N958AS

Part: DOUBLER — CHAFED (FLAP VANE) · airframe 54,121 hrs · 28,969 cycles

RIGHTHAND WING OUTBOARD FLAP INBOARD FIXED VANE L/E DOUBLER IS CHAFED. REPLACED EXISTING DOUBLER PER SRM 51-70-2.

Part: FLOOR PANEL — DELAMINATED (BS 196-256) · airframe 54,121 hrs · 28,969 cycles

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

Part: FLOOR PANEL — DELAMINATED (BS 160-196) · airframe 54,121 hrs · 28,969 cycles

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

Part: FRAME — CRACKED (BS 1418) · airframe 54,121 hrs · 28,969 cycles

FRAME CRACKED. REPLACED FRAME PER SRM 53-03.

Part: FLOOR PANEL — BROKEN (BS 160-200) · airframe 54,121 hrs · 28,969 cycles

CABIN FLOOR PANEL CRACKED WITH DAMAGED INSERTS. REPLACED PANEL PER SRM 53-05 AND DAC DWG S4932106.

Part: STIFFENER — CRACKED (BS 1418) · airframe 54,121 hrs · 28,969 cycles

FRAME STIFFENER CRACKED. REPLACED STIFFENER PER SRM 51-30-5, 51-30-2 AND DAC DWG 5913595.

Part: LONGERON — CRACKED (BS 1418-1419) · airframe 54,121 hrs · 28,969 cycles

LONGERON CRACKED. REMOVED DAMAGED SECTION OF LONGERON. INSTALLED REPLACEMENT SECTION PER SRM 53-02 (SPLICE REPAIR).

Part: FLOOR PANEL — BROKEN (BS 180-200) · airframe 54,121 hrs · 28,969 cycles

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

Part: RIB — DAMAGED (SLAT) · airframe 54,121 hrs · 28,969 cycles

LEFTHAND WING NR 5 L/E SLAT OUTBOARD RIB HOLES OVERSIZED. REPLACED WORN RIB PER SRM 51-10-4 AND 51-30-2.

Part: VANE — GOUGED (TE FLAP) · airframe 54,121 hrs · 28,969 cycles

LEFTHAND WING OUTBOARD FLAP INBOARD VANE L/E DOUBLER REPAIR IS GOUGED. REPLACED EXISTING REPAIR DOUBLER PER SRM 51-70-2.

Part: TRACK — CORRODED (BS 160-200) · corrosion level 2 · airframe 54,121 hrs · 28,969 cycles

CABIN FALSE TRACK IS CORRODED. REPLACED TRACK PER SRM 51-10-3, 51-10-4, 53-14-1, AND 51-30-5.

Part: SEAT TRACK — CORRODED (BS 196-241) · airframe 54,121 hrs · 28,969 cycles

CABIN SEAT TRACK EXISTING REPAIR SPLICE CORRODED. REMOVED DAMAGED SECTION OF TRACK. INSTALLED REPLACEMENT PER SRM 51-10-4 AND 53-05.

Part: CUSP WEB — CRACKED (BS 1297-1301) · airframe 54,121 hrs · 28,969 cycles

CUSP WEB CRACKED. STOP DRILLED CRACK. INSTALLED REPAIR PARTS PER SRM 53-05.

Part: FLOOR PANEL — BROKEN (BS 160-196) · airframe 54,121 hrs · 28,969 cycles

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

Part: TRACK — CORRODED (BS 160-200) · corrosion level 2 · airframe 54,121 hrs · 28,969 cycles

CABIN FLOOR FALSE TRACK IS CORRODED. REPLACED FALSE TRACK PER SRM 51-10-3, 51-10-4, 53-14-1 AND 51-30-5.

Part: FLOOR PANEL — BROKEN (BS 196-256) · airframe 54,121 hrs · 28,969 cycles

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

Part: FLOOR PANEL — DELAMINATED (BS 196-256) · airframe 54,121 hrs · 28,969 cycles

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

Part: SHEAR TIE — CRACKED (BS 1437) · airframe 54,121 hrs · 28,969 cycles

SHEAR TIE IS CRACKED. REPLACED SHEAR TIE PER SRM 51-10-4, 51-30-2 AND 51-30-5.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 54,121 hrs · 28,969 cycles

RIGHTHAND SIDE OF VERTICAL STABILIZER EXTERNAL VERTICAL TO FUSELAGE JOIN STRAP (ATTACH ANGLE) IS CRACKED. REPLACED DAMAGED SECTION OF JOIN STRAP PER SRM 53-05.

