N960AS

Part: SKIN — DAMAGED (BS 229-264) · airframe 51,611 hrs · 27,104 cycles

DENT IN FUSELAGE APPROX 4' FROM L1 DOOR AND 2' BELOW WINDOW BELT REMOVED DAMAGED AREA OF SKIN. FABRICATED AND INSTALLED REPAIR SECTION OF SKIN FINGER DOUBLERS SKIN SPLICE STRAP STRAPS IAW MD80 SRM 53 04 FIG 12C.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL TOP PLY PULLED LOOSE. BOND REPAIRED WITH GLASS CLOTH PER SRM 51-90-0.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,504 hrs · 26,554 cycles

FLOOR PANEL TOP PLY DISBONDED. BOND REPAIRED PANEL WITH GLASS CLOTH PER SRM 51-90-0.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL HAS CORRODED INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.

Part: INSERT — DAMAGED (FLOOR PANEL) · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL HAS BROKEN AND CORRODED INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL TOP PLY IS DISBONDED. BOND REPAIR PANEL WITH GLASS CLOTH PER SRM 51-90-0.

Part: INSERT — DAMAGED (FLOOR PANEL) · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL HAS CORRODED AND BROKEN INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 50,504 hrs · 26,554 cycles

FLOOR PANEL HAS CORRODED INSERTS. REPLACED PANEL PER SRM 53-24-0 AND 53-05.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,504 hrs · 26,554 cycles

FLOOR PANEL TOP PLY DISBONDED. BOND REPAIRED WITH GLASS CLOTH PER SRM 51-90-0.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL TOP PLY IS DISBONDED. BOND REPAIR WITH GLASS CLOTH PER SRM 51-90-0.

Part: FLOOR PANEL — DELAMINATED · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-24-0 AND 53-05.

Part: FLOOR PANEL — DELAMINATED · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.

Part: FLOOR PANEL — DELAMINATED · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-24-0 AND 53-05.

Part: SKIN — DENTED (BS 207-255) · airframe 50,504 hrs · 26,554 cycles

FUSELAGE SKIN DENTED. REPAIRED PER SRM 53-04.

Part: FLOOR PANEL — DELAMINATED · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND DAC DWG 9936640.

Part: VANE — CHAFED (TE FLAP) · airframe 50,504 hrs · 26,554 cycles

LEFTHAND WING OUTBOARD FLAP INBOARD VANE TRAILING EDGE IS CHAFED. REPAIRED DAMAGED AREA WITH BONDED FILLER AND DOUBLER PER SRM 51-70-2.

Part: SKIN — DAMAGED (BS 1253-1263) · airframe 50,504 hrs · 26,554 cycles

FUSELAGE SKIN CREASED AT PRIOR REPAIR. REMOVED EXISTING REPAIR DOUBLER RECONTOURED SKIN AND INSTALLED REPLACEMENT DOUBLER PER SRM 53-04.

Part: FLOOR PANEL — DELAMINATED · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND DAC DWG 9936640.

Part: FLOOR PANEL — DELAMINATED · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-24-0 AND 53-5.

Part: CUSP WEB — CRACKED (BS 218-237) · airframe 50,504 hrs · 26,554 cycles

CUSP WEB CRACKED. REPLACED WEB PER SRM 51-10-4 AMD 51-30-2.

Part: SKIN — DENTED (BS 1266-1278) · airframe 50,504 hrs · 26,554 cycles

FUSELAGE SKIN DENTED AT PREVIOUS REPAIR. REPLACED DAMAGED SECTION AND PREVIOUS REPAIR DOUBLER PER SRM 53-04.

Part: WEB — CORRODED (BS 170-199) · corrosion level 2 · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR MEMBRANE CORRODED. CUT OUT DAMAGED AREA AND INSTALLED REPLACEMENT WEB PER SRM 51-70-4 AND 51-30-2.

Part: FLOOR PANEL — DELAMINATED · airframe 50,504 hrs · 26,554 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-24-0 AND 53-05.

Part: SKIN — DENTED (PAX DOOR) · airframe 50,504 hrs · 26,544 cycles

FORWARD ENTRY DOOR IS DENTED. RECONTOURED DOOR SKIN AND INSTALLED INTERNAL DOUBLER PER SRM 53-04.

Part: SHEAR TIE — CORRODED (BS 1174) · airframe 46,594 hrs · 24,688 cycles

FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51 10 4 51 30 2 AND 51 30 5.

