N312SW

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 79,276 hrs · 73,015 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SLIDE PER MM AND MT.

Part: LIGHT — LOOSE (CABIN) · airframe 78,647 hrs · 72,515 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,647 hrs · 72,515 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 504D, STR 8R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,647 hrs · 72,515 cycles

DURING SCHEDULED HC1 CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 78,647 hrs · 72,515 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 78,647 hrs · 72,515 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT L2 DOOR EEPLS LOOSE BETWEEN ROW 4 TO ROW 16. SECURED EEPLS PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 78,647 hrs · 72,515 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 78,552 hrs · 72,444 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,240 hrs · 72,213 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 972, STR 21L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,240 hrs · 72,213 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 516, STR 16R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,236 hrs · 72,212 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 516, STR 16R. REPAIRED SKIN PER ER.

Part: PRIORITY VALVE — FAULTY (RT MLG) · airframe 78,135 hrs · 72,151 cycles

AIR TURNBACK, RIGHT MLG FAILED TO RETRACT AFTER TAKEOFF. REMOVED AND REPLACED RIGHT MLG LOCK PRIORITY MODULAR VALVE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,940 hrs · 72,014 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CRACKED AT BS 550B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,940 hrs · 72,014 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CRACKED AT BS 550C, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,940 hrs · 72,014 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CRACKED AT BS 550D, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,940 hrs · 72,014 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CRACKED AT BS 550B, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,940 hrs · 72,014 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CRACKED AT BS 550D, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,940 hrs · 72,014 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 699, STR 10R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,940 hrs · 72,014 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 383, STR 15R. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 77,940 hrs · 72,014 cycles

DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CRACKED AT BS 400, BETWEEN STR 13R TO STR 14R. REMOVED AND REPLACED SHEAR TIE PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 77,940 hrs · 72,014 cycles

DURING SCHEDULED OTS CHECK, FOUND SHEAR TIE CRACKED AT BS 400, BETWEEN STR 15R TO STR 16R. REMOVED AND REPLACED SHEAR TIE PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,940 hrs · 72,014 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,940 hrs · 72,014 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 977.8, STR 5R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,940 hrs · 72,014 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 977.8, STR 5R. REPAIRED SKIN PER SRM & MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,233 hrs · 71,506 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 270, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,233 hrs · 71,506 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 727E, STR 5L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,233 hrs · 71,506 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 500B, STR 15L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,233 hrs · 71,506 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 500A, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,237 hrs · 71,507 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 500A, STR 26L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,237 hrs · 71,507 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 727E, STR 5L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,237 hrs · 71,507 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 500B, STR 15L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,237 hrs · 71,507 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 270, STR 16R. REPAIRED SKIN PER ER.

Part: FLAP — DELAMINATED (LT WING) · airframe 77,233 hrs · 71,506 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LENS — BROKEN (CABIN) · airframe 77,014 hrs · 71,358 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 76,465 hrs · 70,954 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,315 hrs · 70,850 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 516A, STR 20R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,315 hrs · 70,850 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500A, STR 21R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 76,286 hrs · 70,828 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,703 hrs · 70,384 cycles

DURING SCHEDULED 2HC1 CHECK, SKIN CRACKED AT BS 906, STR 3L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,703 hrs · 70,384 cycles

DURING SCHEDULED 2HC1 CHECK, SKIN CRACKED AT BS 855, STR 17R. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 75,703 hrs · 70,384 cycles

BULLNOSE LIGHT LENS LOOSE AT ROW 2. SECURED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 75,703 hrs · 70,384 cycles

DURING SCHEDULED 2HC1 CHECK, EEPLS LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,696 hrs · 70,378 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 404, STR 26R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,703 hrs · 70,384 cycles

DURING SCHEDULED 2HC1 CHECK, SKIN CRACKED AT BS 495, STR 9L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,703 hrs · 70,384 cycles

DURING SCHEDULED 2HC1 CHECK, SKIN CRACKED AT BS 947, STR 5R. REPAIRED SKIN PER SWA EA.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT KEEL BEAM CRACKED AT BS 713. REPAIRED BEAM PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT KEEL BEAM CORRODED AT BS 500D. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 559, STR 13R. REPAIRED FRAME PER AAR EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND R/H KEEL BEAM CORRODED BETWEEN BS 625 TO BS 741, STR 27R. R&R BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT KEEL BEAM SHEAR TIE CORRODED AT BS 500D. REPAIRED SHEAR TIE PER BAC DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND R/H KEEL BEAM CORRODED AT BS 533. REPAIRED BEAM PER SRM.

