N741AS

Part: SKIN — CRACKED (L1 DOOR) · airframe 72,093 hrs · 64,277 cycles

L1 DOOR SKIN LOWER HINGE CUTOUT CONTAINED A CRACK AT THE LWR CORNER MEASURING APPROX .0350 INCHES. REMOVED DAMAGE AND INSTALLED DOUBLER PER EA 5210 01215.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,995 hrs · 64,179 cycles

AFT CABIN BULKHEAD EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY, OPS CHECK NORMAL.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 71,831 hrs · 64,021 cycles

SMOKE BARRIER EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,822 hrs · 64,012 cycles

AFTER RECON L2 DOOR INTERIOR EMERGENCY LIGHT INOP. REPLACED L2 DOOR EMERGENCY EXIT LIGHT CHARGER CONTROL UNIT BATTERY PACK.

Part: WIRE — CHAFED (LANDING LIGHT) · airframe 71,794 hrs · 63,989 cycles

WHILE TROUBLESHOOTING SCHEDULED MEL 6215944 FOR LEFT O/B LANDING LIGHT POPS C/B WHEN TURNED ON. FOUND BURNT WIRING WHERE IT GOES INTO A CONDUIT OVER THE NR 1 ENG PYLON. WIRING CHAFED AGAINST CONDUIT CAUSING IT TO SHORT OUT. EVENT BASED TECHNICAL RESPONSE INITATED BY MAINT CONTROL AND ENGINEERING.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 70,936 hrs · 63,152 cycles

SMOKE BARRIER EMERGENCY EXIT LIGHT NOT WORKING PROPERLY. REPLACED BATTERY, OPS OK.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 70,773 hrs · 62,989 cycles

FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED R 2 EXIT LIGHT BATTERY. OPS GOOD.

Part: LIGHT — INOPERATIVE (L-1 DOOR) · airframe 70,773 hrs · 62,989 cycles

FOUND EMERGENCY EXIT LIGHT ABOVE L 1 DOOR INOP. REPLACED LIGHT ASSY. OPS NORMAL.

Part: SKIN — DENTED (BS 1016-1028) · airframe 70,766 hrs · 62,984 cycles

FOUND EXISTING REPAIRS DAMAGED (DENTED) BEYOND LIMITS. REMOVED AND REPLACED DAMAGED REPAIRS PER EA 5330 02044

Part: SKIN — CORRODED (BS 480) · airframe 70,766 hrs · 62,984 cycles

FOUND FWD CARGO PIT SKIN CORRODED. REPAIRED PER SRM 53 10 3 FIG 1.

Part: STRINGER CLIP — MISSING (BS 480) · airframe 70,766 hrs · 62,984 cycles

FOUND FWD CARGO PIT TIE CLIP MISSING. REPLACED MISSING TIE CLIP WITH REPLACEMENT PART PER SRM 51 30 02.

Part: SHEAR TIE — GOUGED (BS 767) · airframe 70,766 hrs · 62,984 cycles

FOUND TOOLING DAMAGE TO SHEAR TIE. REPLACED SHEAR TIE PER SRM 51 30 02.

Part: SKIN — GOUGED (BS 945) · airframe 70,766 hrs · 62,984 cycles

FOUND SKIN GOUGED. REPAIRED IAW EA 5330 02099.

Part: FRAME — CRACKED (BS 348) · airframe 70,766 hrs · 62,984 cycles

FOUND FWD ENTRY FRAME CRACKED AT FASTENER HOLE. REPLACED FRAME PER SRM 53 10 1.

Part: STRINGER — CORRODED (BS 902-947) · corrosion level 2 · airframe 70,766 hrs · 62,984 cycles

FOUND STRINGER CORRODED. REPLACED CORRODED STRINGER WITH NEW PART PER SRM 53 10 1.

Part: STRINGER — CORRODED (BS 380) · corrosion level 2 · airframe 70,766 hrs · 62,984 cycles

FOUND FWD CARGO PIT STRINGER CORRDED. REPLACED STRINGER WITH REPAIR PARTS PER SRM 53 10 01.

Part: STRINGER — CORRODED (BS 940-950) · corrosion level 2 · airframe 70,766 hrs · 62,984 cycles

FOUND STRINGER 22C CORRODED. REPAIRED STRINGER 22C PER SRM 53 10 3.

Part: SILL — CORRODED (BS 947-967) · corrosion level 2 · airframe 70,766 hrs · 62,984 cycles

FOUND R2 DOORWAY SILL CHORD IS CORRODED. REPLACED SILL CHORD PER SRM 57 30 2.

Part: STRINGER — CORRODED (BS 380-384) · corrosion level 2 · airframe 70,766 hrs · 62,984 cycles

FOUND FWD CARGO PIT STRINGER CORRODED. REPAIRED BY FABRICATING AND INSTALLING REPAIR PART PER SRM 53 10 1.

Part: STRINGER — CORRODED (BS 767-780) · corrosion level 2 · airframe 70,766 hrs · 62,984 cycles

FOUND STRINGER 25R CORRODED. REPAIRED STRINGER PER SRM 53 10 3.

Part: STRINGER SPLICE — CORRODED (BS 536-540) · corrosion level 2 · airframe 70,766 hrs · 62,984 cycles

FOUND FWD CARGO STRINGER SPLICE CORRODED. REPLACED WITH FABRICATED REPAIR PART IAW SRM 51 30 02 AND 53 10 01.

Part: STRINGER — CORRODED (BS 380 S27R) · corrosion level 2 · airframe 70,766 hrs · 62,984 cycles

FOUND STRINGER 27R IS CORRODED. REPLACED STRINGER PER SRM 53 10 1 FIG 1.

Part: SLIDE RAFT — MALFUNCTIONED (L1 DOOR) · airframe 70,766 hrs · 62,984 cycles

UPON DEPLOYMENT OF L 1 DOOR SLIDE, SLIDE INFLATED SLOWLY AND LANYARD DID NOT RELEASE. SLIDE DID NOT TOUCH FLOOR (SLIDE) BENT IN HALF. REPLACED L1 SLIDE ASSY PER AMM 25 65 31 201.

Part: FAN — INOPERATIVE (COCKPIT) · airframe 70,251 hrs · 62,494 cycles

DURING DEICING SMOKE BEGAN BILLOWING OUT OF CB PANEL BEHIND CAPT. PACKS WERE OFF, BLEEDS OFF, SMOKE HAD AN ELECTRICAL SMELL. REPLACED FLT DECK AIR COND FAN. CHK'D ALL CB PNLS, E/E COMP, NFF. FOUND WIRE W40-207-08 TERMINAL B1 OF C803 HEATING EXCESSLY UNDER APU LOAD. REPLACED GEN BREAKER ASA P/N 1-2420-9-1012, SN 0076. RETERMINATED TERMINAL AT C803 B1.

Part: FRAME — DENTED (BS 927-947)

DENT IN FUSELAGE SKIN AT BSTA 927-947.5 BETWEEN STRINGERS 18 AND 19 LT. REPAIRED IAW SRM. (K)

Part: SKIN — CRACKED (BS 727B-747)

1.5 INCH CRACK IN FUSELAGE LT SIDE, BSTA 727B-747 JUST BELOW BLUE PAINT LINE 32 INCHES BELOW WINDOW. (S16L) REPAIRED IAW SRM. (K)

Part: ATTACH FITTING — CRACKED (NR 5 SLAT)

DURING L/E LUBE W/C 18412001, FOUND NR 5 L/E SLAT IB SLAT TRACK ATTACH FITTING CRACKED AT MOUNT EAR PN 69-40609-1. REPLACED ATTACH FITTING WITH 69-40609-3 IAW EA TO COMPLY WITH EM 5740-01458 AND AD 2005-20-16. (K)

Part: PLENUM — ODOR (NR 2 A/C BAY)

ANC - FLIGHT DECK FUMES, AFTER LANDING AT SCC ARID SMELL ENTERED FLIGHT DECK, ISOLATED TO LEFT PACK RELEASED PER MEL. FOUND LEFT PACK CHAMBER MIX DUCT BLOWN, DUCT FLANGE PULLED AWAY FROM MIX CHAMBER. REPLACED MIX CHAMBER, REPLACED BOTH COALESCER BAGS. (M)

Part: DOUBLER — SCRATCHED (FUSELAGE)

OKC - LT FUSELAGE EXTERNAL DOUBLER HAS DEEP SCRATCHES BELOW L-1 DOOR CUTOUT AT FS 314, S20L. (MARKED) REMOVED DAMAGED DOUBLER, FABRICATED AND INSTALLED A REPLACMENT DOUBLER IAW AS EA AND AAR EA. (K)

Part: SKIN — GOUGED (FUSELAGE)

OKC - STA 209 UNDER RT FWD FAIRING, SKIN IS GOUGED AT RT AFT CORNER OF CUTOUT FOR DOOR 1103. REMOVED DAMAGE, COMPLIED WITH A HFEC IAW MFG NDT MANUAL, NO DEFECTS WERE NOTED. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW EA. (K)

Part: SKIN — GOUGED (FUSELAGE)

OKC - GOUGES IN SKIN AT B-STA 727A JUST ABOVE S26R. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER, STRUCTURAL FILLER, AND DOUBLER IAW AS EA AND AAR EA. (K)

Part: FRAME — MISDRILLED (FUSELAGE)

