N505SW

Part: FASTENER — CORRODED (CABIN) · airframe 69,949 hrs · 65,988 cycles

R1 DOOR FORWARD GIRT BAR FLOOR MOUNT HAS RUSTY MOUNTING HARDWARE. REPLACED R1 DOOR FORWARD GIRT BAR HARDWARE IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,949 hrs · 65,988 cycles

FUSELAGE SKIN CRACKED ABOVE STRINGER 4R, STA 287-291. REPAIR IAW SRM.

Part: COVER — LOOSE (CABIN) · airframe 69,947 hrs · 65,987 cycles

RIGHT EMERGENCY EXIT LIGHT COVER IS LOOSE. SECURED LIGHT COVER PER AMM.

Part: SUPPORT ANGLE — CRACKED (TE FLAP) · airframe 69,947 hrs · 65,987 cycles

RIGHT WING INBOARD MID FLAP FIXED WING PANEL HAS A CRACK AFT RIGHT CORNER. MARKED IN RED. REMOVE AND REPLACE SUPPORT ANGLE PER SRM 51-40-02.

Part: MOTOR — FAULTY (VBV) · airframe 68,436 hrs · 64,803 cycles

ON CLIMBOUT UNABLE TO MAINTAIN CLIMB N1 WITHOUT EXCEEDING MAX CONT EGT TO MAINTAIN CLIMB N1 REQUIRES 920+ ON NR 1 ENG EGT. REMOVED AND REPLACED VBV MOTOR & VBV STOP INSTALLED NEW FLEX SHAFT PER MM.

Part: MOUNT — CRACKED (R2 DOOR) · airframe 68,361 hrs · 64,755 cycles

R2 DOOR EMERGENCY EVAC SLIDE FORWARD SLIDE MOUNT CRACKED. REMOVED AND REPLACED MOUNT PER AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 67,877 hrs · 64,603 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: TOGGLE — LOOSE (TE FLAP) · airframe 67,789 hrs · 64,370 cycles

AIRCRAFT SHUTTER AND YOKE VIBRATION 210 KTS FLAPS MOVING FROM 2 TO POSITION 5, 2, TO 4 SECONDS. REMOVED AND REPLACED FLAP TOGGLES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,762 hrs · 64,351 cycles

RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 16 TO ROW 17. REPAIRED LIGHT PER MM.

Part: RETAINER — BROKEN (GIRT BAR) · airframe 67,639 hrs · 64,276 cycles

L1 DOOR EMERGENCY EVAC SLIDE AFT FLOOR GIRT BAR RETAINER SPRING BROKEN. REMOVED AND REPLACED RETAINER ASSY PER M/M.

Part: COVER — LOOSE (CABIN) · airframe 66,352 hrs · 63,448 cycles

RT EEPLS COVER LOOSE AT ROW 8. REMOVED AND REPLACED COVER PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 296.5, STR 7R. REPAIRED FRAME IAW EA ER.

Part: LIGHT — DISCHARGED (CABIN) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, LT EMERGENCY EXIT LIGHTS INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT, BS 329, STR 8R. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CACKED AT BS 727A+6, STR 21L. REPAIRED SKIN IAW ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 947.5, STR 19L. REPAIRED FRAME IAW ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 639, STR 16L. REPAIRED FRAME IAW ER AND EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, RT EMERGENCY EXIT LIGHTS INOP. RELAMPED PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD LOWER CHORD HORIZONTAL FLANGE CRACKED AT BS 540, BETWEEN STR 21L TO STR 22L. REPAIRED FLANGE PER ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD LOWER CHORD HORIZONTAL FLANGE CRACKED AT BS 540, STR 25L. REPAIRED FLANGE PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD CARGO DOOR SKIN CUTOUT CRACKED. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR FUSELAGE SKIN CRACKED AT BS 327, WL 210. REPAIRED SKIN IAW EA AND ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 661, BBL 0. REPAIRED BEAM IAW ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 482, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME IAW ATS ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME WEB CRACKED AT BS 332.1, STR 8R. REMOVED AND REPLACED FRAME IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND SUPPORT WEB CRACKED AT BS 344, STR 11R. REPAIRED WEB IAW ER AND EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT BS 772, LBL 17. REPAIRED SUPPORT PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 482A, BETWEEN STR 28R TO STR 28L. REMOVED AND REPLACED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 482A, BETWEEN STR 27R TO STR 26R. REMOVED AND REPLACED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 659 TO BS 669, LBL 24.5. REPAIRED CHORD PER EA AND ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK FOUND, SHEAR TIE CORRODED AT BS 482A, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED FRAME PER SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, STR 16L. REPAIRED BEAM IAW ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT S 747, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME OUTER CHORD CRACKED AT BS 639, STR 16L. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