Part: FUSE — BLOWN (CABIN) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP BETWEEN ROW 2 TO ROW 3. R&R POWER SUPPLY FUSE PER MM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CORRODED BETWEEN BS 1016 TO BS 1018 AT SIX O'CLOCK POSITION. R&R STIFFENER PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND L/H KEEL BEAM CHORD CORRODED AT BS 727, LBL 8. R&R BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME PER ACO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 663, LBL 24.5. REPAIRED BEAM PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 259.5, BETWEEN STR 20L TO STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM LOWER CHORD CRACKED AT BS 663, RBL 24. REPAIRED BEAM PER AAR EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPT CRACKED SUPPORT BRACKET AT BS 727, RBL 25. REMOVED AND REPLACED T-FITTING PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 500D. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 747, STR 25L. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986, BETWEEN STR 19R TO STR 20R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CABIN EMERGENCY EXIT SIGN LENS LOOSE AT BS 907. SECURED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 13R. REPAIRED FRAME PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 500, BETWEEN STR 28R TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500B, STR 16R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND CENTER LONGITUDINAL FLOORBEAM CRACKED AT BS 707. REPAIRED BEAM PER SI.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 5 L/E SLAT LOWER SKIN CRACKED AT OUTBOARD END. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME CRACKED AT BS 847, BETWEEN STR 1R TO STR 2R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING O/B LEADING EDGE NR 4 SLAT UPPER SURFACE DELAMINATED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,465 hrs · 70,202 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,278 hrs · 70,062 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,278 hrs · 70,062 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 25L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,173 hrs · 69,946 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FUSELAGE SKIN SECTION CRACKED AT BS 430 TO BS 500A, STR 16R. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,173 hrs · 69,946 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 484, STR 16R. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 75,173 hrs · 69,946 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 500A, BETWEEN STR 15R & 16R. REPAIRED SHEAR TIE PER SRM.

Part: ACTUATOR — FAULTY (NR 6 SPOILER) · airframe 74,977 hrs · 69,846 cycles

DECLARED EMERGENCY. ON APPROACH SETTING TO FLAP 5 AIRCRAFT STARTED TO VIBRATE, VIBRATION FELT ON FLIGHT CONTROL, DECLARED EMERGENCY. REMOVED AND REPLACED NR 6 FLIGHT SPOILER ACTUATOR PER MM.

Part: COVER — BROKEN (CABIN) · airframe 74,871 hrs · 69,771 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 74,872 hrs · 69,771 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,710 hrs · 69,656 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR, LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,709 hrs · 69,656 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259, BELOW STR 9L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,709 hrs · 69,656 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,709 hrs · 69,656 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,709 hrs · 69,656 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE DOUBLER. REMOVED AND REPLACED SKIN PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 74,709 hrs · 69,656 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 987, STR 27R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 74,709 hrs · 69,656 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 986, STR 24R. REPAIRED SKIN PER SWA EA.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 74,709 hrs · 69,656 cycles

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

Part: SLAT — DELAMINATED (LT WING) · airframe 74,709 hrs · 69,656 cycles

DURING SCHEDULED OTS CHECK, FOUND LT WING 2 SLAT OUTBOARD T/E DELAMINATED. REMOVED AND REPLACED SLAT PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 74,709 hrs · 69,655 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT O/B T/E DELAMINATED. REPAIRED SLAT PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,680 hrs · 69,636 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,680 hrs · 69,636 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 697, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,680 hrs · 69,636 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 691, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,680 hrs · 69,636 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 490, STR 16L. REPAIRED SKIN PER SRM.

Part: ACTUATOR — FAULTY (LT MLG) · airframe 74,168 hrs · 69,262 cycles

DURING APPROACH LT MLG WOULD NOT INDICATE DOWN, RETRACTED GEAR, DID MANUAL EXTENSION GEAR DOWN, INDICATION NORMAL. REMOVED AND REPLACED MLG UPLOCK ACTUATOR AND PRIORITY MODULAR VALVE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,730 hrs · 68,939 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 322, STR 24R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 73,242 hrs · 68,562 cycles

