N688SW

Part: FLAP — DELAMINATED (LT WING) · airframe 80,389 hrs · 59,002 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,638 hrs · 58,408 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 740E, STR 22R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,637 hrs · 58,407 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 727E, STR 23R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,637 hrs · 58,407 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 740E, STR 22R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (PYLON) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT WING PYLON AFT FAIRING LOWER PAN SKIN CRACKED. REMOVED AND REPLACED FAIRING PER ER AND EA.

Part: FRAME SPLICE — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME SPLICE CRACKED AT BS 360, BETWEEN STR 13R TO STR 14R. REPAIRED SPLICE PER ER AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 709 TO BS 711, LBL 24.5. REPAIRED CHORD PER ER AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 667, LBL 24.5. REPAIRED CHORD PER ER AND EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB PER ER AND EA.

Part: SIGN — LOOSE (CABIN) · airframe 779,567 hrs · 58,353 cycles

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

Part: CREASE BEAM — CORRODED (CARGO BAY) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO CREASE BEAM CORRODED. REPAIRED BEAM PER SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO CUTOUT FWD LOWER CORNER DOOR SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CRACKED AT BS 767, BETWEEN STR 19L TO STR 20L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7L. REMOVED AND REPLACED CLIP PER EA AND ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7L. REMOVED AND REPLACED CLIP PER EA AND ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 3L. REMOVED AND REPLACED CLIP PER EA AND ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED CLIP PER EA AND ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6L. REMOVED AND REPLACED CLIP PER EA AND ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5L. REMOVED AND REPLACED CLIP PER EA AND ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 5R. REMOVED AND REPLACED CLIP PER EA AND ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 3L. REMOVED AND REPLACED CLIP PER EA AND ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 1L. REMOVED AND REPLACED CLIP PER EA AND ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 6R. REMOVED AND REPLACED CLIP PER EA AND ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED CLIP PER EA AND ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED CLIP PER EA AND ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER EA AND ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 2L. REMOVED AND REPLACED CLIP PER EA AND ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED CLIP PER EA AND ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CRACKED AT BS 500D RT. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,544 hrs · 58,335 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: HINGE — BROKEN (SPOILER) · airframe 78,943 hrs · 57,861 cycles

RT WING I/B NR 5 GROUND SPOILER HINGE BROKEN AT UPPER SURFACE. REMOVED AND REPLACED HINGE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,701 hrs · 57,684 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 962, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,701 hrs · 57,684 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787+6, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,701 hrs · 57,684 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 754 TO BS 764, STR 19L. REPAIRED SKIN PER SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,701 hrs · 57,684 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747+13, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,701 hrs · 57,684 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 971, STR 22L. REPAIRED SKIN PER SRM.

Part: WINDOW — ARCED (COCKPIT) · airframe 78,512 hrs · 57,530 cycles

L1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED L1 WINDOW PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,272 hrs · 57,363 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 923, STR 25L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,129 hrs · 57,249 cycles

DURING SCHEDULED MV2 CHECK, FOUND LOWER OVERWING EMERGENCY EXIT LIGHT SIGN BULBS INOP. REMOVED AND REPLACED BULB PER MM.

Part: LENS — BROKEN (CABIN) · airframe 77,733 hrs · 56,970 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 76,775 hrs · 56,251 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CRACKED AT BS 311.5 AT UPPER FWD DOOR STOP FITTING. REPAIRED BEAM PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,775 hrs · 56,251 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740E, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,775 hrs · 56,251 cycles

DURING SCHEDULED SPV, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER FWD CORNER CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,772 hrs · 56,250 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER FWD CORNER CUTOUT. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 76,772 hrs · 56,250 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 76,355 hrs · 55,929 cycles

FWD GALLEY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 75,912 hrs · 55,615 cycles

DURING SCHEDULED CV CHECK, FOUND FWD I/B FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,680 hrs · 55,454 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 727E + 13, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,680 hrs · 55,454 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 947, STR 24R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,680 hrs · 55,454 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 880, STR 25R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,680 hrs · 55,454 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 747, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,680 hrs · 55,454 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 753, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,680 hrs · 55,454 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 773, STR 20L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,680 hrs · 55,454 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 747, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,680 hrs · 55,454 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 935, STR 24R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,412 hrs · 55,262 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 486, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,412 hrs · 55,262 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 447, STR 16R. REPAIRED SKIN PER SWA EA.

