SY101 Flashcards

(19 cards)

1
Q

Which control surface controls aircraft movement around the pitch axis?

A

Elevator

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2
Q

The Trim Aid Device (TAD) assists trimming for which control surface during airspeed and power changes?

A

The TAD senses torque, altitude, airspeed, and pitch rate and computes a desired rudder trim tab position.

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3
Q

True or False? Engine exhaust augments the thrust of the propeller.

A

True. Exhaust gases are ejected rearward providing thrust which augments that produced by the propeller.

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4
Q

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

A

The generator function of the starter/generator.

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5
Q

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

A

RMU (Radio Management Unit)

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6
Q

True or False? The VHF navigation system provides VOR, ILS, localizer, and GPS capability.

A

False. The VHF system provides VOR, ILS, localizer, and glideslope capability.

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7
Q

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

A

Electronic Horizontal Situation Indicator (EHSI)

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8
Q

Which standby flight instruments will operate without electrical power?

A

The standby altimeter, airspeed indicator, the ball in the turn and bank indicator, and the magnetic compass.

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9
Q

True or False? The entire canopy structure is engineered to be protected from birdstrikes.

A

False. Only the windscreen and front canopy transparency are protected.

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10
Q

Landing gear extension and retraction is operated by which aircraft system?

A

Hydraulic System

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11
Q

Movement around the roll axis is controlled by which primary control surface(s)?

A

Ailerons

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12
Q

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

A

Rocket Motor

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13
Q

True or False? The magnetic compass is one of the primary flight instruments.

A

False. The magnetic compass is a standby flight instrument.

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14
Q

Secondary aircraft electrical power is provided by what component?

A

24 volt battery

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15
Q

Which aircraft system provides automatic temperature and pressurization control?

A

Environmental Control System

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16
Q

Control of the transponder is provided by which component?

A

Radio Management Unit (RMU)

17
Q

True or False? The canopy is hinged at the rear and opens up.

A

False. The canopy is hinged along the right side and opens to that side.

18
Q

Which primary instrument provides primary attitude display?

A

Electronic Attitude Director Indicator (EADI)

19
Q

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

A

The Emergency Locator Transmitter (ELT) senses impact loads and generates a signal on 121.5 and 406.0 MHz.