N333SW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,376 hrs · 67,968 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 21. RELAMPED LIGHT PER MM.

Part: ACTUATOR — LEAKING (SPOILER) · airframe 76,202 hrs · 67,839 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT WING NR 7 FLIGHT SPOILER LEAKED. REMOVED AND REPLACED ACTUATOR PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 75,799 hrs · 67,544 cycles

DURING SCHEDULED 24Y CHECK, FOUND LOWER FUSELAGE KEEL BEAM CORRODED BETWEEN BS 530 TO BS 540, STR 28R. REMOVED AND REPLACED BEAM IAW SRM AND DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 75,799 hrs · 67,544 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 500C+10 BS 540+10. REPAIRED BEAM PER SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,799 hrs · 67,544 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT SKIN CORRODED BETWEEN BS 787 TO BS 807+3, BETWEEN STR 22R+6 TO STR 26R+3. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,799 hrs · 67,544 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME WEB CRACKED AT BS 277, STR 16R. REMOVED AND REPLACED WEB IAW EA AND DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 75,799 hrs · 67,544 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT KEEL BEAM LOWER O/B FLANGE CORRODED BETWEEN BS 676 TO BS 727. REPAIRED BEAM IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,799 hrs · 67,544 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, LBL 33. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 75,799 hrs · 67,544 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT KEEL BEAM LOWER O/B FLANGE CORRODED BETWEEN BS 676 TO BS 727. REPAIRED BEAM IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,799 hrs · 67,544 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, LBL 2. REMOVED AND REPLACED SHEAR TIE PER IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 75,799 hrs · 67,544 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 500A TO BS 500B. REPAIRED WEB IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,799 hrs · 67,544 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: MOUNT BRACKET — CRACKED (R2 DOOR) · airframe 75,799 hrs · 67,544 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE MOUNT BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 75,799 hrs · 67,544 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 787 TO BS 807. REPAIRED BEAM IAW SRM, MM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,799 hrs · 67,544 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT BEAM CORRODED AT BS 772, LBL 2.5. REPAIRED BEAM IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 75,799 hrs · 67,544 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,799 hrs · 67,544 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT BEAM CORRODED AT BS 727D+6, LBL 7.5. REPAIRED BEAM IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,799 hrs · 67,544 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 75,799 hrs · 67,544 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 867 TO BS 887. REPAIRED WEB IAW DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 75,799 hrs · 67,544 cycles

DURING SCHEDULED 24Y CHECK FOUND, KEEL BEAM CORRODED BETWEEN BS 520 TO BS 540, STR 28L. REPAIRED BEAM IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,779 hrs · 67,544 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: COVER — MISSING (CABIN) · airframe 75,746 hrs · 67,502 cycles

RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT COVER MISSING AT ROW 12. SECURED COVER PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND BULKHEAD DOME WEB CRACKED AT BS 1016, STR 15R. REMOVED AND REPLACED WEB IAW EO.

Part: SIGN — LOOSE (CABIN) · airframe 75,514 hrs · 67,328 cycles

RT OVERWING EMERGENCY EXIT SIGN LENS LOOSE. SECURED SIGN IAW MM.

Part: LIGHT — BROKEN (CABIN) · airframe 74,890 hrs · 66,847 cycles

DURING SCHEDULED MV2 CHECK FOUND, FWD ENTRY LOWER EMERGENCY LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,064 hrs · 66,215 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 910, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,064 hrs · 66,215 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 504, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,063 hrs · 66,214 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 769, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,064 hrs · 66,215 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 769, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,063 hrs · 66,214 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 770, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,064 hrs · 66,215 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 792, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,063 hrs · 66,214 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 511, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,064 hrs · 66,215 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 798, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,064 hrs · 66,215 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 511, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,063 hrs · 66,214 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 910, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,063 hrs · 66,214 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 792, STR 19L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 73,100 hrs · 65,480 cycles

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

Part: SLIDE — UNWANTED DEPLOY (R2 DOOR) · airframe 72,548 hrs · 65,048 cycles

R2 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MT.

Part: COVER — LOOSE (CABIN) · airframe 72,417 hrs · 64,944 cycles

OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT COVER LOOSE AT ROW 10. SECURED COVER PER MM.