OKC - FUSELAGE, STA 597 APPROX RBL 68 CABIN FLOORBEAM HAS MISDRILLED HOLES. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE, DOUBLER, AND TRIPLER. ORDERED AND INSTALLED LOWER CHORD AND FRAME IAW SRM. (K)

Part: WIRE — SHORTED (CARGO SMOKE)

AT CRUISE ALT (30,000 FT) GOT FIRE BELL AND CARGO SMOKE LIGHT. THE CARGO SMOKE PANEL HAD (SMOKE) AND (ARMED) ANNUNCIATIONS. CREW FIRED HALON AND DECLARED EMERGENCY. RETURNED TO DEPARTURE WITH NO FURTHER EVENTS. REPLACED BOTH AFT CARGO FIRE BOTTLES AND SQUIBS. FOUND 14VDC AT PIN 9 OF D9503P OF CEU NR 2, FOUND INTERMITTENT SHORT. FOUND WIRES BARE DUE TO RUBBING ON APU BLEED AIR DUCT AT UPPER LT FWD BAG PIT. REPAIRED ALL AFFECTED WIRES (8 EA) IAW AMM. OPS TEST OF CARGO SMOKE DETECTORS AND FIRE SUPPRESSION SYSTEM GOOD REF AMM. (REF SDR ASAA0410410, SUBM 9/29/04 SAME EVENT AWAITING TEARDOWN REPORT. (K)

Part: CONTROL PANEL — MALFUNCTIONED (FIRE DETECTION)

MULTIPLE FIRE WARNINGS, CARGO FIRE SUPPRESSION ACTIVATED IN THE AFT CARGO PIT. NO EVIDENCE OF FIRE OR SMOKE FOUND. REMOVED AND REPLACED FIRE SUPPRESSION AND SMOKE DETECTION CONTROL PANEL AS A PRECAUTIONARY MEASURE, AND REMOVED AND REPLACED THE LT CARGO PIT FIRE SUPPRESSION BOTTLE AND DRIER UNIT. SDR BEING SENT AS OPEN PENDING THE SHOP FINDINGS ON THE CONTROL PANEL. THE LINE TECH ON SITE IAW THE AMM DETERMINED THE PRELIMINARY CONDITION AS GOOD. (K)

Part: LANDING GEAR — ICED (NLG)

ANC - DURING CLIMB-OUT KODIAK NOSE GEAR UNSAFE LIGHT INDICATION WAS OBSERVED AND NOSE GEAR DROPPED WITH GEAR HANDLE IN 'OFF' POSITION. REMOVED ICE FROM NOSE LANDING GEAR SKIN AREA, THEN LANDING GEAR, OPS CHECK NORMAL. (M)

Part: SKIN — DAMAGED (FUSELAGE)

OAK - DURING SCHEDULED D-CHECK, FOUND REPAIR AT LEFT FUSELAGE SKIN AT STATION 907 AND STRINGER 10L REQUIRES REWORK. REPAIR IAW EA. (M)

Part: SKIN — BENT (FUSELAGE)

OAK - DURING SCHEDULED D-CHECK, FOUND SKIN PATH BELOW CARGO DOOR BENT. REPAIR IAW EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OAK - DURING SCHEDULED D-CHECK, FOUND CABIN FLOORBEAM AT STATION 500A TOP SIDE CORRODED FROM RBL 4 TO RBL 23. REPAIR IAW EA. (M)

Part: DOOR FRAME — DAMAGED (CARGO DOOR)

OAK - DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR NEEDS FRAME MODIFICATION. REPAIR IAW EA. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOOR SUPPORT AT FUSELAGE STATION 540-727B, RIGHT BUTTOCK LINE 24 CORRODED. REPAIRED FLOOR SUPPORT PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 807, LEFT BUTTOCK LINE 62.5- RIGHT BUTTOCK LINE 62.5 CORRODED. REPAIRED FLOORBEAM PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 847, RIGHT BUTTOCK LINE 24.75, RIGHT BUTTOCK LINE 61 CORRODED. REPAIRED FLOORBEAM PER EA. (M)

Part: STRINGER — CRACKED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND STRINGER 16R AT FUSELAGE STATION 500B PLUS 15 CRACKED. REPAIRED STRINGER PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 360, RIGHT BUTTOCK LINE 19, RIGHT BUTTOCK LINE 52 CORRODED. REPAIRED FLOORBEAM PER SRM. (M)

Part: BEAR STRAP — DAMAGED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, REPLACED INTERIM REPAIR TO THE BEAR STRAP AT FUSELAGE STATION 259-277, LEFT BUTTOCK LINE 15.47. REPAIRED BEAR STRAP PER EA. (M)

Part: STRINGER — CRACKED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND STRINGER 24L AT FUSELAGE STATION 350 CRACKED. REPAIRED STRINGER PER SRM. (M)

Part: FLOORBEAM — DAMAGED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND AFTER ACCOMPLISHING A FLOORBEAM REPAIR, THE SHEAR WEB AT FUSELAGE STATION 500A, LEFT BUTTOCK LINE 24 HAS MISALIGNED HOLES. REPAIRED SHEAR WEB PER EA. (M)

Part: SEAT TRACK — DAMAGED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 370-446, RIGHT BUTTOCK LINE 45 PITTED AND GOUGED. REPLACED SEAT TRACK PER SRM. (M)

Part: SKIN PANEL — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE INTERNAL SKIN PANEL AT FUSELAGE STATION 382, STRINGER 28R-28L CORRODED. REPAIRED SKIN PANEL PER EA. (M)

Part: STRUCTURE — CHAFED (NR 2 PYLON)

OKC - DURING SCHEDULED D-CHECK, FOUND THE NR 2 ENGINE PYLON AT FAIRING STATIONS 40 AND 62 CHAFED. REPAIRED PYLON PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 727B, LEFT BUTTOCK LINE 60, RIGHT BUTTOCK LINE 41 CORRODED. REPAIRED FLOORBEAM PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 947, LEFT BUTTOCK LINE 24.75, RIGHT BUTTOCK LINE 24.75 CORRODED. REPAIRED FLOORBEAM PER EA. (M)

Part: SKIN — DAMAGED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, A PREVIOUS SKIN REPAIR WAS NOT CONFIGURED TO THE CURRENT AND REVISED SRM AT FUSELAGE STATION 344, STRINGER 19R. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE FRAME AT FUSELAGE STATION 685, STRINGER 13R-16R CORRODED. REPLACED FRAME PER SRM AND BOEING DRAWING. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 540-727B, RIGHT BUTTOCK LINE 44 CORRODED. REPLACED FLOORBEAM PER SRM. (M)

Part: FITTING — CRACKED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE BULKHEAD FITTING AT FUSELAGE STATION 727, RIGHT BUTTOCK LINE 45.5 CRACKED. REPLACED FITTING PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 540-727B, BUTTOCK LINE 0 CORRODED. REPLACED FLOORBEAM PER SRM. (M)

Part: SKIN PANEL — DENTED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE SKIN PANEL AT FUSELAGE STATION 350, STRINGER 24L DENTED. REPAIRED SKIN PANEL PER SRM. (M)

Part: PRESSURE PANEL — DAMAGED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE PRESSURE WEB AT FUSELAGE STATION 260.5, STRINGER 27L HAS ELONGATED HOLES. REPAIRED WEB PER SRM AND EA. (M)

Part: SKIN — GOUGED (HORIZ STAB)

OKC - DURING SCHEDULED D-CHECK, FOUND THE LEFT HORIZONTAL STABILIZER LEADING EDGE AT STABILIZER STATION 156.55-159 GOUGED. REPAIRED HORIZONTAL STAB PER EA. (M)

Part: FLOORBEAM — DAMAGED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 380, LEFT BUTTOCK LINE 11, RIGHT BUTTOCK LINE WITH ELONGATED HOLES. REPAIRED FLOORBEAM PER EA. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 480-520, RIGHT BUTTOCK LINE 25 CORRODED. REPAIRED SEAT TRACK PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 480, RIGHT BUTTOCK LINE 5, RIGHT BUTTOCK LINE 59 CORRODED. REPAIRED FLOORBEAM PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 260, BUTTOCK LINE 0, LEFT BUTTOCK LINE 10 CORRODED. REPAIRED FLOORBEAM PER SRM. (M)

Part: SKIN PANEL — DENTED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE SKIN PANEL AT FUSELAGE STATION 440-455, STRINGER 25R DENTED. REPAIRED SKIN PANEL PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 520, RIGHT BUTTOCK LINE 60, LEFT BUTTOCK LINE 55 CORRODED. REPAIRED FLOORBEAM PER EA. (M)

Part: SKIN — DAMAGED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, A PREVIOUS SKIN REPAIR WAS NOT CONFIGURED TO THE CURRENT AND REVISED SRM AT FUSELAGE STATION 927, STRINGER 20R. REMOVED PREVIOUS REPAIR AND REPLACED THE NEW REVISED SRM REPAIR. (M)

Part: FRAME — DAMAGED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, THE LOWER CHORD AT FUSELAGE STATION 294, STRINGER 25L HAD A FASTENER LOCATION TRIMMED OUT. REPAIRED LOWER CHORD PER EA. (M)

