N344SW

Part: TAB — DELAMINATED (RT AILERON) · airframe 77,114 hrs · 67,516 cycles

RIGHT AILERON TAB OTBD AFT CORNER DELAMINATED. AILERON TAB REMOVED AND REPLACED PER AMM. RIG AND OP CHECK GOOD PER AMM. REF LOG PAGE 8352261 FOR FCF. TAG NO: 544529 PN ON: 65-46455-22C SN ON: BN148 PN OFF: SN OFF: WN0044.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,432 hrs · 67,009 cycles

SKIN CRACKED AT BS 741, STR 19L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,432 hrs · 67,009 cycles

SKIN CRACKED AT BS 727D+2, STR 19R. REPAIRED SKIN IAW EA AND AAR EA.

Part: MODULE — FAULTY (AC BAY) · airframe 75,887 hrs · 66,588 cycles

VISUAL SMOKE WITH SMELL FROM FIRST OFFICERS MAP LIGHT AREA. REMOVED AND REPLACED AIR CONDITIONING MODULE PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,324 hrs · 66,166 cycles

FUSELAGE SKIN CRACKED AT BS 500D +16, STR 15R. REPAIRED SKIN PER SRM.

Part: ACM — FAULTY (AC BAY) · airframe 75,324 hrs · 66,166 cycles

DIRTY SOCK SMELL IN COCKPIT ON TAKEOFF. DISSIPATED AT LOWER POWER SETTING. NOTICED IN CABIN. REMOVED AND REPLACED LEFT ACM PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 74,447 hrs · 65,492 cycles

LT WING O/B MID FLAP DELAMINATED. REPAIRED MID FLAP PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,447 hrs · 65,492 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,402 hrs · 65,455 cycles

DURING SCHEDULED OTS CHECK, FOUND R1 DOOR FUSELAGE SKIN CRACKED AT BS 302.5, STR 7R UPPER FWD CORNER. REPAIRED SKIN IAW ER AND EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,402 hrs · 65,455 cycles

DURING SCHEDULED OTS CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED IAW MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 74,402 hrs · 65,455 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,398 hrs · 65,454 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 302.5, STR 7R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,951 hrs · 65,125 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO BAY FRAME CRACKED AT BS 500C, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME IAW SI AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,951 hrs · 65,125 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO BAY FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME IAW SI AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,951 hrs · 65,125 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO BAY FRAME CRACKED AT BS 500D, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME IAW SI AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,951 hrs · 65,125 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO BAY FRAME CRACKED AT BS 500D, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME IAW SI AND SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,951 hrs · 65,125 cycles

DURING SCHEDULED SPV CHECK FOUND, STRINGER CRACKED AT BS 667, STR 16L. REPAIRED STRINGER PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 73,951 hrs · 65,125 cycles

EEPLS LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: FUSE — BLOWN (CABIN) · airframe 73,514 hrs · 64,785 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED FUSE PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 73,514 hrs · 64,785 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED WIRE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,514 hrs · 64,785 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 73,469 hrs · 64,747 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SPOILER — DELAMINATED (LT WING) · airframe 73,114 hrs · 64,472 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING NR 3 FLIGHT SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: MODULE — FAULTY (HYD RESERVOIR) · airframe 73,009 hrs · 64,390 cycles

AIR TURNBACK/DECLARED EMERGENCY. FAINT ODOR IN CABIN/COCKPIT AFTER TAKEOFF. REMOVED AND REPLACED HYD RESERVOIR AIR PRESSURE MODULE PER MM.

Part: PANEL — DELAMINATED (MIDFLAP) · airframe 73,009 hrs · 64,390 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING I/B MID FLAP T/E WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PANEL ER MM.

Part: LENS — LOOSE (CABIN) · airframe 72,775 hrs · 64,210 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 26R. REMOVED AND REPLACED CLIP PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER AFT DOOR CUTOUT. REPAIRED SKIN PER SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 500D, BETWEEN STR 13R TO STR 11R. REPAIRED SKIN PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED CLIP PER EA.

