N965AS

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 53,788 hrs · 27,738 cycles

AIRCRAFT LOST PRESSURIZATION AT 35K, DESCENDED TO 14K AND PRESSURIZATION BEGAN TO RECOVER. O2 MASK DID NOT DEPLOY AUTOMATICALLY OR MANUALLY WHEN SELECTED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 49,181 hrs · 24,654 cycles

NUMEROUS EMERGENCY EXIT LIGHT INOPERATIVE IN TAIL COMPARTMENT AREA. REPLACED BATTERIES.

Part: STRUCTURE — CHIPPED (LT AILERON) · airframe 46,256 hrs · 23,251 cycles

LEFTHAND AILERON T/E COMPOSITE CHIPPED. BOND REPAIRED PER SRM 51-90-0.

Part: SKIN — GOUGED (ELEVATOR TAB) · airframe 46,256 hrs · 23,251 cycles

RIGHTHAND ELEVATOR CONTROL TAB GOUGED. REPLACED DAMAGED SECTION OF TAB SKIN PER SRM 51-70-2.

Part: WEDGE — GOUGED (T/E FLAP) · airframe 46,256 hrs · 23,251 cycles

FLAP T/E WEDGE IS GOUGED. REPAIRED PER SRM 51-90-0.

Part: FLOORBOARD — CORRODED (FUSELAGE)

HV-CHECK - PAX CABIN FLOOR PANEL IS WATER DAMAGED AND HAS CORRODED FASTENERS. REPLACED FLOOR PANEL. (K)

Part: FLOOR PANEL — DELAMINATED (PAX CABIN)

HV - CHECK - PAX CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)

Part: FLOORBOARD — DELAMINATED (CABIN)

HV- CHECK - PAX CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)

Part: FLOORBOARD — DELAMINATED (CABIN)

HV - CHECK - PAX CABIN FLOOR PANEL IS DELAMINATED AND CRACKED. REPLACED FLOOR PANEL. (K)

Part: FLOORBOARD — DELAMINATED (CABIN)

HV - CHECK - PAX CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)

Part: TAB — DELAMINATED (LT ELEVATOR)

HV-CHECK - LT ELEVATOR GEAR TAB IS DELAMINATED. BONDED CORE AND INSTALLED REPAIR DOUBLER. (K)

Part: FLOORBOARD — DELAMINATED (CAIBN)

HV - CHECK - PAX CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)

Part: FLOORBOARD — DELAMINATED (CABIN)

HV - CHECK - PAX CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)

Part: VANE — WORN (TE FLAP)

HV-CHECK - LT IB FLAP IB VANE IS WORN AT LEADING EDGE. INSTALLED REPAIR DOUBLER. (K)

Part: GEAR — DENTED (ELEV TAB)

HV - CHECK - LT ELEVATOR GEAR TAB IS DENTED. INSTALLED REPAIR DOUBLER. (K)

Part: SKIN — DENTED (FUSELAGE)

HV - CHECK - RT SIDE OF THE FUSELAGE IS DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLERS, DOUBLERS, AND FINGER DOUBLERS. (K)

Part: SKIN PANEL — ELONGATED (LT WING)

HV- CHECK - LT WING ACCESS PANEL 1392C HAD ELONGATED FASTENER HOLES. REPLACED PANEL. (K)

Part: VANE — CHAFED (TE FLAP)

HV-CHECK - LT OB FLAP NR 1 VANE IB END L/E SKIN IS CHAFED. INSTALLED REPAIR DOUBLER. (K)

Part: SKIN — CHAFED (RT LE FLAP)

HV - CHECK - RT IB FLAP L/E PANEL IS CHAFED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (K)

Part: SKIN — DENTED (RT IB FLAP)

HV - CHECK - RT IB FLAP BOTTOM SKIN DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (K)

Part: SEAT TRACK — GOUGED (FUSELAGE)

OKC - DURING HV CHECK, SEAT TRACK GOUGED AT LUGS. REMOVED DAMAGED SECTION. INSTALLED REPAIR SECTION. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING HV CHECK, FALSE SEAT TRACK CORRODED. REPLACED TRACK. (M)

Part: INTERCOSTAL — CRACKED (FLOORBEAM)

