N331SW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,055 hrs · 67,846 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT O/W EMERGENCY EXIT LIGHT LWR LIGHT INOP. REPLACED LAMP PER MM.

Part: ACTUATOR — LEAKING (SPOILER) · airframe 75,922 hrs · 67,747 cycles

POSSIBLE HYDRAULIC LEAK IN LT WHEEL WELL AREA. REMOVED AND REPLACED I/B GROUND SPOILER ACTUATOR IAW MM.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 75,449 hrs · 67,375 cycles

FWD LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 727E, BETWEEN STR 19R TO STR 20R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 25R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 22R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING AFT FLAP LOWER SKIN DELAMINATED. REMOVED AND REPLACED AFT FLAP IAW MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 727D, BETWEEN STR 19R TO STR 20R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT ANGLE CRACKED AT BS 727, BETWEEN LBL 45.50 TO LBL 24.75. REMOVED AND REPLACED ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 727E+2, STR 18R. REPAIRED SKIN IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT SIDE CHORD CRACKED AT BS 616, WL 208. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 727E+6, STR 20R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 747+2, STR 18R. REPAIRED SKIN IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHORD CORRODED AT BS 727, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED CHORD IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED BETWEEN BS 259.5 TO BS 270, STR 10L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 727E+16.5, STR 20L. REPAIRED SKIN IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 27R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 1006+6, STR 24R. REPAIRED SKIN IAW EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CHORD CRACKED AT BS 663+3, RBL 24.5. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 747+12, STR 18R. REPAIRED SKIN IAW EA.

Part: FRAME — PUNCTURED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME PUNCTURED AT BS 480, STR 8L. REPAIRED FRAME IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 25L. REPAIRED CLIP IAW SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND EMERGNECY EXIT LIGHT INOP DURING EMERGENCY LIGHT TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 787+17, STR 18L. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT VERTICAL ANGLE CRACKED AT BS 727, STR 27R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT VERTICAL ANGLE CRACKED AT BS 727, STR 27L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED BETWEEN BS 947.5 TO BS 927, STR 25R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED BETWEEN BS 927 TO BS 947, STR 26R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: STIFFENER — CRACKED (RT WING) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING STIFFENER 8 LOWER FLANGE CRACKED AT WBL 453. REPAIRED STIFFENER IAW EA AND EO.

Part: STIFFENER — CRACKED (RT WING) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING STIFFENER 7 AND 8 LOWER FLANGE CRACKED AT WBL 355. REPAIRED STIFFENER IAW EA AND EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 947, STR 25R+1. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR AFT UPPER CORNER CUTOUT. REPAIRED SKIN IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 453, STR 7R. REPAIRED STRINGER IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURINGS SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 927+5, STR 21R. REPAIRED SKIN IAW EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM WEB CRACKED BETWEEN BS 713 TO BS 708, RBL 0. REPAIRED WEB IAW SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURINGS SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 355, STR 7R. REPAIRED STRINGER IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CRACKED BETWEEN BS 344 TO BS 360, STR 16L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK FOUND SHEAR TIE CORRODED AT BS 827, BETWEEN STR 27R TO STR 26R. REPAIRED SHEAR TIE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK FOUND STRINGER CLIP CRACKED AT BS 1104, STR 3R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK FOUND STRINGER CRACKED AT BS 927, STR 26R. REPAIRED STRINGER IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 27R TO STR 26R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 747, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 727E+6.5, STR 20L. REPAIRED SKIN IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727C+6, LBL 8.10. REPAIRED CHANNEL IAW EA.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 727E, STR 10L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 500B, BETWEEN STR 28R TO STR 28L. REPAIRED FRAME IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 927, STR 26L. REPAIRED STRINGER IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 907, STR 21R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767+5, LBL 3.0. REPAIRED CHANNEL IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 907, STR 24R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 360, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND WEB CORRODED BETWEEN BS 460 TO BS 480, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FRAME — PUNCTURED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME PUNCTURED AT BS 907, BETWEEN STR 1L TO STR 2L. REPAIRED FRAME IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 907, STR 23R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 907, STR 20R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND WEB CORRODED BETWEEN BS 440 TO BS 460, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 19R. REMOVED AND REPLACED CLIP IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727D+5, RBL 8.10. REPAIRED CHANNEL IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767+5, LBL 8.10. REPAIRED CHANNEL IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727D+5, RBL 8.10. REPAIRED CHANNEL IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND SUPPORT ANGLE CRACKED BETWEEN BS 927 TO BS 947.5, BL 0. REMOVED AND REPLACED ANGLE IAW SRM AND DWG..

