N746AS

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 61,760 hrs · 57,226 cycles

L 1 DOOR EMERGENCY LIGHTS INOP. REPLACED BATTERY, NO HELP CHANGED OUT EXIT LIGHT ASSY.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 61,713 hrs · 57,180 cycles

L1 DOOR INTERIOR EMERGENCY LIGHT INOP. REPLACED PATTERY PACK.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 61,581 hrs · 57,066 cycles

L 1 DOOR EMERGENCY FLASHLIGHT DEAD. REPLACED EMERGENCY FLASHLIGHT BATTERY IAW AMM.

Part: DOOR LATCH — BROKEN (L1 DOOR) · airframe 61,543 hrs · 57,030 cycles

L1 DOOR RELEASE LATCH BROKEN. REPLACED L1 DOOR RELEASE LATCH PER SRM 51-11-21, OPS GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 61,543 hrs · 57,030 cycles

L1 DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 61,011 hrs · 56,510 cycles

L1 AND RT OVERWING EXIT LIGHTS DIM. REPLACED BATTERIES ON L1 AND RT EMERGENCY EXIT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,867 hrs · 56,363 cycles

AFTER RECON TO ALL SEATS L1 AND R1 DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BOTH BATTERY PACKS.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 60,769 hrs · 56,261 cycles

FOUND L2 DOOR EMERGENCY LIGHT AREA LIGHT INOP. REPLACED BATTERY PACK FUNCTION NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 60,769 hrs · 56,261 cycles

EXIT ROW LT SIDE EXIT LIGHT UNDER WINDOW FLASHING STROBE. CYCLED EMERGENCY LIGHTS SWITCH TO OFF THEN BACK TO ARM AND LIGHT STOPPED FLASHING. REPLACED BATTERY PACK OPS NML.

Part: SKIN — CRACKED (BS 1138-1156) · airframe 60,683 hrs · 56,183 cycles

TWO EACH CRACKS FOUND FWD OF BSTA 1156 BETWEEN S2 AND S3 RT. CRACK LENGTH 1.4 INCH CIRCUMFERENTIALLY AND 1 INCH RADIAL. INSTALLED DOUBLER PER ASA EA 5330 02112.

Part: BATTERY — DISCHARGED (BARRIER LIGHT) · airframe 60,352 hrs · 55,869 cycles

DURING RECON 3 PALLET TO 2 PALLET, FOUND SMOKE BARRIER EXIT LIGHT INOP. REPLACED BATTERY PACK PER AMM 33 50 00, OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 46,852 hrs · 26,813 cycles

FOUND R2 DOOR LOWER EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 60,084 hrs · 55,623 cycles

FOUND LT AND RT OVERWING EMERGENCY EXIT LIGHTS ARE DIM. REPLACED BATTERY PACK, OPS CHKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,084 hrs · 55,623 cycles

FOUND LT AND RT OVERWING EMERGENCY EXIT LIGHTS DIM. REPLACED BATTERY PACK OPS CHKS GOOD.

Part: HOSE — SHEARED (OXYGEN SYSTEM) · airframe 59,958 hrs · 55,508 cycles

OXYGEN SUPPLY HOSE TO PSU'S ON MAIN CARGO DOOR FOUND BROKEN. ACCOMPLISHED INTERM REPAIR WITH ALTERNATE HOSE PER EA 3520 01023.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 59,856 hrs · 55,408 cycles

R1 AND R2 DOOR EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK.

Part: LIGHT — INOPERATIVE (RT OVERWING EXIT) · airframe 59,856 hrs · 55,408 cycles

AFTER RECON RIGHT OVERWING PEOPLES EXIT SIGN INOP. REPLACED LIGHT ASSY.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 59,819 hrs · 55,371 cycles

R1 AND R2 DOOR EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED BATTERY PACKS PER AMM 33-5-00-20 FIG 20 ASA SHEET 2.

Part: LIGHT — NONE (CABIN) · airframe 59,856 hrs · 55,408 cycles

R2 EMERGENCY LIGHT INOP LIGHT PLACED ON MEL. OPS TESTED EMERGENCY EXIT LIGHT AND FOUND IT TO BE OPERATING OK REF MM 33-51-01. CLEARS MEL 33 15A.

Part: BATTERY PACK — WEAK (R-1 DOOR) · airframe 59,742 hrs · 55,304 cycles

EMERGENCY LIGHT BY R1 DOOR REMAINS ON. MAINTENANCE REMOVED AND REPLACED BATTERY PACK PER AMM 33 50 00 17 PG 0 FIG 17.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 59,528 hrs · 55,118 cycles

R1 DOOR AND BOTH OVERWING EMERGENCY LIGHTS WILL NOT ILLUM STEADY. REPLACED BATTERIES, OPS NML PER AMM 33 50 01.

Part: FRAME — DENTED (BS 440) · airframe 59,503 hrs · 55,095 cycles

FUSELAGE FRAME DENTED AT SHEAR TIE LOCATION ABOVE STR 21L BS 440. FUSELAGE FRAME AT SHEAR TIE LOCATION ABOVE STR 21L, AT BSTA 440, REPAIRED IAW SRM 53-10-4, FIG 6.

Part: SHEAR TIE — BENT (BS 440) · airframe 59,507 hrs · 55,097 cycles

BS 440 SHEAR TIE ANGLE AFT OF FRAME FOOT ABOVE STR 21L BENT. BSTA 440 SHEAR TIE ANGLE ABOVE STR 21L REPAIRED IAW EA 5330-02044.

Part: SKIN — GROUND DAMAGE (BS 360-440) · airframe 59,503 hrs · 55,095 cycles

AIRCRAFT STRUCK BY FMC LOADER BELOW MAIN CARGO DOOR. DAMAGE IS TO STR 21L AT BS 360-440. AIRCRAFT SKIN AT BS 360 TO 440 STR 21L REPAIRED IAW EA 5330-02044.

Part: STRINGER — CRACKED (BS 440) · airframe 59,503 hrs · 55,095 cycles

FOUND STRINGER 21L CRACKED AT BS 440 AT FRAME LOCATION. STR 21L, BS 440, REPAIRED IAW EA 5330-02044.

Part: FAILSAFE — CRACKED (BS 440) · airframe 59,503 hrs · 55,095 cycles

BS 440 FAILSAFE ANGLE CRACKED AT STR 21L. FAILSAFE ANGLE AT BS 440, STR 21L, REPAIRED IAW EA 5330-02044.

Part: SKIN PANEL — CORRODED (BS 618-635) · corrosion level 2 · airframe 59,021 hrs · 54,683 cycles

CORROSION ON INTERNAL SURFACE OF SKIN PANEL BETWEEN KEEL BEAMS AT BSTA 618 TO 635. REPLACED PANEL WITH FABRICATED REPAIR PART IAW ERO AND EA. (K)

Part: ATTACH ANGLE — CRACKED (BS 348.2) · airframe 59,021 hrs · 54,683 cycles

2 EA CRACKS FOUND AT STOP FITTING FASTENER HOLES AT BS 348.2, S16L. REPLACED INTERCOSTAL ATTACH ANGLE AND WEB FLANGE IAW EA. (K)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

ANC - FOUND ALL FOUR DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED L-1, L-2, R-1 AND R-2 EMERGENCY EXIT LIGHT BATTERY PACKS PER AMM 33-50-0. (M)

Part: BATTERY PACK — DISCHARGED (OVERWING EXITS)

ANC - AFTER PAX CABIN RECONFIG, LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED LEFT AND RIGHT OVERWING EXIT EMERGENCY EXIT LIGHT BATTERY PACKS. OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

ANC - FOUND RIGHT OVERWING LOWER EMERGENCY LIGHT LENS WILL NOT STAY SECURED. LIGHT ALSO INOPERATIVE. REPLACED BATTERY PACK AND LENS ASSEMBLY. OPS CHECK GOOD. (M)

Part: BATTERY PACK — INOPERATIVE (RT OVERWING EXIT)

ANC - FOUND RIGHT OVERWING EXIT SIGN INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. (M)

Part: SEAT TRACK — MISDRILLED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: SEAT TRACK HAS MISDRILLED HOLES. REPLACED SEAT TRACK.

Part: WEB — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: CORROSION IN AFT CARGO WEB. REPLACED WEB

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND CORROSION ON SEAT TRACK AT STATION 727. REMOVED AND REPLACED SEAT TRACK PER SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND CORROSION ON SEAT TRACK. REMOVED AND REPLACED TRACK PER SRM. (M)

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: CORROSION ON UNDERSIDE AT WEB. REPLACED WEB.

Part: WEB — CRACKED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, WEB CRACKED. REPLACED WEB. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND FORWARD CARGO BAY INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: CORROSION ON WEB INTERCOSTAL. REPLACED INTERCOSTAL. (K)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: CORROSION ON AFT CARGO INTERCOSTAL. REPLACED INTERCOSTAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE)

PAE - DURING D-CHECK, FOUND INTERCOSTAL IS CRACKED AT BS 400-420. REMOVED AND REPLACED INTERCOSTAL PER SRM. (M)

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: CORROSION ON WEB ANGLE. REPLACED WEB ANGLE.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: CORROSION ON WEB INTERCOSTAL. REPLACED INTERCOSTAL.(K)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: CORROSION ON LWR SURFACE OF SEAT TRACK. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND DURING D-CHECK, CORROSION ON SEAT TRACK. REMOVED AND REPLACED SEAT TRACK PER SRM. (M)

Part: FRAME — CHAFED (APU DOOR) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND CHAFED FRAME ON APU ACCESS DOOR. REPLACED FRAME. (M)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND DAMAGE AT SKIN LAP, STRINGER 4L. REPAIRED PER EA 5330-01845. (M)

Part: BRACKET — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND CORROSION ON BRACKET. REMOVED AND REPLACED BRACKET PER SRM. (M)

Part: HOUSING — DAMAGED (LT STAB HINGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND LEFT CENTER SECTION HINGE DAMAGED AT CENTER SECTION ATTACH POINT. REPLACED LT STAB HINGE HOUSING. (M)

Part: WEB — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND CORROSION ON WEB. REPLACED WEB. (M)

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: CORROSION ON WEB IB ANGLE BELOW CAPT NR 2 WINDOW. REPLACED WEB IB ANGLE.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND DURING D-CHECK, CORROSION ON FLOORBEAM INTERCOSTAL AT FASTENER HOLE. REMOVED AND REPLACED INTERCOSTAL PER SRM. (M)

Part: WEB — CRACKED (FUSELAGE)

PAE - FOUND DURING D-CHECK, WEB AT STATION 980 HAS A CRACK. REMOVED AND REPLACED WEB PER SRM. (M)

Part: SEAT TRACK — MISINSTALLED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: SEAT TRACK REQUIRES REPLACEMENT DUE TO FASTENER EDGE MARGIN. REPLACED SEAT TRACK.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: CROWN TOOTH DAMAGED ON SEAT TRACK. REPLACED SEAT TRACK.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND CORROSION INTERCOSTAL AND ATTACHMENTS. REPLACED INTERCOSTAL AND ATTACH ANGLES. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

PAE - DURING D-CHECK, FOUND FORWARD CARGO BAY INTERCOSTAL IS CRACKED. REMOVED AND REPLACED INTERCOSTAL PER SRM. (M)

Part: DOOR FRAME — DAMAGED (FUSELAGE)

PAE - DURING D-CHECK, ELONGATED HOLES IN WEB. REPLACED WEB. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - FOUND DURING D-CHECK, CORROSION ON WEB. REMOVED, FABRICATED AND REPLACED WEB PER SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - FOUND DURING D-CHECK, CORROSION ON SEAT TRACK AT BS 947. REMOVED AND REPLACED SEAT TRACK PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - DURING D-CHECK, FOUND CORROSION ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

PAE - DURING D-CHECK, REJECTION INTERCOSTAL IS STILL CRACKED, FORWARD CARGO BAY INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: CORROSION ON SEAT TRACK. REPLACED SEAT TRACK.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs

PAE - DURING D-CHECK, FOUND DAMAGE ON EXTERNAL SKIN AT WING-TO-BODY FAIRING. REPAIRED PER EA. (M)

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: CORROSION ON WEB ANGLE. FABRICATED AND REPLACED WEB IB ANGLE.

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - DURING D-CHECK, FOUND CORROSION ON SEAT TRACK. REMOVED AND REPLACED SEAT TRACK PER SRM. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: CORROSION ON INTERCOSTAL. REPLACED INTERCOSTAL.

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - DURING D-CHECK, FOUND CORROSION ON SEAT TRACK. REMOVED AND REPLACED SEAT TRACK PER SRM. (M)

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: CREASE BEAM WEB IS CRACKED. REPLACED CREASE BEAM WEB.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND DURING D-CHECK, CORROSION ON SEAT TRACK AT BS 727B. REMOVED AND REPLACED SEAT TRACK PER SRM. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND DURING D-CHECK, CORROSION ON INTERCOSTAL AT BS 953. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL PER SRM. (M)

Part: WEB — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: FRAME/FLOOR WEB CRACKED. REPAIRED CRACKED FRAME/FLOOR WEB.

Part: BRACKET — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND T-BRACKET HAS ELONGATED HOLES AT STATION 344. REMOVED, FABRICATED AND INSTALLED T-BRACKET PER SRM. (M)

Part: FAILSAFE — CORRODED (FUSELAGE)

PAE - DURING D-CHECK, FOUND CORROSION ON FAIL/SAFE CHORD. REPLACED FAIL/SAFE CHORD. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND FORWARD CARGO BAY INTERCOSTAL IS CRACKED. REMOVED AND REPLACED INTERCOSTAL PER SRM. (M)

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, WHILE WORKING LAP REPAIR AT BS 951, STRINGER 10R FOUND SUPPORT FITTING CRACKED. REMOVED, FABRICATED AND INSTALLED SUPPORT FITTING. (M)

Part: WEB — GOUGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: AFT CARGO DOOR AFT CUTOUT CLOSURE WEB BETWEEN STRINGERS IS GOUGED. REPLACED WEB.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND CORROSION ON FLOOR SEAT TRACK FLANGE. REMOVED AND REPLACED SEAT TRACK. (M)

Part: WEB — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND CORROSION ON WEB. REPLACED WEB. (M)

Part: WEB — CORRODED (LAVATORY) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: CORROSION ON LAV WEB. REPLACED WEB.

