N744AS

Part: BATTERY PACK — DISCHARGED (ROW 11)

ANC - FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 11. REPLACED REMOTE ASSEMBLY RECEIVER P/N 88-3-2003-1-2, AND BATTERY PACK, THEN LIGHTS OPERATED NORMAL. (M)

Part: RECEIVER — INOPERATIVE (AFT CABIN)

EMERGENCY FLOOR TRACK LIGHTS ILLUMINATED MOMENTARILY AFTER LANDING. REPLACED AFT CABIN REMOTE ASSEMBLY RECEIVER, THEN LIGHTS OPERATED NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

AFTER RECON, FOUND AFT TWO PALLETS EMERGENCY FLOOR TRACK LIGHTS BLINKING. REMOVED AND REPLACED BATTERY PACKS, THEN LIGHTS OPERATED NORMAL. (M)

Part: CONTROL MODULE — INOPERATIVE (EMERGENCY LIGHT)

AFTER RECON FOUND EMERGENCY FLOOR TRACK LIGHTS BLINKING. REMOVED AND REPLACED MID AND AFT CABIN CONTROL MODULES, THEN LIGHTS OPERATED NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

AFTER RECONFIGURATION, FOUND FLOOR TRACK LIGHTS ON SEAT PALLET 8-13 WOULD NOT EXTINGUISH. REMOVED AND REPLACED BATTERY PACK, THEN LIGHTS OPERATED NORMAL. (M)

Part: RETAINER — CRACKED (NR 1 NACELLE)

DURING C-CHECK, FOUND NR 1 ENGINE SEAL RETAINER AT NACELLE STATION 173 CRACKED. REMOVED AND REPLACED RETAINER IAW SRM. (M)

Part: FITTING — CORRODED (FS)

PAE - DURING C-CHECK, FOUND LT UPLOCK SUPPORT FITTING AT BS 685, LT BUTTOCK LINE 70 CORRODED. REMOVED AND REPLACED SUPPORT FITTING IAW MFG DWG. (M)

Part: FAIRING — DENTED (THRUST REVERSER)

DURING C-CHECK, FOUND NR 1 ENGINE THRUST REVERSER FAIRING AT NACELLE STATION 185 DENTED. REMOVED AND REPLACED FAIRING IAW SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FLOORBEAM AT BS 540-727B, LT BUTTOCK LINE 45 CORRODED. REMOVED DAMAGE AND REPAIRED IAW EA. (M)

Part: RIB — GOUGED (NR 2 NACELLE)

DURING C-CHECK, FOUND NR 2 ENGINE COWL RIB REPAIR AT NACELLE STATION 139.04 GOUGED. REMOVED PREVIOUS REPAIR AND INSTALLED DOUBLER IAW SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FLOORBEAM AT BS 986.5, LEFT BUTTOCK LINE 17, RIGHT BUTTOCK LINE 43 CORRODED. REMOVED AND REPLACED FLOORBEAM PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND FLOORBEAM AT BS 1016, LT BUTTOCK LINE 8, LEFT BUTTOCK LINE 13 CORRODED. REMOVED AND REPLACED FLOORBEAM PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND FLOORBEAM AT BODY STATION 540-616, RIGHT BUTTOCK LINE 45 CORRODED. REMOVED CORROSION AND REPAIRED FLOORBEAM PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FLOORBEAM AT BS 663-706, RIGHT BUTTOCK LINE 25 CORRODED. REMOVED CORROSION AND REPAIRED FLOORBEAM PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FLOORBEAM AT BS 663-727, LT BUTTOCK ONE 25 CORRODED. REMOVED AND REPLACED FLOORBEAM IAW SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 727B-947, RIGHT BUTTOCK LINE 25 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M)

Part: FITTING — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND NOSE LANDING GEAR ATTACH FITTING AT BODY STATION 294.5, LT BUTTOCK LINE 3, RT BUTTOCK LINE 3 CORRODED. REMOVED AND REPLACED FITTING IAW SRM. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND STRINGER TIE AT BS 907, STRINGER 19L CORRODED. REMOVED AND REPLACED STRINGER TIE IAW SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND SEAT TRACK AT BS 663-727A, LT BUTTOCK LINE 25 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING C-CHECK, FOUND FRAME AT BS 907, STRINGER 18L-19L CRACKED. REMOVED AND REPLACED FRAME IAW SRM. (M)

Part: ANGLE — CRACKED (FUSELAGE)

PAE - DURING C-CHECK, FOUND MAIN CARGO DOOR ANGLE AT BS 480, LT BUTTOCK LINE 36 CRACKED. REMOVED AND REPLACED ANGLE IAW SRM. (M)

Part: WEB — CRACKED (DOOR FRAME)

PAE - DURING C-CHECK, FOUND MAIN CARGO DOOR WEB AT BS 480, LT BUTTOCK LINE 36 CRACKED. FABRICATED AND INSTALLED REPAIR SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 663-727, BUTTOCK LINE 0 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 663-727B, RIGHT BUTTOCK LINE 25 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 697-616, LT BUTTOCK LINE 45, RT BUTTOCK LINE 45 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FLOORBEAM FLANGE AT BS 420, LEFT BUTTOCK LINE 2, LEFT BUTTOCK LINE 42 CORRODED. REMOVED DAMAGED AREA AND REPAIRED FLOORBEAM PER EA. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 727B-947, LEFT BUTTOCK LINE 25 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FLOORBEAM AT BS 787, LEFT BUTTOCK LINE 65, RIGHT BUTTOCK LINE 65 CORRODED. REMOVED DAMAGED AREA AND REPAIRED TRACK PER EA. (M)

