N692SW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,835 hrs · 59,322 cycles

FWD EEPLS INOP. RELAMPED PER MM.

Part: GASPER FAN — MALFUNCTIONED (CABIN) · airframe 82,695 hrs · 59,216 cycles

ELECTRICAL SMELL IN CABIN AT ROW 16 AND AFT. FOUND GASPER FAN CIRCUIT BREAKER TRIPPED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,625 hrs · 59,162 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 500B+14, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,625 hrs · 59,162 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 420+14, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,625 hrs · 59,162 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 907+12, STR 21R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,625 hrs · 59,162 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 465, STR 16L. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 82,625 hrs · 59,162 cycles

DURING SCHEDULED OTS CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER SOPM.

Part: LENS — BROKEN (CABIN) · airframe 82,652 hrs · 59,162 cycles

DURING SCHEDULED OTS CHECK, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 82,625 hrs · 59,162 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CRACKED AT BS 927, STR 22R. REPAIRED STRINGER PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT WING NR 4 SLAT ON I/B END DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND FWD CARGO COMPARTMENT STRINGER CORRODED BETWEEN BS 500B TO BS 500C, STR 28L. REPAIRED STRINGER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 727E, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND FWD CARGO COMPARTMENT FRAME CORRODED AT BS 500, BETWEEN STR 27R TO STR 28R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 767, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND FWD CARGO COMPARTMENT STRINGER CORRODED BETWEEN BS 500A TO BS 500B, STR 28L. REPAIRED STRINGER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND FWD CARGO COMPARTMENT FRAME CORRODED AT BS 500A, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND FWD CARGO COMPARTMENT STRINGER CORRODED BETWEEN BS 500B TO BS 500C, STR 27R. REPAIRED STRINGER PER SRM.

Part: FLAP — CRACKED (LT WING) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT WING O/B FORE FLAP CRACKED. REMOVED AND REPLACED FORE FLAP PER MT.

Part: FRAME — CORRODED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND FWD CARGO COMPARTMENT FRAME CORRODED AT BS 500C, BETWEEN STR 27L TO STR 28L. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CRACKED AT BS 907, STR 23L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED SPLICE PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED AT BS 986.5, STR 25L. REMOVED AND REPLACED STRINGER PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO FRAME CRACKED AT BS 807, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED FRAME PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT WING NR 2 SLAT T/E INBOARD END DELAMINATED. REMOVED AND REPLACED SLAT PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND ANGLE CRACKED AT BS 616, RBL 63. REPAIRED ANGLE PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO COMPARTMENT CORRODED AT BS 859, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND WEB CRACKED AT BS 616, RBL 63. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: FLAP — DELAMINATED (RT WING) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT WING O/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 3R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BE 727D, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BE 727D, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 8 O'CLOCK POSITION. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 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 82,255 hrs · 58,888 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 1L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 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 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 28L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 700, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 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 82,255 hrs · 58,888 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 82,255 hrs · 58,888 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 81,462 hrs · 58,250 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: HINGE — BROKEN (SPOILER) · airframe 81,462 hrs · 58,250 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING I/B GROUND SPOILER I/B HINGE BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 81,222 hrs · 58,058 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CORRODED AT BS 727D, STR 22L. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 81,222 hrs · 58,058 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 777, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 81,219 hrs · 58,057 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 777, STR 24L. REPAIRED SKIN PER SRM.

Part: WIRE — DAMAGED (CABIN) · airframe 81,064 hrs · 57,936 cycles

DURING SCHEDULED MV3 CHECK, FOUND AFT EMERGENCY EXIT LIGHT INOP. REPAIRED WIRE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,064 hrs · 57,936 cycles

DURING SCHEDULED MV3 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: ACTUATOR — LEAKING (SPOILER) · airframe 81,008 hrs · 57,893 cycles

DECLARED EMERGENCY, "A" HYDRAULIC SYSTEM FAILED. FOUND NR 6 FLIGHT SPOILER ACTUATOR LEAKING. REMOVED AND REPLACED NR 6 FLIGHT SPOILER ACTUATOR PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,208 hrs · 57,272 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EMERGENCY EXIT DOOR SIDEWALL LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,029 hrs · 57,126 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 750, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,029 hrs · 57,126 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 742D, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,029 hrs · 57,126 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 466, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,029 hrs · 57,126 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 734E, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,029 hrs · 57,126 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 741E, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,029 hrs · 57,126 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 727E, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,029 hrs · 57,126 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 485, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,029 hrs · 57,126 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 424, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,029 hrs · 57,126 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 781, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,029 hrs · 57,126 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 795, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,029 hrs · 57,126 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 504, STR 16R. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 80,029 hrs · 57,126 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING I/B MID FLAP T/E DELAMINATED. REPAIRED MID FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,029 hrs · 57,126 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 784, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,029 hrs · 57,126 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 795, STR 18L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 79,874 hrs · 57,008 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,145 hrs · 56,445 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,145 hrs · 56,445 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,145 hrs · 56,445 cycles

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

Part: CONTROL ROD — CORRODED (ELEVATOR TAB) · airframe 79,012 hrs · 56,341 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT ELEVATOR TAB I/B CONTROL ROD CORRODED. REMOVED AND REPLACED ROD PER EA.

