Limitations Flashcards

0
Q

Airplane minimum operating temperature limit

A

-54 C

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1
Q

What is the maximum operating ambient temperature limit?

A

+50 C or ISA +35 C, whichever is lower

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2
Q

Maximum operating altitude

A

25,000 ft ASL

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3
Q

Maximum Operating Altitude for Takeoff

A

10,000 ft ASL

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4
Q

Maximum airspeed for flight in severe turbulence

A

210 KIAS

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5
Q

Maneuvering speed

A

204 KIAS

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6
Q

Maneuvering speed definition

A

Maximum speed with full application of rudder and aileron controls and maneuvers that involve angles of attack near the stall.

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7
Q

Maximum flaps extended speeds

A

These speeds shall not be deliberately exceeded. During deceleration, flaps may be selected at these speeds.

Flaps 5 195 KIAS
Flaps 10 175 KIAS
Flaps 15 165 KIAS
Flaps 35 155 KIAS

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8
Q

Max speed Flaps 5

A

195 KIAS

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9
Q

Max Speed Flaps 10

A

175 KIAS

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10
Q

Max Speed Flaps 15

A

165 KIAS

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11
Q

Max Speed Flaps 35

A

155 KIAS

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12
Q

Landing Gear Operating Speed

A

195 KIAS

The maximum speed at which it is safe to extend or retract landing gear

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13
Q

Landing gear extended speed

A

215 KIAS

The maximum speed with landing gear extended.

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14
Q

What are the Ambient Temperature Limitations on the powerplant?

A

+50 C or ISA +35, whichever is lower

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15
Q

Engine Starter Cranking Limits

A

Start 1: Maximum time on: 70 seconds

Followed by: 2 minutes off

16
Q

On the ground (taxi for takeoff roll to the point of liftoff)
Icing conditions exist when:

A

Static air temperature (SAT) is 10 deg. C or below when precipitation in any form is present, or fog with visibility of 1 mile or less;
Also when operating on ramps, taxiways, or runways where surface snow, ice, slush, or standing water may be ingested by the engines or freeze on engines, nacelles, or engine sensor probes.

17
Q

In flight, after liftoff to landing

Icing conditions exist when:

A

Static air temperature (SAT) is 5 deg C or below and visible moisture is present in any form. Ice accretion on aerodynamic surfaces is not considered to exist at temperatures of -40C or below.

18
Q

In icing conditions, engine intake bypass doors shall be:

A

OPEN

19
Q

What is maximum crosswind component?

A

Maximum crosswind component approved for takeoff and landing on a hard, dry, or wet runway is 32 knots.

20
Q

What is the Maximum Lateral Asymmetry for fuel?

A

Maximum fuel imbalance between contents of main fuel tanks is 600 lb. (This is an in flight limitation only.)

21
Q

Fuel:

Tank 1 and Tank 2 auxiliary pumps must be:

A

ON for takeoff and landing

22
Q

Minimum battery temperature for takeoff is

A

-20deg C

23
Q

Standby battery, Auxiliary battery, and Main battery maximum loadmeter reading for takeoff is:

A

0.1

24
Q

Maximum altitude with the landing gear and/ or flap extended is

A

15,000 feet

25
Q

Setting takeoff power prior to brake release, with the nose of teh airplane more than 45deg out of wind, is prohibited for wind speeds greater than

A

8 kts