Hydraulics Flashcards

1
Q

Minimum dispatch hydraulic fluid quantity levels are:

  • No. 1 system- 3.0 US gallons (11.34 litres); No. 2 system- 1.5 US gallons (5.67 litres).
  • No. 1 system- 3.0 US quarts (2.83 litres); No. 2 system- 1.5 US quarts (1.41 litres).
  • No. 1 system- 1.5 US quarts (1.41 litres); No. 2 system- 3.0 US quarts (2.83 litres).
  • No. 1 system- 1.5 US gallons (5.67 litres); No. 2 system- 3.0 US gallons (11.34 litres).
A
  • No. 1 system- 1.5 US quarts (1.41 litres); No. 2 system- 3.0 US quarts (2.83 litres).
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2
Q

The standby hydraulic pumps:

  • Are gear-type, constant-volume pumps.
  • Provide backup pressure for the No. 1 and No. 2 systems.
  • Operate continuously.
  • Operate only for alternate landing gear extension.
A
  • Provide backup pressure for the No. 1 and No. 2 systems.
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3
Q

The purpose of the PTU is to:
-Retract the gear in the event of a #1 engine failure.
-Retract the gear in the event of a #2 engine failure.
-To power the #2 hydraulic system in the event of fluid loss from the #2
system.
-Transfer hydraulic fluid from #1 hydraulic system to #2 hydraulic system in the event of a fluid loss.

A
  • Retract the gear in the event of a #2 engine failure.
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4
Q

The subsystems actuated by the No. 1 hydraulic system are:
- Landing gear, nosewheel steering, outboard roll spoilers, and upper rudder actuator.
- Flaps, brakes and antiskid, inboard roll spoilers, lower rudder actuator, and the power transfer unit.
- Flaps, landing gear, brakes and antiskid, and ground spoilers.
- Power transfer unit, alternate gear extension, and outboard and inboard
roll spoilers.

A
  • Flaps, brakes and antiskid, inboard roll spoilers, lower rudder actuator, and the power transfer unit.
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5
Q

Illumination of a STBY HYD PUMP HOT caution light indicates:
- Fluid over temperature in the standby system.
- Over temperature of the windings in the electric motor driving the standby
pump.
- The engine driven pump is overheating
- The standby pump is hot.

A
  • Over temperature of the windings in the electric motor driving the standby
    pump.
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6
Q

The main system reservoirs are pressurized by:

  • Cabin pressure
  • A spring in the reservoir
  • Engine bleed air
  • System pressure applied to a differential piston
A
  • System pressure applied to a differential piston
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7
Q

The ENG HYD PUMP caution light illuminates when:

  • EDP output pressure drops below 2,750 psi.
  • EDP output pressure drops below 2,000 psi
  • EDP output pressure drops below 3,000 psi.
  • The power transfer unit is activated.
A
  • EDP output pressure drops below 2,000 psi
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8
Q

The main source of pressure for the No. 1 and No. 2 hydraulic systems is:

  • Electrically driven standby pumps.
  • Battery powered pump.
  • Engine-driven pumps.
  • The power transfer unit.
A
  • Engine-driven pumps.
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9
Q

The number of hydraulic systems on the Dash 8 aircraft is:

  • Three
  • Four
  • One
  • Two
A
  • Three
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