N644SW

Part: ACTUATOR — CRACKED (RT SPOILER) · airframe 58,908 hrs · 46,499 cycles

RIGHT WING NR 5 GND SPOILER OTBD ACTUATOR ROD END CRACKED. R & R ACTUATOR IAW AMM.

Part: CASTING — BROKEN (RT SPOILER) · airframe 58,908 hrs · 46,499 cycles

RIGHT WING NR 5 GND SPOILER INBD HINGE POINT CASTING BROKEN. REPLACED NR 5 GND SPOILER IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 58,857 hrs · 46,464 cycles

LEFT OVERWING EMER EXIT SIGN LOOSE ON MOUNT. SECURED SIGN IAW AMM.

Part: LEVER — FAULTY (COCKPIT) · airframe 57,737 hrs · 45,665 cycles

AFTER GEAR EXTENSION ALL GREEN & ALL RED LIGHTS WERE ILLUMINATED. RETRACTED LG & EXTENDED GEAR A SECOND TIME. AFTER SECOND EXTENSION LIGHTS WERE NORMAL. R & R LG LEVER ASSEMBLY IAW MM.

Part: SENSOR — OUT OF ADJUST (CONTROL LEVER) · airframe 57,718 hrs · 45,646 cycles

DURING APPROACH, LOWERED LANDING GEAR AND THREE RED & THREE GREEN LIGHTS. WENT AROUND, CYCLED GEAR, AND RECEIVED THREE GREEN LIGHTS, NO RED. ADJUSTED LANDING GEAR LEVER CONTROL POSITION SWITCH SENSOR IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,009 hrs · 45,172 cycles

R2 DOOR FUSELAGE SKIN CUT OUT CRACKED AT FWD, LOWER RADIUS BS 844. REPAIRED SKIN CRACK IAW SRM.

Part: ANGLE — CRACKED (LT AILERON) · airframe 57,009 hrs · 45,172 cycles

LEFT WING AILERON BALANCE BAY ANGLE CRACKED AT NR 3 HINGE AREA. R & R ANGLE IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,951 hrs · 45,132 cycles

LEFT EMER LIGHT INOPERATIVE BETWEEN ROW 3 TO 6. R & R BATTERY PACK IAW AMM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 56,397 hrs · 44,764 cycles

NUMBER 7 SPOILER DELAMINATED. R & R SPOILER ASSEMBLY IAW MM.

Part: FUSE — BLOWN (CABIN) · airframe 56,393 hrs · 44,763 cycles

L1 OVERHEAD EMER EXIT LIGHT INOPERATIVE. R & R FUSE IAW AMM.

Part: FUSE — BLOWN (CABIN) · airframe 56,393 hrs · 44,763 cycles

R2 OVERHEAD EMER EXIT LIGHT INOPERATIVE. R & R FUSE IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,393 hrs · 44,763 cycles

LEFT BULLNOSE EMER EXIT LIGHTS INOPERATIVE BETWEEN ROW 3 TO 6. R & R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,393 hrs · 44,763 cycles

L1 DOOR EXTERNAL EMER EXIT LIGHT INOPERATIVE. RE LAMPED LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,393 hrs · 44,763 cycles

RIGHT BULLNOSE EMER EXIT LIGHTS INOPERATIVE AT ROW 16. R & R BULB IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,393 hrs · 44,763 cycles

STRINGER CLIP CRACKED AT BS 380, STRINGER 8L. R & R CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,393 hrs · 44,763 cycles

LEFT BS 887+10 UPPER AFT WINDOW CORNER SKIN CRACKED AT HOLE NR 3. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,393 hrs · 44,763 cycles

SHEAR TIE CRACKED AT BS 380, BETWEEN STRINGER 14L TO 15L. R & R SHEAR TIE IAW DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,393 hrs · 44,763 cycles

SHEAR TIE CRACKED AT BS 380, BETWEEN STRINGER 13L TO 14L. R & R SHEAR TIE IAW DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,393 hrs · 44,763 cycles

SHEAR TIE CRACKED AT BS 380, BETWEEN STRINGER 13L TO 14L. R & R SHEAR TIE IAW DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,393 hrs · 44,763 cycles

LEFT BS 787+10 LOWER FWD WINDOW CORNER SKIN CRACKED AT HOLE NR 10. R & R SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,393 hrs · 44,763 cycles

