 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,719 hrs · 56,342 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,166 hrs · 55,967 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 420, STR 1. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,166 hrs · 55,967 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,166 hrs · 55,967 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 729D, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,077 hrs · 55,890 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 779, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,043 hrs · 55,869 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 540, STR 16R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 60,312 hrs · 54,572 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (L2 DOOR) · airframe 60,312 hrs · 54,572 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR SKIN CRACKED AT LOWER AFT CORNER. REPAIRED SKIN PER SRM.

Part: SIGN — MISSING (EMERGENCY EXIT) · airframe 59,991 hrs · 54,310 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 58,957 hrs · 53,490 cycles

DURING SCHEDULED MV3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FLOORBEAM — CRACKED (BS 665) · airframe 58,497 hrs · 53,155 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 665, BL 0. REPAIRED BEAM PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,497 hrs · 53,155 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 15R TO STR 16R. REPAIRED FRAME PER ER.

Part: STIFFENER — CRACKED (BS 1016) · airframe 58,497 hrs · 53,755 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT BS 1016, STR 4R. REPAIRED STIFFENER PER SRM.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 58,497 hrs · 53,755 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 10 O`CLOCK POSITION. REPAIRED WEB PER ER.

Part: FRAME — CRACKED (BS 188 S17L) · airframe 58,497 hrs · 53,755 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 188 S17R) · airframe 58,497 hrs · 53,755 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 380 S28L) · airframe 58,497 hrs · 53,755 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: KEELBEAM — CORRODED (BS 537) · airframe 58,497 hrs · 53,755 cycles

DURING SCHEDULED 18Y CHECK, FOUND RIGHT KEEL BEAM CORRODED AT BS 537, LBL 6. REPAIRED KEEL BEAM PER SRM.

Part: STIFFENER — CRACKED (BS 1016 S3R) · airframe 58,497 hrs · 53,755 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT BS 1016, STR 3R. REPAIRED STIFFENER PER SRM.

Part: SHEAR TIE — CORRODED (BS 380 S27L) · airframe 58,497 hrs · 53,755 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 380, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: KEELBEAM — CORRODED (BS 505D S28R) · airframe 58,497 hrs · 53,755 cycles

DURING SCHEDULED 18Y CHECK, FOUND RIGHT KEEL BEAM CORRODED AT BS 505D, STR 28R. REPAIRED KEEL BEAM PER SRM.

Part: CREASE BEAM — CORRODED (BS 816) · airframe 58,497 hrs · 53,155 cycles

DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 816, RBL 68. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: CREASE BEAM — CORRODED (BS 510) · airframe 58,497 hrs · 53,155 cycles

DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 510, LBL 68. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: FRAME — CRACKED (BS 440 S26R) · airframe 58,497 hrs · 53,155 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 26R. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 58,497 hrs · 53,155 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT LOWER OUTBOARD END. REPAIRED FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727D S7R) · airframe 58,497 hrs · 53,155 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 277 S10L) · airframe 58,497 hrs · 53,155 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727B S8R) · airframe 58,497 hrs · 53,155 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,497 hrs · 53,155 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,497 hrs · 53,155 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,497 hrs · 53,155 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 58,497 hrs · 53,155 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME PER SRM.

Part: ROD END — BROKEN (THROTTLE CONTROL) · airframe 57,642 hrs · 52,464 cycles

FOLLOWING NORMAL ENGINE START, NR 1 ENGINE FAILED TO RESPOND TO THROTTLE MOVEMENT. REMOVED AND REPLACED NR 1 ENGINE THROTTLE CONTROL BOX PER MM.

Part: SKIN — CRACKED (BS 500D S16R) · airframe 57,067 hrs · 52,017 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 57,067 hrs · 52,017 cycles

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

Part: PRESSURE PANEL — CRACKED (BS 251) · airframe 56,807 hrs · 51,819 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NLG W/W UPPER CEILING PANEL CUTOUT WEB CRACKED AT BS 251.6, LBL 7.75. REPAIRED WEB PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 56,777 hrs · 57,795 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: STRUCTURE — CRACKED (LT WING SPOILER) · airframe 55,898 hrs · 51,314 cycles

CREW REPORTED SLIGHT VIBRATION IN FLIGHT ON LT WING INBOARD GROUND SPOILER. REMOVED AND REPLACED LT INBOARD GROUND SPOILER PER MM.