HV - CHECK - FLOORBEAM INTERCOSTAL IS CRACKED. REPLACED INTERCOSTAL. (K)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING HV-CHECK, FOUND SEAT TRACK CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR PLUG. (M)

Part: VANE — DAMAGED (TE FLAP)

HV - CHECK - FRAME HAS RIVET SET MARKS. REMOVED DAMAGED SECTION. INSTALED REPAIR FILLER, ANGLE, AND PLATE. (K)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

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

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - HV-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

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

Part: SKIN — DENTED (CARGO DOOR)

OKC - HV-CHECK, MID CARGO BAY DOOR IS DENTED. INSTALLED REPAIR DOUBLER. (M)

Part: SKIN — DENTED (MID CARGO DOOR)

OKC - FOUND HV CHECK, MID CARGO BAY DOOR IS DENTED. INSTALLED REPAIR DOUBLER. (M)

Part: SKIN — DENTED (CARGO DOOR)

OKC - HV-CHECK, AFT CARGO BAY DOOR IS DENTED. COLD-WORKED TO ORIGINAL CONTOUR, INSTALLED REPAIR DOUBLER. (M)

Part: SKIN — BENT (FUSELAGE)

HV-CHECK, FORWARD CARGO BAY DOOR CUTOUT IS GOUGED FORWARD OF UPPER DOOR STOP. REMOVED DAMAGE, AND INSTALLED REPAIR DOUBLER. (M)

Part: SKIN — DENTED (CARGO DOOR)

HV-CHECK, MID CARGO BAY DOOR IS DENTED. INSTALLED REPAIR DOUBLER. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - HV-CHK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 42,410 hrs · 21,355 cycles

OKC HV-CHECK - CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)

Part: SKIN — DENTED (CARGO DOOR)

OKC - HV-CHECK, AFT CARGO BAY DOOR IS DENTED. INSTALLED REPAIR DOUBLER. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

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

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - HV-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M)

Part: SKIN — BENT (CARGO DOOR)

HV-CHECK, FORWARD CARGO BAY DOOR IS BENT AROUND DOOR HANDLE. REMOVED DAMAGED SECTION. INSTALLED REPAIR SCUFF PLATE. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - HV-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

HV-CHECK, CABIN FLOOR PANEL HAS CORRODED FASTENERS. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (CABIN)

OKC HV - CHECK - CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)

Part: SKIN — DENTED (CARGO DOOR)

OKC - HV-CHECK, MID CARGO BAY DOOR IS DENTED. INSTALLED REPAIR DOUBLER. (M)

Part: SKIN — DENTED (AFT CARGO DOOR)

OKC - HV-CHECK, AFT CARGO BAY DOOR IS DENTED. INSTALLED REPAIR DOUBLER. (M)

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 42,410 hrs · 21,355 cycles

OKC HV-CHECK - CABIN FLOOR PANEL IS FEREL DAMAGED. REPLACED FLOOR PANEL. (K)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - HV-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 42,410 hrs · 21,355 cycles

OKC HV-CHECK - CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (NM02200500849) (K)

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 42,410 hrs · 21,355 cycles

OKC HV-CHECK - CABIN FLOOR PANEL HAS CORRODED AND CRACKED FASTENERS. REPLACED FLOOR PANEL. (NM02200500849) (K)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 42,410 hrs · 21,355 cycles

OKC HV- CHECK - CABIN FLOOR PANEL IS WATER DAMAGED AND HAS CORRODED FASTENERS. REPLACED FLOOR PANEL. (NM02200500849) (K)

Part: CHANNEL — DENTED (FLOOR PANEL) · airframe 42,410 hrs · 21,355 cycles

OKC HV-CHECK - CABIN FLOOR PANEL HAT CHANNEL DENTED. REPLACED CHANNEL. (K)

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 42,410 hrs · 21,355 cycles

OKC HV- CHECK FLOOR PANEL HAS CORRODED FASTENERS. REPLACED FLOOR PANEL. (NM02200500849) (K)

Part: CHANNEL — DEBONDED (FLOOR PANEL) · airframe 42,410 hrs · 21,355 cycles

OKC HV - CHECK - CABIN FLOOR PANEL HAT CHANNEL DISBONDED. BOND REPAIRED. (K)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 42,410 hrs · 21,355 cycles