LEFT BS 807+10 UPPER AFT WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW SB.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,393 hrs · 44,763 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 8R. R & R CLIP IAW DWG & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,393 hrs · 44,763 cycles

STRINGER CLIP CRACKED AT BS 5004, STRINGER 8R. R & R CLIP IAW DWG & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,393 hrs · 44,763 cycles

STRINGER CLIP CRACKED AT BS 400, STRINGER 8L. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,393 hrs · 44,763 cycles

STRINGER CLIP CRACKED AT BS 597, STRINGER 10L. R & R CLIP IAW DWG & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,393 hrs · 44,763 cycles

STRINGER CLIP CRACKED AT BS 597, STRINGER 5L. R & R CLIP IAW DWG & SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,393 hrs · 44,763 cycles

SHEAR TIE CRACKED AT BS 500D, BETWEEN STRINGER 11R TO 12R. R & R SHEAR TIE IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,393 hrs · 44,763 cycles

STRINGER CLIP CRACKED AT BS 663, STRINGER 10L. R & R CLIP IAW DWG & SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 56,393 hrs · 44,763 cycles

R2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW TC.

Part: BEAM — CRACKED (FUSELAGE) · airframe 55,897 hrs · 44,376 cycles

VERTICAL BEAM CRACKED AT BS 178, RBL 5.7. REPAIRED BEAM IAW EA.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 55,897 hrs · 44,376 cycles

RIGHT WW OTBD TOWER SHAFT SUPPORT CHANNEL OUTER CHORD CRACKED AT BS 348. REPAIRED CHORD IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 55,897 hrs · 44,376 cycles

EXTERIOR FUSELAGE SKIN CORRODED UNDER AFT LAVATORY PAN. REPAIRED SKIN IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 55,897 hrs · 44,376 cycles

SKIN CORRODED BETWEEN BS 986.5+7 INCHES TO 986.5+13 INCHES RBL 8. REPAIRED SKIN IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,897 hrs · 44,376 cycles

INTERCOSTAL WEB CRACKED AT BS 348.2 STRINGER 16L. R & R WEB IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 55,897 hrs · 44,376 cycles

CLIP CRACKED AT BS 348 STRINGER 16L. R & R CLIP IAW EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 55,897 hrs · 44,376 cycles

INTERCOSTAL TO WEB BOTTOM ATTACH CLIP CRACKED AT BS 348 STRINGER 16L. R & R CLIP IAW EA.

Part: STRUCTURE — CRACKED (RT WING) · airframe 55,897 hrs · 44,376 cycles

RIGHT WING TANK LOWER CHORD CUT OUT CRACKED AT RIB 135.5 STRINGER L2. REPAIRED CHORD IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,897 hrs · 44,376 cycles

L1 DOOR AFT FRAME ANGLE CRACKED AT BS 360 STRINGER 15L. R & R ANGLE IAW SRM & DWG.

Part: REINFORCEMENT — CRACKED (FUSELAGE) · airframe 55,897 hrs · 44,376 cycles

FORWARD ENTRY DOOR AFT SIDE OF FRAME 348 STRINGER 16L WEB REINFORCEMENT CRACKED. R & R WEB IAW EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 55,897 hrs · 44,376 cycles

FORWARD PAX DOOR FRAME INNER CHORD CRACKED BS 348 AT FLOOR LEVEL FASTENER HOLE. R & R CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,897 hrs · 44,376 cycles

LEFT FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727 STRINGER 18A. REPAIRED CHORD IAW SWA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 55,897 hrs · 44,376 cycles

MAIN WW PRESS DECK WEB CRACKED BETWEEN BS 663.75 TO 675 BETWEEN RBL 37 TO 44. REPAIRED WEB IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 55,897 hrs · 44,376 cycles

Z CHANNEL CORRODED AT BS 500C+12 LBL 24. REPAIRED Z CHANNEL IAW SRM.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 55,897 hrs · 44,376 cycles

AFT CARGO DOOR FWD END OF CROSSBEAM OUTER CHORD CRACKED. REPAIRED DOOR IAW EA.