Part: BRACKET — LOOSE (EVAC SLIDE) · airframe 75,059 hrs · 55,013 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVACUATION SLIDE COVER FWD GIRT BAR ATTACH BRACKET LOOSE. SECURED BRACKET PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING OUTBOARD T/E FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: SHEAR TIE — CORRODED (BS 787 S27R) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT ASSY CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 939, STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, BETWEEN STR 25L AND STR 27L. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CRACKED (BS 188 S17R) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 188, STR 17R. REPAIRED WEB PER SRM.

Part: CREASE BEAM — CRACKED (BS 188 S17L) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 188, STR 17L. REPAIRED WEB PER SRM.

Part: FITTING — CRACKED (NR 4 SPOILER) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 4 SPOILER OUTBOARD LUG FITTING CRACKED. REPAIRED FITTING PER SWA EA.

Part: LENS — CRACKED (CABIN) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 380, STR 27L. REPAIRED SPLICE PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 27L. REPAIRED SPLICE PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 28L. REPAIRED SPLICE PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 380, STR 28L. REPAIRED SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (716 S10L) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 716, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND BULKHEAD FWD SIDE CRACKED AT BS 1016, STR 6R. REPAIRED BULKHEAD PER SRM.

Part: STRINGER CLIP — CRACKED (BS 716 S4R) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 716, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (BS 500 S28R) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, STR 28R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (BS 460 S28R) · airframe 73,741 hrs · 54,046 cycles

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

Part: SHEAR TIE — CRACKED (BS 380 S15L) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 380, STR 15L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616 S14L) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 14L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 685 S4R) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (BS 986 S25L) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986, STR 25L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (BS 380 S15L) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER 15L CRACKED AT BS 380. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (NR 4 SLAT) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 4 L/E SLAT CRACKED AT INBOARD END. REPAIRED SLAT PER SRM.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6R. REPAIRED WEB PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 460, STR 28R TO STR 28L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 867 S8L) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 867 S8L) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500A S8L) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 787 S8R) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 727C S8R) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 847 S8L) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 559 S8R) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 480 S8R) · airframe 73,741 hrs · 54,046 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: LENS — LOOSE (CABIN) · airframe 73,707 hrs · 54,018 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 22 ABC. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 73,531 hrs · 53,890 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,170 hrs · 53,614 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 72,641 hrs · 53,233 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,216 hrs · 52,914 cycles

DURING SCHEDULED SPV CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FWD CARGO DOOR) · airframe 72,206 hrs · 52,908 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT LOWER FWD CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 72,206 hrs · 52,908 cycles

DURING SCHEDULED C2 CHECK, FOUND RIGHT WING NR 5 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: HINGE — BROKEN (NR 4 SPOILER) · airframe 71,749 hrs · 52,565 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING NR 4 GROUND SPOILER INBOARD HINGE BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 71,188 hrs · 52,127 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE BETWEEN ROW 5 ABC AND ROW 8 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,090 hrs · 52,052 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 516 AND BS 500D, STR 16L AND STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,587 hrs · 51,654 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740D, STR 21R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,295 hrs · 51,441 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740D, STR 21R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,295 hrs · 51,441 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733, STR 21R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,295 hrs · 51,441 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 745, STR 25R. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,614 hrs · 50,915 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,282 hrs · 50,661 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 251.5, STR 24L. REPAIRED SKIN PER SWA EA & SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,282 hrs · 50,661 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT BULBS INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,384 hrs · 49,996 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RIGHT AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: PANEL — CRACKED (BS 695) · airframe 67,318 hrs · 49,188 cycles

DURING SCHEDULED C1 CHECK, FOUND KEELBEAM PANEL CRACKED AT LOWER LT SIDE BS 695. REPAIRED KEEL BEAM PANEL PER SRM.

Part: STRINGER — CORRODED (BS 500D) · airframe 67,256 hrs · 49,138 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 27R, CORRODED AT BS 500D. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SKIN — CRACKED (BS 737D S21L) · airframe 67,256 hrs · 49,138 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737D, STR 21L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 410) · airframe 67,256 hrs · 49,138 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER CUTOUT, BS 410, RBL 2. REPAIRED SKIN PER ER.

