hydaulics Flashcards

1
Q

Engine driven hyd pumps are mounted on what

A

prop reduction gear box

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2
Q

How many psi do the engine driven pumps deliver

A

3000 psi

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3
Q

Describe hyd pumps

A

1 left engine driven w/ standby electric
2 right engine driven w/ PTU
3 DC motor pump
4 alt landing gear (fo driven)

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4
Q

1 Hydraulic System hydraulic pressure for:

A
Flaps (priority)
Anti Skid / Main Brakes (isolation)
Inboard Roll Spoilers (isolation)
Rudder (lower PCU)
Elevator (outboard PCUs)
Power Transfer Unit (priority)
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5
Q

1 hyd reservoir capacity and min quantity

A

8 quart, min 40%

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6
Q

1 standby hyd pump powered by what

A

AC driven

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7
Q

AC driven standby hyd pump auto activates when

A
left engine fail in flight or
flaps greater than 0 and parking brake is off and
number 1 reservoir is not empty and
AC power is available 
(takeoff and landing)
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8
Q

When will the stby hyd press light come on?

A

When pressing the button to activate the standby hyd pump (does not come on automatically)

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9
Q

If pressure in hyd 1 drops below 2100 psi

A

Priority valve closes

lose - flaps and PTU

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10
Q

When does the isolation valve close

A

quantity low

lose: anti-skid/main wheel brakes, inboard roll spoilers

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11
Q

What is the thermal bypass valve?

A

opens to allow fluid to heat exchanger at certain temperature

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12
Q

What is the purpose of the PTU

A

power transfer unit serve as a back-up for #2 main hydraulic system

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13
Q

What is the PTU powered by?

A

Hydraulic system 1

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14
Q

How do you activate the PTU?

A

Press the PTU CNTRL switch light or automatically

light turns on for both manual and automatic activation of PTU

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15
Q

Describe #2 hyd system

A

reservoir located in right nacelle, 12 q capacity, min 40%, pressurized by right engine driven pump (EDP)

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16
Q

2 hyd system provides pressure for

A
Landing Gear
Outboard Roll Spoilers
Nose wheel steering
Emergency / Parking Brakes
Rudder (Upper PCU)
Elevator (Center PCU)
17
Q

What do you lose if Hyd system two becomes low?

A
Isolation valve closes
Landing gear
Outboard Roll Spoilers
Nose wheel steering
Emergency/parking brake
18
Q

When is the PTU on?

A

Takeoff and landing, when the button is pushed, when system two fails

19
Q

Automatic PTU operation occurs if

A

parking brake off and
flaps greater than 0 and
no 1 system press greater than 2400 psi and
hyd no 2 reservoir not empty

20
Q

When will the PTU shut down

A

the ptu will shut down and remain latched out if it does not produce pressure for more than 30 seconds when automatically commanded to do so

21
Q

how is the hyd system cooled

A

fuel, thermal bypass valve opens to heat exchanger for 1 and 2 systems

22
Q

Describe hyd system 3

A

back up system for elevator (inboard PCUs), reservoir located in environmental compartment, 2.6 q capacity min quant 40%, during normal flight in “active standby” with the isolation valve energized closed

23
Q

hyd 3 is powered by

A

Dc motor pump at 2600-3250 psi to keep accumulator pumped up

24
Q

What is the DCMP powered by?

A

standby battery (hot batt bus)

25
Q

When will hyd system 3 activate

A

manually by HYD 3 ISOL VLV switchlight, automatically by lose of syst 1 or 2 and/or dual engine failure

26
Q

When will you get #3 HYD PUMP caution light

A

accumulator pressure below 900 psi in flight or

DCMP operates more than 60 seconds on the ground

27
Q

Firewall shutoff valves operate when

A

engine 1 or engine 2 pull fuel/hyd off handles pulled
no 1 or no 2 hyd reservoir fluid quantity is low
hydraulic fluid over temp
POWERED BY ESSENTIAL BATBUS