Part: PUMP — FAULTY (NR 2 ENGINE) · airframe 55,386 hrs · 44,023 cycles

NR 2 N1 IN CLIMB POWER GOING .6% UP TO .6% BELOW CLIMB POWER BRING BACK POWER A LITTLE & N1 WAS NORMAL. R & R NR 2 ENG FUEL PUMP IAW MT.

Part: ACTUATOR — OUT OF ADJUST (RT SPOILER) · airframe 54,878 hrs · 43,687 cycles

RIGHT WING NR 5 GND SPOILER OTBD ACTUATOR ROD END OUT OF ADJUSTMENT. R & R ACTUATOR IAW AMM.

Part: SPOILER — OUT OF ADJUST (RT WING) · airframe 54,878 hrs · 43,687 cycles

RIGHT WING NR 5 GND SPOILER INBD ACTUATOR OUT OF ADJUSTMENT. R & R SPOILER IAW AMM.

Part: LUG — BROKEN (RT SPOILER) · airframe 54,873 hrs · 43,683 cycles

RIGHT WING NR 5 INBD GND SPOILER INBD ACTUATOR LUG BROKEN. R & R SPOILER IAW AMM.

Part: SLAT — DELAMINATED (RT WING) · airframe 54,108 hrs · 43,161 cycles

RT WING NR 5 SLAT OTBD UPPER AFT AREA DELAMINATED. R & R SLAT IAW AMM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 53,065 hrs · 42,384 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. R&R SLIDE IAW MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,169 hrs · 41,726 cycles

FUSELAGE SKIN CRACKED AT STA 500B +9, ABOVE STR 10R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,169 hrs · 41,726 cycles

FUSELAGE SKIN CRACKED AT BS 500C+14, STR 10L. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 51,543 hrs · 41,280 cycles

R1 DOOR SLIDE LOWER FLAP REQUIRES REPOSITION. RE-INSTALLED PER M/M R1 DOOR SLIDE, C/W M/T 325-61-06

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 51,543 hrs · 41,280 cycles

L1 DOOR SLIDE LOWER FLAP REQUIRES REPOSITION. RE-INSTALLED PER M/M L1 DOOR SLIDE, C/W M/T 325-61-06

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,076 hrs · 40,944 cycles

EMERGENCY LIGHT ABOVE ROW 12DEF INOP. RELAMPED, OPS CHECK GOOD PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

WEB CRACKED BETWEEN BS 867 TO BS 887, STR 25R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 50,042 hrs · 40,178 cycles

LEFT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

FLOORBEAM CRACKED AT BS 328, RBL 59.9. REPAIRED BEAM IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

SHEAR TIE ANGLE CORRODED AT BS 520, BETWEEN STR 27L TO STR 28L. REPLACED ANGLE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

SHEAR TIE ANGLE CORRODED AT BS 500D, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE AW SRM AND DWG.

Part: BEAM — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

L1 DOOR CHANNEL BEAM CRACKED BETWEEN BS 312 TO STA 344 IN LOWER SILL. REMOVED AND REPLACED BEAM IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

VERTICAL BEAM WEB CRACKED AT BS 178, AT RBL 17. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17.0. REPAIRED WEB IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

STRINGER CLIP CRACKED AT BS 380, STRINGER 22L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

TIE CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

ANGLE CORRODED AT BS 360, STR 28L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

CORROSION ON ANGLE AT STA 360, STR 28L. REMOVED AND REPLACED ANGLE PER SRM.

Part: RIB — CRACKED (TE FLAP) · airframe 50,042 hrs · 40,178 cycles

RIGHT WING O/B FORE FLAP O/B HINGE RIB CRACKED AT WBL 355. REMOVED AND REPLACED RIB IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

TIE CLIP CRACKED AT BS 767, STR 16R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

TIE CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

TIE CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

SUPPORT ANGLE CRACKED AT BS 727B, RBL 45.5. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

WEB CRACKED BETWEEN BS 727E TO BS 747, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

L1 DOOR THRESHOLD WEB CORRODED BETWEEN BS 312 TO BS 344. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

TIE CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

ANGLE CRACKED AT BS 787+3, BETWEEN STR 18R TO STR 19R. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

PRESSURE BULKHEAD SKIN CORRODED AT BS 1016, BETWEEN STR 26L TO STR 27R. REPAIRED SKIN IAW ACO AND DWG.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

SUPPORT BRACKET CRACKED AT BS 947.5, BETWEEN STR 24L TO STR 25L. REMOVED AND REPLACED BRACKET IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

WEB CORRODED BETWEEN BS 727D TO BS 727E, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

STRINGER CORRODED AT BS 952, STR 20R. REPAIRED STRINGER PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

SUPPORT ANGLE CRACKED AT BS 727+5, BETWEEN STR 25L TO STR 25R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STR 24R TO STR 25R. REPAIRED FRAME IAW EA.