Part: FRAME — CRACKED (BS 492 S24R) · airframe 55,476 hrs · 50,824 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, BS 492, STR 24R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (BS 491 S26R) · airframe 55,476 hrs · 50,824 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT FWD CARGO DOOR CUTOUT, BS 491, STR 26R. REPAIRED SKIN PER SWA EA.

Part: WINDOW — ARCED (COCKPIT) · airframe 55,406 hrs · 50,767 cycles

AIR TURNBACK/DECLARED EMERGENCY, L1 COCKPIT WINDOW ARCED & SHATTERED. REMOVED AND REPLACED L1 COCKPIT WINDOW & HEAT CONTROLLER PER MM.

Part: SKIN — CRACKED (BS 500C) · airframe 54,790 hrs · 50,314 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 14R. MX FERRY TO DAL. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,162 hrs · 49,828 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,162 hrs · 49,828 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,162 hrs · 49,828 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 18L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (727E) · airframe 53,891 hrs · 49,594 cycles

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

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 53,309 hrs · 49,109 cycles

DURING SCHEDULED C2 CHECK, FOUND NLG W/W RT SIDE WEB CRACKED AT BS 259, WL 174. REPAIRED WEB PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,920 hrs · 48,787 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 971, STR 21L. REPAIRED SKIN PER SWA EA & SRM.

Part: LENS — MISSING (CABIN) · airframe 52,798 hrs · 48,682 cycles

EMERGENCY BULLNOSE LIGHT LENS MISSING AT ROW 1 DEF. INSTALLED LENS ASSY PER MM.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 52,322 hrs · 48,306 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD EMERGENCY EXIT BULLNOSE LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY WIRE CONNECTORS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 52,116 hrs · 48,153 cycles

DURING SCHEDULED RON CHECK, FOUND FWD SECTION OF EEPLS STRIP LOOSE. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: STRUCTURE — DELAMINATED (T/E FLAP) · airframe 51,402 hrs · 47,593 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING T/E OUTBOARD AFT FLAP, DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 51,402 hrs · 47,593 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR HANDLE CUTOUT, LT UPPER CORNER SKIN, CRACKED. REPAIRED DOOR SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,402 hrs · 47,593 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 977, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA.

Part: FITTING — CORRODED (LT WING) · airframe 50,418 hrs · 46,836 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT MLG AFT INBOARD STABILIZER FITTING CORRODED. REMOVED AND REPLACED LT MLG STABILIZER FITTING PER MM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 50,165 hrs · 46,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE AT BS 908, STRINGER 4R, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,165 hrs · 46,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BUTTSTRAP AT BS 908, STRINGER 14L, CRACKED. REPAIRED BUTTSTRAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,165 hrs · 46,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 500D, STRINGER 12R, CRACKED. REPAIRED SKIN PER ERO.

Part: RIB — CRACKED (LT WING) · airframe 50,214 hrs · 46,662 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT WING LOWER RIB AT WBL 135.5, CRACKED. REPAIRED LT WING RIB CHORD PER SB, ERO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,214 hrs · 46,662 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT FWD SERVICE DOOR UPPER HINGE FITTING CASTING, CRACKED. REMOVED AND REPLACED FWD SERVICE DOOR HINGE FITTING PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,214 hrs · 46,662 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE AT BS 360, STRINGERS 14L, CRACKED. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,214 hrs · 46,662 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT CREASE BEAM AT BS 967 TO BS 983, CORRODED. REMOVED AND REPLACED CREASE BEAM PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,214 hrs · 46,662 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 13L AT BS 470, CRACKED. REPAIRED STRINGER SECTION PER ERO.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,205 hrs · 46,655 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE AT BS 420, STRINGER 15L, CRACKED. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,205 hrs · 46,655 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 15L AT BS 374, CRACKED. REPAIRED STRINGER SECTION PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 50,205 hrs · 46,655 cycles

DURING SCHEDULED 1/2D CHECK, FOUND R1 AND L1 DOOR EVAC SLIDES GIRT BAR FLOOR BRACKET FITTINGS CORRODED. REMOVED AND REPLACED FLOOR BRACKET FITTINGS PER MM.

