Hydraulics Flashcards
Which of the following is not controlled by hydraulics?
Ailerons?
What is the nominal pressure created by the engine-driven hydraulic pumps?
3,000 PSI
What provides backup pressure for the #1 Hydraulic System?
Standby Pump
What is controlled by the #1 Hydraulic System?
BARF PIE
- Brakes
- Anti-Skid
- Rudder,
- Flaps
- PTU,
- Inboard roll Spoilers
- Elevators
Which of the following is controlled by the #2 Hydraulic System?
LOSER E
L - landing gear O - outboard spoilers S - steering E - emerg parking brake R - rudder
E - elevators
A minimum quantity of _____% must be present in the #1 and #2 hydraulic systems for aircraft dispatch.
.
40%
A minimum quantity of _____% must be present in the #3 hydraulic system for aircraft dispatch..
45%
True or False: The #1 Hydraulic System can be powered by AC ground power with the engines off.
True
Normal hydraulic pressure from the engine driven hydraulic pump is approximately what PSI?
3,000 PSI
What does the Power Transfer Unit (PTU) do?
Uses #1 System pressure to power System #2
True or False: Hydraulic system pressures and reservoir quantities are normally displayed in analog format at the bottom of the First Officer’s MFD.
True
What electrical source does the standby hydraulic pump need to operate?.
115 AC Power
True or False: The standby pump automatically activates when the #1 engine fails during flight.
True
True or False: Pilots can manually turn on the standby hydraulic pump.
True
True or False: Both main hydraulic systems contain fuel/oil heat exchangers in the associated fuel tank to help cool the hydraulic fluid.
True