Part: WEB — DAMAGED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE WEB AT FUSELAGE STATION 260.5, STRINGER 27L HAS ELONGATED HOLES. REPAIRED WEB PER SRM AND EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 540-727B, BUTTOCK LINE 0 CORRODED. REPLACED FLOORBEAM PER SRM. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE SKIN PANEL AT FUSELAGE STATION 350, STRINGER 24L DENTED. REPAIRED SKIN PANEL PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 847, RIGHT BUTTOCK LINE 24.75, RIGHT BUTTOCK LINE 61 CORRODED. REPAIRED FLOORBEAM PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 294, LEFT BUTTOCK LINE 11 CORRODED. REPLACED DAMAGED SECTION OF FLOORBEAM PER SRM. (M)

Part: FRAME — DENTED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE FRAME AT FUSELAGE STATION 500, STRINGER 25L DENTED. REMOVED DAMAGED AREA AND REPAIRED FRAME PER SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 807-947, RIGHT BUTTOCK LINE 24.75 CORRODED. REPLACED DAMAGED SECTION OF SEAT TRACK PER SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 683-727, RIGHT BUTTOCK LINE 60 CORRODED. REPLACED DAMAGED SECTION OF SEAT TRACK PER SRM. (M)

Part: SHEAR TIE — DAMAGED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND DAMAGED SHEAR TIE AT FUSELAGE STATION 340, STRINGER 26R-27R. REPLACED SHEAR TIE PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 540-663, LEFT BUTTOCK LINE 24 CORRODED. REPLACED FLOORBEAM PER SRM. (M)

Part: SKIN PANEL — DENTED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE SKIN PANEL AT FUSELAGE STATION 219, STRINGER 24L DENTED. REMOVED DAMAGED AREA AND REPAIRED SKIN PANEL PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOOR SUPPORT AT FUSELAGE STATION 660, RIGHT BUTTOCK LINE 48, RIGHT BUTTOCK LINE 52 CORRODED. REPAIRED FLOOR SUPPORT PER SRM. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SEA - DURING SCHEDULED MAINTENANCE INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTING AT SEAT PALLETS 1-11, 3-3 AND 9-2 INOPERATIVE. REPLACED BATTERY PACKS, THEN FLOOR TRACK LIGHTS TESTED NORMAL. (M)

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

ANC - DURING SCHEDULED MAINTENANCE INSPECTION, FOUND EMERGENCY EXIT IDENTIFIER AT THE R2 DOOR WILL NOT ILLUMINATE. REPLACED BATTERY, THEN EXIT IDENTIFIER TESTED NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED MAINTENANCE INSPECTION, FOUND NO LED INDICATION OF AFT CONTROL MODULE FUNCTION. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERIES ON PALLETS 10-5, 5-5, AND 6-9, REMOTE ASSEMBLY RECEIVERS ON PALLETS 10-5 AND 5-5, FORWARD CONTROL MODULE (P/N 87-3-2030-4-1), AND FORWARD AND AFT CONTROL MODULE BATTERIES (P/N 86-2-1015-1), THEN LIGHTS TESTED NORMAL. (M)

Part: RECEIVER — INOPERATIVE (CABIN)

ANC - DURING INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROWS 6 AND 7 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER AND BATTERY, THEN LIGHT TESTED NORMAL. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND AFT CARGO DOOR FRAME AT BS 790-794, STRINGER 23R-26R CORRODED. REMOVED CORROSION AND REPAIRED CARGO DOOR FRAME PER SRM. (M)

Part: SKIN — DENTED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FUSELAGE SKIN AT BS 947, STRINGER 17L DENTED. REPAIRED FUSELAGE SKIN PER EA. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND CHORD AT BS 662, RIGHT BUTTOCK LINE 69 CORRODED. REPAIRED CHORD PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 500B, RIGHT BUTTOCK LINE 20, LEFT BUTTOCK LINE 40 CORRODED. REMOVED AND REPLACED LOWER CHORD PER EA. (M)

Part: CHANNEL — CHAFED (NR 1 NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL U-CHANNEL AT NACELLE STATION 122.25 CHAFED. REMOVED DAMAGED U-CHANNEL AND FABRICATED REPAIRS PER SRM. (M)

Part: LONGERON — CORRODED (NR 2 NACELLE)

PAE - DURNG SCHEDULED C-CHECK, FOUND NR 2 ENGINE COWL LONGERON AT NACELLE STATION 154-184, CORRODED. REMOVED AND REPLACED NR 2 ENGINE COWL LONGERON PER SRM. (M)

Part: BEAM — GOUGED (NR 2 COWLING)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE COWL UPPER EDGE BEAM AT NACELLE STATION 188 GOUGED. REPAIRED DAMAGED COWL PER SRM. (M)

Part: FAIRING — GOUGED (NR 1 NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL FAIRING AT NACELLE STATION 137 GOUGED. REPAIRED DAMAGED COWL FAIRING PER SRM. (M)

Part: ANGLE — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND ANGLE AT BS 993, LEFT BUTTOCK LINE 14.5 CORRODED. REMOVED AND REPLACED ANGLE PER SRM. (M)

Part: RIB — GOUGED (NR 1 NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL RIB AT NACELLE STATION 99.25-116.5 GOUGED. REPAIRED DAMGAED COWL RIB PER SRM. (M)

Part: CHANNEL — GOUGED (NR 1 NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL CHANNEL AT NACELLE STATION 180 GOUGED. REPAIRED DAMAGED COWL CHANNEL PER SRM. (M)

Part: RIB — GOUGED (NR 1 NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL RIB AT NACELLE STATION 200.5 GOUGED. REPAIRED DAMAGED COWL RIB PER SRM. (M)

Part: RIB — GOUGED (NR 1 NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL RIB AT NACELLE STATION 173 GOUGED. REPAIRED DAMAGED COWL PER SRM. (M)

Part: SKIN — GOUGED (NR 1 NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL AT NACELLE STATION 150.25 GOUGED. REMOVED AND REPAIRED DAMAGED AREA PER SRM. (M)

Part: FRAME — GOUGED (NR 1 NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL FRAME AT NACELLE STATION 180 GOUGED. REPAIRED DAMAGED AREA PER SRM. (M)

Part: CHANNEL — CHAFED (NR 1 NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL U-CHANNEL AT NACELLE STATION 122.25-149.25 CHAFED. REMOVED AND REPAIRED DAMAGED AREA PER SRM. (M)

Part: RIB — GOUGED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL RIB AT NACELLE STATION 154 GOUGED. REPAIRED DAMAGED COWL AREA PER SRM. (M)

Part: SKIN — DENTED (NR 2 NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE COWL SKIN AT NACELLE STATION 109.25 DENTED. REMOVED DAMAGED AREA AND REPAIRED LEADING EDGE PER SRM. (M)

Part: SKIN — CRACKED (LT WING LE)

PAE - DURING SCHEDULED C-CHECK, FOUND LEFT WING LEADING EDGE AT WING STAITON 236-369 CRACKED .75 INCH AND CHAFED. REPAIRED LEADING EDGE PER SRM. (M)

Part: SKIN — DAMAGED (NA 1 NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL AT NACELLE STATION 192.65 WITH AN ELONGATED HOLE. REMOVED AND REPAIRED DAMAGED AREA PER SRM. (M)

Part: CHANNEL — CHAFED (NR 1 NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL CHANNEL AT NACELLE STATION 199.25 CHAFED. REMOVED AND REPLACED DAMGAED CHANNEL PER SRM. (M)

Part: GUSSET — GOUGED (NR 1 NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL GUSSET AT NACELLE STATION 218.67 GOUGED. REMOVED AND REPLACED DAMAGED GUSSET PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM FLANGE AT BS 986, LEFT BUTTOCK LINE 17-RIGHT BUTTOCK LINE 37 CORRODED. REMOVED CORROSION AND REPAIRED FLOORBEAM FLANGE PER EA. (M)

Part: SKIN — GOUGED (NR 2 NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE COWL FRAME AT NACELLE STATION 188.64 GOUGED. REMOVED DAMAGED FRAME SECTION AND REPAIRED PER SRM. (M)

Part: SKIN — GOUGED (NR 1 NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL SKIN AT NACELLE STATION 165.25 GOUGED. REMOVED DAMAGED SKIN AND REPAIRED PER SRM. (M)

Part: SKIN — GOUGED (NR 1 NACELLE)

DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL AT NACELLE STATION 205 GOUGED. REMOVED DAMAGE AND REPAIRED NR 1 ENGINE COWL PER SRM. (M)

Part: SKIN — CHAFED (HORIZONTAL STAB)

PAE - DURING SCHEDULED C-CHECK, FOUND LEFT HORIZONTAL STABILIZER AT ELEVATOR STATION 149.12 CHAFED. REMOVED DAMAGED HORIZONTAL STABILIZER WEB AND REPAIRED RIB PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM WEB AT BS 986-1016, RIGHT BUTTOCK LINE 40 RIGHT BUTTOCK LINE 45 CORRODED. REMOVED AND REPLACED FLOORWEB PER SRM. (M)

Part: SKIN — GOUGED (NR 2 NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE COWL AT NACELLE STATION 222.25 GOUGED. REMOVED DAMAGED AREA AND REPAIRED PER SRM. (M)

Part: RIB — GOUGED (NR 1 NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND RN 1 ENGINE COWL RIB AT NACELLE STATION 199 GOUGED. REMOVED DAMAGED AREA AND REPAIRED PER SRM. (M)

Part: SKIN — GOUGED (NR 1 NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL RIB AT NACELLE STATION 207.67 GOUGED. REMOVED DAMAGED AREA AND REPAIRED PER SRM. (M)

Part: CHANNEL — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL U-CHANNEL AT NACELLE STATION 170.25 CRACKED .25 INCH. REMOVED DAMAGED U-CHANNEL AND REPAIRED PER SRM. (M)

