N342SW

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 73,701 hrs · 64,701 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT SIGN LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,701 hrs · 64,701 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,290 hrs · 64,387 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 761, STR 20R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,290 hrs · 64,387 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 942, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,290 hrs · 64,387 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 887, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,290 hrs · 64,387 cycles

DURING SCHEDULE SPV CHECK, FOUND SKIN CRACKED AT BS 740, STR 18R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,887 hrs · 64,067 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B+15, STR 9L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,868 hrs · 64,054 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 500B+15, STR 19L. REPAIRED SKIN PER SRM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 72,532 hrs · 63,794 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 71,745 hrs · 63,187 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FORWARD CARGO DOOR AFT LOWER FRAME AT I/B CUTOUT OF I/B AFT DOOR STOP CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CRACKED AT BS 727B, RBL 24.8. REPAIRED BEAM PER ER AND EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM SHEAR WEB CORRODED BETWEEN BS 387 TO BS 393, LBL 73. REPAIRED BEAM PER SRM AND BAC DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM SHEAR WEB CORRODED BETWEEN BS 449 TO BS 454, LBL 73. REPAIRED BEAM PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 520, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND VERTICAL CHORD CORRODED AT BS 1126, RBL 16. REMOVED AND REPLACED CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 10R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 300, STR 12L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4L. REMOVED AND REPLACED CLIP PER SI AND EA.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING O/B FORE FLAP LOWER SURFACED DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 4R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, BETWEEN BBL 0 TO RBL 46. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 26L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 6L. REMOVED AND REPLACED CLIP PER SI AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 1L. R&R CLIP PER SI AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 8L. REMOVED AND REPLACED CLIP PER SI AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 936, RBL 14. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 4L. REMOVED AND REPLACED CLIP PER SI AND EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND L-ANGLE CORRODED AT BS 308, LBL 55. REMOVED AND REPLACED L-ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED CLIP PER SI AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED CLIP PER SI AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 70,803 hrs · 62,479 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,159 hrs · 61,952 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 972.5, STR 24L. REPAIRED SKIN PER ER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,129 hrs · 61,928 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,507 hrs · 61,437 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 770, STR 18L. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,507 hrs · 61,437 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 824, STR 19L. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,507 hrs · 61,437 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 750, STR 19L. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,507 hrs · 61,437 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 787 +13, STR 19L. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,507 hrs · 61,437 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 729E, STR 19R. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,507 hrs · 61,437 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 747 +17, STR 19L. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,507 hrs · 61,437 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 729D, STR 19L. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,507 hrs · 61,437 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 510D, STR 15L. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,506 hrs · 61,436 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E+2, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,506 hrs · 61,436 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747+17, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,506 hrs · 61,436 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D+10, STR 15L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,506 hrs · 61,436 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787+12, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,506 hrs · 61,436 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D+2, STR 19L. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 68,872 hrs · 60,980 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,445 hrs · 60,672 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 759, STR 18L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,445 hrs · 60,672 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 803, STR 18L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,145 hrs · 59,682 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,770 hrs · 59,392 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT EMERGENCY EXIT SIGNS BULBS INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,381 hrs · 59,133 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 430, RBL 2. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 420, LBL 3. REPAIRED SKIN PER SWA EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CORRODED AT BS 967, STR 27L, LBL 3. REPAIRED STRINGER PER SRM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND BEAR STRAP SKIN CORRODED AT BS 967, STR 27L. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 660, BL 0. REPAIRED BEAM PER SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR SKIN CUTOUT CRACKED AT BS 305, BELOW WL 236. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT E/E EXHAUST PORT OPENING AT BS 379, LBL 2, STR 18R. REPAIRED SKIN PER SWA EA.