Part: CUSP WEB — CORRODED (BS 1098-1117) · airframe 46,594 hrs · 24,688 cycles

FOUND CUSP WEB CORRODED. REPLACED DAMAGED SECTION BY INSTALLING REPAIR DOUBLER PER SRM 51 70 4.

Part: INTERCOSTAL — CRACKED (BS 1287-1307) · airframe 46,594 hrs · 24,688 cycles

FOUND INTERCOSTAL CRACKED. REPLACED INTERCOSTAL PER SRM 51 10 4 51 30 2 AND 51 30 5.

Part: SKIN — DENTED (BS 1252-1257) · airframe 46,594 hrs · 24,688 cycles

FOUND FUSELAGE SKIN DENTED. COLD WORKED DAMAGED SECTION. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53 04.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 46,594 hrs · 24,688 cycles

AFT CARGO DOOR DENTED ON UPPER HALF. REPLACED DAMAGED SECTION OF DOOR SKIN BY INSTALLING EXTERNAL SPLICE PLATE AND TWO FINGER DOUBLERS PER ALASKA AIR EA 5230 01312.

Part: CUSP WEB — CORRODED (BS 1098-1117) · airframe 46,594 hrs · 24,688 cycles

FOUND CUSP WEB CORRODED. REPLACED DAMAGED SECTION BY INSTALLING REPAIR DOUBLER PER SRM 53 05 FIG 96 AND 51 01 PARA 3 B.

Part: WEB — CORRODED (BS 1155-1212) · airframe 46,594 hrs · 24,688 cycles

AFT CARGO BAY THRESHOLD WEB CORRODED. REPLACED WEB PER SRM 51 10 4 51 30 2 AND 51 30 5.

Part: SHEAR TIE — CORRODED (BS 693) · airframe 46,594 hrs · 24,688 cycles

FOUND FRAME SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51 10 04 AND 51 30 5.

Part: LONGERON — CORRODED (BS 1260-1320) · airframe 46,594 hrs · 24,688 cycles

FOUND LONGERON CORRODED. REPLACED DAMAGED SECTION OF LONGERON PER SRM 51 10 4 51 30 2 AND 51 30 5.

Part: INTERCOSTAL — CORRODED (BS 1307-1322) · airframe 46,594 hrs · 24,688 cycles

FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL PER SRM 51 10 4 AND 51 30 5.

Part: FRAME — CORRODED (BS 1322 S29LT RT) · airframe 46,594 hrs · 24,688 cycles

FOUND FRAME CORRODED. REPLACED DAMAGED SECTION OF FRAME BY INSTALLING FOUR REPAIR ANGLES AND FOUR SPLICE PLATES PER SRM 53 03 FIG 2A.

Part: SKIN — CORRODED (BS 1329-1334) · airframe 46,594 hrs · 24,688 cycles

FOUND FUSELAGE SKIN CORRODED. REPLACED DAMAGED SECTION BY INSTALLING REPAIR DOUBLER PER SRM 53 04.

Part: BEAM — CORRODED (BS 1155-1212) · airframe 46,594 hrs · 24,688 cycles

AFT CARGO DOOR CUTOUT LOWER BEAM CORRODED ON LOWER OUTBOARD FLANGE. REPLACED BEAM PER SRM 51 10 4 AND 51 30 5.

Part: INTERCOSTAL — CORRODED (BS 1150-1155) · airframe 46,594 hrs · 24,688 cycles

FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL PER SRM 51 10 4 AND 51 30 5.

Part: INTERCOSTAL — CORRODED (BS 1307-1322) · airframe 46,594 hrs · 24,688 cycles

FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL PER SRM 51 10 4 AND 51 30 2.

Part: SHEAR TIE — CORRODED (BS 1155) · airframe 46,594 hrs · 24,688 cycles

FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51 10 4 AND 51 30 5.

Part: WIRE — LOOSE (EMERGENCY LIGHT)

SEA LINE CHECK, AFT EXIT, CATWALK, PATH EMERGENCY LIGHT INOPERATIVE. RESECURED LOOSE WIRE CONNECTOR AND REPLACED LIGHT. LIGHT THEN OPERATED PROPERLY. (M)

Part: FLOOR PANEL — FRAYED (FUSELAGE)

OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD PANEL IS FRAYING. FIBERGLASS OVERLAY REPAIRED. (M)

Part: PANEL — CHAFED (VERTICAL STAB)

OKC - DURING C-CHECK, VERTICAL STABILIZER PANEL 6308C IS CHAFED. REPLACED PANEL. (M)