Part: WEB — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: CORROSION ON AFT LAV FLOOR WEB. REPAIRED WEB (K)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED SUPPORT ANGLE PER SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND CORROSION ON SEAT TRACK. REMOVED AND REPLACED SEAT TRACK PER SRM. (M)

Part: CHANNEL — BROKEN (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND CHANNEL AND ANGLE (P/N 656361514) SUPPORT END IS BROKEN OFF AT RIVET HOLE. REMOVED, FABRICATED AND REPLACED CHANNEL AND ANGLE SUPPORT PER SRM. (M)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: SCRIBE MARK IN SKIN. REPAIRED IAW EA.

Part: SEAT TRACK — CORRODED · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND DURING D-CHECK, CORROSION ON SEAT TRACK FLANGE AT STATION 480. REMOVED AND REPLACED SEAT TRACK PER SRM. (M)

Part: SILL — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND CORROSION ON UPPER SILL WEB AT STATION 794-847, INBOARD OF STRINGER 18R. REMOVED AND REPLACED PER SRM. (M)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND DAMAGE ON SKIN. REPAIRED PER EA. (M)

Part: WEB — CRACKED (DOOR UPLATCH) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: AFT CARGO DOOR UPLATCH WEB IS CRACKED. REPLACED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: CORROSION ON SEAT TRACK. REPLACED SEAT TRACK.

Part: WEB — CORRODED (LAVATORY) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: CORROSION ON LAV WEB. REPLACED WEB.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE, D-CHECK: DAMAGE ON EXTERNAL SKIN. REPAIRED IAW EA.

Part: FRAME — CORRODED (FUSELAGE)

PAE - DURING D-CHECK, FOUND CORROSION ON FRAME. REPAIRED PER SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND DURING D-CHECK, CORROSION ON SHEAR TIE AT STATION 328. REPAIRED SHEAR TIE PER SRM. (M)

Part: SKIN — DAMAGED (FUSELAGE)

PAE - FOUND DURING D-CHECK, DAMAGE ON EXTERNAL SKIN AT BS 908-913. REPAIRED PER EA 5330-01841. (M)

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND DURING D-CHECK, DAMAGE ON SKIN LAP, MAIN CARGO DOOR. REPAIRED PER EA 5230-01250. (M)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND DAMAGE ON SKIN LAP, MAIN CARGO DOOR. REPAIRED PER EA 5230-01250. (M)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs

PAE - DURING D-CHECK, FOUND DAMAGE ON EXTERNAL SKIN AT BS 907, STRINGER 14L. REPAIRED PER EA 5330-01846. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND SHEAR TIE ANGLE CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. (M)

Part: WEB — CRACKED (FUSELAGE)

PAE - DURING D-CHECK, FOUND WEB CRACKED AT LOWER END. REMOVED AND REPLACED WEB PER SRM. (M)

Part: ANGLE — DAMAGED (FUSELAGE)

PAE - FOUND DURING D-CHECK, DAMAGE IN FASTENER HOLE ON L ANGLE. REMOVED AND REPLACED L ANGLE PER SRM. (M)

Part: SPAR — CRACKED (HORIZONTAL STAB)

PAE - DURING D-CHECK, FOUND HORIZ STAB CENTER SECTION, UPPER AFT SPAR CHORD IS CRACKED. REPAIRED PER EA 5210-01203. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND CORROSION ON STRINGER CLIP. REMOVED, FABRICATED AND INSTALLED STRINGER CLIP PER SRM. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

PAE - DURING D-CHECK, FOUND CORROSION ON STRINGER CLIP. REMOVED, FABRICATED AND INSTALLED STRINGER CLIP PER SRM. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - DURING D-CHECK, FOUND CORROSION ON FRAME DOUBLER AT BS 787, STRINGER 23R, WL 156. REMOVED, FABRICATED AND INSTALLED FRAME DOUBLER PER SRM. (M)

Part: SKIN — GOUGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BTM OF MAIN CARGO DOOR CUTOUT, FUSELAGE STATION 398. REPAIRED PER EA 5330-01861. (M)

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, FOUND CORROSION ON BEAR STRAP AT BS 348. REPAIRED PER EA 5310-02415. (M)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND DURING D-CHECK, DAMAGE ON SKIN A LAP. REPAIRED PER EA 5330-01835. (M)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING D-CHECK, DAMAGE ON SKIN AT LAP. REPAIRED PER EA 5330-01835. (M)

Part: SKIN — DAMAGED (RUDDER) · airframe 56,432 hrs · 52,393 cycles

PAE - MULTIPLE OUTER PLY DAMAGE ON RUDDER L/E. REPAIRED IAW EA.

Part: WEB — CORRODED (EE DOOR CUTOUT) · airframe 56,432 hrs · 52,393 cycles

PAE - CORROSION ON WEB RT SIDE OF E AND E DOOR CUTOUT. REMOVED AND REPLACED.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - CORROSION ON STRINGER. REPLACED STRINGER.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON SKIN LAP. REPAIRED IAW EA.

Part: SKIN — DAMAGED (SKIN LAP) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON SKIN LAP. REPAIRED IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND CORROSION ON STRINGER. REMOVED AND REPLACED STRINGER. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - CORROSION ON FLOORBEAM ON TOP OF LWR FLANGE AROUND NUTPLATE. REMOVED CORROSION AND REPAIRED FLOORBEAM.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - ELONGATED FASTENER HOLE IN STRINGER. REMOVED DISCREPANT AREA, INSTALLED REPAIR STRINGER SPLICE. (M)

Part: STRINGER — CHAFED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - STRINGER CHAFED AT WIRE BUNDLE STANDOFF. REPAIRED STRINGER IAW SRM.

Part: SPLICE — CORRODED (STRINGER) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND CORROSION ON STRINGER SPLICE. REMOVED AND REPLACED STRINGER SPLICE AND CLIP. (M)

Part: SKIN — GOUGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - GOUGES IN SKIN AT BOTTOM OF MAIN CARGO DOOR CUTOUT. REPAIRED IAE EA.(K)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - SCRIBE MARK IN SKIN. REPAIRED IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - CORROSION ON FLOORBEAM UPPER FLANGE. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED.

Part: SILL — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - CORROSION ON MOPSILL, REPLACED. (M)

Part: FRAME — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FRAME DAMAGED. REPAIRED FRAME BY INSTALLING DOUBLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND CORROSION LOWER FLOORBEAM. REPAIRED TRANSVERSE BEAM PER EA. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - LIGHTING STRIKE HOLE IN EXTERNAL SKIN. REPAIRED IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - SUPPORT ANGLE CRACKED. REMOVED, FABRICATED NEW ANGLE AND INSTALLED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON EXTERNAL SKIN. REPAIRED IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE- D-CHECK, DAMAGE ON EXTERNAL SKIN. REPAIRED IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON EXTERNAL SKIN LAP 6 INCHES LONG. REPAIRED IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON EXTERNAL SKIN LAP 4 INCHES LONG. REPAIRED IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

DAMAGE ON EXTERNAL SKIN LAP. REPAIRED IAW EA.

Part: SKIN — DAMAGED (FUSELAGE)

PAE - DAMAGEON EXTERNAL SKIN. REPAIRED PER EA. (M)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE -DAMAGE ON SKIN. REPAIRED IAW EA.

Part: SKIN — DAMAGED (LAP JOINT) · airframe 56,432 hrs · 52,393 cycles

DAMAGE ON EXTERNAL SKIN LAP JOINT, 2 INCH LONG. REPAIRED IAW EA.

Part: SKIN — DAMAGED (LAP JOINT) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON EXTERNAL SKIN LAP JOINT, 18 INCHES LONG. REPAIRED IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON EXTERNAL SKIN AT LAP JOINT. REPAIRED PER EA. (M)

Part: WEB — CORRODED (DOOR FRAME) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND CORROSION AT AFT CARGO DOOR CUTOUT FOWARD FRAME CLOSEOUT PANEL FASTENER HOLES. REPLACED AFT CARGO DOOR CLOSEOUT WEB. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - CORROSION ON FLOORBEAM ON TOP OF LWR FLANGE LWR SURFACE. REPAIRED IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON SKIN. REPAIRED PER EA. (M)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND DAMAGED ON SKIN. REPAIRED PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND CORROSION ON FLOORBEAM AT FASTENER HOLE UPPER AND LOWER SURFACE OF UPPER FLANGE. REPLACED STUB BEAM. (M)

Part: SKIN — DENTED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DENT IN EXTERNAL SKIN UNDER PREVIOUSLY INSTALLED REPAIR. REPAIRED PER EA. (M)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON SKIN LAP. REPAIRED IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND DAMAGE ON SKIN. REPAIRED PER EA. (M)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON EXTERNAL SKIN AT LAP JOINT. REPAIRED PER EA. (M)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND DAMAGED ON EXTERNAL SKIN AT LAP JOINT. REPAIRED PER EA. (M)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND DURING D-CHECK, SCRIBE MARK ON SKIN LAP AT STRINGER 14L. REPAIRED PER EA 5230-01250. (M)

Part: SKIN — DAMAGED (FAIRING)

PAE - SCRIBE MARKS AT RT FWD UPPER AND LOWER WING TO BODY FAIRING. REPAIRED IAW EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - CORROSION ON AFT CARGO DOOR CUT OUT UPPER FRAME CLOSURE WEB. REPLACED UPPER FRAME CLOSURE WEB.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs

PAE - DAMAGE ON SKIN LAP. REPAIRED PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND CORROSION LOWER FLOORBEAM BS 787 STRINGER 18R WL 201. REPAIRED TRANSVERSE BEAM PER EA 5310-02402 AND EO 04-3651. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - MAIN CARGO DOOR FRAME CRACKED. REPLACED FRAME PER SRM. (M)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON SKIN LAP. REPAIRED PER EA. (M)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE AT SKIN LAP. REPAIRED PER EA. (M)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - SCRIBE MARKS AROUND DOUBLER, LWR FWD CORNER OF FWD ENTRY DOOR CUTOUT. REPAIRED IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - SCRIBE MARKS AT SKIN LAP. REPAIRED IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND CRACK INDICATIONS AT SKIN LAP. REPAIRED PER EA. (M)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - SCRIBE MARK IN SKIN. REPAIRED IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - L-ANGLE CRACKED BS 292, 11 INCHES BELOW STRINGER 15L. REPAIRED PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND CORROSION ON FLOORBEAM. REPAIRED PER EA. (M)

Part: SKIN — DAMAGED (FS) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND DAMAGE AT STRINGER 14L, BS 986-1016. REPAIRED PER EA. (M)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE APPROX 2 INCHES LONG. REPAIRED PER EA. (M)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND DAMAGE APPROX 21 INCHES LONG. REPAIRED PER EA. (M)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE AT STRINGER 14L, BS 907-947. REPAIRED PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FLOORBEAM CORROSION AT FASTENER HOLES UPPER FLANGE, UPPER AND LOWER SURFACES. REPAIRED PER EA. (M)

Part: SKIN — DAMAGED (FAIRING) · airframe 56,432 hrs · 52,393 cycles

PAE - SCRIBE MARKS IN EXTERNAL SKIN, AT WING TO BODY FAIRING. REPAIRED SKIN IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - SCRIBE MARK IN EXTERNAL SKIN LAP JOINT STA 359, STRINGER 24L, 2 INCHES LONG. REPAIRED SCRIBE MARK.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DURING VISUAL INSPECTION OF LAP JOINT AT STRINGER 24L IAW ER 04-3622, SEC 1 FOUND ADDITIONAL SCRIBE MARKS FROM BS 259-360.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - SCRIBE MARKS IN EXTERNAL SKIN, ALONG RT FWD WING TO BODY FAIRING. REPAIRED SKIN IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - SCRIBE MARKS IN EXTERNAL SKIN, ALONG RT AFT WING TO BODY FAIRING. REPAIRED SKIN IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - SCRIBE MARKS IN EXTERNAL SKIN, ALONG RT AFT WING TO BODY FAIRING. REPAIRED SKIN IAW EA.

Part: SKIN — DAMAGED (FAIRING) · airframe 56,432 hrs · 52,393 cycles

PAE - SCRIBE MARKS ON EXTERNAL SKIN AT WING TO BODY FAIRING. REPAIRED EXTERNAL SKIN IAW EA.

Part: SKIN — DAMAGED (FAIRING) · airframe 56,432 hrs · 52,393 cycles

PAE - SCRIBE MARKS ON EXTERNAL SKIN AT WING TO BODY FAIRING. REPAIRED EXTERNAL SKIN IAW EA.

Part: SKIN — DAMAGED (FAIRING) · airframe 56,432 hrs · 52,393 cycles

PAE - SCRIBE MARKS ON EXTERNAL SKIN AT WING TO BODY FAIRING. REPAIRED EXTERNAL SKIN IAW EA.

Part: SKIN — DAMAGED (FAIRING) · airframe 56,432 hrs · 52,393 cycles

PAE - SCRIBE MARKS ON EXTERNAL SKIN AT WING TO BODY FAIRING. REPAIRED EXTERNAL SKIN IAW EA.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

PAE - UPPER FRAME SECTION HAS MISDRILLED PILOT HOLES UNDER FRAME CAP. REPAIRED IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

PAE - CORROSION ON SKIN, 3 INCHES BELOW AFT CARGO DOOR CUTOUT, UPPER AFT CORNER. REPAIRED IAW EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

PAE - CORROSION ON WEB. REPLACED WEB.

Part: SKIN — DAMAGED (AFT CARGO DOOR) · airframe 52,097 hrs · 44,561 cycles

PAE - SCRIBE MARK IN EXTERNAL SKIN AT AFT CARGO DOOR. REPAIRED AFT CARGO DOOR IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

PAE - MECHANICAL DAMAGE, 8 AREAS. REPAIRED IAW EA.

Part: SKIN — NICKED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

PAE - NICK IN SKIN. REPAIRED IAW EA.