Part: ANGLE — CRACKED (RT WING) · airframe 50,042 hrs · 40,178 cycles

RIGHT WING TRAILING EDGE ANGLE CRACKED AT RSS 533+12. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

STRINGER CORRODED AT BS 910, STR 27L. REPAIRED STRINGER IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

FRAME CORRODED AT BS 727D, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

STUB FRAME CRACKED AT STA 294.5, BETWEEN STR 7R & STR 8R. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

FLOOR STRUCTURE BEAM CORRODED AT BS 967, BETWEEN RBL 27 TO RBL 42. REPAIRED BEAM PER EA & DWG.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

SUPPORT BRACKET CRACKED AT BS 947.5, BETWEEN STR 24R TO STR 25R. REMOVED AND REPLACED BRACKET IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

FRAME CORRODED AT BS 727E, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

CRACK ON ANGLE BETWEEN STA 277 TO STA 291.5, STR 11R TO STR 12R PAX CABIN. REMOVED AND REPLACED ANGLE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

FLOOR STRUCTURE BEAM CORRODED AT BS 967, LBL 5. REPAIRED BEAM PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

FRAME CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

SUPPORT WEB CRACKED AT BS 727, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

FLOORBEAM CORRODED AT BS 986.5, LBL 35 AND LBL 43. REPAIRED BEAM PER EA AND EO.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

CRACK ON ANGLE BETWEEN STA 277 TO STA 291.5, STR 9R TO STR 10R PAX CABIN. REMOVED AND REPLACED ANGLE PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

CRACK ON ANGLE BETWEEN STA 277 TO STA 291.5, STR 13R TO STR 14R PAX CABIN. REMOVED AND REPLACED ANGLE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

SKIN CRACKED AT BS 332, STR 17R. REPAIRED SKIN IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

FRAME CORRODED AT BS 727E, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 20 TO RBL 43. REPAIRED BEAM PER EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

WEB CORRODED BETWEEN BS 951 TO BS 986.5, RBL 50. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

STIFFENER CRACKED AT BS 727, STR 27R. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

FLOORBEAM CRACKED AT BS 947.5, LBL 53. REPAIRED BEAM IAW EA AND EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

FRAME CORRODED AT BS 727D, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 664.0 AND BS 670, RBL 24.5. REPAIRED CHORD PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 707 TO BS 712, RBL 24.5. REPAIRED WEB IAW EO AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 665 TO BS 674, LBL 24.5. REPAIRED CHORD IAW EA AND EO.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 50,042 hrs · 40,178 cycles

AFT CARGO DOOR SKIN CRACKED BETWEEN BS 827 TO BS 846, STR 24R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

SKIN CRACKED AT BS 520+2, STR 28R. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,042 hrs · 40,178 cycles

FRAME CRACKED AT BS 500B, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME IAW EA.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 49,935 hrs · 40,097 cycles

RIGHT KEEL BEAM ANGLE CRACKED BETWEEN BS 520 TO BS 540. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: RETAINING CLIP — LOOSE (L1 DOOR) · airframe 49,815 hrs · 39,997 cycles

L1 DOOR EMERGENCY EVAC SLIDE AFT RETAINER CLIP LOOSE. REMOVED AND REPLACED CLIP ASSY PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 49,726 hrs · 39,926 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: ATTACH FITTING — BROKEN (RT NR 5 SPOILER) · airframe 49,671 hrs · 39,886 cycles

RIGHT WING NR 5 GROUND SPOILER ATTACH FITTING BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 49,428 hrs · 39,702 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,133 hrs · 39,480 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 639, LBL 45.5. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 48,857 hrs · 39,273 cycles

CRACK LT HORIZONTAL STAB LEADING EDGE APPROX 78 INCHES FROM OUTBOARD EDGE. REMOVED AND REPLACED LEADING EDGE PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,588 hrs · 39,085 cycles

DURING SCHEDULED MV2 CHECK FOUND, L1 DOOR EMERGENCY EXIT FLOOR LIGHT INOP. RELAMPED PER MM.