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

Part: ACTUATOR — FAULTY (RT MLG) · airframe 73,242 hrs · 68,562 cycles

DURING CLIMB RT MLG UNSAFE LIGHT ILLUMINATED. AFTER MOVING GEAR HANDLE TO OFF POSITION RT GEAR FELL OUT OF W/W. CYCLED GEAR, GEAR RETRACTED NORMAL INDICATIONS. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,917 hrs · 68,324 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 455, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 500 S15R) · airframe 72,851 hrs · 68,278 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,549 hrs · 68,036 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 512, BETWEEN STR 16L AND STR 17L. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,549 hrs · 68,036 cycles

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

Part: PUMP — FAILED (NR 1 ENGINE) · airframe 72,119 hrs · 67,721 cycles

AIR TURNBACK / DECLARED EMERGENCY. HYDRAULIC "A" SYSTEM FAILED IN FLIGHT. REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP AND CASE DRAIN LINE PER MM.

Part: CHARGER — FAULTY (CABIN) · airframe 71,895 hrs · 67,542 cycles

FWD CABIN EMERGENCY EXIT LIGHTS ILLUMINATED INTERMITTENTLY. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,742 hrs · 67,422 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505B, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,742 hrs · 67,422 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 475, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,526 hrs · 67,253 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 460, STR 16R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,353 hrs · 67,117 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17L. REPAIRED FRAME PER ER.

Part: STRINGER CLIP — CRACKED (BS 1040 S13L) · airframe 71,353 hrs · 67,116 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 1040, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (BS 258) · airframe 71,353 hrs · 67,116 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 258, WL 181.5, LEFT SIDE. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 678 S10L) · airframe 71,353 hrs · 67,116 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 678, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 258) · airframe 71,353 hrs · 67,116 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 258, WL 170.5, LEFT SIDE. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,644 hrs · 66,560 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 400, STR 16R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 70,489 hrs · 66,429 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,489 hrs · 66,429 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 344, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,687 hrs · 65,816 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 455, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,634 hrs · 65,769 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 923, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,634 hrs · 65,769 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 507, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,634 hrs · 65,769 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,634 hrs · 65,769 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,442 hrs · 65,629 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 372, STR 14L. REPAIRED SKIN PER SWA EA.

Part: BAR — CORRODED (RT WING) · airframe 69,285 hrs · 65,494 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RIGHT WING STABILIZER BAR CORRODED. REMOVED AND REPLACED RIGHT WING STABILIZER BAR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,681 hrs · 65,039 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 14R. REPAIRED SKIN PER SWA EA.

Part: WEDGE — DEBONDED (T/E FLAP) · airframe 68,681 hrs · 65,039 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT WING INBOARD MID FLAP T/E WEDGE DISBONDED AT OUTBOARD END. REMOVED AND REPLACED MID FLAP WEDGE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,681 hrs · 65,039 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 500 S18R) · airframe 68,672 hrs · 65,032 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 18R. REPAIRED SKIN PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,210 hrs · 65,845 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,210 hrs · 65,845 cycles

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

Part: SKIN — CRACKED (BS 415-447) · airframe 69,210 hrs · 65,845 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 415 TO BS 447, BL 0. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,388 hrs · 64,805 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 427, BBL 0, RADIO ALT ANTENNA CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,388 hrs · 64,805 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 910, STR 4L. REPAIRED SKIN PER ER.

Part: STRINGER — CRACKED (BS 360 S15L) · airframe 68,383 hrs · 64,805 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 15L CRACKED AT BS 360. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SKIN — CRACKED (BS 405 S16L) · airframe 67,747 hrs · 64,291 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 405, STR 16L. REPAIRED SKIN PER SWA EA.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 67,747 hrs · 64,291 cycles

DURING SCHEDULED C3 CHECK, FOUND NLG W/W WEB CRACKED AT RT BS 259, WL 174. REPAIRED WEB PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,795 hrs · 63,530 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 516, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,795 hrs · 63,530 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 456, STR 16R. REPAIRED SKIN PER SWA EA.

Part: CABLE — MISROUTED (R2 DOOR) · airframe 66,795 hrs · 63,530 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED EVAC SLIDE CABLE PER MM.

Part: CABLE — MISROUTED (L2 DOOR) · airframe 66,795 hrs · 63,530 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED EVAC SLIDE CABLE PER MM.