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED BETWEEN BS 1007 TO BS 1008, STR 25R. REPAIRED SKIN PER SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727D+5, RBL 3.0. REPAIRED CHANNEL IAW EA.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND INNER CHORD CORRODED BETWEEN BS 360 TO BS 380, STR 17R. REPAIRED CHORD IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 22L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, 22L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 907, BETWEEN STR 18L TO STR 19L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 22R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 597, STR 15R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 827, STR 14L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 520, STR 8L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 663.5, STR 10R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 520, STR 9L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 1R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 907, STR 10L. REPAIRED SKIN IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND WEB CORRODED BETWEEN BS 907 TO BS 927, STR 17L. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: SLAT — CRACKED (RT WING) · airframe 74,518 hrs · 66,659 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING NR 6 SLAT CRACKED FROM O/B EDGE I/B. REPAIRED SLAT PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 73,991 hrs · 66,268 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR CUTOUT FWD LOWER FRAME CRACKED. REMOVED AND REPLACED FRAME PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 73,996 hrs · 66,269 cycles

DURING SCHEDULED OTS CHECK, FOUND RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 73,991 hrs · 66,268 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR LOWER HINGE CUTOUT IN DOOR FRAME CRACKED. REPAIRED FRAME PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 73,996 hrs · 66,269 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD GALLEY DOOR CUTOUT, FWD LOWER FRAME CRACKED. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,996 hrs · 66,269 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER AND EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 73,996 hrs · 66,269 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT ENTRY DOOR LOWER HINGE CUTOUT IN DOOR FRAME CRACKED. REMOVED AND REPLACED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,911 hrs · 66,208 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 19R TO STR 22R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,911 hrs · 66,208 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,911 hrs · 66,208 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 19L TO STR 22L. REPAIRED FRAME PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 73,911 hrs · 66,208 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM CORRODED BETWEEN STR 807 TO BS 827, STR 17R. REPAIRED BEAM PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,911 hrs · 66,208 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 19L TO STR 22L. REPAIRED FRAME PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,911 hrs · 66,208 cycles

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

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 73,911 hrs · 66,208 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT FWD UPPER CORNER HORIZONTAL FAIL SAFE CHORD WEB CRACKED. REMOVED AND REPLACED CHORD PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,427 hrs · 65,849 cycles

DURING SCHEDULED OTS CHECK, FOUND FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,427 hrs · 65,849 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CLIP CRACKED AT BS 986.5, STR 20L. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,427 hrs · 65,849 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 446, STR 26L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,427 hrs · 65,849 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 405 TO BS 415.5, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,427 hrs · 65,849 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 908 TO BS 1016. REMOVED AND REPLACED SKIN PER SRM.

Part: SKIN — CRACKED (BS 923 S24L) · airframe 73,424 hrs · 65,848 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 923, STR 24L. REMOVED AND REPLACED SKIN PANEL PER SRM.

Part: SKIN — CRACKED (BS 446 S26L) · airframe 73,424 hrs · 65,848 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 446, STR 26L. REMOVED AND REPLACED SKIN PANEL PER SRM.

Part: SKIN — CRACKED (BS 978 S21L) · airframe 73,424 hrs · 65,848 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 978, STR 21L. REMOVED AND REPLACED SKIN PANEL PER SRM.

Part: SKIN — CRACKED (BS 953 S23L) · airframe 73,424 hrs · 65,848 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 953, STR 23L. REMOVED AND REPLACED SKIN PANEL PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,135 hrs · 65,632 cycles

RT OVERHEAD EMERGENCY EXIT BULL NOSE LIGHT INOP AT ROW 23. SECURED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 72,638 hrs · 65,227 cycles

DURING SCHEDULED CV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 72,617 hrs · 65,212 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,557 hrs · 65,155 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,496 hrs · 65,100 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 72,118 hrs · 64,794 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 71,786 hrs · 64,538 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER SKIN CRACKED AT STA 120.3. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,786 hrs · 64,538 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER CUTOUT, BS 986, STR 5L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,786 hrs · 64,538 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 810, STR 19L. REPAIRED SKIN PER SRM.

Part: WIRE — DAMAGED (COCKPIT) · airframe 71,560 hrs · 64,370 cycles

AIR TURNBACK / DECLARED EMERGENCY. FUMES IN THE COCKPIT. FOUND DAMAGED WIRING AT LEFT I/B LANDING LIGHT SWITCH. REPLACED LANDING LIGHT SWITCH AND TERMINAL ENDS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,559 hrs · 64,367 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 312, STR 19R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,559 hrs · 64,367 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,559 hrs · 64,367 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,559 hrs · 64,367 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,300 hrs · 63,415 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 500D, STR 16R. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,285 hrs · 63,404 cycles

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

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 70,300 hrs · 63,415 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 2 SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 70,300 hrs · 63,415 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 1 SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,300 hrs · 63,415 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 773, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,300 hrs · 63,415 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 500C, STR 15R. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,285 hrs · 63,404 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,285 hrs · 63,404 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AEM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AEM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 520, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER AEM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 294.5, STR 10L. REPAIRED FRAME PER AEM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 665.5, LBL 24.5. REPAIRED BEAM PER AEM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 291, BETWEEN STR 9R TO STR 15R. REPAIRED FRAME PER AEM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING FWD PLATE CORRODED. REMOVED AND REPLACED FITTING ASSY PER MM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING FWD PLATE CORRODED. REMOVED AND REPLACED FITTING ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 344, BETWEEN STR 23L TO STR 24L. REPAIRED FRAME PER AEM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AEM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 348.2 TO BS 303.9, LBL 58. REPAIRED WEB PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND ZEE ANGLE CORRODED BETWEEN BS 316 TO BS 335, LBL 62. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED CLIP PER SI.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOOR ANGLE CORRODED AT BS 331, LBL 58. REPAIRED ANGLE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM WEB LOWER CHORD CRACKED AT BS 663, RBL 24.5. REPAIRED CHORD PER AEM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CORRODED AT BS 906, STR 26L. REPAIRED STRINGER PER SRM.