Part: LENS — BROKEN (CABIN) · airframe 48,003 hrs · 38,645 cycles

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

Part: SLAT — DELAMINATED (LT WING) · airframe 46,974 hrs · 37,854 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 2 SLAT DELAMINATED AT I/B AND O/B END. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: LENS — BROKEN (CABIN) · airframe 46,610 hrs · 37,588 cycles

DURING SCHEDULED MV2 CHECK FOUND, LT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: COOLING FAN — FAULTY (E&E BAY) · airframe 46,549 hrs · 37,535 cycles

AIR TURNBACK, FLIGHT ATTENDANTS REPORTED SMELL OF SMOKE AROUND ROW 7. REMOVED AND REPLACED E&E EQUIPMENT COOLING FAN PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,550 hrs · 36,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,550 hrs · 36,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,550 hrs · 36,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,550 hrs · 36,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,550 hrs · 36,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 45,550 hrs · 36,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME SHEAR WEB CRACKED AT BS 440, RBL 21. REPAIRED FRAME SHEAR WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,550 hrs · 36,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 3L. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,550 hrs · 36,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,550 hrs · 36,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 3L. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,550 hrs · 36,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,550 hrs · 36,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,550 hrs · 36,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,550 hrs · 36,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8R. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 45,550 hrs · 36,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17.0. REPAIRED WEB PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,550 hrs · 36,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND CARGO FLOOR SUPPORT CORRODED AT BS 773, LBL 2.5. REPAIRED SUPPORT PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,550 hrs · 36,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND CARGO FLOOR SUPPORT CORRODED AT BS 773, LBL 7. REPAIRED SUPPORT PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,550 hrs · 36,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 27L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,550 hrs · 36,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 668 TO BS 672, LBL 24.5. REPAIRED BEAM PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,146 hrs · 34,922 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 513D, STR 10L. REPAIRED SKIN PER EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,643 hrs · 33,838 cycles

DURING SCHEDULED SPV CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT AFT OF WING INOP. CHARGED BATTERIES PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,643 hrs · 33,838 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. CHARGED BATTERIES PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,643 hrs · 33,838 cycles

DURING SCHEDULED SPV CHECK, RIGHT AFT CABIN OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP. CHARGED BATTERIES PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,643 hrs · 33,838 cycles

DURING SCHEDULED SPV CHECK, R2 DOOR INTERIOR EMERGENCY EXIT LIGHT INOP. CHARGED BATTERIES PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 41,643 hrs · 33,838 cycles

DURING SCHEDULED SPV, FOUND NR 1 L/E SLAT LOWER SKIN CRACKED. REPAIRED SLAT PER SRM.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 41,643 hrs · 33,838 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EVACUATION SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 41,249 hrs · 33,547 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. REINSTALLED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 40,791 hrs · 33,211 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EXTERNAL EGRESS LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,600 hrs · 33,079 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY LIGHT PER MM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 40,468 hrs · 32,982 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LOWER FLAP LOOSE. SECURED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,268 hrs · 32,835 cycles

DURING SCHEDULED 12Y CHECK, FOUND SKIN CRACKED BETWEEN BS 385 TO BS 386, LBL 5.5. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,268 hrs · 32,835 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD BILGE AREA BETWEEN LBL 10 TO RBL 7.5, BS 362.5 TO BS 378.5. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,268 hrs · 32,835 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT BETWEEN BS 302 TO BS 304, BETWEEN WL 233 TO WL 238. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,268 hrs · 32,835 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT LOWER STUB FRAME CRACKED AT BS 951 L2 DOOR LOWER FWD CUTOUT. REPAIRED STUB FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,268 hrs · 32,835 cycles

DURING SCHEDULED 12Y CHECK, FOUND SKIN CRACKED BETWEEN BS 951 TO BS 960, BETWEEN STR 7L TO STR 20L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,268 hrs · 32,835 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 304, WL 258. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 40,268 hrs · 32,835 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 500, STR 27R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,268 hrs · 32,835 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN RBL 7 TO RBL 12. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,268 hrs · 32,835 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, LBL 4. REPAIRED SHEAR TIE PER SRM.

