N86SW

Part: CABLE — OUT OF POSITION (ESCAPE SLIDE)

DURING SCHEDULED C1 CHECK, FOUND FWD SERVICE DOOR SLIDE PACK CABLE ROUTED INCORRECTLY. REROUTED CABLE PER MM.

Part: BATTERY PACK — DISCHARGED (RT EMER EXIT)

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHTS (INNER AND OUTER) INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — LOOSE (SERVICE DOOR)

PLASTIC SHROUD AROUND ESCAPE SLIDE ON FWD SERVICE DOOR WAS LOOSE AT THE BOTTOM AND SLIDE FELL OUT. REPACKED SLIDE PER SWA WORK CARD.

Part: VALVE — INOPERATIVE (LANDING GEAR)

DIVERTED TO HOU DUE TO ANTI-SKID INOP GEAR DOWN. COULD NOT GO TO AUS DUE TO WET RUNWAYS. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED PARKING BRAKE VALVE, NO LEAKS OPS CHECKED GOOD PER BOEING MM. REMOVED AND REPLACED EXIT SIGN, OPS CHECKED PER BOEING MM.

Part: MODULE — INOPERATIVE (COCKPIT)

DURING SCHEDULED C1 CHECK, FOUND COCKPIT EMERGENCY LIGHTING INOP. REMOVED AND REPLACED M560 MODULE PER BOEING M/M.

Part: FRAME — CRACKED (BS 639)

DURING SCHEDULED SERVICE CHECK, FOUND FRAME CRACKED .5 INCH AT BS 639 FLOOR LEVEL, RT BELTFRAME. REPLACED FRAME PER BOEING SRM.

Part: DOOR FRAME — CRACKED (FWD SERVICE)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR LOWER FWD DOORWAY STUB FRAME CRACKED 1.5 INCH VERTICALLY AND .5 INCH HORIZONTALLY PROTRUDING FROM LOWER LATCH ROLLER CAMPLATE ASSY. REPLACED FRAME PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND ALL ENTRY SERVICE DOOR EMERGENCY EXIT LIGHT BATTERY PACKS WEAK. REPLACED BATTERY PACKS PER BOEING M/M.

Part: WEB — CORRODED (BS 492/490)

DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR SEAL WEB CORRODED AT BS 492 AND 490, WL 166, RBL 32. REPLACED WEB PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT WL 218, LBL 7 TO 10. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 504)

DURING SCHEDULED D-CHECK, FOUND FWD CARGO BAY FLOOR SUPPORT CORRODED AT BS 504, FROM S25L TO 26R. REPAIRED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 947)

DURING SCHEDULED D-CHECK, FOUND STRINGER 25R AT BS 947 CORRODED. REPLACED CORRODED SECTION PER BOEING SRM.

Part: CLIP — CRACKED (BS 727)

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727B, S18R AND S20R. REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 727)

DURING SCHEDULED D CHECK, FOUND BULKHEAD SUPPORT ANGLE CRACKED AT BS 727+8, WL 156 BL ZERO-LBL 5. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BULKHEAD BS 178 CRACKED AT WL 218, RBL 7 TO 12, AND AT RBL 9.5 TO 12. REPAIRED PER BOEING SRM.

Part: FLOOR BEAM — CORRODED (BS 344)

DURING SCHEDULED D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 344, LBL 7 TO 10, AND AT RBL 2 TO 31. REPAIRED PER BOEING SRM.

Part: SPLICE — CORRODED (BS 907)

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907+5. REPAIRED PER BOEING SRM AND BOEING T1-A51-004.

Part: CHORD — CORRODED (BS 986.6-1006)

DURING SCHEDULED D CHECK, FOUND FLOORBEAM ANGLED CHORD CORRODED AROUND FASTENER HOLES BETWEEN BS 1006 AND 986.5, WL 208, LBL 10 TO 19. REPAIRED PER BOEING SRM.

Part: FLOOR BEAM — CORRODED (BS 1006-1016)

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CHORD CORRODED AROUND FASTENER HOLES BETWEEN BS 1006 AND 1016, WL 208, UNDER WEB. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (FUSELAGE)

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT THE FOLLOWING LOCATIONS: BS 823, AT S26L, BS 341 AT S25R, BS 504, BETWEEN 21R AND 22R, BS 203, 4 INCHES ABOVE S23L, BS 947, AT S19L AND AT BS 891, S25R. REPAIRED ALL PER BOEING SRM.

Part: SKIN — DENTED (BS 370/936/980)

DURING SCHEDULED HD CHECK, FOUND FUSELAGE SKIN DENTED AT BS 370, S25L, AT BS 980, S22L AND AT BS 936 AT S19L. REPAIRED ALL PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 469)

DURING SCHEDULED SERVICE CHECK, FOUND INTERCOSTAL CRACKED AT FWD CARGO THRESHOLD AT BS 469. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 720)

DURING SCHEDULED SERVICE CHECK, FOUND 3 SKIN CRACK ALONG S25L AT BS 720. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED JUST ABOVE POTABLE WATER SERVICE PANEL AT S25L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: EEL — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSEMBLY PER BOEING MM.