Hydraulics Flashcards

1
Q

Normal operating pressure?

A

3,000 psi

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2
Q

Where are system 1 & 2 serviced?

A

Aft equipment bay

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3
Q

How many pumps does each system have?

A

2:
Main pump A (EDP - 1A/2A)
Backup pump B (ACMP - 1B/2B 3A/3B)

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4
Q

How many hydraulic systems?

A

3

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5
Q

Which of the 3 is the largest?

A

3

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6
Q

Which of the 3 is the smallest?

A

1

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7
Q

System 1 powers:

A

(Refer to picture)

RUDDER
ELEVATOR
L AIL
OB SPLRON
OB FLT SPLRS
OB GND SPLRS
L REVERSER
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8
Q

System 2 powers:

A

Refer to picture)

RUDDER
ELEVATOR
AIL R
IB SPLRON
IB FLT SPLRS
IB GND SPLRS
LG ALT EXT
OUTBD BRAKES
REVERSER R
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9
Q

1A/2A are running when:

A

The associated engine is running

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10
Q

Do 1B/2B auto start after engine/EDP failure?

A

No

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11
Q

System 1 & 2 cooling cooled by:

A

Cooled by common air/oil heat exchanger in aft equipment bay (air from ram air scoop moves across heat exchanger)

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12
Q

What 2 switchlights close the Hydraulic Shutoff Valve?

A

HYD SOV

ENG FIRE PUSH

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13
Q

How are 3A/3B actuated?

A

Electrically

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14
Q

How often does 3A normally run?

A

Continuously

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15
Q

System 3 is serviced where?

A

Ground service panel, right side of fuselage, aft of wing root

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16
Q

When does 3B normally run?

A

During periods of high-flow requirement

17
Q

Which pump is automatically powered during AC power failure?

A

3B

18
Q

What do the hydraulic systems power?

A
  • rudder
  • elevators
  • ailerons
  • multifunction spoilers
  • ground spoilers
  • thrust reversers
  • wheel brakes
  • nosewheel steering
  • landing gear
19
Q

What kind of hydraulic fluid?

A

Skydrol

20
Q

Main pumps (A) meet needs of:

A

Normal flight controls

21
Q

Auto Mode causes 1B/2B to operate when:

A
  • their respective bus is powered
  • any generator operating
  • flaps not at 0
22
Q

During Manual Mode, 1B/2B operate when:

A
  • their respective bus is powered

- any generator is operating

23
Q

Where is hydraulic info displayed?

A

Hydraulic Synoptic Page

24
Q

How many reservoirs/accumulators?

A

1 per system

25
Q

System 3 powers:

A
Rudder & Elevator
L & R Ailerons
IB GND SPLRS
LDG GEAR
NW STEERING
INBD BRAKES
26
Q

Does system 3 use a heat exchanger?

A

No

27
Q

Does 3B auto start after 3A failure?

A

No

28
Q

3B Auto Mode: Activated when:

A
  • Associated bus is powered

- Flaps not at 0

29
Q

Are there any flight deck controls for EDP1/2?

A

No

30
Q

Reservoir quantity?

A

45-85%

31
Q

Low pressure?

A

<1800 psi

32
Q

High pressure?

A

3200 psi

33
Q

Pressure relief occurs at:

A

3750 psi

34
Q

High temp?

A

> = 96 C

35
Q

How many accumulators?

A

5 (1 for each system, 1 for each brake system)

36
Q

What color is the hydraulic fluid?

A

Purple

37
Q

How many systems actuate the elevator, rudder, & ailerons?

A

All 3

38
Q

Stab trim rates & priority:

A
CA: .5 deg/sec
FO: .5 deg/sec
AP: .5 deg/sec (flaps in motion)
       .1 deg/sec (flaps stationary)
Mach trim: .03-.06 deg/sec
39
Q

System 3 powers:

A

(Refer to picture)

RUDDER
ELEVATOR
L AIL R
IB GND SPLRS
LDG GEAR
N/W STEER