Part: BEAM — CRACKED (LT MLG WW) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT MLG WHEEL WELL PRESSURE DECK VERTICAL BEAM WEB CRACKED AT BS 664, LBL 31. REPAIRED WEB PER AEM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 420 TO BS 440, STR 17R. REPAIRED WEB PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CORRODED AT BS 906, STR 26L. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM WEB CRACKED BETWEEN BS 705 TO BS 715, LBL 24.5. REPAIRED BEAM PER AEO.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 312 TO BS 344, LBL 59. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND NOSE WHEEL WELL SNUBBER SPRING PLATE SKIN CRACKED AT CEILING ACCESS DOOR CUTOUT, BETWEEN RBL 7.75 TO LBL 7.75. REPAIRED SKIN PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 986.5, BETWEEN STR 6L TO STR 7L. REPLACED FRAME SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 312, RBL 51. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 328, RBL 34. REMOVED AND REPLACED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 967 BETWEEN STR 6L TO STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 947.5, BETWEEN RBL 5 TO RBL 20. REPAIRED BEAM PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR CENTER STUB FRAME CRACKED. REMOVED AND REPLACED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 303, STR 16L. REPAIRED SKIN PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 967, LBL 5. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 9L. REMOVED AND REPALCED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 334, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,262 hrs · 63,389 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: PANEL — DISLODGED (CABIN)

F/A NOTICED AN OVERHEAD CEILING PANEL THAT WAS LOOSE DURING THE MIDST OF THE 2ND LEG OF FLIGHT 2361. BECAME DISLODGED ON LANDING, AND FELL INTO PASSENGER CABIN HITTING TWO PASSENGER`S HEADS.

Part: FLAP — DELAMINATED (LT WING) · airframe 69,989 hrs · 63,178 cycles

DURING SCHEDULED CV CHECK, FOUND LT WING O/B TRAILING EDGE FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (BS 517B S19R) · airframe 69,889 hrs · 63,107 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 517B, STR 19R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,785 hrs · 63,029 cycles

FWD EMERGENCY EXIT DOOR LOWER LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 69,785 hrs · 63,029 cycles

FWD EMERGENCY EXIT DOOR LOWER LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 69,187 hrs · 62,602 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,187 hrs · 62,602 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 960, STR 22L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,187 hrs · 62,602 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 945, STR 22L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,187 hrs · 62,602 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 929, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,187 hrs · 62,602 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 68,606 hrs · 62,203 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,480 hrs · 61,394 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,480 hrs · 61,394 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,480 hrs · 61,394 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,480 hrs · 61,394 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,951 hrs · 61,030 cycles

FUSELAGE SKIN CRACKED AT BS 757, STR 14R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,216 hrs · 60,485 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 24L. REPAIRED SKIN PER SWA EA.

Part: ACTUATOR — CRACKED (LT MLG) · airframe 65,970 hrs · 60,304 cycles

DURING SCHEDULED MV2 CHECK, FOUND LEFT MLG ACTUATOR BEAM ARM FWD LUG CRACKED. REMOVED AND REPLACED ACTUATOR BEAM ARM PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,498 hrs · 59,944 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: TORQUE TUBE — FAILED (ELEVATOR) · airframe 64,005 hrs · 58,836 cycles

DURING SCHEDULED 20Y CHECK, RIGHT AND LEFT ELEVATORS FAIL FREE PLAY CHECK. REMOVED AND REPLACED OUTPUT TORQUE TUBE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,987 hrs · 58,824 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,937 hrs · 58,786 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986, LBL 45 TO RBL 45. REPAIRED FLOORBEAM CHORD PER ER.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,937 hrs · 58,786 cycles

DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8L. REPAIRED FRAME PER SWA EA.

Part: KEELBEAM — CORRODED (BS 500C-500D) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND LEFT KEEL BEAM CORRODED AT BS 500C TO BS 500D, LBL 6.5. REPAIRED KEEL BEAM PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,935 hrs · 58,784 cycles

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

Part: FRAME — CRACKED (BS 616 S17R) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 616, STR 17R. REMOVED AND REPLACED FRAME CHORD PER MM.

Part: FRAME — CRACKED (BS 480 S8L) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 827) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 559) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 520 S8RL) · airframe 63,935 hrs · 58,784 cycles

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

Part: FRAME — CRACKED (BS 500A S8L) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 907 S8L) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 747 S8R) · airframe 63,935 hrs · 58,784 cycles

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

Part: FRAME — CRACKED (BS 827 S8L) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER — CRACKED (BS 360 S15L) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER 15L CRACKED AT BS 360. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500A S16R) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 360 S8L) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 559 S8R) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 520 S8-8LR) · airframe 63,935 hrs · 58,784 cycles

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

Part: FLOORBEAM — CRACKED (BS 947) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CHORD CRACKED AT BS 947, LBL 55. REPAIRED FLOORBEAM CHORD PER ER.

Part: FRAME — CRACKED (BS 827 S8LR) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 907 S8L) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (BS 194) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 194, STR 17R AND STR 17L. REPAIRED FLOORBEAM WEB PER SRM.