Part: SUPPORT FITTING — CRACKED (LT MLG BEAM) · airframe 67,254 hrs · 49,137 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING MLG BEAM OUTBOARD FITTING CRACKED AT STA 222. REPAIRED LT MLG FITTING PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,254 hrs · 49,137 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 25R. REPAIRED SKIN PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 67,254 hrs · 49,137 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,254 hrs · 49,137 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 13L. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 67,254 hrs · 49,137 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 9L CRACKED AT BS 787. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: VERTICAL BEAM — CRACKED (BS 178 BULKHEAD) · airframe 67,254 hrs · 49,137 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM CRACKED AT BS 178, LBL 5.7, WL 186. REPAIRED VERTICAL CHORD PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 67,254 hrs · 49,137 cycles

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

Part: SKIN — CRACKED (BS 520) · airframe 67,016 hrs · 48,949 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 931) · airframe 669,783 hrs · 48,916 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 931, STR 22R. REPAIRED SKIN PER SWA EA AND SRM.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 66,578 hrs · 48,612 cycles

DURING SCHEDULED SERVICE CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. RESEATED LIGHT ASSY CONNECTOR PER MM.

Part: WINDOW — MISSING (R2 DOOR SLIDE) · airframe 66,184 hrs · 48,312 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR VIEWER WINDOW MISSING. INSTALLED VIEWER WINDOW PER MM.

Part: SKIN — CRACKED (BS 941) · airframe 66,069 hrs · 48,216 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941.5, STR 21R. REPAIRED SKIN PER SRM.

Part: WIRE — CHAFED (COCKPIT) · airframe 65,944 hrs · 48,110 cycles

AIR TURNBACK, SMOKE SMELL IN COCKPIT. FOUND WIRE 268-010-08 CHAFED AT CONNECTOR D13730, AFT OF P5 PANEL. SPLICED WIRE PER WDM.

Part: BELTFRAME — CRACKED (BS 500B) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 500B, STR 19L & STR 19R. REPAIRED BELTFRAME PER SWA EA'S.

Part: PRESSURE PANEL — CRACKED (CABIN FLOOR) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BEADED PRESSURE WEB CRACKED BETWEEN BS 663 TO BS 665, LBL 43. REPAIRED WEB PER SWA EA.

Part: SHEAR TIE — CORRODED (BS 927-947) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED BETWEEN BS 927 TO BS 947.5, RBL 13.8. REPAIRED SHEAR TIE PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT R1 DOOR CUTOUT, FWD FRAME NR 4 STOP FITTING. REPAIRED FRAME PER SRM.

Part: KEELBEAM — CRACKED (BS 542) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT KEEL BEAM LOWER CHORD CRACKED AT BS 542. REPAIRED KEEL BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT R1 DOOR CUTOUT, FWD FRAME NR 3 STOP FITTING. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 747) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 747, STR 20R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRAP — CRACKED (BS 178) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BS 178 BULKHEAD VERTICAL STRAP CRACKED AT BL 0, WL 188. REPAIRED STRAP PER SWA EA.

Part: SHEAR TIE — CORRODED (BS 747) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 747, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (BS 178) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT BL 0, WL 189. REPAIRED WEB PER SRM.

Part: STRINGER — CORRODED (BS 734) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 734, STR 27L. REPAIRED STRINGER PER SWA EA.

Part: FRAME — CRACKED (BS 639) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727B) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727B, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (BS 373) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT E/E COOLING EXHAUST OUTLET INTERNAL DOUBLER, BS 373 AND BS 378, LBL 2.8. REPAIRED SKIN PER SWA EA.

Part: TEE FITTING — CORRODED (BS 1016) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 AFT PRESSURE BLKHD UPPER T-CHORD CORRODED AT RBL 24.75. REMOVED AND REPLACED T-CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 65,704 hrs · 47,910 cycles

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

Part: SHEAR TIE — CORRODED (BS 360) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 360, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: GIRT BAR — CORRODED (L1 DOOR) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD BRACKET CORRODED AT BS 312, LBL 56. REMOVED AND REPLACED BRACKET PER SRM.

Part: FRAME — CRACKED (BS 639) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17L. REPAIRED FRAME PER SWA EA.

