13. Hydraulics Flashcards

1
Q

Recall HYDRAULIC SD symbology and color-coding

A

Pre-Flight Hydraulic Fluid Level

Cyan – Normal (levels depicted are post engine start)

L/R Engine Hyd Pump

White – Commanded off

Green – Commanded on

Amber – Commanded on with low pressure. “P” displayed

Auxiliary Pump

White – Commanded off

Green – Commanded on

Amber – Commanded on with low pressure. “P” displayed

Hydraulic Pressure

White – Pressure within limits

Amber – Pressure exceeds high or low limits (value will be boxed)

Hydraulic Power Transfer Unit (PTU)

White - Commanded OFF

Green - Commanded ON

Hydraulic Fluid Quantity

White – Fluid level within limits

Amber - Fluid level below limits (value will be boxed)

Hyd Fluid TEMP HI

Amber – Fluid temp exceeds high limit (display will be boxed)

Hydraulic Fluid Reservoir

White - Fluid level within limits (Reservoir outlined)

Gray - Fluid level within limits

(Fluid shaded)

Amber - Fluid level below limits

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2
Q

Recall the function of the AUX hydraulic switch

A

ON - auxiliary pump is commanded on

OFF - auxiliary pump is commanded off

If the right engine driven pump fails, or the right engine fails, the AUX pump may be used to operate all right system components, including the landing gear

The electrically driven auxiliary pump, located in the right wheel well, has two purposes: to back up the right hydraulic system in flight and to pressurize the hydraulic systems on the ground when the engines are not running

The auxiliary pump has built-in thermal protection and automatically shuts down if it overheats

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3
Q

Recall the function of the HYD CONT RUDDER switch

A

When the switch is pushed, OFF illuminates, hydraulic power to the rudder is shut off, and the rudder reverts to manual operation

Allows selection of manual rudder operation

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4
Q

Recall the function of the TRANS pump switch

A

ON - pump shutoff valve commanded open: transfer pump operative

OFF - pump shutoff valve commanded closed: transfer pump is inoperative

The transfer pump, located in the left wheel well, enables a pressurized system to mechanically power an unpressurized system when both system reservoir quantities are normal

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5
Q

Recall associated precautions with Hydraulic System Test

A

WARNING: Do not establish hydraulic power which will result in flap, slat, or spoiler movement unless the wing/flap area has been cleared of personnel and equipment

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6
Q

Recall the effect of electrical failure on the Engine Driven Hydraulic Pumps

A

When electrical power is removed from an engine-driven pump, the pump defaults to ON

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7
Q

Recall what items are controlled by the L/R hydraulic systems

A

Right Hydraulic System

 Left and right outboard spoilers

 Rudder

 Right thrust reverser

 Landing gear

Left Hydraulic System

 Left and right inboard spoilers

 Left engine thrust reverser

 Elevator augmentation system

Both Hydraulic Systems

 Slats

 Flaps

 Rudder limiter

 Nosewheel steering

 Brakes

 Anti-skid

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