N934AS

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 59,171 hrs · 35,836 cycles

C-CHECK - SHEAR TIE IS CORRODED. REPLACED SHEAR TIE.(K)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 59,171 hrs · 35,836 cycles

C-CHECK - LONGERON 29L INTERCOSTAL IS CORRODED. REPLACED INTERCOSTAL.(K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,171 hrs · 35,836 cycles

C-CHECK - NLG LT TUNNEL FORWARD CUTOUT FRAME, CRACKED. STOP-DRILLED CRACK. INSTALLED REPAIR ANGLE.(K)

Part: SKIN — DENTED (FUSELAGE) · airframe 59,171 hrs · 35,836 cycles

C-CHECK - FUSELAGE SKIN DENTED. HFEC INSPECTION IAW EA REVEALED NO DAMAGE REQUIRING REPAIR. BUT REPETITIVE INSPECTIONS ARE REQUIRED UNTIL NEXT HEAVY MAINTENANCE CHECK. (K)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 59,171 hrs · 35,836 cycles

C-CHECK - INTERCOSTAL CORRODED UNDER FLOOR TRACK. REPLACED INTERCOSTAL. (K)

Part: PAN — CORRODED (AFT FUSELAGE) · airframe 59,171 hrs · 35,836 cycles

C-CHECK - AFT LAV SERVICING PAN IS CORRODED. REPLACED SERVICING PAN.(K)

Part: VANE — DAMAGED (T/E FLAP) · airframe 59,171 hrs · 35,836 cycles

C-CHECK - RT IB FLAP HAS DAMAGED OB VANE. INSTALLED REPAIR FILLER AND DOUBLER.(K)

Part: TEE FITTING — CORRODED (FRAME) · airframe 59,171 hrs · 35,836 cycles

C-CHECK - FRAME TEE FITTING CORRODED BELOW CARGO TRACK. REPLACED TEE FITTING.(K)

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 59,171 hrs · 35,836 cycles

C-CHECK - SHEAR TIE IS CORRODED. REPLACED SHEAR TIE.(K)

Part: VANE — DELAMINATED (RT IB FLAP) · airframe 59,171 hrs · 35,836 cycles

C-CHECK - RT IB FLAP HAS DAMAGED OB VANE DELAMINATED. INSTALLED REPAIR FILLER AND DOUBLER. (K)

Part: SKIN — DENTED (FUSELAGE) · airframe 59,171 hrs · 35,836 cycles

C-CHECK- FUSELAGE SKIN DENTED. HFEC INSPECTION IAW EA REVEALED NO DAMAGE REQUIRING REPAIR. BUT REPETITIVE INSPECTIONS ARE REQUIRED UNTIL NEXT HEAVY MAINTENANCE CHECK.

Part: SKIN — DENTED (FUSELAGE) · airframe 59,171 hrs · 35,836 cycles

C-CHECK - FUSELAGE SKIN DENTED. HFEC INSPECTION IAW EA REVEALED NO DAMAGE REQUIRING REPAIR. BUT REPETITIVE INSPECTIONS ARE REQUIRED UNTIL NEXT HEAVY MAINTENANCE CHECK.(K)

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 59,171 hrs · 35,836 cycles

C-CHECK - SHEAR TIE CORRODED ON AFT SIDE. REPLACED SHEAR TIE.(K)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 59,171 hrs · 35,836 cycles

C-CHECK - FWD LAV SERVICE DOOR CUTOUT IN LOWER AREA. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR DOUBLER IAW EA.(K)

Part: GIRT BAR — OUT OF POSITION (L1 DOOR)

PHX - DURING PREFLIGHT CHECK, FOUND FORWARD PAX L1 DOOR EMERGENCY SLIDE GIRT BAR PULLED FROM FABRIC SLEEVE. RESECURED BAR TO SLIDE FABRIC SLEEVE. (M)

Part: WINDOW — STUCK (COCKPIT)