Part: BEAM — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND CREASE BEAM SUPPORT ANGLE AT BODY STATION 207, RIGHT BUTTOCK LINE 60 CORRODED. REMOVED AND REPLACED CREASE BEAM SUPPORT ANGLE PER SRM. (M)

Part: CHANNEL — CRACKED (NR 1 NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL SKIN AT NACELLE STATION 204.25 CRACKED .5 INCH. REMOVED DAMAGED SKIN SECTION AND REPAIRED PER SRM. (M)

Part: FAIRING — GOUGED (NR 1 NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE FIXED FAIRING PLATES AT NACELLE STATION 208.67 GOUGED. REMOVED AND REPLACED PLATES PER SRM. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND SUPPORT CHANNEL AT BS 994, LEFT BUTTOCK LINE 14-40 CORRODED. REMOVED AND REPLACED SUPPORT CHANNEL PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 1016, RIGHT BUTTOCK LINE 37, LEFT BUTTOCK LINE 38 CORRODED. REMOVED CORROSION AND REPAIRED FLOORBEAM PER SRM AND EA. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND SEAT TRACK AT BS 887-947, RIGHT BUTTOCK LINE 45.5 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM. (M)

Part: COWLING — GOUGED (NR 1 ENGINE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE TAILPIPE COWL AT THRUST REVERSER STATION 100 GOUGED. REPAIRED TAILPIPE COWL PER SRM. (M)

Part: STRAP — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND TENSION STRAP AT BS 328-334, RIGHT BUTTOCK LINE 48 CRACKED 1 INCH. REPAIRED TENSION STRAP PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 1006, LEFT BUTTOCK LINE 14, LEFT BUTTOCK LINE 23 CORRODED. REMOVED CORROSION AND REPAIRED FLOORBEAM PER SRM. (M)

Part: COWLING — GOUGED (NR 2 ENGINE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE EXHAUST COWL AT THRUST REVERSER STATION 102 GOUGED. REPAIRED NR 2 ENGINE EXHAUST COWL PER SRM. (M)

Part: SKIN — CHAFED (LT WING)

PAE - DURING SCHEDULED C-CHECK, FOUND LEFT WING LEADING EDGE AT WING STATION 361-494 CHAFED. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR PER SRM. (M)

Part: COWLING — GOUGED (NR 2 ENGINE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE COWL AT NACELLE STATION 139 GOUGED. REPAIRED NR 2 ENGINE COWL PER SRM. (M)

Part: COWLING — GOUGED (NR 2 ENGINE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE COWL AT NACELLE STATION 205 GOUGED. REPAIRED ENGINE COWL PER SRM. (M)

Part: COWLING — GOUGED (NR 2 ENGINE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE COWL AT NACELLE STATION 136 GOUGED. REPAIRED ENGINE COWL PER SRM. (M)

Part: COWLING — GOUGED (NR 2 ENGINE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE EXHAUST COWL AT THRUST REVERSER STATION 98 GOUGED. REPAIRED NR 2 ENGINE EXHAUST COWL PER SRM. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND INTERCOSTAL AT BS 312-328, RIGHT BUTTOCK LINE 32 CRACKED. REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL PER SRM. (M)

Part: SUPPORT FITTING — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND SUPPORT FITTING AT BS 344, LEFT BUTTOCK LINE 59 CORRODED. REMOVED CORRODED PART, FABRICATED AND INSTALLED NEW PART PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 328-344, RIGHT BUTTOCK LINE 11 CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FLOOR SUPPORT AT BS 328-344, LEFT BUTTOCK LINE 12 CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED NEW SUPPORT PER SRM. (M)

Part: SUPPORT FITTING — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND SUPPORT FITTING AT BS 312, LEFT BUTTOCK LINE 54 CORRODED. REMOVED CORRODED PART, FABRICATED AND INSTALLED NEW PART PER SRM. (M)

Part: COWLING — DAMAGED (NR 1 ENGINE)

PAE - DURING SCHEDULED C-CHECK, FOUND EXISTING REPAIR ON NR 1 ENGINE COWL AT NACELLE STATION 99.5 GOUGED. REMOVED PREVIOUS REPAIR, FABRICATED AND INSTALLED NEW REPAIR PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 328, RIGHT BUTTOCK LINE 11-45 CORRODED. REMOVED, FABRICATED AND INSTALLED UPPER CHORD PER SRM. (M)

Part: FLANGE — CHAFED (NR 2 COWLING)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE NOSE COWL MATING FLANGE AT NACELLE STATION 99.25 CHAFED. REPAIRED FLANGE PER SRM. (M)

Part: COWLING — GOUGED (NR 1 ENGINE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE COWL AT NACELLE STATION 181.25 GOUGED. REMOVED DAMAGE AND REPAIRED COWL PER SRM. (M)

Part: SKIN — DENTED (E/E BAY DOOR)

PAE - DURING SCHEDULED C-CHECK, FOUND E/E BAY DOOR AT BS 325-350, LEFT BUTTOCK LINE 6 RIGHT BUTTOCK LINE 14 DENTED. REMOVED AND REPLACED DAMAGED SKIN PER SRM. (M)

Part: COWLING — GOUGED (NR 2 ENGINE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE EXHAUST COWL AT NACELLE STATION 243.5 GOUGED. REMOVED DAMAGE AND REPAIRED COWL PER SRM. (M)

Part: COWLING — GOUGED (NR 1 ENGINE)

PAE - DURING SCHEDULED C-CHECK, FOUND NR 1 ENGINE TAILPIPE COWL AT THRUST REVERSER STATION 142.6 GOUGED. REMOVED DAMAGED AND REPAIRED COWL PER SRM. (M)

Part: PLATE — GOUGED (NR 1 COWLING)

PAE - DURING SCHEDULED C-CHECK,FOUND NR 1 ENGINE INBOARD COWL PLATE AT NACELLE STATION 180.75 GOUGED. REMOVED AND REPLACED PLATE PER SRM. (M)

Part: SPLICE — DAMAGED (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 16 WERE INOPERATIVE. REPAIRED WIRE SPLICE AT ROW 16 LIGHT ASSEMBLY. LIGHTS THEN OPERATED NORMALLY. (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: RECEIVER — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 18 WOULD NOT EXTINGUISH. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER THEN LIGHTS OPERATED NORMAL. (M)

Part: BATTERY — INOPERATIVE (AFT CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS IN THE AFT PORTION OF THE PASSENGER CABIN INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY (P/N 86210144) AND RECEIVER (P/N 883200312) THEN LIGHTS OPERATED NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROWS 19 AND 20 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY THEN LIGHTS OPERATED NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT IDENTIFIER ON SMOKE BARRIER INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY PACK AND EXIT IDENTIFIER ASSEMBLY, THEN EXIT IDENTIFIER OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT IDENTIFIER ON SMOKE BARRIER INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY PACK AND EXIT IDENTIFIER ASSEMBLY, THEN EXIT IDENTIFIER OPERATED NORMALLY. (M)

Part: RECEIVER — INOPERATIVE (CABIN)

SEA - EMERGENCY EXIT LIGHT RECEIVER NOT INDICATING AT SEAT PALLET G-9. REMOVED AND REPLACED EMERGENCY EXIT LIGHT RECEIVER (P/N 883200312) AND BATTERY PACK (P/N 8821004), THEN OPS CHECKED GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - EMERGENCY EXIT LIGHT RECEIVER NOT INDICATING AT SEAT PALLET G-9. REMOVED AND REPLACED EMERGENCY EXIT LIGHT RECEIVER (P/N 883200312) AND BATTERY PACK (P/N 8821004), THEN OPS CHECKED GOOD. REF ASAA0110639. (M)

Part: TIE CLIP — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON STRINGER TIE AT STATION 532 AND STRINGER 26R. REMOVED AND REPLACED STRINGER TIE IAW SRM. (M)

Part: STRINGER — DAMAGED (FUSELAGE)

PAE - DURING C-CHECK, FOUND DAMAGED STRINGER 12L AT STATION 1037.5. REPAIRED PER SRM. (M)

Part: SKIN — CORRODED (CARGO DOOR)

PAE - DURING C-CHECK, FOUND FORWARD CARGO DOOR INNER SKIN LOWER EDGE 26 IN FROM EDGE OF DOOR IS CORRODED. REPAIRED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT STATION 520 AND STRINGER 27L TO 28L. REPAIR IAW SRM. (M)

Part: FRAME — DENTED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FRAME DENT AT BS 500A BETWEEN STRINGER 24R AND 25R. REPAIRED IAW ENGINEERING REPAIR. (M)

Part: THRESHOLD — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON MAIN CARGO DOOR THRESHOLD WEB AT STATION 400-497. REMOVED AND REPLACED DAMAGED SECTION OF WEB PER SRM AND ENGINEERING REPAIR. (M)

Part: FRAME — DENTED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FRAME DENT AT STATION 420 AND STRINGER 24L. REPAIRED FRAME IAW SRM. (M)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CRACKED STRINGER CLIP AT BS 440 AND STRINGER 24L. REPLACED STRINGER CLIP PER SRM. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON STRINGER 35L CLIP AT BS 827 IN AFT CARGO BAY. REPLACED CLIP IAW SRM. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON STRINGER TIE AT STATION 533 AND STRINGER 27R. REPLACED STRINGER CLIP IAW SRM. (M)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CRACKED STRINGER CLIP AT STATION 440 AND STRINGER 24L. REPLACED STRINGER CLIP PER SRM. (M)