Part: FRAME — CRACKED (BS 480 S8L) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 747 S8R) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747 S8R. REPAIRED FRAME PER SWA EA.

Part: CLEVIS — CORRODED (HORIZONTAL STAB) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND RIGHT AND LEFT HORIZONTAL STABILIZER CLEVIS LUG FACES CORRODED. REPAIRED HORIZONTAL STABILIZER PER SRM.

Part: FRAME — CRACKED (BS 500A S8L) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 188 S17-17LR) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L AND STR 17R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,935 hrs · 58,784 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, LBL 3. REPAIRED SKIN PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 270, LBL 4 TO RBL 4. REPAIRED CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,935 hrs · 58,784 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,935 hrs · 58,784 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 1. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 500A AND BS 500C, STR 17L. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,935 hrs · 58,784 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503C, STR 15L. REPAIRED SKIN PER SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 15R. REPAIRED WEB PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT LOWER OUTBOARD END. REPAIRED SLAT PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 23L. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 23R. REPAIRED WEB PER SRM.

Part: SLAT — CRACKED (RT WING) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 5 L/E SLAT CRACKED AT LOWER INBOARD END. REPAIRED SLAT PER SRM.

Part: SKIN — DEBONDED (T/E FLAP) · airframe 63,935 hrs · 58,784 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD FORE FLAP UPPER SURFACE DISBONDED AT OUTBOARD END. REPAIRED FORE FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,527 hrs · 58,447 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 728D, STR 19R. REPAIRED SKIN PER SWA EA.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,274 hrs · 58,247 cycles

DURING SCHEDULED A2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,013 hrs · 58,099 cycles

DURING SCHEDULED A1 CHECK, FOUND FWD LEFT CABIN BULLNOSE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 62,415 hrs · 57,573 cycles

FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 6 ABC. INSTALLED LIGHT LENS PER MM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 62,022 hrs · 57,269 cycles

FLIGHT DECK L2 WINDOW ARCHED AND CRACKED IN FLIGHT. REMOVED AND REPLACED L2 WINDOW PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,658 hrs · 56,990 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 11 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — DELAMINATED (RT WING SPOILER) · airframe 61,412 hrs · 56,790 cycles

RT WING NR 7 SPOILER DELAMINATED AT INBOARD T/E. REMOVED AND REPLACED SPOILER PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 60,580 hrs · 56,132 cycles

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

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 60,580 hrs · 56,132 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT STA 240. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (BS 933) · airframe 60,580 hrs · 56,132 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 933, STR 24R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,750 hrs · 55,491 cycles

DURING SCHEDULED A1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT ASSY INOP AT ROW 23 DEF. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 59,567 hrs · 55,363 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING NR 6 L/E SLAT LOWER T/E SKIN CRACKED AT AFT RIVET ROW. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 59,567 hrs · 55,363 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING NR 4 L/E SLAT LOWER T/E SKIN CRACKED AT AFT RIVET ROW. REPAIRED SLAT PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,567 hrs · 55,363 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK INOP AT ROW 3 DEF. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,567 hrs · 55,363 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK INOP AT ROW 11 ABC. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,542 hrs · 55,342 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 430, BL 0, NR 3 RADIO ALTIMETER ANTENNA CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 59,542 hrs · 55,342 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER SPLICE CHANNEL CRACKED AT BS 351, STR 14L. REPAIRED SPLICE CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,542 hrs · 55,342 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,542 hrs · 55,342 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,515 hrs · 55,324 cycles

DURING SCHEDULED A1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK PER MM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,375 hrs · 55,223 cycles

DURING SCHEDULED PM CHECK, FOUND EMERGENCY LIGHT BATTERY CHARGER INOP AT BS 753. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 58,790 hrs · 54,772 cycles

AFT EMERGENCY AISLE LIGHT LENS MISSING ABOVE ROW 21. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (BS 740) · airframe 58,667 hrs · 54,674 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740, STR 18R. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,667 hrs · 54,674 cycles

DURING SCHEDULED RON CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CASTING — CRACKED (RT WING SPOILER) · airframe 58,667 hrs · 54,674 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING NR 5 SPOILER INBOARD ACTUATOR ATTACH POINT SUPPORT CASTING CRACKED. REMOVED AND REPLACED CASTING PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 58,667 hrs · 54,674 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 58,585 hrs · 54,602 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,554 hrs · 54,581 cycles

DURING SCHEDULED SERVICE CHECK, R2 DOOR UPPER EMERGENCY EXIT LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY PACK & CHARGER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,708 hrs · 53,128 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,708 hrs · 53,128 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,708 hrs · 53,128 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 19L TO STR 20L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,708 hrs · 53,128 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS FLOOR STRIPS INOP AT ROWS 1 TO ROWS 4, LT SIDE & ROWS 10 TO ROWS 14, RT SIDE. REMOVED AND REPLACED EEPLS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,708 hrs · 53,128 cycles

DURING SCHEDULED C4 CHECK, FOUND LEFT SIDE CABIN EMERGENCY EXIT BULLNOSE LIGHTS INOP. RECHARGED BATTERY PACKS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 56,708 hrs · 53,128 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD GALLEY OVERHEAD EMERGENCY LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,430 hrs · 52,901 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN BULLNOSE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY & POWER SUPPLY PER MM.