SEA - DURING PREFLIGHT CHECK, FOUND RIGHT F/O'S SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. LUBRICATED OPERATING MECHANISM, WINDOW THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

SEA PREFLIGHT CHECK, FOUND FORWARD SERVICE R1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)

Part: FLANGE — CHAFED (CARGO DOOR)

OKC - DURING 30K CHECK, FOUND AFT CARGO BAY DOOR IS CHAFED ON FLANGE AT AFT STOPS. INSTALLED DOUBLER PER EA 5230-01205. (M)

Part: FLANGE — CHAFED (CARGO DOOR)

OKC - DURING 30K CHECK, FOUND AFT CARGO BAY DOOR IS CHAFED ON FLANGE AT FORWARD STOPS. INSTALLED DOUBLERS PER EA 5230-01205. (M)

Part: SKIN — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND AFT CARGO BAY SKIN IS CORRODED AROUND FASTENERS AT FS 1079. INSTALLED DOUBLER PER SRM 53-04. (M)

Part: STRINGER — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND AFT CARGO COMPARTMENT CORROSION IN STRINGER BOTTOM FLANGE 28L STATION 1193-1211. REPAIRED PER SRM. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FLOORBOARD HAS CORRODED INSERTS. REPLACED FLOORBOARD. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FLOORBOARD HAS CORRODED INSERTS AT FS 1117-1174. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND DENT IN SKIN ABOVE LAV SERVICE DOOR. INSTALLED REPAIR DOUBLER. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND L1 DOOR FRAME CRACKED. REPLACED FRAME. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND CABIN FLOORBOARD HAS 15 CORRODED INSERTS AT FS 1113-1174. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: WEB — CRACKED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND RIGHT CUSP WEB AT STATION 218 CRACKED AT INBOARD CORNER. REPAIRED PER SRM. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND RIGHT FLOOR PANEL AT STATION 920-1000 EDGE AND STIFFENER CRACKED AND DISBONDED. REPAIRED IAW SRM. FABRICATED AND BONDED REPAIR PLATE. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND CORROSION ON FRAME 1060. REPLACED FRAME CAP. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC DURING 30K CHECK, FLOORBOARD IS CORRODED AT FS 1113-1174, AND HAS 15 INSERTS EITHER CRACKED, MISSING, OR CORRODED. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND LONGERON CORRODED. SPLICED IN NEW SEGMENT. (M)

Part: LONGERON — CRACKED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND AFT ACCY STATION 1437 LONGERON 2L CRACKED. REPAIRED PER SRM. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FORWARD CARGO DOOR CUTOUT LOWER INNER DOUBLER IS CORRODED. REPLACED DOUBLER. (M)

Part: FITTING — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FRAME FITTING CORRODED. REPLACED FITTING. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 1155-1250. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: INTERCOSTAL — CRACKED (PAX DOOR)

OKC - DURING 30K CHECK, FOUND L1 DOOR INTERCOSTAL CRACKED UNDER DOOR HANDLE. REMOVED AND REPLACED INTERCOSTAL IAW SRM. (M)

Part: FRAME — CHAFED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND EDGE OF FRAME CHAFED. REPAIRED FRAME. (M)

Part: LONGERON — CRACKED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND LONGERON SPLICE AT 28L STATION 689 IS CRACKED. INSTALLED NEW FITTING IAW SRM. (M)

Part: LONGERON — CRACKED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND LONGERON CRACKED. SPLICED IN NEW LONGERON SECTION. (M)

Part: FLOORBOARD — PUNCTURED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD PUNCTURED AT FS 1079-1117. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: FRAME — GOUGED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FRAME 522 ABOVE LONGERON 6L GOUGED AND CRACKED. REPAIRED PER SRM. (M)

Part: SKIN — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FUSELAGE SKIN IS CORRODED UNDER FRAME AT STATION 1287 AT 28R. REPLACED DAMAGED SECTION PER SRM 53-04. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND SEAT TRACK CORRODED. REPLACED SEAT TRACK. (M)

