N969AS

Part: FLOOR PANEL — DELAMINATED (BS 256-313)

C-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)

Part: FLOOR PANEL — DELAMINATED (BS 886-927)

C-CHECK, CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (K)

Part: FLOOR PANEL — DELAMINATED (BS 826-886)

C-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)

Part: FLOOR PANEL — DELAMINATED (BS 1003-1079)

C-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)

Part: FLOOR PANEL — DELAMINATED (BS 389-465)

C-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)

Part: FLOOR PANEL — GOUGED (BS 864-866)

C-CHECK, CABIN FLOOR PANEL GOUGED. REPLACED FLOOR PANEL. (K)

Part: FLOOR PANEL — DELAMINATED (BS 465-541)

C-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)

Part: SKIN — DENTED (BS 174-175)

C-CHECK, FUSELAGE SKIN DENTED. COLD-WORKED AREA BACK TO ORIGINAL CONTOUR AND INSTALLED REPAIR DOUBLER. (K)

Part: SPLINE — CORRODED (TORQUE TUBE)

C-CHECK, RUDDER TAB TORQUE TUBE SPLINE CORRODED. REPLACED RUDDER TAB TORQUE TUBE. (K)

Part: FLOOR PANEL — DELAMINATED (BS 617-693)

C-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)

Part: FLOOR PANEL — DELAMINATED (BS 769-826)

C-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGE AREA. APPLIED GLASS CLOTH REPAIR. (K)

Part: SKIN — DENTED (BS 229-246)

C-CHECK, FUSELAGE DENTED. REMOVED DAMAGED SECTION. INSTALLED INTERNAL DOUBLERS AND INTERNAL STRAPS. (K)

Part: TORQUE TUBE — CORRODED (RUDDER TAB)

C-CHECK, RUDDER TAB TORQUE TUBE LOWER SPLINES CORRODED. REPLACED RUDDER TAB TORQUE TUBE SHAFT ASSEMBLY. (K)

Part: LONGERON — CORRODED (BS 1203-1260)

C-CHECK, LONGERON CORRODED. REPLACED DAMAGED SECTION WITH SPLICES. (K)

Part: FLOOR PANEL — DELAMINATED (BS 1174-1250)

C-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)

Part: CRANK ASSY — CORRODED (RUDDER TAB)

C-CHECK, RUDDER TAB TORQUE TUBE CONTROL CRANK SPLINES CORRODED. REPLACED TORQUE TUB CONTROL CRANK ASSY. (K)

Part: SKIN — DEBONDED (TE FLAP)

C-CHECK, LT WING OB FLAP CENTER PREVIOUS SKIN REPAIR IS DEBONDED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)

Part: CUSP WEB — CORRODED (BS 1210-1211)

C-CHECK, CABIN FLOOR CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)

Part: SPRING — CORRODED (RUDDER)

C-CHECK, RUDDER LOAD FEEL AND TRIM SPRING ASSEMBLY CORRODED. REPLACED RUDDER LOAD FEEL AND TRIM SPRING ASSEMBLY. (K)

Part: SKIN — DENTED (BS 200-229)

C-CHECK, FUSELAGE DENTED. REMOVED DAMAGED SECTION. INSTALLED INTERNAL DOUBLERS, FINGER DOUBLERS, AND INTERNAL STRAP. (K)

Part: FLOOR PANEL — DELAMINATED (BS 313-389)

C-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)

Part: FLOOR PANEL — PUNCTURED (BS 807-826)

C-CHECK, CABIN FLOOR PANEL PUNCTURED. REPLACED FLOOR PANEL. (K)

Part: SKIN — NICKED (TE FLAP)

C-CHECK, RT WING OB FORE FLAP CENTER DENTED ON LE PREVIOUS REPAIR. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)

Part: SKIN — GOUGED (TE FLAP)

C-CHECK, LT WING OB FLAP IB VANE IS GOUGED OF LEADING EDGE. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)

Part: FLOOR PANEL — DELAMINATED (BS 927-1003)

C-CHECK, CABIN FLOOR PANEL DELAMINATED AT FASTENER LOCATIONS. REPLACED FLOOR PANEL. (K)

Part: LONGERON — CORRODED (BS 1237-1298)

C-CHECK, LONGERON CORRODED. REPLACED LONGERON. (K)

Part: DIVERTER — CRACKED (ACM) · airframe 44,051 hrs · 21,851 cycles

C-CHECK- RT ACM(AIR CYCLE MOTOR) DIVERTER IS CHAFED AND CRACKED. REMOVED DAMAGE, WELDED IN FILLER REPAIR IAW EA.

Part: SKIN — CHAFED (LT WING)

C-CHECK- LT WING L/E SURFACE HAS 7 CHAFED AREAS 5 INCHES FROM L/E AND I/B OF NR 5 L/E SLAT TRACK. REMOVED DAMAGED AREAS, THEN HFEC TREATED, PRIMED AND TOPCOATED THOSE AREAS IAW EA.

