SY101 Flashcards

1
Q

Hydraulic System Operates:

A

Landing Gear, Main Gear Doors, Flaps, Speed Brake, and Nose Wheel Steeting

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2
Q

Primary Electrical Power

A

Starter/Generator

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3
Q

Secondary Electrical Power

A

24 V Battery

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4
Q

Backup Electrical Power

A

Auxiliary Battery

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5
Q

External Electrical Power

A

External Power Receptable

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6
Q

Standby Flight Instruments that work without electrical power

A

Airspeed Indicator, Altimeter, the ball in Turn and Bank Indicator, Magnetic Compass

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7
Q

Martin-Baker Seats process

A

Seats ejected from cockpit by gas cartridges; Altitude provided by rocket motor fired at top of seat rails.

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8
Q

VHF system provides:

A

VOR, ILS, localizer, and glideslope capability.

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9
Q

Personal Locator does what?

A

Senses impact loads and generates a signal on 121.5 and 406.0 MHz.

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10
Q

Birdstrike Protection is only found in

A

the windscreen and front canopy transparency

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11
Q

Primary aircraft electircal power is provided by which component of the electrical system?

A

The generator function of the starter/generator.

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12
Q

Tuning for each of the communications and navigation radios and the transponder is provided by which compenenet?

A

RMU

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13
Q

Primary navigation display is provided by which component of the Electronic Flight Instrument System?

A

EHSI

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14
Q

Landing gear extension and retraction is operated by which primary control surface?

A

Hydraulic

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15
Q

What component of the ejection seat provides sufficient altitude for parachute deployment?

A

Rocket motor

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16
Q

Secondary flight electircal power is provided by what compenent?

A

24V battery

17
Q

What aircraft system provides automatic temperature and pressure control?

A

Environmental control system

18
Q

Control of the transponder is provided by which component?

A

RMU

19
Q

Which primary instrument provides primary attitude display?

A

EADI

20
Q

In the event of inadvertent aircract contact with the ground, which component will be activated and generate a radio signal?

A

The personal locator radio beacon senses impact loads and generates a signal on 121.5 and 406.0 MHz.