Part: STRINGER — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND STRINGER IS CORRODED AT FS 1193-1211. REPLACED DAMAGED SECTION WITH SPLICE REPAIR PER SRM 53-02. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FLOORBOARD IS CORRODED AND HAS DEFECTIVE INSERTS AT FS 1174-1250. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - DURING 30K CHECK FLOORBOARD IS DELAMINATED AT FS 826-886. REPLACED FLOORBOARD PER SRM 53-04. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND AFT CARGO SHEAR TIE IS CORRODED. REPLACED SHEAR TIE. (M)

Part: HINGE FITTING — CORRODED (TE FLAP)

OKC - DURING 30K CHECK, FOUND LEFT OUTBOARD FLAP HINGE FITTING AT OUTBOARD ACTUATOR POINT BEARING HOUSING IS CORRODED ON INNER SURFACE. REBORED FITTING AND INSTALLED OVERSIZED BUSHING PER OHM 27-50-5. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FRAME CORRODED. REPLACED FRAME SEGMENT. (M)

Part: STRINGER — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, STRINGER IS CORRODED IN AFT CARGO BAY AT FS 1136-1146. INSTALLED REPAIR CHANNEL PER SRM 53-02. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FLOORBOARD DELAMINATED. REPLACED FLOORBOARD. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND SEAT TRACK CORRODED AT 1144-1182. REPLACED DAMAGED SECTION WITH SPLICE REPAIR PER SRM 53-05. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FLOORBOARD HAS CORRODED INSERTS. REPLACED FLOORBOARD. (M)

Part: FLANGE — CHAFED (CARGO DOOR)

OKC - FOUND 30K CHECK, AFT CARGO BAY DOOR FLANGE IS CHAFED AT LOWER STOPS. BLENDED CHAFED AREA PER EA 5230-01205. (M)

Part: BATTERY PACK — INOPERATIVE (FWD CABIN)

DURING APPROACH, NOTED THAT 1ST CLASS CABIN EMERGENCY TRACK LIGHTING WAS FLASHING. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)

Part: BATTERY PACK — INOPERATIVE (FWD PAX ENTRY)

DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY, INCLUDING BATTERY PACK. LIGHT THEN OPERATED NORMALLY. (M)

Part: CONNECTOR — LOOSE (CABIN)

SJC - DURING PREFLIGHT CHECK, THE EMERGENCY TRACK LIGHTING IN FIRST CLASS CABIN WAS INOPERATIVE. RECONNECTED LOOSE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — INOPERATIVE (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE AT ROW 6. REPLACED TRACK LIGHT MODULE. TRACK LIGHTS THEN OPERATED NORMALLY. (M)

Part: WIRE — SHORTED (CABIN)

OAK - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE BEYOND ROW 26. REPAIRED AND REPOSITIONED CONNECTOR WIRE WHICH WAS SHORTING ON A PNEUMATIC DUCT. (M)

Part: WIRE — FAULTY (CABIN)

PDX - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROWS 6 THROUGH 9. REPAIRED FAULTY WIRING. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MECHANISM — LACK OF LUBE (COCKPIT WINDOW)

LAX - DURING PREFLIGHT CHECK, THE FIRST OFFICERS SLIDING CLEARVIEW WINDOW COULD NOT BE OPENED. LUBRICATED WINDOW MECHANISM. WINDOW THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

ANC - DURING PREFLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND CORROSION ON MID CARGO DOOR BEAM BETWEEN HORIZONTAL LEG OF REPAIR DOUBLER AT FORWARD AND AFT DOOR STOPS. INSTALLED REPAIR TAB ON BEAM PER EA 5310-02055. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND CORROSION ON LONGERON 28L FROM FS 617-636 IN MID CARGO COMPARTMENT. REMOVED CORROSION AND INSTALLED U-CHANNEL DOUBLER FROM FS 617-636 PER EA 5310-02060. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND CORROSION ON LONGERON 28L FROM FS 598-617 IN MID CARGO COMPARTMENT. REMOVED CORROSION AND INSTALLED U-CHANNEL DOUBLER FROM FS 598-617 PER EA 5310-02060. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND CORROSION ON LONGERON 30 FROM FS 560 TO 579 IN MID CARGO COMPARTMENT. REMOVED CORROSION AND INSTALLED SPLICE ON LONGERON PER EA 5310-02056. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