Part: LATCH — BROKEN (ESCAPE ROPE) · airframe 55,992 hrs · 52,558 cycles

CAPTAIN'S EMERGENCY ESCAPE ROPE COMPARTMENT LATCH BROKEN. REMOVED AND REPLACED LATCH ASSY PER MM.

Part: ACTUATOR — LEAKING (RT WING) · airframe 55,970 hrs · 52,538 cycles

DECLARED EMERGENCY. A SYSTEM HYDRAULIC LOST QUANTITY/PRESSURE. REMOVED AND REPLACED NR 7 SPOILER ACTUATOR PER MM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 55,871 hrs · 52,464 cycles

AIR TURNBACK. ON CLIMBOUT, L1 COCKPIT WINDOW ARCED & CRACKED IN 3 PLACES. REMOVED AND REPLACED L1 WINDOW PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,587 hrs · 52,242 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 518, STRINGER 12R, CRACKED. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,587 hrs · 52,242 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO COMPARTMENT SHEAR TIE AT BS 500, BL 0, CORRODED. REPAIRED SHEAR TIE PER SRM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 55,587 hrs · 52,242 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT LENS, CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,587 hrs · 52,242 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 792, STRINGER 19L, CRACKED. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,689 hrs · 51,532 cycles

DURING SCHEDULED A1 CHECK, FOUND LEFT AFT CABIN BULLNOSE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 54,541 hrs · 51,417 cycles

OVERHEAD AISLE LIGHT AT ROW 20 DEF LOOSE. SECURED LIGHT PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,507 hrs · 51,382 cycles

DURING SCHEDULED A2 CHECK, FOUND 2 EACH BULL NOSE EMERGENCY EXIT LIGHTS INOP AT ROWS 1 DEF, 2 ABC. RELAMPED BOTH LIGHTS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,457 hrs · 51,347 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 54,028 hrs · 50,982 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 53,758 hrs · 50,750 cycles

LEFT OVERWING EXIT OVERHEAD SIGN LOOSE. SECURED OVERHEAD SIGN PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,813 hrs · 49,992 cycles

DURING SCHEDULED PM CHECK, FOUND AFT BULLNOSE EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,459 hrs · 49,709 cycles

DURING SCHEDULED SPV, FOUND FUSELAGE SKIN CRACKED AT BS 500D +16, STRINGER 15R. REPAIRED SKIN PER EA.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 52,458 hrs · 49,708 cycles

DURING SCHEDULED SPV, FOUND CORROSION ON BS 1016, VERTICAL STIFFENER AT 6 O'CLOCK POSITION. REPAIRED STIFFENER PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,458 hrs · 49,708 cycles

DURING SCHEDULED SPV, FOUND FUSELAGE SKIN CRACKED AT BS 767 + 3, AT STRINGER 19R. REPAIRED SKIN CRACK PER SRM.

Part: FIRE DETECTOR — FALSE ACTIVATION (APU) · airframe 52,236 hrs · 49,519 cycles

DIVERSION, DURING CRUISE FLIGHT APU WARNING/BELL CAME ON WITH APU OFF. CW CHECKLIST, FIRED THE EXTINGUISHER, RED LIGHT WENT OUT. INSPECTED APU, HOUSING, AND TAILPIPE, FOUND NO EVIDENCE OF FIRE. REMOVED AND REPLACED THE FIRE DETECTOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,128 hrs · 49,435 cycles

DURING SCHEDULED RON, FOUND SKIN CRACKED AT BS 740, STRINGER 20R. REPAIRED SKIN CRACK PER SRM.

Part: FIRE DETECTOR — FALSE INDICATION (APU) · airframe 51,081 hrs · 48,606 cycles

DECLARED EMERGENCY, APU FIRE WARN LIGHT INDICATION. FIRE EXTINGUISHER BOTTLE DISCHARGED. C/W APU COMPT INSPECTION, NO EVIDENCE OF FIRE. REMOVED AND REPLACED APU TAILPIPE FIRE DETECTOR AND HARNESS. OPS CK GOOD PER MM.

Part: TORQUE TUBE — WORN (RT & LT ELEVATOR) · airframe 51,055 hrs · 48,585 cycles

DURING SCHEDULED C2 CHECK, BOTH LT AND RT ELEVATORS FAILED THE FREE PLAY CK. REMOVED AND REPLACED ELEVATOR CONTROL TORQUE TUBE ASSY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,055 hrs · 48,585 cycles

DURING SCHEDULED C2 CHECK, FOUND BULLNOSE EMERGENCY LIGHT INOP AT AFT CABIN. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,602 hrs · 48,202 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 50,417 hrs · 48,060 cycles

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

Part: BATTERY — FAULTY (CABIN) · airframe 50,044 hrs · 47,735 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS ILLUMINATING WHEN SWITCH IS OFF. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER FOR FWD CABIN DOOR EMERGENCY EXIT LIGHTS PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,617 hrs · 47,379 cycles

DURING SCHEDULED A1 CHECK, FOUND BOTH FWD ENTRY & FWD SVC DOOR THRESHOLD EMERGENCY EXIT LIGHTS STAY ILLUMINATED WHEN SW IS IN OFF POSITION. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: STRIP — LOOSE (CABIN) · airframe 48,336 hrs · 46,361 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROWS NR 7 AND NR 8 DEF. SECURED STRIP PER MM.