Part: BEAM — CORRODED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT KEEL BEAM CORRODED AT BS 545. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR SKN CRACKED AT BS 305, WL 236. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 291, STR 17R. REPAIRED FRAME PER SWA EA.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT KEEL BEAM CRACKED AT O/B EDGE, BS 541. REPAIRED BEAM PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS. 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT KEELBEAM CRACKED BETWEEN BS 500C TO BS 542. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS. 500B, STR 8L. R&R CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS. 727D, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CHORD CRACKED AT BS 667, BL 0. REPAIRED CHORD PER SI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 747, BETWEEN STR 9R TO STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 400, BETWEEN STR 9R TO STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 480, BETWEEN STR 9R TO STR 8R. REPAIRED FRAME PER SWA EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND KEEL BEAM CORRODED BETWEEN BS 663 TO BS 727. REPAIRED BEAM PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 907, BETWEEN STR 9R TO STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 867, STR 26R. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CHORD CRACKED AT BS 665, BL 0. REPAIRED CHORD PER SI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 727A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, BETWEEN STR 9R TO STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, BETWEEN STR 9R TO STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BETWEEN BS 294 TO BS 299, STR 18R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CHORD CRACKED AT BS 661, LBL 24. REPAIRED CHORD PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 16R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CHORD CRACKED AT BS 665, LBL 24. REPAIRED CHORD PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CHORD CRACKED AT BS 665, LBL 24. REPAIRED CHORD PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 673, RBL 24. REPAIRED CHORD PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CHORD CRACKED AT BS 669, LBL 24. REPAIRED CHORD PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,345 hrs · 58,408 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,780 hrs · 57,273 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR CUTOUT LOWER AFT CORNER. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 930 S23-24L) · airframe 63,780 hrs · 57,273 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, BETWEEN STR 24L AND STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,238 hrs · 56,899 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739D, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,238 hrs · 56,899 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 743, STR 19L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,113 hrs · 56,808 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 62,585 hrs · 56,406 cycles

DURING SCHEDULED MV3 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 62,118 hrs · 56,058 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 62,118 hrs · 56,058 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — DELAMINATED (NR 3 SPOILER) · airframe 62,038 hrs · 56,000 cycles

LEFT WING INBOARD NR 3 FLIGHT SPOILER DELAMINATED AT INBOARD CORNER. REMOVED AND REPLACED SPOILER PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,731 hrs · 55,757 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,440 hrs · 54,752 cycles

DURING SCHEDULED HC1 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 59,558 hrs · 54,073 cycles

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

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 59,541 hrs · 54,056 cycles

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

Part: WINDOW — ARCED (COCKPIT) · airframe 58,979 hrs · 53,651 cycles

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

Part: STRINGER — CRACKED (BS 1006-1016) · airframe 58,732 hrs · 53,453 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 4L CRACKED AT BS 1006 TO BS 1016. REPAIRED STRINGER PER SRM & ER.

Part: SKIN — CRACKED (BS 407) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 407, RBL 2. REPAIRED SKIN PER ER.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND VERTICAL STAB FAIL-SAFE FITTING LT AND RT LUG FACES CORRODED. REPAIRED VERTICAL STAB FAIL-SAFE FITTING PER ER.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND VERTICAL STAB ATTACH FITTING LT AND RT CLEVIS LUG FACES CORRODED. REPAIRED VERTICAL STAB PER ER.

Part: FRAME — CRACKED (BS 273 S14R) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 273, STR 14R. REMOVED AND REPLACED FRAME WEB PER SRM.

Part: FRAME — CORRODED (BS 993 S17R) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 993, STR 17R. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (BS 867) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4L AND STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616 S5R) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L AND STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 42 TO RBL 58. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (BS 787 S9L) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 9L. REPAIRED FRAME SECTION PER SRM.

Part: SHEAR TIE — CRACKED (BS 967 S6L) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 6L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (BS 947 S10R) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 10R. REPAIRED SKIN SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (BS 847 S4LR) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4L AND STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 737E S4R) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 737E, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727D S4R) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 1138 S15L) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1138, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM AND BOEING DRAWING.

Part: STRINGER CLIP — CRACKED (BS 827 S4R) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 827 S9R) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 9R. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727B S4R) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 360 S16L) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 16L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FLOORBEAM — CORRODED (BS 270) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CORRODED AT BS 270, LBL 11 TO RBL 11. REMOVED AND REPLACED FLOORBEAM PER SRM.

Part: CREASE BEAM — CORRODED (BS 460-500B) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 460 TO BS 500B, LBL 70. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C S4L) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: MOUNT — CORRODED (L1 DOOR GIRT BAR) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR MOUNT CORRODED. REMOVED AND REPLACED AFT GIRT BAR MOUNT PER SRM.

