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ALL.Key
When pushed.and.held, all system pages are displayed.in.succession.at one-second intervals..If.the.ECAM.control.panel.fails,.push and.hold.the.ALL.Key until the desired.system page.appears and.then.release.the.key to maintain.the.display. If only.one.ECAM screen.is available, repeatedly.pressing.the.ALL.Key will.cycle.to the.desired.page.

12.11.06  -.66-
5.3..a320.Throttle.Controls

 

 

,.using.inputsfrom.the.FMGC,.controls.thrust based.on.airplane.speed, altitude.and configuration..The.throttles do.not.move when the.Autothrottle.System.is in use. The.system is armed.in.flight by pushing.the.A/THR.switch on.the.FCU.when.the.throttles are.not in the engagement range.
Transmit signals to.the.FADEC,.which computes and.displays.the.thrust rating.limit and.EPR..The.throttle.can.only.be.moved manually..There.are.five lever positions define by.stops or.detents:
Reverse.Idle,
Forward.Idle,
Climb.(CL),
Continuous Thrust.(FLX/MCT)
and.TakeOff./.Go.Around.(TO/GA)

Autothrottle.Disconnect.Switches.(.Red Buttons.)
When pressed, disconnects the.autothrottle system.
Select.Reverse.Thrust.by.overriding.the.stop .
fitted.at.the FWD.IDLE.position..The.stop.is reset.when.the.throttle.is selected.back.to forward.thrust.
Pitch Trim.Wheels
Provides.mechanical control of horizontal stabilizer trim..Trim.wheels have.priority over electrical control..Use.of trim.wheels does not disconnect the.ELACs,.as the.override mechanism ensures.that the.computers.remain synchronized.with.the.manually selected position.
Trim wheels must be.utilized.when.pitch.direct law.is.in.effect.
Pitch.trim.is automatically.reset.to.0.following touchdown.as the.pitch.attitude.becomes less than.2.5°.
Trim.Position.Scales
Indicate trim.position.in.degrees..Normal.range
is.marked.by.a green.band.
CG Scales
Indicate relation.between.CG.location.and pitch.trim setting.prior.takeoff

-.67-
.
ENG.MASTER.Switches.1.&.2

.  
ON.-LP.fuel.valve.opens, provided.the.ENG.FIRE switch.is.in. During.and automatic start,.the.HP.fuel valve opens, provided.the.ENG.MODE selector.is at IGN/START. During.a manual start,.the.HP.fuel.valve opens, provided.the.ENG.MODE.selector is at IGN/START.and the.ENG.MAN.START.switch.is.ON.

.  
OFF.-Closes the.HP.and.LP.fuel valves. Resets.both.channels of.the.FADEC.

ENG.Mode.Selector

.  
NORM.-Continuous ignition.A.+.B.is selected.when.the.engine.is running and.one.of the following.is.met:

.  
FLEX.or TO/GA.thrust.is selected.on.the.ground

.  
TO/GA.thrust.is.selected.inflight

.  
ENG.ANTI.ICE.switch.is.ON

.  
Engine.surge.or.stall.occurs.in.flight

.  
FLAPS.lever position.is other.then."0".in.flight

 
　
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本文鏈接地址：Flight Deck Documentation AIRBUS A320 空客A320駕駛艙文件(32)