Part: RIB — CRACKED (RT WING LE)

OKC - FOUND C-CHECK, RIGHT WING L/E HAS CRACKED RIB. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLER. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD PANEL IS FRAYING. FIBERGLASS OVERLAY REPAIRED. (M)

Part: FLOOR PANEL — FRAYED (FUSELAGE)

OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD PANEL IS FRAYING. FIBERGLASS OVERLAY REPAIRED. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING C-CHECK, FOUND FUSELAGE DENTED NEAR RIGHT ENGINE COWL DRAIN MAST. COLD WORKED AND INSTALLED REPAIR DOUBLER. (M)

Part: STRUCTURE — CHAFED (CARGO DOOR)

OKC - DURING C-CHECK, FORWARD CARGO BAY DOOR FORWARD AND AFT LOWER EDGES CHAFED. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER. (M)

Part: SKIN — DELAMINATED (RUDDER)

OKC - DURING C-CHECK, FOUND RUDDER T/E IS DELAMINATED. FIBERGLASS BOND REPAIRED. (M)

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

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

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

LAX - DURING PREFLIGHT CHECK, FOUND FIRST CLASS CABIN EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE, BROKEN. RECONNECTED CONNECTOR. LIGHTS THEN OPERATED NORMALLY. (M)

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN TWO FORWARD CABIN LOCATIONS. RECONNECTED CONNECTORS IN BOTH LOCATIONS. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — DISCONNECTED (EMERGENCY LIGHT)

LAX - DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN FORWARD CABIN. RECONNECTED CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND FRAME CORRODED AT FS 1309. REMOVED DAMAGED SECTION. INSTALLED ANGLE, PLATE, AND SPLICES PER SRM 53-03. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD IS DELAMINATED AT FS 808-823. BOND-REPAIRED PER SRM 51-70-3. (M)

Part: FLOORBOARD — PUNCTURED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS PUNCTURE AT FS 920-1003. BOND-REPAIRED PER SRM 51-70-3. (M)

Part: FRAME — CHAFED (FUSELAGE)

OKC - DURNG 15K CHECK, FOUND FRAME CHAFED AT FS 1418. REMOVED DAMAGE. INSTALLED ANGLE, PLATE, AND FILLER PER SRM 53-03 AND 51-10-3. (M)

Part: SKIN — CRACKED (RT WING)

OKC - DURING 15K CHECK, FOUND RIGHT WING LEADING EDGE CRACKED. INSTALLED DOUBLER AND FILLER PER SRM 57-06 AND 51-10-3. (M)

Part: SKIN — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND INNER SKIN CORRODED AT FS 541-548 AND BETWEEN 30 AND 29L AT BODY DRAIN. REPAIRED PER SRM. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND CORROSION ON AND AROUND FASTENERS ON LONGERON 30, STATION 807 AFT TO TERMINATION AT FORWARD SPAR OF FUEL TANK. REPAIRED PER SRM, ASA EA 5310-02266, AND AAR EA 10108. (M)

Part: STRUCTURE — CRACKED (LAVATORY)

OKC - DURING 15K CHECK, FOUND CRACKS IN TRASH SHOOT ABOVE BOX IN RIGHT AFT LAV TRASH VANITY. REPAIRED PER SRM, ASA EA 2540-01113, AND AAR EA 10099. (M)

Part: SKIN — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND AFT CARGO COMPARTMENT STATION 1212, 28L UNDER LONGERON SPLICE CORRODED. REPAIRED PER SRM. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD STATION 808 TO 823, RBL 22 TO RBL 44 DELAMINATED AT CORNER. REPAIRED PER SRM. (M)

Part: SKIN — CRACKED (RT WING)

OKC - DURING 15K CHECK, FOUND RIGHT WING LEADING EDGE BETWEEN STATION XCW 121.688 AND XCW 104.500 CRACKED. REPAIRED PER SRM. (M)

Part: FLOORBOARD — PUNCTURED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD STATION 920 TO 1003, RBL 22 TO RBL 44 PUNCTURED. REPAIRED PER SRM. (M)

Part: FRAME — CHAFED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND AFT ACCESSORY TAIL FRAME CHAFFED AT STATION 1418, STRINGER 20R CHAFFED. REPAIRED PER SRM. (M)

Part: FRAME — CRACKED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND FRAME AT FS 1437 TOP AFT SIDE CRACKED AT FASTENER HOLE RIGHT SIDE OF LONGERON 1. REPAIRED PER SRM. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND AFT CARGO COMPARTMENT STATION 1309 AT LONGERON 30 FRAME CORRODED. REPAIRED PER SRM. (M)

