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Performance Manual > Takeoff Data > Flashcards

Takeoff Data Flashcards

1
Q

Best Climb Speed

A

the greater of the speed for MAX ROC or the flaps up air minimum control speed.

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2
Q

Flaps Up Safety Speed (FUSS)

A

The minimum speed recommended for normal operation with the flaps retracted. FUSS is the greater of 1.25 times the flaps up power off stall speed or the flaps up air minimum control speed.

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3
Q

Operation at FUSS provides __ g of maneuvering capability with all engines operating or __ g of maneuvering capability with one engine inoperative.

A
  1. 7

1. 3

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4
Q

What is V1 based on?

A

runway available

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5
Q

What is Vcef based on?

A

Critical field length

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6
Q

When Type II/IV anti-icing fluid is used, add __ KIAS to the normal rotation speed with the minimum rotation speed of __ KIAS.

A

5

100

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7
Q

___ takeoffs are not approved with anti-icing fluids.

A

Max effort

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8
Q

If the vertical tail is treated with anti-icing fluid, rotation speed must be equal to ___ speed.

A

refusal

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9
Q

Takeoff factor combines the parameters of ___ and ___.

A

field pressure altitude

runway temp

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10
Q

Runway condition: Dry

RCR:

A

23

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11
Q

Runway condition: Wet

RCR:

A

12

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12
Q

Runway condition: Icy

RCR:

A

05

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13
Q

ICAO Report: Good

RCR:

A

23

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14
Q

ICAO Report: Medium

RCR:

A

12

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15
Q

ICAO Report: Poor

RCR:

A

05

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16
Q

Runway Surface Condition (RSC) is a value which relates to depth and type of runway covering such as water or slush, and is reported in tenths of an inch in depth (one inch is the equivalent of an RSC of __)

A

10

17
Q

Only RCR corrections are used for runway contaminants less than __ in depth and only RSC corrections are used for contaminants greater than __ in depth.

A

3 mm

18
Q

Defining conditions for Vmca

A
  1. ATCS operational
  2. Bank angle equal or less than 5 degrees away from failed engine
  3. Max takeoff power on all engines
  4. Max rudder deflection limited by 150 lbs rudder force or max rudder control surface deflection
  5. Minimum flying weight
  6. No. 1 engine failed, prop auto fx’d
  7. Zero rudder trim
19
Q

Defining conditions for Vmca2

A
  1. Bank angle equal or less than 5 degrees away from failed engine
  2. Flaps 50%
  3. Max takeoff power on all engines
  4. Max rudder deflection limited by 150 lbs rudder force or max rudder control surface deflection
  5. Min flying weight
  6. No. 1 & 2 engined failed. No. 2 auto-fx’d and no. 1 prop either windmilling or feathered
  7. Rudder trim required for a 3 degree approach with 3 engines
  8. Gear down
20
Q

Refusal speed

A

Max speed to which the aircraft can accelerate to with engines at takeoff

21
Q

The crosswind limited takeoff run must be initiated with a maximum indicated power level of 2500 HP until 35 kts is reached. At 35 kts the power levers are advanced to full takeoff power. This procedure results in a __ ft penalty to all takeoff distance requirements.

A

200

22
Q

Critical Field Length

A

total runway distance required to accelerate on all engines to Vcef, experience an engine failure, then continue the takeoff or stop within the same distance.

23
Q

Refusal Speed

A

the maximum speed to which the aircraft can accelerate with engines at takeoff power and then stop within the remainder of the runway available, with two engines in reverse, one engine in ground idle, one prop fx’d, and max anti-skid braking.

24
Q

Define Critical Failure Speed

A

speed to which the aircraft can accelerate, lose an engine, and then either continue the takeoff with the remaining engines or stop in the same total runway distance.

25
Q

Brake Energy Limit speed

A

the maximum speed at which anti-skid braking can be applied without exceeding the energy absorption limit of the brake system

26
Q

The brake energy limit speeds are based on the brake temperature prior to ___ being equal to the ambient temperature.

A

taxi

27
Q

The normal rotation speed is scheduled to ensure that the liftoff speed is greater than the air minimum control speed and the obstacle clearance speed is at least __ times the power off stall speed.

A

1.2

28
Q

Vmcg

A

minimum airspeed during the takeoff ground run at which, when the critical engine fails, it is possible to maintain control of the aircraft using the rudder control alone and take off safely using normal piloting skill while maintaining takeoff power on the remaining engines

29
Q

Vmcg assumes maximum lateral deviation from initial runway track of __ ft

A

30

30
Q

The most critical condition for directional control is with the No. 1 engine failed at ___ gross weight

A

light

31
Q

Minimum Power Restoration speed

A

speed that represents the minimum airspeed at which full power may be restored to the opposing outboard engine and the pilot still maintain control of aircraft

32
Q

Attempting to maintain a wings level attitude at light gross weight with one engine inoperative increases Vmca by __ kts with the flaps up and by __ kts with the flaps set at 50%

A

23

43

33
Q

Loss of either utility or booster hydraulic systems results in a __ kt increase in the flaps up Vmca

A

36

34
Q

Loss of either utility or booster hydraulic systems results in a __ kt increase in the flaps 50% Vmca

A

20

35
Q

Define takeoff distance

A

the total distance required to accelerate from brake release to the takeoff speed, liftoff and climb to a 50 ft obstacle

36
Q

Define takeoff ground run

A

the distance required to accelerate from brake release to liftoff

37
Q

Define MFLMETO

A

the length of runway which is required to accelerate to Vcef, experience and engine failure, and stop or continue acceleration to maximum effort takeoff speed within the remaining runway

38
Q

Defined adjusted MFLMETO

A

distance required to accelerate on all engines to Vcef, experience an engine failure, then in the same distance either stop or accelerate to liftoff at or above Vmca and the 3 engine minimum liftoff speed

Performance Manual (2 decks)

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