N947AS

Part: FLOOR PANEL — CORRODED (BS 160-200) · airframe 51,970 hrs · 27,953 cycles

CABIN FLOOR PANEL HAS BROKEN AND CORRODED INSERTS. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG 9936582.

Part: SKIN — CHAFED (FLAP VANE) · airframe 51,970 hrs · 27,953 cycles

RIGHT WING OUTBOARD FLAP INBOARD VANE IS CHAFED ON LEADING EDGE. SMOOTHED CHAFED AREA. INSTALLED REPAIR DOUBLER PER SRM 57 01 57 03 AND 51 70 2.

Part: SKIN — DENTED (BS 1203-1212) · airframe 51,970 hrs · 27,953 cycles

FUSELAGE UNDER BELLY DENTED. COLD FORMED TO ORIGINAL CONTOUR PER EA 5330 02146.

Part: SKIN — DENTED (TE FLAPS) · airframe 51,970 hrs · 27,953 cycles

LEFT WING INBOARD FLAP OUTBOARD VANE HAS MULTIPLE DENTS ON LOWER SURFACE. REMOVED DAMAGED SECTION. INSTALLED SKIN FILLER AND REPAIR DOUBLER PER SRM 57 03.

Part: FLOOR PANEL — BROKEN (BS 160-180) · airframe 51,970 hrs · 27,953 cycles

CABIN FLOOR PANEL HAS BROKEN INSERTS. REPLACED FLOOR PANEL PER SRM 53 05.

Part: SKIN — DENTED (BS 1202-1209) · airframe 51,970 hrs · 27,953 cycles

FUSELAGE SKIN DENTED. COLD FORMED SKIN TO ORIGINAL CONTOUR. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53 04.

Part: FLOOR PANEL — BROKEN (FUSELAGE) · airframe 51,970 hrs · 27,953 cycles

CABIN FLOOR PANEL HAS BROKEN AND MISSING INSERTS. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG 9936582.

Part: SKIN — DENTED (FLAP VANE) · airframe 51,970 hrs · 27,953 cycles

RIGHT WING INBOARD FLAP OUTBOARD VANE HAS MULTIPLE DENTS ON LOWER SURFACE. REMOVED DAMAGED SECTION. INSTALLED SKIN FILLER AND REPAIR DOUBLER PER SRM 57 03.

Part: SKIN — CHAFED (FLAP VANE) · airframe 51,970 hrs · 27,953 cycles

LEFT WING OUTBOARD FLAP INBOARD VANE IS CHAFED ON EXISTING LEADING EDGE REPAIR. REMOVED EXISTING DAMAGED DOUBLER. INSTALLED REPLACEMENT REPAIR DOUBLER PER SRM 57 03 AND 51 70 2.

Part: FLOOR PANEL — CORRODED · airframe 51,970 hrs · 27,953 cycles

CABIN FLOOR PANEL IS CORRODED AND HAS MISSING INSERTS. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG 9936582.

Part: SKIN — DENTED (FLAP VANE) · airframe 51,970 hrs · 27,953 cycles

LEFT WING INBOARD FLAP INBOARD VANE LOWER SURFACE HAS MULTIPLE DENTS AT EXISITNG REPAIR. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREAS OF VANE SKIN AND CORE. INSTALLED CORE PLUG SKIN FILLER AND REPAIR DOUBLER.

Part: FLOOR PANEL — CORRODED · airframe 51,970 hrs · 27,953 cycles

CABIN FLOOR PANEL HAS BROKEN AND CORRODED INSERTS. REPLACED FLOOR PANEL PER SRM 53 05.

Part: FLOOR PANEL — DELAMINATED (BS 200-256) · airframe 51,970 hrs · 27,953 cycles

CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG 9936582.

Part: FLOOR PANEL — CORRODED (BS 146-160) · airframe 51,970 hrs · 27,953 cycles

CABIN FLOOR PANEL HAS CRACKED AND MISSING INSERTS. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG 9936582.

Part: SEAT TRACK — CORRODED (BS 219-222) · corrosion level 1 · airframe 51,970 hrs · 27,953 cycles

FOUND SEAT TRACK CORRODED. REMOVED DAMAGED SECTION OF TRACK. INSTALLED REPAIR CHANNEL AND PLUG PER SRM 53 05.

Part: SKIN — DENTED (PAX DOOR)

GATE-MAIN PAX (L-1) DOOR FORWARD CORNER DENTED BY JETWAY. REPAIRED DENT IAW SRM. (K)

Part: SKIN — DENTED (FS 222)

OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. COLD-WORKED DENTED AREA. INSTALLED INTERNAL REPAIR DOUBLER. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND RIGHT CUSP WEB CORRODED. REMOVED CORRODED SECTION. INSTALLED REPAIR DOUBLER. (M)

Part: SKIN — DENTED (FS 471-487)

OKC - DUIRNG C-CHECK, FOUND FUSELAGE SKIN DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M)

Part: CUSP WEB — CRACKED (FS 1281)

OKC - DURING C-CHECK, FOUND RIGHT CUSP WEB CRACKED. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLER. (M)

Part: FLOOR PANEL — PUNCTURED (FS 541-617)

OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL IS PUNCTURED. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — DAMAGED (CABIN)

OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL IS CREASED ACROSS TOP. REPLACED FLOOR PANEL. (M)