Part: CONTROL ROD — CORRODED (ELEVATOR TAB) · airframe 79,012 hrs · 56,341 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT ELEVATOR TAB O/B CONTROL ROD CORRODED. REMOVED AND REPLACED ROD ASSY PER MM.

Part: CONTROL ROD — CORRODED (ELEVATOR TAB) · airframe 79,012 hrs · 56,341 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT ELEVATOR TAB O/B CONTROL ROD CORRODED. REMOVED AND REPLACED ROD ASSY PER MM.

Part: CONTROL ROD — CORRODED (ELEVATOR TAB) · airframe 79,012 hrs · 56,341 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT ELEVATOR TAB I/B CONTROL ROD CORRODED. REMOVED AND REPLACED ROD ASSY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 78,888 hrs · 56,243 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 78,888 hrs · 56,243 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,410 hrs · 55,865 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 820, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,921 hrs · 55,504 cycles

DURING SCHEDULED THRU CHECK FOUND, SKIN CRACKED AT BS 466, STR 16R. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 787, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 727B, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 887, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER AAR EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND EEPLS LIGHT INOP AT ROW 6. REMOVED AND REPLACED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CUTOUT CRACKED AT BS 305, STR 1L. REPAIRED SKIN PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 188, STR 17L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 907, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER AAR EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT CREASE BEAM CHORD CRACKED AT BS 618. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED BETWEEN BS 868 TO BS 872, STR 25L. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 500D, STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 727B, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER SRM.

Part: FITTING — DAMAGED (GIRT BAR) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING BASE DAMAGED. REMOVED AND REPLACED FITTING PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 559, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER AAR EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 4 SLAT O/B SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME ANGLE CRACKED AT BS 291, STR 11R. REMOVED AND REPLACED ANGLE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT, BETWEEN BS 290 TO BS 305, BETWEEN WL 231 TO WL 259. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND RADIO ALTIMETER BELLY SKIN CUTOUT CRACKED AT BS 410. REPAIRED SKIN PER AAR EA.

Part: LIGHT — LOOSE (CABIN) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND EEPLS LIGHT LOOSE AT ROW 5. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,287 hrs · 55,053 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED BETWEEN BS 686 TO BS 872, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,287 hrs · 55,053 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 24. REPAIRED BEAM PER AAR EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, BETWEEN RBL 1 TO RBL 3. REPAIRED WEB PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT BS 305, BETWEEN WL 257 TO WL 261. REPAIRED SKIN PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 559, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED BETWEEN BS 868 TO BS 872, STR 25L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, LBL 4. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT CREASE BEAM WEB CRACKED BETWEEN BS 636 TO BS 639, BETWEEN LBL 67 TO LBL 71. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BETWEEN BS 868 TO BS 872, STR 25L. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND NOSE WHEEL WELL CEILING WEB CRACKED AT SNUBBER ATTACHMENT, BS 253, BETWEEN RBL 7 TO LBL 7. REPAIRED WEB PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 774, STR 23L. REPAIRED SKIN PER SRM.

Part: FRAME SPLICE — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME SPLICE CRACKED AT BS 440, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 179, RBL 5.7. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 184, RBL 5.7. REPAIRED WEB PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 480, RBL 13. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT CREASE BEAM WEB CORRODED AT BS 370, BETWEEN LBL 61 TO LBL 63. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 500C, STR 26. REPAIRED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 291, WL 260. REPAIRED FRAME PER AAR EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 45. REPAIRED BEAM PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME ANGLE CRACKED AT BS 291, STR 12R. REPAIRED ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED BS 807, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND MLG WHEEL WELL KEEL BEAM PANEL SUPPORT ANGLE CORRODED AT BS 727, BETWEEN LBL 5 TO RBL 5. REMOVED AND REPLACED ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED BS 360, STR 8R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 597 TO BS 578, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 360, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 500D, STR 27L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 767, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO COMPARTMENT FRAME CRACKED AT BS 847, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SRM.

Part: BRACKET — CRACKED (EVAC SLIDE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR FWD EMERGENCY EVAC SLIDE BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO COMPARTMENT FRAME CRACKED AT BS 500C, STR 28L. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 774, STR 23L. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24. REPAIRED BEAM PER AAR EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 45. REPAIRED BEAM PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8L. REMOVED AND REPLACED CLIP PER SWA EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BETWEEN BS 188 TO BS 196, WL 208. REPAIRED SHEAR TIE PER BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 1 L/E SLAT WEDGE DELAMINATED. REPAIRED SLAT WEDGE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 13R & 14R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 2 L/E SLAT WEDGE DELAMINATED. REPAIRED SLAT WEDGE PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 3 L/E SLAT WEDGE DELAMINATED. REPAIRED SLAT WEDGE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 807, STR 8R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 847, STR 9L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM ATTACH ANGLE CRACKED AT BS 639, RBL 45.5. REMOVED AND REPLACED ANGLE PER SRM & ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8L. REPAIRED FRAME PER SRM & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SRM & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 22R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8L. REPAIRED FRAME PER SRM & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,273 hrs · 55,045 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,191 hrs · 54,990 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 955, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,191 hrs · 54,990 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 969, STR 22L. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,560 hrs · 54,560 cycles