Part: FITTING — CORRODED (MLG) · airframe 40,268 hrs · 32,835 cycles

DURING SCHEDULED 12Y CHECK, FOUND MLG WALKING BEAM FWD I/B STAB FITTING CORRODED. REMOVED AND REPLACED FITTING PER ACO.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 40,268 hrs · 32,835 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT KEEL BEAM CORRODED BETWEEN BS 746 TO BS 750. REPAIRED KEEL BEAM PER SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 40,268 hrs · 32,835 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CRACKED AT BS 496, STR 22R. REPAIRED STRINGER PER SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 40,244 hrs · 32,809 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED CHARGER ASSY PER MM.

Part: BUSHING — WORN (LT ELEVATOR TAB) · airframe 37,411 hrs · 30,812 cycles

DURING SCHEDULED HC2 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 2 TAB BUSHING AND BOLT PER SWA EA.

Part: HOOK — LOOSE (GIRT BAR) · airframe 37,402 hrs · 30,806 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 37,402 hrs · 30,806 cycles

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

Part: LENS — CRACKED (CABIN) · airframe 36,489 hrs · 30,080 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 36,479 hrs · 30,074 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 35,711 hrs · 29,479 cycles

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

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 35,680 hrs · 29,459 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR LOWER HINGE BOX CRACKED. REMOVED AND REPLACED HINGE BOX PER SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 35,680 hrs · 29,459 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR UPPER HINGE BOX CRACKED. REMOVED AND REPLACED HINGE BOX PER SRM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 35,680 hrs · 29,459 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTLUMINESCENT STRIP LOOSE BETWEEN ROW 7 ABC AND ROW 9 ABC. SECURED STRIP PER MM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT VERTICAL STAB FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT VERTICAL STAB FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: BEARING — WORN (RT ELEVATOR) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, RIGHT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED INBOARD HORN BEARING PER MM.

Part: BEARING — WORN (LT ELEVATOR) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, LEFT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED INBOARD HORN BEARING PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE CREASE BEAM CORRODED AT BS 996 LEFT SIDE. REPAIRED CREASE BEAM SECTION PER SRM.

Part: FRAME — CRACKED (BS 360 S8R) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: CREASE BEAM — CORRODED (BS 996) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE RIGHT CREASE BEAM CORRODED AT BS 996. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM.

Part: FRAME — CRACKED (BS 827 S8R) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 380 S2L) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 2L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FRAME — CRACKED (BS 907 S8R) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: TORQUE TUBE — CORRODED (T/E FLAP) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD MID FLAP TORQUE TUBE OUTBOARD END CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 14R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM CORRODED AT BS 344, STR 17R. REMOVED AND REPLACED CREASE BEAM PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 440, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT AND RT HORIZONTAL STAB FITTING CLEVIS LUG FACES CORRODED. REPAIRED STAB FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,971 hrs · 28,117 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (NR 1 SLAT) · airframe 33,811 hrs · 28,000 cycles

DURING SCHEDULED C1 CHECK, FOUND LEFT WING NR 1 L/E SLAT CRACKED AT LOWER AFT CORNER. REPAIRED SLAT PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,811 hrs · 28,000 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — LOOSE (L1 DOOR) · airframe 32,788 hrs · 27,179 cycles

DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT LIGHT LOOSE AT L1 DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 32,482 hrs · 26,921 cycles

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

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 31,913 hrs · 26,487 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,620 hrs · 24,721 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD SIDE CHORDS CRACKED AT WL 207. REMOVED AND REPLACED SIDE CHORDS PER SWA ACO.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 29,439 hrs · 24,578 cycles

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

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 28,916 hrs · 24,179 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT LOWER INBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CHAFED (FUSELAGE) · airframe 26,674 hrs · 22,357 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 870, STRINGER 1R, CHAFING. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 26,236 hrs · 22,006 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 26,236 hrs · 22,006 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 25,627 hrs · 21,498 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L1 COCKPIT WINDOW POST CRACKED AT UPPER OUTBOARD CORNER. REPAIRED WINDOW POST PER SRM.