Part: DOOR — CRACKED (THRUST REVERSER)

PAE - DURING C-CHECK, FOUND NR 2 ENGINE DEFLECTOR DOOR SKIN AT THRUST REVERSER STATION 200.70 CRACKED. REMOVED DAMAGED AREA AND REPAIRED SKIN PER OHM. (M)

Part: FITTING — BENT (FUSELAGE)

PAE - DURING C-CHECK, FOUND FITTING AT BS 947, LEFT BUTTOCK LINE 65 BENT. REMOVED AND REPLACED FITTING PER BOEING DRAWING. (M)

Part: LINER — CRACKED (APU BAY)

PAE - DURING C-CHECK, FOUND APU TORQUE BOX LINER AT BS 1104, RIGHT BUTTOCK LINE 20 GOUGED AND CRACKED. REPAIRED TORQUE BOX LINER PER EA. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 807-867, LEFT BUTTOCK LINE 45 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M)

Part: GUSSET — CHAFED (NR 2 COWLING)

PAE - DURING C-CHECK, FOUND NR 2 ENGINE COWL GUSSET AT NACELLE STATION 236 CHAFED. REMOVED AND REPLACED GUSSET PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FLOORBEAM FLANGE AT BS 480, LEFT BUTTOCK LINE 43 CORRODED. REMOVED CORROSION AND REPAIRED FLOORBEAM PER EA. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 887-947, BUTTOCK LINE 0 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 400-480, LEFT BUTTOCK LINE 45 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FLOORBEAM AT BS 867, LEFT BUTTOCK LINE 65 RIGHT BUTTOCK LINE 65 CORRODED. REMOVED DAMAGED AREA AND REPAIRED PER EA. (M)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

PAE - DURING C-CHECK, FOUND SUPPORT ANGLE AT BS 358, RIGHT BUTTOCK LINE 12, RIGHT BUTTOCK LINE 36 CRACKED. REMOVED AND REPLACED SUPPORT ANGLE PER SRM. (M)

Part: DOOR FRAME — GOUGED (APU DOOR)

PAE - DURING C-CHECK, FOUND APU ACCESS DOOR FRAME WEB AT BS 1098, RIGHT BUTTOCK LINE 20 GOUGED. REMOVED AND REPLACED WEB PER SRM. (M)

Part: FAIRING — DENTED (THRUST REVERSER)

PAE - DURING C-CHECK, FOUND NR 1 ENGINE THRUST REVERSER FAIRING AT THRUST REVERSER STATION 185 DENTED. REMOVED AND REPLACED SKIN ON NR 1 ENGINE THRUST REVERSER FAIRING PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FLOORBEAM AT BS 1006, LEFT BUTTOCK LINE 10, RIGHT BUTTOCK LINE 28 CORRODED. REMOVED AND REPLACED FLOORBEAM PER SRM. (M)

Part: SILL — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND AFT ENTRY DOOR MOPSILL AT BS 986.5, LEFT BUTTOCK LINE 45 CORRODED. REMOVED AND REPLACED MOPSILL PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FLOOR SUPPORT AT BS 944-1016, LEFT BUTTOCK LINE 6, LEFT BUTTOCK LINE 15 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 344-400, LEFT BUTTOCK LINE 25 CORRODED. REMOVED CORROSION AND REPAIRED SEAT RACK PER SRM. (M)

Part: SUPPORT ANGLE — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND BULKHEAD SUPPORT ANGLE AT BS 500B, LEFT BUTTOCK LINE 35, RIGHT BUTTOCK LINE 35 CORRODED. REMOVED AND REPLACED BULKHEAD SUPPORT ANGLE PER SRM. (M)

Part: SKIN — CRACKED (L/E SLAT)

PAE - DURING C-CHECK, FOUND RIGHT WING FIXED LEADING EDGE NR 5 SLAT AT WING STATION 440 CRACKED. REMOVED DAMAGE AND INSTALLED DOUBLER PER EA. (M)

Part: SKIN PANEL — CRACKED (FUSELAGE)

PAE - DURING C-CHECK, FOUND SKIN PANEL AT BS 328, RIGHT BUTTOCK LINE 65 CRACKED. REMOVED CRACK, FABRICATED AND INSTALLED REPAIR PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FLOORBEAM AT BS 947, LEFT BUTTOCK LINE 44, RIGHT BUTTOCK LINE 54 CORRODED. REMOVED AND REPLACED FLOORBEAM PER SRM. (M)

Part: CHANNEL — CRACKED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CHANNEL AT BS 301-320, BUTTOCK LINE 0 CRACKED. REMOVED AND REPLACED CHANNEL PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FLOOR SUPPORT AT BS 994, LEFT BUTTOCK LINE 16 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM. (M)

Part: SILL — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND AFT GALLEY DOOR MOP SILL AT BS 907-1006, RIGHT BUTTOCK LINE 52 CORRODED. REMOVED AND REPLACED MOP SILL PER SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 986.5-1006, RIGHT BUTTOCK LINE 18 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M)

Part: ANGLE — GOUGED (NR 2 NACELLE)

PAE - DURING C-CHECK, FOUND NR 2 ENGINE FIXED FAIRING ANGLE AT NACELLE STATION 145 GOUGED. REPAIRED ANGLE PER SRM. (M)

Part: ANGLE — CHAFED (VERTICAL STAB)