Part: SKIN — DELAMINATED (SPOILER) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 7 SPOILER UPPER AND LOWER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT AFT EEPLS INOP. RELAMPED BULB PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CORRODED AT BS 907, LBL 3. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 927, BETWEEN STR 24R TOS TR 25R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 947, BETWEEN STR 22R TOS TR 23R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 11R. REPAIRED SHEAR TIE PER ER AND EA.

Part: LIGHT — WORN (CABIN) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT WORN. REMOVED AND REPLACED LIGHT EPR MM.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 72,104 hrs · 63,689 cycles

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

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT KEEL BEAM CHORD TEE FITTING CRACKED AT BS 727. REPAIRED FITTING PER BAC DWG.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT KEEL BEAM CHORD TEE FITTING CRACKED AT BS 640. REPAIRED FITTING PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22YD CHECK, FOUND L1 ENTRY DOOR FWD GIRT BAR ATTACH FITTING CORRODED. REMOVED AND REPLACED ATTACH FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 25L. REMOVED AND REPLACED CLIP PER BAC DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND CABIN OVERWING ESCAPE HATCH DOORWAY FRAME STA 639, 2 INCHES ABOVE STR 17L FRAME WEB CRACKED. REMOVED AND REPLACED FRAME WEB ASSY PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 16L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 16R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: PLATE — CRACKED (L2 DOOR) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR INTERNAL CLOSE OUT PLATE BETWEEN HINGES CRACKED. REMOVED AND REPLACED PLATE PER BAC DWG.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND LOWER BULKHEAD KEEL BEAM FITTING CRACKED AT BS 727, LBL 6. REMOVED AND REPLACED FITTING PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1012, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 523, BETWEEN STR 15L TO STR 17L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM T-CAP CORRODED AT BS 986, BETWEEN LBL 4 TO LBL 44. REMOVED AND REPLACED T-CAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: BOLT — CORRODED (LT MLG) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT MLG SHOCK STRUT T-BOLT ATTACH BOLT BORE CORRODED. REMOVED AND REPLACED T-BOLT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 907+8.25 TO BS 927+2, STRINGER 24L TO STRINGER 26L. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CRACKED AT BS 673, BL 0. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED ON UPPER SURFACE I/B END. REPAIRED FORE FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CRACKED AT BS 727D, BETWEEN STR 28R TO STR 28L. REPAIRED FRAME PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT BS 729E, LBL 12. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO CHANNEL CORRODED AT BS 732D, LBL 3.0. REMOVED AND REPLACED CHANNEL PER SRM AND EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO CHANNEL CORRODED AT BS 732D, LBL 12.50. REMOVED AND REPLACED CHANNEL PER SRM AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 727E, LBL 3. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO FLOORBEAM ANGLE CORRODED AT BS 860, RBL 2. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 4R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 727E, LBL 17. REPAIRED BEAM PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO CHANNEL CORRODED AT BS 732D, RBL 3.0. REMOVED AND REPLACED CHANNEL PER SRM AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,104 hrs · 63,689 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,706 hrs · 46,321 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REMOVED AND REPLACED R1 DOOR PER EA.

Part: CONTROL LEVER — FAULTY (COCKPIT) · airframe 71,614 hrs · 63,308 cycles

DECLARED EMERGENCY. AFTER SELECTING GEAR DOWN 3 GREEN 3 RED. UNSAFE GEAR INDICATION. MANUALLY EXTENDED. REMOVED AND REPLACED LANDING GEAR LEVER ASSY PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 71,489 hrs · 63,216 cycles