FLT ATTENDANTS REPORTED ELECTRICAL SMOKE SMELL AT ROW 12 TO ROW 14. CEILING LIGHTS INOP IN SAME ROW. RELAMPED LIGHTS PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 76,187 hrs · 54,280 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER CORRODED BS 907, STR 25L. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 76,187 hrs · 54,280 cycles

DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CORRODED AT BS 927.5, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 76,187 hrs · 54,280 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER CORRODED BS 927, STR 25L. REPAIRED STRINGER PER SRM.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 76,187 hrs · 54,280 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN BEAR STRAP AROUND AFT SERVICE PANEL CORRODED BETWEEN BS 947.5 TO BS 967, STR 25L. REMOVED AND REPLACED BEAR STRAP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 76,187 hrs · 54,280 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER CORRODED BS 1013, STR 27L. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 76,187 hrs · 54,280 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER CORRODED BETWEEN BS 933 TO BS 973, STR 26L. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 76,187 hrs · 54,280 cycles

DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CORRODED AT BS 947.5, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 76,187 hrs · 54,280 cycles

DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CORRODED AT BS 947.5, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,187 hrs · 54,279 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 863, STR 25L. REPAIRED PER SWA EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 76,122 hrs · 54,237 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: CHARGER — FAULTY (EMERGENCY LIGHT) · airframe 75,946 hrs · 54,116 cycles

RIGHT AFT CABIN EMERGENCY EXIT LIGHTS ON. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 75,876 hrs · 54,064 cycles

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

Part: HINGE FITTING — CORRODED (NR 6 SPOILER) · airframe 74,851 hrs · 53,288 cycles

DURING SCHEDULED SPV CHECK, FOUND RIGHT WING NR 6 SPOILER INBOARD HINGE FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 74,532 hrs · 53,065 cycles

DURING SCHEDULED HC2 CHECK, FOUND FWD CARGO DOOR SKIN CRACKED AT DOOR HANDLE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,285 hrs · 52,879 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 21R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,803 hrs · 52,518 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 294 AND BS 312, STR 23R AND STR 25R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,803 hrs · 52,518 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, STR 20R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (BS 948 S21R) · airframe 73,465 hrs · 52,245 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 948, STR 21R. REPAIRED SKIN PER SRM.

Part: TANK — FOD (RT WING) · airframe 73,072 hrs · 51,926 cycles

AIR TURNBACK/INFLIGHT SHUTDOWN. CLIMBING THROUGH 22,000 FT NOTICED FUEL INBALANCE. ATTEMPTED TO BALANCE FUEL, RT FUEL TANK FELL 2,000 POUNDS BELOW LT FUEL TANK. INSPECTED FUEL SYSTEM, NO DEFECTS FOUND PER MM. AIRBORNE FROM BNA TO HOU WITH CROSSFEED VALVE OPEN, ALL BOOST PUMPS ON FUEL ONLY USED FROM RT FUEL TANK. INSPECTED FUEL TANKS, FOUND FOD IN TANKS. REMOVED FOD PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,018 hrs · 51,886 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510D, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 73,018 hrs · 51,886 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,018 hrs · 51,886 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 729E, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,018 hrs · 51,886 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513B, STR 17L. REPAIRED SKIN PER SWA EA.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 71,912 hrs · 51,016 cycles

DURING SCHEDULED MV1 CHECK, FOUND NLG W/W PRESSURE PANEL WEB CRACKED AT RIGHT BS 246, WL 170. REPAIRED WEB PER SWA EA.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 71,912 hrs · 51,016 cycles

DURING SCHEDULED MV1 CHECK, FOUND NLG W/W PRESSURE PANEL WEB CRACKED AT RIGHT BS 239, WL 170. REPAIRED WEB PER SWA EA.

Part: STRINGER — CRACKED (BS 747 S24L) · airframe 71,403 hrs · 50,626 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER 24L CRACKED AT BS 747. REPAIRED STRINGER PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT LOWER CORNER. REPAIRED FRAME PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, STR 25L. REMOVED AND REPLACED STRINGER SPLICE PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, LBL 35 TO RBL 5. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM WEB CORRODED AT BS 986, RBL 50. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (BS 992) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 992, RBL 50, WL 209. REPAIRED FRAME SECTION PER ER.

Part: FRAME — CRACKED (BS 1016 S6R) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD FRAME CRACKED AT BS 1016, STR 6R. REPAIRED CHORD PER SRM.

Part: SHEAR TIE — CORRODED (BS 986 S19R) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986.5, STR 19R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 303 S16L) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME SECTION PER ER.

Part: STRINGER — CORRODED (BS 932 S24R) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 24R CORRODED AT BS 932. REPAIRED STRINGER PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD VERTICAL STIFFENER CRACKED AT BS 178, LBL 5.7, WL 184. REPAIRED STIFFENER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 492, STR 27R. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (BS 767 S26L) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 9 TO RBL 13. REPAIRED BULKHEAD PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 277 TO BS 294, RBL 55, WL 208. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 26 TO LBL 54. REPAIRED FLOORBEAM PER SRM.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 2 O'CLOCK POSITION. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (BS 747 S21R) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 4 O'CLOCK POSITION. REPAIRED WEB PER SRM.