Part: STRINGER CLIP — CRACKED (BS 887 S4L) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S4R) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BEAM — CRACKED (VERTICAL STAB) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND VERTICAL STAB RIGHT LOWER MID T/E BEAM CRACKED AT LOWER SECTION. REMOVED AND REPLACED STAB LOWER MID T/E BEAM SECTION PER SRM.

Part: FRAME — CRACKED (BS 400 S9L) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 9L. REPAIRED FRAME SECTION PER SRM.

Part: CREASE BEAM — CORRODED (BS 420-440) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 420 TO BS 440, LBL 70. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: FLOORBEAM — CORRODED (BS 344) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, RBL 1 TO LBL 11. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: FRAME — CRACKED (BS 380 S9R) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 9R. REPAIRED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (BS 793 S19L) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 793, STR 19L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727E S4L) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500B S4R) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 747 S9R) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C S4R) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500A S4R) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 747 S4L) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727D S4L) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500A S4L) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500A S3L) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 747 S11R) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500D S8R) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 738E) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 738E, STR 18L. REPAIRED SKIN PER SRM.

Part: HOOK — LOOSE (L1 DOOR GIRT BAR) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED AFT GIRT BAR HOOK PER SRM.

Part: HOOK — LOOSE (R1 DOOR GIRT BAR) · airframe 58,731 hrs · 53,451 cycles

DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED FWD GIRT BAR HOOK PER SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 58,514 hrs · 53,274 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT OUTER DOOR HANDLE CUTOUT. REPAIRED AFT CARGO DOOR SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 921 S25L) · airframe 57,847 hrs · 52,744 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 921, STR 25L. REPAIRED SKIN PER SWA EA.

Part: STRUCTURE — DELAMINATED (L/E SLAT) · airframe 57,578 hrs · 52,547 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 5 L/E SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,547 hrs · 52,519 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 315, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,537 hrs · 52,509 cycles

DURING SCHEDULED A2 CHECK, FOUND FOUND FUSELAGE SKIN CRACKED AT BS 921, STR 25L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 56,632 hrs · 51,807 cycles

R1 DOOR EVACUATION SLIDE PRESS IND BELOW LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (BS 930) · airframe 56,581 hrs · 51,774 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 22R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,585 hrs · 51,009 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA AND SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 55,062 hrs · 50,590 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: HINGE — BROKEN (R2 DOOR) · airframe 54,213 hrs · 49,916 cycles

R2 DOOR UPPER HINGE LINK ASSY BROKEN. REMOVED AND REPLACED HINGE LINK ASSY PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 53,338 hrs · 49,209 cycles

EMERGENCY EXIT LIGHT ASSY MISSING LENS COVER AT ROW 2 ABC. INSTALLED LENS COVER PER MM.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 53,250 hrs · 49,144 cycles

DURING SCHEDULED A1 CHECK, FOUND FWD RT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,051 hrs · 48,988 cycles

DURING SPV, FOUND FRAME AT BS 500, STRINGER 9L, CRACKED. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,051 hrs · 48,988 cycles

DURING SPV, FOUND STRINGER CLIP AT BS 580, STRINGER 11R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,051 hrs · 48,988 cycles

DURING SPV, FOUND SHEAR TIE AT BS 360, BETWEEN STRINGERS 14R AND 15R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,051 hrs · 48,988 cycles

DURING SPV FOUND SHEAR TIE AT BS 540, STRINGER 10R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,051 hrs · 48,988 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAMES AT RT AND LT BS 188, LBL 33 AND RBL 33, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360) · airframe 53,051 hrs · 48,988 cycles

DURING SPV, FOUND STRINGER CLIP CRACKED BETWEEN BS 360 FROM STRINGER 4L TO STRINGER 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,051 hrs · 48,988 cycles

DURING SPV, FOUND 2 EACH CRACKS ON FLOORBEAM WEB BETWEEN BS 188 TO BS 196, AT LBL 30 AND RBL 30. REMOVED AND REPLACED WEB SECTIONS PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,051 hrs · 48,988 cycles

DURING SPV, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 6 ABC, INOP. RELAMPED LIGHT PER MM.