OKC HV-CHECK - CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (NM02200500849) (K)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 42,410 hrs · 21,355 cycles

OKC HV - CHECK - CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (NM02200500849) (K)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - HV-CHECK, FOUND CABIN FLOOR PANEL IS WATER DAMAGED AND HAS CORRODED FASTENERS. REPLACED FLOOR PANEL. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

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

Part: LANYARD — BROKEN (L1 DOOR SLIDE)

OKC - HV-CHECK, FORWARD PAX (L-1) DOOR EMERGENCY EXIT SLIDE FAILED TO DEPLOY DURING TEST PER TASKCARD 28425002 STEP 2. THE CAUSE WAS DETERMINED TO BE A BROKEN GIRT BAR-TO-SLIDE COVER LATCH LANYARD. IT WAS BROKEN AT THE LATCH END. THE ENTIRE EMERGENCY SLIDE ASSEMBLY, INCLUDING THE DEFECTIVE LANYARD, WAS SHIPPED TO ASA ENGINEERING FOR REVIEW. A REPLACEMENT ASSEMBLY WAS INSTALLED ON AIRCRAFT. (M)

Part: MODULE — DISCONNECTED (EMERGENCY LIGHT)

PDX - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 32. RECONNECTED LOOSE MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: FRAME — GOUGED (FUSELAGE)

DURING C-CHECK, FOUND LEFT VENTRAL AFT ACCESSORY COMPARTMENT FRAME IS GOUGED AND CHAFED. REPAIRED DAMAGED AREAS PER EA 5310-02342. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND PASSENGER CABIN FLOOR PANEL IS CRACKED AT FS 200-256. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: VANE — DAMAGED (TE FLAP)

FOUND DURING C-CHECK, LEFT OUTBOARD FLAP INBOARD VANE ACCESS PANEL IS CREASED. REPLACED FLAP VANE PANEL PER SRM 51-10-4 AND 51-30-1. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS CORRODED INSERTS AT FS 200-256. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: PANEL — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND AFT WING FILLET PANEL 2208C BETWEEN ATTACH RUB STRIP AND FUSELAGE SKIN IS CORRODED. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-04. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS SEVERAL CRACKED AND MISSING INSERTS. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS CORRODED INSERTS AND HOLES NEAR FORWARD ENTRY AT FS 160-200. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: WEB — GOUGED (ACCESSORY BAY)

FOUND C-CHECK, LEFT VENTRAL AFT ACCESSORY COMPARTMENT FRAME, WEB, GOUGED AT FS 1380. REPLACED WEB PER SRM 51-70-4. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS BROKEN AND CORRODED INSERTS AT FS 160-120. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS DISBONDED AT FS 160-200. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS SEVERAL CRACKED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

OKC - DURING C-CHECK, FOUND PASSENGER CABIN FLOOR PANEL HAS BROKEN AND CORRODED INSERTS AT FS 160-120. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — CRUSHED (FUSELAGE)

OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL IS CRUSHED IN SEVERAL LOCATIONS AT FS 140-160. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS DISBONDED AND HAS CRACKED EDGE AT FS 160-180. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS CORRODED INSERTS AND COMPOSIT DAMAGE AT CORNER AT FS 160-200. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: LANYARD — MISRIGGED (ESCAPE SLIDE)

OKC C-CHECK, AFT SERVICE DOOR EMERGENCY SLIDE FAILED TO DEPLOY DURING DEPLOYMENT TEST. SUSPECT MIS-RIGGED LANYARD, BUT INVESTIGATION IS UNDERWAY TO MORE DEFINITIVELY DETERMINE CAUSE. MFG (ENG-G DOC 3053)- MIS-RIGGING APPEARS TO HAVE BEEN IMPROPER FOLDING OF THE HOSE ASSY CONNECTING THE ASPIRATOR TO THE INFLATION RESERVOIR. BUT, ACCORDING TO MFG, THIS KINKING OF THE HOSE WOULD NOT HAVE CAUSED THE FAILURE. ALTHOUGH NO FOREIGN MATERIAL WAS FOUND LODGED INSIDE THE ASPIRATOR, TEMPORARY INGESTION OF BUBBLE WRAP BY THE ASPIRATOR IS CONSIDERED THE MOST PROBABLE CAUSE OF FAILURE. THERE WAS SUBSTANTIAL AMOUNT OF THIS MATERIAL TAPED TO THE FUSELAGE NEAR THE ASPIRATOR. ENTIRE SLIDE WAS REPLACED.