Part: TORQUE TUBE — CORRODED (TE FLAP) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND LEFT INBOARD FORE FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: STRINGER — CORRODED (BS 362 S28L) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 28L CORRODED AT BS 362. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (BS 787 S26R) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — DELAMINATED (LT WING MID FLAP) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING INBOARD MID FLAP OUTBOARD T/E DELMAINATED. REPAIRED MID FLAP PER SRM.

Part: SHEAR TIE — CORRODED (BS 727E S19R) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, STR 19R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FITTING — CORRODED (L1 DOOR) · airframe 71,228 hrs · 50,483 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 25R CORRODED AT BS 908. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,228 hrs · 50,483 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,228 hrs · 50,483 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 23R CORRODED AT BS 848. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 24R CORRODED AT BS 848. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND RIGHT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED AT OUTBOARD END. REPAIRED FORE FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: WEDGE — DELAMINATED (T/E FLAP) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING INBOARD MID FLAP WEDGE LOWER SKIN DELAMINATED AT OUTBOARD END. REPAIRED MID FLAP WEDGE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 22R CORRODED AT BS 848. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: TORQUE TUBE — CORRODED (LT WING TE FLAP) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: TORQUE TUBE — CORRODED (RT WING TE FLAP) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: TORQUE TUBE — CORRODED (RT WING TE FLAP9) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: TORQUE TUBE — CORRODED (LT WING TE FLAP) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: STRINGER CLIP — CRACKED (BS 767 S21R) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 767 S20R) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 20R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING INBOARD MID FLAP OUTBOARD CARRIAGE CORRODED. REMOVED AND REPLACED MID FLAP CARRIAGE PER MM.

Part: FLOORBEAM — CORRODED (BS 344) · airframe 71,228 hrs · 50,483 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, RBL 5, WL 208. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 70,739 hrs · 50,092 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 70,553 hrs · 49,946 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 70,368 hrs · 49,767 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,880 hrs · 49,420 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT EXTERIOR LIGHT INOP AT R1 DOOR. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,880 hrs · 49,420 cycles

DURING SCHEDULED SERVICE CHECK, FOUND SIDEWALL EMERGENCY EXIT LIGHT INOP AT L1 DOOR. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 69,880 hrs · 49,420 cycles

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

Part: FRAME — CRACKED (BS 348 S15L) · airframe 69,766 hrs · 49,330 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 348, STR 15L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SHEAR TIE — CRACKED (BS 967 S7L) · airframe 69,766 hrs · 49,330 cycles

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

Part: FRAME — CRACKED (BS 440) · airframe 69,766 hrs · 49,330 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR FRAME CUTOUT, FWD FRAME CRACKED AT BS 440, NR 1 AND NR 5 DOOR STOP FITTINGS. REMOVED AND REPLACED FRAME SECTION PER BOEING DRAWING AND SRM.

Part: FRAME — CRACKED (BS 291 S19R) · airframe 69,766 hrs · 49,330 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 291.5, STR 16R. REPAIRED FRAME SECTION PER ER.

Part: FRAME — CRACKED (BS 767 S14L) · airframe 69,766 hrs · 49,330 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 14L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 787 S14L) · airframe 69,766 hrs · 49,330 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 14L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 807 S14L) · airframe 69,766 hrs · 49,330 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 14L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (BS 750 S18L) · airframe 69,766 hrs · 49,330 cycles

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

Part: FRAME — CRACKED (BS 348 S15L) · airframe 69,766 hrs · 49,330 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 348, STR 15L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (BS 745 S19R) · airframe 69,766 hrs · 49,330 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 745, STR 19R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (BS 787 S14L) · airframe 69,766 hrs · 49,330 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 14L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SHEAR TIE — CRACKED (BS 967 S7L) · airframe 69,766 hrs · 49,330 cycles

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

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 69,766 hrs · 49,330 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR FRAME CUTOUT, FWD FRAME CORRODED AT STR 24R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 348 S15L) · airframe 69,766 hrs · 49,330 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 348, STR 15L. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 767 S14L) · airframe 69,766 hrs · 49,330 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 14L. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 807 S14L) · airframe 69,766 hrs · 49,330 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 14L. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 358 S15L) · airframe 69,766 hrs · 49,330 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 358, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SKIN — CRACKED (BS 943 S23L) · airframe 69,766 hrs · 49,330 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 23L. REPAIRED SKIN PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 358 S14L) · airframe 69,766 hrs · 49,330 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 358, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 358) · airframe 69,766 hrs · 49,330 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 358, STR 16L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: CASTING — BROKEN (LT SPOILER) · airframe 69,585 hrs · 49,192 cycles

LT WING NR 4 GROUND SPOILER HINGE CASTING BROKEN. REMOVED AND REPLACED NR 4 SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,481 hrs · 49,109 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503, STR 15L, ABOVE WING ILLUMINATION LIGHT. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (BS 739E) · airframe 69,159 hrs · 48,860 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739E, STR 22R. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (BS 941-944) · airframe 68,863 hrs · 48,634 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 941 TO BS 944.5, STR 23R. REPAIRED SKIN PER SWA EA & SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 68,746 hrs · 48,545 cycles