PAE - DURING C-CHECK, FOUND VERTICAL STABILIZER SKATE ANGLE AT BS 1016-1056, RIGHT BUTTOCK LINE 12 CHAFED. REMOVED AND REPLACED SKATE ANGLE PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FLOOR SUPPORT AT BS 967-986.5, RIGHT BUTTOCK LINE 18, LEFT BUTTOCK LINE 18 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FLOOR SUPPORT AT BS 1006-1016, BUTTOCK LINE 0 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 867-947, RIGHT BUTTOCK LINE 45 CORRODED. REMOVED AND REPLACED DAMAGED SEAT TRACK PER SRM. (M)

Part: DOUBLER — CRACKED (NR 2 NACELLE)

PAE - DURING C-CHECK, FOUND NR 2 ENGINE COWL LATCH PIN DOUBLER AT NACELLE STATION 181 CRACKED. REMOVED AND REPLACED DOUBLER PER SRM. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FLOOR WEB AT BS 950-993, RIGHT BUTTOCK LINE 55 CORRODED. REMOVED AND REPLACED FLOOR WEB PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FLOOR SUPPORT AT BS 947-967, LEFT BUTTOCK LINE 18, RIGHT BUTTOCK LINE 18 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM. (M)

Part: FRAME — CHAFED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FRAME AT BS 1104, RIGHT BUTTOCK LINE 27 CHAFED. REMOVED DAMAGED AREA AND REPAIRED FRAME PER SRM. (M)

Part: RIB — GOUGED (NR 2 NACELLE)

PAE - DURING C-CHECK, FOUND NR 2 ENGINE COWL RIB AT NACELLE STATION 152.25, GOUGED. REMOVED DAMAGED AREA AND REPAIRED RIB PER SRM. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND AFT ENTRY DOOR THRESHOLD WEB AT BS 967, LEFT BUTTOCK LINE 52 CORRODED. REMOVED AND REPLACED WEB PER SRM. (M)

Part: ANGLE — CHAFED (VERTICAL STAB)

PAE - DURING C-CHECK, FOUND VERTICAL STABILIZER SKATE ANGLE AT BS 1016-1138, CHAFED. REMOVED AND REPLACED SKATE ANGLE PER SRM. (M)

Part: LONGERON — CHAFED (NR 1 NACELLE)

PAE - DURING C-CHECK, FOUND NR 1 ENGINE COWL LOGINTUDINAL AT NACELLE STATION 175.5 CHAFED. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIRS PER SRM. (M)

Part: SKIN PANEL — CRACKED (LT WING LE)

PAE - DURING C-CHECK, FOUND LEFT WING LEADING EDGE SKIN PANEL AT WS 329 CRACKED. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PER EA. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FRAME AT BS 1006, LEFT BUTTOCK LINE 39 CORRODED. REMOVED DAMAGE AND INSTALLED FABRICATED FRAME SECTION PER SRM. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

PAE - DUIRNG C-CHECK, FOUND APU ACCESS DOOR FRAME AT BS 1100, WATERLINE 220 CRACKED. REMOVED DAMAGE AND INSTALLED FABRICATED FRAME PER SRM. (M)

Part: RIB — CHAFED (THRUST REVERSER)

PAE - DURING C-CHECK, FOUND NR 1 ENGINE OUTBOARD TAILPIPE COWL RIB AT THRUST REVERSER STATION 123.47, WING STATION 191L CHAFED. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM. (M)

Part: WEB — GOUGED (FUSELAGE)

PAE - DURING C-CHECK, FOUND NR 4 FLAP TRACK FAIRING VERTICAL WEB AT BS 700, LEFT BUTTOCK LINE 65 GOUGED. REMOVED AND REPLACED WEB PER SRM. (M)

Part: FILLER — MISSING (RUB STRIP)

PAE - DURING C-CHECK, FOUND NR 2 ENGINE INBOARD COWL RUBSTRIP LOWER CORNER AT NACELLE STATION 99.25, WING STATION 191 MISSING FILLER SECTION. ADDED MISSING FILLER AND INSTALLED STRAP PER SRM. (M)

Part: ANGLE — CHAFED (LT WING TE)

PAE - DURING C-CHECK, FOUND LEFT WING TRAILING EDGE SIDE SUPPORT ANGLE AT WING STATION 337L, WATERLINE 180 CHAFED. REMOVED AND REPLACED SUPPORT PER SRM. (M)

Part: SHROUD — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CARGO BAY CEILING SUPPORT SHROUD AT BS 500A-500B, LEFT BUTTOCK LINE 43 CORRODED. REMOVED AND REPLACED SUPPORT SHROUD PER SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 663-720, LEFT BUTTOCK LINE 45 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND SEAT TRACK AT BS 727-727A, LEFT BUTTOCK LINE 25 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M)

Part: SIGN — INOPERATIVE (CABIN)

ANC - DURING INSPECTION, FOUND EXIT IDENTIFIER AT THE SMOKE BARRIER INOPERATIVE. REMOVED AND REPLACED EXIT IDENTIFIER, THEN LIGHT TESTED NORMAL. (M)

Part: GUIDE — OUT OF ADJUST (L1 DOOR)

OME - AFTER BOARDING, L1 DOOR DIFFICULT TO CLOSE. ADJUSTED L1 DOOR GUIDE ARM, THEN OPERATED NORMAL. (M)

Part: KEELBEAM — CORRODED

PAE - DURING SCHEDULED C-CHECK, FOUND KEEL BEAM FLANGE AT BS 679, RIGHT BUTTOCK LINE 7 RIGHT BUTTOCK LINE 9 WITH A DOUBLER DRILLED HOLE. REPAIRED PER EA. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK,F OUND AFT CARGO BAY FRAME AT BS 767, RIGHT BUTTOCK LINE 9 CORRODED. REMOVED DAMAGE AND REPAIRED PER SRM. (M)