Part: LIGHT — INOPERATIVE (COCKPIT)

SEA - DURING PREFLIGHT CHECK, FOUND COCKPIT OVERHEAD STANDBY EMERGENCY LIGHT FOUND INOPERATIVE. REPLACED LIGHT SOCKET. LIGHT THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

LINE CHECK, FOUND FORWARD PAX L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

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

Part: LIGHT — INOPERATIVE (FWD CABIN)

SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE FORWARD OF ROW 2. REPLACED DAMAGED CONNECTOR SEGMENT. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WIRE — BROKEN (EMERGENCY LIGHT)

SJC - PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING IN FIRST CLASS WAS FOUND INOPERATIVE. REPAIRED BROKEN WIRE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: HEAT EXCHANGER — CLOGGED (A/C PACK)

OAK - HOT INSULATION ODOR AND BLUE HAZE IN CABIN WITH APU ON AND AIR CON PACKS ON. REPLACED BOTH PRIMARY AND SECONDARY (P/N 18406032, S/N 46-5085) HEAT EXCHANGERS, BOTH HAD INGESTED INSULATION BLANKET MATERIAL. OPS CHECK OK. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - FOUND DURING C-CHECK, AFT LOWER FLANGE FRAME CORRODED AT FS 1231. REPLACED DAMAGED SECTION OF FRAME PER SRM 53-03. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING C-CHECK, AFT CARGO BAY TIEDOWN BRACKET IS CORRODED. REPLACED BRACKET PER SRM 51-30-5. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING C-CHECK, AFT CARGO BAY FLOOR TRACK CORRODED AT FASTENER HOLES. REPLACED FLOOR TRACK PER SRM 53-05 AND 51-10-3. (M)

Part: SPACER — CORRODED (FUSELAGE)

OKC - FOUND DURING C-CHECK, AFT CARGO BAY DOOR LOWER BEAM SPACER IS CORRODED. REPLACED EXISTING DOUBLER PER SRM 51-30-5 AND 53-05. (M)

Part: ANGLE — CRACKED (RT MLG WW)

OKC - FOUND DURING C-CHECK, VERTICAL ANGLE IN RIGHT WHEEL WELL IS CRACKED AT FORWARD INBOARD LOWER CORNER. REPLACED ANGLE PER SRM 51-30-5. (M)

Part: SKIN — CRACKED (BARRIER DOOR)

OKC - FOUND C-CHECK, AFT CARGO BAY BARRIER DOOR INTERNAL SKIN IS CRACKED 1.25 INCH. INSTALLED FILLER AND DOUBLER PER SRM 51-70-2. (M)

Part: SKIN — CRACKED (BARRIER DOOR)

OKC - FOUND DURING C-CHECK, FORWARD CARGO BAY BARRIER DOOR SKIN CRACKED. INSTALLED FILLER AND DOUBLER PER SRM 51-70-2. (M)

Part: CLIP — CRACKED (FS 1155)

OKC - FOUND DURING C-CHECK, AFT CARGO BAY BRACKET ANGLE CLIP CRACKED. REPLACED CLIP PER SRM 51-30-1. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING C-CHECK, AFT CARGO BAY TIEDOWN TRACK IS CORRODED AROUND FASTENER HOLES. REPLACED TRACK PER SRM 51-10-4 AND 51-30-1. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING C-CHECK, AFT CARGO BAY LEFT TRACK IS CORRODED AT FS 1079-1222. REPLACED TRACK PER SRM 53-05. (M)

Part: PLATE — CRACKED (CARGO DOOR)

OKC - FOUND DURING C-CHECK, MID CARGO BAY DOOR LOWER SCUFF PLATE IS CRACKED. CUT OUT AND REPLACED DAMAGED AREA PER SRM 53-01. (M)

Part: TORQUE BOX — CORRODED (FUSELAGE)