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

Part: SKIN — CRACKED (BS 783) · airframe 68,731 hrs · 48,534 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 783, BETWEEN STR 21L TO STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 272) · airframe 68,731 hrs · 48,534 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 272, STR 16L. REPAIRED SKIN PER SWA EA & SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,354 hrs · 48,239 cycles

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

Part: SKIN — CRACKED (BS 501D-503D) · airframe 68,253 hrs · 48,165 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 501D TO BS 503D, STR 12L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 494-496) · airframe 68,253 hrs · 48,165 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 494 TO BS 496, STR 10R. REPAIRED SKIN PER SWA EA AND SRM.

Part: BULKHEAD — CRACKED (BS 178) · airframe 68,253 hrs · 48,165 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 178 BLKHD, RBL 5.7, WL 184. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (BS 500A) · airframe 68,232 hrs · 48,147 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (L2 DOOR) · airframe 68,232 hrs · 48,147 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT, UPPER AFT CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 733D-740D) · airframe 68,232 hrs · 48,147 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 733D TO BS 740D, STR 21R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 522) · airframe 68,232 hrs · 48,147 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT EXTERNAL A/C SUPPLY ACCESS CUTOUT, FWD LT CORNER, BS 522.35, STR 28L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 510) · airframe 68,232 hrs · 48,147 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 757) · airframe 68,232 hrs · 48,147 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 21R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 737) · airframe 68,232 hrs · 48,147 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737, STR 19L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,317 hrs · 47,421 cycles

DURING SCHEDULED C2 CHECK, FOUND RT CABIN AISLE BULLNOSE EMERGENCY LIGHT INOP AT ROW 19 AND ROW 20. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — DELAMINATED (LT WING FOREFLAP) · airframe 67,317 hrs · 47,421 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING OTBD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: SKIN — CRACKED (BS 365) · airframe 67,317 hrs · 47,421 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 365, STR 19R. REPAIRED SKIN PER SWA EA AND SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,812 hrs · 47,011 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR VERTICAL EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM.

Part: CONTROLLER — INOPERATIVE (CABON PRESSURE) · airframe 66,658 hrs · 46,877 cycles

AIR TURNBACK, AUTO STANDBY & DC FUNCTION INOP ON PRESSURIZATION CONTROL PANEL. REMOVED AND REPLACED AUTO PRESSURIZATION CONTROLLER PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 66,361 hrs · 46,663 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,347 hrs · 46,652 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 & R2 DOOR) · airframe 66,064 hrs · 46,430 cycles

L2 & R2 EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,824 hrs · 46,235 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 969.5, STR 21L. REPAIRED SKIN PER SRM.

Part: BOTTLE — DISCHARGED (R1 DOOR SLIDE) · airframe 65,790 hrs · 46,207 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,891 hrs · 45,507 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 18R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,382 hrs · 45,090 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 500A, STRINGER 10R, CRACKED. REPAIRED SKIN PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 64,382 hrs · 45,090 cycles

DURING SCHEDULED C3 CHECK, FOUND RT AFT CABIN LOWER EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,382 hrs · 45,090 cycles

DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 760, STRINGER 19L AND BS 750, STRINGER 18R. REPAIRED SKIN SECTIONS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,966 hrs · 44,776 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 22L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,495 hrs · 44,383 cycles

DURING SCHEDULED C2 CHECK, FOUND TEAR STRAP AT BS 890, STRINGER 24R, CRACKED. REPAIRED STRAP PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,495 hrs · 44,383 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 877, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 63,495 hrs · 44,383 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 63,123 hrs · 44,065 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BOTH LT AND RT NR 1 COCKPIT WINDOW POSTS CRACKED AT UPPER CORNERS. REPAIRED RT AND LT WINDOW POSTS PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,123 hrs · 44,065 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 349, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,123 hrs · 44,065 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 500D, STRINGER 27L, CRACKED. REPAIRED SHEAR TIE PER SRM.

Part: STIFFENER — CORRODED (BULKHEAD) · airframe 63,123 hrs · 44,065 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RADIAL STIFFENER AT BS 1016, BL 0, CORRODED. REPAIRED STIFFENER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,123 hrs · 44,065 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 959, STRINGER 17L, CRACKED. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,123 hrs · 44,065 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 25L, BS 969, CORRODED. REPAIRED STRINGER SECTION PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,123 hrs · 44,065 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 665, LBL 30.5, CRACKED. REMOVED AND REPLACED BEADED PRESSURE WEB SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,123 hrs · 44,065 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIES AT BS 500B, LBL 18, BS 500C, LBL 18, BS 500D, LBL 16 TO LBL 19, CORRODED. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,123 hrs · 44,065 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 727D + 6', LBL 2 TO RBL 7, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,123 hrs · 44,065 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 27L AT BS 500D, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,123 hrs · 44,065 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 480, LBL 18, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 63,123 hrs · 44,065 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,123 hrs · 44,065 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 847, RBL 14, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,123 hrs · 44,065 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 767, BETWEEN STRINGER 25R AND STRINGER 26R, CORRODED. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,123 hrs · 44,065 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 27R, BS 500B AND STRINGER 25L, BS 956, CORRODED. REPAIRED STRINGER SECTIONS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,123 hrs · 44,065 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 303.9, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 63,102 hrs · 44,046 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,563 hrs · 43,605 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 515, STRINGER 12R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,563 hrs · 43,605 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM.