Part: SKIN — DAMAGED (AFT CARGO DOOR) · airframe 52,097 hrs · 44,561 cycles

PAE - SCRIBE MARK IN EXTERNAL SKIN AT AFT CARGO DOOR UPPER AFT CORNER. REPAIRED AFT CARGO DOOR IAW EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,432 hrs · 52,393 cycles

PAE - CORROSION ON INTERCOSTAL AND STRINGER CLIP. REMOVED AND REPLACED INTERCOSTAL AND STRINGER CLIP.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - CORROSION ON STRINGER SPLICE. REMOVED AND REPLACED AND STRINGER SPLICE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - CORROSION ON STRINGER. REMOVED AND REPLACED STRINGER.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,432 hrs · 52,393 cycles

PAE - CORROSION ON STRINGER. REMOVED AND REPLACED STRINGER.

Part: SPLICE — CRACKED (STRINGER) · airframe 56,432 hrs · 52,393 cycles

PAE - PRODUCTION SPLICE IS CRACKED. REPLACED STRINGER SPLICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

PAE - CORROSION ON UPPER SILL WEB. REMOVED AND REPLACED SILL WEB.

Part: SPLICE — CORRODED (STRINGER) · corrosion level 2 · airframe 52,097 hrs · 44,561 cycles

PAE - CORROSION ON STRINGER SPLICE. REMOVED AND REPLACED STRINGER SPLICE.

Part: WEB — CORRODED (DOOR FRAME) · airframe 56,432 hrs · 52,393 cycles

PAE - CORROSION AT AFT CARGO DOOR CUT-OUT FWD FRAME CLOSEOUT PANEL FASTENER HOLES. REPLACED AFT CARGO DOOR CLOSE-OUT WEB.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

PAE - DAMAGE ON SKIN. REMOVED DAMAGE AND INSTALLED REPAIR.

Part: DOOR FRAME — DENTED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

PAE - AFT CARGO DOOR CUTOUT UPPER CHORD DENTED. REPLACED CHORD.

Part: SKIN — DENTED (FUSELAGE) · airframe 52,097 hrs · 44,561 cycles

PAE - DENT IN SKIN. REPAIRED IAW EA.

Part: FLOOR PANEL — CRACKED (LAVATORY) · airframe 56,432 hrs · 52,393 cycles

PAE - CRACKED FLOOR WEB IN FWD LAVATORY. REPAIRED WITH DOUBLER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - CRACKED FRAME. REPAIRED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - CORROSION ON FRAME STRAP AND FRAME. REMOVED AND REPLACED FRAME IB AND OB STRAP AND REMOVED AND REPLACED FRAME.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,432 hrs · 52,393 cycles

PAE - CORROSION ON FLOORBEAM LOWER FLANGE, LOWER SURFACE. REPAIRED WITH DOUBLER.

Part: SKIN — CHAFED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FUSELAGE SKIN DAMAGED FROM CHAFING. REMOVED DAMAGED SKIN, FABRICATED, NEW SKIN AND INSTALLED.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - CHAFED STRINGER. REPAIRED IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,432 hrs · 52,393 cycles

PAE - CORROSION ON FLOORBEAM LWR CHORD. REPAIRED FLOORBEAM LWR CHORD IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON SKIN. REPAIRED IAW EA.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,432 hrs · 52,393 cycles

PAE - CORROSION ON AFT GALLEY DOOR MOP SILL. REPLACED MOP SILL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON SKIN. REPAIRED IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON SKIN. REPAIRED IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON SKIN. REPAIRED IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON SKIN. REPAIRED IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON SKIN. REPAIRED IAW EA.

Part: SKIN — DAMAGED · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON SKIN. REPAIRED IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON SKIN. REPAIRED IAW EA.

Part: SKIN — DAMAGED (STA219,230) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON SKIN. REPAIRED IAW EA.

Part: BEAM — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - CORROSION ON LONGITUDINAL BEAM. REMOVED AND REPLACED LONGITUDINAL BEAM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON SKIN. REPAIRED IAW EA.

Part: SKIN — NICKED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - EXTERIOR SKIN HAS NICKS. REPAIRED SKIN IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON SKIN. REPAIRED IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON SKIN. REPAIRED IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON SKIN. REPAIRED IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FRAME IS CORRODED. REMOVED CORRODED CAP, FABRICATED NEW CAP TO BE INSTALLED ON CARD NR 4846121.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - CRACKED STRINGER. REMOVED AND REPLACED STRINGER.

Part: WEB — CORRODED (AFT GALLEY DOOR)

PAE - CORROSION ON THRESHOLD WEB AFT GALLEY DOOR CUT OUT. REMOVED AND REPLACED WEB.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE- CRACK IN FASTENER HOLE IN FRAME. REMOVED AND REPLACED FRAME.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON SKIN LAP. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,432 hrs · 52,393 cycles

CORROSION ON SHEAR TIE. REMOVED SHEAR TIE FABRICATED NEW SHEAR TIE AND INSTALLED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - DAMAGE ON SKIN LAP. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - 50 HOLES HAVE CRACK INDICATIONS AT SKIN LAP. REPAIRED DISCREPANT HOLES IAW EA. OVERSIZED .0312 INCH.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - FOUND 8 EACH, BACC HOLE IN SHEAR TIE. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE- 5 HOLES WITH CRACK INDICATIONS. OVERSIZED HOLES AND INSTALLED REPAIR DOUBLERS.

Part: SKIN — DAMAGED (FUSELAGE)

PAE - DAMAGE IN SKIN AT LAP. BLENDED DAMAGE AND INSTALLED REPAIR DOUBLERS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE - SCRIBE MARKS IN SKIN AT LAP. BLENDED SCRIBE MARKS AND INSTALLED REPAIR DOUBLERS.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,432 hrs · 52,393 cycles

PAE - CORROSION ON UPPER FLANGE OF L-ANGLE. REMOVED CORROSION IN AN AREA 1 INCH X 20 INCHES. REMOVING .075 INCHES FROM AN ORIGINAL .200 INCHES, FOUND TO BE OUT OF LIMITS. REPAIRED IAW EA.

Part: SKIN — GOUGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

PAE- SKIN GOUGED UNDER LAP. BLENDED GOUGED SKIN AND INSTALLED REPAIR DOUBLER.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

DAMAGE AT SKIN LAP. BLENDED DAMAGE AND INSTALLED REPAIR DOUBLER.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

STRINGER 14L AT BS 500-540 REQUIRES REWORK TO CHANGE SHIMMING REQUIREMENTS. REMOVED EXISTING REPAIR, FABRICATED -7, -6, AND -2 DOUBLER`S AND REINSTALLED.

Part: SKIN — SCORED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

LOWER SKIN OF LAP IS SCORED BETWEEN THE CENTER AND LOWER ROW. REPAIRED SKIN IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

DAMAGE ON EXTERNAL SKIN. REPAIRED DAMAGE ON SKIN IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

DAMAGE ON EXTERNAL SKIN. REPAIRED DAMAGE IAW EA.

Part: SKIN — SCORED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

LOWER SKIN OF LAP IS SCORED BETWEEN THE CENTER AND LOWER ROW OF FASTNERS. REPAIRED SKIN IAW EA.

Part: LAP JOINT — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

SCRIBE MARK IN EXTERNAL SKIN LAP JOINT. REPAIRED SCRIBE MARK ON SKIN LAP.

Part: SKIN — DAMAGED (FUSLEAGE) · airframe 56,432 hrs · 52,393 cycles

DAMAGE ON SKIN. REPAIRED DAMAGE ON SKIN.

Part: SKIN — DAMAGED (FUSLEAGE) · airframe 56,432 hrs · 52,393 cycles

SKIN DAMAGED. REPAIRED DAMAGE ON SKIN LAP.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

DAMAGE ON SKIN. REPAIRED DAMAGE ON SKIN.

Part: LAP JOINT — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

DAMAGE ON EXTERNAL SKIN LAP JOINT. REPAIRED DAMAGE ON SKIN LAP.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

DAMAGE ON SKIN. REPAIRED DAMAGE ON SKIN.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

DAMAGE ON SKIN. REPAIRED DAMAGE ON SKIN.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

FUSELAGE SKIN HAS DENT. CUT OUT DAMAGED AREA, AND INSTALLED EXTERNAL SKIN PATCH.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

CORROSION ON FLOORBEAM AT FLANGE AROUND NUT PLATE. REMOVED CORROSION, AND REPAIRED FLOORBEAM.

Part: BUTT JOINT — DAMAGED (FUSELAGE) · airframe 56,432 hrs · 52,393 cycles

DAMAGE ON BUTT SPLICE. REMOVED AND REPLACED BUTT SPLICE.

Part: STRUCTURE — CORRODED (MLG WW)

PAE - FOUND CORROSION AT RIGHT MLG WHEEL WELL ON CHORD. CUTOUT DAMAGED AREA AND SPLICE IN NEW AREA PER SRM. (M)

Part: STRINGER — DAMAGED (FUSELAGE)

PAE - FOUND ELONGATED FASTENER HOLE IN STRINGER 18L UPPER FLANGE AT BS 905. REMOVED DISCREPANT AREA, INSTALLED REPAIR STRINGER SPLICE. (M)

Part: BEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON LONGITUDINAL BEAM. REMOVED AND REPLACED LONGITUDINAL BEAM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOORBAM UPPER CHORD. REPAIRED FLOORBEAM UPPER CHORD AFT FLANGE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION BOTTOM LOWER LOBE OF FLOORBEAM. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED. (M)

Part: STRINGER — CRACKED (FUSELAGE)

PAE - FOUND STRINGER 19R CRACKED .250 INCH AT 2 HOLE LOCATIONS. REMOVED DAMAGED/CRACKED STRINGER, FABRICATED REPAIR PARTS AND INSTALLED. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

PAE - FOUND SHEAR TIE CRACKED AT 2 FASTENER HOLE LOCATIONS. REMOVED AND REPLACED SHEAR TIE. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON SHEARTIE, FORWARD AND AFT SIDES. FOUND CORROSION BLENDOUT TO BE 'OUT OF LIMITS'. REMOVED, FABRICATED AND INSTALLED SHEAR TIE. (M)

Part: FRAME — GOUGED (FUSELAGE)

PAE - FOUND FRAME DAMAGED. REPAIRED FRAME BY INSTALLING DOUBLER. (M)

Part: STRINGER CLIP — DAMAGED (FUSELAGE)

PAE - FOUND STRINGER HAS MECHANICAL DAMAGE TO STRINGER CLIP. REMOVED DAMAGED STRINGER CLIP, FABRICATED NEW STRINGER CLIP AND INSTALLED. (M)

Part: FRAME — CRACKED (FUSELAGE)

PAE - FOUND FRAME CRACKED INBOARD FLANGE STATION 296. REMOVED DAMAGED SECTION OF FRAME, FABRICATED REPAIR PARTS AND INSTALLED. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FRAME. REMOVED DAMGAED PARTS, FABRICATED AND INSTALLED REPAIR PARTS. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

FOUND CORROSION ON STRINGER CLIP. BLENDED CORROSION, FOUND OUT OF LIMITS, FABRICATED AND INSTALLED. (M)

Part: BEAM — CORRODED (FUSELAGE)

FOUND CORROSION ON LONGITUDINAL BEAM. REMOVED AND REPLACED LONGITUDINAL BEAM. (M)

Part: STRINGER — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON STRINGER. REMOVED AND REPLACED STRINGER. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

PAE - CORROSION FOUND ON STRINGER CLIP. REMOVED DAMAGE, FABRICATED AND INSTALLED STRINGER CLIP. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

FOUND CORROSION ON SHEAR TIE. REMOVED, FABRICATED AND INSTALLED SHEAR TIE. (M)

Part: STRINGER — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON STRINGER. REMOVED DAMAGE, FABRICATED AND INSTALLED STRINGER REPAIR. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

FOUND CORROSION ON SHEAR TIE BETWEEN STRINGER 26L AND 27L. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

FOUND CORROSION ON SHEAR TIE AROUND LOWER FASTENER. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE PER SRM. (M)

Part: SKIN — GOUGED (FUSELAGE)

PAE - FOUND FUSELAGE SKIN IS GOUGED AT BS 902 STRINGER 19R. REPAIRED PER SRM. (M)

Part: STRINGER — CORRODED (FUSELAGE)

FOUND CORROSION ON STRINGER BS 787 PLUS 5 INCHES STRINGER 22R WL 155. REMOVED AND REPLACED STRINGER BS 773-792 STRINGER 22R, WL 5. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - FOUND CORROSION C53-107-01-03 ON SEAT TRACK BS 827-867 LBL 25 WL 208. REMOVED AND REPLACED SEAT TRACK BS 827-867 LBL 25, WL 208. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FOUND CORROSION ON FLOOR SEAT TRACK FLANGE STATION 500A THROUGH S TO 500B LBL 45 WL 208. REPLACES SEAT TRACK BS 480-520 LBL 45 WL 200. (M)

Part: WEB — DAMAGED (FUSELAGE)

FOUND AFT WEB SECTION DAMAGED. REPLACED WEB. (M)

Part: COWLING — WORN (NR 2 ENG NOSE)

FOUND NR 2 ENGINE NOSE COWL AFT LIP REPAIR WORN/DENTED. REMOVED AND REPLACED LOWER AFT CAP. (M)

Part: STRINGER — CHAFED (FUSELAGE)

PAE - FOUND CHAFED STRINGER. REMOVED AND REPLACED CHAFED STRINGER. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

FOUND CORROSION ON STRINGER CLIP. REMOVED OLD STRINGER CLIP AND INSTALLED NEW STRINGER CLIP. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON STRINGER CLIP. REMOVED OLD STRINGER CLIP AND INSTALLED NEW STRINGER CLIP. (M)

Part: FRAME — CHAFED (FUSELAGE)

FOUND CHAFED FRAME. REPAIRED FRAME. (M)

Part: STRINGER — CHAFED (FUSELAGE)