Part: LENS — MISSING (CABIN) · airframe 48,283 hrs · 46,325 cycles

DURING SCHEDULED C3 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING AT ROW 19 DEF. INSTALLED LENS PER MM.

Part: SLIDE — LOOSE (AFT SVC DOOR) · airframe 47,244 hrs · 45,495 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 54,320 hrs · 53,792 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT BASE BROKEN. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.

Part: FLOORBEAM — CORRODED (FWD CABIN) · airframe 47,141 hrs · 45,400 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 328, BL 0.0. REPAIRED FLOORBEAM PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 47,141 hrs · 45,400 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 47,141 hrs · 45,400 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14R AND 15R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 47,141 hrs · 45,400 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICES CRACKED (2 EA) AT STR 4R, BS 360 AND 908. REMOVED AND REPLACED STR SPLICES PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 47,141 hrs · 45,400 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 46,290 hrs · 44,712 cycles

DURING SCHEDULED C1 CHECK, FOUND LT OTBD T/E AFT FLAP DELAMINATED AT INBD END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,159 hrs · 43,754 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEBS CRACKED ( 2 EA ) AT BS 179, WL 227, RBL 17.1 & LBL 17.1. R&R WEBS PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,159 hrs · 73,754 cycles

DURING SCHEDULED SPECIAL VISIT FOUND VERTICAL BEAM WEB CRACKED AT BS 180, RBL 17.1 & WL 180. REPAIRED WEB PER SWA RA 1-353-2716.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,802 hrs · 43,446 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 2.25 INCHES LONG AT BS 747, BETWEEN STR 18R & 19R. REPAIRED SKIN PER SRM.

Part: SLAT — CRACKED (LH WING) · airframe 48,576 hrs · 47,277 cycles

DURING SCHEDULED C3 CHECK, FOUND # 2 L/E SLAT CRACKED 6 INCHES LONG ON LOWER SKIN, OTBD OF INBD AUX TRACK. REPAIRED SLAT PER SRM.

Part: CAP — MISSING (CABIN) · airframe 48,576 hrs · 47,277 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS END CAP MISSING AT AFT CABIN. INSTALLED END CAP PER MM.

Part: SLIDE — UNSERVICEABLE (AFT ENTRY DOOR) · airframe 44,411 hrs · 43,113 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 43,944 hrs · 42,713 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 54,568 hrs · 43,225 cycles

DURING SCHEDULED RON CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM.

Part: ATTACH FITTING — CORRODED (LH WING) · airframe 43,808 hrs · 42,594 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LH MLG WALKING BEAM ATTACH FITTING CORRODED. R&R BEAM ATTACH FITTING PER MM.

Part: COVER — LOOSE (AFT CABIN) · airframe 46,737 hrs · 42,534 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER LOOSE AT AFT CABIN. SECURED EEPLS COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,737 hrs · 42,534 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: STIFFENER — CRACKED (MLG WW) · airframe 43,445 hrs · 42,289 cycles

DURING SCHEDULED SERVICE CHECK, FOUND VERTICAL STIFFENERS CRACKED, AT MLG WHEEL WELL, BS 663, RBL 6.4, LBL 6.4. REPAIRED PER SWA RA.

Part: WEB — CRACKED (FUSELAGE) · airframe 43,445 hrs · 42,289 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BEADED WEB CRACKED AT BS 663, LBL 30. REPAIRED PER SWA TI.

Part: COVER — DAMAGED (CABIN) · airframe 42,825 hrs · 41,728 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVER DAMAGED BETWEEN ROWS 1 & 2. REMOVED AND REPLACED TRACK COVER PER MM.

Part: SENSOR — FAULTY (APU) · airframe 42,691 hrs · 41,607 cycles

DECLARED EMERGENCY. DURING APU START, APU FIRE WARNING LIGHT ILLUMINATED. APU FIRE HANDLE PULLED. NO OTHER IND OF APU FIRE. INSPECTED APU AREA FOR EVIDENCE OF FIRE. NO DEFECT NOTED. DEFERRED APU SYS. DURING RON IN HOU, FOUND APU TAILPIPE HARNESS AND SENSOR DEFECTIVE. REMOVED AND REPLACED BOTH PER MM. OPS CK GOOD. APU FIRE BOTTLE REPLACED.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 40,864 hrs · 40,061 cycles

DURING SCHEDULED C3 CHECK, FOUND BOTH FWD DOOR EVACUATON SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED BOTH SLIDES GIRT PLAY OUT PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 40,415 hrs · 39,662 cycles

DURING SCHEDULED RON, FOUND LT WING INBD T/E FLAP DELAMINATED AT LOWER SURFACE. R & R FLAP ASSY PER MM.

Part: RMI — INOPERATIVE (COCKPIT)

DIVERSION, F/O'S RMI INOP WITH HEADING FLAG IN VIEW. DIVERTED TO SEA. RESEATED F/O'S RMI, C/W BITE TEST OF IRS. OPS CK GOOD.