Part: STIFFENER — CHAFED (FS 465-541)

OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL IS CHAFED ON LOWER SURFACE BONDED STIFFENER. REPLACED FLOOR PANEL STIFFENER, HAT CHANNEL. (M)

Part: CUSP WEB — CORRODED (FS 1098-1117)

OKC - FOUND DURING C-CHECK, RIGHT CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INTALLED REPAIR DOUBLER. (M)

Part: LONGERON — DAMAGED (FS 756)

OKC - DURING C-CHECK, FREEZE PLUG IN OVERSIZED HOLE IN LONGERON. REMOVED DAMAGED SECTION. SPLICED IN NEW LONGERON SECTION. (M)

Part: SKIN — DAMAGED (FS 1100)

OKC - FOUND DURING C-CHECK, ELONGATED FASTENER HOLE IN FUSELAGE. REMOVED DAMAGED AREA. INSTALLED INTERNAL REPAIR DOUBLER. (M)

Part: CUSP WEB — CORRODED (FS 1060-1079)

OKC - DURING C-CHECK, FOUND RIGHT CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M)

Part: SKIN — DAMAGED (FS 756)

OKC - DURING C-CHECK, FOUND FREEZE PLUG IN FUSELAGE SKIN OVERSIZED HOLE. REMOVED DAMAGED AREA. INSTALLED EXTERNAL REPAIR DOUBLER. (M)

Part: SKIN — DENTED (FS 569-588)

OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. COLD-WORKED DENTED AREA. INSTALLED INTERNAL REPAIR DOUBLER. (M)

Part: CUSP WEB — CORRODED (FS 237-313)

OKC - DURING C-CHECK, FOUND RIGHT UPPER CUSP WEB CORRODED. REMOVED CORRODED SECTION. INSTALLED REPAIR DOUBLER. (M)

Part: CUSP WEB — CORRODED (FS 522-579)

OKC - DURING C-CHECK, FOUND RIGHT CUSP WEB CORRODED. REPLACED CUSP WEB. (M)

Part: FLOOR PANEL — CHAFED (FS 465-522)

OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M)

Part: CUSP WEB — CORRODED (FS 598-712)

OKC - DURING C-CHECK, FOUND RIGHT CUSP WEB CORRODED. REPLACED CUSP WEB. (M)

Part: STIFFENER — DENTED (FS 693-827)

OKC - FOUND C-CHECK, CABIN FLOOR PANEL STIFFENER, HAT CHANNEL, DENTED. REPLACED HAT CHANNEL. (M)

Part: SKIN — DAMAGED (FS 756)

OKC - FOUND DURING C-CHECK, FREEZE PLUG IN FUSELAGE SKIN. INSTALLED EXTERNAL REPAIR DOUBLER. (M)

Part: CUSP WEB — CORRODED (FS 965-984)

OKC - DURING C-CHECK, FOUND RIGHT CUSP WEB CORRODED. REMOVED CORRODED SECTION. INSTALLED REPAIR DOUBLER. (M)

Part: CUSP WEB — CORRODED (FS 237-313)

OKC - DURING C-CHECK, FOUND RIGHT CUSP WEB CORRODED. REMOVED CORRODED SECTION. INSTALLED REPAIR DOUBLER. (M)

Part: CUSP WEB — CORRODED (FS 522-579)

OKC - DURING C-CHECK, FOUND RIGHT CABIN FLOOR CUSP WEB IS CORRODED. REPLACED WEB. (M)

Part: CUSP WEB — CORRODED (FS 598-712)

OKC - DURING C-CHECK, FOUND RIGHT FUSELAGE CUSP WEB IS EXFOLIATED CORRODED. REPLACED WEB. (M)

Part: SKIN — GOUGED (FS 1305)

OKC - FOUND DURING C-CHECK, FUSELAGE IS GOUGED. REPLACED EXISTING REPAIR DOUBLER. (M)

Part: CUSP WEB — CRACKED (FS 1281)

OKC - DURING C-CHECK, FOUND RIGHT CUSP WEB CRACKED. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLER. (M)

Part: SKIN — DENTED (FS 569-588)

OKC - DURING C-CHECK, FOUND FUSELAGE IS DENTED. COLD-WORKED DAMAGED AREA AND INSTALLED REPAIR DOUBLER. (M)

Part: SKIN — DENTED (FS 471-487)

OKC - DURING C-CHECK, FOUND RIGHT FUSELAGE IS DENTED. REMOVED DAMGAED AREA. INSTALLED REPAIR DOUBLER. (M)

Part: CUSP WEB — CORRODED (FS 1098-1117)

OKC - DURING C-CHECK, FOUND RIGHT CUSP WEB IS CORRODED. REMOVED DAMAGED SECTION OF WEB AND INSTALLED REPAIR DOUBLER. (M)

Part: CUSP WEB — CORRODED (FS 1060-1079)

OKC - DURING C-CHECK, FOUND RIGHT CABIN FLOOR CUSP WEB IS CORRODED. REMOVED DAMAGED SECTION OF WEB AND INSTALLED REPAIR DOUBLER. (M)

Part: LONGERON — DAMAGED (FS 756)

OKC - FOUND DURING C-CHECK, FREEZE PLUG IN LONGERON. REMOVED DAMAGED SECTION AND SPLICED IN NEW SECTION. (M)