PAE - FOUND CHAFED STRINGER. REPAIRED STRINGER. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON E/E BATTERY DOOR CUTOUT FORWARD FRAME. REPAIRED DOOR FRAME, CUTOUT. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON STRINGER CLIP. REMOVED, FABRICATED NEW AND INSTALLED. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING RECON INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHT AT ROW 20 INOPERATIVE. REPLACED BATTERY PACK THEN LIGHT TESTED NORMAL. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ANC - DURING RECON INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 20 INOPERATIVE. REPLACED BATTERY PACK THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING RECON INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 20 INOPERATIVE. REPLACED BATTERY PACK THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ANC - DURING RECON INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 8 INOPERATIVE. REPLACED BATTERY PACK THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ANC - DURING RECON INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 8 INOPERATIVE. REPLACED BATTERY PACK THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY PACK — INOPERATIVE (EXIT SIGN)

ANC - DURING SCHEDULED INSPECTION, FOUND THE EXIT IDENTIFIER ON THE SMOKE BARRIER INOPERATIVE. REPLACED BATTERY PACK, THEN EXIT IDENTIFIER TESTED NORMAL. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ANC - DURING SCHEDULED INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 9 INOPERATIVE. REPLACED BATTERY PACK, THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - EMERGENCY EXIT IDENTIFIER FOR THE RIGHT OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK, THEN EXIT IDENTIFIER TESTED NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - FOUND EMERGENCY FLOOR TRACK LIGHTS ON SEAT PALLET 9-5 INOPERATIVE. REPLACED BATTERY PACK, THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY — DISCHARGED (SMOKE BARRIER)

ANC - FOUND EMERGENCY EXIT IDENTIFIER ON THE SMOKE BARRIER INOPERATIVE. REPLACED BATTERY, THEN EXIT IDENTIFIER TESTED NORMAL. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY SIGN)

ANC - FOUND EMERGENCY EXIT IDENTIFIER ON THE SMOKE BARRIER INOPERATIVE. REPLACED BATTERY, THEN EXIT IDENTIFIER TESTED NORMAL. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SEA - EMERGENCY FLOOR TRACK LIGHTS AT SEAT PALLET 8-9 INOPERATIVE. REPLACED BATTERY PACKS, THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - EMERGENCY EXIT IDENTIFIER ON THE SMOKE BARRIER INOPERATIVE. REPLACED REMOTE ASSEMBLY BATTERY, THEN LIGHT TESTED NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - EMERGENCY FLOOR TRACK LIGHTS AT SEAT PALLET 8-11 INOPERATIVE. REPLACED BATTERY PACKS, THEN LIGHTS TESTED NORMAL. (M)

Part: STRINGER — CRACKED (FUSELAGE)

OKC - DURING SCHEDULED C-CHECK, FOUND STRINGER 26L AT FUSELAGE STATION 767-768.5 CRACKED. REMOVED DAMAGED AREA AND REPAIRED STRINGER PER SRM. (M)

Part: STRINGER — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED C-CHECK, FOUND THE STRINGER 25L AT FUSELAGE STATION 352 CORRODED. REMOVED DAMAGED SECTION OF STRINGER AND REPAIRED PER SRM. (M)

Part: SKIN PANEL — CORRODED (FUSELAGE)

DURING SCHEDULED C-CHECK, FOUND THE INTERNAL SKIN PANEL AT FUSELAGE STATION 334, STRINGER 28L CORRODED. REMOVED CORROSION AND REPAIRED SKIN PER SRM AND EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED C-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 549-727A, LEFT BUTTOCK LINE 24.5 CORRODED. REMOVED CORROSION AND REPAIRED FLOORBEAM PER EA. (M)

Part: STRUCTURE — CHAFED (T/E FLAP)

OKC - DURING SCHEDULED C-CHECK, FOUND THE LEFT WING TRAILING EDGE OF THE MIDFLAP AT WING STATION 175.5 CHAFED. REPAIRED MIDFLAP PER EA. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED C-CHECK, FOUND THE FRAME AT FUSELAGE STATION 787, STRINGER 19L-26L CORRODED. REMOVED CORROSION AND REPAIRED FRAME PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED C-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 540-706, LEFT BUTTOCK LINE 25 CORRODED. REMOVED CORROSION AND REPAIRED FLOORBEAM PER SRM AND EA. (M)

Part: FRAME — DENTED (FUSELAGE)

OKC - DURING SCHEDULED C-CHECK, FOUND THE FRAME AT FUSELAGE STATION 727A, STRINGER 25L-26L CORRODED. REMOVED DAMAGED SECTION OF FRAME AND REPAIRED PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED C-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 520, BUTTOCK LINE 0, LEFT BUTTOCK LINE 24.5 CORRODED. REMOVED CORROSION AND REPAIRED FLOORBEAM PER EA. (M)

Part: FRAME — CORRODED (FUSELAGE)

DURING SCHEDULED C-CHECK, FOUND THE FRAME AT FUSELAGE STATION 887, STRINGER 24L-25L CORRODED. REMOVED DAMAGED SECTION OF FRAME AND REPAIRED PER SRM. (M)

Part: FRAME — CRACKED (FUSELAGE)

OKC - DURING SCHEDULED C-CHECK, FOUND THE FRAME AT FUSELAGE STATION 747, STRINGER 19L - 20L CRACKED AND CHAFED. REMOVED AND REPLACED SECTION AND REPAIRED FRAME PER SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED C-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 360-480, RIGHT BUTTOCK LINE 24 CORRODED. REPLACED SEAT TRACK PER SRM. (M)

Part: SKIN PANEL — DENTED (FUSELAGE)

DURING SCHEDULED C-CHECK, FOUND THE SKIN PANEL AT FUSELAGE STATION 378, WATERLINE 184.1L DENTED. CUT OUT DAMAGE AND REPAIRED PER SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED C-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 540-706, LEFT BUTTOCK LINE 25 CORRODED. REMOVED DAMAGED SECTION OF SEAT TRACK AND REPAIRED PER SRM. (M)

Part: SKIN — CHAFED (LT WING)

OKC - DURING SCHEDULED C-CHECK, FOUND THE LEFT WING LEADING EDGE AT WING STATION 505 CHAFED. REMOVED DAMAGED SECTION OF LEADING EDGE AND REPAIRED PER SRM. (M)

Part: SKIN — DENTED (FS 75)

DURING SCHEDULED C-CHECK, FOUND THE HORIZONTAL STABILIZER LEADING EDGE AT FUSELAGE STATION 1049.602, STABILIZER STATION 75 DENTED. (M)

Part: SKIN — CRACKED (FUSELAGE)

DURNG SCHEDULED C-CHECK, FOUND THE SKIN PANEL AT FUSELAGE STATION 747-749, STRINGER 19R CRACKED. REMOVED DAMAGED SECTION OF SKIN AND REPAIRED PER SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED C-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 727-727B, RIGHT BUTTOCK LINE 60 CORRODED. REPLACED SEAT TRACK PER SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING SCHEDULED C-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 420-500B, RIGHT BUTTOCK LINE 62 CORRODED. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK PER SRM. (M)

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C-CHECK, FOUND THE SKIN PANEL AT FUSELAGE STATION 923-925, STRINGER 19R CRACKED. REMOVED DAMAGED SECTION OF SKIN AND REPAIRED PER SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED C-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 420-480, RIGHT BUTTOCK LINE 45 CORRODED. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK PER SRM. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS BLINKING THROUGH OUT CABIN. REPLACED FIVE BATTERY PACKS, THEN LIGHT TESTED NORMAL. (M)

Part: BATTERY — DISCHARGED (SMOKE BARRIER)

ANC - EMERGENCY EXIT LIGHTS AT ROW 16 AND SMOKE BARRIER INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AT SMOKE BARRIER AND BATTERY PACK (P/N 86-2-1004) AT ROW 16, THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY — DISCHARGED (FWD CABIN)

SEA - FORWARD EMERGENCY SLIDE EXIT LIGHT ILLUMINATED. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY, THEN LIGHT TESTED NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 14 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER AND BATTERY PACK THEN LIGHTS TESTED NORMAL. (M)

Part: RECEIVER — INOPERATIVE (CABIN)

SEA - DURING INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 12 WOULD NOT TEST. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER, THEN LIGHTS TESTED NORMAL. (M)

Part: RECEIVER — INOPERATIVE (CABIN)

SEA - DURING LINE MAINTENANCE CHECK, FOUND THE BATTERY PACK AT ROW 16 NOT WORKING. REMOVED AND REPLACED REMOTE RECEIVER BATTERY. LIGHTS THEN OPERATED PROPERLY. (M)

Part: RECEIVER — FAILED (CABIN)

ANC - DURING INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 13 WOULD NOT EXTINGUISH. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERIES AND RECEIVERS, THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROWS 11, 12 AND 15 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERIES, THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

DURING PREFLIGHT CHECK, FOUND FOUR EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 18. REMOVED AND REPLACED REMOTE RECEIVER BATTERY. LIGHTS THEN OPERATED PROPERLY.

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT SEAT PALLET 7-8 ILLUMINATED. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY, THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING PREFLIGHT CHECK, FOUND FOUR EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROWS 12-14. REMOVED AND REPLACED REMOTE RECEIVER AND BATTERY AT ROW 12 AND BATTERY ONLY AT ROW 14. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ANC - SMOKE BARRIER AND OVERWING EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLIES (3) AT BOTH OVERWING EXITS AND SMOKE BARRIER, THEN LIGHTS TESTED NORMAL. (M)

Part: GUIDE — OUT OF ADJUST (L1 DOOR)

ANC - L1 DOOR WILL NOT CLOSE. ADJUSTED GUIDE ARM PER MM, THEN DOOR OPERATED NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING SCHEDULED INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHT AT ROW 14 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY PACK, THEN LIGHT TESTED NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ANC - DURING SCHEDULED INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHT AT ROW 19 INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY AT ROW 19, THEN LIGHT NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING SCHEDULED INSPECTION, FOUND EMERGENCY EXIT IDENTIFIERS AT L2 AND R2 DOORS INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERIES, THEN LIGHT TESTED NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ANC - DURING SCHEDULED INSPECTION, FOUND EMERGENCY EXIT IDENTIFIER AT LEFT OVERWING EXIT INOPERATIVE. REPLACED LIGHT ASSEMBLY, THEN LIGHT TESTED NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING SCHEDULED INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT LEFT OVERWING EXIT INOPERATIVE. REPLACED REMOTE ASSEMBLY BATTERY, THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING SCHEDULED INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT SEAT PALLETS 9 AND 10 INOPERATIVE. REPLACED REMOTE ASSEMBLY BATTERIES, THEN LIGHTS TESTED NORMAL. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 967, LEFT BUTTOCK LINE 18 CORRODED. REPAIRED FLOORBEAM PER EA. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 332, RIGHT BUTTOCK LINE 68.4 CORRODED. REPAIRED REAR FRAME PER SRM. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND KEELBEAM AT BS 677-727, LEFT BUTTOCK LINE 8 CORRODED. REPAIRED REAR KEELBEAM PER EA. (M)

Part: FITTING — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND SPAR LUGS AT BS 1104, LEFT BUTTOCK LINE 45, RIGHT BUTTOCK LINE 45 CORRODED. REPAIRED REAR SPAR LUGS PER EA. (M)

Part: SPAR — CORRODED (HORIZONTAL STAB)

PAE - DURING SCHEDULED C-CHECK, FOUND FORWARD SPAR AT HORIZONTAL STABILIZER STATION 57.93 CORRODED. REPAIRED REAR FORWARD SPAR PER EA. (M)

Part: SPAR — CORRODED (HORIZONTAL STAB)

PAE - DURING SCHEDULED C-CHECK, FOUND REAR SPAR AT RIGHT HORIZONTAL STABILIZER 67.54 CORRODED. REPAIRED REAR SPAR PER EA. (M)

Part: SPAR — CORRODED (HORIZONTAL STAB)

PAE - DURING SCHEDULED C-CHECK, FOUND REAR SPAR AT LEFT HORIZONTAL STABILIZER 67.54 CORRODED. REPAIRED REAR SPAR PER EA. (M)

Part: FRAME — CRACKED (LT WING)

PAE - DURING SCHEDULED C-CHECK, FOUND CHORD AT LEFT WING STATION 126 CRACKED. REPAIRED REAR CHORD PER SRM. (M)

Part: SKIN — CRACKED (PAX DOOR)

PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL ON L1 DOOR, BODY STATION 342, LEFT BUTTOCK LINE 63.3 CRACKED. REPAIRED SKIN PANEL PER SRM. (M)

Part: SKIN — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL AFT SERVICE DOOR, BS 967, RIGHT BUTTOCK ILNE 59 CRACKED. REPAIRED SKIN PANEL PER SRM. (M)

Part: SKIN PANEL — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL AT BS 378, STRINGER 28L-28R CRACKED. REPAIRED SKIN PANEL PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 1016, LBL 6, LBL 10 CORRODED. REPAIRED FLOORBEAM PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 328, RIGHT BUTTOCK LINE 15, RIGHT BUTTOCK LINE 29 CORRODED. REPAIRED FLOORBEAM PER SRM. (M)

Part: SILL — CORRODED (BS 290-328)

PAE - DURING SCHEDULED C-CHECK, FOUND FORWARD GALLEY DOOR MOPSILL AT BS 290-328, RIGHT BUTTOCK LINE 54 CORRODED. REPAIRED MOPSILL PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 294, LEFT BUTTOCK LINE 20, RIGHT BUTTOCK LINE 60 CORRODED. REPAIRED FLOORBEAM PER SRM. (M)

Part: BEAM — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND CREASE BEAM WEB AT BS 332-344, RIGHT BUTTOCK LINE 61-64 CORRODED. REPAIRED CREASE BEAM WEB PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 312, WATERLINE 208 CORRODED. REPAIRED FLOORBEAM PER SRM. (M)

Part: STRINGER — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 26R AT BS 536 CORRODED. REPAIRED STRINGER PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 1006, LEFT BUTTOCK LINE 10 CORRODED. REPAIRED FLOORBEAM PER SRM. (M)