Part: ADC — FAULTY (E/E BAY) · airframe 52,138 hrs · 48,276 cycles

F/O'S AIRSPEED IND, AND F/O`S ALTIMETER WARNING FLAGS IN VIEW. F/O`S AIR SPEED NEEDLE CYCLED 0 TO 360 TO 0, EVERY 2 MINUTES. DURING LAST 20 MINUTES OF FLIGHT F/A REPORTED BURNED ELECTRICAL SMELL IN CABIN. REMOVED AND REPLACED NR 2 ADC PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 51,725 hrs · 47,974 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: GATE — CRACKED (R2 DOOR) · airframe 51,725 hrs · 47,974 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR AT LOWER AFT GATE, CRACKED. REMOVED AND REPLACED R2 DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,725 hrs · 47,974 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 948, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,725 hrs · 47,974 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 507, STRINGER 14R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,287 hrs · 47,628 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 964, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 50,523 hrs · 47,001 cycles

DURING SCHEDULED 1/2D CHECK, FOUND NLG W/W CEILING WEB AT LT AND RT BRAKE PAD AFT MOUNTS, CRACKED. REPAIRED NLG W/W CEILING WEB PER EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 50,523 hrs · 47,001 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO BAY SKIN BETWEEN BEARSTRAP AND INTERCOSTAL LOWER FLANGE AT BS 844, RBL 17, CORRODED. REPAIRED SKIN PER EA.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 50,523 hrs · 47,001 cycles

DURING SCHEDULED 1/4D CHECK, FOUND MLG W/W BEADED PRESSURE WEB AT BS 673, RBL 36, CRACKED. REPAIRED WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,523 hrs · 47,001 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAMS AT BS 727D + 5, LBL 13, AND BS 774 TO BS 777, LBL 8, CORRODED. REPAIRED FLOORBEAMS PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,523 hrs · 47,001 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO FLOORBEAM AT BS 727D + 5, LBL 13, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,523 hrs · 47,001 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO FLOOR SUPPORT AT BS 774 TO BS 777, LBL 8, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,523 hrs · 47,001 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM FROM, BS 727 + 10 TO BS 780, AT RBL 3, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,523 hrs · 47,001 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,523 hrs · 47,001 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 500 + 2, STRINGER 12R, AND BS 500D + 18, STRINGER 12L, CRACKED. REPAIRED SKIN PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,523 hrs · 47,001 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM AT LT BS 907 TO LT BS 927, CORRODED. REMOVED AND REPLACED CREASE BEAM SECTION PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,523 hrs · 47,001 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 1016, STRINGER 7L, CRACKED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,523 hrs · 47,001 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 727B, STRINGER 25L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,523 hrs · 47,001 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 500B, STRINGER 20L, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,523 hrs · 47,001 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM WEB AT RT BS 360 TO RT BS 380, LT BS 400 TO LT BS 420, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,523 hrs · 47,001 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 500B, STRINGER 20L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 50,523 hrs · 47,001 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT KEEL BEAM FLANGE BS 500D + 2, AND RT KEEL BEAM FLANGE BS 522, CORRODED. REPAIRED KEEL BEAM FLANGE PER EA.

Part: CLIP — CRACKED (FUSELAGE) · airframe 50,523 hrs · 47,001 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS AT BS 727B, STRINGER 25R, BS 727B, STRINGER 25L, BS 727D, STRINGER 23L, BS 727E, STRINGER 23L, BS 747, STRINGER 22L, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,523 hrs · 47,001 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOOR WEB AT BS 270 TO BS 277, CRACKED. REMOVED AND REPLACED FLOOR WEB PER SRM.

Part: FITTING — CORRODED (LT AND RT MLG) · airframe 50,060 hrs · 46,633 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT AND LT MLG FWD HANGER FITTINGS CORRODED. REPAIRED PER EA.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 49,834 hrs · 46,449 cycles

DURING SCHEDULED A2 CHECK, FOUND RT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD AFT CORNER. REMOVED AND REPLACED RT WING OUTBOARD AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,672 hrs · 46,319 cycles

DURING SCHEDULED PM CHECK, FOUND 3 EA FUSELAGE SKIN CRACKS AT BS 500+2, STR 10R, BS 500B, STR 10R, AND BS 787, STR 19L. REPAIRED SKIN SECTIONS PER SRM.

Part: SKIN — CRACKED (LT WING) · airframe 48,113 hrs · 45,035 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING SKIN CRACKED AT INBD FIXED L/E JUST OUTBD OF KRUGER FLAP. REPAIRED SKIN PER SWA EA.