Part: SKIN — CRACKED (ELEVATOR) · airframe 72,353 hrs · 64,697 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER ELEVATOR LOWER T/E SKIN HINGE CRACKED. REPAIRED SKIN PER AWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,355 hrs · 64,898 cycles

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

Part: SKIN — CRACKED (HORIZ STAB) · airframe 72,353 hrs · 64,897 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER T/E SKIN CRACKED AT STA 116.10. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,737 hrs · 64,418 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 394, STR 5R. REPAIRED SKIN PER EA.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 71,626 hrs · 64,327 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 71,553 hrs · 64,272 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,537 hrs · 64,259 cycles

DURING SCHEDULED CV CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 71,418 hrs · 64,166 cycles

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

Part: SKIN — CRACKED (LT WING) · airframe 70,783 hrs · 63,693 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING UPPER WING SKIN CRACKED AT WBL 157. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 520, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 717, BBL 0.07. REPAIRED BEAM PER EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 360, BETWEEN STR 19R TO STR 20R. REPAIRED FRAME PER EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 706 TO BS 714, BBL 0.07. REPAIRED WEB PER EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 344, BETWEEN STR 22L TO STR 23L. REPAIRED FRAME PER EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 663 TO BS 673, LBL 24.5. REPAIRED CHORD PER EO.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND ANGLE SUPPORT CRACKED AT BS 34, STR 11L TO STR 12L. REMOVED AND REPLACED ANGLE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24.8. REPAIRED FLOORBEAM PER EO.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND EMERGENCY LIGHT BATTERY PACK INOP AT FWD GALLEY. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 706, RBL 24.5. REPAIRED FLOORBEAM PER EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 706 TO BS 711, LBL 24.5. REPAIRED FLOORBEAM PER EO.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND EMERGENCY BULLNOSE LIGHTS INOP BETWEEN ROWS 12 & 20. RECONNECTED D2964 CONNECTOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 445.5, STR 16R. REPAIRED SKIN PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND Z-ANGLE CORRODED BELOW R2 DOOR FLOOR SILL. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277.8, STR 11R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR FLOOR FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS PER MM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR FLOOR FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS PER MM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR FLOOR FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS PER MM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FLOOR FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT 12 ABC. RELAMPED PER MM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER FLANGE CORRODED AT BS 328, LBL 2. REPAIRED BEAM PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,549 hrs · 63,519 cycles

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

Part: SIGN — DAMAGED (CABIN) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT OVERWING EMERGENCY EXIT SIGN DAMAGED. REMOVED AND REPLACED SIGN PER MM.

Part: LENS — BROKEN (CABIN) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND UPPER AFT EMERGENCY EXIT LIGHT LENS BROKEN AT LT SIDE. REMOVED AND REPLACED LENS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,543 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,543 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 909, STR 21L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,543 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,543 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,549 hrs · 63,519 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 70,549 hrs · 63,519 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,853 hrs · 62,962 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,853 hrs · 62,962 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,853 hrs · 62,962 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,853 hrs · 62,962 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 69,853 hrs · 62,962 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,853 hrs · 62,962 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,853 hrs · 62,962 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,853 hrs · 62,962 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 750 S19L) · airframe 69,203 hrs · 62,469 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 750, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,203 hrs · 62,469 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 750, BETWEEN STR 18L TO STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,203 hrs · 62,469 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 760, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,203 hrs · 62,469 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 730D TO BS 740E, BETWEEN STR 18L TO STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,203 hrs · 62,469 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,104 hrs · 62,389 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,104 hrs · 62,389 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,104 hrs · 62,389 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,104 hrs · 62,389 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,782 hrs · 62,171 cycles

LOWER LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 68,245 hrs · 61,796 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 68,145 hrs · 61,717 cycles

FWD GALLEY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (LT WING) · airframe 68,025 hrs · 61,640 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING SKIN CRACKED AT FIXED L/E ABOVE SPRING DOOR. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,025 hrs · 61,640 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER FWD CUTOUT REVEAL. REPAIRED SKIN PER SRM.

Part: HINGE — BROKEN (NR 5 SPOILER) · airframe 66,762 hrs · 60,720 cycles

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

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 66,703 hrs · 60,677 cycles

L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. R&R EVAC SLIDE PER MM.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 66,173 hrs · 60,287 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING INBOARD FORE FLAP UPPER INBOARD SURFACE DELAMINATED. REPAIRED FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,174 hrs · 60,287 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 731E, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,569 hrs · 59,819 cycles

FUSELAGE SKIN CRACKED AT BS 797, STR 17L. REPAIRED SKIN PER SRM.

Part: FITTING — WORN (RT ELEVATOR TAB) · airframe 65,414 hrs · 59,710 cycles

DURING SCHEDULED CV CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REPAIRED NR 1 TAB HINGE FITTING PER SWA EA.

Part: BEARING — WORN (RT ELEVATOR) · airframe 64,544 hrs · 59,068 cycles

DURING SCHEDULED 8Y CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BEARING PER MM.

Part: BEARING — WORN (LT ELEVATOR) · airframe 64,544 hrs · 59,068 cycles

DURING SCHEDULED 8Y CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BEARING PER MM.

Part: BOLT — CORRODED (FLAP TRACK) · airframe 64,544 hrs · 59,068 cycles

DURING SCHEDULED 8Y CHECK, FOUND RT WING NR 7 FLAP TRACK BOLT CORRODED. REPAIRED FLAP TRACK PER SWA EA.