Part: STRINGER CLIP — CRACKED (BS 400) · airframe 50,205 hrs · 46,655 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 400 TO BS 420, STRINGER 16L, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,205 hrs · 46,655 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 360, STRINGER 14R, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,176 hrs · 46,627 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 11R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,176 hrs · 46,627 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CABIN FLOORBEAMS CORRODED AT BS 344, LBL 9, BS 967, RBL 5, AND BS 986-987, LBL 26 TO LBL 35. REPAIRED FLOORBEAMS PER SRM AND ERO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,176 hrs · 46,627 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 967 FLOORBEAM CORRODED AT RBL 28, WL 208. REPAIRED FLOORBEAM PER ERO.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 50,176 hrs · 46,627 cycles

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

Part: FITTING — CORRODED (GIRT BAR) · airframe 50,176 hrs · 46,627 cycles

DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR FLOOR MOUNT FITTING PLATES CORRODED. REMOVED AND REPLACED FITTING PLATES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,176 hrs · 46,627 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 11L, (R2 DOOR UPPER HINGE CUTOUT). REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,176 hrs · 46,627 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 380, STRINGER 15L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 50,176 hrs · 46,627 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT 5 DEF. RELAMPED PER MM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 50,165 hrs · 46,617 cycles

STRINGER SPLICE AT BS 360, STRINGER 5L, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,165 hrs · 46,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE AT BS 550B, STRINGER 16L, CRACKED. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,165 hrs · 46,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM AT BS 298, AT BS 328, CORRODED. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM.

Part: BEAM — CORRODED (CABIN FLOOR) · airframe 50,165 hrs · 46,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR BEAM CORRODED FROM BS 616 TO BS 639, STR 17R. REPAIRED BEAM PER ERO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,165 hrs · 46,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CHANNEL CRACKED AT BS 540, LBL 1, WL 208. REMOVED AND REPLACED CHANNEL SECTION PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 50,165 hrs · 46,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN STRAPS CORRODED AT BS 793 AND BS 847, STR 24R. REPAIRED SKIN STRAPS PER SRM.

Part: STRINGER CLIP — CRACKED (BS 747) · airframe 50,165 hrs · 46,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 23L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,165 hrs · 46,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 294, STRINGER 16R, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,165 hrs · 46,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME WEB AT BS 294, STRINGER 11R, CRACKED. REMOVED AND REPLACED FRAME WEB SECTION PER SRM.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 50,165 hrs · 46,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT EMERGENCY EXIT LIGHT LENS FADED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,165 hrs · 46,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT CREASE BEAM AT BS 727B +2 TO BS 727B + 12, CORRODED. REPAIRED CREASE BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 50,165 hrs · 46,617 cycles

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

Part: LENS — MISSING (CABIN) · airframe 49,901 hrs · 46,409 cycles

FORWARD RIGHT EMERGENCY EXIT LIGHT LENS, MISSING. REPLACED LIGHT LENS PER MM.

Part: LINKAGE — WORN (ELEVATOR TAB) · airframe 48,003 hrs · 44,901 cycles

DURING SCHEDULED SERVICE CHECK, RT ELEVATOR TAB FAILED FREEPLAY CHECK. REMOVED AND REPLACED RT ELEV TAB NR 1 HINGE ATTACH HARWARE, AND TAB LOCKOUT MECHANISM LINKAGE PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,672 hrs · 44,620 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 240 AND LBL 10. REPAIRED BULKHEAD WEB PER SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 46,798 hrs · 43,924 cycles

DURING SCHEDULED A2 CHECK, FOUND FWD SVC DOOR VERTICAL EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 45,703 hrs · 43,047 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 5 L/E SLAT DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED NR 5 L/E SLAT PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 45,703 hrs · 43,047 cycles

DURING SCHEDULED C2 CHECK, FOUND LT INBOARD AFT T/E FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED INBOARD AFT T/E FLAP PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 45,703 hrs · 43,047 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT DELAMINATED AT BOTH ENDS. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.