Part: SLIDE — DISLODGED (CABIN)

AFT ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: FRAME — CORRODED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD AFT SIDE, T-CHORD CRACKED, LBL 5.7, WL 184. REPAIRED CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE)

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AROUND FWD SERVICE DOOR UPPER FWD CORNER ON UPPER DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (ELEVATOR TAB)

DURING SCHEDULED 1/4D CHECK, FOUND RT ELEVATOR TAB CRACKED ON UPPER SKIN AT INBOARD HINGE FITTING CUT OUT. REMOVED AND REPLACED RT ELEVATOR TAB ASSY PER MM.

Part: HINGE COVER — LEAKING (PAX DOOR)

AIR TURNBACK, DURING CLIMB, A VERY LOUD PRESS LEAK NOISE OUT OF FWD ENTRY DOOR UPPER HINGE AREA. READJUSTED UPPER DOOR HINGE COVER.

Part: BATTERY PACK — INOP (CABIN)

DURING SCHEDULED RON, FOUND AFT EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — LOOSE (CABIN)

DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK LOOSE AT FWD END. REINSTALLED AND SECURED LIGHT ASSY PER MM.

Part: FAN — OVERHEATED (E&E COMPT)

AIRCRAFT DIVERSION, DURING CRUISE ALT, SMOKE SMELL IN MAIN CABIN AND COCKPIT. DIVERTED TO ABQ. FOUND EQUIPMENT COOLING FAN FAILURE. REMOVED AND REPLACED EQUIPMENT COOLING FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED 18 INCHES BELOW AFT ENTRY DOOR. REPAIRED SKIN PER SRM.

Part: LIGHT — INOP (ROW 3-5)

DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY FLOOR TRACK LIGHTS INOP AT ROWS 3 TO 5. FOUND CANNON PLUG DISCONNECTED, RECONNECTED PER MM.

Part: LIGHT — INOP (FWD ENTRY DOOR)

DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY EXIT LIGHT ABOVE FWD ENTRY DOOR INOP. FOUND DISCONNECTED CANNON PLUG. RECONNECTED CANNON PLUG PER MM.

Part: CONNECTOR — SHORTED (BS 1080)

AIR TURNBACK DUE TO AIRCRAFT YAWED IN FLIGHT. YAW DAMPER INDICATION FULL SCALE LEFT. AIRCRAFT SENT TO DALFORT AND REPAIRED INTERMITTENT SHORT AT CANNON PLUG LOCATED AT BS 1080. OPS CHECKED SYSTEM PER SWA ACO 6960-22.

Part: SKIN — CRACKED (BS 980)

DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACKED 2.5 INCH AT BS 980 S25. REPAIRED PER BOEING SRM.

Part: LAMP — FAILED (SERVICE DOOR)

DURING SCHEDULED SC CHECK, FOUND FWD SERV DOOR EMERGENCY EXIT LIGHTS INOP. RELAMPED PER MM.

Part: SHUTOFF VALVE — FAILED (NR 1 ENGINE)

NR 1 ENGINE FAILED TO START DURING PUSH BACK. RETURNS TO GATE. REMOVED AND REPLACED NR 1 ENGINE FUEL SHUTOFF VALVE PER BOEING MM. OPS CK AND LEAK CK NORMAL. (LPG 260123)

Part: WEB — CRACKED (BS 178 -186)

DURING SCHEDULED D-CHECK, FOUND FLOOR WEB CRACKED FROM BS 178 TO 186. REPLACED PER BOEING SRM.

Part: BEAM — CORRODED (BS 407)

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CORROSION AT BS 407, RBL 69, WL 207. REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 500)

DURING SCHEDULED D-CHECK, FOUND FRAMES CRACKED AT BS 500C AND A, BETWEEN S8 AND 9R. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 787)

DURING SCHEDULED D CHECK, FOUND FRAMES CRACKED AT BS 787, BETWEEN S8 AND 9R, AT BS 400, BETWEEN S8 AND 9L, AND AT BS 440, BETWEEN S8 AND 9L. REPAIRED PER BOEING SRM.

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND SIDE CHORD AT BS 178, RBL 32 CRACKED. REPLACED PER BOEING SRM.

Part: RIB — CRACKED (NR 2 PYLON)

DURING SCHEDULED D-CHECK, NR 2 PYLON AFT HALF RIB CRACKED. REPLACED PER BOEING SRM.

Part: CLIP — CRACKED (BS 727/887)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED BS 727, S11R AND AT BS 887, S10R, AT BS 663, S10L. REPLACED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKS AT LBL 7, LBL 6.7, AND RBL 4.7 AND 6.7. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 1110)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1110, JUST BELOW 13R. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 294)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 294, LBL 53. REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 986.5)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AND DENTED AT BS 986.5 TO BS 1010. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 947)

DURING SCHEDULED D-CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 947, S22L. REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 300)

DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT BS 300, WL 236, LBL 59.9. REPLACED PER BOEING SRM.

Part: SPLICE — CRACKED (BS 907)

DURING SCHEDULED D-CHECK, FOUND STR SPLICE CRACKED AT S4R, BS 907. REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 569)

DURING SCHEDULED D-CHECK, FOUND LT AND RT SKATE ANGLES CRACKED AT BS 569, RBL 48 AND LBL48. REPLACED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED D-CHECK, FOUND FWD LEFT EMERGENCY LIGHT BATTERY WILL NOT CHARGE. REPLACED BATTERY AND CHARGER PER BOEING M/M.