OKC - FOUND DURING C-CHECK, TORQUE BOX WEB UPPER SURFACE CORRODED AT FS 1212. REPLACED WEB SECTION PER SRM 51-70-4. (M)

Part: FLOORBOARD — PUNCTURED (FUSELAGE)

OKC - FOUND DURING C-CHECK, FORWARD CARGO BAY NR 4 FLOORBOARD PUNCTURED AND CORRODED. REPLACED FLOOR PANEL PER SRM 51-10-4. (M)

Part: HINGE — CRACKED (FUSELAGE)

OKC - FOUND DURING C-CHECK, MID CARGO BAY BARRIER DOOR HINGE IS CRACKED. REPLACED HINGE PER SRM 51-10-3, 51-10-4, AND 51-30-1. (M)

Part: ANGLE — CORRODED (BULKHEAD)

OKC - FOUND DURING C-CHECK, AFT CARGO BAY AFT BULKHEAD PANEL MOUNTING STRAP ATTACH ANGLE CORRODED. REPLACED ANGLE PER SRM 51-10-2 AND 51-30-5. (M)

Part: HINGE — CRACKED (BARRIER DOOR)

OKC - FOUND DURING 30K CHECK, FORWARD CARGO BAY BARRIER DOOR HINGE IS CRACKED. REPLACED HINGE PER SRM 51-30-1. (M)

Part: ACCESS PANEL — CRACKED (FUSELAGE)

OKC - FOUND DURING C-CHECK, ACCESS PANEL BENEATH SEAT IN COCKPIT IS BENT AND TORN. INSTALLED DOUBLER PER SRM 53-01. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

OKC - FOUND DURING C-CHECK, SHEAR TIE CORRODED AT FS 1250. REPLACED SHEAR TIE PER SRM 51-10-2, 51-10-3, AND 53-14-3. (M)

Part: HINGE — CRACKED (CARGO DOOR)

OKC - FOUND DURING C-CHECK, AFT CARGO BAY BARRIER DOOR HINGE CRACKED. REPLACED HINGE PER SRM 51-30-1. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

OKC - FOUND DURING C-CHECK, SHEAR TIE IS CORRODED AT FS 1287. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-01, 53-03, AND 51-10-3. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING C-CHECK, TIE DOWN TRACK CORRODED IN AFT CARGO BAY. REPLACED TRACK PER SRM 51-10-2, 51-10-4, 51-30-1, AND 51-30-5. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

OKC - FOUND DURING C-CHECK, FLOOR PANEL CORRODED IN AFT CARGO BAY. REPLACED PANEL PER SRM 51-10-2 AND 51-10-3. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - FOUND DURING C-CHECK, FRAME CORRODED IN AFT CARGO BAY. REPLACED FRAME SEGMENT PER SRM 51-30-2 AND 51-30-5. (M)

Part: GUSSET — CORRODED (CARGO BAY)

OKC - FOUND DURING C-CHECK, GUSSET CORRODED IN AFT CARGO BAY. REPLACED GUSSET PER SRM 51-10-2 AND 51-10-4. (M)

Part: DOME NUT — CORRODED (FUSELAGE)

OKC - FOUND DURING C-CHECK, PANEL LANDING HAS CORRODED DOME NUTS AT FS 786. REPLACED DOME NUTS PER SRM 51-30-2. (M)

Part: MODULE — DISCONNECTED (CABIN)

YVR - DURING PRE-FLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 26. RECONNECTED LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

PDX - DURING LINE CHECK, FOUND EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACK, POWER SUPPLY. LIGHTS THEN OPERATED PROPERLY. (M)

Part: POWER SUPPLY — DISCHARGED (MID CABIN)

PHX - DURING LINE CHECK EXTERIOR, OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED POWER SUPPLY. EMERGENCY LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — DISCONNECTED (CABIN)

PDX - DURING PREFLIGHT CHECK, 1ST CLASS EMERGENCY FLOOR TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. RECONNECTED LOOSE LIGHT MODULE SOCKET. LIGHTS THEN OPERATED NORMALLY. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

PHX - DURING PREFLIGHT, THE EMERGENCY EXIT LIGHTS IN FIRST CLASS WERE FOUND TO BE INOPERATIVE. REPLACED THE POWER SUPPLY AND THE LIGHTS THEN OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING LINE CHECK, OVERWING EMERGENCY LIGHT WAS DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY ASSEMBLY. LIGHT THEN OPERATED NORMALLY. (M)

