CADH Practice Cards 9 Flashcards

Random questions/statements for exam preparation

1
Q

Refer to vector diagram

Vector I acts parallel to …

Vector diagram in forward flight
A

the relative airflow

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

The most common method of starting the engines on a large civilian helicopter is …

A

electric starter motors

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

A helicopter with an anti-clockwise rotating main rotor system is hovering to the left in nil wind. The maximum angle of attack is at position …

A

6 o’clock or aft of the aircraft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

A common recovery action to correct retreating blade stall, and settling with power is …

A

decrease angle of attack

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Helicopter rotor diameter is 35 ft, it is operating at 2600 lb AUW. The approximate disc loading is …

A

2.6 lb/sq ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

The coning angle refers to …

A

the smaller angle between the tip path plane and the logitudinal axis of the blade

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Refer to diagram

The vector labelled E is …

A

total reaction

The diagram is of the autorotaive drive region

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

The term ‘Soft in Plane’ is associated with …

A

the leading and lagging freedom of the main rotor blades

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Ground effect is useful to a height of …

A

half a rotor diameter

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Refer to the diagram

The vector labelled H is …

A

autorotative force

The diagram is of the autorotaive drive region

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

One of the main causes of hunting is …

A

geometric imbalance

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

The swash plate is used to …

A

transfer cyclic and collective control movements to the rotor disc

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

The best angle of climb airspeed in a helicopter which has the ability to hover OGE is …

A

mainly dependant on the power available

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Refer to vector diagram

Vector J acts perpendicular to …

Vector diagram in forward flight
A

rotor thrust

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Coning angle will increase is thrust …

A

increases, or centrifugal force (rotor RPM) decreases

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

To hover over a spot, minimum power will be required when the wind speed is approximately …

17
Q

During a steep approach to land with an IAS of 8 kt and a high relative ground speed you may experience problems with yaw control due to …

A

weather cock stability and LTE issues

18
Q

To settle with power the following conditions are required …

A

a descent rate, nearly zero airspeed, power applied

19
Q

The cyclic control on a helicopter alters the …

A

pitch on each blade consecutively and independently of the other blades (relative to the mast)

20
Q

Main rotor reverse thrust is most useful on a large helicopter to …

A

pin it to the deck of a moving vessel or helideck

21
Q

A rotor aerofoil section is symmetrical because …

A

it minimises movement for the centre of pressure in all flight conditions

22
Q

Refer to Power Curve Diagram

The speed represented by the letter E is the speed for …

The Power Curve
A

maximum excess power

23
Q

When taxiing rapidly sideways to the left, the helicopter experiences uncommanding yawing. Unless careful attention to pedal input is made the helicopter may experience …

A

uncontrolled yawing to the right due to vortex ring induced LTE

24
Q

Flapback is compensated by …

A

cyclic feathing

25
Q

What is the rate of descent required to induce settling with power …

A

300 ft/min

26
Q

You notice that engine RPM is high and manifold pressure is low, the action you would take is …

A

decrease throttle, increase collective

27
Q

The collective control on a helicopter changes the …

A

pitch of each blade an equal amount (relative to the hub)

28
Q

The term ‘Disc Solidity’ refers to …

A

the ratio of blade area to disc area

29
Q

The first rotor system to incorporate a flapping hinge was designed by …

A

Juan de la Cierva

30
Q

Overpitching is caused by …

A

the engine at a given power setting being unable to overcome rotor drag

31
Q

The vibration associated with transverse flow effect (inflow roll) is caused by …

A

loss of lift over the rear of the disk

32
Q

The rigid rotor has …

A

feathering freedom only

33
Q

Refer to Power Curve Diagram

The speed represented by the letter D is the speed for …

The Power Curve
A

maximum forward speed

34
Q

Retreating blade stall is most likely to occur at …

A

high speed, low RPM, steep turn

35
Q

A semi ridged rotor can …

A

feather, flap and cone

36
Q

Flapping is movement of the rotor blades which help …

A

overcome dissymmetry of lift in forward flight

37
Q

Advantages of a shrouded (Fenestron) tail rotor over a conventional tail rotor are …

A

elimination of asymmetry of lift means the blades only need feathering freedom and not flapping freedom

38
Q

During normal approach to land in light wind at a HLS located within a ground hollow, a hazardthat needs special attention is …

A

re-circulation prior to shutdown