Part: FRAME — CRACKED (AFT CARGO DOOR) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND AFT CARGO DOOR FWD LOWER FRAME CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT HORIZONTAL STABILIZER LOWER T/E SKIN CRACKED AT STA 179. REMOVED AND REPLACED HORIZONTAL STABILIZER PER MM.

Part: FRAME — CRACKED (BS 500C S21L) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 21L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (BS 410) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, BL 0. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 430 S28L) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, STR 28L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD CARGO DOOR CUTOUT LOWER AFT CORNER. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CRACKED (BS 727C S14R) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 727C, STR 14R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 277 S10R) · airframe 64,498 hrs · 59,032 cycles

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

Part: STRINGER — CRACKED (BS 277 S10R) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 10R CRACKED AT BS 277. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (BS 360 S15L) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 15L CRACKED AT BS 360. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (BS 767 S14R) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 14R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (BS 380 S8R) · airframe 64,498 hrs · 59,032 cycles

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

Part: FRAME — CRACKED (BS 380 S16L) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 616 S5L) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S10L) · airframe 64,498 hrs · 59,032 cycles

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

Part: STRINGER CLIP — CRACKED (BS 520 S16R) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S6R) · airframe 64,498 hrs · 59,032 cycles

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

Part: STRINGER CLIP — CRACKED (BS 520 S15L) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 460 S16L) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 380 S6L) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 727A S8R) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 727D S8R) · airframe 64,498 hrs · 59,032 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727D S4R) · airframe 64,498 hrs · 59,032 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727A S7R) · airframe 64,498 hrs · 59,032 cycles

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

Part: STRINGER — CRACKED (BS 440 S7L) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 7L CRACKED AT BS 440. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (BS 440 S7L) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500A S8L) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,498 hrs · 59,032 cycles

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

Part: STRINGER CLIP — CRACKED (BS 500D S8L) · airframe 64,498 hrs · 59,032 cycles

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

Part: STRINGER CLIP — CRACKED (BS 500 S16L) · airframe 64,498 hrs · 59,032 cycles

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

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND NLG W/W UPPER CEILING PANEL CRACKED AT LBL 7.75. REPAIRED PANEL PER ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 16R. REPAIRED FRAME PER SWA EA.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND NLG W/W UPPER CEILING PANEL CRACKED AT RBL 7.75. REPAIRED PANEL PER ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 14L. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,498 hrs · 59,032 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,498 hrs · 59,032 cycles

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

Part: SKIN — CRACKED (BS 444 S28R) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 444, STR 28R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 451 S28L) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 451, STR 28L. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CRACKED (BS 328) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 328, LBL 28. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (BS 444 S28R) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 444, STR 28R. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 732 LBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR FWD FRAME CRACKED AT SNUBBER CUTOUT. REMOVED AND REPLACED DOOR PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 400 AND BS 420, LBL 70. REMOVED AND REPLACED WEB PER SRM.

Part: SKIN — CRACKED (BS 727D-727E) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727D AND BS 727E, STR 19R. REPAIRED SKIN PER SWA EA.

Part: BULKHEAD — CRACKED (BS 1016 S23L) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 23L. REPAIRED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 360 AND BS 380, RBL 70. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,498 hrs · 59,032 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 20R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,399 hrs · 58,956 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 14L. REPAIRED SKIN PER SWA EA.

Part: SLAT — DELAMINATED (LT WING) · airframe 64,399 hrs · 58,956 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 5 L/E SLAT DELAMINATED AT T/E. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 64,399 hrs · 58,956 cycles

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

Part: SLAT — CRACKED (RT WING) · airframe 64,322 hrs · 58,895 cycles

DURING SCHEDULED A1 CHECK, FOUND RIGHT WING NR 4 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SWA EA.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 64,246 hrs · 58,836 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 2 ABC. SECURED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,491 hrs · 58,205 cycles

DURING SCHEDULED C3 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 15 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,491 hrs · 58,205 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND BATTERY CHARGER PER MM.

Part: STRUCTURE — DELAMINATED (T/E FLAP) · airframe 62,559 hrs · 57,460 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,507 hrs · 57,420 cycles

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

Part: SKIN — CRACKED (BS 500D S16R) · airframe 61,588 hrs · 56,711 cycles

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

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 61,588 hrs · 56,711 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 DOOR FUSELAGE SKIN BEAR STRAP CRACKED AT LOWER FWD CORNER. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CRACKED (BS 350 S16L) · airframe 61,530 hrs · 56,661 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 350, STR 16L. REMOVED AND REPLACED SHEAR TIE PER EA.

Part: SHEAR TIE — CRACKED (BS 295 S10L) · airframe 61,528 hrs · 56,660 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 295, STR 10L. REMOVED AND REPLACED SHEAR TIE PER EA.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 61,528 hrs · 56,660 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER ACO.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,528 hrs · 56,660 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 450) · airframe 61,528 hrs · 56,660 cycles

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

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 61,528 hrs · 56,660 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER ACO.