Part: FLOOR PANEL — BROKEN (BS 200-256) · airframe 54,121 hrs · 28,969 cycles

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

Part: FLOOR PANEL — BROKEN (BS 148-160) · airframe 54,121 hrs · 28,969 cycles

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

Part: FRAME — DENTED (FUSELAGE) · airframe 51,966 hrs · 27,952 cycles

NLG WHEELWELL LEFT FRAME JUST FORWARD OF LEFT INNER BULKHEAD WAS DENTED. REPLACE FRAME PER SRM 51 30 02.

Part: WINDOW — STUCK (COCKPIT) · airframe 51,626 hrs · 27,796 cycles

CAPTAIN SIDE SLIDING WINDOW WOULD NOT OPEN. ADJUSTED WINDOW CAM FOLLOWER. OP CHECKED OK.

Part: ENGINE — FAILED (RIGHT) · airframe 51,619 hrs · 27,793 cycles

EN ROUTE SAN SEA - RIGHTHAND ENGINE R OIL STRAINER CLOGGING ANNUNCIATED. CREW SHUTDOWN ENGINE AS PRECAUTION AND DIVERTED TO SMF. SUBSEQUENTLY FOUND METAL CONTAMINATION IN THE OIL FILTER SUGGESTING IMPENDING INTERNAL FAILURE. REMOVED ENGINE. WILL BE SENT TO SHOP FOR INVESTIGATION.

Part: WINDOW — STUCK (COCKPIT) · airframe 51,525 hrs · 27,742 cycles

DURING TAXI TO GATE, COCKPIT LEFT SLIDING WINDOW WOULD NOT OPEN. ADJUSTED UPPER CAM FOLLOWER.

Part: WINDOW — STUCK (COCKPIT) · airframe 51,518 hrs · 27,739 cycles

ON TAXI TO GATE, COCKPIT LEFT SLIDING WINDOW WOULD NOT OPEN. REALIGNED UPPER FORWARD GUIDE PIN.

Part: SKIN — GOUGED (TE FLAP) · airframe 50,409 hrs · 27,215 cycles

RIGHT OUTBOARD FLAP INBOARD VANE IS GOUGED ON EXISTING REPAIR AT INBOARD LEADING EDGE. REMOVED EXISTING REPAIR DOUBLER. INSTALLED SKIN FILLER AND EXTERNAL DOUBLER PER SRM 57 03.

Part: SHEAR TIE — CORRODED (BS 693 S29-30R) · corrosion level 1 · airframe 50,409 hrs · 27,215 cycles

FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 51 10 4 51 10 3 AND 51 30 5.

Part: SKIN — GOUGED (TE FLAP) · airframe 50,409 hrs · 27,215 cycles

LEFT OUTBOARD FLAP INBOARD VANE IS GOUGED ON EXISTING REPAIR AT INBOARD LEADING EDGE. REMOVED EXISTING REPAIR DOUBLER. INSTALLED SKIN FILLER AND EXTERNAL DOUBLER PER SRM 57 03.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,408 hrs · 27,215 cycles

SHEAR TIE CORRODED OUT OF LIMITS AT FS 1211 BETWEEN LONGERONS 29R AND 30. REMOVED DAMAGED SHEAR TIE FABRICATED AND INSTALLED A REPLACEMENT SHEAR TIE IAW MD 80 SRM 51 10 4 51 40 3 AND 51 30 5.

Part: RIB — GOUGED (L/E SLAT) · airframe 50,408 hrs · 27,215 cycles

THE RT NR 4 SLAT O B FITTING (RIB ASSY) IS GOUGED OUT OF LIMITS. REMOVED DAMAGED RIB ASSY LOCATED DRILLED AND INSTALLED A REPLACEMENT RIB ASSY IAW MD 80 SRM 51 10 4 AND 51 30 8

Part: SKIN — MISDRILLED (FUSELAGE) · airframe 50,408 hrs · 27,215 cycles

FUSELAGE SKIN HAS MECHANICAL DAMAGE. (MISDRILLS DUE TO PREVIOUSLY ACCOMPLISHED STOP DRILLS ON THE R H ENGINE PYLON UPPER AFT FAIRING SUPPORT ANGLE) CUT OUT DAMAGED AREA OF SKIN. FABRICATED AND INSTALLED A FILLER EXTERNAL DOUBLER AND TWO TAPERED SHIMS IAW AAR EA 11608 AND ASA EA 5330 02116.