Part: SKIN — DENTED

OKC - DURING C-CHECK, FOUND FUSELAGE IS DENTED. COLD-WORKED DAMAGED AREA AND INSTALLED REPAIR DOUBLER. (M)

Part: SKIN — DENTED (FS 1174)

OKC - FOUND DURING C-CHECK, AFT CARGO BAY DOOR SKIN IS DENTED. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M)

Part: FLOOR PANEL — CHAFED (FS 465-541)

OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL HAS CHAFE MARKS ON LOWER SURFACE BONDED STIFFENER. REPLACED STIFFENER. (M)

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

SEA - PREFLIGHT CHECK, AFT SERVICE L2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)

Part: LANYARD — DISCONNECTED (R1 DOOR) · airframe 46,207 hrs · 25,091 cycles

PRE-FLIGHT CHECK - FWD SERVICE (R-1) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (K)

Part: WINDOW — STUCK (COCKPIT)

YVR - PREFLIGHT CHECK, FOUND RIGHT FIRST OFFICERS SLIDING CLEARVIEW WINDOW COULD NOT OPEN. RESECURED UPPER CAM FOLLOWER IN TRACK. WINDOW THEN OPERATED PROPERLY. (M)

Part: WINDOW — STUCK (COCKPIT)

DURING PREFLIGHT CHECK, FOUND RIGHT FIRST OFFICERS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. REPOSITION FORWARD UPPER ALIGNMENT PIN IN TRACK. WINDOW THEN OPERATED PROPERLY. (M)

Part: WINDOW — STUCK (COCKPIT)

SEA - DURING PREFLIGHT CHECK, RIGHT FIRST OFFICERS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. REINSTALLED LOCK/UNLOCK PIN IN LINK. WINDOW THEN OPERATED PROPERLY. (M)

Part: WINDOW — STUCK (COCKPIT)

SEA - DURING PREFLIGHT CHECK, RIGHT FIRST OFFICERS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED GUIDE PIN IN UPPER LEFT CORNER. WINDOW THEN OPERATED PROPERLY. (M)

Part: WINDOW — STUCK (COCKPIT)

LAX - PREFLIGHT CHECK, RIGHT FIRST OFFICERS SLIDING CLEARVIEW WINDOW WOULD NT OPEN. REALIGNED WINDOW. WINDOW THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (L2 DOOR SLIDE)

SEA - AFT SERVICE L-2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)

Part: PANEL — DELAMINATED (FUSELAGE)

OKC - DURING C-CHECK, FOUND LEFT LOWER VOR ANTENNA PANEL IS DELAMINATED. REMOVED AND REPLACED DAMAGED SECTION PER EA 3450-01028. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING C-CHECK, FOUND INTERCOSTAL IS CRACKED ON UPPER FLANGE AT FS 1287-1307. REPLACED INTERCOSTAL PER SRM 51-30-2. (M)

Part: TIE — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND FRAME TIE CORRODED AT FS 1098 BETWEEN LONGERON 27L-28L. REMOVED DAMAGED AREA. INSTALLED FILLER AND REPAIR ANGLES PER SRM 51-70-5. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND LONGERON 28R IS CORRODED AROUND FASTENERS AT FS 1039-1046. REMOVED DAMAGE AND INSTALLED DOUBLER AND TRIPLER PER EA 5310-02369. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND INTERCOSTAL IS CORRODED AT FS 1211-1231 AT LONGERON 29L. REPLACED INTERCOSTAL PER SRM 51-30-5. (M)

Part: FRAME — CORRODED (FUSLEAGE)

OKC - FOUND DURING C-CHECK, FRAME IS CORRODED AT NUMBER LOCATIONS BETWEEN LONGERON 28L AND 28R AT FS 1079. REMOVED DAMAGED AREA AND INSTALLED DOUBLER AND FILLER PER SRM 53-03. (M)

Part: SPLICE — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND L30 SPLICE AT STATION 585 IS CORRODED. REMOVED DAMAGED SPLICE AND INSTALLED NEW IAW 51-30-5. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

OKC - FOUND DURNG C-CHECK, LEFT INTERCOSTAL IN AFT PIT AT STATION 1307-1322 IS CRACKED. REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW IAW 51-30-2. (M)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

OKC - DURING C-CHECK, FOUND OVERWING EMERGENCY EVACUATION LIGHT INOPERATIVE. REPLACED ASSOCIATED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

SEA - PREFLIGHT CHECK, FOUND FORWARD AFT SERVICE DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)

SEA PREFLIGHT CHECK, FRONT EMERGENCY FLOOR TRACK LIGHT INOPERATIVE. RECONNECTED WIRING. LIGHTS THEN OPERATED PROPERLY. (M)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

SEA PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 21. RECONNECTED LOOSE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)

ONT PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT WIRING DISCONNECTED AT ROW 6. RECONNECTED WIRING AT ROW 6. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (SLIDE)

SAN PREFLIGHT CHECK, FOUND FORWARD PAX L-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)

Part: FAIRING — CRACKED (STABILIZER)

OAK - DURING 15K CHECK, FOUND RIGHT STABILIZER OUTBOARD LOWER HINGE FAIRING IS BENT AND CRACKED. REPLACED FAIRING PER SRM 51-30-1. (M)