Part: RECEIVER — INOPERATIVE (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT SEAT PALLET 3-3 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AND RECEIVER AT SEAT PALLET 3-3, THEN LIGHTS OPERATED NORMAL. (M)

Part: BATTERY — DISCHARGED (ROW 20)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT ROW 20 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AND RECEIVER AT ROW 20, THEN LIGHTS OPERATED NORMAL. REF ASAA0210054. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT ROW 20 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AND RECEIVER AT ROW 20, THEN LIGHTS OPERATED NORMAL. (M)

Part: BULKHEAD — CRACKED (FUSELAGE)

ANC - DURING SCHEDULED MAINTENANCE, FOUND AFT PRESSURE BULKHEAD AT BS 1016, RBL 1 CRACKED. REPAIRED PER EA. (M)

Part: GUIDE — OUT OF ADJ (L1 DOOR)

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

Part: CONNECTOR — DISCONNECTED (CABIN)

SEA - OVERHEAD EMERGENCY EXIT SIGN AT ROW 20 DOES NOT ILLUMINATE. RECONNECTED CANNON PLUG, THEN OPS CHECKED GOOD. (M)

Part: HINGE — LACK OF LUBE (L1 DOOR)

ANC - L1 DOOR DIFFICULT TO CLOSE. LUBED DOOR HINGE ATTACH POINTS, THEN OPS CHECKED GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

FAI - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTING INOPERATIVE AT ROWS 2-3. REMOVED AND REPLACED BATTERY PACK, OPERATIONAL CHECKS NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE, FOUND EMERGENCY SMOKE BARRIER EXIT INOPERATIVE. REMOVED AND REPLACED BATTERIES OPERATIONAL CHECK NORMAL. (M)

Part: WIRE — LOOSE (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. SECURED LOOSE WIRE THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT IDENTIFIER ON L1, R1 AND R2 DOORS INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERIES (3) AND ALL SIGNS OPERATED NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT AT LEFT AND RIGHT OVERWING EXIT DOORS INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERIES AND BOTH SIGNS OPERATED NORMAL. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS IN THE MID CABIN INOPERATIVE DUE TO CANNON PLUG BEING DISCONNECTED. RECONNECTED CANNON PLUG, THEN LIGHTS TESTED NORMAL. (M)

Part: RECEIVER — INOPERATIVE

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROWS 8 AND 12 FLASHING ON AND OFF. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVERS AND BATTERIES. LIGHTS THEN TESTED NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROWS 8 AND 12 FLASHING ON AND OFF. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVERS AND BATTERIES. LIGHTS THEN TESTED NORMAL. REF ASAA0110559. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROWS 8 AND 12 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVERS AND BATTERIES. LIGHTS TESTED NORMAL. REF ASAA0110557. (M)

Part: RECEIVER — INOPERATIVE (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROWS 8 AND 12 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVERS AND BATTERIES. LIGHTS TESTED NORMAL. (M)

Part: SIGN — INOPERATIVE (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT SIGN INOPERATIVE. REPLACED EMERGENCY EXIT SIGN, SIGN THEN TESTED NORMAL. (M)

Part: DOOR — OUT OF ADJ (L1)

JNU - DURING MAINTENANCE CHECK, FOUND L1 DOOR DIFFICULT TO OPEN AND CLOSE. ADJUSTED L1 DOOR PER MM AND DOOR OPENED NORMALLY. (M)

Part: RECEIVER — INOPERATIVE (CABIN)

JNU - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROW 26 WOULD NOT EXTINGUISH. REPLACED EMERGENCY EXIT BATTERY PACK AND REMOTE ASSEMBLY RECEIVER, LIGHTS THEN TESTED NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

JNU - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROW 26 WOULD NOT EXTINGUISH. REPLACED EMERGENCY EXIT BATTERY PACK AND REMOTE ASSEMBLY RECEIVER, LIGHTS THEN TESTED NORMAL. REF ASAA0110491. (M)

Part: RECEIVER — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS P/N 88-3-2003-1-2, 88-2-1004, WOULD NOT ILLUMINATE. REPLACED EMERGENCY EXIT BATTERY PACK AND REMOTE ASSEMBLY RECEIVER, LIGHTS THEN TESTED NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT WOULD NOT EXTINGUISH. REPLACED EMERGENCY EXIT BATTERY PACK, LIGHTS THEN TESTED NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (FWD CABIN)

SEA - DURING FLIGHT EMERGENCY EXIT LIGHTS ON THE FORWARD SEAT PALLET ILLUMINATED. REMOVED AND REPLACED BATTERY PACK, THEN LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — INOPERATIVE

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERIES THEN EXIT LIGHTS OPERATED NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT IDENTIFIER FAILED RECON TEST. REMOVED AND REPLACED REMOTE LIGHT ASSEMBLY AND REMOTE ASSEMBLY BATTERY THEN EXIT LIGHTS OPERATED NORMAL. REF ASAA0110375. (M)

Part: SIGN — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT IDENTIFIER FAILED RECON TEST. REMOVED AND REPLACED REMOTE LIGHT ASSEMBLY AND REMOTE ASSEMBLY BATTERY THEN EXIT LIGHTS OPERATED NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS FAILED RECON TEST. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY THEN EXIT LIGHTS OPERATED NORMAL. (M)

Part: STRINGER — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 17L AT BS 179, CRACKED. REPAIRED PER EA. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND INTERCOSTAL AT BS 178, WATERLINE 207 CRACKED. REPAIRED PER EA. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 924, STRINGER 19L CORRODED. REPAIRED PER SRM. (M)

Part: BULKHEAD — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND WEB AT BS 178, WATERLINE 234 CRACKED. REPAIRED PER EA. (M)

Part: BULKHEAD — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND WEB AT BS 178, WATERLINE 218 CRACKED. REPAIRED PER EA. (M)

Part: FRAME — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND CHORD AT BS 178, WATERLINE 184 CRACKED. REPAIRED PER EA. (M)

Part: SKIN PANEL — DAMAGED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL FASTENER HOLE AT BS 835, WATERLINE 299 DAMAGED. REPAIRED PER EA. (M)

Part: FRAME — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND CHORD AT BS 178, WATERLINE 195-207 CRACKED. REPAIRED PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 986.5, WATERLINE 208 CORRODED. REPAIRED PER EA. ( M)

Part: STRUCTURE — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND LT MLG WW CUTOUT AT BS 663-727, WATERLINE 150 CORRODED. REPAIRED PER SRM. (M)

Part: STRINGER — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 25L AT BS 924 CORRODED. REPAIRED PER EA. (M)

Part: SKIN — DENTED (NACELLE)

PAE - DURING SCHEDULED C-CHECK, FOUND FAIRING SKIN AT NACELLE STATION 113.79, NACELLE WATERLINE 126.14 DENTED. REPAIRED PER EA. (M)

Part: BATTERY PACK — INOPERATIVE

PAE - DURING SCHEDULED C-CHECK, FOUND EMERGENCY EXIT LIGHTS AT THE RIGHT OVERWING EXIT WOULD NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK AND LIGHTS TESTED NORMAL. (M)

Part: SKIN PANEL — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL AT BS 951, WATERLINE 246 CRACKED. REPAIRED PER SRM. (M)

Part: FRAME — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND CHORD AT BS 178, WATERLINE 207 CRACKED. REPAIRED PER EA. (M)

Part: FRAME — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND FRAME AT BS 480, STRINGER 2R CRACKED. REPAIRED PER EA. (M)

Part: STRINGER — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 21L AT BS 810, CORRODED. REPAIRED PER SRM. (M)

Part: STRINGER — CRACKED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 27R AT BS 490, CRACKED. REPAIRED PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND CHORD AT BS 668-670, RBL 25 CORRODED. REPAIRED PER EA. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

PAE - DURING SCHEDULED C-CHECK, FOUND KEEL BEAM AT BS 525-530, STRINGER 28R CORRODED. REPAIRED PER EA. (M)

Part: CONTROL UNIT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS IN THE MID CABIN INOPERATIVE. REMOVED AND REPLACED CONTROL MODULE, THEN LIGHTS OPERATED NORMALLY. (M)

Part: RECEIVER — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE ON SEAT PALLET 6-4, ROW 11. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER, THEN LIGHTS TESTED NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT AT LEFT OVERWING EXIT DOOR INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AND SIGN OPERATED NORMAL. (M)

Part: RECEIVER — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS ON SEAT PALLET 6-10 INOPERATIVE. REPLACED REMOTE ASSEMBLY BATTERY AND RECEIVER, LIGHTS FUNCTION NORMAL. REF ASAA0110110. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS ON SEAT PALLET 6-10 INOPERATIVE. REPLACED REMOTE ASSEMBLY BATTERY AND RECEIVER, LIGHTS FUNCTION NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EXIT LIGHTS ON SEAT PALLET 5-7 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AND RECEIVER AND LIGHTS OPERATED NORMALLY. (M)

Part: RECEIVER — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EXIT LIGHTS ON SEAT PALLET 5-7 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AND RECEIVER AND LIGHTS OPERATED NORMALLY. REF ASAA0110098. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS ON SMOKE BARRIER AND ROW 9 FAILED OPERATIONS TEST. REPLACED REMOTE ASSEMBLY BATTERY FOR SMOKE BARRIER AND ROW 9, LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROW 8 WILL NOT EXTINGUISH. REMOVED AND REPLACED BATTERY PACK, LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT OVER L2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT BATTERY PACK, LIGHTS THEN TESTED NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (MID CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND LEFT OVERWING EMERGENCY TRACK LIGHT EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK, EXIT SIGN TESTED NORMAL. (M)

Part: BATTERY — DISCHARGED (FWD CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND L-1, R-1, AND R-2 DOOR EMERGENCY EXIT IDENTIFIERS INOPERATIVE. REPLACED BATTERIES FOR L-1 AND R-1 DOOR EXIT IDENTIFIERS. REPLACED LIGHT ASSEMBLY FOR R-2 DOOR. ALL OPS CHECK NORMALLY. (M)

Part: LIGHT — INOPERATIVE (AFT CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND L-1, R-1, AND R-2 DOOR EMERGENCY EXIT IDENTIFIERS INOPERATIVE. REPLACED BATTERIES FOR L-1 AND R-1 DOOR EXIT IDENTIFIERS. REPLACED LIGHT ASSEMBLY FOR R-2 DOOR. ALL OPS CHECK NORMALLY. REF ASAA0010180. (M)

Part: LIGHT — INOPERATIVE (AFT CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND L-1, R-1, AND R-2 DOOR EMERGENCY EXIT IDENTIFIERS INOPERATIVE. REPLACED BATTERIES FOR L-1 AND R-1 DOOR EXIT IDENTIFIERS. REPLACED LIGHT ASSEMBLY FOR R-2 DOOR. ALL OPS CHECK NORMALLY. REF ASAA0010180. (M)

Part: BATTERY PACK — DISCHARGED (SEAT)

SEA-DURING MAINTENANCE CHECK FOUND EMERGENCY EXIT LIGHTS ON SEAT PALLET INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK AND RECEIVER AND LIGHTS OPERATED NORMALLY.

Part: SIGN — INOPERATIVE (SMOKE BARRIER)

SEA DURING MAINTENANCE CHECK THE SMOKE BARRIER EXIT TO REAR EXIT IDENTIFIER WAS FOUND TO BE INOPERATIVE. REPLACED EXIT IDENTIFIER AND THE BATTERY PACK SYSTEM OPERATED NORMALLY.

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - PRIOR TO FLT 55, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE DIM OR INOPERATIVE. REPLACED BATTERY PACKS AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING TAXI OUT FOR FLIGHT 55, THREE EMERGENCY EXIT TRACK LIGHTS ILLUMINATED. RETURNED TO GATE. REPLACED BATTERY PACK AT PALLET 7-2 AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURNIG MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPAIRED AFT EMERGENCY EXIT TRACK LIGHT WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT AT ROW 5 WAS FOUND TO BE INOPERATIVE. REPLCED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (ROW 12)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTING FOR SEVERAL PALLET RECEIVERS WAS FOUND INOPERATIVE. REPLACED BATTERY PACK AT ROW 12 AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROW 10)

ANC - PRIOR TO FLIGHT 153, AN EMERGENCY EXIT TRACK LIGHT WAS FOUND INOPERATIVE AT ROW 10. RELEASED PER MEL 33-19B. MAINTENANCE SUBSEQUENTLY SLICED WIRING AT LIGHT SOCKET AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, SEAT PALLET 6-1 EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROW 16 AND AT THE RIGHT OVERWING EXIT WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACKS AT BOTH POSITIONS AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE R-1 DOOR EMERGENCY EXIT LIGHT WAS FOUND LOW ON POWER. REPLACED BATTERY PACK AND THE LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (ROW 18)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 18 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: HANDLE — LACK OF LUBE (PAX DOOR)

ANC - PRIOR TO FLIGHT 153, THE L2 DOOR WAS FOUND DIFFICULT TO CLOSE. LUBRICATED HANDLE AND DOOR OPERATED NORMALLY. (M)

Part: RECEIVER — INOPERATIVE (CABIN)

ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE ON SEAT PALLET 9-1. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER. LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

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

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, R1 DOOR LOWER EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK THE R2 DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHT OPERATED NORMALLY. (X)

Part: BATTERY — DISCHARGED (CABIN)

SEA - PRIOR TO FLT 63, THE EMERGENCY FLOOR TRACK LIGHTING AND THE R1 AND L2 DOOR RECEIVERS WERE FOUND INOPERATIVE. REPLACED THE EMERGENCY FLOOR TRACK LIGHTING MID-CABIN TRANSMITTER, THE R1 DOOR RECEIVER BATTERIES, AND THE L2 DOOR RECEIVER. ALL LIGHTS OPERATED NORMALLY. REF: OPER CONTROL NRS ASAA9910240 AND 99ZZZX4628.