Part: SKIN — CRACKED (BS 468 S16R) · airframe 66,171 hrs · 63,051 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 468, S16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 500C) · airframe 66,171 hrs · 63,051 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 913) · airframe 65,996 hrs · 62,924 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 913, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 512) · airframe 65,502 hrs · 62,555 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 512.5 TO BS 516A, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 306-308) · airframe 65,502 hrs · 62,555 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 306 TO BS 308.5, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 373) · airframe 64,881 hrs · 62,033 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 373, STR 17R. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 466) · airframe 64,881 hrs · 62,033 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 466, STR 26L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 500A) · airframe 64,342 hrs · 61,600 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 412.375) · airframe 64,342 hrs · 61,600 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 412.375, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 514.50) · airframe 64,342 hrs · 61,600 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514.50, STR 15L. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,172 hrs · 61,462 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK HOUSING & CHARGER PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 64,040 hrs · 61,351 cycles

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

Part: SPLICE — CORRODED (E / E BAY) · airframe 63,668 hrs · 61,038 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER SPLICE CORRODED AT BS 360, STR 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 63,658 hrs · 61,030 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FWD & AFT FAILSAFE CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.

Part: FRAME — CRACKED (COCKPIT FLOOR) · airframe 63,658 hrs · 61,030 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE STUB FRAMES CRACKED AT BS 188, LT & RT SIDE, WL 208. REMOVED AND REPLACED STUB FRAMES PER SRM.

Part: WEB — CRACKED (COCKPIT FLOOR) · airframe 63,658 hrs · 61,030 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FLOOR WEB CRACKS BETWEEN BS 188 TO BS 196, LT & RT SIDE, WL 208. REPAIRED FLOOR WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,658 hrs · 61,030 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME INNER CHORD CRACKED AT BS 348, LBL 50, WL 208. REPAIRED FRAME INNER CHORD PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,628 hrs · 61,012 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 360, STR 28R TO STR 28L, WL 149. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,628 hrs · 61,012 cycles

DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 712, LBL 25, WL 203. REPAIRED FLOORBEAM PER BFG ER.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 63,628 hrs · 61,012 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, STR 22R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,619 hrs · 61,005 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, STR 25L TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,619 hrs · 61,005 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, STR 25L TO STR 27L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,619 hrs · 61,005 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE SHEAR TIES CORRODED AT BS 787 & BS 807, STR 26L TO STR 26R. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: FITTING — CORRODED (L1 DOOR SLIDE) · airframe 63,619 hrs · 61,005 cycles

DURING SCHEDULED D-CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD & AFT GIRT BAR FLOOR FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,619 hrs · 61,005 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB AT BS 312, RBL 60. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,619 hrs · 61,005 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 870, STR 26R. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,619 hrs · 61,005 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE SHEAR TIES CORRODED AT BS 727E & BS 747, STR 27L TO STR 26R. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 63,619 hrs · 61,005 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB ATTACH FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,619 hrs · 61,005 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 907, STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,601 hrs · 60,989 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA CRACKS AT BS 1016 PRESSURE BULKHEAD DOME CAP WEB, 6 & 7 O'CLOCK POSITIONS. REPAIRED WEB PER BFG ER.

Part: STRINGER CLIP — CRACKED (BS 727A) · airframe 63,601 hrs · 60,989 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727A, STR 5L & STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,601 hrs · 60,989 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, LBL 15 TO LBL 35, WL 208. REPAIRED FLOORBEAM PER BFG ER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,601 hrs · 60,989 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 1010, STR 7L. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,601 hrs · 60,989 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,601 hrs · 60,989 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 17 TO RBL 50, WL 208. REPAIRED FLOORBEAM PER BFG ER.

Part: FLOORBEAM — CRACKED (BS 727B) · airframe 63,601 hrs · 60,989 cycles

DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, BETWEEN LBL 45 & RBL 45. REPAIRED FLOORBEAM PER BFG ER.

Part: FRAME — CRACKED (BS 727) · airframe 63,601 hrs · 60,989 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BETWEEN BS 727B TO BS 727E, STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,576 hrs · 60,967 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 489, RBL 7. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FWD CARGO BAY) · airframe 63,576 hrs · 60,967 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 460, LBL 18. REPAIRED FRAME PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,576 hrs · 60,967 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED BETWEEN BS 466 TO BS 470, LBL 1 TO RBL 1. REPAIRED SKIN PER SRM & BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,576 hrs · 60,967 cycles

DURING SCHEDULED D-CHECK, FOUND 2 CRACKS IN FRAME AT BS 380, STR 15R & STR 16R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,576 hrs · 60,967 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,576 hrs · 60,967 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 480, STR 12L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FWD CARGO BAY) · airframe 63,576 hrs · 60,967 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500, LBL 4. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 294) · airframe 63,576 hrs · 60,967 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294.5, STR 11L, STR 12L & STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: RIB — CRACKED (LT WING) · airframe 63,576 hrs · 60,967 cycles

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

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 63,576 hrs · 60,967 cycles

DURING SCHEDULED D-CHECK, FOUND LT CREASE BEAM WEB CRACKED AT BS 500C + 14. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: FRAME — CRACKED (BS 440) · airframe 63,576 hrs · 60,967 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 440, STR 9R. REPAIRED FRAME PER SRM.

