Limits Flashcards

1
Q

Max Tailwind Component -Takeoff

A

15 Knots

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2
Q

Max Tailwind Component - Landing

A

15 Knots

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3
Q

Max Operating Altitude

A

41,000

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4
Q

Max T/O and Landing Altitude

A

8,400

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5
Q

Min. T/O and Landing Temperature

A

-54C

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6
Q

Severe Turbulence Penetration Speed

A

Lesser of 280 Knots or .76M

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7
Q

Autopilot must be disengaged:

A

Below 1000’ AGL on T/O
Below 50’ AGL single channel appr.
Below 500’ AGL manual Cat3a HGS

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8
Q

Engine warm-up/cool-down:

A

3 minutes

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9
Q

Max time using T/O thrust

A

2 engines: 5 min
1 engine: 10 min

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10
Q

Engine Start switches must be in Cont:

A

Take-off
Landing
Anti-ice operations
Hail, sleet, moderate to heavy rain

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11
Q

Engine Start switches must be in FLT:

A

Sever Turbulence

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12
Q

Minimum oil temp for T/O thrust:

A

NG - none
Max - 31C

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13
Q

Reverse thrust prohibited:

A

In flight

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14
Q

APU Bleed and Electric load limit:

A

10,000 ft

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15
Q

APU bleed only load limit

A

17,000 ft

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16
Q

APU electric load limit:

A

41,000 ft

17
Q

APU max Operating altitude

A

41,000’

18
Q

APU bleed switch must be closed for _ min after start

A

2 min

19
Q

APU bleed switch must be closed for _ min. before shutdown

A

1 min

20
Q

Avoid power above _ with the APU bleed air valve open

A

Idle power

21
Q

When another source is pressurizing the L Duct, the APU bleed switch must be _

A

Closed

22
Q

Max Flap extension Altitude:

A

20’000 ft

23
Q

Minimum Altitude for speed brake:

A

1000 ft

24
Q

Max Flap setting for use of the speed brake:

A

10 degrees

25
Q

Minimum Fuel temperature:

A

-37C

26
Q

Max fuel imbalance for taxi, take-off and Landing:

A

1000 lbs

27
Q

Unless main tanks are _ , center tanks limited to _

A

Full

1000 lbs

28
Q

Center tanks pumps must be off unless:

A

Pilot on flight deck
<1000 lbs in tank(unless fueling or tx)
No low press light

29
Q

Min fuel quantity in respective tank for electric hydraulic pump operation:

A

1675