Part: SKIN — DENTED (FUSELAGE)

PAE - DURING C-CHECK, FOUND DENT ON EXTERNAL SKIN AT BS 1037.5 AND STRINGER 9L AND 21. REPAIRED SKIN IAW DOUBLER. (M)

Part: FRAME — DENTED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FRAME DENTED AT STRINGER 25R AND BS 727A. REPAIRED IAW SRM. (M)

Part: STRINGER — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON STRINGER 26R AND STATION 419. REPAIRED PER SRM. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON STRINGER TIE AT STATION 533 AND STRINGER 27L. REPAIRED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT STATION 520 BETWEEN STRINGER 26L AND 27L. REPAIRED SHEAR TIE IAW SRM. (M)

Part: WEB — DAMAGED (FUSELAGE)

PAE - DURING C-CHECK, FOUND SHEAR BEAM WEB TEMPORARY REPAIR AT STATION 727 LBL 65 AND WL 190. REPLACED SHEAR BEAM WEB IAW SRM. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON STRINGER CLIP AT BS 986.5 AND STRINGER 27R. REPLACED CLIP AND STRINGER IAW SRM. (M)

Part: FRAME — DENTED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FRAME DENT AT BS 400 AND STRINGER 24L. REPAIRED PER SRM. (M)

Part: ANGLE — CRACKED (CARGO DOOR)

PAE - DURING C-CHECK, FOUND FORWARD CARGO DOOR LOWER FRAME WEB OUTER SKIN ANGLE AT LOWER FORWARD DOOR STAY FITTING CRACKED. REPLACES WEB IAW EA. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON FORWARD SURFACE AFT FRAME OF AFT CARGO DOOR CUT OUT AT STRINGER 25R TO 23R. REPAIRED DAMAGED FRAME BY INSTALLING DOUBLER PER ENGINEERING REPAIR. (M)

Part: FRAME — DENTED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FRAME DENT AT STATION 500 BETWEEN STRINGER 24R AND STRINGER 25R. REPAIRED IAW SRM. (M)

Part: SILL — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON LEFT OVERWING EXIT SILL. REPLACED SILL IAW SRM. (M)

Part: FRAME — DENTED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FRAME DENT AT BS 500A BETWEEN STRINGER 24L AND 25L. REPAIRED IAW ENGINEERING REPAIR. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE -DURING C-CHECK FOUND CORROSION ON SHEAR TIE STATION 520 BETWEEN STRINGER 26L AND 27L. REPAIRED IAW SRM. (M)

Part: STRINGER — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON STRINGER 27R AT STATION 531. REPAIRED IAW SRM. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION AT FORWARD CARGO DOOR END FRAME 15 INCHES TO 34 INCHES FROM FORWARD EDGE. REPLACED IAW SRM. (M)

Part: STRINGER — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 27R AT BODY STATION 531-533, CORRODED. REPAIRED PER SRM. (M)

Part: TIE — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER TIE AT BODY STATION 727A, STRINGER 27L CORRODED. REPAIRED PER SRM. (M)

Part: RECEIVER — INOPERATIVE (CABIN)

ANC - DURING SCHEDULED MAINTENANCE CHECK, FOUND FLOOR TRACK LIGHTING AT SEAT PALLET 9 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER THEN LIGHTS TESTED NORMAL. (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: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROW 11 WERE SLOW TO RESPOND AND WOULD NOT EXTINGUISH. REMOVED AND REPLACED BATTERY PACK P/N 8821004, AND REMOTE ASSEMBLY RECEIVER P/N 883200312, THEN LIGHTS TESTED NORMAL. (M)

Part: RECEIVER — DEFECTIVE (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROW 11 WERE SLOW TO RESPOND AND WOULD NOT EXTINGUISH. REMOVED AND REPLACED BATTERY PACK P/N 8821004, AND REMOTE ASSEMBLY RECEIVER P/N 883200312, THEN LIGHTS TESTED NORMAL. REF ASAA0110571 (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS ON SEAT PALLET 10-3 AND SMOKE BARRIER WOULD NOT TEST. REMOVED AND REPLACED BATTERY PACK AND REMOTE ASSEMBLY BATTERY, THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS ON SEAT PALLET 10-3 AND SMOKE BARRIER WOULD NOT TEST. REMOVED AND REPLACED BATTERY PACK AND REMOTE ASSEMBLY BATTERY, THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTS AND EXIT LIGHTS ON THE SMOKE BARRIER WOULD NOT TEST AFTER AIRCRAFT RECONFIGURATION. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERIES ON THE SMOKE BARRIER AND THE AFT MOST SEAT PALLET, THEN LIGHTS OPERATED NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE ON SEAT PALLET 9-4, ROW 16. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AND RECEIVER, THEN LIGHTS TESTED NORMAL. REF ASAA0110208. (M)

Part: RECEIVER — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE ON SEAT PALLET 9-4, ROW 16. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AND RECEIVER, THEN LIGHTS TESTED NORMAL. (M)

Part: CONTROL HANDLE — DIRTY (COCKPIT)

ANC - AFTER DEPARTURE FROM ANC ON FLIGHT 45, THE LEFT MAIN GEAR FELL BACK DOWN BUT RETRACTED WHEN GEAR LEVER CYCLED BACK UP. FOUND GEAR HANDLE SHAFT DIRTY AND GUMMED UP. WHEN PULLED OUT IT WOULD NOT DROP INTO DETENTS. CLEANED HANDLE SHAFT AND LUBED, HANDLE TESTED WITH GEAR PINNED, HANDLE DROPS FREELY INTO DETENTS. ACCOMPLISHED GEAR SWING, OPS NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND AFT EMERGENCY EXIT IDENTIFIER INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AND SIGN WORKED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT ON SMOKE BARRIER WILL NOT TEST. REPLACED BATTERY AND RECEIVER, LIGHT OPERATED NORMAL. (M)

Part: RECEIVER — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT ON SMOKE BARRIER WILL NOT TEST. REPLACED BATTERY AND RECEIVER, LIGHT OPERATED NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND SMOKE BARRIER EMERGENCY EXIT LIGHT FAILS TEST. REPLACED SMOKE BARRIER EMERGENCY EXIT BATTERY, LIGHTS THEN TESTED NORMAL. (M)

Part: SKIN — MISMARKED (FUSELAGE)

YXD - DURING SCHEDULED MAINTENANCE, FOUND SKIN PANEL INSTALLED AT TIME OF MANUFACTURE, AT BODY STATION 727-908, STRINGER 14R-20R WAS INCORRECT PART NUMBER. (M)

Part: SILL — CRACKED (CARGO BAY)

YXD - DURING HEAVY MAINTENANCE, FOUND LOWER CARGO DOOR SILL CRACKED AT STATION 368, WATERLINE 208. REPAIRED PER EA 5310-01888. (M)

Part: HINGE — LACK OF LUBE (L2 DOOR)

ANC - DURING MAINTENANCE CHECK, FOUND L2 DOOR HARD TO OPEN. LUBED HINGES, DOOR OPERATED NORMALLY. (M)

Part: ACTUATOR — MALFUNCTIONED (NLG)

OTX-DURING FLIGHT 151 OME TO OTZ, CREW REPORTED NOSE GEAR FREE FALLS DOWN WHEN THE GEAR HANDLE PLACED IN OFF POSITION. CONTINUED FLIGHT TO OTZ, LANDED WITHOUT INCIDENT. A/C INSPECTED AND FERRIED TO ANC FOR REPAIRS, LANDED WITHOUT INCIDENT. SERVICED NOSE STRUT, LUBRICATED NOSE GEAR, REMOVED AND REPLACED NLG UPLOCK ACTUATOR. ACCOMPLISHED GEAR SWING, SYSTEM OPERATED NORMALLY. REMOVED NLG UPLINK ACTUATOR WAS SENT TO SHOP FOR INSPECTION AND/OR REPAIR.

Part: LATCH — LACK OF LUBE (PAX DOOR)

ANC-PRIOR TO FLIGHT 22 THE L1 DOOR WOULD NOT CLOSE. INSPECTED DOOR LATCHES FOR PROPER ALIGNMENT, CHECKS NORMAL. LUBRICATED LATCHES AND ROLLERS. THE L1 DOOR OPERATED NORMALLY.