Part: PLENUM — WORN (RT HEAT EXCHANGE)

OAK - DURING 15K CHECK, FOUND RIGHT HEAT EXCHANGER PLENUM AREA WORN THROUGH DUE TO RUBBING ON EXIT DUCT. CUT OUT DAMAGED AREA AND WELDED IN A DOUBLER PER DRS 10.225. (M)

Part: LINK — CORRODED (RUDDER LIMITER)

OAK - FOUND DURING 15K CHECK, RUDDER THROW LIMITER LINK IS CORRODED. REPLACED LINK PER MM 27-20-06. (M)

Part: CRANK ASSY — CORRODED (RUDDER LIMITER)

OAK - FOUND DURING 15K CHECK, RUDDER THROW LIMITER CRANK ASSY IS CORRODED. REPLACED CRANK ASSY PER MM 27-20-06. (M)

Part: DOOR — CRACKED (LT NACELLE)

OAK - FOUND DURING 15K CHECK, LEFT ENGINE NACELLE CRACKED ON UPPER DOOR. REPLACED DAMAGED SECTION ARE REPAINTED PER SRM 51-10 AND EA 5410-0054. (M)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING 15K CHECK, FOUND MID CARGO BAY BARRIER DOOR SUPPORT BEAM CRACKED ON INBOARD SIDE. INSTALLED DOUBLERS ON BEAM PER SRM 52-10. (M)

Part: FAIRING — CRACKED (HORIZONTAL STAB)

OAK - DURING 15K CHECK, FOUND LEFT HORIZONTAL STAB FAIRING CRACKED AT ATTACH POINT. INSTALLED DOUBLER PER EA 5520-01156 AND SRM'S 51-10-3 AND 55-03. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND FLOOR SUPPORT CRACKED IN FORWARD PASSENGER COMPARTMENT NEAR FLIGHT ATTENDANT SEAT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 51-30-2. (M)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND MID CARGO BAY BARRIER DOOR SUPPORT BEAM IS CRACKED. INSTALLED DOUBLER ON BEAM PER SRM 51-10-3. (M)

Part: SUPPORT — CORRODED (CARGO TRACK)

OAK - DURING 15K CHECK, FOUND AFT CARGO BAY TIE DOWN TRACK SUPPORT IS CORRODED AT FS 1117 BETWEEN LONGERON 28R AND 27R. REPLACED TIE DOWN TRACK SUPPORT PER SRM 51-10-4 AND 30-5. (M)

Part: SHIM — CORRODED (DOOR SILL)

OAK - FOUND DURING 15K CHECK, PASSENGER L1 DOOR SILL DRAIN SHIM CORRODED. REPLACED SHIM PER SRM 51-10-4. (M)

Part: ATTACH BRACKET — CRACKED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND TRIM AND LOAD FEEL CENTERING SPRING ACTUATOR ATTACH BRACKET IS CRACKED AT FS 1485. REPLACED BRACKET PER SRM 51-10-3 AND 10-4. (M)

Part: BRACKET — CORRODED (FUSLEAGE)

OAK - FOUND DURING 15K CHECK, RUDDER YAW DAMPNER ACTUATOR ATTACH BRACKET CORRODED. REPLACED BRACKET PER MM 20-30-01. (M)

Part: ATTACH BRACKET — CRACKED (FUSELAGE)

OAK - FOUND DURING 15K CHECK, E/E ATTACH ANGLE BRACKET IS CRACKED AT AFT SIDE OF TERMINAL END OF LONGERON 7R AT FS 1463. REPLACED BRACKET PER SRM 51-10-2 AND 30-5. (M)

Part: ATTACH ANGLE — CORRODED (FUSELAGE)

OAK - FOUND 15K CHECK, ATTACH ANGLE IS CORRODED BETWEEN FS 1212 AND 1222 OUTBOARD OF LONGERON 30 IN AFT CARGO BAY. REPLACED ATTACH ANGLE PER SRM 51-10-3 AND 4. (M)

Part: FLOOR PANEL — CORRODED (FUSLEAGE)

OAK - FOUND DURING 15K CHECK, E/E FLOOR PANEL IS CORRODED AT FS 160-218. REPLACED SUPPORT PER SRM 53-01 AND 51-30-2. (M)

Part: TRANSITION PANEL — CORRODED (CARGO BAY)

OAK - FOUND DURING 15K CHECK, AFT CARGO BAY TRANSITION PANEL IS CORRODED. REPLACED PANEL PER SRM 51-10-4. (M)

Part: SUPPORT BRACKET — CRACKED (RT FUEL LINE)

OAK - FOUND DURING 15K CHECK, RIGHT FUEL TANK FUEL LINE SUPPORT BRACKET IS CRACKED ON OUTBOARD SIDE. REPLACED SUPPORT BRACKET PER SRM 51-30-1 AND 10-4. (M)

Part: FLOOR SUPPORT — CORRODED (E/E BAY)

DURING 15K CHECK, E/E FLOOR SUPPORT IS CORRODED AT FS 180-190. REPLACED SUPPORT PER SRM 53-01 AND 51-30-2. (M)

Part: STRAP — CRACKED (SIDEWALL SUPPORT)