Part: TRANSMITTER — FAILED (CABIN)

SEA - PRIOR TO FLT 63, THE EMERGENCY FLOOR TRACK LIGHTING AND THE R1 AND L2 DOOR RECEIVERS WERE FOUND INOPERATIVE. REPLACED THE EMERGENCY FLOOR TRACK LIGHTING MID-CABIN TRANSMITTER, THE R1 DOOR RECEIVER BATTERIES, AND THE L2 DOOR RECEIVER. ALL LIGHTS OPERATED NORMALLY. REF: OPER CONTROL NRS 99ZZZX4628 AND 99ZZZX4629. (X)

Part: RECEIVER — FAILED (CABIN)

SEA - PRIOR TO FLT 63, THE EMERGENCY FLOOR TRACK LIGHTING AND THE R1 AND L2 DOOR RECEIVERS WERE FOUND INOPERATIVE. REPLACED THE EMERGENCY FLOOR TRACK LIGHTING MID-CABIN TRANSMITTER, THE R1 DOOR RECEIVER BATTERIES, AND THE L2 DOOR RECEIVER. ALL LIGHTS OPERATED NORMALLY. REF: OPER CONTROL NRS ASAA9910240 AND 99ZZZX4629.

Part: BATTERY PACK — DISCHARGED (ROWS 14-15)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 14 AND 15 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT NEAR THE L1 DOOR WAS FOUND TO BE FLASHING CONTINUOUSLY. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M)

Part: RECEIVER — INOPERATIVE (ROW 12)

SEA - PRIOR TO FLIGHT 65, THE EMERGENCY EXIT LIGHT RECEIVER AT ROW 12 WAS FOUND TO BE INOPERATIVE. REPLACED RECEIVER AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (ROW 5)

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

Part: BATTERY PACK — DISCHARGED (L1 DOOR)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR AND RIGHT OVERWING EXIT LIGHTS WERE FOUND TO BE VERY DIM. REPLACED BATTERY PACKS AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - PRIOR TO FLIGHT 61, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M)

Part: HANDLE — INOPERATIVE (AIRSTAIR DOOR)

ANC - PRIOR TO FLT 41, THE AFT AIRSTAIR DOOR HANDLE WAS FOUND TO BE INOPERATIVE. INSPECTED AND FOUND THE PUSH PULL CABLE SHEAR RIVET BROKEN. REPLACED SHEAR RIVET AND THE DOOR HANDLE OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (ROWS 14 & 15)

JNU - PRIOR TO FLT 61, THE EMERGENCY EXIT FLOOR TRACK LIGHTS ILLUMINATED AT ROWS 14 AND 15. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X)

Part: TRANSMITTER — INOPERATIVE (R1 DOOR)

SEA - PRIOR TO FLT 65, THE R1 AND L2 DOOR EMERGENCY LIGHTS WOULD NOT TEST. REPLACED R1 DOOR TRANSMITTER AND L2 DOOR RECEIVER, LIGHTS OPERATED NORMALLY. REF: OPER CNTRL NR 99ZZZX2832. (X)

Part: RECEIVER — INOPERATIVE (L2 DOOR)

SEA - PRIOR TO FLT 65, THE R1 AND L2 DOOR EMERGENCY LIGHTS WOULD NOT TEST. REPLACED R1 DOOR TRANSMITTER AND L2 DOOR RECEIVER, LIGHTS OPERATED NORMALLY. REF: OPER CNTRL NR ASAA9910135.

Part: RECEIVER — DEFECTIVE (ROWS 14 AND 20)

SEA - DURING MAINTENANCE CHECK, SEVERAL EMERGENCY EXIT LIGHT RECEIVERS WOULD NOT TEST PROPERLY. REPLACED RECEIVERS AT ROWS 14 AND 20, AND BATTERY AT ROW 18 AND AT THE R-1 DOOR. ALL EMERGENCY EXIT LIGHTS OPERATED NORMALLY. REF: OPER CNTRL NR 99ZZZX2833. (X)

Part: BATTERY — DISCHARGED (ROW 18)

SEA - DURING MAINTENANCE CHECK, SEVERAL EMERGENCY EXIT LIGHT RECEIVERS WOULD NOT TEST PROPERLY. REPLACED RECEIVERS AT ROWS 14 AND 20, AND BATTERY AT ROW 18 AND AT THE R-1 DOOR. ALL EMERGENCY EXIT LIGHTS OPERATED NORMALLY. REF: OPER CNTRL NR ASAA9910130.

Part: BATTERY — DISCHARGED (CABIN)

SEA - PRIOR TO FLIGHT 65, THE R1 EMERGENCY EXIT LIGHT WOULD NOT TEST PROPERLY. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - FLT 41 - PRIOR TO DEPARTURE, THE EMERGENCY EXIT FLOOR TRACK LIGHTS REMAINED ON. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: RECEIVER — DEFECTIVE (ROW 11)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 11 WERE FOUND TO BE INOPERATIVE. REPLACED RECEIVER AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DEFECTIVE (PALLET 6-1)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS ON SEAT PALLET 6-1 WERE FOUND TO BE INTERMITTENT. REPLACED SEAT PALLET DURING RECON AND LIGHTS OPERATED NORMALLY. (M)

Part: WEB — CORRODED (BS 847)

PHX - DURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT WEB CORRODED AT STATION 847 FROM STRINGER 19R TO 25R. REPAIRED PER EM 5300-01014. (M)

Part: FLOORBEAM — CORRODED (BS 947)

PHX - DURING D-CHECK, FOUND THE MAIN CABIN FLOORBEAM AT STATION 947 CORRODED FROM LBL 32 TO RBL 54, TOP AND BOTTOM OF UPPER CHORD. REPAIRED PER SRM 51-30-2. (M)

Part: WEB — CRACKED (BS 767-787)

PHX - DURING D-CHECK, FOUND CRACKED WEB AT THE AFT CARGO COMPARTMENT, FORWARD SIDE DOOR, STRINGER 25R, STATION 767 TO 787. REPAIRED PER SRM 51-30-2. (M)

Part: INTERCOSTAL — CRACKED (BS 500-520)

PHX - DURING D-CHECK, FOUND INTERCOSTAL AT STATION 500B TO 520 CRACKED AND DENTED. REPAIRED PER SRM 51-40-3 AND DRAWING 69-41757. (M)

Part: INTERCOSTAL — CORRODED (BS 787)

PHX - DURING D-CHECK, FOUND AFT CARGO COMPARTMENT ATTACH PLATE AT WEB INTERCOSTAL CORRODED AT STATION 787. REPAIRED PER SRM 51-30-2. (M)

Part: LIGHT — INOPERATIVE (R1 DOOR)

SEA - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY WAS FOUND TO BE MISSING. INSTALLED R1 DOOR EMERGENCY EXIT LIGHT ASSY, OPS NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - FLT 9000 - CREW REPORTED THAT THE AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER. LIGHT OPERATED NORMALLY. (M)

Part: CHARGER — INOPERATIVE (CABIN)

SEA - FLT 9000 - CREW REPORTED THAT THE AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER. LIGHT OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT EMERGENCY EXIT LIGHT, SMOKE BARRIER LIGHT, AND THE RIGHT OVERWING EXIT LIGHTS WERE INOPERATIVE. REPLACED AFT EMERGENCY EXIT LIGHT AND SMOKE BARRIER LIGHT BATTERIES AND THE RIGHT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY. ALL LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (RT EMER EXIT)

SEA - DURING MAINTENANCE CHECK, THE AFT EMERGENCY EXIT LIGHT, SMOKE BARRIER LIGHT, AND THE RIGHT OVERWING EXIT LIGHTS WERE INOPERATIVE. REPLACED AFT EMERGENCY EXIT LIGHT AND SMOKE BARRIER LIGHT BATTERIES AND THE RIGHT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY. ALL LIGHTS OPERATED NORMALLY. (M)

Part: SEAT TRACK — CORRODED (BS 375-520)

PHX - DURING D-CHECK, FOUND THE SEAT TRACK CORRODED FROM STATION 375 TO 520, LBL 60. REPAIRED PER SRM 51-30-0. (M)

Part: FLOORBEAM — CORRODED (BS 787)

PHX - DURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT FLOORBEAM LOWER SURFACE CORRODED AT STATION 787, LBL 20 TO LBL 24. REPAIRED PER EA 5310-01656. (M)

Part: FLOORBEAM — CORRODED (BS 727)

PHX - DURING D-CHECK, FOUND TEH MAIN CABIN FLOORBEAM CORRODED AT STATION 727B FROM RBL 25 TO RBL 60, LBL 45 TO LBL 60. REPAIRED PER SRM 51-30-2. (M)

Part: SILL — CORRODED (L2 DOORWAY)

PHX - DURING D-CHECK, FOUND THE L2 DOOR THRESHOLD AREA INBOARD CHORD OF DOOR SILL CORRODED AT STATION 947 TO 986, LBL 55. REPAIRED PER SRM 51-40-4. (M)

Part: BULKHEAD — CORRODED (BS 1156)

PHX - DURING D-CHECK, FOUND THE BULKHEAD LOWER SECTION CORRODED AT STATION 1156, LBL 6. REPAIRED PER 51-30 AND 51-10-2. (M)

Part: INTERCOSTAL — CORRODED (BS 270)

PHX - DURING D-CHECK, FOUND THE INTERCOSTAL AND 'Z' ANGLE CORRODED AT STATION 270, LBL 60-RBL 60. REPAIRED PER SRM 51-40-2. (M)

Part: SKIN — DENTED (VERT STABILIZER)

PHX - DURING D-CHECK, FOUND THE RIGHT SIDE OF THE VERTICAL STABILIZER DENTED 10 INCHES ABOVE PITOT TUBE FIN STATION 81.1. REPAIRED PER SRM 5530-30-3. (M)

Part: SKIN — CORRODED (BS 344)

PHX - DURING D-CHECK, FOUND THE INTERNAL SKIN CORRODED AT STATION 344, STRINGER 27L. REPAIRED PER EA 5310-01651. (M)

Part: FLOORBEAM — CORRODED (BS 967)

PHX - DURING D-CHECK, FOUND THE MAIN CABIN FLOORBEAM CORRODED ON THE UPPER CAP AT STATION 967, RLB 8 TO RBL 45. REPAIRED PER EA 5310-01662. (M)

Part: SHEAR TIE — CORRODED (BS 747)

PHX - DURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT SHEAR TIE AT FRAME CORRODED AT STATION 747 BETWEEN STRINGER 26R AND STRINGER 27R. REPAIRED PER 53-10-4, 51-10-1, AND 53-10-2. (M)

Part: STRINGER — CORRODED (BS 804)

PHX - DURING D-CHECK, FOUND STRINGER 26L CORRODED AT STATION 804. REPAIRED PER SRM 53-10-2. (M)

Part: FLOORBEAM — CORRODED (BS 328)

PHX - DURING D-CHECK, FOUND THE FLOORBEAM CORRODED AT STATION 328, RLB 73. REPAIRED PER SRM 51-10-6 AND 53-10-9. (M)

Part: BULKHEAD WEB — CRACKED (BS 1016)

PHX - DURING D-CHECK, FOUND THE AFT PRESSURE BULKHEAD WEB CRACKED FROM FOUR CONSECUTIVE FASTENERS AT AFT ROW WHERE IT ATTACHES TO THE 'Y' CHORD AT STATION 1016. REPAIRED PER EA 5310-01659. (M)

Part: FLOORBEAM — CORRODED (BS 420)

PHX - DURING D-CHECK, FOUND THE FLOORBEAM END CAP UPPER SURFACE CORRODED AT STATION 420, LBL 60. REPAIRED PER EA 5310-01658. (M)

Part: FLOORBEAM — GOUGED (BS 294.5)

PHX - DURING D-CHECK, FOUND THE FLOORBEAM GOUGED AT STATION 294.5, LBL 10 TO RBL 50. REPAIRED PER SRM 53-10-09. (M)

Part: SEAT TRACK — CORRODED (BS 727-787)

PHX - DURING D-CHECK, FOUND THE MAIN CABIN SEAT TRACK CORRODED FROM STATION 727B TO 787, LBL 25. REPAIRED PER SRM 53-10-2 AND 53-10-5. (M)

Part: ANGLE — CORRODED (BS 979-986)

PHX - DURING D-CHECK, FOUND THE AFT ENTRY AREA TORQUE BOX FOR AIRSTAIR MECHANISM HAS CORRODED ANGLE EXTRUSIONS AT STATION 979 TO 986, LBL 48. REPAIRED PER SRM 51-40-4 AND DRAWING 65-67393. (M)

Part: FRAME — CORRODED (BS 947)

PHX - DURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT FRAME AT STATION 947 CORRODED FROM STRINGER 23L TO 24L. REPAIRED PER SRM 51-40-3 AND 51-40-4. (M)

Part: THRESHOLD — CORRODED (BS 259-360)

PHX - DURING D-CHECK, FOUND THE L1 DOOR THRESHOLD HAS CORROSION IN VARIOUS LOCATIONS ALONG ENTIRE LENGTH STATION 259.5 TO 360. REPAIRED PER SRM 51-30-2. (M)

Part: THRESHOLD — CORRODED (BS 294-328)

PHX - DURING D-CHECK, FOUND THE R1 DOOR THRESHOLD CORRODED IN VARIOUS PLACES FROM STATION 294 TO 328. REPAIRED PER SRM 51-30-2. (M)

Part: FRAME — CORRODED (BS 807)

PHX - DURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT STATION 807 FRAME CORRODED AT STRINGER 25R. REPAIRED PER 51-40-3. (M)

Part: FLOORBEAM — CORRODED (BS 500)

PHX - DURING D-CHECK, FOUND THE FLOORBEAM LOWER CAP, LOWER SURFACE, FORWARD FLANGE CORRODED AT STATION 500B BETWEEN LBL 25 AND LBL 45. REPAIRED PER EA 5310-01655. (M)

Part: LIGHT — INOPERATIVE (CABIN)

PHX - AFTER TEST FLIGHT CREW REPORTED THAT THE AFT CABIN OVERHEAD EMERGENCY LIGHT WOULD NOT ILLUMINATE. REPLACED LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (M)

Part: SILL — CORRODED (CARGO DOORWAY)

PHX - DURING D-CHECK, FOUND THE MAIN CARGO DOOR SHEAR WEB LOWER SILL CORRODED AT STATION 344 TO 520. REPAIRED PER SRM 51-30-2. (M)