Part: FRAME — CHAFED (FUSELAGE) · airframe 44,051 hrs · 21,851 cycles

C-CHECK - AFT ACCESSORY COMPARTMENT FRAME CHAFED AT LONGERON 20R. REMOVED DAMAGED SECTION AND INSTALLED REPAIR ANGLE IAW SRM.(K)

Part: SKIN — DELAMINATED (T/E FLAP VANE)

C-CHECK- RT IB FLAP VANE HAS DELAMINATION ON LOWER SURFACE. REMOVED DAMAGED SECTION, AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM.

Part: SKIN — DENTED (TE FLAP)

C-CHECK- RT IB FLAP LOWER SURFACE IS DENTED 24 INCHES FROM THE T/E AND 17.5 INCHES FROM IB FAIRING SEAL. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER IAW SRM.

Part: WIRE HARNESS — MISROUTED (CABIN)

SEA BTB NON-ROUTINE LINE CHECK-SPARKS AND SMOKE NOTED COMING FROM OVERHEAD GRILL BETWEEN L1 DOOR AND FORWARD GALLEY. INSP REVEALED THAT A WIRE BUNDLE WAS CHAFING ON A PLENUM DUCT CLAMP, SOME OF THE WIRING WAS SHORTING ON CLAMP, AND HAD BURNED THROUGH 1 FOOT FORWARD OF S3-25 TERMINAL STRIP. IT WAS FURTHER DETERMINED THAT THE WIRING BUNDLE HAD BEEN MIS-ROUTED, AND DUCT CLAMP HAD BEEN IMPROPERLY INSTALLED. REPAIRED DAMAGED WIRING. REROUTED WIRING BUNDLE, ALSO REPLACED PLENUM DUCT AND CLAMP. OPS CHECKED OK.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 44,051 hrs · 21,851 cycles

C-CHECK-MAIN CABIN FLOOR PANEL IS DELAMINATED AT CORNER. REPLACED FLOOR PANEL IAW SRM.(K)

Part: RETAINER — CRACKED (HEAT EXCHANGER) · airframe 44,051 hrs · 21,851 cycles

C-CHECK-HEAT EXCHANGER RAM AIR (Y) DUCT HAS BROKEN RETAINER ON LT SIDE. REMOVED DAMAGE, WELDED IN REPAIR TAB IAW EA.

Part: SKIN — DENTED (T/E FLAP) · airframe 44,051 hrs · 21,851 cycles

C-CHECK- RT IB FLAP LOWER SURFACE IS DENTED 11.5 INCHES FROM T/E AND 19.25 INCHES FROM IB FAIRING SEAL. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,051 hrs · 21,851 cycles

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

Part: HANDLE — MALFUNCTIONED (SERVICE DOOR)

LAS - POST FLIGHT INSPECTION, FOUND AFT SERVICE L2 DOOR COULD NOT BE OPENED FROM INSIDE. REPLACED DOOR HANDLE AND RETAINING PIN, BOLT P/N 2705574. DOOR THEN OPENED PROPERLY. (M)

Part: LINKAGE — OUT OF ADJUST (COCKPIT WINDOW)

ANC - DURING PREFLIGHT CHECK, FOUND LEFT CAPTAINS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED SLIDING MECHANISM IN TRACK. WINDOW THEN OPERATED PROPERLY. (M)

Part: LINKAGE — DISCONNECTED (COCKPIT WINDOW)

ANC - DURING PREFLIGHT CHECK, FOUND LEFT CAPTAINS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. RECONNECTED LINKAGE. WINDOW THEN OPERATED PROPERLY. (M)

Part: ROD — OUT OF POSITION (CLEARVIEW WINDOW)

LAX PREFLIGHT CHECK, LEFT CAPTAINS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. REPOSITIONED ACTUATING ROD GUIDE PIN. WINDOW THEN OPERATED PROPERLY. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING 15K CHECK, FUSELAGE SKIN DENTED AT FS 327-350. INSTALLED CLASS 1 REPAIR PER SRM 53-04. (M)

Part: VANE — PUNCTURED (TE FLAP)

OKC DURING 15K CHECK, FOUND RIGHT WING INBOARD FLAP VANE, FOREFLAP, IS PUNCTURED. INSTALLED DOUBLER PER SRM 51-70-2 AND EA 5750-01876. (M)

Part: FRAME — CRACKED (FUSELAGE)

OKC - DURING 15K CHECK, FRAME IS CRACKED IN AFT CARGO BAY AT FS 1231. REPLACED DAMAGED SECTION AND SPLICED IN NEW SECTION PER SRM 53-05. (M)