OAK - FOUND DURING 15K CHECK, FORWARD CARGO BAY LEFT SIDEWALL SUPPORT STRAP CRACKED. REPLACED SUPPORT PER SRM 53-01. (M)

Part: SKIN — DENTED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND LOWER FUSELAGE IS DENTED AT FS 294 AT LONGERON 29L. INSTALLED DOUBLER PER SRM 53-04, 51-30-5, AND 51-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND FLOOR SUPPORT CORRODED AT FS 1117 AT FASTENER HOLES. REPLACED SUPPORT PER SRM 51-10-4. (M)

Part: SPLICE — CORRODED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND SPLICE IS CORRODED AT LONGERON 28L BETWEEN FS 1174 AND 1187 IN AFT CARGO BAY. REPLACED SPLICE PER SRM 51-30-5 AND 10-4. (M)

Part: SKIN — DENTED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND OUTER FUSELAGE DENTED FROM FS 275-294 AT LONGERON 29 LOCATION. CUT OUT DENTED AREA. INSTALLED DOUBLER AND SKIN PLUG PER SRM 53-04. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND FLOOR WEB CRACK AT FS 1250 UNDER SEAT 32 F/D. STOP DRILLED CRACK AND INSTALLED DOUBLER AT RIGHT CUSP MEMBRANE WEB. (M)

Part: WEB — CRACKED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND FLOOR MEMBRANE CRACKED AT FS 1293 ON RIGHT SIDE, OUTBOARD OF OUTBOARD TRACK. CUT OUT DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 53-05. (M)

Part: MEMBRANE — CRACKED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND FLOOR MEMBRANE CRACKED AT FS 1322, OUTBOARD OF OUTBOARD SEAT TRACK. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01. (M)

Part: WEB — CRACKED (FUSELAGE)

OAK - DURING 15K CHECK, FUSELAGE MEMBRANE WEB CRACKED IN TWO PLACES AT FS 1293. STOP DRILLED AND INSTALLED DOUBELR EPR SRM 53-05. (M)

Part: BRACKET — CRACKED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND RIGHT OVERWING TO BODY FAIRING SUPPORT BRACKET IS CRACKED. REPLACED BRACKET PER SRM 51-10-04, 30-2 AND 10-3. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND FLOOR SUPPORT CORRODED AT FS 256. REPLACED SUPPORT PER SRM 51-30-5. (M)

Part: DOOR — CRACKED (MLG)

OAK - DURING 15K CHECK, FOUND RIGHT MLG DOOR AFT OUTBOARD CORNER CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 52-05. (M)

Part: DOOR — CRACKED (MLG)

OAK - DURING 15K CHECK, FOUND LEFT MLG DOOR CRACKED AT OUTBOARD CORNER. REPLACED EXISTING CORNER DOUBLER PER SRM 52-04. (M)

Part: FITTING — CRACKED (FLOOR SUPPORT)

OAK - DURING 15K CHECK, FOUND FLOOR SUPPORT FITTING BETWEEN PANELS C1 AND C2 IS CRACKED. REPLACED FITTING PER SRM 51-30-5. (M)

Part: FITTING — CRACKED (FLOOR SUPPORT)

OAK DURING 15K CHECK, FOUND FLOOR SUPPORT FITTING BETWEEN PANELS C1 AND C2 IS CRACKED. REPLACED FITTING PER SRM 51-30-5. (M)

Part: CONNECTOR — DISCONNECTED (FWD CABIN)

DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE AT ROWS 1-3. REATTACHED CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: CONNECTOR — LOOSE (CABIN)

SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS IN 1ST CLASS CABIN INOPERATIVE. REATTACHED LOOSE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LANYARD — DETACHED (EVAC SLIDE)

PDX - DURING PREFLIGHT CHECK, THE FORWARD DOOR EMERGENCY SLIDE 'ACTIVATION CABLE' LANYARD WAS FOUND TO BE LOOSE. REATTACHED LANYARD. (M)

Part: CONNECTOR — LOOSE (CABIN)

SJC - DURING PREFLIGHT CHECK, EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN FORWARD CABIN. RECONNECTED LOOSE MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — DISCONNECTED (CABIN)

SEA - DURING PREFLIGHT CHECK, EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED LOOSE MODULE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — DISCONNECTED (CABIN)

SAN - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED LIGHT MODULE AT ROW 3. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — INOPERATIVE (CABIN)

PDX - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE FORWARD OF ROW 3. RECONNECTED DISCONNECTED LIGHT MODULE AND REPLACED ANOTHER. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING PREFLIGHT CHECK, FOUND FIRST FIVE EMERGENCY TRACK LIGHTS INOPERATIVE. RECONNECTED LIGHTS. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 28. RECONNECTED LIGHTS. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — INOPERATIVE (CABIN)

SEA - DURING LINE CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE FROM ROW 22 TO 30. REPLACED FOUR LIGHT MODULES. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — DISCONNECTED (FWD CABIN)

SEA - DURING PREFLIGHT CHECK, FOUND INOPERATIVE EMERGENCY TRACK LIGHTS IN 1ST CLASS CABIN. RECONNECTED LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LIGHT — BROKEN (CABIN)

SEA - DURING PREFLIGHT CHECK, FOUND TWO INOPERATIVE EMERGENCY TRACK LIGHTS AT ROWS 29 AND 33. REPLACED BROKEN LIGHT MODULES. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WIRE — DISCONNECTED (FWD CABIN)