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

Part: HINGE — BROKEN (SPOILER) · airframe 71,272 hrs · 63,042 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING I/B GROUND SPOILER HINGE BROKEN. REMOVED AND REPLACED GROUND SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,471 hrs · 62,403 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,471 hrs · 62,403 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 738.4E, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,471 hrs · 62,403 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 921.75 TO BS 924.75, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,471 hrs · 62,403 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED AT BS 729.25E, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,746 hrs · 61,824 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 20R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,746 hrs · 61,824 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D+5, STR 16L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 69,746 hrs · 61,824 cycles

DURING SCHEDULED HC2 CHECK, FOUND STR CLIP BROKEN AT BS 767, STR 19R. REMOVED AND REPLACED CLIP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,686 hrs · 61,780 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,580 hrs · 61,700 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT ENTRY LOWER EMERGENCY EXIT LIGHTS INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,580 hrs · 61,700 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD SERVICE LOWER EMERGENCY EXIT LIGHTS INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,305 hrs · 61,499 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 934, STR 22R. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 68,849 hrs · 61,173 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,795 hrs · 61,130 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 68,225 hrs · 60,710 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 68,136 hrs · 60,639 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVER LOOSE AT ROW 7. SECURED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,136 hrs · 60,639 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 385, STR 26R. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 68,136 hrs · 60,639 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS LOOSE BETWEEN ROW 8 TO ROW 15. SECURED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,136 hrs · 60,639 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 413, STR 26R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 67,683 hrs · 60,301 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,611 hrs · 60,248 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT AT LOWER FWD CORNER INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 67,498 hrs · 60,156 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,359 hrs · 60,062 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,359 hrs · 60,062 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 11R TO STR 13R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,261 hrs · 59,990 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500C, STR 15L. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,763 hrs · 59,631 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 15. REMOVED AND REPLACED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,763 hrs · 59,631 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT FWD NOSE WHEEL WELL SKIN CRACKED AT BETWEEN BS 239 TO BS 247. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 304, WL 261L. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 291, WL 233. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BETWEEN BS 290 TO BS 291, WL 234.5. REPAIRED SKIN PER ER.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 500D TO BS 520, STR 28L. REPAIRED BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 500C TO BS 500D, LBL 65. REPAIRED BEAM PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT KEEL BEAM CORRODED AT BS 510C. REPAIRED BEAM PER SRM.

Part: RIB — CORRODED (RT WING) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING LOWER CHORD CRACKED AT BS 135.5, BETWEEN STR 2R TO STR 3R. REPAIRED CHORD PER ACO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, RBL 3. REPAIRED BEAM PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT FWD CARGO BAY, BS 492, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 380 TO BS 400, LBL 65. REPAIRED WEB PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT BS 440, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT CREASE BEAM CORRODED BETWEEN BS 460 TO BS 480, LBL 65. REPAIRED BEAM PER SRM.

Part: AILERON — DELAMINATED (RT WING) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING AILERON DELAMINATED. REPAIRED AILERON PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 727B TO BS 727C, LBL 65. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR, BETWEEN BS 303 TO BS 304, BETWEEN WL 233 TO WL 261. REPAIRED SKIN PER ER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 420 TO BS 500D, LBL 65. REPAIRED WEB PER SRM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. REMOVED AND REPLACED HOOK PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING I/B AFT FLAP T/E WEDGE SKIN UPPER I/B CORNER DELAMINATED. REPAIRED SKIN PER SRM.

Part: RIB — CRACKED (LT WING) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING LOWER CHORD CRACKED AT BS 135, BETWEEN STR 2L TO STR 3L. REPAIRED CHORD PER ACO.