Part: WEB — CRACKED (MLG W/W) · airframe 25,627 hrs · 21,498 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 671, LBL 42. REPAIRED WEB PER SWA EA.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 25,627 hrs · 21,499 cycles

DURING SCHEDULED RON, FOUND RT WING NR 6 L/E SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,627 hrs · 21,499 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 727E, RBL 3 TO LBL 12, CORRODED. REPAIRED FLOORBEAM SECTION PER EA.

Part: SLIDE — DISCHARGED (L2 DOOR) · airframe 25,121 hrs · 21,081 cycles

L2 DOOR EVAC SLIDE LOW PRESSURE IND. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 24,246 hrs · 20,375 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 24,175 hrs · 20,314 cycles

FWD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED FWD EMERGENCY EXIT LIGHT ASSEMBLY PER MM.

Part: ARM — BROKEN (KRUEGER FLAP) · airframe 23,680 hrs · 19,933 cycles

NR 4 KRUEGER FLAP ACTUATOR ARM BROKEN. REMOVED AND REPLACED KRUEGER FLAP ACTUATOR ARM PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 23,322 hrs · 19,657 cycles

DURING RON, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE PER MM.

Part: INDICATOR — OUT OF POSITION (SLIDE BOTTLE) · airframe 21,743 hrs · 18,425 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 21,607 hrs · 18,313 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: FITTING — CRACKED (SPOILER) · airframe 21,288 hrs · 18,063 cycles

DURING SCHEDULED PM CHECK, FOUND RT WING INBOARD GROUND SPOILER ACTUATOR OUTBOARD ATTACH FITTING BROKEN. REMOVED AND REPLACED SPOILER ASSY PER MM.

Part: COVER — LOOSE (L2 DOOR) · airframe 20,693 hrs · 17,579 cycles

AFT ENTRY DOOR EVACUATION SLIDE COVER LOOSE. SECURED SLIDE COVER PER MM.

Part: COVER — LOOSE (L2 DOOR) · airframe 20,666 hrs · 17,559 cycles

AFT ENTRY DOOR EVACUATION SLIDE COVER LOOSE. SECURED EVACUATION SLIDE COVER PER MM.

Part: LENS — BROKEN (FWD ENTRY DOOR) · airframe 20,417 hrs · 17,386 cycles

FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED EXIT LIGHT COVER PER MM.

Part: RETAINER — LOOSE (AFT SVC DOOR) · airframe 19,742 hrs · 16,842 cycles

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

Part: PIN — CORRODED (MLG TRUNNION) · airframe 19,640 hrs · 16,763 cycles

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

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 18,555 hrs · 15,876 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 14,429 hrs · 12,379 cycles

EEPLS FLOOR TRACK COVER LOOSE AT FWD CABIN. R&R TRACK COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 14,057 hrs · 12,066 cycles

EEPLS LOOSE AT EXIT ROW. SECURED EEPLS TRACK COVER PER MM.

Part: SLIDE — DETACHED (AFT SERVICE DOOR) · airframe 13,361 hrs · 11,515 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE ASSY FELL OUT OF CONTAINER. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 13,120 hrs · 11,335 cycles

EEPLS WIRES EXPOSED AT ROW 12. SECURED WIRING PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 12,685 hrs · 10,977 cycles

EMERGENCY EXIT LIGHTS HAVE WIRES EXPOSED. REPAIRED EXIT LIGHTING PER MM.

Part: COVER — MISSING (CABIN) · airframe 12,414 hrs · 10,773 cycles

EEPLS TRACK COVER MISSING AT OVERWING EXIT ROW. REPLACED TRACK COVER PER MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR)

L-2 DOOR EVACUATION SLIDE BOTTLE PRESSURE LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: TIRE — FAILED (MLG)

NR 1 MAIN TIRE TREAD SEPARATED FROM WHEEL ON TAKEOFF. INSPECTED AND FOUND CENTER AND INNER GEAR DOORS DAMAGED ON LEFT MAIN GEAR. REPLACED GEAR DOORS, AND NR 1 WHEEL ASSEMBLY PER BOEING M/M.

Part: CIRCUIT BREAKER — FAILED (NR 1)

RETURNED TO ABQ DUE TO NR 1 TRANSFORMER RECTIFIER C/B TRIPPING. INSPECTED AND FOUND C/B C819 AND WIRES MELTED ON TERMINAL B1. REPAIRED WIRING AND REPLACED BREAKER PER M/M.