Part: FLOOR SKIN — CRACKED (COCKPIT) · airframe 63,564 hrs · 60,956 cycles

DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOOR SKIN CRACKED AT BS 244, RBL 15. REPAIRED FLOOR SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,564 hrs · 60,956 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,564 hrs · 60,956 cycles

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

Part: STRINGER CLIP — CRACKED (BS 597) · airframe 63,564 hrs · 60,956 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 597, STR 7R & STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706) · airframe 63,564 hrs · 60,956 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 10L & STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,564 hrs · 60,956 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME UPPER STRUCTURE IS CRACKED AT BS 663, STR 1L TO STR 3L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616) · airframe 63,564 hrs · 60,956 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 616, STR 3L, STR 5L & STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,564 hrs · 60,956 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 639, STR 17L, WL 210. REPAIRED FRAME CHORD PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,384 hrs · 60,791 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 489, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,384 hrs · 60,791 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 939 TO BS 942, STR 21L. REPAIRED SKIN PER SRM.

Part: BOLT — WORN (RT ELEV TAB) · airframe 63,006 hrs · 60,508 cycles

DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB CONTROL PUSHROD BOLTS & SPACERS PER MM.

Part: FRAME — CRACKED (R1 DOOR) · airframe 63,006 hrs · 60,508 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR LOWER FRAME CRACKED AT AFT DOOR STOP FITTING CUTOUT. REMOVED AND REPLACED DOOR PER MM.

Part: SLIDE — READS LOW (R1 DOOR) · airframe 62,781 hrs · 60,332 cycles

R1 DOOR EVAC SLIDE LOW PRESSURE IND. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,055 hrs · 59,788 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,055 hrs · 59,788 cycles

DURING SCHEDULED C1 CHECK, FOUND 3 EA FUSELAGE SKIN CRACKS AT BS 370, STR 26L, BS 377, STR 19R, AND BS 366, STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,055 hrs · 59,788 cycles

DURING SCHEDULED C1 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 767, STR 19L AND BS 727E, STR 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,025 hrs · 59,766 cycles

FUSELAGE SKIN CRACKED AT BS 376, STR 8L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,550 hrs · 59,400 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 20R, CRACKED. REPAIRED SKIN PER EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 61,289 hrs · 59,174 cycles

DURING SPV, FOUND LT HORIZONTAL STAB LOWER RIB CHORD AT STATION 120, CRACKED. REMOVED AND REPLACED LT HORIZONTAL STAB RIB CHORD SECTION PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 61,224 hrs · 59,120 cycles

DURING SCHEDULED C4 CHECK, FOUND LOWER RT KEEL BEAM CHORD AT BS 500A, STRINGER 28R, CORRODED. REPAIRED KEEL BEAM PER EA.

Part: CABLE — FRAYED (L2 DOOR SLIDE) · airframe 61,220 hrs · 59,114 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED L2 DOOR EVAC SLIDE CABLE PER MM.

Part: CABLE — MISROUTED (R2 DOOR SLIDE) · airframe 61,220 hrs · 59,114 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED R2 DOOR EVAC SLIDE CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,028 hrs · 58,963 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 793.5, STRINGER 18L, BS 840, STRINGER 15L, CRACKED. REPAIRED SKIN PER EA & SRM.

Part: MOTOR — FAILED (NR 2 ENGINE) · airframe 60,643 hrs · 58,658 cycles

AT 8000 FT AND BELOW EXPERIENCED SEVERAL LOUD BUMPS WHICH SHOOK. THE AIRCRAFT SOURCE SEEMED TO BE FROM RIGHT, SIDE SLIGHT YAW (NOT IN PEDALS). REMOVED AND REPLACED NR 2 ENGINE VBV MOTOR AND BLEED VALVE, PER MM. REMOVED AND REPLACED NR 2 ENGINE MEC AND CIT SENSOR PER MM.

