Hydraulics Flashcards

1
Q

Which of the following is not controlled by hydraulics?

A

Ailerons?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

What is the nominal pressure created by the engine-driven hydraulic pumps?

A

3,000 PSI

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

What provides backup pressure for the #1 Hydraulic System?

A

Standby Pump

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

What is controlled by the #1 Hydraulic System?

BARF PIE

A
  • Brakes
  • Anti-Skid
  • Rudder,
  • Flaps
  • PTU,
  • Inboard roll Spoilers
  • Elevators
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Which of the following is controlled by the #2 Hydraulic System?

LOSER E

A
L - landing gear
O - outboard spoilers
S - steering
E - emerg parking brake
R - rudder

E - elevators

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

A minimum quantity of _____% must be present in the #1 and #2 hydraulic systems for aircraft dispatch.
.

A

40%

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

A minimum quantity of _____% must be present in the #3 hydraulic system for aircraft dispatch..

A

45%

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

True or False: The #1 Hydraulic System can be powered by AC ground power with the engines off.

A

True

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Normal hydraulic pressure from the engine driven hydraulic pump is approximately what PSI?

A

3,000 PSI

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

What does the Power Transfer Unit (PTU) do?

A

Uses #1 System pressure to power System #2

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

True or False: Hydraulic system pressures and reservoir quantities are normally displayed in analog format at the bottom of the First Officer’s MFD.

A

True

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

What electrical source does the standby hydraulic pump need to operate?.

A

115 AC Power

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

True or False: The standby pump automatically activates when the #1 engine fails during flight.

A

True

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

True or False: Pilots can manually turn on the standby hydraulic pump.

A

True

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

True or False: Both main hydraulic systems contain fuel/oil heat exchangers in the associated fuel tank to help cool the hydraulic fluid.

A

True

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

How many volts minimum are needed to run the DC motor pump for the #3 Hydraulic System?

A

24 V

17
Q

When running off of the DC motor pump, what does the #3 hydraulic system get pressurized at?

A

2,600 - 3250 PSI

18
Q

When does the # 3 HYD PUMP caution light illuminate?

A

System pressure falls below 900 PSI &/or DC Motor pump is operating longer than 60 seconds on the ground

19
Q

The Auxiliary Hydraulic System provides power for _____.

A

The emergency landing gear system

20
Q

Nose wheel steering is powered by which hydraulic system?

A

2 Hydraulic system

21
Q

1 Hydraulic

BARF PIE

A
B - brakes
A - anti-skis
R - rudder
F - flaps
P - PTU
I - inboard spoilers
E - elevator
22
Q

2 Hydraulic

LOSER E

A
L - landing gear
O - outboard spoilers
S - steering
E - emerg parking brake
R - rudder

E - elevators

23
Q

3 Hydraulic

A

Elevators

24
Q

Engine Accessory Gearbox

FOD P

A

F - fuel pump
O - oil pump
D - DC starter/generator
P - permanent magnetic alternator (PMA)

25
Q

Prop Reduction Gearbox

HAPP

A

H - hyd pump (main)
A - a/c generator
P - pitch control unit (PCU)
P - prop oil pump/prop overspeed governor

26
Q

A/C Bus

MAST

A

M - most de-ice/anti-ice components
A - aux fuel pumps
S - standby hyd pumps
T - TRUs