PDX - DURING LINE CHECK, FOUND CABIN FLOOR EMERGENCY TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE FROM ROW 1 THROUGH 9. REPAIRED BROKEN WIRE AT ROW 6 AND REPLACED FORWARD EMERGENCY LIGHT BATTERY POWER SUPPLY PACK. LIGHTS THEN OPERATED PROPERLY. (M)

Part: COALESCER BAG — DIRTY (A/C BAY)

PDX - DURING CRUISE (SJC-PDX), NOTED 'GASEOUS SMELL' IN PASSENGER CABIN. REPLACED BOTH AIR CONDITIONING PACK COALESCER BAGS. ALSO, WASHED LEFT AND RIGHT MLG WHEEL WELLS, AFT AIRCRAFT BELLY AND APU INLET. NO ODOR NOTED UPON TEST WITH APU-SUPPLIED AIR. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: MODULE — DAMAGED (CABIN)

LAX - DURING LINE CHECK, AN EMERGENCY FLOOR TRACK LIGHTING MODULE WAS FOUND TO BE INOPERATIVE. REPAIRED LIGHT MODULE SOCKET PER SRM 20-10-03. REPLACED BULB IN MODULE. LIGHT THEN OPERATED NORMALLY. (M)

Part: LIGHT — DAMAGED (CABIN)

SEA - DURING PREFLIGHT CHECK, FOUND TWO EMERGENCY FLORO TRACK LIGHTS DAMAGED/MISSING AT ROWS 22. REPLACED LIGHT ASSEMBLIES AT ROW 22. LIGHTS THEN OPERATED NORMALLY. (M)

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

LAX - DURING PRE-FLIGHT CHECK, R1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD BETWEEN GIRT BAR AND SLIDE COVER. (M)

Part: LIGHT — INOPERATIVE (CABIN)

PDX - DURING LINE CHECK, PORTABLE EMERGENCY LIGHT WAS DETERMINED TO INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

PDX - DURING SERVICE CHECK, OVERHEAD EMERGENCY LIGHTS AT ROWS 14-17 WERE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED ASSOCIATED BATTERY PACK ASSEMBLIES. LIGHTS THEN OPERATED PROPERLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

PDX - DURING SERVICE CHECK, OVERHEAD EMERGENCY LIGHTS AT AFT CABIN DOOR WERE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED ASSOCIATED BATTERY PACK ASSEMBLIES. LIGHTS THEN OPERATED PROPERLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

PDX - DURING SERVICE CHECK, FIVE OVERHEAD EMERGENCY LIGHTS AT ROWS 14-17 WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACKS. LIGHTS THEN OPERATED PROPERLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

PDX - DURING SERVICE CHECK, FIVE OVERHEAD EMERGENCY LIGHTS AT ROWS 14-17 WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACKS. LIGHTS THEN OPERATED PROPERLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURNG LINE CHECK, OVERHEAD EMERGENCY LIGHTS AT ROWS 13-17 WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACKS. LIGHTS THEN OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING PREFLIGHT, COCKPIT OVERHEAD EMERGENCY LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED BATTERY ASSEMBLIES. LIGHTS THEN OPERATED NORMALLY. (M)

Part: DOUBLER — DAMAGED (FUSELAGE)

PHX - DURING SCHEDULED ACARS AND EGPWS SYSTEM INSTALLATION, REMOVAL OF PREVIOUSLY INSTALLED REPAIR DOUBLER TO ACCESS NR 3 VHF ANTENNA AT BASE OF AFT CARGO AREA REVEALED SKIN CORROSION. REMOVED SKIN CORROSION AND INSTALLED NEW DOUBLER. (M)