Part: SWITCH — INOPERATIVE (CABIN)

SEA - DURING LINE SERVICE CHECK, FLIGHT ATTENDANTS EMERGENCY LIGHTING SWITCH WAS DETERMINED TO BE INOPERATIVE. REPLACE FLIGHT ATTENDANTS EMERGENCY LIGHTING SWITCH. LIGHTS THEN OPERATED NORMALLY. (M)

Part: LIGHT — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK, EMERGENCY TRACK LIGHTS AT CABIN ROW 1 WERE DETERMINED TO BE INOPERATIVE. RECONNECTED LIGHT MODULE. LIGHTS THEN OPERATED NORMALLY. (M)

Part: SOCKET — DEFECTIVE (CABIN)

SFO - DURING LINE CHECK, ONE LEFT OVERWING EMERGENCY LIGHT WAS DETERMINED TO BE INOPERATIVE. REPLACED LIGHT SOCKET ASSEMBLY. LIGHT OPERATED NORMALLY. (M)

Part: POWER SUPPLY — DISCHARGED (AFT CARGO BAY) · airframe 28,912 hrs · 14,799 cycles

PDX-DURNING LINE CHECK, EXTERIOR OVERWING EMERGENCY LIGHTING WAS DETERMINED TO BE INOPERATIVE. REPLACED EXTERIOR EMERGENCY LIGHTING POWER SUPPLY. LIGHTS OPERATED NORMALLY.

Part: WIRE — DISCONNECTED (AFT CABIN)

SEA - PRIOR TO FLT 199, THE EMERGENCY TRACK LIGHTS WERE FOUND INOPERATIVE. INSPECTED AND FOUND WIRING AND LIGHT ASSEMBLIES DISCONNECTED. RECONNECTED WIRING AND LIGHTS, SYSTEM OPERATES NORMAL. (M)

Part: LIGHT — INOPERATIVE (FWD CABIN)

EMERGENCY EXIT TRACK LIGHTS IN THE FIRST CLASS SECTION WOULD NOT ILLUMINATE WITH THE SWITCH ON.REPLACED INOPERATIVE LAMP ASSEMBLY AT ROW 2 AND LIGHTS OPERATED NORMALLY.

Part: POWER SUPPLY — DISCHARGED (MID CABIN)

SEA - DURING MAINTENANCE CHECK, BOTH AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED THE POWER SUPPLY AND THE LIGHTS OPERATED NORMALLY. (M)

Part: MODULE — INOPERATIVE (MID CABIN)

SEA PRIOR TO FLIGHT 394 THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 21-24 WERE FOUND TO BE INOPERATIVE. REPLACED LIGHT MODULE ASSEMBLY AND THE LIGHTS OPERATED NORMALLY.

Part: WIRE — DISCONNECTED (ROW 24) · airframe 28,163 hrs · 14,442 cycles

SEA - DURING MAINTENANCE CHECK, THE MULTIPLE EMERGENCY EXIT TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED AND REPLACED DAMAGED TRACK SECTIONS AND THE LIGHTS OPERATED NORMALLY. (X)

Part: HOOK — BINDING (PAX DOOR) · airframe 28,125 hrs · 14,425 cycles

PHX - FLT 726 - PRIOR TO FLIGHT, THE L1 DOOR HOLD OPEN WAS FOUND BINDING. INSPECTED AND RELEASED AIRCRAFT FOR FERRY FLIGHT TO OAK FOR REPAIR. OAK MAINTENANCE RIGGED THE L1 DOOR HOLD OPEN HOOK AND THE DOOR OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN) · airframe 14,987 hrs · 14,659 cycles

ANC - DURING MAINTENANCE CHECK, SEVERAL EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING/LIGHTS AND ALL LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

ANC - DURING MAINTENANCE CHECK, SEVERAL EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING/LIGHTS AND ALL LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHT AT ROW 17 WAS FOUND INOPERATIVE. RECONNECTED WIRES TO LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, ALL FOUR UPPER OVERWING EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (M)

Part: RELAY — FAILED (MID CABIN)

DURING 30K CHECK THE OVERWING EMERGENCY EXIT LIGHTS ILLUMINATED WHEN GENERATOR BUSSES WERE TRANSFERRED. REPLACED RELAY R2-271 AND LIGHTS OPERATED NORMALLY.

