6a) Landing Gear hydro system

6a) Landing Gear hydro system

Professional Development

11 Qs

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6a) Landing Gear hydro system

6a) Landing Gear hydro system

Assessment

Quiz

Other

Professional Development

Easy

Created by

Joey Reichelt

Used 27+ times

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11 questions

Show all answers

1.

MULTIPLE CHOICE QUESTION

2 mins • 1 pt

What holds the main landing gear in the up and locked position?

Friction washer

Uplock actuator

Continuous hydraulic pressure

Landing gear travel limit switch

2.

MULTIPLE CHOICE QUESTION

2 mins • 1 pt

What slows down the main landing gear to make a gentle contact with the upper bumper stop?

Flow regulator

Pressure reducer

MLG hydraulic motor

Controllable bypass valve

3.

MULTIPLE CHOICE QUESTION

2 mins • 1 pt

The right main landing gear is slow retracting (UP) and exceeds time limitations.  No excessive system pressure loss was observed during operation.  What is the most probable cause of this malfunction?

Selector valve installed in the down line

Flow regulator installed in the down line

Flow regulator installed in the up line

MLG Uplock Brake Assembly

4.

MULTIPLE CHOICE QUESTION

2 mins • 1 pt

After gear UP operation, when the hydraulic system is depressurized, or electrical power removed from the aircraft, what position will the landing gear selector valve be in?

Up

Down

Neutral

Half Trail

5.

MULTIPLE CHOICE QUESTION

2 mins • 1 pt

When the nose landing gear is down and locked a down lock plunger extends from the aft end of the nose landing gear actuating cylinder.  The extended plunger____

actuates a down limit switch to indicate the nose gear is unsafe

de-energizes the main landing gear selector valve

exposes a groove filled with fluorescent paint

none of the above

6.

MULTIPLE CHOICE QUESTION

2 mins • 1 pt

The landing gear selector valve is a ___________ operated valve

Three-way, 2 position, solenoid

Three-way, 2 position, manual

Four-way, 3 position, solenoid

Four-way, 3 position, manual

7.

MULTIPLE CHOICE QUESTION

2 mins • 1 pt

After gear DOWN operation, when the hydraulic system is depressurized, and electrical power removed from the aircraft, what position will the landing gear selector valve be in?

Down

Neutral

Center

Up

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