Week 1 & 2 Flashcards

1
Q

Three Main Flight Controls of a fixed wing aircraft

A

Ailerons, Elevators, Rudders

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2
Q

What is the rotary wing equivalent to Rudder Pedals

A

Tail Rotor Pedals/Anti-torque pedals

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3
Q

What are the two flight controls that control the flight of a helicopter through the MAIN ROTOR

A

Cyclic and Collective

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4
Q

What is the full rotating of the blades called on a helicopter?

A

Disk

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5
Q

What does the CYCLIC give you?

A

Pitch/Roll

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6
Q

When you pull collective, each blade generates more ______

A

lift

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7
Q

When you PULL the COLLECTIVE, the engine would need to input

A

More Power

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8
Q

When the collective is pulled hard, and not enough counter-torque pedal can be applied, ______ ___ _______ __________ _________________ occurs

A

Loss of Tail Rotor Effectiveness

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9
Q

On a North American Helicopter, the pilot uses _______ pedal to fight torque

A

Left

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10
Q

What is in between the two swash plates, allowing the top plate to turn?

A

Swash Plate Bearing

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11
Q

The compressor turbines turn the _______ _____ set of turbines

A

Power Shaft

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12
Q

The top swash plate is connected to the blades through ______ _____

A

Pitch Links

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13
Q

The lift vector is at…?

A

Right angles to the rotor disk

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14
Q

The Collective is responsible for two things…?

A

Altitude and Forward Airspeed

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15
Q

As the Main Rotor rotates, the helicopter wants to spin in the opposite direction, this is called…?

A

Torque Reaction

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16
Q

What do helicopters tend to do when hovering without any inputs from the pilot?

A

Drift sideways, Fly forwards

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17
Q

Main Rotor Pitch links are attached to the?

A

Rotating Swash Plate

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18
Q

How does the Mast and the Rotating Swash Plate rotate in sync?

A

Through the use of Scissor Links

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19
Q

The Final Link to the blades from the Flight Controls are called?

A

Pitch Links

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20
Q

_________ _________ connect the Pilot and Co-Pilot Flight Controls

A

Torque Tubes

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21
Q

_____ ________ are designed to change the direction of a push/pull tube

A

Bell Cranks

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22
Q

Cyclic makes the Swash Plates ______

A

Tilt

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23
Q

Cyclic attachments have to be ___ _________ apart

A

90 Degrees

24
Q

On the Cyclic, the Red Trigger is for _______________

A

Communication (PTT)

25
What are the two different switches on the collective stick?
Landing Lights and Starter Switch
26
Collective Sticks also often have a _______ - ______ throttle
Twist - Grip
27
True or False: Main rotor RPM Remains Constant?
True
28
\_\_\_\_\_\_\_\_\_ _________ slows the up and down movement of the collective
Friction Control
29
Ground Effect occurs when the helicopter is within _____ \_\_\_\_\_\_\_\_\_ __________ from the ground
1/2 Rotor Diameter
30
If the Main rotor on a Helicopter spins CLOCKWISE, which direction does the tail rotor BLOW air?
To the RIGHT of the helicopter
31
What does "IGE" stand for?
In Ground Effect
32
What does "OGE" Stand for?
Out of ground effect
33
If you can see the **white nav light** of an aircraft, where is it moving,relative to your position?
Away from you
34
If the **green nav light** is on the **left** side, where is the aircraft moving, relative to your position?
Towards you
35
Can you hover at higher altitudes in IGE or OGE?
IGE
36
\_\_\_\_\_\_\_\_\_\_ _____________ - a force occurs 90 degrees from the force applied in the direction of rotation
Gyroscopic Precession
37
When does Translational Lift occur?
At the transition period between hover and horizontal flight
38
\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_ occurs when the engine fails, allows the blades to spin freely to allow a safe landing
Autorotation
39
What does the rotor system do when the engine power train fails?
Disengages from the engine to allow free spinning in the direction of rotation
40
Which of Newton's laws is torque and torque reaction?
Newton's Third Law
41
Which rotor configuration is this?
Tandem
42
Which rotor configuration is this?
Coaxial
43
Which rotor configuration is this?
44
To give the helicopter fuselage **D****irectional Control,**a __________ \_\_\_\_\_\_\_ _________ is vertically mounted on the tail. In order to keep the fuselage straight when increasing power, the**pitch**of the tail rotor is increased, using the**foot pedals**
Variable Pitch Rotor
45
During normal operation, the direction of the flow of air is \_\_\_\_\_\_\_\_\_\_
Downward
46
During autorotation, the direction of the airflow through the main rotor is \_\_\_\_\_\_\_\_\_\_
Upwards
47
During Autorotation, the ______ must be maintained at a safe level
RPM
48
What is the problem with having a **high** Nr during autorotation?
Overspeed and structural damage
49
What is the problem with a **Low** Nr during autorotation?
Helicopter can't slow rate of descent/ will crash
50
When the engine fails, and the blades begin to autorotate, what must the pilot do?
Drop the collective stick
51
Which factors affect the RPM of the blades during autorotation
Air Density(Altitude), Temperature, weight
52
\_\_\_\_\_\_\_\_\_\_\_\_\_ __________ is the tendency for the whole helicopter to drift in the direction of the tail rotor thrust
Translational Tendency
53
What type of tail-rotor configuration is this?
Fenestron
54
What type of tail-rotor is this?
NOTAR
55
Locate the servos, push/pull tubes, bell cranks
56
On a **free turbine** helicopter, what is the twist-grip used to control?
Compressor RPM
57
A ________ \_\_\_\_\_ is often placed on top of the collective, containing trim switches, landing lights, searchlights, and the starter button.
Switch box