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB)

OAK - DURING SCHEDULED C-CHECK, A CRACK FOUND IN THE LEFT HORIZONTAL LEG OF THE LEFT DORSAL FIN ATTACH ANGLE AT STATION 1485. REPAIRED PER EA 5530-01065. (M)

Part: BATTERY — DISCHARGED (ESCAPE SLIDE)

OAK - DURING SCHEDULED C-CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE FAILED LAMP BATTERY TEST. REMOVED AND REPLACED SLIDE, SYSTEM OPERATES NORMALLY. (M)

Part: BATTERY — DISCHARGED (AFT CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD CEILING EMERGENCY LIGHTS AT ROWS 28-31 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CATWALK AREA WERE FOUND INOPERATIVE. REPLACED QUICK DISCONNECT FITTING AND WIRE TERMINAL FOR FORWARD LIGHT ASSEMBLY, REPLACED LAMP IN AFT LIGHT ASSEMBLY, AND REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN) · airframe 44,399 hrs · 28,448 cycles

SEA - DURING MAINTENANCE CHECK, THE FORWARD AISLE OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERIES IN BATTERY PACK AND LIGHT OPERATED NORMALLY. (X)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERABLE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X)

Part: LIGHT — INOPERABLE (CABIN)

PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERABLE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. PART TC: 17,240. (X)

Part: LAMP — INOPERATIVE (CABIN)

SEA - AFTER ARRIVAL OF FLIGHT 655, CREW REPORTED ONE EMERGENCY FLOOR TRACK LIGHT IN THE FORWARD CABIN WAS FOUND INOPERATIVE. REPLACED LAMP MODULE AND OPERATED NORMALLY. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

OAK - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: MECHANISM — OUT OF ADJUST (L1 DOOR)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WAS FOUND TO RUB ON THE FRAME DURING OPENING AND CLOSING. ADJUSTED THE L1 DOOR BAYONET ROD AND OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (ROW 4)

SEA - PRIOR TO DEPARTURE OF FLIGHT 624, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHT COVER AT ROW 4 WAS OUT OF TRACK. REPAIRED WIRE IN FLOOR TRACK AND REPLACED COVER AND OPERATED NORMALLY. (M)

Part: AIR DIST — ODOR (CABIN)

OAK - AIR TURNBACK OF FLIGHT 445, CREW REPORTED ELECTRICAL ODOR IN CABIN DURING CLIMB-OUT PASSING 12,000 FT. ONE MINUTE LATER SMOKE WAS REPORTED IN CABIN, SWITCHED TO EMERGENCY POWER BUT ODOR AND SMOKE CONTINUED. TURNED OFF RIGHT AIR CONDITIONING PACK AND ODOR AND SMOKE DISSIPATED AFTER 3 TO 4 MINUTES. LANDED WITHOUT INCIDENT. INSPECTED RIGHT ENGINE INLET AND EXHAUST, NO DEFECT NOTED. ACCOMPLISHED RUN UP OF RIGHT ENGINE, OPERATED RIGHT AIR CONDITIONING PACK AND ACCOMPLISHED AIR QUALITY CHECK, NO ODOR OR DEFECT NOTED. REPLACED BOTH WATER SEPARATOR COALESCERS AND RELEASED FOR SERVICE. (M)

Part: BATTERIES — DISCHARGED (CABIN)

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

Part: CABLE — DISCONNECTED (TAILCONE)

PDX - DURING MAINTENANCE CHECK, THE TAILCONE RELEASE CABLE WAS FOUND DISCONNECTED FROM THE CAM MECHANISM. RECONNECTED THE TAILCONE RELEASE CABLE TO THE CAM MECHANISM. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 1 TO 8 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: POWER SUPPLY — DEFECTIVE (CABIN)

