
6a) Landing Gear hydro system
Authored by Joey Reichelt
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Professional Development
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11 questions
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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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