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

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND CHANNEL CRACKED AT BS 360, STR 4R. REPAIRED CHANNEL IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 967, BETWEEN STR 6L TO STR 7L. REMOVED AND REPLACED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME WEB CRACKED AT BS 947, STR 19R. REPAIRED FRAME IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 727C, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 375, STR 17R. REPAIRED SKIN IAW ER.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 772, LBL 8. REPAIRED SUPPORT IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 45. REPAIRED CHORD PER ER AND ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME WEB CRACKED AT BS 986.5, STR 20R. REMOVED AND REPLACED WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 273, STR 16L. REPAIRED SKIN IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 859, RBL 3. REPAIRED SUPPORT IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT BS 772, LBL 12. REPAIRED SUPPORT IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND PRESSURE DECK WEB CRACKED BETWEEN BS 665 TO BS 675, BETWEEN RBL 35 TO RBL 45. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 400, STR 15R. REMOVED AND REPLACED STRINGER SECTION IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 16R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 19L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,121 hrs · 63,305 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 66,121 hrs · 63,305 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE. REMOVED AND REPLACED LENS IAW MM.

Part: LENS — MISSING (CABIN) · airframe 65,812 hrs · 63,097 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 7. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,811 hrs · 63,097 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 927+6, STR 25L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,811 hrs · 63,097 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 747+4, STR 19L. REPAIRED SKIN PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,811 hrs · 63,097 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CORRODED BETWEEN BS 986 TO BS 1016, STR 25L. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,811 hrs · 63,097 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CLIP CRACKED AT BS 967, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 65,810 hrs · 63,096 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,810 hrs · 63,096 cycles

DURING SCHEDULED OTS CHECK FOUND, RT EEPLS INOP AT ROW 20. RELAMPED PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 65,810 hrs · 63,096 cycles

DURING SCHEDULED OTS CHECK FOUND, LT AFT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. CHARGED BATTERY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,810 hrs · 63,096 cycles

DURING SCHEDULED OTS CHECK FOUND, RT EEPLS INOP BETWEEN ROW 16 TO ROW 17. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,810 hrs · 63,096 cycles

DURING SCHEDULED OTS CHECK FOUND, LT EEPLS INOP BETWEEN ROW 14 TO ROW 15. RELAMPED PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,810 hrs · 63,096 cycles

DURING SCHEDULED OTS CHECK FOUND, STRINGER CORRODED AT BS 947.5, STR 25L. REPAIRED STRINGER PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,811 hrs · 63,096 cycles

DURING SCHEDULED SPV CHECK FOUND, STRINGER CLIP CRACKED AT BS 727B, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,811 hrs · 63,096 cycles

DURING SCHEDULED SPV CHECK FOUND, STRINGER CLIP CRACKED AT BS 727C, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,810 hrs · 63,096 cycles

DURING SCHEDULED OTS CHECK FOUND, LT CREASE BEAM WEB CORRODED AT BS 767+10. REMOVED AND REPLACED WEB PER SRM.

Part: WIRE — BROKEN (CABIN) · airframe 65,810 hrs · 63,096 cycles

DURING SCHEDULED OTS CHECK FOUND, LT EEPLS WIRE BROKEN. REMOVED AND REPLACED WIRE PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,810 hrs · 63,096 cycles

DURING SCHEDULED OTS CHECK FOUND, LT CREASE BEAM WEB CORRODED AT BS 747+4, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 665,811 hrs · 63,096 cycles

DURING SCHEDULED OTS CHECK FOUND, STRINGER CLIP CRACKED AT BS 727C, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 685,811 hrs · 63,096 cycles

DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CORRODED AT BS 987, BETWEEN STR 24L TO STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,809 hrs · 63,095 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 380+16, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,809 hrs · 63,095 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 747+16, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,809 hrs · 63,095 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 747+7, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,809 hrs · 63,095 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 927+6, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,809 hrs · 63,095 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 967+5, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,809 hrs · 63,095 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 747+13, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,809 hrs · 63,095 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 747+4, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,809 hrs · 63,095 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 747 + 13, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,809 hrs · 63,095 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 747 + 7, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,809 hrs · 63,095 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 747 + 16, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,809 hrs · 63,095 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 390, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,809 hrs · 63,095 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 927 + 6, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,809 hrs · 63,095 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 747 + 4, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,809 hrs · 63,095 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 967 + 5, STR 25L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,589 hrs · 62,944 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 482, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,589 hrs · 62,944 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 482A, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,589 hrs · 62,944 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 482, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,589 hrs · 62,944 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 482A, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,589 hrs · 62,944 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 482A, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: BRACKET — LOOSE (R1 DOOR) · airframe 65,589 hrs · 62,944 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD ATTACHMENT BRACKET LOOSE. REMOVED AND REPLACED BRACKET PER SOPM.