Part: ARM — STIFF (PAX DOOR)

ANC - CREW REPORTED L1 DOOR DIFFICULT TO CLOSE. ADJUSTED GUIDE ARM, THEN OPS CHECKED GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

JNU - DURING MAINTENANCE CHECK, FOUND RED EMERGENCY FLOOR TRACK LIGHTS IN AFT CABIN INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY THEN LIGHTS OPERATED NORMAL. (M)

Part: BATTERY — INOPERATIVE

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS ON SEAT PALLET 3 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AND LIGHT OPERATED NORMALLY. (M)

Part: GUIDE — OUT OF ADJ (L1 DOOR)

ANC - DURING MAINTENANCE CHECK, FOUND L1 DOOR DIFFICULT TO CLOSE. ADJUSTED GUIDE ARM AND DOOR OPERATED NORMALLY. (M)

Part: HANDLE (L2 DOOR)

ANC - DURING MAINTENANCE CHECK, FOUND L1 DOOR DIFFICULT TO OPERATE. CLEANED AND LUBED HANDLE AND HANDLE OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (MID CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND BATTERY FOR SMOKE BARRIER EMERGENCY EXIT LIGHT DISCHARGED. REMOVED AND REPLACED BATTERY PACK AND LIGHT OPERATED NORMALLY. (M)

Part: RECEIVER — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROW 14 WERE INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER AND BATTERY. LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROW 14 WERE INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER AND BATTERY. LIGHTS OPERATED NORMALLY. REF ASAA0110016. (M)

Part: FRAME — CORRODED (FUSELAGE)

DURING SCHEDULED C-CHECK, CORROSION AND DOUBLE DRILLED HOLES IN THE OUTBOARD CHORD AT BODY STATION 727, STRINGER 20-25L. REPAIRED PER EA 5310-01877.

Part: STRUCTURE — CORRODED (FUSELAGE)

DURING SCHEDULED C-CHECK FOUND BODY STATION 1006, WATERLINE 156, BUTTOCK LINE 0 TO LEFT BUTTOCK LINE 12 CORRODED. REPAIRED PER SRM 51-40-2.

DURING SCHEDULED C-CHECK FOUND STRINGER TIE AT BODY STATION 540, STRINGER 24R CORRODED. REPAIRED PER SRM 51-30-2. PAGE 8.

Part: STRINGER CLIP — CORRODED (FUSELAGE)

DURING SCHEDULED C-CHECK. FOUND STRINGER TIE AT BODY STATION 540, STRINGER 26R CORRODED. REPAIRED PER SRM 51-30-2, PAGE 8.

Part: STRINGER CLIP — CORRODED (FUSELAGE)

DURING SCHEDULED C-CHECK, FOUND STRINGER TIE AT STATION 540, STRINGER 27L CORRODED. REPAIRED PER SRM 51-30-2, PAGE 8.

Part: STRUCTURE — DAMAGED (FUSELAGE)

DURING SCHEDULED C-CHECK, FOUND TWO SHORT EDGE MARGIN HOLES AT STATION 480, STRINGER -4R. REPAIRED PER EA 5310-01878.

Part: THRESHOLD — CRACKED (CARGO DOOR)

DURING SCHEDULED C-CHECK, AFT CARGO DOOR CENTER THRESHOLD HAS NUMEROUS CRACKS AND FORWARD CARGO DOOR CENTER THRESHOLD SCUFF PLATES HAS NUMEROUS CRACKS ON RADIOUS AND ON THE EDGES.REPAIRED PER EA 5330-01470.

Part: PLATE — CRACKED (DOOR SILL)

DURING SCHEDULED C-CHECK, AFT AND FWD CARGO DOOR SILL PLATE HAS CRACKS IN RADIUS. REPAIRED PER EA 5330-01470.

Part: CHARGER — INOPERATIVE (MID CABIN)

ANC-DURING MAINTENANCE CHECK THE OVERWING EXIT LIGHTS REMAINED ILLUMINATED WITH NO POWER FAILURE.REPLACED BATTERY CHARGER AND SYSTEM OPERATED NORMAL.

Part: BATTERY — DISCHARGED (EMERGENCY EXIT)

ANC - PRIOR TO FLIGHT 145, THE LEFT EMERGENCY EXIT LIGHT FAILED TO ILLUMINATE. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M)

Part: GUIDE — OUT OF ADJ (PAX DOOR)

SEA - PRIOR TO FLIGHT 66, THE L1 DOOR WAS DIFFICULT TO CLOSE. ADJUSTED THE L1 DOOR GUIDE ARM AND THE DOOR OPERATED NORMALLY. (M)

Part: LATCH — LACK OF LUBE (PAX DOOR)

ANC - PRIOR TO FLIGHT 61, THE L1 DOOR HOLD OPEN LATCH WAS FOUND TO BE DIFFICULT TO SECURE DOOR IN THE OPEN POSITION. LUBRICATED LATCH AND DOOR HOLD OPEN OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (NR 2 PALLET)

ANC - DURING MAINTENANCE CHECK, THE NR 2 SEAT PALLET EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: DOOR LATCH — OUT OF ADJ (PAX DOOR)

ANC - DURING MAINTENANCE CHECK, THE L1 DOOR HANDLE WAS DIFFICULT TO LOCK. ADJUSTED L1 DOOR UPPER GUIDE ARM AND LUBRICATED THE DOOR. DOOR OPERATED NORMALLY. (M)

Part: LAP JOINT — GOUGED (FUSELAGE)

SEA - DURING MAINTENANCE CHECK, THE SKIN LAP AT BS 290, STRINGER 19R UPPER SKIN LAP WAS FOUND TO BE GOUGED. REPAIRED PER EA 5330-01436. (M)

