PPL General Flashcards

1
Q

Speed for maximum endurance?

A

Speed that consumes the less fuel

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2
Q

What is the compass lubber line?

A

Line showing aircraft heading on the compass

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3
Q

What is pre-ignition

A

Fuel/air mixture ignited too soon because of hot carbon particles

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4
Q

What will VSI indicate if static source is blocked?

A

Level flight

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5
Q

What is Newton’s third law

A

When one body exerts a force on a second body, the second body simultaneously exerts a force equal in magnitude and opposite in direction to the first body.

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6
Q

What is lift formula?

A

Lift = Cl x p/2 x V^2 x S

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7
Q

List radio readability scale (1 to 5)

A
  1. unreadable;
  2. readable now and then;
  3. readable with difficulty;
  4. readable; and
  5. perfectly readable.
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8
Q

What is slow flight?

A

Slow flight is the speed range between stalling speed and the speed for maximum
endurance.

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9
Q

Ground to air visual sign one need Fuel or Oil?

A

L

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10
Q

To which pressure source is the altimeter connected?

A

Static source

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11
Q

In the turn coordinator gyroscope, the supporting ring (gimbal) of the rotor is ___ to the longitudinal axis of the aircraft.

A

Tilted 35 degrees

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12
Q

What does the mixture controls?

A

The amount of fuel sucked by the nozzle

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13
Q

Wing tip vortices rotation from behind?

A

Clockwise on left, anticlockwise on right

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14
Q

Sign of carburetor icing on variable pitch propeller?

A

Decrease in manifold pressure

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15
Q

Ball + turn on same side= slipping or skidding?

A

Slipping

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16
Q

Formula to determine aircraft balance

A

Weight = moment / moment-arm

17
Q

Static port blocked.

What will Altimeter do?

A

Stop moving

18
Q

What instrument does pitot tube blockage affects?

A

Only Airspeed indicator

19
Q

Complete pitot blockage. What will airspeed indicate during climb/descent?

A

Will act like an altimeter.

20
Q

What will happen to altimeter if partial blockage of pitot tube?

A

slowly decrease to zero

21
Q

Name of speed bottom of white arc

A

Vs0 (power off, full flaps, stall speed)

22
Q

Name of speed on the Altimeter

A

IAS (Indicated Airspeed)

23
Q

What is CAS

A

Calibrated Airspeed

IAS corrected for Positional Error

24
Q

Rule of thumb to correct CAS for altitude and temperature?

A

add 2% to IAS for every 1000ft of pressure altitude increase

eg. 6000ft with 100kt → (6x2=) 12% to 100kt = 112kt.

25
Q

How will Airspeed react if pitot is blocked during climb?

A

Airspeed will increase (over-read) during a climb

26
Q

How will Airspeed react if pitot is blocked during descent?

A

Airspeed will under-read during descent

27
Q

What happens if static system is blocked?

  • Altimeter
  • VSI
  • Airspeed indicator during descent
  • Airspeed indicator during climb
A
  • Altimeter → frozen
  • VSI → constant zero
  • Airspeed indicator during descent → over-read (increase) STALL RISK
  • Airspeed indicator during climb → under-read (decrease)
28
Q

What happens to Airspeed indicator for partial leakage?

A

Slowly goes to zero

29
Q

What is “clean configuration”

A

Flaps and gear retracted

30
Q

Altimeter: What is the name of bottom of green arc?

A

Vs1: Power off stalling speed clean configuration

31
Q

Airspeed: name of upper limit of green arc

A

Vno: Maximum structural cruising speed

32
Q

Formula for bank angle stalling speed

A

Vst = Vs * sqrt(load_factor)

33
Q

As the CG moves ___ (forward/rearward) the stall speed ___ (increases/decreases)

A

As the CG moves forward the stall speed ___ increases

34
Q

An increase in weight ____ the stalling airspeed (increases/decreases). Why?

A

An increase in weight increases the stalling airspeed.

Because wing will fly at higher AoA for the same airspeed as compared to when it is lightly loaded. Will reach critical AoA sooner.