Part: SKIN — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN CORRODED AT STATION 769 TO 788 UNDER FAIRING RUB STRIP AND AROUND FASTENER HOLES. INSTALLED DOUBLER, FILLERS, ANGLE, SHIMS, TRIPLER, AND SPLICE PER EA 5330-01708. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND PASSENGER CABIN FLOORBOARD CRACKED AT FS 889-927. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FOUND DURING 15K CHECK, CABIN FLOORBOARD HAS SEVERAL CORRODED INSERTS AND LARGE TORN AREA FROM FS 1155 TO 1250. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: BEAM — CORRODED (FUSELAGE)

FOUND DURING 15K CHECK, AFT CARGO BAY DOOR BEAM IS CORRODED IN SEVERAL PLACES. REPLACED DOOR BEAM PER SRM 51-30-5. (M)

Part: SKIN — CORRODED (FUSELAGE)

FOUND DURING 15K CEHCK, FUSELAGE SKIN CORRODED AT FS 769-788, BETWEEN LONGERON 30 AND 29R UNDER FAIRING RUB STRIP AND AROUND FASTENER HOLES. REPAIRED PER EA 5330-01708. (M)

Part: FLOORBOARD — DEBONDED (FUSELAGE)

FOUND DURING 15K CHECK, CABIN FLOORBOARD HAS LARGE SOFT, DEBONDED, AREA FROM FS 1117 TO 1174. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: SKIN — CRACKED (NACELLE)

FOUND DURING 15K CHECK, LT ENGINE UPPER COWL IS CRACKED. REPAIRED PER EA 7110-01208 AND SRM 54-06. (M)

Part: FLOORBOARD — GOUGED (FUSELAGE)

DURING 15K C-CHECK, FOUND CABIN FLOOR PANEL HAS SEVERAL GOUGES BETWEEN FS 1117 AND 1174. REPLACED DAMAGED FLOOR PANEL PER SRM 53-05. (M)

Part: STRUCTURE — CRACKED (SUB FLOOR)

FOUND SUB FLOORING IS CRACK AT FS 200. REPLACED DAMAGED SUB-FLOORING SECTION PER SRM 51-70-4. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FOUND DURING 15K CHECK, FLIGHT DECK FLOORBOARD DELAMINATED AND CORRODED AT FS 125-160. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FOUND DURING 15K CHECK, CABIN FLOORBOARD HAS SEVERAL WATER DAMAGED INSERTS AT FS 218-256. REPLACED FLOORBOARD IAW SRM 53-05. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND DURING 15K CHECK, FLOOR SUPPORT CORRODED AT FS 1098-1193. REPLACED FLOOR TRACK PER SRM 51-30-1, 51-10-2, 51-10-4, AND 51-10-3. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - FOUND DURING 15K CHECK, CABIN FLOOR PANEL IS DELAMINATED AT TWO LOCATIONS BETWEEN FS 541 AND 617. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FOUND DURING 15K CHECK, CABIN FLOORBOARD IS CORRODED BETWEEN FS 598-636. REPLACED FLOORBOARD PER SRM 53-24-0. (M)

Part: FLOORBOARD — TORN (FUSELAGE)

FOUND FLOORBOARD FIBERGLASS CLOTH TORN FROM UPPER SURFACE AT FS 1079-1117. REPLACED FLOORBOARD PER SRM 53-03. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FOUND DURING 15K CHECK, FLIGHT DECK HAS CORRODED FLOORBOARD INSERTS AT FS 150-160. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: FLOORBOARD — CORRODED (FS)

FOUND DURING 15K CHECK, CABIN FLOORBOARD HAS CORRODED AND SOME MISSING INSERTS AT FS 160-200. REPLACED FLOORBOARD PER SRM 53-05. (M0

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - FOUND 15K CHECK, CABIN SEAT TRACK IS CORRODED AT FS 1098-1217. REPLACED SEAT TRACK PER SRM 53-05. (M)

Part: FLOORBOARD — DEBONDED (FUSELAGE)

DURING 15K CHECK FOUND CABIN FLOOR PANEL IS DISBODED AT CORNER AND CREASED THROUGH MIDDLE AT FS 465-522. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: FLOORBOARD — DEBONDED (FUSELAGE)

FOUND DURING 15K CHECK, CABIN FLOOR PANEL IS DISBONDING AROUND INSERTS AT FS 190-256. REPLACED FLOORBOARD [ER SRM 53-05. (M)

Part: FLOORBOARD — CORRODED (FS)

FOUND DURING 15K CHECK, CABIN FLOOR PANEL IS CORRODED AROUND INSERTS AT FS 160-190. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FOUND DURING 15K CHECK, FLOOR PANEL HAS MULTIPLE CRACKS AND PUNCTURES ON BOTTOM SURFACE AT FS 796-826. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOORBOARD — BROKEN (FUSELAGE)

FOUND DURING 15K CHECK, CABIN FLOOR INSERTS ARE DAMGED, SOME BROKEN AND SOME PULLED, BETWEEN FS 1117 AND 1174. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FOUND DURING 15K CHECK, CABIN FLOOR EDGES HAVE BEEN WATER DAMAGED BETWEEN FS 1003 AND 1074. REPLACED FLOORBOARD PER SRM 53-24-0. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