Part: ARM — OUT OF ADJ (PAX DOOR)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WAS FOUND TO BE DIFFICULT TO CLOSE AND LATCH. LUBRICATED AND ADJUSTED L1 DOOR GUIDE ARM, DOOR OPERATED NORMALLY. (M)

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE)

ANC - DURING MAINTENANCE CHECK, THE L1 DOOR SLIDE WAS FOUND TO HAVE LOW PRESSURE. REPLACED WITH SERVICEABLE SLIDE ASSEMBLY. ROUTED REMOVED SLIDE ASSEMBLY FOR INSPECTION AND REPAIR. (M)

Part: ROD — OUT OF ADJ (PAX DOOR)

ANC - DURING MAINTENANCE CHECK, THE L1 DOOR WAS FOUND DIFFICULT TO CLOSE. ADJUSTED UPPER HINGE ARM ROD AND DOOR OPERATED NORMALY. (M)

Part: FUSE — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EXIT IDENTIFIER WAS FOUND INOPERATIVE. REPLACED BATTERY, NO HELP. REPLACED FUSE IN BATTERY PACK AND EXIT IDENTIFIER OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (ROW 11)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHT BATTERY PACK AT ROW 11 WAS FOUND TO BE WEAK. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: A/C PACK — ODOR (LT PACK)

JNU - FLT 76 - FUMES RESEMBLING BURNED RUBBER REPORTED IN CABIN AFTER TAKEOFF. FLIGHT ATTENDANT REPORTED MILD HAZE OVERHEAD IN FORWARD CABIN AREA. AIRCRAFT RETURNED TO JNU AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND ENGINES, NO SMELL NOTED. RAN ENGINES TO TAKEOFF POWER, FOUND SMELL EMANATING FROM LEFT AIR CONDITIONING PACK SYSTEM. NO SMELL NOTED FROM RIGHT AIR CONDITIONING PACK SYSTEM. RELEASED LEFT PACK PER MEL 21-16. (M)

Part: BATTERY — DISCHARGED (SMOKE BARRIER)

SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY LIGHT WOULD NOT TEST. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M)

Part: BEARING — LACK OF LUBE (PAX DOOR)

ANC - PRIOR TO FLIGHT 41, THE L1 DOOR WOULD NOT CLOSE. INSPECTED AND LUBRICATED DOOR BEARINGS AND BEARING CUPS, DOOR OPERATES NORMALLY. (M)

Part: DOOR LATCH — LACK OF LUBE (PAX DOOR)

ANC - PRIOR TO FLIGHT 153, THE L1 DOOR WOULD NOT CLOSE. INSPECTED AND LUBRICATED DOOR, DOOR OPERATES NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (ROW 5)

SEA - AFTER RECON AND PRIOR TO FLIGHT 356, THE EMERGENCY EXIT TRACK LIGHT RECEIVER WOULD NOT TEST. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (PAX DOOR)

SEA - DURING MAINTENANCE CHECK, THE R1 DOOR LOWER EMERGENCY EXIT IDENTIFIER WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHT AT FORWARD PALLET WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: GUIDE — OUT OF ADJ (L1 DOOR)

PAE - DURING SCHEDULED C-CHECK, FOUND L1 DOOR DIFFICULT TO CLOSE. ADJUSTED GUIDE ARM AND RESET STOP PINS. DOOR OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - PRIOR TO FLIGHT 65, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WOULD NOT EXTINGUISH. REPAIRED GROUND WIRE ON MID TRANSMITTER AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — INOPERATIVE (ROW 16)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 16 PALLET. REPLACED BATTERY AND RECEIVER, LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (ROW 16)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 16 PALLET. REPLACED BATTERY AND RECEIVER, LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, BOTH INTERIOR OVERWING EMERGENCY EXIT SIGNS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (ROWS 6/7)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 6/7. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (ROW 16)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 16 WERE FOUND INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (ROW 8-10)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WILL NOT TURN ON OR OFF ON SEAT PALLET 8-10. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (ROW 8-11)

ANC - DURING MAINTENANCE CHECK, THE TWO FORWARD EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE ON SEAT PALLET 8-11. REPAIRED BROKEN WIRE AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (PALLET 6-1)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE ON SEAT PALLET 6-1. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY LIGHT WOULD NOT TEST. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD SEAT PALLET EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (SMOKE BARRIER)

SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M)

Part: RIB — WORN (COWL)

SEA - DURING SCHEDULED C-CHECK, THE NR 1 ENGINE INBOARD COWL 3RD RIB WAS FOUND TO BE WORN. REPAIRED PER EA 7110-01071. (M)

Part: FLOORBEAM — CORRODED (BS 787)

SEA - DURING SCHEDULED C-CHECK, FOUND CORROSION IN THE LOWER FORWARD FLANGE OF THE FLOORBEAM AT STATION 787 FROM 0 BBL TO 63 LBL. REPAIRED PER EA 5310-01597. (M)

Part: SKIN — CORRODED (WING)

SEA - DURING SCHEDULED C-CHECK, THE NR 3 LEADING EDGE SLAT ACTUATOR CUTOUT WAS FOUND TO BE CRACKED. REPAIRED PER EA 5720-01059. (M)

Part: FLOORBEAM — CORRODED (BS 947)

SEA - DURING SCHEDULED C-CHECK, FOUND CORROSION ON THE UPPER SURFACE OF THE FLOORBEAM ON BOTH FORWARD AND AFT FLANGES AT STATION 947.5 FROM LBL 30 TO RBL 60. REPAIRED PER EA 5310-01605 AND BOEING TELEX ASA-SEA-95-030RR. (M)