Part: STRINGER CLIP — CRACKED (BS 294 S11L) · airframe 61,528 hrs · 56,660 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SWITCH — FAULTY (EMERGENCY LIGHTS) · airframe 61,528 hrs · 56,660 cycles

DURING SCHEDULED SPV CHECK, EMERGENCY EXIT LIGHTS ILLUMINATED WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED COCKPIT LIGHT SWITCH PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,528 hrs · 56,660 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 61,362 hrs · 56,537 cycles

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

Part: SKIN — CRACKED (BS 738D S19R) · airframe 61,311 hrs · 56,498 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 738D, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 61,235 hrs · 56,422 cycles

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

Part: PRESSURE PANEL — CRACKED (BS 295) · airframe 61,127 hrs · 56,320 cycles

DURING SCHEDULED A1 CHECK, FOUND NLG WW PRESSURE PANEL CRACKED AT RIGHT BS 259.5, WL 174. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 505C S15R) · airframe 61,127 hrs · 56,320 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505C, STR 15R. REPAIRED SKIN PER SWA EA.

Part: LENS — MISSING (CABIN) · airframe 60,842 hrs · 56,089 cycles

BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 1 DEF. INSTALLED LIGHT LENS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,785 hrs · 56,039 cycles

DURING SCHEDULED C4 CHECK, FOUND SIDEWALL EMERGENCY EXIT LIGHT INOP AT R2 DOOR. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,785 hrs · 56,039 cycles

DURING SCHEDULED C4 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT 16 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 970 S21L) · airframe 60,785 hrs · 56,039 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 21L. REPAIRED SKIN PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,477 hrs · 55,192 cycles

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

Part: GLOWSTRIP — WORN (CABIN) · airframe 59,897 hrs · 55,355 cycles

DURING SCHEDULED SERVICE CHECK, FOUND MID CABIN EEPLS PHOTOLUMINESCENT STRIP WORN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 59,891 hrs · 55,349 cycles

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

Part: SKIN — CRACKED (BS 947) · airframe 58,046 hrs · 53,885 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 24R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,046 hrs · 53,885 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BULLNOSE EMERGENCY LIGHT INOP AT ROW 4 DEF. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (BS 927) · airframe 58,046 hrs · 53,885 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 24L. REPAIRED SKIN PER SWA EA AND SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,253 hrs · 53,264 cycles

DURING SCHEDULED A1 CHECK, FOUND RIGHT AFT EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,081 hrs · 53,144 cycles

DURING SCHEDULED A2 CHECK, FOUND RT AFT CABIN BULLNOSE EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF LIMITS (L2 DOOR) · airframe 57,081 hrs · 53,144 cycles

DURING SCHEDULED A2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,081 hrs · 53,144 cycles

DURING SCHEDULED A2 CHECK, FOUND R1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 57,059 hrs · 53,126 cycles

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

Part: SKIN — CRACKED (RT WING SLAT) · airframe 56,910 hrs · 53,002 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT T/E LOWER SKIN CRACKED. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 56,910 hrs · 53,002 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: FITTING — CRACKED (LT WING) · airframe 56,332 hrs · 52,561 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT WING MLG HYDRAULIC ACTUATOR ATTACH FITTING CRACKED AT WS 134.5. REMOVED AND REPLACED FITTING PER SRM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 56,332 hrs · 52,561 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT NR 2 & NR 3 STOP FITTING CUTOUTS. REMOVED AND REPLACED DOOR PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 56,332 hrs · 52,561 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 665.5, RBL 39.5. REPAIRED WEB PER SRM.

Part: SHIM — CRACKED (FUSELAGE) · airframe 56,332 hrs · 52,561 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN SHIM CRACKED AT BS 314, STR 17R. REMOVED AND REPLACED SHIM PER SWA EA.

Part: RIB — CRACKED (LT WING) · airframe 56,332 hrs · 52,561 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT WING RIB CHORD CRACKED AT WBL 135.5, FWD OF AFT SPAR. REPAIRED RIB PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,332 hrs · 52,561 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM T-CHORD CRACKED AT BS 660.5, BL 0. REPAIRED FLOORBEAM PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,332 hrs · 52,561 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,332 hrs · 52,561 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 297, STR 17R. REPAIRED SKIN PER SWA EA.

Part: FLOOR SUPPORT — CRACKED (FUSLEAGE) · airframe 56,332 hrs · 52,561 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 EA CRACKS AT NR 2 LONGITUDINAL FLOOR SUPPORT TEE, BS 664 & BS 668.5. REPAIRED FLOOR SUPPORT PER SWA EA.