Part: FLAP — CRACKED (RT WING) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING O/B AFT FLAP CRACKED. REPAIRED AFT FLAP PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SUPPORT ANGLE CRACKED BETWEEN BS 292 TO BS 301, LBL 64. REMOVED AND REPLACED ANGLE PER SRM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING I/B AFT FLAP T/E WEDGE LOWER I/B CORNER DELAMINATED. REPAIRED WEDGE PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 5 SLAT T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 1 SLAT O/B END UPPER T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME WEB CRACKED AT BS 400, STR 8L. REPAIRED WEB PER SWA EA.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 2 SLAT I/B END UPPER T/E LOWER SURFACE DELAMINATED. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT CREASE BEAM CORRODED BETWEEN BS 747 TO BS 797, WL 208. REPAIRED BEAM PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 2 SLAT O/B END UPPER T/E LOWER SURFACE DELAMINATED. REPAIRED SLAT PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT BS 500, STR 28R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 328, RBL 30. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 709 TO BS 713, WL 202, BL 0. REPAIRED WEB PER SI.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 328, LBL 30. REPAIRED BEAM PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CORRODED AT BS 980, STR 27L. REMOVED AND REPLACED STRINGER PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 270, LBL 18. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME WEB CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME WEB CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,558 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME WEB CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,557 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 25R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,557 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,557 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 21L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,557 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 25L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 66,557 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT KEEL BEAM CORRODED AT BS 500D. REPAIRED KEEL BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,506 hrs · 59,440 cycles

DURING SCHEDULED SC CHECK, FOUND SKIN CRACKED AT BS 517, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,506 hrs · 59,440 cycles

DURING SCHEDULED SC CHECK, FOUND SKIN CRACKED AT BS 727E, BETWEEN STR 19R TO STR 20R. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 66,349 hrs · 59,338 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 65,802 hrs · 58,950 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,370 hrs · 58,653 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: CHARGER — FAULTY (EMERGENCY LIGHTS) · airframe 64,858 hrs · 58,285 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. R&R BATTERY CHARGER PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 64,858 hrs · 58,285 cycles

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

Part: SIGN — MISSING (EMERGENCY EXIT) · airframe 64,280 hrs · 58,256 cycles

AFT CABIN EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 64,310 hrs · 57,864 cycles

DURING SCHEDULED MV1 CHECK, L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: HINGE — BROKEN (NR 5 SPOILER) · airframe 64,043 hrs · 57,671 cycles

DURING SCHEDULED C2 CHECK, FOUND RIGHT WING NR 5 SPOILER HINGE AT OUTBOARD ACTUATOR BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — DELAMINATED (NR 6 SPOILER) · airframe 64,006 hrs · 57,644 cycles

RIGHT NR 6 SPOILER DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — DELAMINATED (NR 9 SPOILER) · airframe 64,006 hrs · 57,644 cycles

RIGHT NR 9 SPOILER DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED SPOILER PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 63,601 hrs · 57,345 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,243 hrs · 57,064 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 291, STR 16R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,243 hrs · 57,064 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, LBL 2. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,243 hrs · 57,064 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 390, RBL 2. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,243 hrs · 57,064 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, BL 0. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,243 hrs · 57,064 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259, STR 17R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,243 hrs · 57,064 cycles

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

Part: FITTING — LOOSE (GIRT BAR) · airframe 63,165 hrs · 57,005 cycles

R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.

Part: LENS — MISSING (CABIN) · airframe 63,056 hrs · 56,932 cycles

DURING SCHEDULED C1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 6ABC. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,056 hrs · 56,932 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,158 hrs · 56,229 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 978 S21L) · airframe 62,158 hrs · 56,229 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 978, STR 21L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 61,807 hrs · 55,940 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 61,234 hrs · 55,495 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 61,234 hrs · 55,495 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 61,021 hrs · 55,337 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 60,183 hrs · 54,708 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD FORE FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (BS 727E S18R) · airframe 59,753 hrs · 54,406 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18R. REPAIRED SKIN PER SWA EA.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 59,492 hrs · 54,207 cycles

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

Part: TAB — CRACKED (LT ELEVATOR) · airframe 58,494 hrs · 53,452 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT ELEVATOR TAB CRACKED AT L/E UPPER CUTOUT INBOARD HINGE. REMOVED AND REPLACED TAB PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,494 hrs · 53,452 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,494 hrs · 53,452 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 348, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,494 hrs · 53,452 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 58,420 hrs · 53,391 cycles

DURING SCHEDULED SPV CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 6 ABC TO ROW 8 ABC. REMOVED AND REPLACED EEPLS PHOTOLUMINESCENT STRIP PER MM.