Part: WIRE — LOOSE (LIGHT)

ANC LINE CHECK, FOUND AFT EXIT CATWALK SIDE PANEL EMERGENCY LIGHT INOPERATIVE. RESECURED LOOSE WIRE CONNECTOR. LIGHT THEN OPERATED PROPERLY. (M)

Part: SKIN — DENTED (FLAP VANE)

DURING C-CHECK, FOUND RT WING INBOARD FLAP OUTBOARD FLAP VANE UPPER SURFACE DENTED. INSTALLED REPAIR DOUBLER. (M)

Part: RIB — CRACKED (NR 4 SLAT)

DURING C-CHECK, FOUND LT WING NR 4 SLAT ACCESS CUTOUT RIB CRACKED. INSTALLED REPAIR DOUBLER PER EA 5740-01447. (M)

Part: SKIN — GOUGED (FLAP VANE)

DURING C-CHECK FOUND, LT WING OUTBOARD FLAP INBOARD FLAP VANE LEADING EDGE GOUGED. REMOVED DAMAGE. INSTALLED REPAIR FILLER AND DOUBLER. (M)

Part: SKIN — GOUGED (FUSELAGE)

FOUND DURING C-CHECK, FUSELAGE SKIN GOUGED. REMOVED DAMAGE. REPAINTED. (M)

Part: SKIN — DELAMINATED (FLAP VANE)

FOUND DURING C-CHECK, LT WING INBOARD FLAP VANE OUTBOARD SEGMENT DELAMINATED. REMOVED DAMAGE. INSTALLED REPAIR FILLERS AND DOUBLERS. (M)

Part: SKIN — DENTED (ELEVATOR)

FOUND DURING C-CHECK, LT ELEVATOR ANTI-FLOAT TAB UPPER SURFACE DENTED. INSTALLED REPAIR DOUBLERS. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

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

Part: SKIN — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND FUSELAGE SKIN CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M)

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

SEA - PREFILGHT CHECK, FOUND FIRST FIVE EMERGENCY TRACK LIGHTS TESTS INOPERATIVE, TWICE. RECONNECTED MODULE CONNECTOR, TWICE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: TAB — DENTED (ANTIFLOAT)

OKC - DURING 15K CHECK, FOUND LEFT ANTI-FLOAT TAB UPPER SURFACE IS DENTED. APPLIED FILLER PER SRM 55-04. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND WEB IS CORRODED AT LONGERON 18L NEAR L2 DOOR. REMOVED CORROSION. INSTALLED FILLER AND DOUBLER PER SRM 53-01. (M)

Part: SKIN — GOUGED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN IS GOUGED AT STATION 235. REMOVED DAMAGED SECTION. REPAIRED WITH FILLER AND DOUBLER PER SRM 53-04. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING 15K CHECK, FOUND LEFT INBOARD SEAT TRACK IS CORRODED AT FS 1098-1165. REPLACED SEAT TRACK PER SRM 51-10-4 AND 51-30-5. (M)

Part: SPLICE — CORRODED (LONGERON)

OKC - DURING 15K CHECK, FOUND LONGERON SPLICE AT L1 AT FS 750-769 IS CORRODED. REPLACED SPLICE PER SRM 51-30-5. (M)

Part: STRINGER — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND STRINGER IS CORRODED UNDER LOWER FLANGE AT FS 1212. REMOVED DAMAGED SECTION. REPLACED WITH SPLICE PER SRM 53-02, 51-10-3, AND 51-60-0. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND INTERCOSTAL IS CORRODED AT FS 1221. REPLACED INTERCOSTAL PER SRM 51-10-4, 51-10-2, AND 51-30-5. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURNG 15K CHECK, FOUND FUSELAGE SKIN IS DENTED AT FS 237. INSTALLED DOUBLER PER SRM 53-04. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND RIGHT INBOARD SEAT TRACK IS CORRODED AT FS 200-247. REPLACED SEAT TRACK PER SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND LEFT OUTBOARD SEAT TRACK IS CORRODED AT FS 1106-1185. REPLACED DAMAGED TRACK PER SRM 51-10-4 AND 51-30-5. (M)