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

Part: FLOOR PANEL — DEBONDED (FUSELAGE)

FOUND DURING 15K CHECK, FLOOR PANEL DISBONDED AT EDGE AT FS 769-826. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

FOUND DURING 15K CHECK, CABIN FLOOR PANEL IS DELAMINATED IN TWO PLACES BETWEEN FS 465-541. REPLACED FLOORBOARD IAW SRM 53-05. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FOUND DURING 15K CHECK, CABIN FLOORBOARD JUST INSIDE L1 ENTRY IS CORRODED AROUND INSERTS AT FS 148-196. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND SEAT TRACK IS CORRODED FROM FS 1098 TO 1193. REPLACED TRACK IAW SRM 51-30-1, 10-2, 10-4, AND 10-3. (M)

Part: LIGHT — MALFUNCTIONED (CABIN)

OAK - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR WOULD NOT EXTINGUISH WITH SWITCH OFF. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M)

Part: LIGHT — MALFUNCTIONED (FWD PAX ENTRY)

PDX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR ILLUMINATED WITH SWITCH TURNED OFF. REPLACED LIGHT ASSEMBLY, INCLUDING BATTERY PACK. LIGHT THEN OPERATED NORMALLY. (M)

Part: LANYARD — DISCONNECTED (EVAC SLIDE)

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

Part: HARNESS — FAILED (SERVICE DOOR)

DURING C CHECK, FORWARD SERVICE DOOR EMERGENCY SLIDE HARNESS FAILED SYSTEM CHECK. REPLACED EMERGENCY SLIDE. SYSTEM CHECKED, OK.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)

DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE AT ROW 21. REPLACED CONNECTOR WIRE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

OAK - FOUND C-CHECK, AFT CARGO BAY DOOR JAMB BEAM IS CORRODED IN SEVERAL PLACES. REMOVED CORRODED AREA, ADDED FILLER, AND INSTALLED DOUBLER PER EA 5310-02122. (M)

Part: MECHANISM — OUT OF ADJUST (L1 DOOR)

SEA - FOUND L1 DOOR DIFFICULT TO OPEN. ADJUSTED DOOR MECHANISM. DOOR THEN OPENED NORMALLY. (M)

Part: MODULE — DISCONNECTED (CABIN)

PDX - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 7. RECONNECTED DISCONNECTED LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

PDX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT ON AND WILL NOT TURN OFF. REPLACED PORTABLE LIGHT ASSEMBLY. LIGHT THEN OPERATED NORMALLY. (M)

Part: MODULE — INOPERATIVE (CABIN)

SEA - DURING LINE CHECK, NUMEROUS EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN FORWARD CABIN. REPLACED INOPERATIVE MODULES. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — INOPERATIVE (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

LAX - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE IN VARIOUS LOCATIONS THROUGH OUT CABIN. RECONNECTED/REPAIRED LIGHTS. LIGHT THEN OPERATED PROPERLY. (M)

Part: PLUG — OUT OF POSITION (CABIN)

PDX - DURING LINE MAINTENANCE CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE ROWS 6-9. REINSTALLED PLUG IN TRACK LIGHTING MODULE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING LINE CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE FROM ROW 6 TO 9. RECONNECTED WIRING TO LIGHT MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (EVAC SLIDE)

PHX - DURING PRE-FLIGHT CHECK, THE AFT SERVICE DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

LAX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE LIGHT. OP TESTED OK. (M)

Part: PIN — MISSING (WINDOW)

PDX - DURING PREFLIGHT CHECK, THE CAPTAINS SLIDING CLEARVIEW WINDOW COULD NOT BE OPENED. REINSTALLED PIN IN WINDOW HINGE LINKAGE. WINDOW THEN OPERATED PROPERLY. (M)

Part: BATTERY — DISCHARGED (FWD PAX ENTRY)

OAK - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE LIGHT. OP TESTED OK. (M)

Part: LANYARD — DISCONNECTED (SERVICE DOOR)

SEA - FORWARD GALLEY DOOR LANYARD BETWEEN GIRT BAR AND SLIDE COVER BECAME DISCONNECTED. REATTACHED LANYARD. (M)

Part: MODULE — INOPERATIVE (CABIN)

LAX - DURING PREFLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE AT ROW 30. REPLACED LIGHT MODULE SOCKET AND RELAMPED. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LANYARD — DETACHED (R1 DOOR)

SEA - DURING PRE-FLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE GIRT BAR TO LATCH LANYARD WAS FOUND DETACHED. REATTACHED LANYARD. (M)

Part: MODULE — DISCONNECTED (CABIN)

ANC - DURING PREFLIGHT CHECK, EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED LOOSE LIGHT MODULES. LIGHT THEN OPERATED PROPERLY. (M)