Part: SKIN — CRACKED (BS 930 S21R) · airframe 58,177 hrs · 53,195 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 21R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 58,177 hrs · 53,195 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 58,177 hrs · 53,195 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: HOOK — LOOSE (L1 DOOR GIRT BAR) · airframe 57,282 hrs · 52,494 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. REMOVED AND REPLACED HOOK PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 57,282 hrs · 52,494 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,242 hrs · 52,456 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 20L. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 57,242 hrs · 52,456 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NLG W/W CEILING PANEL CUTOUT CRACKED AT BS 251.625, LBL 7.75 & RBL 7.75. REPAIRED PANELS PER SWA EA.

Part: SKIN — CRACKED (BS 735) · airframe 57,157 hrs · 52,388 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 735, STR 25R. REPAIRED SKIN PER SRM.

Part: SLIDE — ACTIVATED (R2 DOOR) · airframe 53,053 hrs · 49,240 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE IAW MM.

Part: CABLE — MISROUTED (R2 DOOR SLIDE) · airframe 56,283 hrs · 51,754 cycles

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

Part: SKIN — CRACKED (BS 740D) · airframe 55,888 hrs · 51,456 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740D, STR 19R. REPAIRED SKIN PER SRM.

Part: HINGE FITTING — CRACKED (R1 DOOR) · airframe 54,812 hrs · 50,599 cycles

R1 DOOR UPPER HINGE BOX HOUSING CRACKED. REMOVED AND REPLACED UPPER HINGE BOX PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 54,808 hrs · 50,596 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT NLG W/W FWD PRESSURE SIDE PANEL CRACKED AT BS 243.7, WL 168.5. REPAIRED PANEL PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,313 hrs · 50,197 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 24R. REPAIRED SKIN PER SRM.

Part: SLIDE — DISCHARGED (L2 DOOR) · airframe 53,655 hrs · 49,694 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 & R2 DOORS) · airframe 52,367 hrs · 48,680 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 AND L1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED BOTH R2 AND L1 DOOR EVAC SLIDES PER MM.

Part: SKIN — DELAMINATED (LT WING FOREFLAP) · airframe 52,367 hrs · 48,680 cycles

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

Part: LINE — CHAFED (HYD SYSTEM) · airframe 52,149 hrs · 48,497 cycles

DIVERSION, COMPLETE B-SYSTEM HYDRAULIC FAILURE. REMOVED AND REPLACED HYDRAULIC LINE ON B-SYSTEM PUMP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,568 hrs · 48,008 cycles

DURING SCHEDULED A1 CHECK, FOUND FWD LT EEPLS INOP. RELAMPED FWD EEPLS PER MM.

Part: SIGN — LOOSE (EMERGENCY EXIT) · airframe 51,216 hrs · 47,719 cycles

FWD RT OVERHEAD EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: CLEVIS — CRACKED (RT MLG) · airframe 50,395 hrs · 47,053 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT MLG BEAM ARM FWD CLEVIS LUG CRACKED. REMOVED AND REPLACED RT MLG CLEVIS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,157 hrs · 46,866 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 639 FRAME INBD CHORD CRACKED AT WL 208, RT SIDE. REPAIRED FRAME PER ERO.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 50,131 hrs · 46,849 cycles