Part: LENS — BROKEN (CABIN) · airframe 65,589 hrs · 62,944 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,485 hrs · 62,864 cycles

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

Part: LENS — MISSING (CABIN) · airframe 64,722 hrs · 62,328 cycles

RT EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 13. INSTALLED LENS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,552 hrs · 62,198 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,552 hrs · 62,198 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 12. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 64,387 hrs · 62,085 cycles

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

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 63,986 hrs · 61,806 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,919 hrs · 61,757 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 265, STR 9L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,919 hrs · 61,757 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 432, STR 17R. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,151 hrs · 61,214 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CRACKED AT BS 420, STR 1. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,151 hrs · 61,214 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 923, STR 24R. REPAIRED SKIN PER SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 63,151 hrs · 61,214 cycles

DURING SCHEDULED OTS CHECK, FOUND CRACK ON DOUBLER STRAP ON AFT CARGO DOOR OPENING AT LOWER EDGE. REMOVED AND REPLACED DOUBLER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,151 hrs · 61,214 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 893, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,151 hrs · 61,214 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 488B, STR 16R. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,151 hrs · 61,214 cycles

DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CRACKED AT BS 887, BETWEEN STR 24R TO STR 25R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,151 hrs · 61,214 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 424, STR 0. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,151 hrs · 61,214 cycles

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

Part: BATTERY PACK — WEAK (CABIN) · airframe 62,950 hrs · 61,077 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT BATTERY VOLTAGE WEAK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,750 hrs · 60,928 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 831, STR 17L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,610 hrs · 60,839 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,610 hrs · 60,839 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 404 TO BS 408, STR 16R. REPAIRED SKIN PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,610 hrs · 60,839 cycles

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

Part: WIRE — ARCED (WINDOW HEAT) · airframe 62,047 hrs · 60,472 cycles

R1 COCKPIT WINDOW HEAT WIRES ARCED DURING FLIGHT. REMOVED AND REPLACED WINDOW PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,844 hrs · 60,359 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT AFT EXTERNAL EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,522 hrs · 60,164 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: FITTING — CORRODED (GIRT BAR) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR BOTH FITTING SPACER PLATES CORRODED. REMOVED AND REPLACED FITTING ASSY PER MM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR BOTH FITTING SPACER PLATES CORRODED. REMOVED AND REPLACED FITTING ASSY PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT KEEL BEAM LOWER T-CHORD CORRODED AT BS 485B, STR 28R. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR AFT LOWER CORNER INNER CUTOUT SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. REPAIRED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR AFT LOWER CORNER EDGE FRAME CRACKED. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: PANEL — LOOSE (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND LOWER KEEL BEAM PANEL LOOSE BETWEEN BS 663 TO BS 727. REMOVED AND REPLACED PANEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT KEEL BEAM CRACKED AT BS 711, LBL 5. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 61,423 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER MT.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 794, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND NR 2 L/E SLAT LOWER SKIN CRACKED. REPAIRED SLAT SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 1L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CRACKED AT BS 440, STR 4L. REMOVED AND REPLACED STRINGER PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 1 SLAT I/B WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 2 SLAT O/B WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 1 SLAT LOWER SURFACE CRACKED. REMOVED AND REPLACED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,424 hrs · 60,095 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: GASPER FAN — FAULTY (CABIN) · airframe 61,222 hrs · 59,959 cycles

ELECTRICAL / PLASTIC BURNING SMELL / FUMES IN CABIN AFTER 3 HRS IN FLT. TURNED OFF GASPER FAN, RECIRC FAN & GALLEY PWR. ODOR SUBSIDED WITHIN 30 SECS. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,832 hrs · 59,722 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 482B +20, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,858 hrs · 59,078 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 783, STR 25L. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 59,858 hrs · 59,078 cycles

DURING SCHEDULED MV1 CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7, WL 182. REPAIRED WEB PER SWA EA.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 58,451 hrs · 57,851 cycles

