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SIFT (Army Aviation Information) Practice Test 2024/2025 Exam Questions and Detailed Answers | Get it 100% Correct Answers

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SIFT (Army Aviation Information) Practice Test 2024/2025 Exam Questions and Detailed Answers | Get it 100% Correct Answers The typical structure of a helicopter is a ______ (fill in the blank) with a ____ (fill in the blank) protruding upward out of it. -

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SIFT (Army Aviation Information)
Practice Test 2024/2025 Exam Questions
and Detailed Answers | Get it 100%
Correct Answers



The typical structure of a helicopter is a ______ (fill in the blank) with a

____ (fill in the blank) protruding upward out of it. - 🧠ANSWER

✔✔Fuselage (the body of the craft), Mast.


The engine of the craft drives power upward through the ____ (fill in the

blank) to the rotor blades, which are controlled by the pilot. - 🧠ANSWER

✔✔Mast


This main rotor is used to generate ____ (fill in the blank). - 🧠ANSWER

✔✔Thrust.


____ (fill in the blank) is balanced by a second rotor, usually a tail rotor,

which is intended to account for the effects of ____ (fill in the blank). -

🧠ANSWER ✔✔Thrust, Torque.




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,What are the two main types of aircraft? - 🧠ANSWER ✔✔Rotorcraft and

Fixed Wing.

The main advantage of a helicopter over an airplane is its ability to takeoff

____ (fill in the blank). It can also ____ (fill in the blank). This means

helicopters can be used to takeoff from and land in places that would be

impossible for planes. They can also perform tasks such as dropping cargo

or troops into challenging positions. - 🧠ANSWER ✔✔Vertically, Hover.


What are the different Helicopter types? - 🧠ANSWER ✔✔Single Main

Rotor, Tandem Rotor, and Coaxial Rotor.

This is the most common design for a helicopter- a ____ (fill in the blank)

rotor generating power, with a secondary rotor, such as a tail rotor, used to

offset the effects of torque. One disadvantage of this design is that some

power is used for countering ____ (fill in the blank), rather than being used

solely for lift. - 🧠ANSWER ✔✔A Single Main Rotor, Torque.


This helicopter design features two main rotating blade sections: front and

rear. Each set of blades rotates counter to the other, meaning that torque is

automatically offset. There is no need for additional measures, such as a

tail rotor, to deal with torque. Because of this, all of the power from the

engine can be used to lift. Consequently, ____ (fill in the blank) helicopters

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, are some of the fastest and most powerful in existence. - 🧠ANSWER

✔✔Tandem Rotor Helicopter.


This type of helicopter features two sets of blades rotating above and

beneath each other. The two sets of blades are mounted to the same mast,

but rotate in opposite directions to each other. This has the advantage of

reducing ____ (fill in the blank) and allowing for greater cargo and

passenger capacity as a result. - 🧠ANSWER ✔✔Coaxial Rotor Helicopter,

Payload.

____ (fill in the blank) is created by the engine, or engines, of the

helicopter. It is transferred into motion via the ____ (fill in the blank) and

____ (fill in the blank). Sufficient ____ (fill in the blank) is needed to

overcome the drag and the weight of the helicopter and keep moving it

forward. - 🧠ANSWER ✔✔Thrust, Mast and Rotors, Thrust.


____ (fill in the blank) is a force which acts against thrust. In the case of

helicopters, drag is caused by the shape and size of the aircraft disrupting

the flow of air as it travels. There are several types of ____ (fill in the blank)

which impact helicopters. - 🧠ANSWER ✔✔Drag




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