Part: WEB — CRACKED (BS 663-665) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BEADED PRESSURE WEB CRACKED BETWEEN BS 663 TO BS 665, LBL 32. REPAIRED WEB PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 65,704 hrs · 47,910 cycles

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

Part: STRINGER CLIP — CRACKED (BS 294) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294.5, STR 12L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (BS 847) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847, BETWEEN STR 23L TO STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: KEELBEAM — CORRODED (BS 727) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT KEEL BEAM CORRODED AT BS 727. REPAIRED KEEL BEAM PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND NLG W/W RIGHT FWD SIDE PRESSURE PANEL CRACKED AT BS 243.7, WL 168.5. REPAIRED WEB PER SWA EA.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND NLG W/W LEFT FWD SIDE PRESSURE PANEL CRACKED AT BS 240, WL 168.6. REPAIRED WEB PER SWA EA.

Part: SKIN — CRACKED (BS 787) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, BETWEEN STR 20L TO STR 23L. REPAIRED SKIN PER SRM.

Part: FLOOR SUPPORT — CRACKED (BS 662) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED D-CHECK, FOUND NR 3 LONGITUDINAL FLOORBEAM UPPER T-CHORD CRACKED AT BS 662, RBL 24.82. REPAIRED FLOORBEAM IAW EA.

Part: STRINGER CLIP — CRACKED (BS 294) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED CLIP IAW SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 65,704 hrs · 47,910 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOOR BEAM CORRODED AT BS 986.5, RBL 45. REMOVED AND REPLACED FLOORBEAM UPPER T-CHORD IAW SRM.

Part: SKIN — CRACKED (BS 739D-739E) · airframe 65,590 hrs · 47,818 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 739D TO BS 739E, STR 23L. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (BS 504C) · airframe 65,590 hrs · 47,818 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504C, STR 15R. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (BS 789) · airframe 65,590 hrs · 47,818 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 789, STR 18L. REPAIRED SKIN PER SRM.

Part: LIGHT — WORN (CABIN) · airframe 65,590 hrs · 47,818 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS STRIP WORN AT ROW 1 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: SKIN — CRACKED (BS 740) · airframe 65,251 hrs · 47,534 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740, STR 18R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 730) · airframe 65,251 hrs · 47,534 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730, STR 18R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 500D) · airframe 65,251 hrs · 47,534 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 12R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 741) · airframe 65,251 hrs · 47,534 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 741, STR 19R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 514) · airframe 65,251 hrs · 47,534 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,684 hrs · 47,080 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, BL 0. REPAIRED SKIN PER SWA EA & SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,805 hrs · 46,365 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 178 BULKHEAD, RBL 17.1, WL 225. REPAIRED WEB PER SRM.

Part: WINDOW — ARCED (COCKPIT) · airframe 63,412 hrs · 46,052 cycles

ARCING OBSERVED ON L1 COCKPIT WINDOW IN TOP RT CORNER. WINDOW HEAT SWITCHED OFF. OUTER PANE L1 COCKPIT WINDOW CRACKED. REMOVED AND REPLACED L1 COCKPIT WINDOW AND HEAT CONTROLLER.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 62,212 hrs · 45,133 cycles

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

Part: SKIN — CORRODED (KEEL) · airframe 61,827 hrs · 44,826 cycles

DURING SCHEDULED SERVICE CHECK, FOUND KEEL BEAM SKIN AT BS 500, CORRODED. REMOVED AND REPLACED SKIN SECTION PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,822 hrs · 44,823 cycles

DURING SCHEDULED C3 CHECK, FOUND 4 EACH FUSELAGE SKIN CRACKS AT BS 747, BS 755, STRINGER 24L, BS 727D, STRINGER 22R, BS 747, STRINGER 18R. REPAIRED SKIN PER EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,822 hrs · 44,823 cycles

DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 500D, BS 520, STRINGER 12L.

Part: SKIN — DELAMINATED (LT WING FOREFLAP) · airframe 61,822 hrs · 44,823 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: ENGINE — VIBRATION (NR 2) · airframe 61,635 hrs · 44,662 cycles

AT CLIMB POWER, NR 2 ENGINE HAD VIBRATION AND HUM-VIBRATION METER AT 5.0, REDUCING N1 TO 83 PERCENT VIBRATION METER WAS AT 4.0, AND HUM-VIBRATION METER SLIGHTLY LOWER. HUM-VIBRATION ONLY WENT AWAY WITH N1 BELOW 48 PERCENT. REMOVED AND REPLACED NR 2 ENGINE PER MT 371-00-01.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,059 hrs · 44,193 cycles

DURING SCHEDULED A2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,493 hrs · 43,715 cycles

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

Part: BRACKET — MISSING (GIRT BAR) · airframe 59,905 hrs · 43,241 cycles

DURING PREFLIGHT CK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR AFT MOUNTING FLOOR BRACKET MISSING. INSTALLED BRACKET PER MM.