Part: BRACKET — BROKEN (RT WING)

OKC - DURING 15K CHECK, FOUND RIGHT WING LEADING EDGE AT APPROX XRS 100 CABLE BRACKET BROKEN. REPAIRED PER ASA EA 5740-01365 AND AAR EA 10105. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING 15K CHECK, FOUND 1ST CLASS EMERGENCY FLOOR TRACK LIGHTS ILLUMINATE WHEN EXTERNAL POWER IS TURNED OFF, EVEN THOUGH EMERGENCY SWITCH REMAINS IN 'OFF' POSITION. REPLACED ASSOCIATED BATTERY PACK, POWER SUPPLY. LIGHTS THEN OPERATED PROPERLY. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN DENTED FORWARD OF NR 1 WINDOW. REMOVED EXISTING DOUBLER. INSTALLED NEW SKIN DOUBLER, FINER DOUBLER AND STRAPS PER SRM 53-04, 51-10-3, AND 51-30-2. (M)

Part: FLOORBOARD — CORRODED (CABIN)

OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 1134-1174. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: FLOORBOARD — WORN (FUSELAGE)

OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS WORN V-FLANGES AND U-CHANNELS AT FS 970-1003. REPLACED DAMAGED/WORN PARTS PER SRM 53-24-0, 51-30-8, AND 51-10-4. (M)

Part: INSERT — CORRODED (FLOORBOARD)

OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 160-180. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: INSERT — CORRODED (FLOORBOARD)

OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 180-200. REPLACED FLOORBOARD PER SRM 53-05 AND 51-10-4. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 1130. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: INSERT — CRACKED (FLOORBOARD)

OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS CRACKED INSERTS AT FS 160-200. REPLACED FLOORBOARD PER SRM 53-05 AND 51-10-4. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 1079-1155. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND FLIGHT COMPARTMENT FLOOR PANEL AT FS 158 HAS CORRODED FASTENERS AND WASHERS. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AND BROKEN FASTENERS AT FS 1134-1174. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND FORWARD LAVATORY FLOORBOARD EDGE DELAMINATED. REPAIRED SECTION WITH FIBERGLASS PER MM 25-41-13. (M)

Part: FLOORBOARD — DELAMINATED (CABIN FLOOR)

OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD IS DELAMINATED AT FS 200-256. BOND-REPAIRED EDGE PER SRM 51-90-0. (M)

Part: INSERT — CORRODED (FLOORBOARD)

OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 160-200. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - DURNG 15K CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 160-180. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN IS DENTED AT FS 725. INSTALLED DOUBLER PER SRM 53-04. (M)

Part: SKIN — CRACKED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND NOSE WHEELWELL LEFT AFT DOOR AFT HINGE CUTOUT OUTER SKIN IS CRACKED. STOP-DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-05. (M)

Part: FLOORBOARD — PUNCTURED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD IS PUNCTURED AT FS 1118-1160. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND PASSENGER CABIN FLOORBOARD IS CRACKED AT FS 820-920. REPLACED FLOOR PANEL PER SRM 51-10-4. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND SHEAR TIE IS CORRODED AT FS 1231 IN AFT CARGO BAY. REPLACED SHEAR TIE PER SRM 51-10-2, 3 AND 4. (M)

Part: SKIN — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN IS CORRODED UNDER DRAIN HOLE COVER AT FS 1293. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 53-04 AND 51-30-5. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND PASSENGER CABIN FLOORBOARD IS DELAMINATED AT FS 887-947. REPLACED FLOOR PANEL PER SRM 53-24. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND CUSP WEB IS CORRODED ON LOWER SIDE AT FORWARD OUTBOARD AT FS 731-750. INSTALLED DOUBLER PER SRM 51-70-4. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND RIGHT INBOARD SEAT TRACK IS CORRODED, EXFOLIATED, AT FS 220. REPLACED DAMAGED TRACK PER SRM 53-05, 53-20-1 AND 51-30-1. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD IS DELAMINATED AT FS 880-920. REPAIRED WITH FIBERGLASS OVERLAY PER SRM 51-70-3. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND PASSENGER FLOORBOARD IS CORRODED AT FS 256. REPLACED FLOOR PANEL PER SRM 53-05 AND 51-10-4. (M)

Part: FLOORBOARD — CORRODED (CABIN)