Part: SKIN — CRACKED (WING)

SEA - DURING SCHEDULED C-CHECK, THE NR 3 LEADING EDGE SLAT UPSTOP CUTOUT WAS FOUND TO BE CRACKED. REPAIRED PER EA 5720-01059. (M)

Part: FLOORBEAM — CORRODED (BS 787)

SEA - DURING SCHEDULED C-CHECK, FOUND CORROSION IN THE LOWER FORWARD FLANGE OF THE FLOORBEAM AT STATION 787 FROM CENTERLINE TO RBL 63. REPAIRED PER EA 5310-01597. (M)

Part: BEAM — GOUGED (RT MLG)

SEA - DURING SCHEDULED C-CHECK, A GOUGE WAS FOUND ON THE RT MAIN LANDING GEAR BEAM FORWARD CORNER. REPAIRED PER EA 5710-01047 AND BOEING TELEX ASA-SEA-94-0131RR. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 8 WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — MISSING (CABIN)

ANC - DURING MAINTENANCE CHECK, ONE RED EMERGENCY FLOOR TRACK LIGHT WAS FOUND TO BE MISSING AT NR 6 PALLET. REPLACED LIGHT ASSEMBLY, LAMP, AND LENS. OPS CHECK NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING RECON, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO INOPERATVIE AT ROW 14. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD SEAT PALLET EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE ON PALLET 5-9. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: RECEIVER — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 14 AND ROW 18 WERE FOUND INOPERATIVE. REPLACED RECEIVER AT ROW 14, BATTERY AT ROW 18, AND AFT TRANSMITTER. LIGHTS OPERATED NORMALLY. REF: OPERATOR CONTROL NR 98ZZZX377. (X)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 14 AND ROW 18 WERE FOUND INOPERATIVE. REPLACED RECEIVER AT ROW 14, BATTERY AT ROW 18, AND AFT TRANSMITTER. LIGHTS OPERATED NORMALLY. REF: OPERATOR CONTROL NR ASAA9710131.

Part: RECEIVER — INOPERATIVE (CABIN)

ANC - AFTER RECON WAS COMPLETED, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 18 AND 19. REPLACED RECEIVER AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 14 AND THE SMOKE BARRIER LIGHT WOULD NOT TEST PROPERLY. REPLACED RECEIVERS AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING RECONFIGURATION OF THE AIRCRAFT CABIN THE CENTER CEILING EMERGENCY EXIT SIGN AT THE OVERWING EXIT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHT OPERATED NORMALLY. (M)

Part: RIB — GOUGED (NR 2 ENGINE)

SEA - DURING 'C' CHECK, SEVERAL GOUGES WERE FOUND ON NR 2 ENGINE INBOARD FIXED COWL FOURTH RIB. REPAIRED PER EA 5420-01003 AND BOEING SRM. (M)

Part: SKIN — DENTED (BS 409-413)

SEA - DURING C-CHECK, A SMOKE DENT WAS FOUND IN THE SKIN BENEATH THE LOWER EDGE OF THE UPPER DECK CARGO DOOR AT BS 410. REPAIRED PER EA 5330-01296 AND BOEING TELEX ASA-SEA-97-0245RR. (M)

Part: SKIN — CHAFED (NR 3 LE FLAP)

SEA - DURING 'C' CHECK, A CHAFED AREA WAS FOUND ON THE LEADING EDGE BULLNOSE OF THE NR 3 LEADING EDGE FLAP AT STATION 100. REPAIRED PER EA 5750-01247 AND BOEING TELEX ASA-SEA-97-0260RR. (M)

Part: FLOORBEAM — CORRODED (BS 500)

SEA - DURING C-CHECK, THE FLOORBEAM AT BS 500A UPPER AFT FLANGE UPPER SURFACE WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01537 AND BOEING TELEX ASA-SEA-96-0260RR. (M)

Part: FITTING — CORRODED (BS 947-986)

SEA - DURING 'C' CHECK, THE AFT AIRSTAIR ARM HINGE BOLT HOLES IN THE FORWARD AND AFT FITTINGS WERE FOUND TO BE CORRODED. REPAIRED PER EA 5260-01051 AND BOEING TELEX ASA-SEA-96-0166RR. (M)

Part: FLANGE — CORRODED (BS 947)

SEA - DURING 'C' CHECK, THE AFT AIRSTAIR UPPER ARM ATTACH FLANGE FORWARD FACE WAS FOUND TO HAVE MINOR CORROSION. REPAIRED PER EA 5260-01061 AND BOEING TELEX ASA-SEA-96-0166RR. (M)

Part: RIB — CHAFED (LT ELEVATOR)

SEA - DURING 'C' CHECK, THE UPPER T-CHORD ON THE LEFT ELEVATOR BALANCE BAY 2 OUTBOARD RIB UPPER CHORD WAS FOUND CHAFED. REPAIRED PER EA 5520-01048 AND BOEING SRM. (M)

Part: RIB — GOUGED (NR 2 ENGINE)

SEA - DURING 'C' CHECK, SEVERAL GOUGES WERE FOUND ON NR 2 ENGINE INBOARD FIXED COWL FOURTH RIB. REPAIRED PER EA 5420-01003 AND BOEING SRM. REFERENCE ASAA9710054.