ANC - PRIOR TO DEPARTURE OF FLT 89 - CREW REPORTED THE COCKPIT EMERGENCY LIGHTS WOULD NOT ILLUMINATE WITH THE EMERGENCY LIGHTS SWITCH IN THE ON POSITION OR IN THE ARMED POSITION AND ELECTRICAL POWER OFF. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

PDX - DURNG MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE TAIL CONE AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SJC - FLT 446 - CREW REPORTED AFT CABIN EMERGENCY LIGHTS ILLUMINATED AFTER AIRCRAFT SHUTDOWN COMPLETED. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: HOLD OPEN HOOK — BENT (L1 DOOR)

SEA - AFTER ARRIVAL OF FLT 371, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN AND LATCH IN OPEN POSITION. FOUND HOLD OPEN HOOK BENT AND DOOR CONTROL ROD LOCK LOOSE. REPLACED DOOR HOLD OPEN HOOK, TIGHTENED AND SAFTIED CONTROL ROD LOCK AND DOOR OPERATED NORMALLY. REFERENCE ASAA9680156

Part: CNTRL ROD LOCK — LOOSE (L1 DOOR)

SEA - AFTER ARRIVAL OF FLT 371, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN AND LATCH IN OPEN POSITION. FOUND HOLD OPEN HOOK BENT AND DOOR CONTROL ROD LOCK LOOSE. REPLACED DOOR HOLD OPEN HOOK, TIGHTENED AND SAFTIED CONTROL ROD LOCK AND DOOR OPERATED NORMALLY. (M)

Part: MECHANISM — OUT OF ADJUST (L1 DOOR)

LAX - DURING MAINTENANCE CHECK, THE L1 DOOR WAS FOUND TO OVER ROTATE ON THE OUTBOARD PIVOT OF THE HINGE, AND THE HOLD OPEN HOOK DID NOT CATCH THE PIN. RERIGGED THE L1 DOOR, ADJUSTED THE LATCHING CAM AND HOLD OPEN HOOK ACTUATING ARM AND DOOR OPERATED NORMALLY. (M)

Part: HOLD OPEN HOOK — BENT (L1 DOOR)

SEA - PRIOR TO DEPARTURE OF FLIGHT 330, CREW REPORTED THE L1 DOOR BINDS WHEN CLOSING. FOUND THE L1 DOOR HOLD OPEN HOOK BENT, REPLACED THE HOLD OPEN HOOK AND OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (L1 DOOR)

PDX - DURING MAINTENANCE CHECK, THE L-1 DOOR PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY 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. (M)

Part: MECHANISM — OUT OF ADJUST (L1 DOOR)

SEA - DURING MAINTENANCE CHECK, THE L-1 DOOR GUST LOCK WAS FOUND NOT OPERATING PROPERLY. RERIGGED DOOR PER MM AND ADJUSTED GUST LOCK MECHANISM AND OPERATED NORMALLY. (M)

Part: ANGLE — CRACKED (FS 826)

OAK - DURING 30K CHECK, ATTACH ANGLE WAS FOUND CRACKED AT FS 826 ON CENTER WING TO FUSELAGE ATTACH POINT ON RIGHT FORWARD CORNER UNDER CABIN FLOOR PANEL E9. REPLACED ATTACH ANGLE IAW DC-9 SRM 51-30-05. (M)

Part: EVAC SLIDE — FAILED (L2 DOOR)

SEA - DURING TRAINING DEMONSTRATION, THE L2 DOOR EMERGENCY EVACUATION SLIDE WAS DEPLOYED. AS THE SLIDE BEGAN TO DEPLOY, A RUPTURE OCCURRED AT THE UPPER END OF THE SLIDE. THE SLIDE CONTINUED TO DEPLOY BUT HAD A COMPLETE AIR LOSS. REPLACED THE L2 DOOR EMERGENCY EVACUATION. (M)

Part: EEL BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, BOTH AFT OVERWING EMERGENCY EXIT SIGNS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (W)