Part: DOOR FRAME — CRACKED (SERVICE DOOR) · airframe 48,113 hrs · 45,035 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR FRAME CRACKED AT AFT LOWER DOOR STOP. REPAIRED FRAME PER SRM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 47,484 hrs · 44,502 cycles

EMERGENCY EXIT LIGHT LENS BROKEN NEXT TO FWD F/A SEAT. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS PER MM.

Part: PIN — CORRODED (LT MLG TRUNNION) · airframe 47,190 hrs · 44,263 cycles

DURING SCHEDULED C1 CHECK, FOUND LT MLG TRUNION PIN CORRODED. REMOVED AND REPLACED LT MLG TRUNNION PIN PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 47,024 hrs · 44,130 cycles

EEPLS SECTION LOOSE. SECURED EEPLS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,559 hrs · 43,780 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR CUTOUT FWD CENTER STUB FRAME CRACKED. REPAIRED STUB FRAME PER SWA EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 45,709 hrs · 43,107 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,074 hrs · 41,743 cycles

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

Part: SLAT — DELAMINATED (LT WING) · airframe 43,017 hrs · 40,886 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 1 L/E SLAT DELAMINATED APPROX 2 INCH SQUARE ON TOP OTBD T/E. REPAIRED L/E SLAT PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 42,515 hrs · 40,460 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD SVC AND FWD ENTRY DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 42,082 hrs · 40,093 cycles

DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LOOSE & LENS MISSING AT ROW 3 ABC. SECURED LIGHT & INSTALLED LENS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,082 hrs · 40,093 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 814, LBL 18 TO RBL 3. REPAIRED FLOORBEAM PER SWA RA 1-353-2668.

Part: ROD END — CORRODED (LH ELEVATOR) · airframe 42,082 hrs · 40,093 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BOTH LH ELEVATOR TRIM TAB ACTUATING ROD ENDS CORRODED AT FWD END. R&R ROD ENDS PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 40,832 hrs · 39,029 cycles

DURING SCHEDULED SPECIAL VISIT FOUND WEB CRACKED AT BS 178, LBL 27, WL 207. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 39,612 hrs · 38,015 cycles

DURING SCHEDULED C4 CHECK, FOUND 1.5 RT HORIZ STAB LOWER SKIN CRACKED AT REAR SPAR, 6'' OTBD OF ROOT. REPAIRED SKIN PER SRM.

Part: WINDOW — LEAKING (COCKPIT) · airframe 39,122 hrs · 37,608 cycles

AIR TURNBACK, PRESS AIR LEAK AROUND BOTTOM OF FIRST OFFICERS FORWARD WINDOW. RE-TORQUED ALL SCREWS ON WINDOW AND PER MM.

Part: SKIN — CRACKED (FUSELAGE KEEL) · airframe 37,792 hrs · 36,444 cycles

DURING SCHEDULED C2 CHECK, FOUND KEELBEAM SKIN CRACKED BETWEEN RT SIDE OF WHEEL WELL. REPAIRED SKIN PER SRM

Part: CABLE — LOOSE (ESCAPE SLIDE) · airframe 36,882 hrs · 35,677 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE RELEASE CABLE ATTACH BOLT LOOSE. TIGHTENED BOLT PER MM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 986 WL 208 ON PREVIOUS REPAIR. REPAIRED BEAM PER ER 99-0269.

Part: SPAR — CRACK (LEFT WING REAR)

DURING SCHEDULED D-CHECK, FOUND THRU EDDY CURRENT INSPECTION, LT WING REAR SPAR CRACKED AT FASTENER HOLE (APPROX FROM WS 285 TO I/B). REPAIRED SPAR PER ER 99-0263.

Part: FRAME — CRACKED (BS 616)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 616, WL 202. REPAIRED FRAME PER ER NO NR 99-0270.

Part: FLOORBEAM — CRACKED (BS 947)

DURING SCHEDULED D-CHECK, FOUND CRACKED FLOORBEAM TOP FLANGE BS 947, LBL 53. REPAIRED PER SRM.

Part: FRAME — CRACKED (BS 480)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 480, BETWEEN STRINGERS 8R TO 9R. REPAIRED FRAME PER ER NR 99-0306.

Part: SKIN — CORRODED (BS 931-986)

DURING SCHEDULED D-CHECK, FOUND CORROSION AT BS 931 TO 986 WEB, WL 208, RBL 48 TO 55. REPAIRED WEB PER SRM.

