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737 > 737 Limitations > Flashcards

737 Limitations Flashcards

1
Q

Maximum Takeoff Tailwind Component

A

15 KTS

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2
Q

Maximum Landing Tailwind Component

A

15 KTS

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3
Q

Maximum Operating Altitude

A

FL 410

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4
Q

Maximum Takeoff and Landing Altitude

A

8400’

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5
Q

Minimum Takeoff and Landing Temperature

A

-54 Celsius

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6
Q

Maximum Operating Speed Limit

A

Observe Vmo/Mmo and Gear/Flap Placards

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7
Q

Severe Turbulence Penetration Target Speed

A

280KIAS/.76 *Whichever is lower

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8
Q

With either one or both engine BLEED air switches on…

A

Do not operate air conditioning packs in HIGH for takeoff, approach, or landing.

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9
Q

When must the engine anti-ice system be ON

A

Must be ON during all ground and flight operations when icing conditions exist or are anticipated, except during climb and cruise below -40c SAT. Must be on prior to and during decent including temps below -40c

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10
Q

On takeoff do not engage the autopilot below?

A

1000’ AGL

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11
Q

For single channel operation during approach, the autopilot shall not remain engaged below?

A

50’ AGL

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12
Q

For manually flown HGS AIII approach, the autopilot shall not remain engaged below?

A

500’ AGL

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13
Q

Use of aileron trim with autopilot engaged is?

A

Prohibited

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14
Q

Maximum Time Limit for Takeoff Thrust

A

5 minutes *10 minutes allowed in the event of the loss of thrust on one 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
Operation in hail, sleet or moderate to heavy rain

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16
Q

ENGINE START switches must be in the FLT position for:

A

Operation in severe turbulence

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17
Q

Minimum Oil Temperature before setting takeoff thrust

A

737NG = NA
737MAX = 31c

18
Q

Intentional selection of reverse thrust in flight is?

A

Prohibited

19
Q

Bleed and APU Electrical Use

A

10,000’

20
Q

APU Bleed Use

A

17,000’

21
Q

APU GEN Use

A

FL 410

22
Q

APU Max Operating Altitude

A

FL 410

23
Q

Ensure APU BLEED air switch is closed for how many minutes after APU start?

A

2 minutes

24
Q

Ensure APU BLEED air switch is closed for how many minutes prior to APU shutdown?

A

1 minute

25
Q

APU bleed valve may be open during engine start?

A

True. But avoid engine power above idle

26
Q

Except for engine start, the APU bleed valve must be closed when another source is pressurizing the left bleed air duct.

A

True

27
Q

Maximum flap extension altitude is?

A

20,000’

28
Q

Holding in icing conditions with the flaps extended is?

A

Prohibited

29
Q

Do not deploy speed brakes in flight below

A

1000’ AGL

30
Q

In flight, do not extend the SPEED BRAKE lever beyond

A

The FLIGHT DETENT

31
Q

Do not deploy speed brakes with more than Flaps

A

10 extended

32
Q

Manually overriding the Load Alleviation System

A

Is not authorized

33
Q

Minimum fuel temperature is

A

-37c unless the actual fuel freeze point is known

34
Q

The allowable lateral fuel imbalance between Main Tanks 1 and 2 must be scheduled to be?

A

Zero

35
Q

Fuel imbalance must not exceed what for taxi, takeoff, flight or landing?

A

1000 lbs

36
Q

Main Wing Tanks must be scheduled to be full if the Center Tank contains more than

A

1000 lbs

37
Q

For ground operation, Center Tank FUEL PUMP must not be positioned to ON unless?

A

The Center tank fuel quantity exceeds 1000 lbs. Except when defueling or transferring fuel

38
Q

Center Tank Fuel Pumps must not be on unless

A

Personnel are available in the flight deck to monitor LOW PRESSURE lights

39
Q

For ground and flight ops, the corresponding Center Tank Fuel Pump switch must be positioned OFF when

A

The LOW PRESSURE light illuminates.

40
Q

If the center Tank is empty, position both Center Tank FUEL PUMP switches to

A

OFF

41
Q

Ground operation of the electric hydraulic pump requires how much fuel?

A

1675 lbs in respective fuel tank.

737 (18 decks)

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