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

Part: SKIN — CRACKED (BS 847 S24L) · airframe 57,304 hrs · 56,970 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,081 hrs · 56,790 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 763, BETWEEN STR 19L AND STR 22L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 56,693 hrs · 56,474 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHTS) · airframe 55,958 hrs · 55,843 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,808 hrs · 55,701 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 952, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 65,808 hrs · 55,701 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 65,808 hrs · 55,701 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,808 hrs · 55,701 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 807-827 S17L) · airframe 54,817 hrs · 54,738 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 807 AND BS 827, STR 18L AND STR 17L. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 54,282 hrs · 54,205 cycles

DURING SCHEDULED BRDG CHECK, FOUND LEFT WING NR 2 LEADING EDGE SLAT TRAILING EDGE DELAMINATED. REPAIRED SLAT PER SRM.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 54,282 hrs · 54,205 cycles

DURING SCHEDULED BRDG CHECK, FOUND FWD CARGO DOOR AFT FRAME LOWER STOP FITTING LOWER CHORD CRACKED. REMOVED AND REPLACED CHORD PER SRM.

Part: COVER — CRACKED (EMERGENCY LIGHTS) · airframe 54,282 hrs · 54,205 cycles

DURING SCHEDULED BRDG CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT COVER CRACKED. REMOVED AND REPLACED LIGHT COVER PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

DURING SCHEDULED BRDG CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 657 AND BS 669, LBL 24.5. REPAIRED FLOORBEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

DURING SCHEDULED BRDG CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 662, RBL 24.5. REPAIRED FLOORBEAM PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 54,282 hrs · 54,205 cycles

DURING SCHEDULED BRDG CHECK, FOUND LEFT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

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

Part: SLAT — DELAMINATED (RT WING) · airframe 54,282 hrs · 54,205 cycles

DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING NR 5 L/E SLAT UPPER INBOARD T/E DELAMINATED. REPAIRED SLAT PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 54,282 hrs · 54,205 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 8L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 8L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 9L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 639, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 616, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 783, STR 20L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,282 hrs · 54,205 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 788 S24L) · airframe 54,282 hrs · 54,205 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 788, STR 24L. REPAIRED SKIN PER SRM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 54,246 hrs · 54,168 cycles

AT 18,000 FT FLIGHT DECK R2 WINDOW SHATTERED WITH ELECTRICAL ARCHING, NO PRESSURIZATION PROBLEMS NOTED. REMOVED AND REPLACED R2 WINDOW, WINDOW HEAT WIRING HARNESS AND HEAT CONTROLLER PER MM.

Part: ATTACH FITTING — BROKEN (NR 4 SPOILER) · airframe 54,092 hrs · 54,025 cycles

DURING SCHEDULED A2 CHECK, FOUND LEFT WING NR 4 SPOILER INBOARD LUG BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 53,930 hrs · 53,855 cycles

DURING SCHEDULED C1 CHECK, FOUND LEFT WING INBOARD MIDFLAP DELAMINATED AT INBOARD EDGE. REMOVED AND REPLACED LEFT WING INBOARD MIDFLAP PER MM.

Part: SIGN — DISLODGED (EMERGENCY LIGHTS) · airframe 53,450 hrs · 53,371 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN FELL OFF. INSTALLED EXIT SIGN PER MM.

Part: SKIN — CRACKED (BS 757 S17L) · airframe 52,300 hrs · 52,155 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 17L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 877 S23R) · airframe 52,300 hrs · 52,155 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 877, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 445) · airframe 51,761 hrs · 51,570 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 445, STR 16R. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 51,740 hrs · 51,544 cycles

FOUND LT FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,491 hrs · 51,271 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,491 hrs · 51,271 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 816, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 943) · airframe 50,846 hrs · 50,590 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 872) · airframe 50,846 hrs · 50,590 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 872, STR 24R. REPAIRED SKIN PER SRM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 50,635 hrs · 50,358 cycles

DURING SCHEDULED C1 CHECK, FOUND LT EXTERIOR UPPER EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: FRAME — CRACKED (BS 455) · airframe 49,884 hrs · 49,603 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 455, STR 24R. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (BS 400) · airframe 49,884 hrs · 49,603 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 24R. REPAIRED FRAME PER BFG ER.