Part: INTERCOSTAL — CORRODED (BS 927-947)

PHX - DURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT INTERCOSTAL CORRODED AT STATION 927 TO 947 BETWEEN STRINGER 25R AND 26R. REPAIRED PER SRM 51-20-1 AND DRAWING 69-41473. (M)

Part: FLOORBEAM — CORRODED (BS 520)

PHX - DURING D-CHECK, FOUND THE FLOORBEAM CORRODED AT STATION 520, LBL 45 TO RBL 60. REPAIRED PER SRM 51-30. (M)

Part: INTERCOSTAL — CORRODED (BS 380-400)

PHX - DURING D-CHECK, FOUND THE INTERCOSTAL CORRODED AT STATION 380 TO 400, STRINGER 25L. REPAIRED PER SRM 51-10-6. (M)

Part: DOUBLER — CORRODED (BS 967-986)

PHX - DURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT SKIN DOUBLER AROUND THE OUTFLOW VALVE CORRODED BETWEEN STATION 967-986, STRINGER 22R STRINGER 25R. REPAIRED PER 53-10-3 AND DRAWING 6551627. (M)

Part: SUPPORT — CORRODED (BS 663)

PHX - DURING D-CHECK, FOUND THE MAIN CARGO FLOOR SUPPORT CORRODED AT STATION 663, RBL 45 - RBL 60. REPAIRED PER SRM 53-10-01. (M)

Part: SHEAR TIE — CORRODED (BS 787)

PHX - DURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT SHEAR TIE AT THE FRAME CORRODED AT STATION 787 BETWEEN STRINGER 26R AND 27R. REPAIRED PER SRM 53-10-2. (M)

Part: STRINGER — CORRODED (BS 947)

PHX - DURING D-CHECK, FOUND STRINGER 22L CORRODED AT STATION 947. REPAIRED PER SRM 53-10-2. (M)

Part: SEAT TRACK — CORRODED (BS 340-460)

PHX - DURING D-CHECK, FOUND THE SEAT TRACK CORRODED AT STATION 340 TO 460, LBL 45. REPAIRED PER SRM 51-10-1, 51-30-2 AND 53-10-2. (M)

Part: SPLICE — CORRODED (BS 907)

PHX - DURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT STRINGER 25R SPLICE AT STATION 907 TO 927 CORRODED. REPAIRED PER SRM 51-30-2. (M)

Part: SILL — CORRODED (BS 787-847)

PHX - DURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT INNER DOOR WEB CORRODED AT STATION 787-847 IN LOWER DOOR SILL. REPAIRED PER SRM 53-10-2. (M)

Part: SUPPORT — CORRODED (BS 707)

PHX - DURING D-CHECK, FOUND THE MAIN CABIN FLOOR SUPPORT CORRODED AT STATION 707, RBL 25 - RBL 45. REPAIRED PER SRM 53-10-1 AND DRAWING 65-54988. (M)

Part: SEAT TRACK — CRACKED (BS 727-767)

PHX - DURING D-CHECK, FOUND THE SEAT TRACK CRACKED AT STATION 727B TO 767, BL 0. REPAIRED PER SRM 53-10-2. (M)

Part: FLOORBEAM — CORRODED (BS 460)

PHX - DURING D-CHECK, FOUND THE FORWARD CARGO COMPARTMENT FLOORBEAM LOWER FLANGE CORRODED AT STATION 460, LBL 24 TO LBL 44. REPAIRED PER EA 5310-01663. (M)

Part: BATTERY PACK — DISCHARGED (R1 DOOR)

ANC - DURING FLIGHT, THE EMERGENCY EXIT LIGHT AT THE R1 DOOR INOPERATIVE. COULD NOT DUPLICATE. REPLACED BATTERY PACK AS PRECAUTIONARY AND LIGHT OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (ROW 8)

ANC - PRIOR TO FLIGHT 1271 - ONE EMERGENCY EXIT TRACK LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 8. RELAMPED, NO HELP. RELEASED PER MEL 33-19. SUBSEQUENTLY REPLACED LAMP ASSEMBLY AND LIGHT OPERTED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR LIGHTS WOULD NOT WORK FROM FLIGHT DECK SWITCH. REPLACED RECEIVER BATTERY AT ROW 3 AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (R1 DOOR)

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

Part: LIGHT — INOPERATIVE (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 17. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR LOWER EMERGENCY EXIT LIGHT WAS FOUND TO BE DIM. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M)

Part: RECEIVER — INOPERATIVE (CABIN)

ANC - DURING RECON OF AIRCRAFT, FOUND TWO EMERGENCY EXIT LIGHT INOPERATIVE ON ONE PALLET AND ALL EMERGENCY EXIT LIGHTS INOPERATIVE ON THE SECOND PALLET. REPLACED BATTERY PACK ON ONE PALLET AND REPLACED THE RECEIVER AND BATTERY PACK ON THE SECOND PALLET. ALL EMERGENCY EXIT LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING RECON OF AIRCRAFT, FOUND TWO EMERGENCY EXIT LIGHT INOPERATIVE ON ONE PALLET AND ALL EMERGENCY EXIT LIGHTS INOPERATIVE ON THE SECOND PALLET. REPLACED BATTERY PACK ON ONE PALLET AND REPLACED THE RECEIVER AND BATTERY PACK ON THE SECOND PALLET. ALL EMERGENCY EXIT LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR EXIT IDENTIFIER WAS FOUND TO BE DIM, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE, AND THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED RESPECTIVE BATTERIES AND ALL LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR EXIT IDENTIFIER WAS FOUND TO BE DIM, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE, AND THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED RESPECTIVE BATTERIES AND ALL LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR EXIT IDENTIFIER WAS FOUND TO BE DIM, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE, AND THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED RESPECTIVE BATTERIES AND ALL LIGHTS OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EXIT IDENTIFIER WAS FOUND DIM, R2 DOOR EMERGENCY EXIT IDENTIFIER WAS FOUND INOPERATIVE, AND THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED R1 AND R2 DOOR EMERGENCY EXIT IDENTIFIER BATTERIES AND THE SMOKE BARRIER LIGHT ASSEMBLY. ALL LIGHTS OPERATED NORMALLY. REF: OPERATOR CONTROL NR 98ZZZX3401. (X)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EXIT IDENTIFIER WAS FOUND DIM, R2 DOOR EMERGENCY EXIT IDENTIFIER WAS FOUND INOPERATIVE, AND THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED R1 AND R2 DOOR EMERGENCY EXIT IDENTIFIER BATTERIES AND THE SMOKE BARRIER LIGHT ASSEMBLY. ALL LIGHTS OPERATED NORMALLY. REF: OPERATOR CONTROL NR ASAA9810050.

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE LT AND RT AFT EMERGENCY EXIT STROBE LIGHTS REMAINED ILLUMINATED AFTER LIGHTS WERE TURNED OFF. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (X)

Part: LIGHT — INOPERATIVE (CABIN)

ANC - FLT 152 - PRIOR TO FLT, THE EMERGENCY EXIT LIGHTS ON PALLET NR 8 WERE FOUND TO BE INOPERATIVE. REPLACED LIGHT ASSY AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING RECON/MAINTENANCE CHECK, THE NR 1 AND NR 2 SEAT PALLET EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE BATTERY PACKS AND THE LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - PRIOR TO FLIGHT, THE R2 EMERGENCY EXIT TRACK LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING RECON, THE LEFT OVERWING EXIT IDENTIFIER, AFT ENTRY EXIT IDENTIFIER, AND THE SMOKE BARRIER EXIT LIGHT WERE FOUND TO BE INOPERATIVE. REPLACED THE LEFT OVERWING EXIT IDENTIFIER BATTERY PACK, THE AFT ENTRY EXIT IDENTIFIER BATTERY PACK, AND THE SMOKE BARRIER EXIT LIGHT ASSEMBLY AND ALL LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING RECON, THE AFT SEAT PALLET EMERGENCY EXIT LIGHTS AND AFT THREE BATTERY PACKS WERE FOUND TO BE INOPERATIVE. REPLACED AFT SEAT PALLET RECEIVER AND AFT THREE BATTERY PACKS AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING RECON, THE LEFT OVERWING EXIT IDENTIFIER, AFT ENTRY EXIT IDENTIFIER, AND THE SMOKE BARRIER EXIT LIGHT WERE FOUND TO BE INOPERATIVE. REPLACED THE LEFT OVERWING EXIT IDENTIFIER BATTERY PACK, THE AFT ENTRY EXIT IDENTIFIER BATTERY PACK, AND THE SMOKE BARRIER EXIT LIGHT ASSEMBLY AND ALL LIGHTS OPERATED NORMALLY. (M)

Part: RECEIVER — INOPERATIVE (CABIN)

SEA - DURING RECON, THE AFT SEAT PALLET EMERGENCY EXIT LIGHTS AND AFT THREE BATTERY PACKS WERE FOUND TO BE INOPERATIVE. REPLACED AFT SEAT PALLET RECEIVER AND AFT THREE BATTERY PACKS AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (R2 DOORS)

SEA - DURING MAINTENANCE CHECK, THE R1 AND R2 DOOR EMERGENCY IDENTIFIERS WERE FOUND TO BE INOPERATIVE. REPLACED R1 DOOR LIGHT ASSEMBLY AND THE BATTERY PACK AND THE LIGHTS OPERATED NORMALLY. (M)

Part: LIGHTS — INOPERATIVE (R1 DOORS)

SEA - DURING MAINTENANCE CHECK, THE R1 AND R2 DOOR EMERGENCY IDENTIFIERS WERE FOUND TO BE INOPERATIVE. REPLACED R1 DOOR LIGHT ASSEMBLY AND THE BATTERY PACK AND THE LIGHTS OPERATED NORMALLY. (M)

Part: TRANSMITTER — INOPERATIVE (CABIN)

ANC - FLT 54 - DURING FLIGHT IT WAS REPORTED THAT THE EMERGENCY EXIT FLOOR TRACK LIGHTS ILLUMINATED UNCOMMANDED AND THEN EXTINGUISHED AFTER A FEW MINUTES. REPLACED FORWARD AND AFT TRANSMITTERS AND LIGHTS OPERATED NORMALLY. (M)

Part: TRANSMITTER — INOPERATIVE (CABIN)

ANC - DURNIG DESCENT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS ILLUMINATED AND THEN EXTINGUISHED AFTER 20 SECONDS. REPLACED MID CABIN TRANSMITTER AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

JNU - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTS REMAINED ILLUMINATED ON SEAT PALLET 2. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: SIGN — INOPERATIVE (CABIN)

ANC - FLT 46 - DURING FLIGHT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 10-12 AND THE WALL MOUNTED EXIT IDENTIFIER BY THE AFT AIRSTAIR DOOR ILLUMINATED. REPLACED BATTERY PACK AT ROWS 11 AND 12, AND THE AFT EXIT IDENTIFIER AND ALL LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - FLT 46 - DURING FLIGHT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 10-12 AND THE WALL MOUNTED EXIT IDENTIFIER BY THE AFT AIRSTAIR DOOR ILLUMINATED. REPLACED BATTERY PACK AT ROWS 11 AND 12, AND THE AFT EXIT IDENTIFIER AND ALL 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 10-12. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD AND AFT CENTER AISLE EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE L2 AND R2 EXTERIOR EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X)

Part: SKIN — WORN (TE FOREFLAP)

SEA - DURING C-CHECK, LOOSE RIVETS WERE FOUND IN THE RIGHT OUTBOARD FOREFLAP SKIN. REPAIRED PER EA 5750-01263 AND BOEING TELEX ASA-SEA-97-0479RR. (M)

Part: FLOORBEAM — CORRODED (BS 947)

SEA - DURING C-CHECK, CORROSIOIN WAS FOUND AROUND THE NUTPLATE HOLES ON THE AFT LOWER FLANGE OF BS 947 FLOORBEAM. REPAIRED PER EA 5310-01565 AND BOEING TELEX ASA-SEA-97-0484RR. (M)

Part: SKIN — CORRODED (WS 240)

SEA - DURING C-CHECK, CORROSION PITTING WAS FOUND IN THE LEADING EDGE SKIN ON THE LEFT WING STATION L/E 240. THE PITTING IS LOCATED APPROXIMATELY 1 INCH BELOW THE APEX OF THE LEADING EDGE AND IS IN THE AREA THAT IS COVERED BY THE PYLON FAIRING. REPAIRED PER EA 5720-01132 AND BOEING TELEX ASA-SEA-97-0487RR. (M)

Part: RETRACT MECH — OUT OF ADJUST (TE MID FLAP)

SEA - DURING C-CHECK, A PROBLEM WAS ENCOUNTERED DURING RIGGING OF THE OUTBOARD AFT FLAP TO MID FLAP. REPAIRED PER EA 5750-01061 AND BOEING TELEX ASA-SEA-97-0489RR. (M)

Part: FLOORBEAM — CORRODED (BS 947.5)

SEA - DURING C-CHECK, CORROSION WAS FOUND ON THE UPPER AND LOWER SURFACES ON THE FORWARD FLANGE EDGE OF BS 947.5 FLOORBEAM AT LBL 4.25, 9.50, AND 15.25. REPAIRED PER EA 5310-01564 AND BOEING TELEX ASA-SEA-97-0315RR. (M)

Part: FLOORBEAM — CORRODED (BS 986.5)

SEA - DURING C-CHECK, CORROSION WAS FOUND ON THE FLOORBEAM UPPER TEE CHORD AT BS 986.5. REPAIRED PER EA 5310-01562. (M)

Part: FITTING — CORRODED (AFT AIRSTAIR)

SEA - DURING C-CHECK, CORROSION WAS FOUND ON THE AFT AIRSTAIR FORWARD TRANSMISSION MOUNT BRACKET FITTING. REPAIRED PER EA 5260-01064 BOEING TELEX ASA-SEA-97-0469RR. (M)

Part: FLOORBEAM — CORRODED (BS 986.5)

SEA - DURING C-CHECK, THE CLIP NUTS WERE FOUND CORRODED ON THE FLOORBEAM AT STATION 986.5, RBL 25. REPAIRED PER EA 5310-01561. (M)

Part: SPAR — GOUGED (LT TE MID FLAP)