Part: SPLICE — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND STRUCTURAL SPLICE IS CORRODED AT FS 1212 IN AFT CARGO BAY AREA. REMOVED CORROSION AND TREATED PER EA 5310-02309. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND LONGERON 23R CORRODED AT FS 769-788. REMOVED CORROSION AND INSTALLED REPAIR U-CHANNEL PER SRM 53-02. (M)

Part: TRUNNION — GOUGED (LT MLG)

OKC - DURING 15K CHECK, FOUND LEFT MLG FORWARD TRUNNION FITTING IS GOUGED ON LOWER SIDE. REMOVED DAMAGE, PERFORMED HFEC, FLAP PEEN, AND TREATED AND PRIMED AREA PER EA5740-01373. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND CABIN FLOOR PANEL IS DELAMINATED AT FS 886-927. REPLACED FLOOR PANEL PER SRM 51-01. (M)

Part: SKIN — CORRODED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN CORRODED AT AFT LAVATORY SERVICE PANEL. REMOVED CORROSION AND INSTALLED REPAIR STRAP PER EA 5320-01635. (M)

Part: FLOORBOARD — PUNCTURED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND CABIN FLOOR PANEL IS PUNCTURED AT FS 1041. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND CABIN FLOOR PANEL HAS DAMAGED CORE AT FS 655. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLANGE — CRACKED (WASTE CHUTE)

OKC - DURING 15K CHECK, FOUND LEFT AFT LAVATORY WASTE CHUTE MOUNTING FLANGE CRACKED. STOP-DRILLED CRACKS AND INSTALLED DOUBLER PER EA 2540-01116. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN IS DENTED AT FS 1398. INSTALLED DOUBLER PER SRM 53-04. (M)

Part: BEAM — CORRODED (FUSELAGE)

DURING INSPECTION, FOUND AFT PIT LOWER FLANGE ON BEAM AT CARGO DOOR IS CORRODED AT STATION 1182. REPAIRED BY REMOVED DAMAGED BEAM, INSTALLED NEW BEAM IAW MD80 SRM 51-30-2, 51-30-5, 51-10-3. (M)

Part: SKIN — TOOL DAMAGE (FUSELAGE)

OKC - DURING INSPECTION, FOUND RIVET SET MARK AT STATION 398, LONGERON 30, ON SKIN. REPAIRED BY COLD WORKED AREA, COMPLIED WITH HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-04. (M)

Part: SHEAR TIE — CORRODED (FS 1193)

OKC - DURING INSPECTION, FOUND AFT PIT STATION 1193 BETWEEN STRINGER 20 AND 29L SHEAR TIE CORRODED. REPAIRED BY REMOVED DAMAGE, FABRICATED REPAIR SHEAR TIE AND SPLICE IAW MD80 SRM 53-03. (M)

Part: FLOOR PANEL — DEBONDED (FS)

OKC - DURING 15K CHECK, FOUND EXISTING CABIN FLOOR PANEL REPAIR DOUBLER HAS DISBONDED AT FS 1155-1250. REBONDED DOUBLER EPR SRM 51-70-1. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND CABIN FLOOR PANEL IS DELAMINATED AT FS 1003-1041. REPLACED PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — DEBONDED (FUSELAGE)

OKC - DURING 15K CHECK, FOUND CABIN FLOOR PANEL JOINING STRIP HAS DISBONDED AT FS 1155-1250. REBONDED JOINING STRIP PER SRM 51-70-1. (M)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE)

DURING 15K CHECK, FOUND CABIN FLOOR PANEL IS PUNCTURED AT FS 1079-1155. FILLED PUNCTURE WITH FIBER RESIN AND GLASS OVERLAY PER SRM 51-70-1. (M)

Part: SKIN — DENTED (L1 DOOR)

SEA PREFLIGHT CHECK, FOUND FORWARD PAX DOOR DENTED, CAUSING DOOR TO BE DIFFICULT TO OPEN. REPAIRED DENT PER SRM 52-05. RERIGGED DOOR. DOOR THEN OPERATED PROPERLY. (M)

Part: SKIN — DENTED (PAX DOOR)

PREFLT CHECK, FORWARD PAX DOOR SKIN IS DENTED CAUSING DOOR TO BE HARD TO OPEN. REPAIRED DENT PER SRM 52-05 AND 51-10-03. DOOR THEN OPERATED PROPERLY. (M)

Part: DOOR — OUT OF RIG (PAX DOOR)