Part: LONGERON — CHAFED (NR 2 ENGINE)

SEA - DURING 'C' CHECK, THE NR 2 ENGINE INBOARD FIXED COWL AFT UPPER LONGERON AND RIB WERE FOUND TO HAVE CHAFING MARKS. REPAIRED PER EA 5410-01018 AND BOEING SRM. (M)

Part: ANGLE — CORRODED (BS 986.5)

SEA - DURING 'C' CHECK, THE ANGLE JUST FORWARD OF THE AFT GALLEY ADJACENT TO THE FLOORBEAM AT STATION 986.5 AND LBL 39 WS FOUND TO BE CORRODED AND CRACKED. REPAIRED PER EA 5320-01350 AND BOEING SRM. (M)

Part: FLANGE — CORRODED (BS 986)

SEA - DURING 'C' CHECK, THE AFT AIRSTAIR UPPER ARM ATTACH FLANGE AFT FACE WAS FOUND TO HAVE MINOR CORROSION. REPAIRED PER EA 5260-01062 AND BOEING TELEX ASA-SEA-96-0166RR. (M)

Part: FLOORBEAM — CORRODED (BS 400)

SEA - DURING 'C' CHECK, THE FLOORBEAM FORWARD AND AFT UPPER FLANGE WAS FOUND TO BE CORRODED ON THE LOWER SURFACE. REPAIRED PER EA 5310-01536 AND BOEING TELEX ASA-SEA-96-0177RR. (M)

Part: FLOORBEAM — CORRODED (BS 690-700)

SEA - DURING 'C' CHECK, THE LONGINUDINAL FLOORBEAM OUTBOARD FLANGE AT LBL 25, BS 690 TO BS 700 WAS FOUND TO BE CORRODED AND CRACKED. REPAIRED PER EA 5310-01535 AND BOEING TELEX ASA-SEA-96-0254RR. (M)

Part: FLOORBEAM — CORRODED (BS 520)

SEA - DURING 'C' CHECK, THE FLOORBEAM FORWARD UPPER FLANGE WAS FOUND TO BE CORRODED ON THE LOWER SURFACE. REPAIRED PER EA 5310-01538 ADN BOEING TELEX ASA-SEA-96-0266RR. (M)

Part: ANGLE — CRACKED (BS 530)

SEA - DURING 'C' CHECK, THE ANGLE JUST FORWARD OF THE HEAT EXCHANGER COMPARTMENT, ADJACENT TO STRINGER 22L WAS FOUND CRACKED APPROXIMATELY .50 INCH IN LENGTH. THE CRACK INITIATED FROM THE FASTENER HOLE AND RAN TO THE EDGE OF THE HORIZONTAL FLANGE. REPAIRED PER EA 5320-01304 AND BOEING SRM 51-40-2. (M)

Part: BATTERY — DISCHARGED (CARGO COMPT)

SEA - DURING MAINTENANCE CHECK, THE NR 3 PALLET EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE LEFT OVERWING EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHT OPERATED NORMALLY. (M)

Part: HINGE PLATE — LACK OF LUBE (L-1 DOOR)

SEA - FLT 64 - CREW REPORTED, L-1 DOOR HARD TO CLOSE. CLEANED AND LUBED HINGE PLATE BEARING SURFACE. INSPECTED DOOR, NO DEFECTS FOUND. DOOR OPERATED NORMALLY. (M)

Part: BATTERY PACK — DEFECTIVE (CARGOCOMPT)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACKLIGHTS WERE FOUND INOPERATIVE ON 1 PALLET. REPLACED BATTERY PACK AND LIGHTSOPERATED NORMALLY. (M)

Part: ACTUATOR — LEAKING (NLG)

ANC-ATB - FLT 122 - ON TAKEOFF FROM ANC, NOSE LANDING GEAR FAILED TO RETRACT. AIRCRAFT RETURNED TO ANC AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND 'B' NUT ON NLG LOCK ACTUATOR LEAKING. TIGHTENED 'B' NUT, PERFORMED RETRACTION CHECK AND GEAR OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING RECON, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT PALLET 1-5. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING CREW PREFLIGHT, THE CREW REPORTED THAT THE AFT EMERGENCY FLOOR TRACK LIGHTS STAYED ON WITH THE SWITCH IN THE OFF POSITION. REMOVED AND REPLACED BATTERY PACK. (W)

Part: LIGHT — INOPERATIVE (L-2 DOOR)

SEA - DURING MAINTENANCE CHECK, THE INTERIOR EMERGENCY EXIT LIGHT OVER THE L-2 DOOR WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

JNU - DURING MAINTENANCE CHECK, FOUND ONE SEAT PALLET TRACK LIGHTS INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT ASSY — DEFECTIVE (AIRSTAIR DOOR)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT OVER THE AIRSTAIR DOOR WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: EEL ASSY — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT AIRSTAIR DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (X)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE FORWARD RIGHT EMERGENCY EXIT SLIDE LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHT OPERATED NORMALLY. (X)

Part: MIX CHAMBER — LEAKING (RT PACK)

OME - AIR TURN BACK OF FLT NR 58, CREW REPORTED SMOKEY ODOR IN CABIN DURING CLIMB-OUT. REPLACED RIGHT AIR CONDITIONING PACK SHUTOFF VALVE AND MIX CHAMBER AND OPERATED NORMALLY. (M)

Part: PACK SHUTOFF VLV — LEAKING (RT PACK)

OME - AIR TURN BACK OF FLT NR 58, CREW REPORTED SMOKEY ODOR IN CABIN DURING CLIMB-OUT. REPLACED RIGHT AIR CONDITIONING PACK SHUTOFF VALVE AND MIX CHAMBER AND OPERATED NORMALLY. REFERENCE NR ASAA9510085.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 20. REPLACED BATTERY PACK AND BATTERY CHARGER, LIGHTS OPERATED NORMALLY. (M)

Part: EEL BATT CHARGER — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 20. REPLACED BATTERY PACK AND BATTERY CHARGER, LIGHTS OPERATED NORMALLY. REF ASAA9510077.

