767

• Landing lights are located at the left and right inner wings: leading edge and nose gear
• Slide raft pressure viewer for each passenger door escape slide is located:

  • in the lower portion of the door itself
• If pax oxygen is deployed-


  Fastne seat belt and return to seat signs illuminate regardless of the selector position
• Pressure in the crew oxygen system is indicated on the -

  EICAS status display
• Passenger oxygen system is activated if the cabin altitude exceeds -

  14000ft
• The slide raft pressure viewer for each pax door escape slide is located -

  In the lower portion of the door itself
• An illuminated INOP light in the pack reset switch indicates -

  The pack is overheated or there is a fault in the auto controller
• The purpose of the recirculation fans is to-

  Save fuel
• In the supply bleed system as thrust increases -


  The HP valve closes and the LP valve opens
• Air for engine cowling anti ice system is taken from the -

  Dedicated LP stage for engine anti ice
• An android switch automatically closes the outflow valve -


  When the cabin altitude exceeds 11000ft
• The forward facing window is heated -

  Electricly for anto ice plus air con for anti fogging
• Wing anti ice&


  Provides engine bleed air to three outboard slats
• Aircraft probes are heated -


  When an engine is running
• Control of the auto throttle is by the -

  AFDS mode control panel and thrust mode select panel
• When the aircraft is on the ground, switching on the flight director will cause it to engage in the following modes-

  TO (pitch) TO (ROLL) MODES
• Go around mode is automatically armed when-

  Glodeslope is captured or flaps are extended
• A land 2 indication on the autopilot stayis annunciator may be displayed when

  Three autopilots are engaged
• The alert function of the cabin interphone system calls


  All other interior stations
• The recordings on the cockpit voice recorder system come from

  Cockpit area conversation and audio control panel transmission
• The service interphone switch on the accessory panel when selected off

  De activates all microphones at external jacks except the jack marked FLIGHT at the apu control panel
• After DRIVE disconnection an IDG can be reconnected

  Only on ground by maintenance
• An illuminated AC BUS OFF light indicates the

  AC BUS is not powered
• On an approach below 200ft with three autopilot armed for landing a generator fail (APU NOT RUNNING) the centre autopilot


  Remains powered by the standby battery system
• When the hydraulic driven generator is signalled to run


  The main battery DISCH light and the APU BAT DISCH light may illuminate
• The ground handling bus

  Can be powered by the external power on the ground
• An illuminated AC bus off light indicates the

  AC bus is not powered
• An illuminated white APU run light indicates the apu


  May be used to supply electrical power and bleed air
• If the APU selector is selected to off, it shuts down the APu 


  If the APU bleed valve is closed and the cooling cycle is complete
• What is required for starting the APU

  Two batteries
• The primary engine parameters displayed on the eicas upper CRT ARE

  N1 and EGT
• A red EGT after limit on the EGT DISPLAY

  doors during the engine start until the engine start cycle is fully completed
• Reverse thrust cannot be selected unless

  The thrust levers are in the idle position
• A discharged engine fire extinguisher bottle is indicated by


  Engine fire bottle discharge light, and EICAS advisory message ENG BTL 1 OR 2
• Pulling the engine fire switch causes on the selected engine

  The bleed air valve to close and the fire bell to silence
• An APU fire signal will cause

  On the ground a horn in the nose gear strut to sound
• If more than one flight control shut off light is illuminated the EICAS advisory message changes to

  FLT CONT VALS
• When using the alternate flap selector, with the flap 20 selected the leading edge slats are

  In the mid range position
• Automatic stabilizer trim rate is

  Hall the electric or manual trim rate
• With a single autopilot engaged using the electric trim switches on the control wheel will


  Cause the autopilot to disengage