Exercises 4 - 10 Flashcards

(70 cards)

1
Q

Primary effect of elevator

A

Pitch

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2
Q

Primary effect of aileron

A

Roll

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3
Q

Primary effect of rudder

A

Yaw

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4
Q

Secondary effect of rudder

A

Roll

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5
Q

Secondary effect of roll

A

Yaw

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6
Q

Yaw causes roll because of (2)

A

Outer wing moves faster than inner wing, generates more lift.
Dihedral Aircraft has outer wing presented to airflow at greater angle of attack, generating more lift

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7
Q

Secondary effect of elevator

A

Changing airspeed

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8
Q

Why are ailerons’ effectivity not affected by power changes

A

They are outside the slipstream

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9
Q

3 ways to increase lift

A

Increase airspeed.
Increase angle of attack.
Increase camber.

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10
Q

Slipstream effect most pronounced under conditions of

A

High power and low airspeed

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11
Q

High power and low airspeed makes slipstream effect more pronounced because (2)

A

Corkscrew is tighter and angle of attack is greater

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12
Q

Normal (clockwise) slipstream causes what control effect

A

Left yaw

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13
Q

Reducing power causes a

A

Pitch down tendency

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14
Q

Increasing power causes a

A

Pitch up tendency

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15
Q

Effect of raising flap

A

Nose pitches down and airspeed increases

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16
Q

Effect of extending flap

A

Nose pitches up and speed reduces

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17
Q

Mixture should be fully rich below

A

3000’

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18
Q

Whilst taxying, always

A

Pull elevator towards you

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19
Q

Level flight check

A

Power 2200RPM, Attitude, Trim

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20
Q

FREDA

A

Fuel, Radio, Engine, Direction, Altimeter

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21
Q

Scanning check

A

Lookout, Attitude, Instruments

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22
Q

If neither straight nor level:

A

Level wings, set correct pitch attitude, check balance

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23
Q

Straight and Level at 2350 RPM, gives you an attitude at

A

95kts

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24
Q

Straight and level at 1900 RPM, gives you an attitude at

A

70kts

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25
If climbing/too fast while straight and level
Reduce power, adjust attitude, re-trim
26
If descending/too fast
Leave power, higher attitude, re-trim
27
Straight and level with flap
Power 1900 RPM 20 degree flap Power 2200 RPM Attitude Trim
28
DABLE
Direction Airspeed Balance Lookout Engine
29
DABLE check: Direction
Direction Indicator
30
DABLE check: Airspeed
Airspeed Indicator
31
DABLE check: Balance
Ball
32
When levelling off from climb, anticipate the lookout by:
50'
33
Vx
Best angle
34
Vy
Best rate
35
Vx is for
Clearing obstacles
36
Climbing at 70-80kts is better than Vx, Vy because
Better groundspeed, visibility and engin cooling
37
Vy is for
Gaining altitude as fast as possible
38
Descending in a glide
Power close throttle, Maintain attitude until 65kts and pitch down to glide at 65kts Trim
38
When descending, do what?
Carb heat
39
When descending, adjust DABLE to
Engine warm every 500'
40
When descending in a glide, anticipate level off by
100'
41
When cruise descending, anticipate level off by
50'
42
Cruise descending
Power 1800RPM Attitude pitch down to maintain cruise speed Trim
43
Whenever levelling off after a descent, do what
Carb heat
44
Go-around items
Carb heat cold Power full Attitude shallow climb Flaps 20 Trim Safe height rest of flaps Re-trim
45
Descending with flap
Glide 65kts Flaps 20 Pitch down to maintain 65kts Trim
46
Descending with power
Glide 65kts Power 1500RPM Pitch up to maintain 65kts Trim Power controls rate of descent
47
Whilst in a powered descent, what controls the ROD
Power
48
Why is control column pulled back during a bank to maintain level flight?
Increase amount of lift from the wing to equal the weight
49
Max angle of bank during climbing turns
15
50
Max angle of bank during descending turns
30
51
Whilst in a climbing/descending turn, what control is used to maintain airspeed?
Elevator
52
HASELL
Height Airframe Security Engine Location Lookout
53
HASELL check: height
HASELL check: at least 3000'
54
HASELL check: airframe
Flaps or clean
55
HASELL check: security
Seatbelts and no loose objects
56
HASELL check: engine
Temp, pressure, carb heat
57
HASELL check: location
Airspace, built-up area, clouds, danger zones
58
HASELL check: location acronym
ABCD
59
HASELL check: ABCD
Airspace, built-up area, clouds, danger zones
60
HASELL check: lookout
90 degree or 180 degree turns
61
Straight and level slow flight
Power 1500RPM Attitude piitch up to maintain level flight Trim Power increase by 100RPM increments at Vs1+10 to 1900RPM Trim
62
VS1
Clean stall speed
63
VS0
Full flaps stall speed
64
Standard stall recovery
Push control column forward Prevent further yaw Full power and carb heat in
65
Factors affecting the stall: Power
Slower onset stalll, higher nose attitude
66
Factors affecting the stall: Flap
Faster onset stall, lower nose attitude but more abrupt stall
67
Factors affecting the stall: Power and Flap
Normal onset stall, normal nose attitude and possible wing drop
68
Factors affecting the stall: Weight
Increased stalling speed
69
Factors affecting the stall: Power, Flap and Power & Flap whole effect
Reduced stalling speed