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Alaska Boeing 737 MAX > Boeing 737 Limitations > Flashcards

Boeing 737 Limitations Flashcards

1
Q

OPERATIONAL LIMITATIONS Maximum Takeoff Tailwind Component (AFM)

A

15 kts

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2
Q

OPERATIONAL LIMITATIONS
Maximum Landing Tailwind Component (AFM)

A

15 kts

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3
Q

OPERATIONAL LIMITATIONS
Maximum Operating Altitude (ft)

A

41,000

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4
Q

OPERATIONAL LIMITATIONS
Maximum Takeoff and Landing Altitude

A

8,400

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5
Q

OPERATIONAL LIMITATIONS
Minimum Takeoff and Landing Temperature

A

minus 54 C

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6
Q

AIRSPEED
Maximum Operating Limit (AFM)

A

Observe Vmo/Mmo and Gear/Flap Placards

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7
Q

AIRSPEED
Maximum Operating Limit (AFM)

A

Observe Vmo/Mmo and Gear/Flap Placards

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8
Q

AIRSPEED
Severe Turbulence Penetration Target Speed

A

280 KIAS/.76M*

*Whichever is lower

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9
Q

AIR
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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10
Q

ANTI-ICE, RAIN
When must the engine anti-ice system be ON?

A

During all ground and flight operations when icing conditions exist or are anticipated, except during climb and cruise below -40C SAT.
Engine anti-ice must be ON prior to and during descent in all icing conditions, including temperatures below -40C SAT.

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11
Q

ANTI-ICE, RAIN
(MAX) When must engine anti-ice be turned OFF?

A

When not in actual or anticipated icing conditions

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12
Q

AUTOMATIC FLIGHT
Do not engage the autopilot below ________ AGL on _______

A

1,000 ft, takeoff (AFM/ASA)

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13
Q

AUTOMATIC FLIGHT
For single channel operation during approach, the autopilot shall not remain engaged below______ (AFM).

A

50 ft AGL

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14
Q

AUTOMATIC FLIGHT
For manually flown HGS AIII approach, the autopilot shall not remain engaged below _________.

A

500 ft AGL.

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15
Q

AUTOMATIC FLIGHT
Use of aileron trim with the autopilot engaged is _________

A

prohibited. (AFM)

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16
Q

ENGINES, APU
Warm-up: Engines must be operated for a minimum of ________ prior to takeoff (ASA)

A

3 minutes

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17
Q

ENGINES, APU
Cool-down: Engines must be operated at or near idle (taxi thrust acceptable) for a minimum of ________ prior to shutdown (ASA)

A

3 minutes

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18
Q

ENGINES, APU
Maximum Time Limit for Takeoff Thrust
(AFM)

A

5 minutes*

*10 minutes allowed in the event of the loss of thrust on one engine during takeoff

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19
Q

ENGINES, APU
ENGINE START switches must be in the CONT position for: ______ ______ ______ _______
(AFM/ASA)

A
  • Anti-ice operation
  • Landing
  • Operation in hail, sleet, or moderate to heavy rain
  • Takeoff
    (ALOT)
20
Q

ENGINES, APU
ENGINE START switches must be in the FLT position for: ______________

A

Operation in severe turbulence

21
Q

ENGINES, APU
Minimum Oil Temperature before setting takeoff thrust

A

NG = No minimum
MAX = 31C

22
Q

ENGINES, APU
Intentional selection of reverse thrust in flight is _____________. (AFM)

A

prohibited.

23
Q

ENGINES, APU
Max altitude for Bleed and Electric Load on APU?

A

10,000’

24
Q

ENGINES, APU
Max altitude for Bleed only Load on APU?

A

17,000’

25
Q

ENGINES, APU
Max altitude for Electric only Load on APU?

A

41,000’

26
Q

ENGINES, APU
Max operating altitude for APU?

A

41,000’

27
Q

ENGINES, APU
Ensure APU BLEED air switch is _________ for ____ _________ after start

A

closed, 2 minutes

28
Q

ENGINES, APU
Ensure APU BLEED air switch is _________ for ____ _________ prior to shutdown

A

closed, 1 minute

NOTE: When the APU switch is moved to OFF, this delay is met automatically

29
Q

ENGINES, APU
APU bleed valve may be _______ during engine start, but avoid ______ ________ _______

A

open, engine power above idle.

30
Q

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

A

closed

31
Q

FLIGHT CONTROLS
Maximum flap extension altitude (AFM)

A

20,000’

32
Q

FLIGHT CONTROLS
Holding in icing conditions with flaps extended is __________

A

prohibited.

33
Q

FLIGHT CONTROLS
Do not deploy speed brakes in flight below __________ ft AGL.

A

1,000

34
Q

FLIGHT CONTROLS
In flight, do not extend the SPEED BRAKE lever beyond __________ ___________ (AFM)

A

the FLIGHT DETENT.

35
Q

FLIGHT CONTROLS
Do not deploy the speed brakes with more than flaps___ ___________.

A

10 extended *
Although not prohibited, the use of speed brakes with Flaps 1-10 extended should be avoided as much as possible.

36
Q

FLIGHT CONTROLS
700W/900ER
Manually overriding the Load Alleviation System is _____ _____________.

A

not authorized.

37
Q

FUEL
Minimum fuel temperature

A

-37 C, unless actual fuel freeze point is known

38
Q

FUEL
Allowable lateral imbalance between Main Tanks 1 & 2 must be _______ _________

A

scheduled to be zero.

39
Q

FUEL
Fuel imbalance must not exceed __________ for ________, _________, ________, or __________. (AFM)

A

1,000 lbs, taxi, takeoff, flight, landing.

40
Q

FUEL
Main Wing Tanks must be scheduled to be _______ if the Center Tank contains more than __________. (AFM)

A

full, 1,000 lbs.

41
Q

FUEL
For ground operations, Center Tank FUEL PUMP switches must not be positioned to ______ unless __________

A

ON, the Center Tank fuel quantity exceeds 1,000 lbs, except when defueling or transferring fuel.

42
Q

FUEL
Center Tank Fuel Pumps must not be ON unless ______________

A

personnel are available in the Flight Deck to monitor LOW PRESSURE lights.

43
Q

FUEL
For ground and flight operations, the corresponding Center Tank Fuel Pump switch must be positioned ______ when the LOW PRESSURE light illuminates

A

OFF

44
Q

FUEL
For ground and flight operations, if the Center Tank is empty, position both Center Tank FUEL PUMP switches to _______. (AFM/ASA)

A

OFF

45
Q

HYDRAULICS
Ground operation of electric hydraulic pump requires minimum of _________ in respective fuel tank.

A

1675 lbs

Alaska Boeing 737 MAX (18 decks)

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