Landing Gear Systems Test

An Anti-skid system is deactivated at a ground speed of

15-20 MPH

Which statement is true with respect to an aircraft equipped with hydraulically operated multi-disk brake assemblies?

Do not set the parking brakes when the brakes are hot

What should be checked when a strut bottoms out during landing

Fluid level

A blue discoloration of bearing rollers is an indication of

Overheating

What is the function of the internal cam assembly in a nose gear shock strut?

Straightens the nose wheel[s] for retraction

When an Air/ oil type of landing gear shock strut is used, the initial shock of landing is cushioned by

The fluid being forced through a metered opening

To Prevent a very rapid extension of an oleo strut after initial compression resulting from landing impact

Various Types of valves

Spongy brakes are caused by

air in the brake system

A high speed aircraft tire with a sound cord body and bead may be recapped

an indefinite number of times

Aircraft tire pressure should be checked

at least once a week or more often

The_____gives the tire the needed strength to assure a firm mounting on the wheel

bead

If the antiskid system malfunctions,the pilot can

dissable it without affecting normal braking

12. The purpose of a sequence valve in a hydraulic retractable landing gear is to

ensure operation of the landing gear and gear doors in the proper order

Aside from an external leak in the line,what will cause parking brakes to creep continuosly to the OFF position?

internal leak in the master cylinder or parking brake valve

After performing maintenance on an aircraft landing gear which may have afffected the system operation,it is usually necesary to

make an operational check with the aircraft on jacks

The fusible plugs installed in some aircraft wheels will

melt a a specified elevated temperature

Excesive wear in the center of the tread of an aircraft tire is an indication of

overinflation

The brake control valve in a Power Brake System is more of a

regulator valve

most aircraft,the oil level of a shock strut is checked by

releasing the air charge and seeing that the oil is to the level of the filler plug

The metering pins in oleo shock struts serve to

retard the flow of oil as the strut is compressed

The valve that isolates the emergency brake system from the normal power brake control system is a

shuttle valve

If a shock strut bottoms out after it has been properly serviced,the

strut should be disassembled and inspected for the cause of the problem

If a shock strut bottoms out after it has been properly serviced, the

strut should be disassembled and inspected for the cause of the problem

If system "A" of a dual power brake actuating system fails, system "B"

take over and provide pressure for braking

The pressure source for power brakes is

the main hydraulic system

Excesive wear in the shoulder area of an aircraft tire is an indication of

underinflation

Aircraft brakes rquiring a large volume of fluid to operate the brakes generally

use power control valves

Why is it necessary that tires on split rim wheels be deflated before removing the wheel from the axle?

As a safety precaution in case the bolts that hold the wheel halves together are weakened or damaged

In brake service work, the term "bleeding " is the process of

B. withdrawing fluid from the system for the purpose of removing air that has

The main advantages of a carbon brake are

Better heat absorbing qualities and lighter weight

When bleeding aircraft brakes,one of the indications that the air has been purged from the system is

firm brake pedals

Lock out deboosters act as

hydraulic fuses

The initial inflation of a newly assembled tire is done

in a special safety cage