SEA PREFLIGHT CHECK, FORWARD PAX DOOR DIFFICULT TO OPEN. RERIGGED DOOR. DOOR THEN OPERATED PROPERLY. (M)

Part: SPRING — BROKEN (WINDOW)

LAX PREFLIGHT CHECK, LEFT CAPTAINS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. REPLACED UPPER LOCK BAR SPRING. WINDOW THE OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (AFT CABIN)

SEA - DURING PREFLIGHT CHECK, NOT ALL EMERGENCY TRACK LIGHTING ILLUMINATED UPON TEST. REPAIRED DAMATED WIRING IN FORWARD CABIN. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (ROW 6)

SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE FORWARD OF ROW 6. REPLACED BROKEN WIRE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WINDOW — JAMMED (COCKPIT)

OAK - DURING PREFLIGHT CHECK, FOUND CAPTAINS CLEARVIEW WINDOW JAMMED IN CLOSED POSITION. ADJUSTED WINDOW PER MM 56-10-03. WINDOW THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

SEA - DURING LINE CHECK, FOUND EMERGENCY SLIDE LANYARD 'NOT ROOTED' (DISCONNECTED) AT AFT LEFT SERVICE L-2 DOOR. 'ROOTED', REATTACHED, LANYARD. (M)

Part: LANYARD — DISCONNECTED (DOOR SLIDE)

SEA - DUIRNG PREFLIGHT CHECK, FOUND FORWARD SERVICE R-1 DOOR SLIDE LANYARD BETWEEN HAD BECOME DISCONNECTED. REATTACHED LANYARD. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

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

Part: MODULE — BROKEN (CABIN)

ANC - FOUND DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHT MODULE BROKEN IN FORWARD CABIN. RECONNECTED MODULE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — BROKEN (CABIN)

SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHT MODULE BROKEN NEAR FORWARD GALLEY. REPLACED MODULE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

DURING PREFLIGHT CHECK LANYARD BETWEEN GIRT BAR AND SLIDE COVER WAS FOUND DISCONNECTED. REATTACHED LANYARD.

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

DURING PREFLIGHT CHECK, LANYARD BETWEEN GIRT BAR AND SLIDE COVER, BECAME DISCONNECTED. REATTACHED LANYARD.

Part: CONNECTOR — DISCONNECTED (CABIN)

DURING PREFLIGHT CHECK SOME EMERGENCY TRACK LIGHTS IN 1ST CLASS CABIN WERE FOUND TO BE INOPERATIVE. REATTACHED LOOSE CONNECTORS. LIGHTS THEN OPERATED PROPERLY.

Part: LONGERON — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND PITTING CORROSION ON LONGERON 29R, AFT CARGO BAY DOOR BEAM. REPLACED BEAM PER SRM 51-30-5. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, AFT CARGO BAY DOOR JAMB BEAM WAS FOUND TO BE CORRODED ON HORIZONTAL AND VERTICAL LEGS FROM FS 1155-1212. REPLACED DOOR JAMB BEAM PER SRM'S 51-10-3, 51-30-2, AND 51-30-5. (M)

Part: SKIN — DAMAGED (T/E FLAP)

OAK - DURING C-CHECK, DETERMINED RIGHT OUTBOARD FLAP SKIN TEMP REPAIR REQUIRED REPLACEMENT WITH PERMANENT REPAIR. REPLACED TEMP REPAIR DOUBLER WITH PERMANENT REPAIR DOUBLER PER EA 5750-01526 REV B. (M)

Part: LANYARD — DISCONNECTED (EVAC SLIDE)

SEA - FORWARD SERVICE R-1 DOOR EMERGENCY SLIDE LANYARD DISCONNECTED. REATTACHED LANYARD. (M)

Part: WIRE — BROKEN (AFT CABIN)

SEA - DURING LINE CHECK, FOUND BROKEN WIRE IN EMERGENCY TRACK LIGHTS AT ROW 20-31. REPLACED BROKEN WIRE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: CONNECTOR — DISCONNECTED (AFT CABIN)

PDX - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE, AT ROW 29. RESECURED ELECTRICAL CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING PREFLIGHT CHECK, FIRST CLASS EMERGENCY FLOOR TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. RECONNECTED WIRING BETWEEN MODULES. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING PREFLIGHT CHECK, 1ST CLASS EMERGENCY FLOOR TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. RECONNECTED WIRING BETWEEN MODULES. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (L1 DOOR)

