Search Header Logo

6a) Landing Gear hydro system

Authored by Joey Reichelt

Other

Professional Development

Used 28+ times

6a) Landing Gear hydro system
AI

AI Actions

Add similar questions

Adjust reading levels

Convert to real-world scenario

Translate activity

More...

    Content View

    Student View

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

Access all questions and much more by creating a free account

Create resources

Host any resource

Get auto-graded reports

Google

Continue with Google

Email

Continue with Email

Classlink

Continue with Classlink

Clever

Continue with Clever

or continue with

Microsoft

Microsoft

Apple

Apple

Others

Others

Already have an account?