V Speeds Flashcards

1
Q

Vcef

A

Critical Engine Failure Speed
The speed you can accelerate to on all 4 engines, lose one, and then either continue the takeoff or abort within the same distance on 3 engines

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2
Q

Vnef

A

Non-Critical Engine Failure Speed
The speed at which you can accelerate on all 4 engines and then stop with 2000 feet remaining

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3
Q

S1

A

Decision Speed
Prior to this speed you can abort after it you are committed to takeoff

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4
Q

Vr

A

Refusal Speed
The maximum speed which the aircraft can accelerate under normal conditions and stop within the remaining runway

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5
Q

Vmca

A

Inflight Minimum Control Speed
the min speed at which you can lose an outboard engine an d maintain straight-line directional control using the following:
1. Full rudder deflection
2. Not more than 5 degrees of bank
3. 3 engines at TRT

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6
Q

Vmcg

A

Min Controllable Gnd Speed
The min speed at which you can lose an outboard and maintain directional control with engines at takeoff N1

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7
Q

Vrot

A

Rotation Speed
The speed at which you change from the 3 point attitude to the takeoff attitude. It is reached 3 seconds prior to takeoff speed

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8
Q

Vto

A

Takeoff Speed
The speed at which the aircraft must be accelerated prior to leaving the ground.
Always greater than Vmca

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9
Q

Vmb

A

Maximum Braking Energy Decsion Speed
Highest speed from which the aircraft can be stopped without exceeding maximum energy absorption capability of the brakes.

50 million foot pounds for carbon brakes

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10
Q

Vnb

A

Normal Brake Energy Decision Speed
50% of Vmb (25 million foot pounds)

You will egress if you abort above this speed.

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11
Q

Vcb

A

Cautionary Brake Energy Decsion Speed
80% of Vmb, thermal fuse plugs may melt, only used in non-critical takeoff planning

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12
Q

Critical Takeoff Considerations

A
  1. CFL + 2000 > Runway Available
  2. CRN < 4
  3. S1>Vcb
  4. Obst Clearance < 1.0% of Obst Dist from DER

TRT or MCL recommeded for critcal takeoffs

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13
Q

TRT

A

Takeoff Rated Thrust
affected by temp, press, acm on/off, anti-ice on/off, PMC on/off
*If EGT limit is reached before TRT N1, abort

limit 5 mins

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14
Q

MCL

A

Maximum Climb
250 KCAS below 10,000
280 KCAS above 10,000

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15
Q

MIN

A

Minimum N1
The lowest setting at that will achieve minimum performance requirements

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16
Q

CRN

A

Climb Reference Number

does not equate to a climb gradient

17
Q

MCT

A

Max Continuous Thrust

18
Q

MCR

A

Maximum Cruise Thrust

19
Q

Basic Airplane Weight

A

weight of aircraft, engine oil, survival kits, oxygen, and unusable fuel

20
Q

Operating Aircraft Weight

A

Basic Aircaft Weight plus weight of crew, pax, cargo

21
Q
A