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SIFT Army Aviation Information Section Exam Questions and Answers

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SIFT Army Aviation Information Section Exam Questions and Answers A Helicopter - Is a type of rotorcraft that is able to takeoff and land vertically, hover, and fly forward, backward, and side to side (laterally). Thrust engine - an engine that produces power and delivers it to overhead and tail rotors (on most helicopters) via one or more transmissions and drive shafts. Fuselage - Main Body of the helicopter Mast - Shaft protruding from the top Cowling - On the upper part of the fuselage of many helicopters, it covers the aircrafts engine and transmission. two to six rotor blade - How many rotor blades are attached to the mast via a rotor head? Flybar - also called a stabilizer bar. upper and lower swashplates, blade grips, control rods, pitch and scissor links, teeter or coning hinges, pitch horns, and counterweights - Rotor systems consist of what components? 2 | P a g e Katelyn Whitman© 2025, All Rights Reserved. enhance flight stability by keeping the bar stable as the rotor spins, and to reduce crosswind thrust on the blades - What is the Flybars Function? cyclic collective, throttle and pedals - what are the pilot's flight instruments and controls? Avionics - what are electronics used for navigation, communications and aircraft systems term? Weapons controls - How does the pilot use weapons from a military helicopter cockpit? weight, lift, thrust, and drag - what are the four aerodynamic forces that act on a helicopter when it is airborne? Lift - what is the force that counteracts an aircrafts weight and causes a helicopter to rise into the air and stay aloft. Lift - is produced by airfoils - rotor blades, in the case of helicopters - that move through the air at a speed sufficient to create a pressure differential between the two sides of the airfoils. Thrust - is an aircraft's forward force, which is created by one or more engines, and is transformed in the case of helicopters into rotary motion via the components mentioned. Generally, _______ acts parallel to the aircrafts longitudinal axis, but not always. 3 | P a g e Katelyn Whitman© 2025, All Rights Reserved. Drag - opposes thrust; it is a rearward- acting force caused by airflow passing over the aircraft's structure and becoming disrupted. ________ acts parallel to the relative wind. Profile, induced and parasite - what are the three types of drag? Profile drag - Drag created by the blades' frictional resistance increases. Consists of skin friction created by surface imperfections and form drag. Induced drag - Drag created by air circulating around each rotor blade as it spins and creates lift; the circulation causes a vortex behind each blade. Parasite drag - Drag created by helicopter components and attached equipment that do not contribute to lift, including the fuselage, tail section, skids or wheels, externally mounted engines, sensors and weapons. Bernoulli's Principle - Scientific Principle that en

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SIFT Army Aviation

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Uploaded on
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Written in
2024/2025
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SIFT Army Aviation Information
Section Exam Questions and Answers

A Helicopter - ✔✔Is a type of rotorcraft that is able to takeoff and land vertically, hover,

and fly forward, backward, and side to side (laterally).


Thrust engine - ✔✔an engine that produces power and delivers it to overhead and tail

rotors (on most helicopters) via one or more transmissions and drive shafts.


Fuselage - ✔✔Main Body of the helicopter


Mast - ✔✔Shaft protruding from the top


Cowling - ✔✔On the upper part of the fuselage of many helicopters, it covers the

aircrafts engine and transmission.


two to six rotor blade - ✔✔How many rotor blades are attached to the mast via a rotor

head?


Flybar - ✔✔also called a stabilizer bar.


upper and lower swashplates, blade grips, control rods, pitch and scissor links, teeter or

coning hinges, pitch horns, and counterweights - ✔✔Rotor systems consist of what

components?



Katelyn Whitman© 2025, All Rights Reserved.

,2|Page


enhance flight stability by keeping the bar stable as the rotor spins, and to reduce

crosswind thrust on the blades - ✔✔What is the Flybars Function?


cyclic collective, throttle and pedals - ✔✔what are the pilot's flight instruments and

controls?


Avionics - ✔✔what are electronics used for navigation, communications and aircraft

systems term?


Weapons controls - ✔✔How does the pilot use weapons from a military helicopter

cockpit?


weight, lift, thrust, and drag - ✔✔what are the four aerodynamic forces that act on a

helicopter when it is airborne?


Lift - ✔✔what is the force that counteracts an aircrafts weight and causes a helicopter to

rise into the air and stay aloft.


Lift - ✔✔is produced by airfoils - rotor blades, in the case of helicopters - that move

through the air at a speed sufficient to create a pressure differential between the two

sides of the airfoils.


Thrust - ✔✔is an aircraft's forward force, which is created by one or more engines, and

is transformed in the case of helicopters into rotary motion via the components

mentioned. Generally, _______ acts parallel to the aircrafts longitudinal axis, but not

always.



Katelyn Whitman© 2025, All Rights Reserved.

, 3|Page


Drag - ✔✔opposes thrust; it is a rearward- acting force caused by airflow passing over

the aircraft's structure and becoming disrupted. ________ acts parallel to the relative

wind.


Profile, induced and parasite - ✔✔what are the three types of drag?


Profile drag - ✔✔Drag created by the blades' frictional resistance increases. Consists of

skin friction created by surface imperfections and form drag.


Induced drag - ✔✔Drag created by air circulating around each rotor blade as it spins

and creates lift; the circulation causes a vortex behind each blade.


Parasite drag - ✔✔Drag created by helicopter components and attached equipment that

do not contribute to lift, including the fuselage, tail section, skids or wheels, externally

mounted engines, sensors and weapons.


Bernoulli's Principle - ✔✔Scientific Principle that energy cannot be created or

destroyed- only its form can be changed - and a system's total energy does not increase

or decrease


Conservation of energy - ✔✔Bernoulli's principle is based off this. It says that in a

steady flow the sum of all forms of mechanical energy- a fluids potential energy plus its

kinetic energy - along a streamline is the same at all points.


Potential energy - ✔✔what kind of energy would be left in the helicopter if it were

airborne when it ran out of fuel?



Katelyn Whitman© 2025, All Rights Reserved.

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