ME Flashcards

1
Q

Definition of an absolute ceiling?

A

The highest altitude at which an aircraft can maintain level flight.

Max thrust available = thrust required = total drag at minimum drag speed

RoC and AoC equals 0

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2
Q

Definition of a service ceiling?

A

The highest density altitude at which an aircraft can, in clean configuration and at Vy, sustain a climb at 100ft/min

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3
Q

What is happening when an ME aircraft lose an engine?

A

The aircraft yaws and rolls towards the inoperative engine.

Because the operative engine creates more thrust, it induces a yaw. Being faster, it also creates more lift, inducing the roll. The induced flow of the operative engine also adds lift, increasing the roll.

If not feathered, the windmilling prop of the inoperative engine greatly increases drag, increasing the aforementioned effects.

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4
Q

What should you do to get a zero side slip in the event of losing an engine?

A

Rudder + light roll towards the operative engine

Ball centered on the left or right line (halfway out of the center cage)

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5
Q

Definition of the critical engine?

A

The engine whose failure would most adversely affect the performance or handling qualities of the aircraft.

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6
Q

On a PA27, which one is the critical engine?

A

Left one

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7
Q

Explain why, on a twin-engine which both engines turn CW, the left engine is the critical engine.

A

At high angles of attack, due to P-Factor, the descending blades are creating more thrust. The thrust moment of the right engine (from the centerline of the aircraft) being bigger, the right wing tends to go faster.

If on top of that you lose the left engine, that’s where you’ll have to apply most rudder (to counteract a greater yawing moment).

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8
Q

Definition of the Vmc?

A

Velocity of minimum control / Minimum control speed

The minimum speed at which it is possible to retain control of the aircraft and maintain straight flight, through the use of maximum rudder deflection and not more than 5° bank angle.

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9
Q

What happens if a twin-engine aircraft goes below Vmc?

A

There may be no sufficient rudder authority to counteract the yawing movement and maintain directional control of the aircraft.

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10
Q

What are the factors affecting Vmc?

A
  • Bank angle
  • Propeller
  • Power setting
  • Altitude
  • Weight
  • C of G
  • Flaps
  • Gears
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11
Q

How does the bank angle affect the Vmc?

A

Too much bank angle adversely affects the performance. As much as 3kts per degree of bank. Keep a low bank angle to avoid enter a sideslip.

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12
Q

How does the propeller affect the Vmc?

A

A windmilling propeller creates a lot of drag. Remember to feather it as soon as you have confirmed the inoperative engine.

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13
Q

How does the power setting affect the Vmc?

A

A low power setting will decrease the adverse effects of losing an engine.

However, going on a too low power setting also decrease overall performance!

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14
Q

How does the altitude affect the Vmc?

A

At high altitudes, air being less dense, the power will decrease, reducing the effects of running on one engine.

Vmc will therefore decrease with an increase in altitude or OAT. But it could go below the Vs, which is not good.

This also means that if you lose altitude, your Vmc will increase (and you will be able to keep it above Vs)

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15
Q

How does C of G affect the Vmc?

A

An aft center of gravity will increase the Vmc, as the arm through will the rudder acts will be shorter.

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16
Q

How does weight affect the Vmc?

A

Less weight will increase the Vmc.

With less lift required, you reduce the horizontal component of lift available to counteract the roll. Therefore you need more rudder.

However, overall, more weight will adversely affect the performance of the aircraft.

17
Q

How do flaps affect the Vmc?

A

With full flaps, your wings are generating more lift (so more horizontal component of the lift), therefore less rudder is needed.

18
Q

How do gears affect the Vmc?

A

Gears have variable effects on Vmc, depending on the aircraft. Keep in mind that Vmc certification is done gears up.

19
Q

Overall, what can you do to reduce the Vmc?

A
  • Reduce bank angle (to avoid sideslip)
  • Feather the dead engine propeller (to reduce its drag)
  • Reduce power (but not too much, to keep some performance)
  • Keep a good altitude (but remember to stay above Vs)
  • The greater the weight, the better (you’ll be able to use more horizontal component of lift, therefore less rudder)
  • Forward C of G (so your rudder is more efficient)
  • Flaps down (so you have more lift, reducing the need of rudder)
  • Gears : it depends on the aircraft. Vmc certif is done gears up.
20
Q

When going full throttle at T/O, what should be the manifold pressure indication, in regard with static MP, and why?

A

The MP should be around 1 inHg less than the static MP, because of the resistance caused by air filter and bends in intake pipes.

21
Q

If you use incorrect bank angle during engine failure, how much performance can you lose?

A

Vmc can increase by 3 knots per degree of incorrect bank

You lose 30 fpm of climb capacity per degree of incorrect bank

22
Q

What is the purpose of giving a MZFW (max zero fuel weight) on an aircraft?

A

It helps to prevent overstress on wing spar

23
Q

Why is an engine more critical than the other?

A

P.A.S.T. !

P : P-Factor : with angle of attack, the downgoing blade creates more thrust
A : Accelerated airflow : the accelerated airflow over the wings is not centered, inducing a roll
S : Slipstream : slipstream of the left engine operative will help to counteract the yaw to the right
T : Torque : it induces a roll to the left, which may be helpful for the loss of right engine

24
Q

What is your immediate reaction if you go below Vmc?

A

Reduce power to decrease the yawing movement and recover rudder authority.

25
Q

How is Vmc tested/determined?

A
  • all engines developing maximum rated power at the time of critical engine failure
  • the aircraft is at a minimum practical test weight with a rearmost center of gravity
  • landing gear retracted, flaps in take-off position and the propeller of the failed critical engine windmilling