DURING SCHEDULED 1/2D CHECK, FOUND KEELBEAM CRACKED AT BS 540, STR 28L AND STR 28R. REPAIRED KEEL BEAM PER ERO.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 50,131 hrs · 46,849 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 2 EA STRINGER SPLICES CRACKED AT BS 540, STR 10L, AND BS 360, STR 6L. REPAIRED STR SPLICES PER SRM AND ERO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,128 hrs · 46,846 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED AT BS 294.5, LBL 45.6. REPAIRED FLOORBEAM SECTION PER SRM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 50,128 hrs · 46,846 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR WEB CORRODED BETWEEN RT BS 400 AND RT BS 420, ABOVE AND BELOW FLOOR LEVEL. REPAIRED SHEAR WEB PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,128 hrs · 46,846 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 6L CRACKED FROM BS 360 TO BS 380. REPAIRED STRINGER SECTION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,128 hrs · 46,846 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 5L CRACKED AT BS 380. REPAIRED STRINGER PER SRM.

Part: RIB — DAMAGED (HORIZONTAL STAB) · airframe 50,128 hrs · 46,846 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT HORIZONTAL STAB RIB CREASED AT STAB STATION 129.50, LOWER TEE CHORD. REPAIRED LT STAB RIB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,128 hrs · 46,846 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT CREASE BEAM WEB CORRODED AT BS 418, RBL 70.53. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,128 hrs · 46,846 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR WEB CORRODED BETWEEN BS 500 AND BS 500A, RT SIDE OF FUSELAGE. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,128 hrs · 46,846 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME CRACKED AT BS 188, WL 207, RT SIDE 1 ABOVE FLOOR TO 1 BELOW FLOOR. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 50,128 hrs · 46,846 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,128 hrs · 46,846 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STRINGER 24R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 50,128 hrs · 16,846 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,128 hrs · 46,846 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIES CRACKED AT BS 360, BETWEEN STRINGERS 13L, 14L AND 15L. REPAIRED SHEAR TIES PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,128 hrs · 46,846 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT SHEAR WEB CORRODED AT BS 1016. REMOVED AND REPLACED SHEAR WEB PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,128 hrs · 46,846 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,128 hrs · 46,846 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT CREASE BEAM CORRODED BETWEEN BS 947 AND BS 987. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,128 hrs · 46,846 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 986, RBL 24. REPAIRED PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,128 hrs · 46,846 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 440 STRINGER 4R, AND BS 380, STRINGER 2L. REMOVED AND REPLACED STRINGER CLIPS SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,128 hrs · 46,846 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME IN E/E COMPARTMENT CRACKED AT BS 344, BETWEEN STRINGERS 23L AND 24L. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,128 hrs · 46,846 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIPS CRACKED AT BS 480, STRINGER 4L AND BS 616, STRINGER 4R. REMOVED AND REPLACED TIE CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,128 hrs · 46,846 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727, STRINGER 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRIP — LOOSE (CABIN) · airframe 49,566 hrs · 46,401 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,566 hrs · 46,407 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR AFT LOWER CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,566 hrs · 46,407 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR FWD LOWER CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,628 hrs · 45,638 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 10R, BS 500B AND BS 500C. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,628 hrs · 45,638 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT BULB INOP. REMOVED AND REPLACED BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,704 hrs · 44,907 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514, ABOVE STR 10R. REPAIRED SKIN PER SRM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 47,704 hrs · 44,907 cycles

DURING SCHEDULED C1 CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHING AT NR 1 ELEVATOR TAB HINGE ATTACH POINT PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 46,751 hrs · 44,162 cycles

DURING SCHEDULED C4 CHECK, FOUND LT HORIZ STAB LOWER SKIN CRACKED AT AFT SPAR RIVET ROW, CENTER BALANCE BAY. REPAIRED SKIN PER SRM.

