Limitations Flashcards

1
Q

Maximum tailwind component for takeoff

A

15 kts

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2
Q

Maximum tailwind component for landing

A

10 kts (may be authorized up to 15 kts if specified in Ops Advisory page or by F4 message

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3
Q

Severe turbulent air penetration speed

A

280kts/.76M

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4
Q

Max altitude with flaps extended

A

20,000ft

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5
Q

Holding in icing condition with flaps extended

A

Prohibited

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6
Q

Minimum altitude for speed brake deployment

A

1,000ft RA

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7
Q

3RA-3VM: Speedbrakes cannot be deployed with flaps ____

A

40 degrees

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8
Q

Limitation on Rapid Flight Control Movements

A

Avoid rapid and large ALTERNATING control inputs especially in combination with changes in pitch, roll, or yaw (e.g. large side slip angles) as they may result in structural failure at any speed, including below VA

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9
Q

Reverse Thrust is prohibited

A

In flight

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10
Q

Aileron trim is prohibited

A

With autopilot engaged

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11
Q

Minimum altitude for autopilot engagement after takeoff

A

400ft AGL

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12
Q

Minimum altitude for autopilot engagement during approach

A

50ft AGL

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13
Q

While autopilot engaged, do not select LVL CHG on final approach below

A

1000ft AFE

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14
Q

Maximum altitude for APU Bleed Air + Electrical (in flight)

A

10,000ft

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15
Q

Maximum altitude for APU Bleed Air

A

17,000ft

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16
Q

Maximum altitude for APU Electrical load

A

41,000ft

17
Q

Weather Radar must not be used where?

A

In a hangar

18
Q

When must HF Radio not be used?

A

During refueling operations

19
Q

Vmo/Mmo

A

340kts/.82M

20
Q

Maximum Operating Alititude

A

41,000ft

21
Q

Maximum altitude for Takeoff and Landing

A

8,400ft

22
Q

Max Crosswind for Takeoff and Land on Dry Runways

A

3AA-3PX: 33kts

3RA-3VM: 32kts

23
Q

Anytime passengers are on board,

A

At least 1 floor level exit must be open or armed

24
Q

All doors must be armed

A

On revenue flights

25
Q

Packs must not be in HIGH when one or both engine bleed air switches ON, and

A

For takeoff, approach and landing

26
Q

Maximum cabin differential pressure

A

9.1psi

27
Q

Maximum altitude for unpressurized flight following an in flight depressurization

Maximum altitude when aircraft is dispatched for unpressurized flight

A

14,000ft

10,000ft

28
Q

Icing Conditions Exist when

A

OAT on the ground and for takeoff, or TAT inflight is 10 degrees or below and

Visible moisture in any form is present such as clouds, fog with visibility of one mile or less, rain, snow, sleet and ice crystals
OR
When operating in ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines or freeze in the engines or nacelles.

29
Q

Engine ignition must be ____ when operating in icing conditions

A

ON

30
Q

Prior to descent in all icing conditions including temperatures below -40C SAT, engine anti-ice must be

A

ON

31
Q

Engine ignition for operating in heavy rain

A

CONT

32
Q

Minimum oil quantity prior to engine start

A

3AA-3PX: 12qts

3RA-3VM: 14qts

33
Q

Maximum allowable on the ground difference between captain and first officer altitude displays for RVSM

A

50ft (sea level to 5,000ft)

60ft (5,001ft to 10,000ft)

34
Q

Maximum fuel tank temperature

A

49 degrees C

35
Q

Minimum Fuel Tank temperature

A

-43 degrees C, or 3 degrees above the fuel freezing point temperature limit, whichever is higher

36
Q

Maximum fuel imbalance

A

1,000lbs

37
Q

Main tanks must be full if center tank contains more than

A

1,000lbs