Part: SKIN — CRACKED (L1 DOOR) · airframe 56,332 hrs · 52,561 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FLOOR SUPPORT — CRACKED (CABIN FLOOR) · airframe 56,332 hrs · 52,561 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 3 EA CRACKS AT NR 3 LONGITUDINAL FLOOR SUPPORT TEE, BS 662.5, BS 665.5 & BS 669. REPAIRED FLOOR FLOOR SUPPORT PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,273 hrs · 52,517 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 2, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,273 hrs · 52,517 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 20R. REPAIRED SKIN PER SWA EA.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 55,386 hrs · 51,839 cycles

EMERGENCY EXIT PHOTOLUMINESCENT STRIP AT ROW 8 ABC, LOOSE. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 54,994 hrs · 51,536 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD EPPLS PHOTOLUMINESCENT STRIPS WORN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIPS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,994 hrs · 51,536 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 540, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,243 hrs · 50,076 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 328, STRINGER 28R, CRACKED. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,243 hrs · 50,076 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 53,236 hrs · 50,068 cycles

DURING SCHEDULED C4 CHECK, FOUND RT NR 4 L/E SLAT INBOARD END DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 53,236 hrs · 50,068 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,236 hrs · 50,068 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR FRAME UPPER HINGE CUTOUT LOWER RADIUS, CRACKED. REPAIRED DOOR FRAME CUTOUT LOWER RADIUS PER EA.

Part: LENS — CRACKED (CABIN) · airframe 52,286 hrs · 49,325 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: CABLE — MISROUTED (R2 DOOR) · airframe 52,286 hrs · 49,325 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED SLIDE CABLE PER MM.

Part: HOOK — LOOSE (L2 DOOR) · airframe 52,286 hrs · 49,325 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE HOOK LOOSE. REMOVED AND REPLACED FASTENERS SECURING SLIDE CONTAINER PER MM.

Part: SPRING — WORN (AILERON FEEL) · airframe 50,959 hrs · 48,281 cycles

AILERONS SLUGGISH WHEN TURNING FROM EITHER DIRECTION. REMOVED AND REPLACED AILERON FEEL AND CENTERING MECHANISM SPRINGS PER MM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 50,819 hrs · 48,163 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICES CRACKED (3 EA) BS 360 AT STR 4L, BS 360 AT STR 10L AND BS 908 AT STR 4R. REMOVED AND REPLACED STRINGER SPLICES PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,819 hrs · 48,163 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CRACKED (2 EA) STR 11R, BS'S 385 AND 425. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,819 hrs · 48,163 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND WINDOW CUTOUT FWD UPPER CORNER CRACKED AT RT WINDOW NR 11. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,810 hrs · 48,163 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED AT BS 1011, STRINGER 7L. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,328 hrs · 47,758 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 10L, BS 500C AND BS 500D. REPAIRED SKIN PER SRM.

Part: DUCT — LOOSE (NR 2 ENGINE) · airframe 50,079 hrs · 47,565 cycles

DUAL AIR TURNBACK, NR 2 ENG OVERHEAT LIGHT ILLUMINATED WITH THROTTLE LEVER ADVANCEMENT. FOUND NR 2 ENG 9TH STG PNEUMATIC BLEED AIR DUCT MANIFOLD LOOSE. TIGHTENED DUCT MANIFOLD BOLTS PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 49,672 hrs · 47,226 cycles

FWD CABIN INBD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT AND BATTERY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,454 hrs · 47,037 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 48,437 hrs · 46,222 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LEFT WING OTBD AFT FLAP DELAMINATED ON LOWER SURFACE. REPAIRED LEFT OTBD AFT FLAP PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 48,437 hrs · 46,222 cycles

DURING SCHEDULED 1/2D CHECK, FOUND KEEL BEAM CORRODED AT BS 541, STR 28R. REMOVED AND REPLACED SECTION OF KEEL BEAM PER SRM AND SWA EA.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 48,386 hrs · 46,180 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: CAP — LOOSE (CABIN) · airframe 48,103 hrs · 45,957 cycles

EEPLS END CAP LOOSE AT FWD END. SECURED END CAP PER MM.

Part: SWITCH — FAILED (L/E FLAP) · airframe 48,010 hrs · 45,880 cycles

AIR TURNBACK, AFTER TAKEOFF WITH FLAPS SELECTED UP, L/E FLAP TRANSIT LIGHT REMAINED ILLUMINATED AND NR 2 L/E FULL EXTEND LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED NR 2 KRUEGER FLAP EXTEND SWITCH PER MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 47,760 hrs · 45,666 cycles

DURING SCHEDULED SERVICE CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 663.5, RBL 6.15. REPAIRED STIFFENER PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,470 hrs · 45,413 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 520, WL 255, RT. REPAIRED SKIN PER SRM.

