.
CRANK -.The.start.valve.opens provided.the.ENG.MAN.START switch.is ON.and.N2.is.less than.10%. Ignition.is not supplied.
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IGN /.START.-.Provides.continuous.ignition if.the ENG MASTER.switch.is.ON.and.N2 is.at.idle or.greater. During.and automatic start, on.airplanes placarded.:EXTENDED.DRY.CRANK",.expect ignition.and.fuel.flow 50.seconds after.ENG.MASTER.switch.is selected.ON. On.airplanes without the.placard, expect.ignition.and.fuel.flow between.approximately.15% and.20%.N2. During.a manual start the.HP.fuel.valve.is open.and.ignition.is selected.when.the.ENG MASTER.switch.is.selected ON.
FIRE.Light
Illuminates when.the.respective.fire warning.is activated.and.during.engine.fire test.
FAULT.Light
Illuminates amber in the.event.of an.automatic.start.abort, or a.disagreement.between.the.HP.fuel valve.position.of FADEC.channel.A.and.B.
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5.5..Speed.Brake,.Trim.and.Flap.Lever.Panels(.A320.)
Speed Brake
Speed Brake.Lever
Lever.provides.the.following.speed.brake.and ground.spoiler.functions:
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Manually pushing.lever.down.and.aft inflight, selects surface.position.of Speed.Brakes..A."hard.point:.is provided.at.the.1/2.position.
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Speed.Brake.deflection.is.limited.to approximately.1/2 with.an.autopilot engaged, regardless.of.lever.position.
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Pulling.the.lever.up.to.the.RET position arms the.ground.spoilers.to automatically.extend.for.landing or when.executing.a.rejected.takeoff.
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Trim
RUD.Trim.Selector
Controls the.Rudder.Trim.actuator which moves the.neutral point of the articial.feel.at.a rate.of 1 degree.per.second.of rudder.travel. Selector is deactivated.with A/P engaged.
RUD.Trim.Position.Indicator
Displays.Rudder Trim direction.(L.or R).and value.(0°.to.20°).
RUD Trim.RESET.Switch
When pushed, the.FAC.commands the.Rudder Trim.actuator.to.the.zero.trim.position.
Flaps
Flap.Lever
Commands.flaps and.slats for.simultaneous operation.to.selected.position..Lever.must be pulled.out.of detent prior.to.positioning. Detents are.provided.at positions 1.and.3.to avoid.excessive.flap/slat.travel.by.a.single action.
When the.flap.lever.is.in.any.position.other then."0".in.flight,.idle.RPM.is increased (approach.idle) and.continuous ignition.is activated.
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s
Parking.Brake.System
Parking.Brake.Handle
Sets the.Parking.Brake.by pulling.the.handle and.then.turning.it.clockwise. Activation.of the Parking.Brake.deactivates all other braking modes. "PARK.BRK".is displayed.on.the ECAM.memo page.
Landing.Gear.Gravity.Extension.System
Gravity.Gear.EXTN.Handle Provides Landing.Gear.extension.in.the.event of electrical, hydraulic or.mechanical.failure. The.handle.must be.extended.and.then.rotated clockwise.three.turns.to.shut off hydraulic pressure, open.the.doors.and.unlock the.gear.
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本文链接地址：Flight Deck Documentation AIRBUS A320 空客A320驾驶舱文件(33)