Part: STRINGER CLIP — CRACKED (BS 348) · airframe 49,884 hrs · 49,603 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 348, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 351) · airframe 49,884 hrs · 49,603 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 351, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,884 hrs · 49,603 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (BS 188-196) · airframe 49,884 hrs · 49,603 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FLOOR WEB CRACKED BETWEEN BS 188 TO BS 196, LT & RT SIDE, WL 208. REPAIRED FLOOR WEB PER SRM.

Part: FRAME — CRACKED (BS 188) · airframe 49,884 hrs · 49,603 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STUB FRAMES CRACKED AT BS 188, LT & RT SIDE, WL 208. REPAIRED STUB FRAMES PER SRM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 49,155 hrs · 48,865 cycles

IN ALL PHASE OF FLIGHT - VIBRATION FELT & TAIL OSCILLATION. REMOVED AND REPLACED LT ELEVATOR TAB INBOARD HINGE HARDWARE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,846 hrs · 48,526 cycles

DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 48,630 hrs · 48,309 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, WL 180, LBL 5.7. REPAIRED WEB PER SRM.

Part: TRU — FAULTY (COOLING FAN) · airframe 48,610 hrs · 48,287 cycles

DIVERSION/DECLARED EMERGENCY. LOST CABIN PRESSURE, NR 1 TRANSFORMER RECTIFIER & EQUIPMENT COOLING FAN INOP. REMOVED AND REPLACED NR 1 TRANSFORMER RECTIFIER & NR 1 ENGINE GENERATOR PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 48,380 hrs · 48,070 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-INSTALLED SLIDE PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 48,380 hrs · 48,070 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED LIGHT COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,041 hrs · 47,762 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR UPPER AFT CORNER, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,041 hrs · 47,762 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT AFT SERVICE DOOR UPPER HINGE, CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,041 hrs · 47,762 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR FWD FRAME AT THIRD STOP CRACKED. REPAIRED FRAME PER EA.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 47,393 hrs · 47,177 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BEADED PRESSURE WEB AT BS 663.75, LBL 39.5, CRACKED. REPAIRED PRESSURE WEB PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,393 hrs · 47,177 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 932, STRINGER 23L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,393 hrs · 47,177 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 482 + 16, STRINGER 10L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,393 hrs · 47,177 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 790, STRINGER 17L, CRACKED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,393 hrs · 47,177 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STINGER CLIP AT BS 706, STRINGER 10R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 47,393 hrs · 47,177 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,393 hrs · 47,177 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH CRACKS AT BS 1016 PRESSURE BULKHEAD DOME WEB CENTER SECTION AT 7 O'CLOCK AND 12 O'CLOCK POSITION. REPAIRED WEB SECTIONS PER EA.

Part: RIB — CRACKED (RT WING) · airframe 47,393 hrs · 47,177 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT WING LOWER RIB CHORD AT WBL 135.5, CRACKED. REPAIRED RT WING RIB CHORD PER EA.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,913 hrs · 46,674 cycles

DURING SCHEDULED PM CHECK, FOUND AFT ENTRY AND AFT SERVICE EMERGENCY EXIT OVERHEAD LIGHTS INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,652 hrs · 46,412 cycles

DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROWS 6 ABC, 8 ABC, INOP. RELAMPED EMERGENCY EXIT LIGHTS PER MM.

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 46,202 hrs · 45,925 cycles

R2 DOOR EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,355 hrs · 45,058 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STRINGER 21L AND BS 938, STRINGER 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,839 hrs · 44,571 cycles

DURING SCHEDULED SC, FOUND SKIN CRACKED AT BS 515 TO BS 517 AT STRINGER 12L. REPAIRED SKIN CRACK PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 44,374 hrs · 44,137 cycles

EEPLS LOOSE AT MID CABIN. SECURED EEPLS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 44,374 hrs · 44,137 cycles

LT OVERWING EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,104 hrs · 43,897 cycles

EEPLS INOP BETWEEN ROWS NR 10 AND 11. REPAIRED EEPLS PER MM.