Part: BRACKET — LOOSE (FWD CABIN DOORS) · airframe 46,667 hrs · 44,750 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH BRACKET FASTENERS LOOSE. REMOVED AND REPLACED BRACKET FASTENERS PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 46,650 hrs · 44,763 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED (2 EA) AT BS 179, WL 227, RBL 17.1 AND LBL 17.1. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (NLG W/W) · airframe 46,650 hrs · 44,736 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND NLG W/W SKIN CRACKED AT LT FWD OF NLG DOOR BELL CRANK. REPAIRED SKIN PER SWA RA.

Part: CHECK VALVE — FAILED (E/E BAY) · airframe 46,646 hrs · 44,734 cycles

AIR TURNBACK, NO PRESSURIZATION AFTER TAKEOFF, CONFIGURED FOR SINGLE PACK OPS. REMOVED AND REPLACED AFT CARGO DOOR SEAL AND REMOVED AND REPLACED EQUIP COOLING PRESSURIZATION CHECK VALVE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 46,501 hrs · 44,610 cycles

EEPLS LOOSE. SECURED EEPLS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 44,795 hrs · 43,217 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER BROKEN AT ROW 3 & COVER MISSING AT ROW 17. REPLACED COVERS PER MM.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 44,165 hrs · 42,671 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT PER MM.

Part: BEAM — CRACKED (NLG WW) · airframe 42,222 hrs · 41,054 cycles

DURING SCHEDULED SERVICE CHECK, FOUND .9 CRACK IN NOSE WHEEL WELL EXTENDING FROM UPPER ROW FASTENERS OF CENTER BEAM WEB. REPAIRED NLG W/W WEB PER SRM.

Part: LENS — MISSING (CABIN) · airframe 41,120 hrs · 40,112 cycles

FWD ENTRY EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 40,535 hrs · 39,602 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 11.5 AND LBL 10.5. REPAIRED BULKHEAD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 40,535 hrs · 39,602 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 11.5, WL 234. REPAIRED BULKHEAD PER SRM.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 40,535 hrs · 39,602 cycles

DURING SCHEDULED 1/2 D CHECK, FOUND AFT CARGO BAY LONGITUDINAL FLOOR SUPPORTS CORRODED AROUND SCREW HOLES, BS 767-792 AND BS 807-827, RBL 7. REPAIRED BEAMS PER SWA RA NR 1-A53-2021.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 40,535 hrs · 39,602 cycles

DURING SCHEDULED 1/2 D CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN HAS A CRACK .75 LONG AT REAR SPAR. REPAIRED SKIN PER SRM.

Part: FRAME — BROKEN (FUSELAGE) · airframe 40,535 hrs · 39,602 cycles

DURING SCHEDULED 1/2 D CHECK, FOUND BS 178 BULKHEAD T-CHORD BROKEN, LBL 26, WL 207. REPAIRED CHORD PER SRM.

Part: COVER — MISSING (CABIN) · airframe 40,535 hrs · 39,602 cycles

DURING SCHEDULED 1/4 D CHECK, FOUND EEPLS TRACK COVERS MISSING AND CRACKED THROUGH OUT CABIN FLOOR. R & R TRACK COVERS AND INSTALLED MISSING ONES PER MM.

Part: SKIN — CRACKED (BS 947)

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 947, STRINGER 25L. REPAIRED SKIN PER SRM.

Part: REGULATOR — INOPERATIVE (NR 1 ENGINE)

DIVERSION, NR 1 ENG PNEU BLEED VALVE INOP AFTER TAKEOFF. DURING CRUISE PRESS INDICATED 10 PSI, NR 2 ENG INDICATED 42 PSI. DIVERTED TO DAL. REMOVED AND REPLACED NR 1 ENH PNEU BLEED PRESS REGULATOR PER MM.

Part: LIGHT ASSY — LOOSE (CABIN FLOOR)

EEPLS COVER LOOSE AND INOP IN AFT SECTION. SECURED LOOSE COVER AND LIGHT ASSY. OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED RON, FOUND AFT EMERGENCY EXIT LIGHT INOP. REPAIRED BROKEN WIRE AT PIN CONNECTOR D2966 PER MM.

Part: LIGHT — BROKEN (CABIN)

FWD OUTBOARD EMERGENCY FLASHLIGHT PLASTIC STRAP BROKEN. REMOVED AND REPLACED PLASTIC STRAP PER MM.

Part: STRAP — CRACKED (NR 2 PYLON)

DURING SCHEDULED SERVICE CHECK, FOUND A 2.5 INCH LONG CRACK ON NR 2 PYLON STRAP UNDER THE FRAME, NAC STA 236 RT. REMOVED AND REPLACED STRAP PER SRM.

Part: BULB — FAILED (RT EMER EXIT)

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND EMERGENCY RT OVERWING LIGHT INOP. RELAMPED LIGHT ASSY PER MM.