Part: CYLINDER — CORRODED (LT MLG) · airframe 45,771 hrs · 43,357 cycles

DURING SCHEDULED RON, FOUND LT MLG AFT TRUNNION, AFT FACE CORRODED. REMOVED AND REPLACED LT MLG OUTER CYLINDER ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (AFT ENTRY DOOR) · airframe 44,945 hrs · 42,694 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: FLAP — DELAMINATED (LH WING) · airframe 42,281 hrs · 40,531 cycles

DURING SCHEDULED BC3 CHECK, FOUND OTBD T/E AFT FLAP DELAMINATED. R&R OTBD T/E AFT FLAP PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 41,664 hrs · 40,014 cycles

EEPLS LOOSE AT OVERWING EXIT. SECURED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 41,280 hrs · 39,679 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 41,212 hrs · 39,616 cycles

FWD CABIN OUTBOARD EMERGENCY FLASHLIGHT INOP. Removed and replaced EMERGENCY FLASHLIGHT PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,088 hrs · 38,678 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS SECTION INOP AT AFT CABIN. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 40,057 hrs · 38,654 cycles

FWD INBOARD EMERGENCY FLASHLIGHT WOULD NOT TEST. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: BATTERY PACK — OUT OF POSITION (CABIN) · airframe 39,733 hrs · 38,405 cycles

SEVERAL EEPLS BULBS INOP IN CABIN. RESEATED BATTERY PACK PER MM. OPS CHECK GOOD.

Part: INDICATOR — OUT OF POSITION (EVACUATION SLIDE) · airframe 38,523 hrs · 37,377 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 37,584 hrs · 36,582 cycles

DURING SCHEDULED C2 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED, STA 155 FWD OF FRONT SPAR. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 37,183 hrs · 36,218 cycles

FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN)

DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP ON FWD SECTION. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (UPPER FUSELAGE)

EXTERNAL FUSELAGE SKIN CRACKED, APPROX BS 540, STRINGER 10R. REPAIRED SKIN PER SRM.

Part: SLIDE — DETACHED (PAX DOOR)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: LENS — MISSING (ROW 18)

EMERGENCY EXIT LENS MISSING ON OVERHEAD BIN, ROW 18D. INSTALLED LENS PER MM.

Part: BULKHEAD CHORD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 VERTICAL CHORD CRACKED AT WL 195. REPLACED DAMAGED SECTION PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 947)

DURING SCHEDULED D-CHECK, FOUND UPPER FLOORBEAM CHORD CRACKED AT BS 947. REPLACED PER BOEING SRM.

Part: SPLICE — CRACKED (BS 907)

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

Part: FLOORBEAM — CORRODED (BS 294.5)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER T CHORD CORRODED AT BS 294.5. REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 935)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 935, 4 BELOW S23R. REPAIRED PER BOEING SRM.

Part: STRAP — CORRODED (BS 727)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM TIE STRAP CORRODED AT BS 727D+6. REPAIRED PER BOEING SRM.

Part: BEAM — CORRODED (BS 727)

DURING SCHEDULED D-CHECK, FOUND CARGO FLOORBEAM CORRODED AT BS 727E+3. REPAIRED PER BOEING SRM.

Part: LAMP — FAILED (ROW 23)

DURING SCHEDULED SC CHECK, FOUND A WHITE EMERGENCY FLOOR TRACK LIGHT INOP AT ROW 23DEF. RELAMPED PER BOEING M/M.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND A .5625 INCH FUSELAGE SKIN CRACK AT AFT ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED PER BOEING SRM.

Part: ACTUATOR — FAILED (NR 3 LE SLAT)

RETURNED TO AUS DUE TO NR 3 L/E SLAT NOT RETRACTING. REPLACED L/E SLAT ACTUATOR PER BOEING M/M.

Part: ELECT SYST — ODOR (COCKPIT)

AFTER ENGINE START, CREW EXPERIENCED AN ELECTRICAL TYPE SMELL IN COCKPIT. GASPER FAN WAS OFF. SUSPECTED OVERHEAD PANEL. INSPECTED WITH PANELS LOWERED. STARTED BOTH ENGINES, UNABLE TO DUPLICATE PROBLEM.

Part: SKIN — GOUGED (BS 356)

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 356, BELOW S18R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 383)

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN DENTED AT BS 383, BELOW S24R. REPAIRED PER BOEING SRM.