Part: BATTERY PACK — DISCHARGED (MID CABIN) · airframe 56,388 hrs · 49,753 cycles

SEA - AFTER RECONFIGURATION OF THE AIRCRAFT, THE EMERGENCY EXIT LIGHTS FAILED CHECK. REPLACED BATTERY PACKS AND MID-TRANSMITTER, LIGHTS OPERATED NORMALLY. REF: OPER CNTRL NR 20001121SH007. (X)

Part: TRANSMITTER — INOPERATIVE (MID CABIN) · airframe 56,388 hrs · 49,753 cycles

SEA - AFTER RECONFIGURATION OF THE AIRCRAFT, THE EMERGENCY EXIT LIGHTS FAILED CHECK. REPLACED BATTERY PACKS AND MID-TRANSMITTER, LIGHTS OPERATED NORMALLY. REF: OPER CNTRL NR ASAA010132. (X)

Part: RECEIVER — INOPERATIVE (MID CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHTS AT ROWS 12, 18 AND SMOKE BARRIER DID NOT TEST PROPERLY. REPLACED BATTERY FOR SMOKE BARRIER AND ROW 18. REPLACED RECEIVER FOR ROW 12. ALL LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (MID CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHTS AT ROWS 12, 18 AND SMOKE BARRIER DID NOT TEST PROPERLY. REPLACED BATTERY FOR SMOKE BARRIER AND ROW 18. REPLACED RECEIVER FOR ROW 12. ALL LIGHTS OPERATED NORMALLY. (M)

Part: GUIDE — FROZEN (PAX DOOR)

SEA - PRIOR TO FLIGHT 61, THE L1 DOOR WAS FOUND TO BE HARD TO CLOSE. REPLACED THE GUIDE ARM AND ADJUSTED, DOOR OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (MID CABIN)

ANC - PRIOR TO FLIGHT 20, THE EMERGENCY FLOOR LIGHTING ILLUMINATED AT ROW 14. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: SNUBBER — INOPERATIVE (PAX DOOR)

ANC - PRIOR TO FLIGHT 148, THE L1 DOOR WAS DIFFICULT TO CLOSE. REPLACED SNUBBER AND DOOR OPERATED NORMALLY. (M)

Part: SKIN — DENTED (FUSELAGE)

PAE - DURING C-CHECK, A DENT WAS FOUND IN THE FUSELAGE SKIN AT BS 338, STRINGER 17L, BELOW THE FORWARD ENTRY DOOR. REPAIRED PER BFG ENGINEERING REPAIR NR 00-0887PB, BAC SRM. (M)

Part: FRAME — DAMAGED (FUSELAGE)

PAE - DURING C-CHECK, THE UPPER FUSELAGE FRAME STATION 480, STRINGER 5R, RBL 28, HOLES WERE FOUND TO HAVE SHORT EDGE MARGIN. REPAIRED PER EM 5310-01719. (M)

Part: BRACKET — DAMAGED (C DOOR ACTUATOR)

PAE - DURING C-CHECK, THE MAIN CARGO DOOR LATCH ACTUATOR MOUNTING BRACKET FASTENERS WERE PULLED THROUGH THE SKIN AT BS 430, WL 228. REPAIRED PER BFG ENGINEERING REPAIR NR 00-0860P3. (M)

Part: FRAME — CRACKED (BULKHEAD)

PAE - DURING C-CHECK, THE AFT VERTICAL BULKHEAD BS 727 LEFT OUTBOARD CHORD CRACKED. REPAIRED PER EM 5310-01380. (M)

Part: DOUBLER — CRACKED (BEARSTRAP)

PAE - DURING SCHEDULED C-CHECK, A CRACK WAS FOUND IN THE BEARSTRAP AT THE FORWARD UPPER CORNER OF THE MAIN CARGO DOOR CUTOUT. REPAIRED PER BFG ENGINEERING REPAIR NR 00-0903P3 AND BOEING TELEX BFG-PAN-00-01150H. (M)

Part: BATTERY — DISCHARGED (EXIT SIGN)

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

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 2, 3, AND 14 WOULD NOT TEST. REPLACED BATTERIES AT ROWS 2 AND 14. REPLACED RECEIVER AT ROW 3, ALL LIGHTS OPERATED NORMALLY. (M)

Part: RECEIVER — INOPERATIVE (ROWS 2,3 & 14)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 2, 3 AND 14 WOULD NOT TEST. REPLACED BATTERIES AT ROWS 2 AND 14. REPLACED RECEIVER AT ROW 3, ALL LIGHTS OPERATED NORMALLY. REF ASAA0010078.(M)

Part: BATTERY PACK — DISCHARGED (ROW 12)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 12 WILL NOT TEST PROPERLY. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (M)

Part: LIGHT — MALFUNCTIONED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE R2 DOOR EMERGENCY EXIT IDENTIFIER WAS FOUND TO BE DIM. REPLACED LIGHTS ASSEMBLY AND LIGHT OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (ROW 27)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROW 27 REMAINED ILLUMINATED. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (ROW 12)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 12. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

SEA - AFTER RECON AND PRIOR TO FLIGHT 65, THE SMOKE BARRIER EXIT IDENTIFIER AND THE EMERGENCY EXIT LIGHTS AT ROWS 12 AND 18 WOULD NOT TEST PROPERLY. REPLACED SMOKE BARRIER BATTERY AND 2 EACH RECEIVERS, ALL LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (EXIT LIGHT)

SEA - AFTER RECON AND PRIOR TO FLIGHT 65, THE SMOKE BARRIER EXIT IDENTIFIER AND THE EMERGENCY EXIT LIGHTS AT ROWS 12 AND 18 WOULD NOT TEST PROPERLY. REPLACED SMOKE BARRIER BATTERY AND 2 EACH RECEIVERS, ALL LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - PRIOR TO FLIGHT 65, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 12, 16, AND 18 WERE FOUND TO BE INOPERATIVE. REPLACED 3 EACH BATTERY PACKS AND 1 EACH RECEIVER AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - PRIOR TO FLIGHT 65, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 12, 16, AND 18 WERE FOUND TO BE INOPERATIVE. REPLACED 3 EACH BATTERY PACKS AND 1 EACH RECEIVER AND LIGHTS OPERATED NORMALLY. (M)

Part: STRINGER — CRACKED (FUSELAGE)

PHX - DURING SCHEDULED MAINTENANCE CHECK, FOUND AFT PIT STRINGER AT STATION 847 CRACKED. REMOVED, FABRICATED AND REPLACED SECTION OF STRINGER 19R PER SRM. (M)

Part: BATTERY — DISCHARGED (ROW 16)

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

Part: GUIDE ARM — OUT OF ADJUST (L2 DOOR)

ANC - PRIOR TO FLIGHT 146, THE L2 DOOR WAS FOUND TO BE DIFFICULT TO CLOSE AND LATCH. ADJUSTED GUIDE ARM AND DOOR OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND INOPERATIVE AT PALLETS 3-10 AND 7-4. REPLACED BATTERY PACKS AND LIGHTS OPERATED NORMALLY. (X)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE ON PALLET 8-7. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE SMOKE BARRIER STROBE LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (X)

Part: BATTERY PACK — DISCHARGED (ROW 18)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHT TEST FAILED ON PALLET AT ROW 18. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - PRIOR TO FLIGHT 152, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE ON THE 3RD PALLET FROM AFT. REPLACED BATTERY IN AFT TRANSMITTER AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (ROW 17)

ANC - PRIOR TO FLT 147, TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. CHECKED AND RELEASED PER MEL 33-19A. SUBSEQUENTLY REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X)

Part: BEARING — LOOSE (RT WINDOW)

SEA - FLT 887 - PRIOR TO FLIGHT, CREW REPORTED THAT THE F/O'S SIDE WINDOW WOULD NOT CLOSE. INSPECTED AND FOUND LOWER FORWARD BEARING LOOSE. REPLACED BEARING AND WINDOW OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - FLT 43 - PRIOR TO FLIGHT, CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTS ILLUMINATED WHEN THE LIGHT SWITCH WAS IN THE 'OFF' POSITION. REPLACED BATTERY PACK ON PALLET 7-4, AND LIGHTS OPERATED NORMALLY. (X)

Part: SKIN — CORRODED (BS 787-907)

PDX - DURING D-CHECK, FOUND THE EXTERNAL FUSELAGE SKIN FROM BS 787 TO BS 907, STR 20R TO STR 26R LIGHTLY PITTED WITH CORROSION. REPAIRED PER SRM 51-10-1 AND SRM 51-30-2. (X)

Part: SEAT TRACK — CORRODED (BS 727)

PHX - DURING D-CHECK, FOUND THE MAIN CABIN SEAT TRACK CORRODED ON TOP AND BOTTOM SIDES, BS 727B-747, BL 0. REPAIRED PER SRM 53-10-1. (M)

Part: STRINGER — CORRODED (BS 962)

PHX - DURING D-CHECK, FOUND AFT CARGO PIT STRINGER 24R, AT APPROXIMATELY BS 962, CORRODED. REPAIRED PER SRM 53-10-3. (X)

Part: FLOORBEAM — CORRODED (BS 727)

PDX - DURING C-CHECK, FOUND THE PASSENGER CABIN STUB FLOORBEAM CORRODED AROUND FASTENER HOLES ON TOP SIDE, BS 727, RBL 54.0. REPAIRED PER DWG 65-46547; SRM 53-10-1. (X)

Part: STRINGER — CORRODED (BS 947-987)

PHX - DURING C-CHECK, FOUND AFT CARGO PIT STR 27L CORRODED FROM BS 947 TO BS 987. REPAIRED PER SRM 53-10-2, FIG 9. (X)

Part: SKIN — GOUGED (BS 907)

PHX - DURING C-CHECK, FOUND EXTERNAL FUSELAGE SKIN AT BS 907, STR 10L, GOUGED. REPAIRED PER SRM 53-30-3, FIG. 16. (X).