Part: COVER — CRACKED (R1 DOOR SLIDE) · airframe 60,406 hrs · 58,463 cycles

R1 DOOR EVAC SLIDE PRESSURE IND LENS COVER CRACKED. REMOVED AND REPLACED LENS COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,247 hrs · 58,329 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 20L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,367 hrs · 57,648 cycles

DURING SCHEDULED C2 CHECK, FOUND 2 CRACKS ON FUSELAGE SKIN AT BS 390, STRINGER 17R. REPAIRED SKIN CRACKS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,861 hrs · 57,266 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 3.4 LONG FUSELAGE SKIN CRACKED AT BS 415, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,912 hrs · 56,491 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 312, BELOW 18R. REPAIRED SKIN PER SRM.

Part: INDICATOR — OUT OF LIMITS (ESCAPE SLIDE) · airframe 57,063 hrs · 55,808 cycles

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

Part: INDICATOR — OUT OF LIMITS (ESCAPE SLIDE) · airframe 57,063 hrs · 55,808 cycles

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

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 56,970 hrs · 55,733 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,407 hrs · 55,291 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 270.875 & BS 274, AT STR 16L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 56,126 hrs · 55,078 cycles

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

Part: AILERON — DELAMINATED (LT WING) · airframe 55,772 hrs · 54,806 cycles

DURING SCHEDULED C2 CHECK, FOUND LT AILERON DELAMINATED ON LOWER SKIN BETWEEN NR 2 AND NR 3 HINGES. REMOVED AND REPLACED LT AILERON PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 55,772 hrs · 54,806 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 1 L/E SLAT DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED NR 1 L/E SLAT PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 55,772 hrs · 54,806 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.

Part: LENS — MISSING (CABIN) · airframe 55,763 hrs · 54,799 cycles

DURING SCHEDULED C2 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 14 ABC. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 55,721 hrs · 54,769 cycles

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

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 55,225 hrs · 54,369 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT HORIZ STAB L/E SKIN CRACKED 90 OTBD OF ATTACH LUG. REPAIRED RT HORIZ STAB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,029 hrs · 53,404 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT LT BS 352, WL 243. REPAIRED SKIN PER SWA EA.

Part: SIGN — DELAMINATED (CABIN) · airframe 54,018 hrs · 53,395 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH LEFT AND RIGHT PHOTO-LUMINESCENT EMERGENCY EXIT STRIPS DELAMINATED AT ROW NR 9. REMOVED AND REPLACED STRIPS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,029 hrs · 53,404 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT RT STA 502, WL 236. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,018 hrs · 53,395 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,899 hrs · 53,302 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 25R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 53,892 hrs · 53,298 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 53,824 hrs · 53,242 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,108 hrs · 57,142 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGERS CRACKED (2 EA) STR 13L BETWEEN BS 380 AND BS 400, AND BS 616, STR 4L. REPAIRED STRINGERS PER CASCADE ERO.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,782 hrs · 53,205 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BELOW STR 14R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,782 hrs · 53,205 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REPAIRED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,782 hrs · 53,205 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 234 AND LBL 15. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,915 hrs · 52,487 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKINS CRACKED (4 EA) AT STR 4R, BS'S 460, 500A, 500B AND 727E. REPAIRED SKINS PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,780 hrs · 52,379 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (6 EA) BETWEEN BS 480 AND BS 486, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,780 hrs · 52,379 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 10R. REPAIRED SKIN PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,780 hrs · 52,379 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 3.5 INCHES LONG AT BS 738, STR 20L. REPAIRED SKIN PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED 2 1/2 INCH LONG AT BS 500C+ 6, ABOVE STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,989 hrs · 51,742 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED 1 1/4 INCH LONG AT BS 727, STR 20L. REPAIRED SKIN PER SRM.

Part: SLIDE — LOOSE (AFT ENTRY DOOR) · airframe 51,952 hrs · 51,710 cycles

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

Part: WINDOW — CRACKED (FUSELAGE) · airframe 51,675 hrs · 51,471 cycles

( DIVERSION )…………………………..R1 COCKPIT WINDOW ARCED & SHATTERED. R&R WINDOW & WINDOW HEAT CONTROLLER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,057 hrs · 50,966 cycles

DURING SCHEDULED C1 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS, BS 482, STRINGERS 10R & 4R, AND BS 787, STR 10L.. REPAIRED SKIN PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,057 hrs · 50,966 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STRINGER 10L. REPAIRED SKIN PER SWA RA.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 50,529 hrs · 50,508 cycles

