Hydraulics

Question 1

Each hydraulic system has a fluid reservoir located in the _______.

Answer 1

main wheel well area

Question 2

_______ pressurizes the System A and B reservoirs.

Answer 2

regulated (engine) bleed air

Question 3

_______ pressurizes the Standby System reservoir.

Answer 3

System B Reservoir pressure

Question 4

The letters RF (white) appear anytime Hydraulic System quantity is _______.

Answer 4

below 76 percent and the aircraft is on the ground.

Question 5

The ELEC 2 pump ON/OFF switch controls the ______ Electric Motor-Driven Pump.

Answer 5

Hydraulic System A

Question 6

Positioning either (number 1 or 2) Engine driven hydraulic pump switch to OFF ______ the Blocking Valve. System pressure is maintained by the Electric Motor Pump.

Answer 6

closes

Question 7

Normal pressure for Hydraulic System A and B is ______ psi and the maximum system pressure is ______ psi.

Answer 7

3000+-200/3500

Question 8

The OVERHEAT (amber) light on the Hydraulic Panel indicates ______.

Answer 8

an Electric Motor-Driven pump has overheated

Question 9

The Power Transfer Unit (PTU) provides normal rates of operation for the ______ if the System B Engine-Driven Pump output drops below a specific value.

Answer 9

Autoslats and Leading Edge Devices (LED)

Question 10

Losing Hydraulic System A or B automatically initiates Standby Hydraulic System operation if _______.

Answer 10

all of the above

Question 11

_______ automatically initiates Standby Hydraulic System operation.

Answer 11

main rudder PCU Force Flight Monitor (FFM) activation

Question 12

Positioning _____ allows the Standby System to power the rudder and thrust reversers.

Answer 12

either FLT CONTROL to STBY RUD

Question 13

The STANDBY HYD LOW QUANTITY (amber) light indicates ________.

Answer 13

the quantity is approximately half empty.