Part: COALESCER BAG — DIRTY (A/C BAY)

ZIH - DURING CLIMB AT 10K FEET ALTITUDE, BURNING RUBBER/ELECTRICAL FIRE SMELL WAS DETECTED IN VICINITY OF ROW 15. REMOVED OVERHEAD PANELS AT ROWS 13-17 AND INSPECTED LIGHTS, BALLASTS, AND EMERGENCY BATTERIES. REPLACED LEFT AIR CONDITIONING SYSTEM COALESCER BAG. RAN ENGINE AND LEFT AC PACK FOR 45 MINUTES. COULD NOT DUPLICATE ODOR. RELEASED AIRCRAFT FOR SERVICE. (M)

Part: LANYARD — DISCONNECTED (R1 DOOR)

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

Part: DOOR — OUT OF RIG (L1)

JUN - AFTER TAXI UP TO GATE, L1 DOOR FORWARD LEFT CREW/PAX DOOR WAS FOUND TO BE DIFFICULT TO OPEN. RIGGED L1 DOOR. THE DOOR THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

OAK - DURING C-CHECK, THE LEFT FORWARD ENTRY PORTABLE EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE PORTABLE EMERGENCY LIGHT ASSEMBLY WITH A SERVICEABLE UNIT. (M)

Part: SKIN — DAMAGED (RT WING)

SEA - DURING LINE CHECK, FOUND RIGHT LOWER WING DAMAGE AT XRS 509.5 FROM FRONT TO REAR REAR. INITIATED PERIODIC INSPECTION PER EA 5720-01193, WITH FINAL RESOLUTION TO BE ACCOMPLISHED AT NEXT C-CHECK. OAK - DURING C-CHECK, INSTALLED EXTERNAL DOUBLER FROM FRONT SPAR TO REAR SPAR PER EA 5730-01086. (M)

Part: SLIDE — FAILED (CABIN)

OAK - DURING C-CHECK, AFT REAR DOOR EMERGENCY SLIDE HARNESS FAILED SYSTEM CHECK. REPLACED EMERGENCY SLIDE PER T/C 24653002. SYSTEM CHECKED OK. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ANC - DURING LINE CHECK, FOUND SOME EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE THROUGHOUT CABIN. RESEATED TRACK LIGHTING MODULES. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

PDX - DURING SERVICE CHECK, FOUND SEVERAL EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN ON RIGHT SIDE. RESEATED TRACK LIGHTING MODULES. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

PDX - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROWS 6, 7 AND 8. REPLACED TRACK LIGHTING BASE AND COVER IAW EA 3350-01014. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 6-7. REPLACED LAMP MODULE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING SERVICE CHECK, FORWARD CABIN PORTABLE EMERGENCY LIGHT WAS DETERMINED TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

SEA - DURING PRE-FLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE PULLED OUT OF PLACE. REINSTALLED LANYARD PROPERLY. (M)

Part: LANYARD — DISCONNECTED (EVAC SLIDE)

ANC - DURING PREFLIGHT CHECK, L2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD BETWEEN GIRT BAR AND SLIDE COVER. (M)

Part: WIRE — DISCONNECTED (ROWS 6-7)

SEA - PRIOR TO DEPARTURE, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 6 AND 7 WERE FOUND INOPERATIVE. RECONNECTED LOOSE WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — WILL NOT TEST (OVERWING) · airframe 28,227 hrs · 14,264 cycles

PHX - DURING 30K CHECK, THE OVERWING EMERGENCY EXIT LIGHTS FAILED THE LUMINOSITY CHECK. REPLACED THE BATTERY PACK AND THE LIGHTS OPERATED NORMALLY. (X)

Part: SKIN — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE FUSELAGE AT FS 826 WAS FOUND CORRODED ON THE UNDERWING BELLY SKIN, OUTER SURFACE. REMOVED CORROSION AND REPAIRED PER EA 5310-01803 AND EA 10-5310-0317. (M)

Part: SKIN — CHAFED (FUSELAGE)

PHX - DURING 30K CHECK, THE CENTER CARGO DOOR WAS FOUND CHAFED ON THE DOOR INNER PAN AT BOTH HINGE ARM CUTOUT LOCATIONS. REPAIRED PER EA 5230-01105 AND EA 10-5230-0297. (M)

Part: SPAR CAP — DAMAGED (HORIZONTAL STAB)

PHX - DURING 30K CHECK, FOUND AN ELONGATED LEADING EDGE CAP ATTACH FASTENER HOLE IN THE LEFT HORIZONTAL STABILIZER FORWARD LOWER SPAR CAP FLANGE AT STATION XHS=90. REPAIRED PER EA 5510-01093 AND EA 10-5510-0319. (M)

Part: PAN — GOUGED (CARGO DOOR)