OKC - DURING 15K CHECK, FOUND FLIGHT DECK FLOOR PANEL FASTENERS AND WASHERS ARE CORRODED AT FS 155. REPLACED DAMAGED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOORBOARD — PUNCTURED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND PASSENGER CABIN FLOORBOARD IS PUNCTURED AT FS 1034-1060. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND FRAME IS CORRODED AT FS 1250. REPLACED DAMAGED FRAME SECTION PER SRM 53-03 AND 51-10-2. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND RIGHT OUTBOARD SEAT TRACK IS CORRODED, EXFOLIATED, AT FS 220. REPLACED DAMAGED TRACK PER SRM 53-05, 53-10-1, AND 51-30-1. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN DENTED AT FS 1263. INSTALLED REPAIR DOUBLER PER SRM 53-04. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN IS DENTED AT FS 1287. INSTALLED REPAIR DOUBLER PER SRM 53-04. 9M)

Part: SKIN — GOUGED (VERTICAL STAB)

OAK - FOUND C-CHECK, VERTICAL STABILIZER SKIN GOUGED AT UPPER ATTACH POINT FOR ELEPHANT EAR FAIRING. REPLACED DAMAGED SKIN PER SRM 51-10-4, 51-10-3, AND 51-30-2. (M)

Part: ANGLE — CORRODED (FUSELAGE)

OAK - FOUND C-CHECK CORROSION ON Z-ANGLE IN AFT CARGO BAY AT FS 1145-1155 ABOVE LONGERON 28R. REPLACED Z-ANGLE PER SRM 51-10-4, 51-10-3, 51-30-1, AND 51-30-2. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OAK - FOUND C-CHECK, CORRODED ON LONGERON 30 AT FS 1007. REPLACED DAMAGED SECTION PER EA 5310-02147. (M)

Part: SPLICE — CORRODED (FUSELAGE)

OAK - FOUND CORROSION ON C-CHECK, LONGERON 30 SPLICE SECTION AT FS 1200-1240 IN AFT CARGO BAY. REPLACED SPLICE SECTION PER BAC DWG 5936050, SRM 51-10-4, AND 51-30-5. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OAK - FOUND C-CHECK, FOUND CORROSION ON SCREW HOLES AND MOUNT SCREWS ON LEFT TIEDOWN TRACK IN AFT CARGO BAY AT FS 1007 TO 1307 ABOVE LONGERON 28L. REPLACED TIEDOWN TRACK PER SRM 51-10-4, 51-30-1, AND 51-10-3. (M)

Part: DOOR FRAME — WORN (FUSELAGE)

OAK - FOUND C-CHECK, FORWARD ACCESSORY COMPARTMENT DOOR JAMB FOUND WORN IN SEVERAL AREAS AROUND CIRCUMFERENCE. INSTALLED DOUBLER ON DOOR JAMB PER SRM 53-01 AND 53-10-3. (M)

Part: FRAME — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, AFT CARGO BAY FLOOR SUPPORT CIRCUMFERENTIAL FRAME CORRODED ON AFT SIDE AT FS 1271. REPLACED FRAME PER SRM 51-10-3, 51-C1, 53-C3, 51-10-4, AND 51-10-3B. (M)

Part: SPLICE — CORRODED (FUSELAGE)

OAK - FOUND C-CHECK, SPLICE CORRODED AROUND FASTENERS IN AFT CARGO BAY AT FS 1250-1271, L30. REPLACED SPLICE PER SRM 53-02, 51-10-4, 51-10-3, 51-10-3B, AND 51-30-5. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

OAK C-CHECK, RIGHT MLG AFT DOOR JAMB HAS 1 INCH CRACK AT UPPER END. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01, 51-10-2, AND 51-30-1. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: MECHANISM — DAMAGED (PAX DOOR)

PHX - L1 DOOR HOLD OPEN MECHANISM WILL NOT LATCH. STRAIGHTENED HOLD OPEN HOOK. DOOR NOW LATCHES OPEN NORMALLY. (M)

Part: BATTERY — DISCHARGED (PORTABLE LIGHT)

OAK - PREFLIGHT CHECK, FOUND FORWARD PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT BATTERY. LIGHT THEN OPERATED NORMALLY. (M)

Part: RECEPTACLE — DEFECTIVE (CABIN)

SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 2 AND 10. RELAMPED AT ROW 2 AND REPLACED RECEPTACLE AT ROW 10. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WINDOW (COCKPIT)

