N64SW

Part: INDICATOR — MOVED (PAX DOOR)

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (BS 747 & 767)

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED BS 747 AND 767, STRINGER 16R. REPAIRED SKIN PER SRM.

Part: COFFEEMAKER — FAILED (GALLEY)

BURNING ELECTRICAL SMELL IN AFT GALLEY. SMELL COMING FROM UPPER COFFEE MAKER HEATING BLANKET WHICH HAD RESIDUAL MOISTURE. REMOVED MOISTURE FROM HEATING BLANKET. OPS CK GOOD.

Part: BATTERY — DISCHARGED (E & E COMP)

DURING SCHEDULED C2 CHECK, FOUND OVERHEAD EMERGENCY LIGHTS INOP. REMOVED AND REPLACED AIRCRAFT BATTERY PER MM.

Part: CONTROL CABLE — FRAYED (RT TE FLAP)

DURING SCHEDULED D-CHECK, FLAP EXTENSION CHECKS, ON FUNCTIONAL FLT CK RT FLAP CABLES BROKE. REMOVED DAMAGED CABLES AND REPLACED WITH NEW ONES. REPAIRED ALL HIDDEN DAMAGE ON RT I/B MIDFLAP PER OHM 57-53-22. OPERATIONAL TESTED OK PER MM 57-53-22.

Part: BATTERY — DISCHARGED (EMER EXIT)

DURING SCHEDULED D-CHECK, FOUND EXTERIOR EMERGENCY OVERWING LIGHT AT BS 773R INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING MM.

Part: CHANNEL — CRACKED (BS 360)

DURING SCHEDULED D-CHECK, FOUND STRINGER CHANNEL CRACKED AT BS 360, S14L. INSTALLED NEW CHANNEL PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 294)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294, LBL 11. REMOVED AND REPLACED UPPER CHORD FLOORBEAM PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 218, RBL 8.7 UNDER STRAPS. FABRICATED AND INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: STRAP — CRACK (BS 1028)

DURING SCHEDULED D-CHECK, FOUND CRACK IN CIRCUMFERENTIAL TEAR STRAP AT BS 1028, RBL 30 AND 34. FABRICATED AND INSTALLED STRAP PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT WL 234, LBL 9. FABRICATED AND INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: WEB — CORRODED (BS 1002)

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB BODY CORRODED AT BS 1002, WL 208, RBL 49. INSTALLED NEW WEB PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 344, LBL 27.5, 41.5, 46, AND 54. FABRICATED AND INSTALLED NEW UPPER CHORD AND SPLICE ANGLES PER BOEING SRM.

Part: BULKHEAAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 218, LBL 7.7 UNDER STRAPS AND STIFFENERS. FABRICATED AND INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: COFFEEMAKER — INOPERATIVE (AFT GALLEY)

IN FLIGHT NOTED AN ELECTRICAL TYPE SMELL AT AFT GALLEY AREA. DISCONNECTED POWER TO COFFEEMAKERS. REPLACED AFT LOWER COFFEEMAKER PER BOEING M/M.

Part: SLIDE — LOW PRESS (SERVICE DOOR)

DURING SERVICE CHECK, FOUND FWD SERVICE DOOR SLIDE PRESSURE LOW. REPLACED PER BOEING M/M.

Part: SKIN — CRACKED (FUSELAGE)

DURING WALKAROUND CHECK, FOUND A FUSELAGE SKIN CRACK ABOVE WING/BODY FAIRING \N\NREPAIRED PER BOEING SRM

Part: LINE — RUPTURED (RT MLG ACTUATOR)

RETURNED TO SDF DUE TO LOSS OF A SYSTEM HYDRAULIC FLUID. INSPECTED AND FOUND RT MAIN GEAR ACTUATOR LINE RUPTURED. REMOVED AND REPLACED LINE PER BOEING M/M.

Part: SKIN — CRACKED (FUSELAGE)

DURING WALKAROUND CHECK, FOUND A SKIN CRACK AT UPPER AFT SECTION OF FUSELAGE UNDER PREVIOUS REPAIR. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED C3 CHECK, FOUND A 2 INCH FUSELAGE SKIN CRACK AT BS 727A AT S17R. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHTING INOPERATIVE OVER AFT LEFT AND RIGHT EXIT DOORS. REPLACED BATTERY PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND EMERGENCY EXIT LIGHT ASSEMBLY ABOVE FWD SERVICE DOOR INOP. REPLACED PER BOEING M/M.

Part: FRAME — CRACKED (BS 298)

DURING SCHEDULED D-CHECK, FOUND BS 298 FWD GALLEY DOORWAY FWD CUTOUT FRAME CRACKED AT WL 260. REPLACED DAMAGED SECTION PER BOEING SRM.

Part: FRAME — CRACKED (BS 291.5)

DURING SCHEDULED D-CHECK, FOUND BS 291.5 FRAME WEB CRACKED AT WL 235 AND WL 241. REPAIRED PER BOEING SRM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED TERMINAL CHECK, RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT AT AFT ENTRY DOOR INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND EMERGENCY TRACK LIGHTING INOPERATIVE AT MID CABIN AREA. RELAMPED PER BOEING M/M.

Part: SWITCH — FAILED (NR 6 LE SLAT)

RETURNED DUE TO NR 6 L/E SLAT TRANSIT LIGHT INDICATION AND REQUIRED 1.5 TO 2.5 OF RT RUDDER TRIM TO FLY LEVEL. REPLACED NR 6 SLAT ROD END SWITCH AND CHECKED RIGGING PER BOEING M/M.

Part: START VALVE — MALFUNCTIONED (NR 1)

EN ROUTE, NUMBER 1 ENGINE START VALVE LIGHT ILLUMINATED. PERFORMED ENGINE SHUTDOWN AS PRECAUTIONARY. LANDED WITHOUT INCIDENT AT HOU. REPLACED ENGINE START PRESSURE SWITCH, START VALVE AND OPERATION CHECKED PER BOEING M/M.

Part: BATTERY PACK — DISCHARGED (FWD ENTRY)

DURING SCHEDULED TERMINAL CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.