PHX - DURING 30K CHECK, THE CENTER CARGO DOOR WAS FOUND GOUGED ON THE INNER PAN OF THE DOOR ON THE AFT SIDE. REPAIRED PER EA 5230-01109 AND EA 10-5230-0316. (M)

Part: FRAME — MISREPAIRED (FUSELAGE)

PHX - DURING 30K CHECK, WHILE ACCOMPLISHING FRAME REPAIR OF A DENT AT FS 731, LONGERON 24L PER PRELIMINARY EA 1590-EG-0005, ADDITIONAL DAMAGE IN THE FORM OF IMPROPER REPAIR FASTENER SPACING OCCURRED TO THE FRAME UPPER FLANGE AND NESTER FORMER. REPAIRED PER EA 5310-01804 AND EA 10-5310-0318. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE RIGHT CABIN FLOOR CUSP BEAM WAS FOUND CORRODED BETWEEN FS 484 AND 503. REPAIRED PER SRM 53-10-3. (M)

Part: LONGERON — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT FS 1231, BEAM LONGERON 29R, WAS FOUND CORRODED AT THE RADIUS OF THE LOWER HORIZONTAL LEG. REPAIRED PER SRM 51-30. (M)

Part: SLIDE — FAILED (TAILCONE EXIT)

PHX - DURING 30K CHECK, THE TAILCONE EXIT EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE TAILCONE EXIT EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED 30K CHECK, THE AFT CARGO COMPARTMENT STATION 1287 BETWEEN LONGERON 29L TO 30L SHEAR TIE WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT FLOORBOARD SUPPORT AT FS 1155, LONGERON 28L TO 29R WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER SRM 51-30-1. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN FLOOR CUSP BEAM WEB BETWEEN STATION 503 AND 579, RBL 56 WAS FOUND CORRODED. REPAIRED PER SRM 51-30-2. (M)

Part: BEAM — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN CUSP BEAM WEB AT FS 448, RBL 56 WAS FOUND CORRODED. REPAIRED PER SRM 53-01. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN FLOOR CUSP BEAM WEB BETWEEN STATION 588 AND 617, RBL 56 WAS FOUND CORRODED. REPAIRED PER SRM 53-01, FIG 4. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN FLOOR SUPPORT AT FS 200, RBL 45-55 WAS FOUND CORRODED. REPAIRED PER SRM 51-30. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE CUSP MEMBRANE AT FS 1142, LBL 58 ON THE TOP SURFACE WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER SRM 53-01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN FLOOR SUPPORT AT FS 200, BL 0 WAS FOUND CORRODED. REPAIRED PER SRM 53-14-1, FIG 11. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN FLOOR SUPPORT AT L1 DOOR, FS 160-200, LBL 50 WAS FOUND CORRODED. REPAIRED PER SRM 51-30. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE RIGHT MAIN CABIN SEAT TRACK AT FS 400 TO 474, RBL 22 WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER SRM 53-05, FIG 4B. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN FLOOR U-CHANNEL FOR THE GALLEY ATTACH FITTING WAS FOUND CORRODED AT FS 200-218, RBL 55. REPAIRED PER SRM 51-30. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN FLOOR CUSP BEAM WEB AT FS 1041, RBL 56 WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER SRM 53-01, FIG 4. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30 K CHECK, THE MAIN CABIN FLOOR WEB AT FS 160-200, RBL 56 T0 LBL 56 WAS FOUND CORRODED. REPAIRED PER SRM 51-30. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN FLOOR SUPPORT AT FS 200, LBL 13 WAS FOUND CORRODED. REPAIRED PER SRM 51-30. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN CUSP BEAM WEB AT FS 446 AND 465, RBL 56 WAS FOUND CORRODED. REPAIRED PER SRM 53-01, FIG 4. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN FLOOR SUPPORT AT FS 180, RBL 25 WAS FOUND CORRODED. REPAIRED PER SRM 53-14-1, FIG 11. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE WEB IN THE AFT CARGO COMPARTMENT WAS FOUND CORRODED ON THE UPPER FLANGE AT FS 1307 AND 1320 BETWEEN LONGERON 27L AND 28L. REMOVED CORROSION AND REPAIRED PER SRM 53-01, FIG 4 AND 51-30-5. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PHX - DURNG 30K CHECK, THE LEFT MAIN CABIN FLOOR CUSP BEAM WEB AT FS 1174 TO 1193, LBL 56 WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER SRM 53-01, FIG 1 AND FIG 4. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE WEB IN THE AFT CARGO COMPARTMENT WAS FOUND CORRODED ON THE UPPER FLANGE AROUND NUTPLATE HOLES AT FS 1307 AND 1320 BETWEEN LONGERON 27R AND 28R. REMOVED CORROSION AND REPAIRED PER SRM 51-30-2 AND 51-30-5. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN CUSP BEAM WEB AT FS 674 TO 693, LBL 56 WAS FOUND CORRODED. REPAIRED PER SRM 53-01 FIG 4. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN CUSP BEAM WEB AT STATION 636 TO 655, LBL 56 WAS FOUND CORRODED. REPAIRED PER SRM 53-01 FIG 4. (M)