Part: COVER — MISSING (CABIN) · airframe 43,497 hrs · 43,319 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER MISSING AT ROW NR 12. INSTALLED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 43,497 hrs · 43,319 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: PUMP — FAULTY (NR 1 ENGINE HYD) · airframe 43,428 hrs · 43,251 cycles

AIR TURNBACK, ON GEAR RETRACT 'A' SYSTEM HYD PUMP LIGHTS AND MASTER CAUTION LIGHTS ILLUMINATED, 'A' SYSTEM HYD PRESS DROPPED TO 1000 PSI. REMOVED AND REPLACED ENGINE DRIVEN HYD PUMP 'A' AND CASE DRAIN FILTER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 43,172 hrs · 43,007 cycles

DURING SCHEDULED PM CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 3. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,863 hrs · 42,317 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS SECTION INOP IN AFT CABIN. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 42,842 hrs · 42,691 cycles

EEPLS SECTION LOOSE NEAR GALLEY. SECURED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,833 hrs · 42,685 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 24L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 42,675 hrs · 42,541 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS SECTION INOP IN AFT CABIN. RELAMPED EEPLS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 41,732 hrs · 41,674 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 1. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,661 hrs · 41,603 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACK 4 INCHES LONG AT BS 750, STR 18L. REPAIRED SKIN PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 40,779 hrs · 40,774 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 1. REMOVED AND REPLACED EEPLS COVER PER MM

Part: LIGHT — LOOSE (CABIN) · airframe 40,237 hrs · 40,268 cycles

OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW NR 19 ABC. SECURED LIGHT ASSY PER MM.

Part: DOOR — CRACKED (FWD SVC DOOR) · airframe 39,804 hrs · 39,847 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR FRAME CRACKED AT AFT LOWER DOOR STOP. REMOVED AND REPLACED FWD SVC DOOR PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 39,804 hrs · 39,847 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EEPLS INOP IN FWD CABIN. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,537 hrs · 39,593 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 23L. REPAIRED SKIN PER SRM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 39,429 hrs · 39,486 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,946 hrs · 39,036 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515, 1 INCH ABOVE STR 10L. REPAIRED SKIN PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,906 hrs · 38,996 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 20L. REPAIRED SKIN PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 38,906 hrs · 38,996 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 7. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 38,906 hrs · 38,996 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS 4, 11, 14, 15, 17, 18 AND 19. REMOVED AND REPLACED COVERS PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 38,051 hrs · 38,224 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT OUT OF ADJUST. REPOSITIONED SLIDE PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 37,417 hrs · 37,619 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND WEBS CRACKED (2 EA) AT BS 178, WL 207 & LBL 26.5, WL 234 & LBL 9.0. REMOVED AND REPLACED WEBS PER SRM & SWA ACO 7338-53.

Part: BEAM — CRACKED (FUSELAGE) · airframe 37,410 hrs · 37,610 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAMS CRACKED ( 2 EA ) AT BS 183, WL 183 & RBL 5.7, WL 223 & RBL 17.1. R&R VERTICAL BEAMS PER SWA RA 1-353-2655.

Part: WEB — CRACKED (FUSELAGE) · airframe 37,410 hrs · 37,610 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL WEBS CRACKED ( 2 EA ) AT BS 180, WL 207 & RBL 26, BS 178, WL 219 & LBL 12. REPAIRED WEBS PER SRM.

Part: STRUCTURE — CRACKED (LT WING) · airframe 37,115 hrs · 37,320 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT WING L/E CRACKED NEAR NR 1 KRUEGER FLAP, CRACK IS .4375. REPAIRED L/E PER SWA RA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,388 hrs · 36,610 cycles

DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL EMERGENCY LIGHTS INOP AT AFT CABIN. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — MISSING (CABIN) · airframe 36,196 hrs · 36,429 cycles

DURING RON, FOUND EEPLS TRACK COVER MISSING AT MID CABIN. INSTALLED TRACK COVER PER MM.

Part: SOLENOID — LOOSE (GEAR HANDLE) · airframe 34,415 hrs · 34,658 cycles

DECLARED EMERGENCY, DURING LANDING, GEAR EXTENDED, RECEIVED 3 GREEN AND 3 RED LIGHT INDICATIONS. ACOMMPLISHED QRH MANUAL EXTENSION WHICH RESULTED IN 3 GREEN LIGHTS. LOOSE WIRE FOUND ON GEAR HANDLE SOLENOID. SECURED WIRE, CLEANED WIRE AND LUBED GEAR HANDLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,608 hrs · 33,828 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED, BS 940 TO 944, STRINGER 23L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (WING ROOT) · airframe 33,608 hrs · 33,828 cycles

DURING SCHEDULED C2 CHECK, FOUND LT EXTERNAL EMERGENCY LIGHT AT WING ROOT INOP. RELAMPED PER MM.

Part: COVER — LOOSE (CABIN) · airframe 32,490 hrs · 32,698 cycles

EEPLS TRCK LOOSE AT MID CABIN. SECURED TRACK COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED D CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REPAIRED WIRING AT LIGHT'S PIN CONNECTOR PER MM.

