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OIL.Pressure.Indication
Represented.by.pointer.and.digital.display..The digital.indication.pulses if oil pressure.exceeds 390.psi (increasing).or.385.(decreasing)..Both indications become.amber.below 80.psi and red.below 60.psi.
OIL.Temperature.Indication
Displays.Oil.Temperature.in.°C..The.indication pulses above.156°C.(increasing).or.150°C (decreasing). It.becomes amber.if the temperature.exceeds.156°C.for.more than.15 minutes or.instantaneously.when.above 165°C.
IGN Indication
Displays.during.start sequence. The.selected Ignitors."A".or "B".or "AB".are.displayed.when supplied.
Start.Valve.Indication

Displays.positive.of start.valve..A horizontal line through.the.circle.signifies the.valve.is.fully open. A.vertical.line.signifies the.valve.is.fully closed.
Engine Bleed.Pressure

Displays.Bleed.Pressure.upstream.from.the precooler..The.value.becomes amber.below 21 psi when.N2 exceeds.10%.with.the.engine.start valve.not.closed.or.when.Bleed.over-pressure is detected.

VIB.Indications
Displays.N1 and.N2 Vibration.levels. The indication.pulses above.5.0..The.data.is also displayed.on.the.ECAM cruise.page.
OIL.Filter.Indication
Displays.Filter.status..An.amber.CLOG massage.appears in.case.of excessive pressure.loss.across the.main.oil.scavenge.
F.Filter.Indication
Displays.fuel.Filter.status. An.amber CLOG massage.appears in.case.of excessive pressure.loss.across the.fuel.filter.
Permanent.Data
TAT,.SAT.& GW
Message.Area.

-.54-
.
LDG.Gear.Lights
Display.proximity detector.information.received from.LGCIU.1..The.LDG.GEAR.indicator.panel does not illuminate.when.LGCIU.1.is not electrically.powered.
.  
UNLK.-Illuminate.red.if the.gear.is not locked.in.the selected.position.

.  
Lights -Illuminate.geen.if.the.gear.is locked.down.

 

AUTO/BRK.Switches
Arm the required.deceleration.rate..The.ON light.illuminates blue.to.indicate.positive arming..The.DECEL light.illuminates green when.actual airplane.deceleration.corresponds to.80%.of.the.selected.rate.
.  
LO -.Selected.for landing. If.the deceleration.rate.from reverse.thrust.is not adequate, progressive pressure.is applied.to the.brakes.four.seconds after.ground.spoiler.deployment.to provide.a.fixed.deceleration.rate.

.  
MED.-.Selected.for landing. If.the deceleration.rate.from reverse.thrust.is not adequate, progressive pressure.is applied.to the.brakes two.seconds after.ground.spoiler.deployment.to provide.a.fixed.deceleration.rate.

.  
MAX -Selected.for takeoff..During.an aborted.takeoff,.maximum.brake pressure.is applied.when.ground spoilier.deployment occurs.

 

A/SKID.&.N/W.STRG.Switch
.  ON

.  
If green.hydraulic pressure.is available:

.  
　
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本文鏈接地址：Flight Deck Documentation AIRBUS A320 空客A320駕駛艙文件(27)