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING 30K CHECK THE AFT CARGO COMPARTMENT STA 1250 AT LONG. 30 BOTH SIDES, SHEAR TIE CLIPS CORRODED. REPAIRED PER SRM 51-30-3.

Part: LONGERON — CORRODED (FUSELAGE)

DURING 30K CHECK AFT CARGO COMPARTMENT STA 1220 LONG. 30 WAS FOUND TO BE CORRODED WHERE THE STUB FRAME CONNECTS TO THE LONGERON. REPAIRED PER SRM 51-30-0.

Part: BATTERY — DISCHARGED (CABIN)

DURING 30K CHECK EMERGENCY EXIT LIGHT BATTERIES AT OVERHEAD BIN AT ROW 26 R/H SIDE AND AT OVERHEAD PANEL BETWEEN FWD LAV AND FWD GALLEY WERE FOUND TO BE DISCHARGED (WOULD NOT ACCEPT CHARGE) REPLACED BATTERIES AT BOTH LOCATIONS AND SYSTEM OPERATED NORMALLY.

Part: SKIN — DENTED (FUSELAGE)

DURING 30K CHECK THE LT SIDE OF THE FUSELAGE SKIN WAS FOUND TO BE DENTED ON THE MAINFRAME STA 120 JUST BELOW LONG 18L. REPAIRED PER SRM 53-04.

Part: CARGO TRACK — CORRODED (CARGO BAY)

PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT, RIGHT AFT CARGO TRACK WAS FOUND TO BE CORRODED AROUND THE FASTENER HOLES AT STATION 1212-1307, STRINGER 16R. REPAIRED PER SRM 51-30-0. (M)

Part: BATTERY — DISCHARGED (MID CABIN)

DURING 30K CHECK THE CABIN OVERHEAD EMERGENCY LIGHTS FROM ROW 13-22 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY.

Part: FRAME — GOUGED (FUSELAGE)

DURING 30K CHECK THE LT FRAME WAS FOUND GOUGED AT STA 1041 JUST ABOVE LONG. 18L. REPAIRED PER SRM 53-14-3.

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, THE FLOOR WEB AT STATION 994, LONGERON 18R WAS FOUND TO BE CORRODED. REPAIRED PER SRM 53-01. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING 30K CHECK THE INTERCOSTAL WAS FOUND TO BE CRACKED AT STA 180, LBL 60. REPAIRED PER SRM 51-30-0.

Part: BATTERY PACK — DISCHARGED (MID CABIN)

DURING 30K CHECK BOTH EMERGENCY OVERWING EVACUATION LIGHTS FAILED TO ILLUMINATE.REPLACED EMERGENCY OVERWING EVACUATION LIGHT BATTERY PACK AND LIGHTS OPERATED NORMALLY.

Part: FRAME — CORRODED (FUSELAGE)

DURING 30K CHECK CORROSION WAS FOUND ON THE AFT SIDE OF THE FRAME AT STA 1250 FROM LONG. 28L TO 28R. REPAIRED PER SRM 53-03.

Part: CARGO TRACK — CORRODED (CARGO BAY)

PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT LEFT CARGO TRACK AT STATION 1220-1309, LONGERON 16L WAS FOUND TO BE EXFOLIATED. REPAIRED PER SRM 51-30-5. (M)

Part: SLIDE — FAILED (PAX DOOR)

PHX - DURING 30K CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE R1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)

Part: SLIDE — FAILED (PAX DOOR)

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 — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB, FS 598 TO 712, LONGERON 18L. REMOVED AND REPLACED WEB IAW DC9 SRM 51-30-01. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON FLOOR WEB, FS 740, LONGERON 18R. REMOVED AND REPLACED WEB FROM FS 710 TO 788 IAW DC9 SRM 51-30-02 AND 51-30-05. (M)

PHX-DURING 30K CHECK CORROSION WAS FOUND ON SUB FLOOR CUSP WEB, FS 1180, LBL 56.REMOVED DAMAGED MATERIAL AND INSTALLED FILLER AND DOUBLER IAW DC9 SRM 53-14-03.