Part: GLOWSTRIP — MISSING (ROW 6-8) · airframe 59,787 hrs · 43,154 cycles

PHOTOLUMINESCENT STRIP MISSING FROM ROW 6 TO ROW 8 LT SIDE. REINSTALLED NEW SECTION OF STRIP.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,518 hrs · 42,944 cycles

DURING SCHEDULED SPECIAL VISIT AT SAT AEROSPACE, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,518 hrs · 42,944 cycles

DURING SCHEDULED SPECIAL VISIT AT SAT AEROSPACE, FOUND OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 2 DEF. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,284 hrs · 42,749 cycles

DURING SCHEDULED PMC CHECK, FOUND 2 FUSELAGE SKIN CRACKS AT BS 727E+3, STR 22L AND BS 727E+17, STR 24R. REPAIRED SKIN PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 58,111 hrs · 41,846 cycles

DURING SCHEDULED C3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED EXIT LIGHT LENS PER MM.

Part: SLIDE — OUT OF ADJUST (AFT ENTRY DOOR) · airframe 58,111 hrs · 41,846 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,669 hrs · 41,482 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT UPPER FWD CORNER OF AIRSTAIR CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,669 hrs · 41,482 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED ON FO'S FWD WINDOW POST. REPAIRED SKIN PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 57,669 hrs · 41,482 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 650 AND BS 663. REPAIRED KEEL BEAM PER SRM.

Part: CONTROLLER — FAILED (COCKPIT) · airframe 57,591 hrs · 41,425 cycles

CABIN PRESSURE ALTITUDE WARNING HORN SOUNDED AT 35K, INITIATED PROCEDURES WITH EMERGENCY DESCENT. FOUND, PRESSURE CONTROLLER FAILURE. REMOVED AND REPLACED PRESSURE CONTROLLER PER MM.

Part: PIN — CORRODED (LT/RT MLG TRNION) · airframe 56,899 hrs · 40,875 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11251-32, FOUND BOTH LT AND RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT AND RT MLG TRUNNION PINS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,831 hrs · 40,830 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT BS 750 AT STR 19R, BS 755 AT STR 21R AND BS 763 AT STR 19R. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (NOSE) · airframe 56,639 hrs · 40,689 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 201, AT LBL 4.75, RBL 4.75, WL 209, AT LBL 4.75 AND WL 234, AT RBL 12. REPAIRED WEB PER SRM.

Part: SLIDE — OUT OF ADJUST (CABIN) · airframe 56,322 hrs · 40,439 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDES GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,937 hrs · 40,155 cycles

RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,365 hrs · 39,695 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 24L, BS 727E AND BS 737. REPAIRED SKIN PER SRM.

Part: DUCT CLAMP — LEAKING (MLG W/W) · airframe 55,071 hrs · 39,445 cycles

DECLARED EMERGENCY, DIVERSION, DURING CLIMB LOST CABIN PRESSURATION, MASKS DEPLOYED. FOUND DUCT AT AFT MLG W/W LEAKING. TIGHTENED CLAMP PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,464 hrs · 38,929 cycles

DURING SCHEDULED C3 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT IN AFT CEILING INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 54,464 hrs · 38,929 cycles

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

Part: ACTUATOR — FAILED (L/E FLAP) · airframe 54,331 hrs · 38,820 cycles

AIR TURNBACK, AFTER TAKEOFF NR 2 KRUEGER FLAP WOULD NOT RETRACT. REMOVED AND REPLACED NR 2 KRUEGER FLAP ACTUATOR PER MM.

Part: SLIDE — LOOSE (FWD ENTRY DOOR) · airframe 54,159 hrs · 38,668 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: SLAT — CRACKED (LH WING) · airframe 51,795 hrs · 36,723 cycles

DURING SCHEDULED C4 CHECK, FOUND # 2 L/E SLAT CRACKED .75 INCH LONG AT INBD LOWER T/E. REPAIRED # 2 SLAT PER SWA RA 1-357-1114.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,795 hrs · 36,723 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACK (2 EA) AT BS 727E, STR 18R & BS 747, STR 25R. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 50,605 hrs · 35,691 cycles

DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LENS MISSING AT RT OVERWING EXIT. REPLACED BULL NOSE LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,039 hrs · 35,211 cycles

DURING SCHEDULED C2 CHECK, FOUND 1.5 INCH LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 727E, STR 22L. REPAIRED SKIN PER SRM.

