Limitations Flashcards

1
Q

Maximum landing tailwind component is _____ kts.

A

15

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2
Q

Maximum takeoff tailwind component is _____ kts.

A

15

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3
Q

Maximum operating altitude is ______.

A

41000’

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4
Q

Maximum takeoff and landing altitude is _____ ft.

A

8400

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5
Q

Severe Turbulence Penetration airspeed is_____.

A

280 KIAS / .76M

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6
Q

With engine bleed air switches ____”,” do not operate the air conditioning packs in ____ for takeoff”,” approach or landing.

A

ON / HIGH

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7
Q

Engine TAI must be ON when icing conditions exist or anticipated”,” except during climb or cruise below _____.

A

-40 degrees SAT

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8
Q

Do not engage the autopilot below _____ AGL on takeoff.

A

1000’

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9
Q

For single channel ILS operation during approach”,” the autopilot shall not remain engaged below _____ feet AGL.

A

50’

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10
Q

For manually flown HGS AIII approach”,” the autopilot shall not remain engaged below _____ AGL.

A

500’

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11
Q

Use of aileron trim with autopilot engaged is _____.

A

prohibited

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12
Q

Operate the engines for a minimum of _____ minutes prior to takeoff.

A

3

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13
Q

Operate engines at or near idle (taxi thrust acceptable) for a minimum of _____ minutes prior to shutdown.

A

3

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14
Q

Maximum time limit for Takeoff Thrust”,” assuming normal takeoff with both engines operating”,” is _____ minutes.

A

5

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15
Q

Maximum time limit for Takeoff Thrust”,” in the event of loss of engine thrust during takeoff is _____ minutes.

A

10

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16
Q

ENGINE START Switches must be in the CONT position for _____. (Select ALL correct answers.)

A

1) takeoff
2) landing
3) anti-ice operation

17
Q

Maximum start EGT is _____ degrees.

A

725

18
Q

ENGINE START Switches must be in the FLT position for _____.

A

operation in severe turbulence

19
Q

Engine Starter Duty Cycle (normal starts) – limit the first start attempt to a maximum of _____.

A

2 minutes

20
Q

Intentional use of reverse thrust in flight is _____.

A

prohibited

21
Q

Maximum altitude for APU operation with electrical loads only is _____ feet.

A

41000’

22
Q

Maximum altitude for APU operation with bleed loads only is _____ feet.

A

17000’

23
Q

Maximum operating altitude for the APU is _____ feet.

A

41000’

24
Q

Maximum altitude for APU operation with both bleed and electrical loads is _____ feet.

A

10000’

25
Q

APU bleed valve may be open during engine start, but avoid engine power _____ .

A

above idle

26
Q

Maximum flap extension altitude is _____ feet.

A

20000

27
Q

Do not deploy speedbrakes in flight at radio altitudes less than _____ feet.

A

1000

28
Q

Random fuel imbalance must not exceed ________ lbs for taxi”,” takeoff”,” flight or landing.

A

1000

29
Q

Minimum fuel temperature is ____ degrees C unless the actual fuel freeze point is known.

A

-37

30
Q

(Ground operation) DO NOT turn Center Tank Fuel pumps ON unless center tank fuel quantity exceeds _____ lbs.”,” except when defueling or transferring fuel.

A

1000

31
Q

Operating Electric Hydraulic Pumps on the ground requires a minimum of ______ lbs of fuel in the respective tank.

A

1675

32
Q

The minimum takeoff and landing temperature (C) is:

A

-54