Part: FITTING — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN FLOOR SUPPORT MOUNT FITTING AT FS 160, RBL 10 WAS FOUND CORRODED. REPAIRED PER SRM 51-30. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE SUB FLOOR WEB AT FS 148-156, RBL 53 WAS FOUND CORRODED. REPAIRED PER SRM 53-01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN FLOOR SUPPORT AT FS 200, LBL 56 WAS FOUND CORRODED. REPAIRED PER SRM 51-30. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN FLOOR SUPPORT AT L1 DOOR, FS 160-200, LBL 45 WAS FOUND CORRODED. REPAIRED PER SRM 51-30. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN FLOORBOARD SUPPORT AT STATION 200, RBL 58 WAS FOUND CORRODED. REPAIRED PER SRM 51-30. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE LEFT MAIN CABIN FLOOR CUSP BEAM WEB AT FS 1231 TO 1250, LBL 56 WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER SRM 53-14-3, FIG 12. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE FLOOR SUPPORT AT FS 160-200, RBL 6 WAS FOUND CORRODED. REPAIRED PER SRM 53-14-1. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN FLOOR SUPPORT AT LBL 6, FS 160-200 WAS FOUND CORRODED. REPAIRED PER SRM 51-30. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN FLOOR SUPPORT AT FS 160-200, RBL 50 WAS FOUND CORRODED. REPAIRED PER SRM 51-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE MAIN CABIN FLOOR SUPPORT AT FS 200, RBL 9 TO 43 WAS FOUND CORRODED. REPAIRED PER SRM 51-30. (M)

Part: SLIDE — WILL NOT TEST (PAX DOOR) · airframe 28,227 hrs · 14,264 cycles

PHX - DURING 30K CHECK, THE L2 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE L2 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (X)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: CONNECTOR — DISCONNECTED (ROWS 13-16)

SEA DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 13 THROUGH 16 WERE FOUND INOPERATIVE. RECONNECTED CONNECTOR TO LIGHT ASSEMBLY IN FLOOR TRACK AND LIGHTS OPERATED NORMALLY. (X)

Part: CONNECTOR — LOOSE (CABIN)

PHX - PRIOR TO DEPARTURE OF FLT 721 - CREW REPORTED THE EMERGENCY FLOOR TRACK RED LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. SECURED LOOSE CONNECTOR IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

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

Part: WINDOW — OUT OF ADJUST (RT COCKPIT)

SEA - AFTER ARRIVAL OF FLIGHT 472, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOULD NOT OPEN. ADJUSTED UPPER LOCK BAR LINKAGE AND OPERATED NORMALLY. (M)

Part: HINGE PIN — LOOSE (COCKPIT WINDOW)

PDX - AFTER ARRIVAL OF FLT 317, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW OPERATING MECHANISM DETACHED. FOUND WINDOW LOWER AFT HINGE PIN MIGRATING OUT. REINSTALLED HINGE PIN AND OPERATED NORMALLY. (M)

Part: POWER SUPPLY — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WOULD NOT EXTINGUISH. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

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

Part: WINDOW — OUT OF ADJUST (LT COCKPIT)

SEA - PRIOR TO DEPARTURE OF FLIGHT 231, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. ADJUSTED WINDOW MECHANISM AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - PRIOR TO DEPARTURE OF FLIGHT 366, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 8 FORWARD WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: WINDOW — OUT OF ADJUST (LT COCKPIT)

SEA - PRIOR TO DEPARTURE OF FLIGHT 451, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. ADJUSTED WINDOW UPPER GUIDE MECHANISM AND OPERATED NORMALLY. (M)

Part: LOCK — BINDING (COCKPIT)

FAI - PRIOR TO DEPARTURE OF FLIGHT 80, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOULD NOT OPEN. FREED WINDOW UPPER LOCK MECHANISM AND OPERATED NORMALLY. (M)

Part: LOCK MECH — BINDING (COCKPIT)

FAI - AFTER ARRIVAL OF FLIGHT 97, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOULD NOT OPEN. LUBRICATED WINDOW UPPER LOCK MECHANISM AND OPERATED NORMALLY. (M)

Part: SLIDE — MALFUNCTIONED (PAX DOOR)

OAK - DURING C-CHECK, THE L2 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE L2 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND DIM. REPLACED SECOND FROM FORWARD LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE RED EMERGENCY FLOOR TRACK LIGHT AT THE AFT GALLEY WAS FOUND INOPERATIVE. REPLACED LAMP MODULE AT AFT GALLEY AND OPERATED NORMALLY. (M)

Part: BEARING — WORN (SERVICE DOOR)

SEA - ARRIVAL OF FLT 88, CREW REPORTED THE L2 DOOR WOULD NOT FULLY OPEN. REPLACED THE UPPER HINGE TORQUE TUBE BEARING AND OPERATED NORMALLY. (M)