Part: STRINGER — CRACKED (BS 360 - 386)

DURING SCHEDULED D-CHECK, FOUND STRINGER 5L CRACKED, BS 360-386. SPLICED STRINGER SECTION PER SRM.

Part: SPAR — CRACKED (HORIZONTAL STAB)

DURING SCHEDULED D-CHECK, FOUND RT HORIZONTAL STAB FRONT SPAR CHORD CRACKED, STA 57.93. REPAIRED SPAR CHORD PER ER NR 99-6467.

Part: FRAME — CRACKED (BS 747 - 907)

DURING SCHEDULED D-CHECK, FOUND 6 FUSELAGE FRAME CRACKS, BS 747, LBL 60, BS 827, LBL 60 AND RBL 60, BS 867 LBL 60 AND RBL 60, AND BS 907, LBL 60. REPAIRED FRAMES PER ER NR 99-6438.

Part: POST — CRACKED (COCKPIT WINDOW)

DURING SCHEDULED D-CHECK, FOUND L1 COCKPIT WINDOW POST CRACKED, UPPER LT SECTION. REPAIRED PER SWA RA NR 1-A53-1156.

Part: FRAME — CRACKED (BS 616)

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 616, RBL 64, WL 201. REPAIRED FRAME PER SRM.

Part: CLIP — CRACKED (BS 685)

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED, BS 685, STRINGER 11L, AND BS 706, STRINGERS 11L AND 11R. REMOVED AND REPLACED CLIPS PER SRM.

Part: CLIP — CRACKED (BS 277)

DURING SCHEDULED D CHECK, FOUND 2 EACH STRINGER CLIPS CRACKED, BS 400, STRINGER 15L, AND BS 277, STRINGER 15R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FRAME — CRACKED (BS 616)

DURING SCHEDULED D CHECK, FOUND BS 616 FUSELAGE FRAME CRACKED, LBL 64. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (BS 270)

DURING SCHEDULED D CHECK, FOUND BS 270 FLOORBEAM UPPER SURFACE CORRODED, LBL 11-RBL 11. REMOVED AND REPLACED UPPER CHORD SECTION PER SRM.

Part: SKIN — DELAMINATED (LE FLAP)

DURING SCHEDULED D CHECK, FOUND NR 3 L/E SLAT INBOARD END DELAMINATED. REPAIRED SLAT PAR ER NR 99-6418 AND SRM.

Part: SKIN — CREASED (BS 183 - 188)

DURING SCHEDULED D CHECK, FOUND FUSELAGE EXTERNAL SKIN CREASED BETWEEN BS 183-188, WL 190 RH SIDE. REPAIRED SKIN PER SRM.

Part: BRACKET — CORRODED (CABIN)

DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR BOTH EVACUATION SLIDE ATTACH FLOOR BRACKETS CORRODED. REMOVED AND REPLACED BOTH BRACKETS PER SRM.

Part: STRINGER — CRACKED (BS 907)

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICES CRACKED, BS 907, STRINGERS 4L AND 4R. REPAIRED SPLICES PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD CRACKED AT 5 EACH PLACES, BETWEEN LBL 7 AND RBL 7. REPAIRED BULKHEAD PER SRM.

Part: FRAME — CRACKED (BS 312)

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 312, STRINGER 6L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED D CHECK, FOUND BS 328 FLOORBEAM CORRODED ON UPPER SURFACE, LBL 27 TO RBL 49. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED D CHECK, FOUND BS 312 FLOORBEAM UPPER SURFACE CORRODED, LBL 1 TO LBL 19. REPAIRED BEAM PER SRM.

Part: SLIDE — LOOSE (SERVICE DOOR)

DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE GIRT DRAGGING ON FLOOR. REINSTALLED SLIDE ASSY PER MM.

Part: WEB — CRACKED (LT MLG WW)

DURING SCHEDULED SPECIAL VISIT, FOUND LT MLG WHEEL WELL PRESSURE WEB CRACKED NEXT TO TOWER SHAFT. REPAIRED WEB PER ER NR 99-6239.

Part: WIRE — EXPOSED (CABIN)

ESCAPE PATH LIGHTING HAS EXPOSED WIRES AT MID CABIN. RESECURED TRACK LIGHTING COVER PER MM.

Part: FRAME — DAMAGED (BS 827)

BELTLOADER CONTACTED FUSELAGE SKIN UNDER AFT CARGO DOOR CAUSING BELTFRAME AND SHEAR TIE DAMAGE AT BS 827. REPAIRED PER BOEING SRM.