Part: EEL BATT PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, TWO WHITE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 15 WERE FOUND INOPERATIVE. RELAMPED ONE LIGHT AND RELEASED THE REMAINING LIGHT PER MEL 33-19. SUBSEQUENTLY RELAMPED BATTERY PACK AT ROW 15 AND LIGHTS OPERATED NORMALLY. REMOVED PLACARD. (Z)

Part: ARM — OUT OF ADJUST (L1 DOOR)

ANC - FLT 112 - DIFFICULT TO GET L-1 DOOR HANDLE ALL THE WAY CLOSED. ADJUSTED UPPER LOCKING ARM AND DOOR OPERATED NORMALLY. (Z)

Part: HANDLE — LACK OF LUBE (L1 DOOR)

ANC - FLT 50 - DIFFICULT TO GET L1 DOOR HANDLE ALL THE WAY CLOSED. LUBED HANDLE ASSEMBLY AND OVER MECHANISM, DOOR OPERATED NORMALLY. (Z)

Part: COVER — LOOSE (L-1 DOOR HINGE)

JNU - FLT 65 - CREW REPORTED, THE L-1 DOOR WAS DIFFICULT TO CLOSE. REATTACHED LOOSE HINGE COVER TRIM ON L-1 DOOR AND OPERATED NORMALLY. (W)

Part: EEL ASSY — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT OVER THE L2 AIRSTAIR DOOR WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (W)

Part: FLOOR BEAM — CORRODED (BS 727B)

SEA - DURING D-CHECK, FLOOR BEAM AT BS 727B WAS FOUND TO BE CORRODED ON THE UPPER CHORD FLANGES. REPAIRED PER EA 5310-01323 AND BOEING TELEX ASA-SEA-95-0098RR. (Z)

Part: SPAR — CRACKED (LT HORIZ STAB)

SEA - DURING D-CHECK, THE LEFT HORIZONTAL STABILIZER REAR SPAR UPPER LUG WAS FOUND CORRODED AND A CRACK WAS DETECTED IN THE BORE OF THE UPPER LUG. REPAIRED PER EA 5510-01026 AND BOEING TELEX ASA-SEA-950082RR. (Z)

Part: BULKHEAD — CRACKED (BS 727)

SEA - DURING D-CHECK, THE LOWER OUTBOARD CHORD OF BS 727 BULKHEAD, LBL 27 AND 38 WAS FOUND CRACKED. REPAIRED PER EA 5310-01325 AND BOEING TELEX ASA-SEA-95-0111RR. (Z)

Part: BULKHEAD — CRACKED (BS 727)

SEA - DURING D-CHECK, LOWER OUTBOARD CHORD OF BS 727 BULKHEAD, RBL 38 AND 27 WAS FOUND CRACKED. REPAIRED PER EA 5310-01326 AND BOEING TELEX ASA-SEA-95-0111RR. (Z)

Part: FLOOR BEAM — CORRODED (BS 685)

SEA - DURING D-CHECK, THE LONGITUDINAL FLOOR BEAM AT RBL 45.5 BETWEEN BS 670 AND 690 AND WAS FOUND CORRODED IN SEVERAL LOCATIONS. REPAIRED PER EA 5310-01329 AND BOEING TELEX ASA-SEA-95-0094RR. (Z)

Part: FLOOR BEAM — CORRODED (BS 727B)

SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE UPPER CHORD FLANGES OF THE FLOOR BEAM AT BS 727B. REPAIRED PER EA 53-10-01323 AND BOEING TELEX ASA SEA-95-0095RR. (Z)

Part: FLOORBEAM — CRACKED (FS 520)

SEA - DURING D-CHECK, FOUND CRACKS IN STA 520 FLOOR SUPPORT BEAM AT THE FOLLOWING LOCATIONS, LBL 45, RBL 24.5 AND RBL 45. MAINTENANCE REPAIRED CRACKS USING EA 5310-01318, EA 5310-01319 AND EA 5310-01320. (W)

Part: FLOORBEAM — CORRODED (BS 500)

SEA - DURING D-CHECK, CORROSION WAS FOUND ON FLOORBEAM AT BS 500B. MAINTENANCE ACCOMPLISHED REPAIR PER SRM 51-10-6 AND EA 5310-01324. (W)

Part: KEEL BEAM — CRACKED (BS 540)

SEA - DURING D-CHECK, A CRACK WAS FOUND ON THE HORIZONTAL FLANGE OF THE KEEL BEAM CHORD AT BS 540, LBL 6.30. THE CRACK WAS APPROXIMATELY 2 INCHES IN LENGTH AND APPEARS TO HAVE ORIGINATED AT THE AFT MACHINE STEP AND TRAVELED FORWARD. REPAIRED CRACK PER EA 5310-01315. (W)

Part: FLOORBEAM — CORRODED (BS 547.5)

SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE FLANGE OF THE FLOORBEAM UPPER CHORD AT STA 547.5. REPAIRED CHORD PER EA 5310-01317 AND BOEING TELEX ASA-SEA-94-0310RR. (W)

Part: KEEL BEAM — CORRODED (BS 647-727)

SEA - DURING D-CHECK, SURFACE CORROSION WAS FOUND AROUND THE FASTENER HOLES OF KEEL BEAM BS 647 TO 727, LBL 6.5. REPAIRED KEEL BEAM PER EA 5310-01321 AND BOEING TELEX ASA-SEA-95-0057RR. (W)