SEA - DURING PREFLIGHT CHECK, L-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED FROM SLIDE COVER LATCH. REATTACHED LANYARD BETWEEN GIRT BAR AND DOOR SLIDE COVER LATCH. (M)

Part: LIGHT — INOPERATIVE (FWD CABIN)

PDX - DURING PREFLIGHT CHECK, EMERGENCY FLOOR TRACK LIGHTS IN 1ST CLASS SECTION WERE FOUND TO BE INOPERATIVE. REPLACED DAMAGED SECTION OF WIRING. LIGHTS THEN OPERATED NORMALLY. (M)

Part: GUIDE — OUT OF ADJUST (COCKPIT WINDOW)

SEA - DURING PREFLIGHT CHECK, THE CAPTAINS SLIDING CLEAR VIEW WINDOW COULD NOT BE OPENED. ADJUSTED WINDOW LATCH GUIDE. WINDOW THEN OPERATED PROPERLY. (M)

Part: MODULE — DISCONNECTED (CABIN)

SEA - DURING A PREFLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED MODULE IN FIRST CLASS. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — DISCONNECTED (CABIN)

SEA - DURING A LINE MAINTENANCE CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED MODULE IN AFT PART OF FIRST CLASS. LIGHTS THEN OPERATED PROPERLY. (M)

Part: BATTERY PACK — DISCHARGED (TAILCONE)

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

Part: PIN — NOT SEATED (COCKPIT)

SEA - DURING PREFLIGHT CHECK, THE CAPTAINS SLIDING CLEARVIEW WINDOW COULD NOT BE OPENED. RESEATED WINDOW UPPER ARM PIN. WINDOW THEN OPERATED PROPERLY. (M)

Part: MODULE — DISCONNECTED (CABIN)

SEA - DURING PRE-FLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS DISCONNECTED AT ROW 3. RECONNECTED LIGHT MODULE SOCKET. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WINDOW (COCKPIT)

SEA - DURING PREFLIGHT CHECK, IT WAS DETERMINED THAT THE CAPTAINS SLIDING CLEARVIEW WINDOW COULD NOT BE OPENED. RESET ACTUATOR CAM UPPER LOCK BAR IN CHANNEL. WINDOW THEN OPERATED PROPERLY. (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: SLIDE — OUT OF POSITION (R1 DOOR)

SEA - DURING PRE-FLIGHT CHECK, FOUND R1 SLIDE PACK OFF DOOR. REINSTALLED SLIDE PACK IN DOOR SHROUD. (M)

Part: WIRE ROPE — OUT OF POSITION (TAILCONE)

PDX - DURING SERVICE CHECK, FOUND TAILCONE RELEASE CABLE OFF ONE OF THE CAMS. PROPERLY LOOPED RELEASE CABLE OVER CAM. (M)

Part: LIGHT — LOOSE (CABIN)

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

Part: BATTERY — DISCHARGED (TAILCONE)

SEA - DURING MAINTENANCE CHECK, THE TAILCONE SLIDE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: WIRE — DISCONNECTED (CABIN)

SEA - PRIOR TO FLT 400 - THE EMERGENCY EXIT FLOOR TRACK LIGHTS IN FIRST CLASS WOULD NOT ILLUMINATE. REPLACED WIRING SECTION AND THE LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

LAX - FLT 251 - CREW REPORTED EMERGENCY EXIT FLOOR TRACK LIGHTING IN FIRST CLASS INOPERATIVE. SECURED LOOSE TRACK LIGHT AND LIGHTING OPERATED NORMALLY. (M)

Part: DOOR — OUT OF ADJ (MAIN PAX)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WAS BINDING ON THE FUSELAGE DURING CLOSING. ADJUSTED THE L1 DOOR RIG PER DC9 MM AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN) · airframe 29,794 hrs · 16,846 cycles

LAX - FLT 243 - PRIOR TO DEPARTURE , FLIGHT CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTS IN THE FIRST CLASS CABIN WERE FOUND INOPERATIVE. RE-CONNECTED LOOSE WIRING IN TRACK AND LIGHTS OPERATED NORMALLY. (X)

Part: LIGHT — INOPERATIVE (ESCAPE SLIDE)

PHX - DURING 30K CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)

Part: WEB — CRACKED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CRACK IN CUSP WEB AT FS 220, RBL 50. REMOVED DAMAGED MATERIAL AND INSTALLED FILLER AND DOUBLER IAW DC9 SRM 53-01, FIG 4. (M)