SEA - DURING C-CHECK, THE LEFT INBOARD FLAP SHIELD WAS FOUND TO BE GOUGED. REPAIRED PER EA 5750-01262. (M)

Part: APU INLET — WORN (BS 1064)

SEA - DURING C-CHECK, THE APU INLET JAMB ASSEMBLY AFT OF THE INLET CUTOUT AT BS 1064 RT SIDE WAS FOUND TO HAVE 3 LOOSE BOLTS AND ELONGATED HOLES. REPAIRED PER EA 5310-01563. (M)

Part: DOOR — WORN (A/C BAY)

SEA - DURING C-CHECK, THE RIGHT AIR CONDITIONING BAY DOOR ALUMINUM FOIL PLY WAS FOUND TO BE WORN AT VARIOUS LOCATIONS. REPAIRED PER EA 5240-01026 AND BOEING TELEX ASA-SEA-97-0443RR. (M)

Part: SKIN — GOUGED (LT TE MIDFLAP)

SEA - DURING C-CHECK, THE RIGHT OUTBOARD MIDFLAP LEADING EDGE WAS FOUND TO BE GOUGED. REPAIRED PER EA 5750-01261, BOEING TELEX ASA-SEA-97-470RR, AND ASA-SEA-97-0471RR. (M)

Part: FLOORBEAM — CORRODED (BS 259.5)

SEA - DURING C-CHECK, CORROSION WAS FOUND ON THE FLOORBEAM UPPER AFT CHORD AND ON THE UPPER EDGE OF THE VERTICAL WEB AT BS 259.5. REPAIRED PER EA 5310-01560 AND BOEING TELEX ASA-SEA-95-0224RR. (M)

Part: DOOR — WORN (A/C BAY)

SEA - DURING C-CHECK, THE LEFT AIR CONDITIONING BAY DOOR ALUMINUM FOIL PLY WAS FOUND TO BE WORN AT VARIOUS LOCATIONS. REPAIRED PER EA 5240-01026 AND BOEING TELEX ASA-SEA-97-0443RR. (M)

Part: HINGE — GOUGED (BS 986.5)

SEA - DURING C-CHECK, A GOUGE WAS FOUND ON THE AFT AIRSTAIR, AFT UPPER HINGE, INBOARD FLANGE. REPAIRED PER EA 5260-01065 AND BOEING TELEX ASA-SEA-96-0166RR. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT AT THE LT OVERWING EXIT WAS FOUND INOPERATIVE. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (X)

Part: CRANKSHAFT — WORN (AFT AIRSTAIR)

ANC - DURING MAINTENACNE CHECK, FOUND THE AFT AIRSTAIRS WOULD NOT EXTEND IN EMERGENCY. REPLACED LOCK-OUT CRANK SPLINE SHAFT AND ADJUSTED RIGGING. AFT AIRSTAIRS OPERATE NORMALLY. TT: 38,772 HOURS. TC: 36,960. (X)

Part: BATTERY — DISCHARGED (R2 DOOR)

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

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 18. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE L2 AND R2 EXTERIOR EMERGENCY EXIT LIGHTS WERE FOUND TO ILLUMINATE WITH POWER REMOVED FROM THE AIRCRAFT AND THE EMERGENCY LIGHT SWITCH IN THE 'OFF POSITION. REPLACED BATTERY PACK AND THE LIGHTS OPERATED NORMALLY. (M)

Part: DOOR HANDLE — FROZEN (L-1)

BET - FLT 42 - L-1 DOOR WOULD NOT OPEN FROM THE OUTSIDE. APPLIED HEAT TO EXTERIOR DOOR HANDLE AREA AND DOOR OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT IDENTIFIERS AT R1, R2, L2, AND LT OVERWING EMERGENCY EXITS WERE FOUND DIM. REPLACED BATTERY PACK AND ALL LIGHTS OPERATED NORMALLY. (M)

Part: ROD END — OUT OF ADJUST (L1 DOOR)

ANC - FLT 143 - PRIOR TO DEPARTURE THE L1 DOOR WAS FOUND TO BE HARD TO CLOSE. ADJUSTED L1 DOOR GUIDE ARM ROD END AND DOOR OPERATED NORMALLY. (M)

Part: APU — MALFUNCTIONED (AFT FUSELAGE)

ANC - FLT 113 - DURING APU START ATTEMPT, GROUND PERSONNEL REPORTED THAT FLAMES WERE EVIDENT FROM THE APU EXHAUST. CREW DISCONTINUED START ATTEMPT AND DISCHARGED APU FIRE BOTTLE. REPLACD APU AND APU FIRE BOTTLE. ALLIED SIGNAL CONCLUDED THAT THE TURBINE SEALS WERE LEAKING AND THE TURBINE BEARING WAS GALLED. IT APPEARED THAT THE ROTATING GROUP HAD AN UNBALANCE THAT WAS CAUSING VIBRATION. NO APPARENT REASON OR INDICATION FOR THE EXHAUST FLAMES COULD BE FOUND. THE APU WAS DISASSEMBLED, INSPECTED AND REPAIRED BY ALLIED SIGNAL. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY — DISCHARGED (CARGO COMPT)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE ON PALLET 7-5. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, NUMEROUS EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED THREE EACH BATTERY PACKS AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 12 THROUGH 16. REPLACD BATTERY AND RECEIVER AND LIGHTS OPERATED NORMALLY. (M)

Part: RECEIVER — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 12 THROUGH 16. REPLACD BATTERY AND RECEIVER AND LIGHTS OPERATED NORMALLY. REFERENCE ASAA9610134.

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 18. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: EXIT SIGN — INOPERATIVE (R2 DOOR)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - FLT 64 - PRIOR TO DEPARTURE IT WAS REPORTED THAT THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 8 ILLUMINATED WITH SWITCH IN ARMED POSITION AND BUSSES POWERED. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: CASTING — BROKEN (BS 480)

YAK - FLT 66 - THE MAIN CARGO DOOR ACTUATOR CASTING BROKE WHILE DOOR WAS BEING OPENED. MAINTENANCE MANUALLY CLOSED MAIN CARGO DOOR AND RELEASED AIRCRAFT FOR MAINTENANCE FERRY FLIGHT TO SEA FOR REPAIR. THE AIRCRAFT WAS INDUCTED INTO C-CHECK UPON ITS ARRIVAL INTO SEA AND THE MAIN CARGO DOOR ACTUATOR CASTING IS CURRENTLY IN WORK. (M)

Part: CASTING — CRACKED (BS 480)

YAK - FLT 66 - THE MAIN CARGO DOOR ACTUATOR CASTING BROKE WHILE DOOR WAS BEING OPENED. MAINTENANCE MANUALLY CLOSED MAIN CARGO DOOR AND RELEASED AIRCRAFT FOR MAINTENANCE FERRY FLIGHT TO SEA FOR REPAIR. THE AIRCRAFT WAS INDUCTED INTO C-CHECK UPON ITS ARRIVAL INTO SEA AND THE MAIN CARGO DOOR ACTUATOR CASTING IS CURRENTLY IN WORK. REFERENCE ASAA9610128.

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE L2 AND R2 DOOR EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (LTOVERWING)

ANC - DURING MAINTENANCE CHECK, THE LEFT OVERWING EMERGENCYEXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLY AND LIGHTOPERATED NORMALLY. (M)

Part: DNLOCK SENSOR — INTERMITTENT (NLG)

SEA - FLT 861 - ON ARRIVAL, CREW REPORTED THE NOSE LANDING GEAR DOWN AND LOCKED (GREEN) LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. RECYCLED GEAR AND LIGHT EXTINGUISHED. LANDED WITHOUT INCIDENT. UNABLE TO DUPLICATE MALFUNCTION ON GROUND, CYCLED GEAR MULTIPLE TIMES AND OPERATED NORMALLY. REPLACED NOSE LANDING GEAR DOWNLOCK SENSOR AS PRECAUTIONARY MEASURE. (M)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT PALLET 9-6. REPLACED BATTERY AT PALLET 9-6 AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

JNU - DURING MAINTENANCE CHECK, THE TWO AFT MOST RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRES AND LIGHTS OPERATED NORMALLY. (X)

Part: DOOR MECHANISM — OUT OF ADJUST (L2 DOOR)

ANC - DURING MAINTENANCE CHECK, THE L-1 ENTRY DOOR WAS DIFFECULT TO CLOSE. ADJUSTED L1 DOOR MECHANISM PER MM AND DOOR OPERATED NORMALLY.

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING CREW PRE-FLIGHT, CREW REPORTED THE RT WING EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPLACED EXIT LIGHT BATTERY PACK AND LIGHT OPERATED NORMALLY. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE AFT SERVICE DOOR AND AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W)

Part: LG ACCY UNIT — DEFECTIVE (E/E COMPT)

SEA - AFTER DEPARTURE FROM KTN PASSING 256 KTS, GREEN NLG LIGHT CAME ON WITH GEAR UP. SLOWED AIRCRAFT AND CYCLED GEAR, LIGHT REMAINED ON. CYCLED LANDING GEAR C/B AND LIGHT WENT OUT. ACCELERATED THROUGH 270 KTS, LIGHT CAME ON AGAIN. AFTER 1 MINUTE, LIGHT WENT OUT ON ITS OWN AND STAYED OUT FOR REMAINDER OF THE FLIGHT, UNTIL GEAR EXTENSION. MAINTENANCE VERIFIED THE INTEGRITY OF THE NLG UP AND DOWN LOCK SENSORS AND ASSOCIATED WIRING IN THE NOSE WHEEL WELL. COMPLIED WITH GEAR SWINGS, UNABLE TO DUPLICATE MALFUNCTION. REMOVED AND REPLACED LANDING GEAR ACCESSORY MODULE. FUNCTIONAL CHECK GOOD. (M)

Part: DNLOCK SENSOR — INOPERATIVE (NLG)

SMF - FLT 415 - AIR TURN BACK DUE TO NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF. RECYCLED GEAR TWO TIMES AND LIGHT REMAINED ON. NOSE LANDING GEAR WOULD EXTEND IN THE OFF POSITION. LANDED WITHOUT INCIDENT. INSPECTED NOSE LANDING GEAR AND RELEASED AIRCRAFT FOR MAINTENANCE FERRY FLIGHT TO OAK. OAK MAINTENANCE REPLACED THE NLG LOCK ACTUATOR AND THE NLG DOWN LOCK SENSOR. GEAR OPERATED NORMALLY DURING ENTIRE GEAR CYCLE. REFERENCE ASAA9610021.

Part: LOCK ACTUATOR — INOPERATIVE (NLG)

SMF - FLT 415 - AIR TURN BACK DUE TO NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF. RECYCLED GEAR TWO TIMES AND LIGHT REMAINED ON. NOSE LANDING GEAR WOULD EXTEND IN THE OFF POSITION. LANDED WITHOUT INCIDENT. INSPECTED NOSE LANDING GEAR AND RELEASED AIRCRAFT FOR MAINTENANCE FERRY FLIGHT TO OAK. OAK MAINTENANCE REPLACED THE NLG LOCK ACTUATOR AND THE NLG DOWN LOCK SENSOR. GEAR OPERATED NORMALLY DURING ENTIRE GEAR CYCLE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS ON THE NR 1 PALLET WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X)

Part: EEL ASSY — DEFECTIVE (CABIN)

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

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS WAS FOUND INOPERATIVE. REPLACED REMOTE FLOOR PROXIMITY LIGHT ASSEMBLY AND BATTERY; LIGHTS OPERATED NORMALLY. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: EEL ASSY — INOPERATIVE (CABIN)

ANC - DURING MAINTENANCE CHECK, THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND DIM. REPLACED LIGHT ASSEMBLY AND BATTERY; LIGHT OPERATED NORMALLY. REFERENCE OPERATOR CONTROL NR 95ZZZX6298. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE R-1 OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. CHARGED BATTERY PACK AND LIGHT OPERATED NORMALLY. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHT WAS FOUND INOPERATIVE AT ROW 20. REPLACED BATTERY PACK AND LIGHT OPERATED NORMALLY. (X)

Part: BATTERY — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND DIM. REPLACED LIGHT ASSEMBLY AND BATTERY; LIGHT OPERATED NORMALLY. REFERENCE OPERATOR CONTROL NR ASAA9510101. (X)

Part: EEL ASSY — INOPERATIVE (CABIN)

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

Part: EEL ASSY — DEFECTIVE (CABIN)

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

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

ANC - PRIOR TO DEPARTURE OF FLIGHT NR 7831, CREW REPORTED ONE SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS IN MAIN CABIN WERE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL BATT PACK — DISCHARGED (CABIN)

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

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EXIT LIGHT WOULD NOT EXTINGUISH AFTER TEST. REPLACED THE BATTERY PACK AND LIGHT OPERATED NORMALLY. (M)

Part: EEL BATTERY — DISCHARGED (CABIN)

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

Part: EEL BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, TWO WHITE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 5. REPLACED BATTERY AND LIGHTS OPERATED NORMAL. (W)

Part: EEL BATT PACK — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS REMAINED ON AT ROWS 14 AND 15. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W)

Part: EEL BATTERY PACK — DEFECTIVE (CABIN)

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

Part: EEL RECEIVER — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, TWO EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 7 WERE FOUND INOPERATIVE. REMOVED AND REPLACED RECEIVER AT ROW 7 AND LIGHTS OPERATED NORMALLY. (W)

Part: HANDLE — FROZEN (L1 DOOR)

ANC - DURING MAINTENANCE CHECK, THE L1 DOOR EXTERIOR HANDLE WOULD NOT OPEN DOOR. HEATED AND LUBRICATED DOOR HANDLE, OPERATED NORMALLY. (W)

Part: DOOR HANDLE — STIFF (FWD CABIN)

ANC - DURING CHECK, THE LT FWD ENTRY DOOR HARD TO LATCH. MAINTENANCE ADJUSTED DOOR UPPER GUIDE ARM. (W)

Part: EEL ASSY — DEFECTIVE (CABIN)

SEA - FLT 65 - PRIOR TO DEPARTURE, CREW REPORTED THE FWD BULKHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED 'EXIT TO REAR' LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (W)