EMERGENCY FLASHLIGHT INOP IN AFT CABIN LOWER POSITION. R&R EMERGENCY FLASHLIGHT PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 50,383 hrs · 50,369 cycles

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

Part: WEDGE — DELAMINATED (L/E SLAT) · airframe 50,135 hrs · 50,148 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING NR 3 L/E SLAT T/E WEDGE DISBONDED, 75 PERCENT OF PANEL. REMOVED AND REPLACED NR 3 SLAT PER MM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 49,594 hrs · 49,718 cycles

EEPLS TRACK COVER LOOSE AT ROW 9. SECURED TRACK COVER PER MM.

Part: SLIDE — LOOSE (SERVICE DOOR) · airframe 49,146 hrs · 49,337 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED EVAC SLIDE ASSY PER MM.

Part: ENGINE — VIBRATION (NR 2) · airframe 49,130 hrs · 49,316 cycles

AIR TURNBACK, NR 2 ENGINE VIBRATION ON CLIMB-OUT. INSPECTED NR 2 ENGINE PER MM - NO ABNORMALITIES FOUND. RAN BOTH ENGINES AT T/O POWER FOR SEVERAL MINUTES. OK FOR SERVICE.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 48,926 hrs · 49,149 cycles

AFT SVC EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. RE-ADJUSTED SLIDE ASSY PER MM.

Part: CONTROL CABLE — OUT OF ADJ (TE FLAPS) · airframe 48,786 hrs · 49,034 cycles

DIVERSION, T/E FLAPS INDICATED NOT FULLY RETRACTED AT ALTITUDE. L/E DEVICES SHOW FULLY RETRACTED. AUTO PILOT DISCONNECTED. RETARDED THROTTLES AND GEAR WARNING HORN SOUNDED. ADJUSTED FLAP CONTROL CABLES WFA, WFA AND FLAP FOLLOW-UP CABLES WFFA AND WFFB PER MM. REPAIRED WIRE TO FLAP CABLE BREAK DETECT SWITCH PER WDM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,448 hrs · 48,743 cycles

ON WALKAROUND, FOUND 3 INCH SKIN CRACK LT SIDE, NEAR WING ILLUMINATION LIGHT. REPAIRED SKIN PER SRM.

Part: SWITCH — INOPERATIVE (CABIN) · airframe 47,366 hrs · 47,827 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT F/A''S EMERGENCY LIGHT SWITCH INOP. REMOVED AND REPLACED SWITCH PER MM.

Part: SPAR — CRACKED (LT ELEVATOR) · airframe 47,187 hrs · 47,655 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT ELEVATOR REAR SPAR CRACKED NEAR SECOND I/B TAB HINGE. REMOVED AND REPLACED LT ELEVATOR ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,187 hrs · 47,655 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD LT SIDE CHORD CRACKED, WL 207. REPAIRED CHORD SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,187 hrs · 47,655 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 300, STRINGER 4L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,187 hrs · 47,655 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS AFT ENTRY DOOR CUTOUT UPPER FWD CORNER STUB FRAME CRACKED. REMOVED AND REPLACED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,187 hrs · 47,655 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 986 FLOORBEAM UPPER SURFACE CORRODED. REMOVED AND REPLACED FLOORBEAM UPPER T-CAP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,187 hrs · 47,655 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 947 FLOORBEAM CRACKED, LBL 56. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,187 hrs · 47,655 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 515, STRINGER 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,187 hrs · 47,655 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 516, STRINGER 10R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,187 hrs · 47,655 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD RIGHT O/B CHORD CRACKED, WL 207. REPAIRED CHORD SECTION PER SRM.

Part: FLOORBEAM — CORRODED (GALLEY) · airframe 47,187 hrs · 47,655 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 344 FLOORBEAM UPPER SURFACE CORRODED, LBL 11. REPAIRED FLOORBEAM PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,187 hrs · 47,655 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 663 BULKHEAD CRACKED, LBL 32. REPAIRED WEB PER TRM TI-353-046.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 47,187 hrs · 47,655 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 312 FLOORBEAM UPPER SURFACE CORRODED, LBL 11 TO RBL 11. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (SERVICE DOOR) · airframe 47,187 hrs · 47,655 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR AFT FRAME CRACKED AT 3RD DOOR STOP. REPAIRED FRAME PER T1-152-003.