Part: SKIN — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND ON FUSELAGE SKIN AT FS 180, LONGERON 19R TO 20R. REMOVED CORROSION AND TREATED AREA IAW DC9 SRM 53-04. (M)

Part: FRAME — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON FRAME AT FS 1155, LONGERON 29L TO 29R. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN FLOORBOARD SUPPORT FROM FS 160 TO 200, RBL 57. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-14-01, FIG 11. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK AT FS 237, RBL 48. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-05, FIG 4F. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON SHEAR TIE AT FS 1022, LONGERON 28L TO 29L. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30-05. (M)

Part: CARGO TRACK — DAMAGED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND ON CARGO COMPARTMENT TIEDOWN TRACK AT FS 1008, LONGERON 28L. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-05, FIG 4G. (M)

Part: FRAME — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON FRAME AT FS 1079, LONGERON 30. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW ASA EA 5310-01782. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK FROM FS 1079 TO 1098, LBL 24. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-05. (M)

Part: FRAME — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON FRAME AT FS 1231, LONGERON 30 TO 27R. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-03, FIG 2A. (M)

Part: FRAME — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON FRAME AT FS 1231, LONGERON 25L TO 27L. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-03, FIG 2A. (M)

Part: FITTING — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON FRAME FITTING AT FS 1136, RBL 60. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30. (M)

Part: SHEAR TIE — DAMAGED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND ELONGATED HOLE IN SHEAR TIE AT FS 1231, LONGERON 30 TO 29R. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-14-03. (M)

Part: WEB — CORRODED (FUSELAGE)

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

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 580 TO 595, RBL 60. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-14-02. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CARGO COMPARTMENT TIEDOWN TRACK FROM FS 1212 TO 1250, LONGERON 27R TO 28R. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-10-04 AND 51-30-01. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB AT FS 505, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INSTALLED FILLER AND DOUBLER IAW DC9 SRM 53-01. (M)

Part: WEB — CRACKED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CRACK IN CUSP WEB AT FS 1035, LBL 54. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER IAW DC9 SRM 53-01, FIG 4. (M)

Part: LONGERON — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON LONGERON 30 FROM FS 1193 TO 1211. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW ASA EA 5310-01784. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK FROM FS 1136 TO 1174, LBL 48. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-24-00, FIG 6. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 1193 TO 1231, RBL 60. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-10-05. (M)

Part: SKIN — GOUGED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND GOUGES IN FUSELAGE SKIN FROM FS 170 TO 184, LONGERON 26R. REPAIRED WITH INTERNAL AND EXTERNAL DOUBLERS IAW ASA EA 5330-01422. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON SHEAR TIE AT FS 1155, LONGERON 30 TO 29R. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN FLOORBOARD SUPPORT AT FS 200, LBL 8 TO LBL 11. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-14-01. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 864 TO 886, LONGERON 18L. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER IAW DC9 SRM 53-01, FIG 4. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB AT FS 880, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-01, FIG 4. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 826 TO 845, RBL 60. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER IAW DC9 SRM 53-01, FIG 4. (M)

Part: SKIN — CRACKED (RT WING)

PHX - DURING 30K CHECK, FOUND CRACK IN RIGHT WING L/E SKIN AT DCS 193. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-10-03, 51-10-04, AND 51-30-00. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB AT FS 940, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER IAW DC9 SRM 53-01, FIG 4, PAGE 3. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN FLOORBOARD SUPPORT AT FS 200, RBL 8 TO RBL 47. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-14-01. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 693 TO 702, RBL 58. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30-02 AND 51-30-04. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 845 TO 864, LBL 54 TO LBL 60. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER IAW DC9 SRM 53-01, FIG 4. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CARGO COMPARTMENT TIEDOWN TRACK FROM FS 1215 TO 1322, LONGERON 28L. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON SHEAR TIE AT FS 1212, LONGERON 28L TO 28R. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-14-03, 51-10-02, AND 51-30. (M)

Part: WEB — CRACKED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CRACK IN SUBFLOOR WEB AT FS 148, BL 0. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER REPAIR IAW DC9 SRM 53-01, FIG 4. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CARGO COMPARTMENT TIEDOWN TRACK SUPPORT AND LT AT FS 1008, LONGERON 28L. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30-01. (M)

Part: SKIN — CRACKED (LT WING)

