Operating Limitations Flashcards

1
Q

Max operating Altitude

A

FL 410

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2
Q

Max Air Temp for TO and Landing

A

ISA +35C, +50C, 122F

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3
Q

Min. Temp approved for TO

A

-40C, -40F

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4
Q

When the ambient temp. Is -30C (-22F) or below for engine start

A

The Engine must be motored for 60 seconds, and the fan must rotate before engine start is initiated

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5
Q

For TO or landing on runways covered with standing water, slush or snow, or icing conditions..

A

Both igniters on both engines must be on continuously

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6
Q

Maximum runway slopes for take off and landing

A

+2% uphill

-2% down hill

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7
Q

Max tailwind component for take off and landing

A

10 knots

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8
Q

Maximum occupancy, including no more than 19 passengers, must not exceed the lesser of the following

A

22, or the # of seats for which takeoff and landing accommodation is provided.

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9
Q

Rotation rates should not exceed

A

3° per second

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10
Q

Pitch trim must be set according to

A

Aircraft computed center of gravity

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11
Q

Take off it’s trend initial target for rotation is

A

10°

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12
Q

Max Press. Altitude for TO and Landing

A

10,000 ft.

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13
Q

Engine cowl anti-ice system must be on when (Flight and Ground)

A

OAT is 10°C (50°F) or below and visible moisture in any form is present (such as fog with vis. Of 1 mi. Or less, rain, snow, sleet and ice crystals).

Also, when those same temps are present when operating on runways or taxiways where surface contamination is present.

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14
Q

The engine cowl anti-ice system must be on

A

At or above FL 220:

  • When ice is indicated by ice detection system
  • When in icing conditions if an ice detector has failed.

Below FL 220:

  • When in icing conditions
  • When ice is detected by the ice detection system
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15
Q

Wing anti-ice system. Ground operations.

A

Must be on for final taxi prior to TO. IF OAT is 5°C ( 41°F) or below, unless type 2,3, or 4 fluids have been applied.
Single engine taxi operations are prohibited in these conditions.

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16
Q

Icing conditions exist on the ground when

A

OAT is 5°C (41°F) or below and

  • visible moisture in any form is present below 400 feet AGL
  • the runway is wet or contaminated
  • in the presence of any precipitation
17
Q

L Heat or R Heat may go out during taxi, but..

A

Must be verified on prior to take off.

If wing anti-ice is not required for TO. It should be selected off just prior to take off

18
Q

Wing anti-ice system must be selected and confirmed on for take off when

A

The OAT is 5°C (41°F) or below and moisture is present

19
Q

If wing anti-ice is selected on for take off, what also must be selected on?

A

Cowl anti-ice must also be selected on

20
Q

When type 2,3, or 4 anti-ice fluids have been applied, the wing anti-ice system must..

A

Only be selected and confirmed on just prior to thrust increase for take off

21
Q

Icing conditions exist in flight at…

A

A TAT of 10°c (50°F) or below and visible moisture encountered, except when the SAT is -40°C. (40°F)

22
Q

Supercooled large droplet icing (SLD)

A

Wing anti-ice and Cowl anti-ice must be on, leave icing conditions when side window icing occurs

23
Q

Take off is permitted with frost adhering to

A
  • The upper surface of the fuselage

- The underside of the wing, that is caused by cold soaked fuel

24
Q

In addition to a visual check, a tactile check of the wing leading edge wing upper surface and wing rear upper surface is required during walk around when

A

The outside air temperature is 5°C (41°F) or less

  • The wing fuel temperature is 0° C or less
  • The atmospheric conditions have been conducive to frost formation