Part: STIFFENER — CRACKED (MLG WW) · airframe 49,636 hrs · 34,876 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 663 VERTICAL STIFFENERS CRACKED AT LBL 6.5 & RBL 6.5. REMOVED AND REPLACED VERTICAL STIFFENERS PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 49,594 hrs · 34,838 cycles

DURING SCHEDULED D-CHECK, FOUND STR 27L CORRODED FROM BS 500B TO BS 500D. REPAIRED STR PER SRM & ER.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 49,594 hrs · 34,838 cycles

DURING SCHEDULED D-CHECK, FOUND KEEL BEAM CORRODED AT BS 721, RBL 7 & BS 500D, LT SIDE. REPAIRED KEEL BEAM PER ER''S & SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 49,544 hrs · 34,838 cycles

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM CRACKED AT RBL 17.1, WL 191. REPAIRED VERTICAL BEAM PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,594 hrs · 34,838 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 787 & 727C, BETWEEN STR 8R & 9R, BS 767& 827 BETWEEN STR 8L & 9L, & BS 887, BETWEEN STR 8L & 9L. REPAIRED FRAMES PER ER & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,594 hrs · 34,838 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, BETWEEN STR 8R & 9R. REPAIRED FRAME PER ER.

Part: BEAM — CRACKED (BULKHEAD) · airframe 49,594 hrs · 34,838 cycles

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAMS CRACKED AT LBL 17.1, WL 184 & RBL 5.7, WL 184. REPAIRED VERTICAL BEAMS PER ER.

Part: SPLICE — CRACKED (STRINGER) · airframe 49,594 hrs · 34,838 cycles

DURING SCHEDULED D-CHECK, FOUND STR SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM & T1-A51-002.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 49,594 hrs · 34,838 cycles

DURING SCHEDULED D-CHECK, FOUND KEEL BEAM CORRODED AT BS 723, LBL 7. REPAIRED KEEL BEAM PER ER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,594 hrs · 34,838 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGERS CRACKED AT BS 400, STR 4R, BS 440, STR 16L. REPAIRED STRINGERS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,594 hrs · 34,838 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, RBL 68, WL 268. REPAIRED FRAME PER ER & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,594 hrs · 34,838 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, BETWEEN STR 1L & 2L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,594 hrs · 34,838 cycles

DURING SCHEDULED D-CHECK, FOUND STR CLIPS CRACKED AT BS 400, STR 4R, BS 440, STR 16L, BS 616, STR 5L & BS 727C, STR 3L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: FITTING — CORRODED (RT MLG) · airframe 49,594 hrs · 34,838 cycles

DURING SCHEDULED D-CHECK, FOUND RT MLG STABILIZER BEAM FITTING CORRODED. REMOVED AND REPLACED STABILIZER FITTING PER MM.

Part: RIB — CRACKED (LT WING) · airframe 49,554 hrs · 34,838 cycles

DURING SCHEDULED D-CHECK, FOUND LT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN S-2 & S-3. REPAIRED RIB LOWER CHORD PER ER.

Part: STRINGER CLIP — CRACKED (CABIN) · airframe 49,594 hrs · 34,838 cycles

DURING SCHEDULED D-CHECK, FOUND STR CLIPS CRACKED AT BS 500A, STR 16L, BS 380, STR 1, BS 277 STR 15R & BS 616, STR 8L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: STRINGER — CRACKED (CABIN) · airframe 49,594 hrs · 34,838 cycles

DURING SCHEDULED D-CHECK, FOUND STR CRACKED AT BS 400, STR 4L. REPAIRED STR PER SRM.

Part: STRINGER CLIP — CRACKED (CABIN) · airframe 49,554 hrs · 34,838 cycles

DURING SCHEDULED D-CHECK, FOUND STR CLIPS CRACKED AT BS 727, STR 6R, BS 727A STR 3R, 727C STR 5R & STR 6R, BS 727D, STR 1, STR 2L, STR 5L/R, STR 6L, STR 7L, STR 8L & STR 9L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: CREASE BEAM — CORRODED (CABIN) · airframe 49,594 hrs · 34,838 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED FROM BS 950 TO BS 996, RBL 48 TO RBL 52. REPAIRED CREASE BEAM WEB PER SRM.

