Citation Mustang – Landing gear and Brakes - SmartCockpit - Airline training guides, Aviation, Operations, Safety

With the NO TIRE SPINDOWN amber CAS message displayed in the CAS window:

The flight crew shall not deploy the speedbrakes.

The flight crew shall not select flaps beyond approach.

Airspeed should be reduced to 150 KIAS.

Damage to the wheel well from loose tread. and debris could result.

Correct! Wrong!

When using the emergency brakes, the pilot shall not:

Pump the emergency brake handle and use the parking brake.

Use the speedbrakes.

Use the parking brake.

Pump the emergency brake handle.

Correct! Wrong!

The gear cannot be retracted when the airspeed is above _____

175 KIAS.

185 KIAS.

180 KIAS.

170 KIAS.

Correct! Wrong!

At extension, if the nose gear does not lock in the down position, the gear panel indications are:

All four lights extinguished.

Red light illuminated, green LH and RH lights illuminated.

Red light extinguished, green LH and RH lights illuminated.

Red light illuminated and all three green lights extinguished.

Correct! Wrong!

The ANTISKID FAIL CAS amber message displays when:

Loss of the power brakes.

Loss of the speedbrakes.

Loss of touchdown protection.

Loss of the emergency brakes.

Correct! Wrong!

What landing gear systems are affected if a WOW message appears prior to touchdown?

The power brakes may be inoperative.

The antiskid system may not operate normally.

The parking brake may be inoperative.

The emergency brake system may be inoperative.

Correct! Wrong!

On the ground, the LANDING GEAR handle is prevented from movement to the GEAR UP position by:

Hydraulic pressure.

Mechanical detents.

A manually applied handle locking device.

A spring-loaded locking solenoid.

Correct! Wrong!

Normally, the landing gear is hydraulically actuated, but if the normal gear actuation system fails, the gear can be mechanically and electrically released and extended.

False.

True.

Correct! Wrong!

The gear can be mechanically and pneumatically (not electrically) released and extended.

Each main gear wheel incorporates three fusible plugs that:

Blow out if the tire is overserviced with air.

Is thrown out by centrifugal force if maximum wheel speed is exceeded.

Are DC powered.

Melt, deflating the tire if an overheated brake event occurs.

Correct! Wrong!

Each inboard-retracting main gear uses two hydraulic actuators (one for uplock release and one for gear actuation). Three more hydraulic actuators perform these duties for the forward-retracting nose gear.

True.

False.

Correct! Wrong!

Landing gear downlocks are disengaged:

When hydraulic pressure is applied to the retract side of the main gear actuators and the nose gear downlock release actuator.

By mechanical linkage as the gear begins to retract.

By action of the gear squat switches.

By removing the external downlock pins.

Correct! Wrong!

Before movement of the aircraft on the ground:

Speedbrakes should be extended.

Flaps should be extended to TO.

Disengage the rudder (gust) lock.

Emergency exit should be removed.

Correct! Wrong!

At airspeeds up to 250 KIAS, the gear can be extended (VLO). The aircraft can be flown with the gear extended at airspeeds up to _____

210 KIAS (VLE).

250 KIAS (VLE).

230 KIAS (VLE).

255 KIAS (VLE).

Correct! Wrong!

It takes _____ to extend the landing gear.

Ten seconds.

Six seconds.

Fiveteen seconds.

Nine seconds.

Correct! Wrong!

When using the emergency brake:

Nosewheel steering is inoperative.

The handle should be pumped.

Differential braking is not available.

Antiskid protection is provided.

Correct! Wrong!

The landing gear uplocks are:

Mechanically held engaged by springs.

Pneumatically engaged.

Hydraulically disengaged.

Mechanically held engaged by springs and hydraulically disengaged.

Correct! Wrong!

Citation Mustang – Landing gear and Brakes