Part: FITTING — BROKEN (LT WING) · airframe 62,166 hrs · 43,270 cycles

LT WING OUTBD FORE FLAP ATTACH FITTING BROKEN. REMOVED AND REPLACED LT WING OUTBD FORE FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 61,994 hrs · 43,141 cycles

DURING SCHEDULED A2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 61,898 hrs · 43,068 cycles

RT WING OUTBOARD AFT FLAP T/E DELAMINATED. REPAIRED RT WING T/E FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,585 hrs · 42,830 cycles

DURING SCHEDULED C4 CHECK, FOUND SKIN CRACKS AT BS 520, STRINGER 10R AND BS 747, STRINGER 23R. REPAIRED SKIN CRACKS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,902 hrs · 47,294 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 727E -747, STR 21R. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 60,902 hrs · 42,294 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 201, RBL 5.5. REPAIRED WEB PER SRM.

Part: SKIN — BULGED (RT WING TE FLAP) · airframe 60,902 hrs · 42,294 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND RT WING OUTBD MID FLAP SKIN BULGED. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,661 hrs · 42,094 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,895 hrs · 41,460 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 767 AT STR 24L AND BS 870 AT STR 24R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,993 hrs · 40,751 cycles

DURING SCHEDULED C3 CHECK, FOUND SEVERAL LOWER EMERGENCY EXIT LIGHTS AT BOTH CABIN SVC DOORS AND FWD ENTRY DOOR LAMPS INOP. RELAMPED EXIT LIGHTS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,993 hrs · 40,751 cycles

DURING SCHEDULED C1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.

Part: CABLE — MISROUTED (SERVICE DOOR) · airframe 58,993 hrs · 40,751 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,993 hrs · 40,751 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED JUST AFT OF BS 727E, STR 24L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,661 hrs · 39,636 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: SKIN — CRACKED (AFT SVC DOOR) · airframe 57,219 hrs · 39,312 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD LOWER CORNER OF AFT SVC DOOR CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,219 hrs · 39,312 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 22R. REPAIRED SKIN PER SRM.

Part: CIRCUIT BOARD — FAULTY (E/E COMP) · airframe 56,908 hrs · 39,072 cycles

NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER RAISING GEAR HANDLE. REMOVED AND REPLACED PRINTED CIRCUIT BOARDS M983 AND M1215 PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 58,419 hrs · 37,769 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 55,410 hrs · 37,871 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SPAR — CORRODED (HORIZ STAB) · airframe 54,969 hrs · 37,502 cycles

DURING SCHEDULED D-CHECK, FOUND LT STAB UPPER REAR SPAR CHORD CORRODED 37 INCHES FROM OUTBOARD END. REPAIRED SPAR CHORD PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,969 hrs · 37,502 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 294, WL 208 AND LBL 47. REPAIRED FLOORBEAM PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,969 hrs · 37,502 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 312, WL 254 AND LBL 61. REPAIRED FRAME PER SRM.

Part: SKIN — CORRODED (FUSELAGE.) · airframe 54,969 hrs · 37,502 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 468, UNDER NR 1 DME ANTENNA. REPAIRED SKIN PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 54,969 hrs · 37,502 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED, BS 867 AND BS 887, LT SIDE. REPAIRED CREASE BEAM PER SRM.

Part: CLIP — CRACKED (AFT FUSELAGE) · airframe 54,969 hrs · 37,502 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED, BS 1104, STRINGER 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,969 hrs · 37,502 cycles

DURING SCHEDULED D CHECK, FOUND 2 EA STRINGER CLIPS CRACKED, BS 663, STRINGERS 10L AND 10R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 54,969 hrs · 37,502 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEBS CORRODED, BS 790 RT SIDE AND BS 639 TO 663 LT SIDE. REPAIRED WEB SECTIONS PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,969 hrs · 37,502 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED, BS 360, BETWEEN STRINGERS 14L AND 15L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,969 hrs · 37,502 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA STRINGER CLIPS CRACKED, BS 597, STRINGERS 5L AND 7L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 54,969 hrs · 37,502 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 24L CORRODED, BS 500B+9. REPAIRED STRINGER SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,969 hrs · 37,502 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION AT FLOORBEAM UPPER CHORD, BS 312, LBL 20 TO RBL 22, WL 208. REMOVED AND REPLACED UPPER CHORD SECTION PER SRM.