PDX - DURING PREFLIGHT CHECK, FIRST OFFICERS SLIDING CLEARVIEW WINDOW WAS DIFFICULT TO OPEN. LUBRICATED WINDOW TRACKS. WINDOW THEN OPERATED PROPERLY AND EASILY. (M)

Part: BATTERY PACK — DISCHARGED (TAILCONE)

PDX - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHT IN TAILCONE WAS DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACK AND REPAIRED WIRING. LIGHT THEN OPERATED PROPERLY. (M)

Part: ACM — FAILED (A/C BAY)

SEA - JUST AFTER TAKEOFF, BURNED RUBBER/INSULATION SMELL WAS NOTED IN COCKPIT. REOCCURRED DURING BEGINNING OF DESCENT. REPLACED LEFT COOLING TURBINE ASSY AND BOTH LEFT AND RIGHT COALESCER. PERFORMED AIR QUALITY CHECK AND NO ODOR WAS EVIDENT. (M)

Part: LIGHT — MISSING (CABIN)

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

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, INTERIOR EMERGENCY LIGHT OVER L2 DOOR WAS DETERMINED TO BE INOPERATIVE. REPLACED BATTERIES WITHIN ASSOCIATED BATTERY PACK. LIGHT THEN OPERATED NORMALLY. (M)

Part: LIGHT — DEFECTIVE (CABIN)

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

Part: SEAT TRACK — CORRODED (FUSELAGE)

PHX: DURING 30K CHECK CORROSION WAS FOUND SEAT TRACK, FS 200 TO 237, RBL 45.REMOVED AND REPLACED SEAT TRACK SECTION IAW DC9 SRM 53-05, FIG 4.

Part: SKIN — DAMAGED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND DENTS, GOUGES AND FASTENER SPACING DISCREPANCIES WERE FOUND IN LOWER AFT AREA OF THE L1 DOOR SURROUNDING SKIN PANELS AND INTERNAL DOOR JAMB DOUBLER, FS 188.5 TO 229, LONGERON 16L TO 21L. REPLACED THE UPPER SKIN ON THE AFT SIDE OF THE L1 DOOR, THE LOWER SECTION OF THE DOOR JAMB DOUBLER, THE UPPER AFT AREA OF THE LOWER SKIN PANEL, AND LONGERON 20L FROM FS 207 TO 229 IAW ASA EA 5330-01429 AND DC9 SRM 51-10-01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON FLOOR SUPPORT, FS 1155, BL 0. REMOVED AND REPLACED FLOOR SUPPORT SECTION IAW DC9 SRM 51-30. (M)

Part: SEAT TRACK — DAMAGED (CABIN)

PHX - DURING 30K CHECK, FOUND ON LEFT INBOARD SEAT TRACK, FS 1085 TO 1231, LBL 24. REMOVED AND REPLACED SEAT TRACK SECTION IAW DC9 SRM 53-05, FIG 4. (M)

Part: SKIN — DENTED (FUSELAGE)

PHX - DURING 30K CHECK, FUSELAGE SKIN WAS FOUND DENTED, FS 256, LONGERON 8R TO 9R, AND EXTERNAL DOUBLER WITH DISCREPANT OVER SIZE HOLES. ACCOMPLISHED EXTERNAL DOUBLER REPAIR IAW ASA EA 5330-01428 AND DC9 SRM 53-04, FIG 12B. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB, FS 218 TO 237, LBL 46 TO LBL 61. REMOVED AND REPLACED WEB IAW DC9 SRM 53-14-02, FIG 4. (M)

Part: SEAT TRACK — CORRODED (CABIN)

PHX - DURING 30K CHECK, FOUND CORROSION ON LEFT OUTBOARD SEAT TRACK, FS 1212 AND 1250, LBL 45. REMOVED AND REPLACED SEAT TRACK SECTION IAW DC9 SRM 53-05, FIG 4. (M)

Part: WEB — CRACKED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CRACK IN CUSP WEB, FS 218, LBL 46. REMOVED DAMAGED MATERIAL AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-01, FIG 4. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON WEB, FS 610, LONGERON 18L. REMOVED DAMAGED MATERIAL AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-01, FIG 4. (M)

Part: WEB — CRACKED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CRACK IN FLOOR WEB, FS 195, LBL 45. REMOVED DAMAGED MATERIAL AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-01, FIG 4. (M)

Part: SKIN — DENTED (FUSELAGE)