Part: BRACKET — CORRODED (ESCAPE SLIDE) · airframe 49,594 hrs · 34,838 cycles

DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BRACKET CORRODED. REMOVED AND REPLACED GIRT BRACKET PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,594 hrs · 34,838 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,594 hrs · 34,838 cycles

DURING SCHEDULED D-CHECK, FOUND STR 14L CRACKED AT BS 360, WL 230. REPAIRED STR PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 49,594 hrs · 34,838 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,594 hrs · 34,834 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BL 0, WL 148. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,594 hrs · 34,838 cycles

DURING SCHEDULED D-CHECK, FOUND 2 STRINGERS CRACKED AT BS 381, STR 4L & BS 420, STR 4L. REPAIRED STRINGERS PER SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 49,085 hrs · 34,414 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING I/B TRAILING EDGE AFT FLAP DELAMINATED AT O/B TRAILING EDGE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 47,791 hrs · 33,312 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND AFT UPPER EMERGENCY FLASHLIGHT BATTERY LOW. R&R FLASHLIGHT BATTERY PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

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

Part: WIRE — FAILED (FLAP INDICATOR)

ABORTED TAKEOFF, TAKE-OFF WARNING HORN SOUNDED AND NR 4 L/E FLAP TRANSIT LIGHT INOP. REPAIRED WIRING CONNECTING TO NR 4 L/E FLAP DOWN POS INDICATOR SWITCH PER MM.

Part: TRANSMITTER — ERRATIC (RT TE FLAP)

AIR TURNBACK, AFTER TAKEOFF T/E FLAPS WOULD NOT FULLY RETRACT. REPAIRED WIRE AT 5C ON FLAP ASYMMETRY SWITCH. REMOVED AND REPLACED FLAP POSITION INDICATOR. REMOVED AND REPLACED R123 RELAY AND REMOVED AND REPLACED RT FLAP TRANSMITTER PER MM.

Part: SKIN — DELAMINATED (RT AILERON TAB)

DURING SCHEDULED C4 CHECK, FOUND RT AILERON TAB DELAMINATED INBD OF PUSHRODS. REMOVED AND REPLACED AILERON TAB PER MM.

Part: OVERHEAT LOOP — INOP (NR 2 PYLON)

DURING DESCENT, RT WING OVERHEAT LIGHT ILLUMINATED, PERFORMED QRH ITEMS AND LIGHT REMAINED ON UNTIL AFTER ENG SHUT DOWN. OPENED AND INSPECTED A/C BAY AND L/E FLAP AREA, FOUND NO LEAKS. RECLOSED A/C BAY DOOR. REPLACED M488 ENG/PYLON LOOP PER M/M.

Part: WEB — DAMAGED (CARGO DOORWAY)

DURING SCHEDULED 1/4 D-CHECK, FOUND WEB DAMAGED AT FWD LOWER CORNER OF AFT CARGO DOORWAY. REPAIRED PER TII-A53-35.

Part: FLOORBEAM — CORRODED (BS 770)

DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED FLOORBEAM AND SEVERAL HOLES AT BS 770, RBL 3. REMOVED AND REPLACED PER BOEING SRM.

Part: BOW TIE — WORN (LT HORIZ STAB)

DURING SCHEDULED 1/4 D-CHECK, FOUND LT BOW TIE WORN. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 727)

DURING SCHEDULED 1/4 D-CHECK, FOUND FWD BULKHEAD DIAGONAL SUPPORT CRACKED AT BS 727, BL 0. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOOR — CORRODED (BS 860)

DURING SCHEDULED 1/4 D-CHECK, FOUND FLOOR PANEL TRANSITION ANGLE CORRODED ALONG UPPER SURFACE AT BS 860, LBL 21, RBL 21. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — DAMAGED (BS 777)

DURING SCHEDULED 1/4 D-CHECK, FOUND FOUR HOLES IN FLOORBEAM AT BS 777, RBL 8. REPAIRED PER SRM.

Part: SKIN — CRACKED (BS 727)

DURING SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 2.5 LONG BELOW STR 23R AT BS 727D. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727)

DURING SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 2.5 LONG ABOVE STR 23R FWD AT BS 727E. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — SCRATCHED (BS 1088)

DURING SCHEDULED B/C4 CHECK, FOUND FUSELAGE SKIN SCRATCHED 11 IN LENGTH, AT BS 1088. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING WALKAROUND CHECK, FOUND AFT EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PER BOEING M/M.