Part: FRAME — CRACKED (AFT CABIN) · airframe 54,969 hrs · 37,502 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT 2 EA PLACES, BS 616, LBL65 AND RBL 65, WL 200. REPAIRED FRAME PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 54,506 hrs · 37,131 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER LOOSE AT ROW 1. SECURED COVER PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 54,396 hrs · 37,036 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND WEB CRACKED ( 3 EA )AT BS 178, BETWEEN LBL 1.0 & LBL 12.0, BETWEEN WL 187 & WL 218. REPAIRED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 54,396 hrs · 37,036 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND WEB CRACKED AT BS 178, WL 187 & RBL 1.0. REPAIRED WEB PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,396 hrs · 37,036 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND INTERCOSTAL CRACKED AT BS 178, LBL 24 & WL 207. REPAIRED INTERCOSTAL PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 54,396 hrs · 37,036 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEBS CRACKED (2 EA) AT BS 178, RBL 17.1 & WL 235, LBL 17.1 & WL 227. REMOVED AND REPLACED WEBS PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 54,396 hrs · 37,036 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND L ANGLES CRACKED ( 2 EA ) AT BS 178, WL 207, LBL 24 & RBL 24. R&R ANGLES PER SRM.

Part: TRACK — LOOSE (CABIN) · airframe 53,751 hrs · 36,471 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: SLAT — CRACKED (RH WING) · airframe 53,742 hrs · 36,463 cycles

DURING SCHEDULED C3 CHECK, FOUND 2 EA CRACKS AT # 5 L/E SLAT LOWER SKIN AFT ROW OF RIVETS, CRACKS ARE 1 & 5/8 IN LENGTH. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,763 hrs · 35,612 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD UPPER CORNER OF AIRSTAIR DOOR CUTOUT. REPAIRED SKIN PER SWA RA.

Part: FLAP — DELAMINATED (LT WING) · airframe 52,763 hrs · 35,612 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD FOREFLAP DELAMINATED AT T/E, INBOARD CORNER. REMOVED AND REPLACED FOREFLAP PER MM.

Part: COVER — LOOSE (CABIN) · airframe 52,763 hrs · 35,612 cycles

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

Part: CONNECTOR — INOPERATIVE (COCKPIT) · airframe 51,788 hrs · 34,856 cycles

AIR TURNBACK, L1 WINDOW HEAT WENT INOP. RETURNED TO OAK PER DISPATCH REQUEST. R&R WINDOW HEAT CONTROLLER & FOUND CANNON PLUG D4640 LOOSE. RECONNECTED AND OPS CHECK GOOD PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 51,752 hrs · 34,824 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE ASSY PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 51,568 hrs · 34,655 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN BULGED AFT OF E&E DOOR (APPROX BS 360), RBL 4 TO LBL 12. REPAIRED SKIN PER SRM.

Part: INDICATOR — ERRATIC (COCKPIT) · airframe 50,416 hrs · 33,701 cycles

AIR TURNBACK, NR 1 ENG OIL TEMP INDICATED 165 DEGS. ATTEMPTED TO REDUCE TEMP BY REDUCING POWER, NO EFFECT. DURING DESCENT OIL TEMP INDICATION BECAME ERRATIC, THEN STABILIZING TO 120 DEG. REMOVED AND REPLACED NR 1 ENG OIL TEMP IND AND OIL TEMP BULB PER MM.

Part: SKIN — CRACKED (BS 747)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 747, BETWEEN STRINGERS 22R-23R. REPAIRED SKIN PER SRM.

Part: KEEL BEAM — CORRODED (BS 610-630)

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM STRESS PANEL CORRODED BETWEEN BS 610 TO BS 630. REMOVED AND REPLACED PANEL PER ER 99-6004.

Part: SKIN — CRACKED (FUSELAGE.)

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUT OUT FUSELAGE SKIN CRACKED. REPAIRED SKIN PER ER NR 99-5992.

Part: KEEL BEAM — CORRODED (BS 500-727)

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CORRODED ON RT LOWER CHORD. REMOVED AND REPLACED KEEL BEAM RT LOWER CHORD FROM BS 500D TO 727 PER SRM.

Part: SPLICE — CRACKED (BS 727)

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM INBD TEE SPLICES CRACKED, BS 727, BOTH LT AND RT SIDES. REMOVED AND REPLACED TEE SPLICES PER SRM.

Part: ANGLE — CORROSION (BS 727)

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM SUPPORT ANGLE CORRODED, BS 727, LBL 8. REMOVED AND REPLACED SUPPORT ANGLE PER SRM.

Part: SHEAR TIE — CRACKED (BS 520)

DURING SCHEDULED 1/4D CHECK, FOUND BS 520 SHEAR TIE CRACKED, STRINGER 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STOP — WORN (RT EMER EXIT DR)

DURING SCHEDULED C3 CHECK, FOUND SEVERAL WORN STOPS AT RT EMERGENCY OVERWING EXIT HATCH. REMOVED AND REPLACED STOPS PER MM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED SC CHECK, FOUND (EMERGENCY EXIT ROW) ONE EMERGENCY LIGHT INOP FLOOR TRACK LIGHTING. RELAMPED PER MM.

Part: LIGHT — INOP (CABIN)

DURING SCHEDULED SC CHECK, FOUND (EMERGENCY EXIT ROW) ONE EMERGENCY FLOOR TRACK LIGHT INOP. RELAMPED FLOOR TRACK LIGHT PER M/M.