Part: STRINGER — CRACKED (BS 500)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP 19R CRACKED AT BS 500D. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 194/976/312)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 194, 976, 312. REPAIRED PER BOEING SRM.

Part: SILL — CORRODED (BS 953-987)

DURING SCHEDULED D-CHECK, FOUND MOPSILL CORROSION AT BS 953 TO 987, WL 209, LBL 52. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND STRINGER 17L CRACKED AT BS 178, RBL 32 WL 207. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 344, LBL 42, WL 42. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CORRODED (BS 1033)

DURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD BS 1033 CORRODED AT ATTACH SUPPORT ANGLE AT RBL 11. REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 837)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT FWD CARGO DOOR SKIN CUTOUT, BS 837. REPAIRED PER ACO 6621-53 AND BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT LBL 0.7 AND RBL 0.5. REPAIRED PER TRAMCO EWO 97-0623.

Part: SKIN — CRACKED (SERV DOORWAY)

DURING SCHEDULED D-CHECK, FOUND CRACK AT LOWER AFT CORNER OF FWD SERVICE DOORWAY CUTOUT AT BS 329, RBL 66, WL 209. REPAIRED PER BOEING SRM.

Part: SKIN — DAMAGED (BS 245.5)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DAMAGE FROM LIGHTNING STRIKES AT BS 245.5, RBL 23, AND AT BS 239, RBL 21. REPAIRED PER BOEING SRM.

Part: SKIN — CREASE (BS 460)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CREASED AT BS 460, RBL 5 LBL 5. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (SERV DOORWAY)

DURING SCHEDULED D-CHECK, FOUND CRACK AT LOWER HINGE CUTOUT, LOWER CORNER ON FUSELAGE SKIN AT AFT SERVICE DOORWAY, WL 228. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 350)

DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT BS 350, AT FWD ENTRY DOOR STOP FITTING NR 9. REPLACED PER BOEING SRM.

Part: SKIN — GOUGED (BS 367-369)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 367 TO 369, LBL 33 TO 39, ABOVE 4 AND 6L, AND AT BS 990, WL 185, S23L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (SERV DOORWAY)

DURING SCHEDULED D-CHECK, FOUND CRACK AT UPPER HINGE CUTOUT UPPER CORNER ON FUSELAGE SKIN AT AFT SERVICE DOORWAY, WL 254. REPAIRED PER BOEING SRM.

Part: CHORD — CORRODED (BS 270)

DURING SCHEDULED D-CHECK, FOUND Z-ANGLE CHORD BODY CORRODED AT BS 270. REPAIRED PER BOEING SRM.

Part: FLOOR WEB — CORRODED (BS 1030)

DURING SCHEDULED D-CHECK, FOUND FLOOR WEB BODY AT BS 1030 CORRODED. REPLACED PER BOEING SRM.

Part: STRAP — CRACKED (BS 336/330)

DURING SCHEDULED D-CHECK, FOUND STABILIZER STRAPS CRACKED AT BS 336, LBL 22, AND AT BS 330, LBL 46 WL 200. REPLACED BOTH PER BOEING SRM.

Part: SILL — CORRODED (BS 320-346)

DURING SCHEDULED D-CHECK, FOUND MOPSILL CORROSION AT BS 320 TO 346, WL 208, LBL 56 TO 59. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 1002, WL 233, LEFT SIDE AND AT BS 1130 TO 1137, AT S11L. REPAIRED PER BOEING SRM.

Part: SILL — CORRODED (BS 272-333)

DURING SCHEDULED D-CHECK, FOUND MOPSILL CORROSION AT BS 272 TO 333, WL 209, RBL 55. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 936)

DURING SCHEDULED D-CHECK, FOUND SHEAR WEB UPPER ATTACH ANGLE CRACKED AT BS 936, BL 0. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND STRINGER 17L CRACKED AT BS 178, LBL 32 WL 207. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 986, AT LBL 44. REPAIRED PER BOEING SRM.

Part: DOOR SKIN — CRACKED (AFT GALLEY)

DURING SCHEDULED B/C1 CHECK, FOUND AFT GALLEY DOOR UPPER HINGE CUTOUT TOP FWD CORNER CRACKED. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (NR 2 ENG STRUT)

DURING SCHEDULED QUARTER D-CHECK, FOUND NUMBER 2 ENGINE STRUT INNER SKIN CRACKED AT O/B EDGE OF PANEL 5827R OPENING. CRACK RUNS BEYOND STOP DRILL AND UNDER CROWN SKIN. INSTALLED DOUBLER PER ACO 6135-54.

Part: STRAP — CRACKED (BS 312)

DURING SCHEDULED QUARTER D-CHECK, FOUND STABILIZING STRAP IN E/E COMPT CRACKED AT BS 312, AT BOTTOM OF FLOORBEAM, BL 0. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: STRAP — CRACKED (BS 312)

DURING SCHEDULED 1/4 D-CHECK, FOUND STABILIZING STRAP CRACKED AT E/E COMPARTMENT, BS 312, BOTTOM OF FLOOR BEAM BL 0. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.