Part: INDICATOR — INOPERATIVE (RIGHT)

RIGHT WING FUEL QUANTITY BEGAN DROPPING DURING FLIGHT CAUSING THE INABILITY TO MAINTAIN BALANCED FUEL LOAD. AIRCRAFT DIVERTED TO CLE AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND RT MAIN FUEL QUANTITY INDICATOR INOP. REPLACED PER BOEING M/M.

Part: LIGHTS — INOPERATIVE (CABIN)

DURING BOARDING, PASSENGER KICKED FLOOR TRACK LIGHTING COVER AND ASSOCIATED WIRING LOOSE, DISABLING 4 WHITE LIGHTS. REPAIRED WIRES AND REPLACED COVER PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

AT GATE FOUND AN EMERGENCY EXIT LIGHT INOP. RELAMPED AND RESECURED LIGHT ASSEMBLY PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

AT GATE, FOUND EMERGENCY TRACK LIGHTING INOP AT ROWS 6, 7 AND 8. REPLACED EXIT LIGHT LOWER SUPPLY BASE PER BOEING M/M.

Part: WIRE — DISCONNECTED (CABIN)

DURING WALK-AROUND, FOUND SIX WHITE EMERGENCY TRACK LIGHTS INOP. INSPECTED AND FOUND WIRE PULLED FROM LIGHT ASSEMBLY AT ROW 18. REPAIRED AND OP CHECKED PER BOEING M/M.

Part: BRAKE LINE — RUPTURED (LT MLG)

EN ROUTE, NOTED HYDRAULIC QUANTITY DROP. DIVERTED TO ELP AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND LEFT MAIN GEAR BRAKE LINE LEAKING. REMOVED, REPLACED LINE AND LEAKED CHECKED PER BOEING M/M.

Part: WEB — CRACKED (BS 1088)

DURING SCHEDULED MAINT CHECK, FOUND WEB HOLE CRACK AT BS 1088 BULKHEAD. REPAIRED PER SWA RA 1-553-1234.

Part: WEB — CRACKED (BS 726)

DURING SCHEDULED MAINT CHECK, FOUND WEB CRACKED AT BS 726 STRINGER 18A, RIGHT SIDE. REPAIRED PER SWA RA 1-553-1233.

Part: CHORD — CRACKED (BS 294)

DURING SCHEDULED MAINT CHECK, FOUND FORWARD GALLEY DOORWAY INNER CHORD CRACKED AT BS 294. REPAIRED PER SWA RA 1-553-1228.

Part: WEB — CRACKED (AFT CARGO DR WAY)

DURING SCHEDULED 1/2 D CHECK, FOUND WEB CRACKED AND TORN OUT AT LOWER FWD END OF AFT CARGO DOORWAY. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: WEB — CRACKED (CARGO DOORWAY)

DURING SCHEDULED 1/2 D CHECK, FOUND AFT CARGO DOOR WEB CRACKED AND TORN AT AFT END OF DOORWAY. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOOR BEAM — CORRODED (BS 947)

DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM FORWARD FLANGE SCREW HOLE CORROSION AT BS 947, LBL 5, AND RBL 5. REPAIRED PER SWA RA 1-553-1229.

Part: FLOOR BEAM — CORRODED (BS 987)

DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM FORWARD FLANGE SCREW HOLE CORROSION AT BS 987, LBL 35. REPAIRED PER SWA RA 1-553-1230.

Part: FLOOR BEAM — CORRODED (BS 987)

DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM FORWARD FLANGE SCREW HOLE CORROSION AT BS 987, LBL 15. REPAIRED PER SWA RA 1-553-1232.

Part: FLOOR BEAM — CORRODED (BS 987)

DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM FORWARD FLANGE SCREW HOLE CORROSION AT BS 987, RBL 23, 28, 32, 36, 40, AND 43. REPAIRED PER SWA RA 1-553-1232.

Part: FLOOR BEAM — CORRODED (BS 987)

DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM FORWARD FLANGE SCREW HOLE CORROSION AT BS 987, RBL 26. REPAIRED PER SWA RA 1-553-1231.

Part: ANGLE — CORRODED (BS 294)

DURING SCHEDULED 1/2 D CHECK, FOUND FORWARD GALLEY RIGHT SIDE Z-ANGLE CORRODED BETWEEN BS 294 TO 312, BELOW THRESHOLD ATTACH POINTS. REPAIRED PER SWA RA 1-553-1228.