Part: SENSOR — FAILED (RT MLG)

AIRCRAFT EN ROUTE FROM TPA TO ABQ DIVERTED DUE TO RIGHT LANDING GEAR RED LIGHT FLICKERS ON AND OFF CRUISE. THREE GREEN LIGHTS FOR LANDING. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED RT MAIN LANDING GEAR UPLOCK SENSOR. GEAR SWUNG. OPS CHECK GOOD PER BOEING MM.

Part: SKIN — DENTED (LT HORIZ STAB)

DURING SCHEDULED BC 3 CHECK, FOUND LT HORIZ STAB HAS A DENT 4 FT FROM FUSELAGE. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — PUNCTURED (BS 870)

DURING WALKAROUND CHECK, FOUND A SKIN PUNCTURE AND 7 CREASE AT BS 870 BETWEEN STRINGERS 25 AND 26. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (R1 DOORWAY)

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER AFT R1 DOOR CUTOUT. REPAIRED PER BOEING SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED RON CHECK, FOUND FWD EGRESS LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING MM.

Part: BATTERY — DISCHARGED (CABIN)

DURING RON CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT FWD SERVICE DOOR AND AFT BULLNOSE. REPLACED BATTERY PACK PER BOEING M/M.

Part: TAT PROBE — INOPERATIVE (FUSELAGE)

DIVERTED TO PHX, DUE TO TAT PROBE HEAT INOP. REMOVED AND REPLACED TAT PROBE AND OP CHECKED PER BOEING M/M.

Part: FLOORBEAM — CORRODED (BS 727-947)

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORROSION AROUND NUTPLATES AT BS 727-947, RBL 3 AND 8. REPLACED FLOORBEAM SECTION PER BOEING SRM.

Part: SKIN — GOUGED (BS 817)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 817, RBL 26. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED D-CHECK, FOUND AFT ENTRY DOOR AND AFT SERVICE DOORS UPPER HINGE CUTOUTS CRACKED. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED BC3 CHECK, FOUND AFT SERVICE DOOR LOWER HINGE OPENING, LOWER FWD CORNER CRACKED EXTENDING FROM OPENING TO UNDER DOUBLER PLATE. REPAIRED PER SWA RA 1-353-1659.

Part: CONNECTOR — SHORTED (NR 1 ENG TR UNIT)

EN ROUTE, NR 1 ENGINE REVERSER UNLOCKED LIGHT ILLUMINATED, ACCOMPANIED BY MID CABIN VIBRATION AND NOISE. AIRCRAFT DIVERTED TO HOU AND MADE AN UNEVENTFUL LANDING. TROUBLESHOT AND FOUND A SHORT AT ISOLATION VALVE CONNECTOR PLUG. REPLACED CONNECTOR PER BOEING M/M.

Part: SENSORS — OUT OF ADJUST (NR 1 ENGINE)

EN ROUTE, NR 1 ENGINE REVERSER LIGHT ILLUMINATED INTERMITTENTLY FOR ABOUT 40 SECONDS, ALONG WITH SLIGHT VIBRATION AT MID CABIN AREA. ALSO, OVERHEAD REVERSER LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO ABQ AND MADE AN UNEVENTFUL LANDING. LOCKED OUT REVERSER PER SPECIAL PROCEDURES. LANDED WITHOUT INCIDENT. ADJUSTED REVERSER UNLOCK SENSORS PER BOEING M/M.

Part: FLOORBEAM — CRACKED (CABIN)

DURING SCHEDULED C1 CHECK, FOUND FLOORBEAM STRAP CRACKED UNDERNEATH FWD ENTRY DOOR. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — BROKEN (BS 312)

DURING SCHEDULED C1 CHECK, FOUND FLOORBEAM STRAPS BROKEN AND CRACKED ABOVE AIRSTAIR SHROUD AT BS 312, BL 0 AND BL 12. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 328)

DURING SCHEDULED C1 CHECK, FOUND FLOORBEAM STRAP CRACKED ABOVE AIRSTAIR SHROUD AT BS 328, LBL 12 AND 33. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING WALKAROUND CHECK, FOUND CABIN AFT UPPER EMERGENCY FLASHLIGHT WOULD NOT CHARGE. REPLACED BATTERY PER BOEING M/M.

Part: ELEV FEEL UNIT — MALFUNCTIONED (TAIL)

AIRCRAFT WAS DIFFICULT TO ROTATE ON TAKEOFF. NOSE WOULD NOT COME UP WITH NORMAL BACK PRESSURE. NOSE FINALLY ROSE AFTER SEVERAL INCHES OF ADDITIONAL YOKE DISPLACEMENT. RESISTANCE WAS NOT EXCESSIVE, BUT DISPLACEMENT WAS. RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. REPLACED ELEVATOR FEEL AND CENTERING UNIT PER BOEING M/M. UNIT WAS FOUND TO HAVE A BENT INPUT ARM.

Part: HYD LINE — RUPTURED (RT MLG)

DURING CLIMBOUT, EXPERIENCED SYSTEM A HYDRAULIC PRESSURE LOSS. AIRCRAFT RETURNED TO ONT AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND HYDRAULIC LINE TO RIGHT MAIN GEAR UPLOCK ACTUATOR RUPTURED. REPLACED LINE AND SERVICED SYSTEM PER BOEING M/M.