Part: DOUBLER — MISDRILLED (BS 847)

PHX - DURING D-CHECK, FOUND DOUBLE HOLES IN AFT CARGO DOOR, AFT FRAME SKIN DOUBLE FROM STRINGER 20 TO 24 RT, BS 847. REPAIRED PER EA 5330-01377. (M)

Part: FRAME — CORRODED (BS 727)

PHX - DURING D-CHECK, FOUND EXTERNAL FUSELAGE, LOWER SIDE FRAME AT STA 727 FROM STR 26L TO STR 26R CORRODED ON BOTTOM SIDE. REPAIRED PER SRM 51-30-2. (X)

Part: FRAME — CORRODED (BS 987)

PHX - DURING D-CHECK, FOUND AFT CARGO PIT FRAME AT BS 987 CORRODED FROM STR 18L TO STR 18R. REPAIRED PER SRM 51-30-2. (X)

Part: STRINGER — CORRODED (BS 365)

PHX - DURING D-CHECK, FOUND STRINGER 27R AND ADJACENT SKIN CORRODED AT BS 365. REPAIRED PER SRM 51-10-3. (M)

Part: STRINGER — CORRODED (BS 322-326)

PHX - DURING D-CHECK, FOUND STR 26R, BS 322 TO BS 326, CORRODED. REPAIRED PER SRM 53-10-3. (X)

Part: STRINGER — CORRODED (BS 294.5)

PHX - DURING D-CHECK, FOUND STR 25R, BS 294.5 TO BS 348, CORRODED. REPAIRED PER SRM 53-10-3. (X)

Part: SUPPORT — CRACKED (BS 332-344)

PHX - DURING D-CHECK, FOUND THE R-1 SERVICE DOOR FRAME SUPPORT, TOP AFT LOCATION 332 RT CRACKED. REPAIRED PER SB 737-53-1108, REV 5. (X)

Part: SUPPORT — CORRODED (BS 580-727)

PHX - DURING D-CHECK, FOUND THE LONGITUDINAL SEAT TRACK SUPPORTS CORRODED AT BS 580 - BS 727B, LBL 24.5, BL ZERO, RBL 24.5 AND RBL 45.5. REPAIRED PER EA 5320-01373. (X)

Part: SKIN — GOUGED (BS 685)

PHX - DURING D-CHECK, FOUND THE FUSELAGE AT STA 685 BETWEEN STR 4L AND STR 5L GOUGED. REPAIRED PER SRM 53-30-3, FIG 2. (X)

Part: SEAT TRACK — CORRODED (BS 540)

PHX - DURING D-CHECK, FOUND THE MAIN CABIN SEAT TRACK CORRODED AT BS 540, LBL65. REPAIRED PER SRM 53-10-5, FIG 7. (X)

Part: SKIN — CORRODED (BS 727-887)

PHX - DURING D-CHECK, FOUND THE EXTERNAL FUSELAGE SKIN FROM BS 727 TO BS 887, STR 25L TO STR 25R LIGHTLY PITTED WITH CORROSION. REPAIRED PER EA 5330-01378. (X)

Part: SEAT TRACK — GOUGED (BS 864.5)

PHX - DURING D-CHECK, FOUND THE MAIN CABIN SEAT TRACK GOUGED BS 864.5, LBL 45.5. REPAIRED PER SRM 53-10-5, FIG 8. (M)

Part: SEAT TRACK — CORRODED (BS 727)

PHX - DURING D-CHECK, FOUND THE PASSENGER CABIN SEAT TRACK CORRODED ON TOP AND BOTTOM SIDES AT BS 727A TO BS 727B, RBL 62.5. REPAIRED PER SRM 53-10-5, FIG 7. (X)

Part: STRINGER — CORRODED (BS 906)

PHX - DURING 'D' CHECK, FOUND OUTBOARD SIDE OF STRINGER 25L AT STATION 906 CORRODED. REPAIRED PER SRM 51-40-2. (M)

Part: T-CHORD — CORRODED (BS 351.2-360)

PHX - DURING D-CHECK, FOUND THE E/E COMPARTMENT T-CHORD COMMON TO STR 27R CORRODED FROM STA 351.20 TO STA 360. REPAIRED PER EA 5310-01691. (X)

Part: KEEL BEAM — CORRODED (BS 727)

PHX - DURING D-CHECK, FOUND THE EXTERNAL FUSELAGE LOWER SIDE, KEEL BEAM 27L BETWEEN STA 727 - STA 727A CORRODED ON BOTTOM SIDE. REPAIRED PER EA 5310-01687. (X)

Part: KEEL BEAM — CORRODED (BS 727)

PHX - DURING D-CHECK, FOUND THE EXTERNAL FUSELAGE LOWER SIDE, KEEL BEAM 27R BETWEEN STA 727 - STA 727A CORRODED ON BOTTOM SIDE. REPAIRED PER EA 5310-01687. (X)

Part: BULKHEAD CHORD — DAMAGED (BS 178)

PHX - DURING D-CHECK, FOUND BS 178 BULKHEAD VERTICAL CHORD, LBL 5.7 AND WL 195, PUNCTURED AND CRACKED. REPAIRED PER SRM 53-10-11, FIG 8. (X)

Part: SKIN — DENTED (BS 827)

PHX - DURING 'D' CHECK, FOUND EXTERNAL FUSELAGE SKIN AT BS 827, STRINGER 20L DENTED WITH RIPPLES GOING AFT. REPAIRED PER SRM 53-30-3, FIG 1. (M)

Part: STRINGER — CORRODED (BS 927)

PHX - DURING D-CHECK, FOUND STRINGER 21R CORRODED BEYOND LIMITS AT BS 927. REPAIRED PER SRM 53-10-3, FIG 1. (M)

Part: FLOORBEAM — CORRODED (BS 727)

PHX - DURING D-CHECK, FOUND THE MAIN CABIN FLOORBEAM CORRODED ON TOP AND BOTTOM SIDES OF FLANGE AT BS 727B, BL ZERO TO 56. REPAIRED PER SRM 51-40-3. (X)

Part: BEAM — CORRDOED (BS 663)

PHX - DURING D-CHECK, FOUND THE PASSENGER CABIN FLOOR SUPPORT I BEAM CORRODED ON TOP AND BOTTOM SIDES, BS 663, RBL 45.5 TO 61.0. REPAIRED PER SRM 51-30-2 AND 51-30-3. (M)

Part: SKIN — CRACKED (BS 422-426)

PHX - DURING D-CHECK, FOUND EXTERNAL SKIN CENTER LINE BS 422 TO 426 BETWEEN STRINGER 28L AND 28R CRACKED. REPAIRED PER SRM 53-30-3 AND 53-30-4. (M)

Part: SNUBBER — INOPERATIVE (L2 DOOR)

ANC - PRIOR TO FLT 22, THE LT AFT ENTRY DOOR HANDLE WAS DIFFICULT TO OPERATE. REPLACED SNUBBER AND LUBRICATED DOOR, DOOR OPERATED NORMALLY. ACFT TT: 51,541 HOURS. ACFT TC: 45,577. (X)

Part: PIN — CRACKED (COCKPIT WINDOW)

ANC - FLT 147 - THE CAPTAINS SLIDING WINDOW WAS FOUND TO BE HARD TO CLOSE. INSPECTED AND FOUND THE GUIDE PIN CRACKED. REPLACED THE CAPTAINS SLIDING WINDOW AND THE WINDOW OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

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

Part: BATTERY — DISCHARGED (ROW 12)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 12. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - PRIOR TO FLT 124 - THE EMERGENCY EXIT FLOOR TRACK LIGHTS ILLUMINATED. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FIRST CLASS EMERGENCY EXIT FLOOR TRACK LIGHT LEFT TRANSMITTER WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 2 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - FL 43 - DURING PREFLIGHT, CREW REPORTED THAT THE EMERGENCY EXIT TRACK LIGHTS AT PALLET 6-2 WOULD NOT EXTINGUISH AFTER TEST. REPLACED BATTERY PACK AT PALLET 6-2 AND LIGHTS OPERATED NORMALLY. (M)

Part: ANGLE — CRACKED (BS 540)

SEA - DURING C-CHECK, CRACKS WERE FOUND IN THE LEFT UPPER WING TO BODY DRAG ANGLE AND FRAME SPLICE ANGLE. REPLACED ANGLE PER EA 5310-01572. (M)

Part: FLOORBEAM — CORRODED (BS 500)

SEA - DURING C-CHECK. FOUND CORROSION WAS FOUND IN THE LOWER FORWRD FLANGE OF THE FLOORBEAM AROUND A FASTENER HOLE AT STATION 500, LBL 9. REPAIRED PER EA 5310-01579. (M)

Part: RIB — WORN (HORIZ STABILIZER)

SEA - DURING C-CHECK, WEAR WAS FOUND AT THE HORIZONTAL STABILIZER TRAILING EDGE RIBS AT STATION 66.54, 94.07, AND 121.9. REPAIRED PER EA 5510-01066 AND BOEING TELEX'S ASA-SEA-91-0202RR AND ASA-SEA-97-004RR. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - FLT 30 - PRIOR TO FLT, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT PALLET POSITION 9. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY EXIT LIGHTS WERE FOUND TO BE DIM. REPLACED BATTERY TO SMOKE BARRIER LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ANC - DURING MAINTENANCE CHECK, AN EMERGENCY EXIT FLOOR TRACK LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 20. RELEASED PER MEL 33-19. SUBSEQUENTLY REPAIRED LIGHT ASSEMBLY AT ROW 20 AND LIGHT OPERATED NORMALLY. (M)

Part: MECHANISM — LACK OF LUBE (L2 DOOR)

ANC - DURING MAINTENANCE CHECK, THE L2 DOOR WAS FOUND DIFFICULT TO MOVE THROUGH FULL TRAVEL OF OPEN TO CLOSE. CLEANED AND LUBRICATED L2 DOOR AND DOOR OPERATED NORMALLY. ACFT TT: 48,253 HOURS. ACFT TC: 42,759. (X)

Part: LATCH MECHANISM — LACK OF LUBE (L2 DOOR)

ANC - FLT 46 - DURING GROUND OPERATIONS, THE LEFT AFT ENTRY DOOR, AIRSTAIR WAS VERY DIFFICULT TO CLOSE. INSPECTED LEFT AFT DOOR HINGE AND LATCH MECHANISM, NO DEFECTS NOTED. LUBED DOOR HINGES AND LATCH MECHANISM, DOOR OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (CABIN)

ANC - DURING RECON, FOUND THE LAST FIVE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE. REPAIRED BROKEN WIRE AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHTS ON PALLET 4-5 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: MODULE — INOPERATIVE

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS CYCLED ON AND OFF. REPLACED FORWARD CONTROL MODULE AND LIGHTS OPERATED NORMALLY. (M)

Part: RECEIVER — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT PALLET 2. REPLACED BATTERY AND RECEIVER AND LIGHTS OPERATED NORMALLY. REFERENCE ASAA9710029.