Part: BATTERY CHARGER — INOPERATIVE (ROW 3 & 5)

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND EMERGENCY LIGHTING BY SEATS 3 AND 5 INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: LIGHT — INOPERATIVE (ROW 3 & 5)

DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT INOP AT ROWS 3 AND 5. RELAMPED PER MM.

Part: BATTERY CHARGER — INOPERATIVE (RT EMER EXIT)

DURING SCHEDULED 1/4D CHECK, FOUND RT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY CHARGER PER MM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED SC CHECK, FOUND EMERGENCY LIGHT AT ROW 22 LEFT SIDE INOP. REMOVED AND REPLACED LAMP PER MM.

Part: CHARGER — INOP (CABIN)

DURING SCHEDULED SC CHECK, FOUND FWD SECTION TRACK LIGHTS INOP. REMOVED AND REPLACED FWD CHARGER PER MM, OPS CHECK GOOD.

Part: SKIN — CRACKED (NR 6 LE SLAT)

DURING SCHEDULED BC1 CHECK, FOUND A .125 INCH CRACK IN NR 6 SLAT LOWER T/E SKIN 18 INCHES FROM ACTUATOR. REPAIRED PER SWA RA 1-357-0634.

Part: SKIN — DENTED (BS 907)

DURING SCHEDULED C4 CHECK, FOUND DENTED FUSELAGE SKIN FWD OF BS 907 AND O/B OF STR 27L. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (CARGO COMPT)

DURING SCHEDULED C4 CHECK, FOUND FWD CARGO UPLATCH INTERCOSTAL CRACKED. REMOVED AND REPLACED PER BOEING SRM.

Part: SENSOR — MALFUNCTIONED (NR 4 LE FLAP)

AFTER TAKEOFF WITH FLAP LEVER UP, HAD LE FLAPS TRANSIT LIGHT AND AN OVERHEAD INDICATIONS OF NR 4 KRUEGER FLAP EXTENDED. AIRCARAFT RETURN TO BHM AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED PROX SENSOR FOR NR 4 KRUEGER DOWN INDICATION PER BOEING MM. SYSTEM CHECKED OK, OPS NORMAL.

Part: FITTING — CRACKED (BS 867)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT FITTING AT BS 867, STR 8L AND 9L. REPAIRED PER TRAMCO EWO 98-0042.

Part: STRINGER — CRACKED (BS 907)

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER SPLICE AT BS 907, STR 4L. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (NR 1 PYLON)

DURING SCHEDULED D-CHECK, FOUND NR 1 PYLON AFT LOWER L STIFFENER CRACKED. REPAIRED PER BOEING SRM.

Part: SUPPORT — CRACKED (LT PYLON)

DURING SCHEDULED D-CHECK, FOUND L/W PYLON I/B T/E SUPPORT LONGERON UNDER SPRING DOOR ASSY IS CRACKED. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (NR 1 PYLON)

DURING SCHEDULED D-CHECK, FOUND NR 1 PYLON UPPER AFT I/B L-CLIP CRACKED. REPAIRED PER BOEING SRM.

Part: CLIP — CRACKED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 787 STR 22L, BS 787 STR 23L, BS 767 STR 23 LT, BS 747 STR 22L. REPAIRED PER BOEING SRM.

Part: FRAME — CORRODED (BS 747/787/827)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT FITTING AT BS 747 STR 8-9R, BS 787 STR 8-9R, BS 827 STR 8-9L, BS 827 STR 8-9R, BS 867 STR 8-9R, BS 747 STR 8-9L. REPAIRED PER TRAMCO 98-0042.

Part: BULKHEAD — CORRODED (BS 500D)

DURING SCHEDULED D-CHECK, FOUND CORROSION AT BS 500D STR 26L TO 26R LOWER CENTER BULKHEAD SUPPORT ANGLE. REPAIRED PER BOEING SRM.

Part: SKIN — DAMAGED (BS 785)

DURING SCHEDULED D-CHECK, FOUND SKIN DAMAGE AT BS 785, WL 214, RBL 71, BELOW STR 16R. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 500)

DURING SCHEDULED D-CHECK, FOUND IS CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 500A, STR 8 TO 9 RT. REPAIRED PER BOEING PER SRM.

Part: FRAME — CRACKED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 520 STR 8-9 RT, BS 500C STR 8-9 RT, BS 440 STR 8-9 LT, BS 400 STR 8-9 RT. REPAIRED PER TRAMCO EWO 98-0042.

Part: DOUBLER — CRACKED (BS 1139)

DURING SCHEDULED D-CHECK, FOUND AT BS 1139 WL 262.5, LBL 35 FWD SIDE OF THE DOUBLER CRACKED. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 400)

DURING SCHEDULED D-CHECK, FOUND FRAME IS CRACKED AT BS 400 BETWEEN STR 8 TO 9 LT. REPAIRED PER TRAMCO EWO 98-0042.