Part: CARGO TRACK — CORRODED (CARGO BAY)

PHX - DURING 30K CHECK, FOUND CORROSION ON CARGO TRACK, FS 1155-1211, LONGERON 29R. REMOVED AND REPLACED CARGO TRACK SECTION IAW DC9 SRM 51-30. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON SUB FLOOR WEB, FS 180-200, LBL 6 TO RBL 6. REMOVED DAMAGED MATERIAL AND INSTALLED REPAIR SECTION IAW DC9 SRM 51-30-02 AND 53-01. (M)

Part: CARGO TRACK — CORRODED (CARGO BAY)

PHX - DURING 30K CHECK, FOUND CORROSION ON CARGO TRACK, FS 1079-1155, RBL 16. REMOVED CORROSION AND FOUND TRACK OUT OF LIMITS FROM FS 1108 TO 1155. REPLACED CARGO TRACK SECTION IAW DC9 SRM 51-30. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PHX-DURING 30K CHECK CORROSION WAS FOUND ON SEAT TRACK, FS 1100-1307, LBL 22.REMOVED CORROSION AND FOUND TRACK OUT OF LIMITS FROM FS1100 TO 1165. REPLACED SEAT TRACK SECTION FROM FS 1040 TO 1165 IAW DC9 SRM 53-05, FIG 4B.

Part: WIRE — FAILED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE TWO EMERGENCY FLOOR TRACK RED LIGHTS FOR THE L2 DOOR EXIT WERE FOUND INOPERATIVE. REPLACED THE WIRING IN THE FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (ROW 1)

SEA - AFTER ARRIVAL OF FLT 483 - CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTING AT ROW 1 WAS DISLODGED FROM TRACK. REPLACED BROKEN WIRES IN FLOOR TRACK ASSEMBLY, REINSTALLED LIGHTING INTO TRACK AND OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (ROW 20/23)

SEA - DURING MAINTENANCE CHECK, ONE EMERGENCY FLOOR TRACK LIGHT AT ROW 20 AND TWO AT ROW 23 WERE FOUND INOPERATIVE. REPLACED LAMP MODULES AND OPERATED NORMALLY. (M)

Part: WIRE — DAMAGED (CABIN)

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

Part: WIRE — DAMAGED (CABIN)

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

Part: MECHANISM — OUT OF ADJUST (L2 DOOR)

SEA - DURING MAINTENANCE CHECK, THE L2 DOOR WOLD NOT LATCH OPEN. ADJUSTED DOOR HOLD OPEN MECHANISM AND OPERATED NORMALLY. (M)

Part: BOTTLE — DISCHARGED (SLIDE)

SEA - PRIOR TO DEPARTURE OF FLT 376, CREW REPORTED THE L1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS LOW. REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE ASSY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 1 TO 6 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - FLT 446 - PRIOR TO DEPARTURE, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FIRST CLASS CABIN WERE INOPERATIVE. REPLACED THE BATTERY PACK AND REPAIRING WIRING IN PART OF SECTION, LIGHTS OPERATED NORMALLY. (M)

Part: RELEASE — LACK OF LUBE (TAILCONE)

SEA - DURING TAILCONE EMERGENCY RELEASE CHECK FROM THE AFT CABIN ENTRY DOOR POSITION, THE TAILCONE FAILED TO RELEASE. LUBRICATED TAILCONE RELEASE MECHANISM AND TAILCONE RELEASED NORMALLY. (M)

Part: EMERG EVAC SLIDE — LOW PRESSURE (INFLATION BOTTLE)

PDX - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE R1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)

Part: LIGHT — DEFECTIVE (CABIN)

LAX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT 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: LIGHT — DEFECTIVE (CABIN)

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

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: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, FORWARD 4 EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED LIGHTS/WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: HOLD OPEN LATCH — OUT OF ADJUST (L1 DOOR)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR HOLD OPEN HOOK WOULD NOT ENGAGE. ADJUSTED HOLD OPEN LATCH AND OPERATED NORMALLY. (M)

Part: PORTABLE EEL — DEFECTIVE (CABIN)

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