Part: FRAME — CORRODED (CARGO DOORWAY)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON AFT CARGO DOOR CUTOUT FRAME, BS 794 BETWEEN STRINGERS 22R TO 28R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (NR 6 LE SLAT)

DURING SCHEDULED D-CHECK, FOUND CRACKS EMITTING FROM NR 6 SLAT ON LOWER LE SKIN AT I/B AUX TRACK. REPAIRED PER ER 99-0228P1 AND BOEING DRAWING 65C30133.

Part: SKIN — CORRODED (BS 996-1005)

DURING SCHEDULED D-CHECK, FOUND CORROSION AT FUSELAGE SKIN AT BS 996 TO 1005 BETWEEN STRINGERS 2L-3L. REPAIRED PER SRM.

Part: FRAME — CRACKED (BS 440 & 480)

DURING SCHEDULED D-CHECK, FOUND 2 EA CRACKED FRAMES AT BS 440 AND 480, BETWEEN STRINGERS 8L-9L. REPAIRED PER SRM AND ER NR 99-0283.

Part: FRAME — CRACKED (CARGO DOORWAY)

DURING SCHEDULED D-CHECK, FOUND CRACK AT DOOR CUT OUT FRAME, BS 492. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (BS 359)

DURING SCHEDULED D-CHECK, FOUND CRACK AT STRINGER 14L, BS 359. REPAIRED PER SRM.

Part: FRAME — CRACKED (FUSELAGE)

DURING SCHEDULED D CHECK, FOUND 5 EA FRAMES CRACKED BETWEEN STR 8-9L, BS 827, 867, 907, AND BETWEEN STR 8-9R, BS 787, 867. REAPAIRED FRAMES PER ER NR 99-0283.

Part: FRAME — CRACKED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND 4 FRAMES CRACKED AT BS 400, 440, 500C, 500A BETWEEN STRINGERS 8R-9R. REPAIRED PER SRM AND ER 99-0283.

Part: CLIP — CRACKED (BS 927)

DURING SCHEDULED D-CHECK, FOUND 3 STRINGER CLIPS CRACKED AT BS 927 STRINGERS 27R, 26R AND 27L. REMOVED AND REPLACED CLIPS PER SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND THRU ULTRASONIC INSPECTION 2 CRACKS AT BULKHEAD WEB BS 178 LBL 5 AND RBL 5. REPAIRED PER SRM.

Part: STRINGER — CRACKED (BS 907)

DURING SCHEDULED D-CHECK, FOUND STRINGER 4L CRACKED AT TWO FASTENER HOLES BS 907. REPAIRED PER SRM.

Part: FRAME — CRACKED (BS 295)

DURING SCHEDULED D-CHECK, FOUND STUB FRAME CRACKED AT BS 295 RBL 54.5 WL 209. REMOVED AND REPLACED FRAME PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND THRU ULTRASONIC INSPECTION 2 CRACKS AT BS 178 BULKHEAD, LBL 5-RBL 5. REPAIRED PER SRM.

Part: FLOORBEAM — MISDRILLED (BS 967)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 967 WITH AN OBLONG HOLE THRU UPPER CHORD, RBL 51.5, WL 208. REPAIRED BEAM PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND THRU ULTRASONIC INSPECTION, BULKHEAD CRACKED AT BS 178, LBL 7, WL 212. REPAIRED PER SRM.

Part: SKIN — GOUGED (BS 423)

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 423, AT S18R. REPAIRED PER SWA RA 1-353-1575.

Part: FAIRING — UNSECURED (NR 2 TE FLAP)

IN FLIGHT, NOTED NR 2 FLAP CANOE FAIRING LOOSE FROM MOUNT. AIRCRAFT RETURNED TO STL AND MADE AN UNEVENTFUL LANDING. INSPECTED, RESECURED FAIRING PIVOT BUSHING BOLT PER BOEING M/M.

Part: SEAL — FAILED (NR 1)

EXPERIENCED NUMBER 1 ENGINE OIL PRESSURE DROP AND THE CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. AIRCRAFT LANDED AT AMA WITHOUT INCIDENT. REPLACED OIL SEAL, LEAK CHECKED AND PERFORMED POWER ASSURANCE RUN PER BOEING M/M.