PDX - DURING LINE CHECK, FIRST CLASS EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED EMERGENCY TRACK LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND CORROSION AROUND FASTENERS ON LONGERON 30 FROM FUSELAGE STATION 1003 TO 1070 IN AFT CARGO BAY. REMOVED DAMAGED SECTION. SPLICED IN NEW SECTION PER EA 5310-02049. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING PREFLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN CABIN (PRECISE LOCATION UNSPECIFIED). REPLACED DISCHARGED BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

LAX - DURING PREFLIGHT CHECK, FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. RECONNECTED LIGHT MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: HOOK — OUT OF ADJ (L1 DOOR)

SEA - DURING PREFLIGHT CHECK, IT WAS DETERMINED THAT THE DOOR HOLD OPEN LATCH DOES NOT ALWAYS LINE UP WITH PIN. ADJUSTED HOLD-OPEN HOOK PER MM 52-11-00, PP 511-512A, STEPS 1-6. MECHANISM THEN OPERATED PROPERLY. (M)

Part: LATCH — BROKEN (CABIN)

PDX - DURING PRE-FLIGHT CHECK, FOUND ONE OF THE TWO L2 GIRT BAR LATCHES ON THE FLOOR BROKEN. REPLACED BROKEN LATCH. GIRT BAR INSERTION COULD THEN BE DONE PROPERLY. (M)

Part: CONNECTOR — LOOSE (CABIN)

ANC - DURING PRE-FLIGHT CHECK, FOUND 1ST CLASS CABIN EMERGENCY TRACK LIGHTING TO BE INOPERATIVE. RECONNECTED LOOSE TRACK LIGHT MODULE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M)

Part: CONNECTOR — LOOSE (CABIN)

FLT 237 - DURING FLIGHT, FLIGHT ATTENDANT ACCIDENTALLY TURNED ON EMERGENCY LIGHTS AND DISCOVERED THAT TRACK LIGHTS IN THE 1ST CLASS CABIN TO BE INOPERATIVE. RECONNECTED LOOSE TRACK LIGHT MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

SEA - DURING PRE-FLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED LOOSE CONNECTOR TO FLOOR TRACK LIGHTS MODULES. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. REMOVED AND REPLACED FLOOR TRACK LIGHT MODULES. LIGHTS THEN OPERATED PROPERLY. (M)

Part: BATTERY — DISCHARGED (COCKPIT)

LAX - DURING PREFLIGHT, COCKPIT EMERGENCY EXIT LIGHTS FOUND INOPERATIVE. REPLACED BATTERIES. EXIT LIGHTS OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 13 TO 16. REPAIRED BROKEN WIRES AND TRACK COVERS. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

PDX - DURING PRE-FLIGHT CHECK, EIGHT EMERGENCY FLOOR TRACK LIGHTING MODULES WERE DETERMINED TO BE INOPERATIVE IN THE FIRST CLASS CABIN. REPLACED DEFECTIVE EMERGENCY FLOOR TRACK LIGHTING MODULES. LIGHT THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING LINE CHECK, EMERGENCY FLOOR TRACK LIGHTING MODULE WAS DETERMINED TO BE INOPERATIVE, WIRES WERE BROKEN. REPLACED EMERGENCY FLOOR TRACK LIGHTING MODULE. LIGHT THEN OPERATED PROPERLY. (M)

Part: LIGHT — DISCONNECTED (CABIN)

SEA - DURING PREFLIGHT CHECK, EMERGENCY FLOOR TRACK LIGHTING MODULE WAS DETERMINED TO BE UNPLUGGED AND INOPERATIVE. RECONNECTED EMERGENCY FLOOR TRACK LIGHING MODULE. LIGHT THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 32. REMOVED AND REPLACED FLOOR TRACK MODULE. OPERATIONAL CHECKS NORMAL. (M)

Part: LIGHT — DISCONNECTED (CABIN)

SEA - DURING PREFLIGHT CHECK, 1ST CLASS CABIN EMERGENCY FLOOR TRACK LIGHTS AT ROW 3 WERE DETERMINED TO BE INOPERATIVE. REATTACHED TRACK ELECTRICAL CONNECTIONS. LIGHTS THEN OPERATED NORMALLY. (M)

Part: LIGHT — DISCONNECTED (CABIN)

LAX - DURING PREFLIGHT CHECK, SOME OF THE 1ST CLASS CABIN EMERGENCY FLOOR TRACK LIGHTS WERE DETERMINED TO BE INOPERATIVE. REATTACHED TRACK ELECTRICAL CONNECTIONS. LIGHTS THEN OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTING AT ROW 24-27 WAS DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY ASSEMBLY. LIGHTS THEN OPERATED NORMALLY. (M)

Part: WIRE — LOOSE (1ST CLASS CABIN) · airframe 33,441 hrs · 18,728 cycles

SFO-DURING PREFLIGHT CHECK, A SECTION OF EMERGENCY TRACK LIGHTING IN THE 1ST CLASS CABIN AT SEAT 1D WAS DETERMINED TO BE INOPERATIVE. RE-SECURED LOOSE WIRING, LIGHTS OPERATED NORMALLY.