Part: BRACKET — OUT OF ADJUST (SERVICE DOOR) · airframe 45,703 hrs · 43,047 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE RETAINING BRACKET OUT OF ADJUST. ADJUSTED BRACKET PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,703 hrs · 43,047 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.6, JUST ABOVE STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,777 hrs · 42,306 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SERVICE DOOR FUSELAGE SKIN CUTOUT CRACKED AT LOWER AFT CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,307 hrs · 41,097 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 759, BELOW STR 19R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (FWD CABIN DOORS) · airframe 42,139 hrs · 40,146 cycles

DURING SCHEDULED C2 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT BAR ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: WEB — CRACKED (RT MLG W/W) · airframe 41,771 hrs · 39,850 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 663, RBL 41. REPAIRED WEB PER SRM AND SWA T1.

Part: LIGHT — LOOSE (CABIN) · airframe 41,771 hrs · 39,850 cycles

DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 12 DEF. SECURED LIGHT PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,771 hrs · 39,850 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VHF ANTENNA BLANKING PLATE CORRODED AT BS 727D TO 727E, BL O. REPAIRED SKIN PER SWA RA AND SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 41,771 hrs · 39,850 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 663, LBL 33. REPAIRED WEB PER SWA RA.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 40,906 hrs · 39,136 cycles

EMERGENCY FLASHLIGHT INOP IN FWD CABIN. RESEATED FLASHLIGHT PER MM, OPS CK GOOD.

Part: WEB — CRACKED (FUSELAGE) · airframe 40,553 hrs · 38,826 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEBS CRACKED ( 9 EA ) AT BS 178, LBL 20-RBL 28. REPAIRED WEBS PER SRM.

Part: BUSHING — WORN (RH ELEVATOR) · airframe 40,256 hrs · 38,578 cycles

DURING SCHEDULED BC4 CHECK, FOUND RH ELEVATOR TAB INBD HINGE BUSHING WORN. R&R HINGE BUSHING PER MM.

Part: CONTROLLER — INOPERATIVE (NR 1 ENGINE) · airframe 36,009 hrs · 34,998 cycles

ABORTED TAKEOFF. NR 1 ENG PMC INOP. ENG LIGHT ILLUMINATED, PULLED THROTTLES BACK AT ABOUT 20 KNOTS. OK TO CONTINUE PER MEL 73-7, LATER IN HOU REMOVED AND REPLACED NR 1 ENG PMC PER MM.

Part: SKIN — CRACKED (RT HORZ STAB)

DURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED, STA 157.10 AT REAR SPAR. REPAIRED SKIN PER ER NR 99-5774.

Part: FRAME — CRACKED (BS 480 & 500)

DURING SCHEDULED D CHECK, FOUND CRACKED FUSELAGE FRAMES, BS 500C ,STR 8L-9L AND STR 8R-9R, BS 500A, STR 8L-9L, BS 480, STR 8R-9R. REPAIRED FRAMES PER ER NR 99-5734.

Part: FRAME — CRACKED (BS 907, 864, 827)

DURING SCHEDULED D CHECK, FOUND CRACKED FUSELAGE FRAMES, BS 907, STR 8L-9L , BS867, STR 8R-9R, BS 827, STR 8R-9R. REPAIRED FRAMES PER ER NR.

Part: LIGHT — INOP (CABIN)

DURING SCHEDULED D CHECK, FOUND EMERGENCY AISLE OVERHEAD LIGHT INOP, BS 790. REMOVED AND REPLACED FUSE IN POWER SUPPLY PER MM

Part: KEEL BEAM — CORRODED (BS 722.8)

DURING SCHEDULED D CHECK, FOUND CORROSION AT NUTPLATE HOLE ON KEEL BEAM, BS 722.8, RBL 6.5. REPAIRED KEEL BEAM PER ER NR 99-5733.