Part: BULKHEAD SHROUD — DAMAGED (BS 727)

DURING SCHEDULED D-CHECK, FOUND AT BS 727 BULKHEAD CEILING TO BULKHEAD APU DUCT SHROUD DAMAGED. REPAIRED PER BOEING MM.

Part: SUPPORT — CORRODED (BS 860)

DURING SCHEDULED D-CHECK, FOUND CORROSION AT BS 860, RBL 3, WL 154 ON FLOOR SUPPORT. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 907)

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER SPLICE AT BS 907 STR 24R. REPAIRED PER BOEING SRM.

Part: FRAME — CORRODED (BS 616)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 616, LBL 63, WL 200. REPAIRED PER SWA T1-A53-026.

Part: FRAME — CRACKED (BS 787)

DURING SCHEDULED D-CHECK, FOUND CRACKED AT HAT FITTING AT BS 787, STR 8L AND 9L. REPAIRED PER TRAMCO EWO 98-0042.

Part: LIGHT — BROKEN (CABIN)

DURING SCHEDULED D-CHECK, FOUND EMERGENCY EXIT OVERHEAD TRACT LIGHT AT ROW 7 ABC, BROKEN OFF AT LIGHT HOUSING. REMOVED AND REPLACED PER BOEING MM.

Part: SKIN — DENTED (BS 969)

DURING SCHEDULED D-CHECK, FOUND SKIN DENTED AND GOUGED AT BS 969, WL 188, LBL 64. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 440/500)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 440, STR 8-9 RT, BS 500A STR 8-9 RT. REPAIRED PER TRAMCO EWO 98-0042.

Part: SUPPORT — CORRODED (BS 435-400)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOOR/SIDEWALL SUPPORT AT BS 435 TO 400, RBL 24, WL 158.5. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 727)

DURING SCHEDULED D-CHECK, FOUND CRACKED AT HAT FITTING AT BS 727B, STR 8R AND 9R. REPAIRED PER TRAMCO EWO 98-0042.

Part: ANGLE — CRACKED (RT PYLON)

DURING SCHEDULED D-CHECK, FOUND R/W PYLON L-ANGLE STIFFENER CRACKED AT I/B SIDE. REMOVED AND REPLACED PER BOEING SRM.

Part: STRAP — CRACKED (BS 1139)

DURING SCHEDULED D-CHECK, FOUND LOWER SPLICE STRAP AT BS 1139, WL 258, LBL 40 WAS CRACKED PASSED LIGHTENING HOLE ABOUT 1.5 INCH FROM EDGE. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CORRODED (WINGS)

DURING SCHEDULED D-CHECK, FOUND BOOST PUMP CUTOUT UPPER SURFACE OF LOWER SKIN HAS CORROSION DAMAGE. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 727)

DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 727D+5 RBL 3 WL 152. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 1104)

DURING SCHEDULED D-CHECK, FOUND CRACK IN FRAME AT BS 1104, RBL 10, 1 INCH O/B OF STRINGER 2R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 907)

DURING SCHEDULED D-CHECK, FOUND UPON REMOVAL OF SIDE SKIN AT BS 907, CIRCUMFERENTIAL STRAP TO BE CRACKED AT 220R. REMOVED AND REPLACED PER BOEING SRM.

Part: DOOR — DENTED (BS 1121)

DURING SCHEDULED D-CHECK, FOUND APU DOOR OUTER SKIN DENTED AT BS 1121 WL 224 RBL 10. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (DOOR)

DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOORWAY UPPER HINGE CUTOUT FED UPPER CORNER HAS 3 INCH CRACK. REPAIRED PER BOEING SRM.

Part: WEB — CRACKED (BS 179)

DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 179, WL 208, RBL 28. REMOVED AND REPLACED PER BOEING SRM.

Part: KEEL BEAM — DAMAGED (BS 706-727)

DURING SCHEDULED D-CHECK, FOUND SEVEN WORKING FASTENERS IN KEEL BEAM LOWER FLANGE UPPER SURFACE AT BS 706 TO 727, RBL 7. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 863)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN IS GOUGED AT BS 863, STR 1. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 380)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, S24R. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED SEVERAL PLACES. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SERVICE CHECK, FOUND AFT EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: COFFEEMAKER — INOPERATIVE (FWD GALLEY)

EN ROUTE, F/A NOTED ELECTRICAL BURNING SMELL IN FWD GALLEY. INSPECTED, REPLACED COFFEEMAKER AND RAIL ASSEMBLY PER BOEING M/M.

Part: SKIN — GOUGED (BS 341/347)

DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 341 AND 347, S17L. REPAIRED BOTH PER SWA RA 1-353-1515.

Part: SKIN — OIL CANNING (BS 500)

DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN OIL CANNING AT BS 500 , S17L AND BS 500A, AT S22L. REPAIRED BOTH PER SWA RA 1-353-1515.