Part: MODULE — LOOSE (CABIN)

SJD - DURING PREFLIGHT CHECK, A SECTION OF EMERGENCY TRACK LIGHTING IN THE 1ST CLASS CABIN AREA WAS DETERMINED TO BE INOPERATIVE. RE-SECURED LOOSE WIRING. LIGHTS THEN OPERATED NORMALLY. (M)

Part: POWER SUPPLY — DISCHARGED (FWD CABIN)

OAK - PRIOR TO FLIGHT 399, THE EMERGENCY EXIT LIGHT IN THE FLIGHT DECK DID NOT ILLUMINATE WITH SWITCH ON. REPLACED THE POWER SUPPLY AND THE LIGHT OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - PRIOR TO FLIGHT 445 - THE FLIGHT STATION EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATE NORMALLY. (M)

Part: FLASHLIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE PORTABLE EMERGENCY EXIT LIGHT AT THE L-1 DOOR WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: HANDLE — LACK OF LUBE (PAX DOOR)

SEA - ON ARRIVAL OF FLT 196, CREW REPORTED L-1 DOOR DIFFICULT TO OPEN, HANDLE APPEARS TO BE LOOSE. DOOR OPERATED NORMALLY. LUBRICATED DOOR HINGES, LATCH ROLLERS AND MECHANISM AS PRECAUTIONARY MEASURE. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD FOUR EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED CONNECTOR TO LIGHT ASSEMBLY IN FLOOR TRACK AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

PHX - PRIOR TO DEPARTURE OF FLT 721, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X)

Part: CONNECTOR — DISCONNECTED (CABIN)

SEA - FLT 198 - PRIOR TO DEPARTURE CREW REPORTED SOME EMERGENCY EXIT FLOOR TRACK LIGHTS IN THE FIRST CLASS CABIN WERE INOPERATIVE. FOUND APPROXIMATELY A SIX INCH SECTION OF THE MOUNTING TRACK MISSING FORWARD OF ROW 1 D-F. PERFORMED INTERIM REPAIR TO THE TRACK COVER, RECONNECTED THE CONNECTOR IN THE FLOOR TRACK AND THE LIGHTS OPERATED NORMALLY. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

PDX - FLT 503 - PRIOR TO DEPARTURE, CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED CONNECTOR IN FLOOR TRACK AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - FLT 444 - CREW REPORTED, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

ONT - RETURN TO GATE OF FLIGHT 439, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: LINER — LOOSE (L1 DOOR)

PDX - FLT 601 - AFTER ARRIVAL, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. FOUND DOOR INTERIOR LINER LOOSE AND CATCHING ON FORWARD FLIGHT ATTENDANT JUMP SEAT. INSTALLED MISSING FASTENER IN DOOR LINER AND OPERATED NORMALLY. (X)

Part: HINGE — DAMAGED (RT TE FLAP)

OAK - DURING 30K CHECK, DAMAGE WAS FOUND ON RT WING OUTBOARD FLAP INBOARD HINGE INBOARD UPPER ATTACH LUB. REPAIRED IAW ASA EA 5740-01168. (X)

Part: FITTING — CORRODED (LT SPOILER)

OAK - DURING 30K CHECK, FOUND CORROSION ON LEFT WING INBOARD FLIGHT SPOILER INBOARD HINGE BRACKET TRUNNION END BEARING LOCK BOLT HOLE. REPAIRED IAW ASA EA 5740-01170. (M)

Part: LONGERON — CORRODED (BS 1136-1146)

OAK - DURING 30K CHECK, FOUND CORROSION ON LONGERON 28R AT FS 1137. REPAIRED IAW ASA EA 5310-01689. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - PRIOR TO DEPARTURE OF FLT 622, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. REPAIRED BROKEN WIRE IN FLOOR TRACK AND OPERATED NORMALLY. (X)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS AT ROWS 24R AND 26L WERE INTERMITTENT. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: MECHANISM — LACK OF LUBE (SERVICE DOOR)

SEA - FLT 601 - AFTER ARRIVAL, CREW REPORTED THE R1 DOOR WAS DIFFICULT TO OPEN AND CLOSE. LUBED THE R1 DOOR MECHANISM AND OPERATED NORMALLY. AIRCRAFT TT: 23,499 HOURS. AIRCRAFT TC: 13,628. (X)

Part: LIGHT — BROKEN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. REPLACED LIGHT ASSEMBLY AT ROW 3 AND OPERATED NORMALLY. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

LAX - PRIOR TO FLT 513 - CREW REPORTED, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE IN FIRST CLASS. REINSTALLED LOOSE ELECTRICAL LIGHT CONNECTOR AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. REPLACED DEFECTIVE WIRING IN TRACK AND OPERATED NORMALLY. (M)

Part: LIGHT — BROKEN (CABIN)

SEA - PRIOR TO DEPARTURE OF FLIGHT 530, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. REPLACED LIGHT SOCKET ASSEMBLY AND TRACK COVER AND OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS AT ROW 24 RT AND 26 LT WERE FOUND INOPERATIVE. CLEANED LIGHT ASSEMBLY CONTACTS AND OPERATED NORMALLY. (M)

Part: SKIN — CRACKED (RT WING)