PHX - DURING 30K CHECK, FUSELAGE SKIN WAS FOUND DENTED, FS 120, APPROXIMATELY 3 INCHES BELOW LONGERON 18L. ACCOMPLISHED INTERNAL DOUBLER REPAIR IAW DC9 SRM 53-04, FIG 38. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB, FS 1188 TO 1212, LONGERON 18R. REMOVED AND REPLACED WEB IAW DC9 SRM 51-30. (M)

Part: WEB — CRACKED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CRACK IN CUSP WEB SUB FLOOR PANEL, FS 220, RBL 40. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-01 PAGE 8. (M)

Part: BEAM — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON PREVIOUS REPAIR DOUBLER ON AFT CARGO COMPARTMENT LOWER DOOR BEAM, LONGERON 28R. REMOVED AND REPLACED DOUBLER IAW DC9 SRM 53-05, FIG 63. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB, FS 1155 TO 1174, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-01. (M)

Part: WEB — CORRODED (CARGO DOOR SILL)

PHX - DURING 30K CHECK, FOUND CORROSION ON AFT CARGO COMPARTMENT LOWER DOOR SILL WEB, FS 1155 TO 1212, LONGERON 28R TO 29R. REMOVED AND REPLACED WEB IAW DC9 SRM 51-30. (M)

Part: LONGERON — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON LONGERON 30, FS 1241. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB, FS 1136 TO 1174, LONGERON 18L. REMOVED DAMAGED MATERIAL AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-01, FIG 4. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB, FS 1098 TO 1117, LONGERON 18R. REMOVED AND REPLACED WEB IAW DC9 SRM 51-30. (M)

Part: WEB — CRACKED (FUSELAGE)

PHX - DURNG 30K CHECK, FOUND CRACK IN CUSP WEB, FS 1260, LONGERON 18R. REMOVED AND REPLACED WEB IAW DC9 SRM 53-05, FIG 97. (M)

Part: LONGERON — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON LONGERON 29R, FS 1260. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-02, FIG 18. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB, FS 282, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-14-02, FIG 4. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CARGO TRACK, FS 1003 TO 1155, LONGERON 28R. REMOVED AND REPLACED CARGO TRACK IAW DC9 SRM 53-01, FIG 1. (M)

Part: SPAR — CRACKED (HORIZONTAL STAB)

PHX - DURING 30K CHECK, FOUND CRACK AND BEND WAS FOUND IN LEFT HORIZONTAL STABILIZER REAR SPAR CAP AT STATION XHS 158. REMOVED AND REPLACED SPAR CAP IAW DC9 SRM 51-30-05. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON WEB, FS 685, LONGERON 18L. REMOVED DAMAGED MATERIAL AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-01. (M)

Part: BEAM — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON PREVIOUS REPAIR DOUBLER ON MID CARGO COMPARTMENT LOWER DOOR BEAM, LONGERON 28R. REMOVED AND REPLACED DOUBLER IAW DC9 SRM 51-30-05. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON WEB, FS 1215, LONGERON 27R TO 28R. REMOVED AND REPLACED WEB IAW DC9 SRM 51-30. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB, FS 563, LONGERON 18R. REMOVED AND REPLACED WEB IAW DC9 SRM 51-30-02. (M)

Part: BATTERY — DISCHARGED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY LIGHTS IN THE FLIGHT COMPARTMENT WERE FOUND DIM. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: POWER SUPPLY — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE FLIGHT COMPARTMENT WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: SLIDE — DEFECTIVE (TAILCONE)

OAK - DURING C-CHECK, THE TAILCONE EXIT EMERGENCY EVACUATION SLIDE LIGHT TEST FIXTURE WAS FOUND MISSING. REPLACED THE TAILCONE EXIT EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)

Part: LONGERON — CORRODED (BS 1212-1250)

OAK - DURING C-CHECK, FOUND CORROSION ON LONGERON 29L AT FS 1231. SPLICED IN NEW SECTION OF LONGERON 29L IAW DC9 SRM 53-02, PAGES 48-53. (M)

Part: LIGHT — INOPERATIVE (ROW 21-23)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 21 TO 23 WERE FOUND INOPERATIVE. REPLACED BROKEN LAMP MODULE AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 24 TO 28 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 22 TO 24 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 22 TO 24 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: PIN — SHEARED (L2 DOOR)

SEA - AFTER ARRIVAL OF FLT 195 - CREW REPORTED THE L2 DOOR HANDLE IS OUT OF POSITION WITH DOOR CLOSED. REPLACED SHEARED HANDLE RETAINING PIN 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 5730-01044. (M)