Part: WIRE — DEFECTIVE (CABIN)

ONT - PRIOR TO DEPARTURE OF FLT 531, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. REPAIRED WIRE IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: HOLD OPEN HOOK — BENT (L1 DOOR)

ONT - FLT 595 - PRIOR TO DEPARTURE, CREW REPORTED THE L1 DOOR WOULD NOT CLOSE. REPLACED THE DOOR HOLD OPEN HOOK AND OPERATED NORMALLY. AIRCRAFT TT: 21,095 HOURS. AIRCRAFT TC: 10,731.(X)

Part: LIGHT — DEFECTIVE (CABIN)

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

Part: HANDLE PIN — BROKEN (L2 DOOR)

SEA - AFTER ARRIVAL OF FLT 513, CREW REPORTED THE L2 DOOR HANDLE WOULD NOT CLOSE PROPERLY. REPLACED THE L2 DOOR HANDLE RETAINING PIN AND OPERATED NORMALLY. (M)

Part: RETAINING PIN — BROKEN (L2 DOOR)

SEA - AFTER ARRIVAL OF FLT 191, CREW REPORTED THE L2 DOOR HANDLE WAS NOT POSITIONED CORRECTLY. REPLACED THE L2 DOOR HANDLE RETAINING PIN AND OPERATED NORMALLY. (M)

Part: INFLATION BOTTLE — HIGH PRESSURE (L1 DOOR)

PDX - DURING MAINTENANCE CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND HIGH. REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)

Part: WIRE — BROKEN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 6 TO 9 WERE FOUND INOPERATIVE. REPAIRED BROKEN WIRE IN TRACK AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 6 TO 8 WERE FOUND INOPERATIVE. RECONNECTED WIRING IN TRACK ASSEMBLY AND 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: SLIDE — FAILED TEST (TAILCONE)

OAK - DURING C-CHECK, THE TAILCONE EMERGENCY EVACUATION SLIDE EMERGENCY LIGHTS FAILED TEST. REPLACED THE TAILCONE EMERGENCY EVACUATION SLIDE. (M)

Part: SLIDE — FAILED TEST (L2 DOOR)

OAK - DURING C-CHECK, THE L2 DOR EMERGENCY EVACUATION SLIDE EMERGENCY LIGHTS FAILED TEST. REPLACED THE L2 DOOR EMERGENCY EVACUATION SLIDE. (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: WIRE — BROKEN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 6 TO 9 WERE FOUND INOPERATIVE. REPAIRED WIRING AT ROW 6 AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 14 TO 16 WERE FOUND INOPERATIVE. RECONNECTED WIRE AT ROW 17 AND OPERATED NORMALLY. (M)

Part: LIGHT — DEFECTIVE (CABIN)

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

Part: WIRE — DISCONNECTED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS AT ROW 6 WERE FOUND INOPERATIVE. FOUND WIRING DISCONNECTED, RECONNECTED WIRING AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - PRIOR TO DEPARTURE OF FLT 203 - CREW REPORTED, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING AT ROW 3 AND OPERATED NORMALLY. (M)

Part: LAMP — DEFECTIVE (CABIN)

PDX - FLT 56 - EMERGENCY EXIT FLOOR TRACK LIGHTING INOPERATIVE ROWS S30 AND 32/33. RELAMPED AND INSTALLED NEW SECTION OF TRACK; LIGHTS OPERATED NORMALLY. REFERENCE: OPERATORS CONTROL NR 96ZZZX3853. (X)

Part: TRACK — DEFECTIVE (CABIN)

PDX - FLT 56 - EMERGENCY EXIT FLOOR TRACK LIGHTING INOPERATIVE ROWS S30 AND 32/33. RELAMPED AND INSTALLED NEW SECTION OF TRACK; LIGHTS OPERATED NORMALLY. REFERENCE: OPERATORS CONTROL NR ASAA9680154.

Part: WIRE — BROKEN (CABIN)

LAX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTSFROM ROW 30 AFT WERE FOUND INOPERATIVE. REPAIRED BROKEN WIRE AT ROW 31 ANDOPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. RECONNECTED WIRING AT ROW 2 AND OPERATED NORMALLY. (X)

Part: TRACK LIGHT — DEFECTIVE (FWD CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AT ROW 2 AND OPERATED NORMALLY. (W)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 25 TO 28 WERE FOUND INOPERATIVE. RECONNECTED WIRING AND 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: EEL WIRING — DISCONNECTED (CABIN)

LAX - FLT 255 - PRIOR TO DEPARTURE, CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT THE OVERWING EXIT AREA WERE INOPERATIVE. REPAIRED BROKEN WIRING IN FLOOR TRACK LIGHTS AT OVERWING EXIT AREA, AND LIGHTS OPERATED NORMALLY. (W)