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT PALLET 2. REPLACED BATTERY AND RECEIVER AND LIGHTS OPERATED NORMALLY. (M)

Part: TRANSMITTER — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE MID CABIN EMERGENCY EXIT FLOOR TRACK LIGHT TRANSMITTER WAS FOUND TO BE INOPERATIVE. REPLACED TRANSMITTER AND LIGHTS OPERATED NORMALLY. (M)

Part: SLIDE BOTTLE — LOW PRESSURE (L1 DOOR)

SEA - DURING SCHEDULED MAINTENANCE, THE L1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE EMERGENCY EVACUATION SLIDE. (M)

Part: SUPPORT BEAM — WORN (RIGHT MLG)

SEA - DURING C-CHECK, THE RIGHT MAIN LANDING GEAR SUPPORT BEAM WAS IDENTIFIED WITH A WEAR MARK ON THE RIGHT SIDE UPPER FLANGE, FORWARD EDGE. REPAIRED PER EA 5740-01126 AND BOEING TELEX ASA-SEA-97-0037RR. (M)

Part: FLOOR BEAM — CORRODED (BS 1006)

SEA - DURING C-CHECK, THE FLOOR BEAM UPPER FORWARD FLANGE AT BS 1006 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01508 AND BOEING TELEX ASA-SEA-97-0038RR. (M)

Part: FLOOR BEAM — CORRODED (BS 344)

SEA - DURING C-CHECK, THE FLOOR BEAM UPPER FORWARD FLANGE AT BS 344 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01509 AND BOEING TELEX ASA-SEA-97-0039RR. (M)

Part: EVAC SLIDE — WORN (L1 DOOR)

SEA - DURING CHECK, THE FORWARD ENTRY DOOR EMERGENCY ESCAPE SLIDE GIRT LOWER SIDE WAS FOUND TO BE WORN IN FABRICATED. REPLACED FORWARD ENTRY DOOR EMERGENCY ESCAPE SLIDE. (M)

Part: CHORD — CRACKED (BS 727)

SEA - DURING C-CHECK, THE COMPENSSION CHORD AT BS 727 WAS FOUND CRACKED IN THE RADIUS AT BL 0.0. COMPLETED INTERMIN REPAIR PER EA 5310-01506 AND BOEING SERVICE BULLETIN 737-53-1072. CHORD REQUIRES REPLACEMENT AT NEXT D-CHECK. (M)

Part: SKIN — CRACKED (BS 380)

SEA - DURING C-CHECK, THE FUSELAGE SKIN WAS FOUND CRACKED AT THE AFT END OF THE CUTOUT FOR THE COOLING EXHAUST DUCT, BS 380, BL 0. REPAIRED PER EA 5330-01275 AND BOEING SERVICE BULLETIN 737-53-1117. (M)

Part: HINGES — LACK OF LUBE (L1 DOOR)

SEA - FLT 65 - PRIOR TO DEPARTURE, CREW REPORTED THE L1 DOOR WAS HARD TO CLOSE. MAINTENANCE CLEANED AND LUBED THE UPPER AND LOWER DOOR HINGES, AND THE DOOR OPERATED NORMALLY. (M)

Part: RECEIVER — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT WERE FOUND TO BE INOPERATIVE AT ROW 14. REPLACED RECEIVER AND LIGHTS OPERATED NORMALLY. (M)

Part: KEEL BEAM — CORRODED (BS 500)

SEA - DURING NON ROUTINE MAINTENANCE INSPECTION, CORROSION WAS FOUND ON THE KEEL BEAM LOWER CHORD AT THE FORWARD PRODUCTION SPLICE WITH STRINGER 28R, BS 500. REPAIRED PER B737-200 SRM 53-10-3, ASA EA 5310-01404 AND BOEING TELEX ASA-SEA-96-0078RR. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 5 WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: UPLOCK SENSOR — OUT OF ADJUST (NLG)

SEA - AIR TURN BACK OF FLT 65 - CREW REPORTED, THE NOSE LANDING GEAR UNSAFE LIGHT ON WITH GEAR HANDLE IN OFF POSITION, EXTINGUISHES WITH GEAR HANDLE IN UP POSITION. CYCLED GEAR AND GOT SAME RESULTS. FOUND NOSE LANDING GEAR UPLOCK SENSOR ADJUSTED TO MAXIMUM LIMIT. ADJUSTED SENSOR TO MINIMUM LIMIT AND ACCOMPLISHED GEAR SWING, OPERATION AND INDICATION NORMAL. (M)

Part: MIDFLAP — WORN SKIN (WS 254)

SEA - DURING C-CHECK, A WEAR MARK WAS FOUND ON THE RIGHT MIDFLAP LOWER WING SKIN AS A RESULT OF RUBBING ON THE NR 7 FLAP TRACK FAIRING WHEN THE FLAPS ARE RETRACTED. REPAIRED PER EA 5750-01195 AND BOEING TELEX ASA-SEA-96-0008RR DATED 1/8/96. (M)

Part: ANGLE — CRACKED (BS 727)

SEA - DURING C-CHECK, A 1 INCH CRACK WAS FOUND ON THE BS 727 FORMED ANGLE COMPRESSION CHORD AT RBL 25. REPAIRED PER EA 5310-01390. (M)

Part: SPAR — CRACKED (LT ELEV)

SEA - DURING C-CHECK, THE REAR SPAR AT THE INBOARD HINGE FITTING FOR THE LEFT ELEVATOR TAB WAS FOUND CRACKED. REPAIRED PER EA 5520-01031. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 8 AND 9. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - ON ARRIVAL OF FLT 87, CREW REPORTED EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 6 AND 7 COME ON INADVERTENTLY. UNABLE TO DUPLICATE PROBLEM. REPLACED BATTERY PACK AS PRECAUTIONARY MEASURE AND LIGHTS OPERATED NORMALLY. (X)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

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

Part: EEL BATTERY — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS ON SEAT PALLET 5-8 WERE FOUND INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

SEA - FLT 7958 - SMOKE BARRIER EMERGENCY EXIT LIGHT ILLUMINATED ON THE GROUND. REPLACED BATTERY PACK AND LIGHT OPERATED NORMALLY. (M)

Part: EEL BATT PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER 'EXIT TO REAR' EMERGENCY LIGHTS WERE FOUND TO BE DIM. REPLACED BATTERY PACK ON SMOKE BARRIER AND LIGHTS OPERATED NORMALLY. (Z)

Part: EEL BATT PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS ON SEAT PALLET 7 TO 10 WOULD NOT EXTINGUISH. REPLACED BATTERY PACK TO RECEIVER AND LIGHTS OPERATED NORMALLY. (Z)

Part: EEL — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER 'EXIT TO REAR' LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSY AND OPERATED NORMALLY. (W)

Part: LOCK RING — MISSING (L-1 DOOR)

OME - FLT 51 - CREW REPORTED, UNABLE TO OPEN L-1 DOOR. FOUND LOCK RING MISSING FROM UPPER GUIDE ARM. REPLACED RING AND DOOR OPERATED NORMALLY. (W)

Part: EEL LAMP — FAILED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS ON PALLET 7 TO 5 AND 8 TO 7 WERE FOUND INOPERATIVE. RELAMPED AND LIGHTS OPERATED NORMALLY. (W)

Part: LOCK ACTUATOR — MALFUNCTIONED (NLG)

ANC - FLT 145 - DURING APPROACH ON GEAR EXTENSION THE NOSE GEAR REMAINED UP. RECYCLED GEAR AND ALL LANDING GEAR EXTENDED. MAINTENANCE REPLACED THE NOSE GEAR HYDRAULIC MODULE AND THE NOSE GEAR LOCK ACTUATOR. NOSE GEAR RETRACTED AND EXTENDED NORMALLY ON GEAR SWING PER BOEING MM. REF 95ZZZW107.

Part: LANDINIG GEAR MO — MALFUNCTIONED (NLG)

ANC - FLT 145 - DURING APPROACH ON GEAR EXTENSION THE NOSE GEAR REMAINED UP. RECYCLED GEAR AND ALL LANDING GEAR EXTENDED. MAINTENANCE REPLACED THE NOSE GEAR HYDRAULIC MODULE AND THE NOSE GEAR LOCK ACTUATOR. NOSE GEAR RETRACTED AND EXTENDED NORMALLY ON GEAR SWING PER BOEING MM. REF ASAA9537.