Part: LANYARD — DISCONNECTED (TAILCONE)

PDX - DURING INSPECTION OF THE TAILCONE EMERGENCY EVACUATION SLIDE THE AUTOMATIC DEPLOY LANYARD WAS FOUND DISCONNECTED FROM THE GIRT TAB. CONNECTED THE AUTOMATIC DEPLOY LANYARD TO THE GIRT TAB. (M)

Part: HINGE MECHANISM — OUT OF ADJUST (SERV DOOR)

PDX - AFTER CATERING AIRCRAFT, THE R1 DOOR WAS REPORTED DIFFICULT TO CLOSE. FOUND DOOR HINGE LOCKOUT BAYONET PIVOT SHIM TOO TIGHT. RESHIMMED BAYONET PIVOT AND LUBED MECHANISM AND DOOR OPERATED NORMALLY. (M)

Part: LIGHT — DEFECTIVE (CABIN)

PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT NEON CHARGE LAMP DID NOT ILLUMINATE WITH SWITCH IN THE ARMED POSITION. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (X)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (W)

Part: EEL — DEFECTIVE (CABIN)

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

Part: THROTTLE SWITCH — DEFECTIVE (FWD PEDESTAL)

SEA - ON ARRIVAL OF FLT 451 CREW REPORTED, DURING APPROACH WHEN THE LANDING GEAR WAS EXTENDED, THE GEAR WARNING HORN SOUNDED AND ALL THREE GEAR UNSAFE LIGHTS ON. CYCLED LANDING GEAR, APPROXIMATELY 15 SECONDS AFTER GEAR EXTENDED THE SECOND TIME, THE WARNING HORN SILENCED AND ALL GEAR POSITION LIGHTS INDICATED DOWN AND LOCKED. REPLACED THE LANDING GEAR HANDLE SWITCH AND THE LEFT THROTTLE SWITCH ASSEMBLY. ACCOMPLISHED GEAR SWING AND OPERATED NORMALLY. REFERENCE ASAA9580136.

Part: GEAR SWITCH — DEFECTIVE (CTR INST PANEL)

SEA - ON ARRIVAL OF FLT 451 CREW REPORTED, DURING APPROACH WHEN THE LANDING GEAR WAS EXTENDED THE GEAR WARNING HORN SOUNDED AND ALL THREE GEAR UNSAFE LIGHTS ON. CYCLED LANDING GEAR, APPROXIMATELY 15 SECONDS AFTER GEAR EXTENDED THE SECOND TIME, THE WARNING HORN SILENCED AND ALL GEAR POSITION LIGHTS INDICATED DOWN AND LOCKED. REPLACED THE LANDING GEAR HANDLE SWITCH AND THE LEFT THROTTLE SWITCH ASSEMBLY. ACCOMPLISHED GEAR SWING AND OPERATED NORMALLY. REFERENCE 95ZZZM226.

Part: THROTTLE SWITCH — DEFECTIVE (FWD PEDESTAL)

SEA - ON ARRIVAL OF FLIGHT NR 375, CREW REPORTED UPON DEPARTURE FROM SFO WHEN THE LANDING GEAR WAS RETRACTED THE GEAR WARNING HORN SOUNDED AND ALL THREE GEAR UNSAFE LIGHTS ON, GEAR APPEARED TO RETRACT NORMALLY. CYCLED LANDING GEAR AND RETRACTION APPEARED NORMAL EXCEPT ALL THREE GEAR UNSAFE LIGHTS REMAINED ILLUMINATED FOR APPROXIMATELY 30 SECONDS, THEN EXTINGUISHED. FOUND PINS 'V' AND 'Y' OF CONNECTOR P1-1194 SHORTED WITH RIGHT THROTTLE ADVANCED OR RETARDED. REPLACED AND ADJUSTED RIGHT THROTTLE SWITCH ASSEMBLY. (M)

Part: EEL BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 30 AFT WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (W)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - EMERGENCY EVACUATION TRACK LIGHT INOP NEAR ROW 10. MAINTENANCE SECURED WIRES. (W)

Part: TRIM — DETACHED (L1 DOOR)

LAX - AFTER ARRIVAL OF FLT 534 - FLIGHT ATTENDANT REPORTED THE L1 DOOR WAS DIFFICULT TO CLOSE. FOUND DOOR TRIM DISPLACED AND LOWER INSERT DETACHED. REATTACHED INSERT AND REPOSITIONED TRIM AND OPERATED NORMALLY. (M)