Part: LINE — CRACKED (NLG STEERING)

NOSE WHEEL STEERING INOP AFTER LANDING. FOUND WATER LEAK FROM CRACKED FWD LAV DRAIN LINE FREEZING NLG STEERING PULLEYS. REMOVED AND REPLACED DRAIN LINE, CLEANED BELLY INTERIOR. LEAK AND OPS CK GOOD PER MM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND BULL NOSE EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGER PER MM.

Part: LIGHT — INOP (CABIN)

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

Part: SKIN — CRACKED (UPPER FUSELAGE)

DURING WALK ARROUND INSPECTION, FOUND APPROX A 8 INCH LONG CRACK ON FUSELAGE CROWN 4 FEET FWD OF ANTI COLLITION LIGHT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 510)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 510, ABOVE STRINGER 11L. REPAIRED SKIN PER SRM.

Part: HOOK — LOOSE (PAX DR GIRT BAR)

AFT ENTRY DOOR EMERGENCY EVACUATION SLIDE GIRT BAR LATCH HOOK HAS BROKEN SCREW. REMOVED AND REPLACED LATCH HOOK ASSY PER MM.

Part: SKIN — CRACKED (BS 770)

DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACKED 2.5 INCHES AT S19R, BS 770. REPAIRED PER BOEING SRM.

Part: BATTERY PACK — DISCHARGED (LT & RT OVERWING)

DURING SCHEDULED SERVICE CHECK, FOUND BOTH OVERWING EMERGENCY HATCH DOOR LIGHTS ARE INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY TRACK LIGHTS WOULD NOT TURN-OFF WITH BATTERY POWER IN OFF AND EMERGENCY LIGHTS SWITCHED TURN IN OFF POSITION. REMOVED AND REPLACED FWD AND AFT FLOOR TRACK LIGHTING BATTERY PACKS PER BOEING MM.

Part: FLIGHT CONTROLS — SHIMMY (WING/EMPENNAGE)

AIR RETURN, ON CLIMBOUT A/C STARTED TO SHAKE/SHIMMY AT 160-180 KTS. FLAPS DOWN. AT 210-250 KTS CLIMBING CONTINUE SHAKE/SHIMMY LEVEL FLIGHT (10K) 230-250 KTS NOT AS BAD DURING DESCENT. CLEAN 230-210 KTS, SHAKING NOT AS BAD AS LEVEL FLT. FLAPS 5 GEAR DOWN 170 KTS. PRONOUNCED SHAKE/SHIMMY (NOT FISHTAIL). INSPECTED ALL FLIGHT CONTROLS, LANDING GEAR DOORS AND ENGINES RAN ENGINES AT TAKEOFF POWER. ISOLATED FOUND NO FAULTS ON INSPEC AND TEST FLIGHT REVEALED NO PROBLEMS PER BOEING MM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE OUTER SKIN CRACKED AT LOWER HINGE RADIUS OF AFT SERVICE DOOR UNDER PRODUCTION LAP JOINT DOUBLER. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND RIGHT SIDE MID CABIN EMERGENCY EXIT LIGHT INOP \N\NREPLACED BATTERY PACK PER BOEING M/M

Part: BATTERY CHARGER — INOPERATIVE (CABIN)

DURING RON CHECK, FOUND THAT CABIN EMERGENCY TRACK LIGHTS WOULD NOT DISARM. REPLACED AFT BATTERY CHARGER PER BOEING M/M.

Part: SKIN — CRACKED (BS 757)

DURING SCHEDULED TERMINAL CHECK, FOUND A 3 INCH FUSELAGE SKIN CRACK AT BS 757, BELOW S19R. REPAIRED PER BOEING SRM.

Part: WINDOW POST — CRACKED (L1/R1 COCKPIT)

DURING SCHEDULED BC1 CHECK, FOUND R1 AND L1 C-D COCKPIT WINDOW POSTS CRACKED. INSTALLED REPAIR PER SWA RA 1-A53-1156.

Part: FRAME — CRACKED (BS 827)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827 S9L AT FASTENER HOLE. REPAIRED PER BOEING SRM.

Part: FLOOR BEAM — CORRODED (BS 344)

DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 344 LBL 35 LBL 7.5 BL 0 AND RBL 1.5. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 312)

DURING SCHEDULED C1 CHECK, FOUND FLOORBEAM STRAPS CRACKED AT RBL 32 AND AT LBL 12 BS 312 IN E AND E COMPARTMENT. REPAIRED PER BOEING SRM.