SEA - RIGHT WING LOWER SURFACE SKIN CRACKED AT FORWARD OUTBOARD RADIUS OF FUEL PANEL DOOR CUTOUT. REPAIRED PER ASA EA 5730-01047. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS AT ROWS 24 RIGHT AND 26 LEFT FLICKER. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS AT ROWS 24 AND 26 FLICKER OFF AND ON. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)

Part: LIGHT — DEFECTIVE (CABIN)

PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: LAMP MODULE — BROKEN (CABIN)

SEA - FLT 44 - TWO RED AND SIX WHITE EMERGENCY EXIT FLOOR TRACK LIGHTS IN FIRST CLASS SECTION WERE FOUND INOPERATIVE DURING PRE-FLIGHT CHECK. REPLACED TWO LAMP MODULE ASSEMBLIES AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 19 TO 21 WERE FOUND INOPERATIVE. REPAIRED WIRING AT ROW 19 AND OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (CABIN)

SJC - PRIOR TO DEPARTURE OF FLIGHT 419, CREW REPORTED THE EMERGENCY FLOR TRACK LIGHTS FROM ROWS 13 TO 16 WERE INOPERATIVE. REPAIRED WIRING AT ROW 13 AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SAN - PRIOR TO DEPARTURE OF FLT 511, CREW REPORTED ALL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. FOUND ALL EMERGENCY LIGHTS HAD BEEN LEFT IN OPERATION AND BATTERIES DISCHARGED. FERRIED AIRCRAFT TO SFO AND REPLACED THE BATTERIES FOR ALL INTERIOR EMERGENCY LIGHTS AND REPLACED THE POWER SUPPLY FOR THE EXTERIOR OVERWING EMERGENCY LIGHTS AND ALL OPERATED NORMALLY. (M)

Part: POWER SUPPLY — DEFECTIVE (CABIN)

SAN - PRIOR TO DEPARTURE OF FLT 511, CREW REPORTED ALL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. FOUND ALL EMERGENCY LIGHTS HAD BEEN LEFT IN OPERATION AND BATTERIES DISCHARGED. FERRIED AIRCRAFT TO SFO AND REPLACED THE BATTERIES FOR ALL INTERIOR EMERGENCY LIGHTS AND REPLACED THE POWER SUPPLY FOR THE EXTERIOR OVERWING EMERGENCY LIGHTS AND ALL OPERATED NORMALLY. REFERENCE ASAA9680260.

Part: WIRE — BROKEN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 29 TO 31 WERE FOUND INOPERATIVE. REPAIRED BROKEN WIRE AT ROW 31 AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (TAILCONE)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHT IN THE TAILCONE AREA WAS FOUND INOPERATIVE. REPAIRED BROKEN WIRING AND LIGHT OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (L1 DOOR)

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

Part: SEAT TRACK — CORRODED (Y1003-Y1322)

PAE - DURING 15K CHECK, CORROSION WAS FOUND ON SEAT TRACK AT Y1003 TO Y1322, X PLUS 45, Z MINUS 43. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 53-05. (M)

Part: SKIN DOUBLER — CORRODED (Y1168)

PAE - DURING 15K CHECK, CORROSION WAS FOUND ON EXTERNAL SKIN AT Y1168, LONGERON 29L TO 30L. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW ASA EA 5330-01208. (M)

Part: SUPPORT — CORRODED (Y769-Y788)

PAE - DURING 15K CHECK, CORROSION WAS FOUND ON CARGO TRACK SUPPORT NUTPLATE AT Y769 TO Y788, X-16, Z-46. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-60-00 AND 53-01. (M)

Part: SHEAR TIE — CORRODED (Y1231)

PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FRAME AND SHEAR TIE FASTENERS AT Y1231, X PLUS 12 TO X-7, Z-50. CORROSION REMOVAL ON FRAME FROM X PLUS 12 TO X-7 WAS WITHIN LIMITS, X-7 WAS OUT OF LIMITS. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-10-04 AND 53-01. (M)

Part: SHEAR TIE — CORRODED (Y1079)

PAE - DURING 15K CHECK, CORROSION WAS FOUND ON SHEAR TIE FASTENERS AT Y1079, Z-69 LONGERON 28L TO 28R. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-30-05, 53-01 AND 53-03. (M)

Part: FRAME — CORRODED (Y1271)

PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FRAME AT Y1271, X PLUS 19 TO X-19. CORROSION REMOVAL FROM X PLUS 19 TO X-14 WAS WITHIN LIMITS, X-14 TO X-19 WAS OUT OF LIMITS. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-20-00, 51-30-02 AND 53-03. (M)

Part: SKIN — CORRODED (Y788)

PAE - DURING 15K CHECK, CORROSION WAS FOUND ON EXTERNAL SKIN AT Y788, LONGERON 28R TO 29R. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 53-04. (M)

Part: CHANNEL — CORRODED (Y1211-Y1212)

PAE - DURING 15K CHECK, CORROSION WAS FOUND ON INTERCOSTAL CHANNEL AT Y1211 TO Y1212, X-3, Z-50. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-04. (M)

Part: EEL BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 14 TO 17 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL BATT PACK — DISCHARGED (L2 DOOR)

SEA - DURING SHOP INSPECTION OF L2 DOOR EMERGENCY EVACUATION SLIDE (REMOVED DUE TO TIME LIMIT) THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE WHEN SLIDE WAS DEPLOYED. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W)