PHX - DURING 30K CHECK, FOUND CRACK IN LEFT WING L/E SKIN SPLICE AT XFS 164. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-10-04. (M)

Part: SKIN — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON FUSELAGE SKIN AT FS 294, LONGERON 1. REMOVED CORROSION AND TREATED AREA IAW DC9 SRM 51-10-03. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB AT FS 575, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER AND SHIM IAW DC9 SRM 53-01, FIG 4. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB AT FS 735, RBL 58 TO RBL 60. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-01, FIG 4. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 1098 TO 1117, RBL 54 TO RBL 60. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-01. (M)

Part: LONGERON — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON LONGERON 29L ROM FS 1231 TO 1271. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30-02 AND 51-30-05. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN FLOORBOARD SUPPORT FROM FS 200 TO 214, RBL 57. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURNG 30K CHECK, FOUND CORROSION ON SUBFLOOR WEB FROM FS 160 TO 200, LBL 14 TO RBL 50. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-14-01, FIG 11. (M)

Part: SLIDE — WILL NOT TEST (PAX DOOR)

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

Part: WINDOW — STUCK (COCKPIT)

PDX - AFTER ARRIVAL OF FLT 102, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOULD NOT OPEN. REINSTALLED UPPER GUIDE BEARING INTO TRACK AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - PRIOR TO DEPARTURE OF FLIGHT 720, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - PRIOR TO DEPARTURE OF FLIGHT 87, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN AND MID CABIN WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

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

Part: MECHANISM — LACK OF LUBE (L1 DOOR)

PDX - PRIOR TO DEPARTURE OF FLIGHT 453, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO UNLATCH FROM THE FULL OPEN POSITION. LUBRICATED THE DOOR HOLD OPEN MECHANISM AND OPERATED NORMALLY. (M)

Part: BOTTLE — LOW PRESSURE (L1 DOOR SLIDE)

LAX - PRIOR TO DEPARTURE OF FLIGHT 84, CREW REPORTED THE L1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS LOW. REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE MID CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: CONNECTOR — LOOSE (CABIN)

ANC - PRIOR TO DEPARTURE OF FLIGHT 115, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. SECURED CONNECTOR IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 2 TO 7 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: SLIDE — MALFUNCTIONED (R1 DOOR)

OAK - DURING C-CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE R1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (X)

Part: FRAME — CRACKED (BS 1485)

OAK - DURING C-CHECK, A 2 INCH CRACK WAS FOUND IN FUSELAGE CANTED FRAME AT STA 1485 ADJACENT TO THE AFT ENTRANCE STAIR DOOR JAMB RT SIDE AT THE VENTRAL STAIR ACTUATOR MOUNT BRACKET ATTACH POINT. REMOVED DAMAGED AREA AND SPLICED IN NEW MATERIAL IAW ASA E.A. 5310-01588. (X)

Part: POWER SUPPLY — DEFECTIVE (CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY LIGHTS IN THE TAILCONE AREA WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY 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 5730-01045. (M)

Part: HOLD OPEN HOOK — BENT (L1 DOOR)

SEA - PRIOR TO DEPARTURE OF FLT 332, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO LATCH OPEN. STRAIGHTENED THE HOLD OPEN HOOK AND OPERATED NORMALLY. (M)

Part: HOLD OPEN HOOK — DEFECTIVE (L1 DOOR)

SEA - PRIOR TO DEPARTURE OF FLT 457 - CREW REPORTED, THE L1 DOOR WAS DIFFICULT TO LATCH OPEN. REPLACED THE HOLD OPEN HOOK ASSEMBLY AND OPERATED NORMALLY. (M)

Part: LIGHT — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 21 TO 28 WERE FOUND INOPERATIVE. REPLACED LIGHT SOCKET ASSEMBLY AND OPERATED NORMALLY. (M)

Part: POWER SUPPLY — DEFECTIVE (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

OAK - DURING MAINTENANCE CHECK, THE RIGHT FORWARD OVERWING EMERGENCY EXIT IDENTIFIER SIGN WAS FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M)

Part: LIGHT — DEFECTIVE (CABIN)

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

Part: BOTTLE — LOW PRESS (L1 DOOR)

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

Part: PORTABLE EEL — DEFECTIVE (CABIN)

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

Part: EEL BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGNCY EXIT LIGHTS WERE FOUND INOPERATIVE AT ROWS 19-22. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE AT ROWS 19-22. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 29 AFT WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (W)