Limit Flashcards

1
Q

Flight Maneuvering load acceleration

A

Flaps up………………. +2.5 to -1

Flaps down………….. +2 to 0

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2
Q

Maximum takeoff and landing tailwind component

A

15 knots

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3
Q

Max Operating Alt

A

41,000

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4
Q

Maximum Takeoff and Landing Alt

A

8400

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5
Q

Minimum Takeoff and landing temp

A

-54 C

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6
Q

Maximum Operating Limit Speed

A

Observe Vmo/Mmo and gear/flap placards

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7
Q

Severe turbulence penetration speed

A

280/.76 (whichever is lower)

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8
Q

When BLEED air switches are on…

A

Don’t operate packs in HIGH for takeoff, approach or landing

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9
Q

When icing conditions exist on ground or flight…

A

Engine Anti-Ice must be on. Except during climb and cruise if it is below -40C SAT. Prior to descent engine anti-ice must be on in icing conditions including temps below -40C SAT.

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10
Q

Do not engage the autopilot below ________ AGL on takeoff

A

1000 ft

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11
Q

For single channel operation during approach, the autopilot shall not remain engaged below ______ AGL.

A

50 ft

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12
Q

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

A

500 ft.

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13
Q

Use of _______ ______ with autopilot engaged is prohibited.

A

Aileron trim

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14
Q

Maximum time limit for takeoff thrust

A

5 minutes (10 mins if single engine during takeoff)

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15
Q

ENGINE START switches must be in the CONT position for

A

Takeoff, Landing, Anti-Ice operation, hail, sleet or moderate to heavy rain

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16
Q

ENGINE START switches must be in the FLT position for

A

Severe turbulence

17
Q

Minimum oil temp before setting takeoff thrust on the MAX?

A

31C

18
Q

Intentional selection of reverse thrust in flight is _________.

A

Prohibited.

19
Q

The APU can supply bleed and Electrics up to _________ ft.

A

10,000

20
Q

The APU can provide bleed only up to _______.

A

17,000

21
Q

The APU can provide electric only up to _______.

A

41,000

22
Q

Max operating altitude for the APU?

A

41,000

23
Q

Ensure that APU BLEED switch is closed for ___ minutes after start and ___ minute prior to shutdown.

Note: When the APU switch is moved to OFF, this time delay is met mechanically. APU bleed valve may be open during engine start, but avoid engine power above idle. Except for engine start, the APU bleed valve must be closed when another source is pressurizing the left bleed air duct.

A

2, 1

24
Q

Maximum flap extension altitude

A

20,000

25
Q

Holding in icing conditions with flaps extended is

A

Prohibited

26
Q

Do not deploy speed brakes in flight below _____ AGL.

A

1,000 ft

27
Q

In flight, do not extend the speed brake lever beyond the _____ detent.

A

Flight

28
Q

Do not deploy speed brakes with more than flaps ____ extended.

A

10

29
Q

Can you override the LOAD ALLEVIATION SYSTEM?

A

No

30
Q

Minimum fuel temperature

A

-37C (unless fuel freeze point is known)

31
Q

To operate electric hydraulic pumps on the ground you must have _____ lbs in respective fuel tank.

A

1675

32
Q

Center tank fuel pumps must not be on unless…

A

personnel in flight deck monitor LOW PRESSURE lights.

33
Q

On ground, center tank FUEL PUMP switches can’t be turned on unless center tank exceeds ______ lbs.

A

1000 (except when defueling or transferring fuel)

34
Q

When LOW PRESSURE light illuminates

A

Center tank fuel pumps must be off. If center tank is empty, position both center tank fuel pump switches to OFF.

35
Q

Allowable lateral imbalance from Main Tank 1 and 2 must be scheduled to be____.

A

Zero

36
Q

Transient fuel imbalance must not exceed ______ lbs for taxi, takeoff, flight, or landing

A

1000

37
Q

Main Wing Tanks must be scheduled to be full if ____________.

A

Center Tank contains more than 1000 lbs.