Part: FRAME — CRACKED (FUSELAGE)

DURING SCHEDULED D CHECK, FOUND 6 EACH CRACKS ON FUSELAGE FRAMES BS 827 BETWEEN STRINGERS 8L-9L, BS 787 BETWEEN STRINGERS 8L-9L, BS 867 BETWEEN STRINGERS 8L-9L, BS 747, BETWEEN STRINGERS 8R-9R, BS 727D, BETWEEN STRINGERS 8R-9R AND BS 727B, BETWEEN STRINGERS 8R-9R. REPAIRED FRAMES PER ER 99-5734.

Part: FRAME — CRACKED (BS 400 & 440)

DURING SCHEDULED D CHECK, FOUND 4 EACH CRACKS ON FUSELAGE FRAMES, BS 400 BETWEEN STRINGERS 8L-9L AND 8R-9R AND BS 440 BETWEEN STRINGERS 8L-9L AND 8R-9R. REPAIRED FRAMES PER ER 99-5734.

Part: SWITCH — INOP (CABIN)

DURING SCHEDULED D CHECK, FOUND AFT ATTENDANT EMERGENCY LIGHTS PANEL SWITCH INOP. REMOVED AND REPLACED SWITCH PER MM, AND WDM.

Part: LENS — CRACKED (RT EMER EXIT)

DURING SCHEDULED D CHECK, FOUND RT EMERGENCY EGRESS LIGHT LENS CRACKED, BS 727 PLUS 10. REMOVED AND REPLACED LENS PER MM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED D CHECK, FOUND CORROSION AT FLOORBEAM UPPER FACE, BS 986, RBL 43 - LBL 43. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (BS 616)

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT LOWER INBOARD FASTENER HOLE, BS 616, LBL64, WL 200. REPAIRED FRAME PER ER NR 99-5743.

Part: WEB — CORRODED (BS 636-639)

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED, BS 636-639, RT SIDE. REPAIRED WEB SECTION PER SRM.

Part: SPLICE — CRACKED (BS 907)

DURING SCHEDULED D-CHECK, FOUND 2 STRINGER SPLICES CRACKED, BS 907, STRINGERS 4L AND 4R. REMOVED AND REPLACED STRINGER SPLICES PER SRM.

Part: FLOORBEAM — CORRODED (BS 967)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOORBEAM, BS 967, RBL 42. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOORBEAM UPPER SURFACE, BS 328, RBL 28- RBL 35. REPAIRED BEAM PER SRM.

Part: LIGHT — DAMAGED (ROW 9)

EMERGENCY ESCAPE LIGHT AT BULLNOSE PUSHED THRU, ROW 9. RESECURED LIGHT PER MM.

Part: SLIDE — LOW PRESS (AFT RT DOOR)

DURING WALKAROUND CHECK, FOUND AFT RIGHT DOOR SLIDE PRESS LOW. REPLACED PER BOEING M/M.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED UNDER STRAP AT RBL 6.7, WL 211.5 TO 212.75. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED UNDER STRAP AT RBL 4.7, WL 198.75 TO 199.75, AND AT WL 201.5 TO 202.5. REPAIRED PER BOEING SRM.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN)

AT 37,000, CABIN ALTITUDE ALERT WARNING SOUNDED. SWITCHING TO MAN OR STANDBY MODES, NO HELP. DESCENDED TO LEVEL WHERE PRESSURE WAS REGAINED. LANDED WITHOUT INCIDENT. FWD OUTFLOW VALVE FAILED TEST. REPLACED VALVE AND SYSTEM CHECKED OK PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED TERM CHECK, FOUND AFT CENTER CEILING EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY AND OPS CHECKED PER BOEING M/M.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND AFT CEILING EMERGENCY EXIT LIGHT SIGN INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: SKIN — CRACKED (RT HORZ STAB)

DURING SCHEDULED BC3 CHECK, FOUND CRACK AT RT HORZ STAB AT RIB STA 120.3 AND 129.5 ON AFT SPAR ON RT LOWER IN SPAR. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (RT HORZI STAB)

DURING SCHEDULED 1/4 D-CHECK, FOUND LOWER SKIN OF RIGHT HORZI STAB CRACKED BETWEEN STA 120 AND 129. REPAIRED PER SWA RA 1-355-0215.