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NEW Alaska B737 Systems > Limitations > Flashcards

Limitations Flashcards

1
Q

Maximum Tailwind for Takeoff and Landing

A

15 knots

*10 kts for takeoff on contaminated runway

*5 kts for landing IF BA < GOOD and LDA < 7,000’

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2
Q

Maximum Steady State and Gust Wind

A

Steady State - 50 knots

Gust - 20 knots

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3
Q

Maximum Takeoff Crosswind (dry runway)

A

700 - 40kts

8/900 - 33kts

MAX - 34kts

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4
Q

Maximum Takeoff Crosswind WET/BA GOOD

A

25 knots

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5
Q

Maximum Landing Crosswind (dry runway)

A

700 and MAX - 40 knots

800 and 900 - 37 knots

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6
Q

Maximum Operating Altitude

A

41,000’

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7
Q

Maximum Takeoff and Landing Altitude

A

8,400’

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8
Q

Minimum Temperature for Takeoff and Landing (max?)

A

Minimum -54C

Maximum +54C at sea-level

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9
Q

Maximum Operating Speed Limit

A

Vmo/Mmo and Gear/Flap placards

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10
Q

Severe Turbulence Penetration Target Speed

A

280 KIAS / .76M

Whichever is lower

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11
Q

When must the A/C packs not be in HIGH?

A

Takeoff, approach, and landing

If engine bleed(s) ON

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12
Q

When must EAI be on?

A

During all ground and flight operations when icing conditions exist or are anticipated

Except during climb/cruise below -40C SAT

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13
Q

Minimum altitude to engage autopilot

A

1,000’ AGL

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14
Q

Minimum altitude to leave autopilot engaged

A

50’ AGL for single-channel approaches

500’ AGL for hand-flown HGS AIII

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15
Q

Aileron trim with autopilot engaged?

A

Prohibited

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16
Q

Engine warm-up and cool-down time

A

3 minutes

31C oil temperature for 737MAX

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17
Q

Maximum time for takeoff thrust

A

5 minutes

Unless OEI then 10 minutes

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18
Q

Engine Start switches must be in CONT for

A

Takeoff

Landing

Anti-Ice operation

Rain (moderate to heavy), hail, and sleet

19
Q

Engine Start Switches must be in FLT for

A

Severe turbulence

20
Q

Minimum oil temperature before setting takeoff thrust

A

31C

MAX only

21
Q

Reverse thrust selection in-flight

A

Prohibited

22
Q

APU altitude limits

A

41,000’ - Operating and electrics
17,000’ - Bleed load
10,000’ - Bleed and electrical load

23
Q

APU Bleed warm-up/cool-down time

A

2 minutes for warm up

1 minute for cool down (automatically met)

24
Q

Maximum Flap Extension Altitude

A

20,000’

25
Q

Holding in icing conditions with flaps extended

A

Prohibited

26
Q

Minimum height for speed brake deployment in-flight

A

1,000’ AGL

27
Q

Maximum speed brake deployment position in-flight

A

FLIGHT DETENT

28
Q

Maximum flap position for speed brake deployment

A

Flaps 10

*Avoid with flaps extended if possible

29
Q

Load alleviation system

A

Manual override prohibited

30
Q

Maximum altimeter differences

A

50’ between CA and FO on the ground
75’ between CA or FO and field elevation
200’ in flight for RVSM

31
Q

Minimum fuel temperature (max?)

A

-37C

Unless fuel freeze point is known

Then freeze point +3C minimum -43C

(Maximum +49C)

32
Q

Maximum fuel imbalance between main tanks

A

Scheduled to be zero

Fuel imbalance must not exceed 1,000lbs for taxi, takeoff, flight, or landing

33
Q

How much fuel can be in the center tank if main tanks are less than full?

A

1,000lbs

Main tanks must be scheduled to be full if the Center Tank has more than 1,000lbs

34
Q

Center Tank Fuel Pump Limits

A

Must not be on unless personnel in flight deck to monitor LOW PRESSURE lights, and

Center fuel quantity must be > 1,000lbs to operate them on the ground, except for defueling or transferring fuel (also no pax onboard), and

Center fuel pump must be switched OFF when LOW PRESSURE light illuminates, intentional dry running of center fuel pump prohibited

35
Q

Minimum fuel quantity for ground operation of electric hydraulic pumps?

A

1,675lbs in respective main fuel tank

*does not apply after landing

36
Q

*Bleed duct pressure limits

A

60 psi - Max
18 psi - Min in-flight
15 psi - Min on the ground

Report differential > 20 psi to MX

Also, do not operate packs in HIGH for takeoff, approach, or landing

37
Q

*Cold soaked fuel frost

A

Up to 1/8” permitted on lower wing

Upper wing
-within the “box”
-OAT >= 4C
-Fuel temp >= -16C
-No precipitation or visible moisture

38
Q

*Assumed temperature thrust reduction

A

Prohibited for

-Windshear
-Contaminated runway
-MEL (antiskid, EEC ALTN, dual FMC inop)
-27k bump

39
Q

*Cargo door wind limits

A

Fully open up to 40 knots

CANOPY up to 65 knots

Lower door to CANOPY if door begins oscillating

40
Q

*Navigation performance scales

A

RNP < 0.3 - A/P or NPS required

RNP < 0.11 - NPS required

41
Q

*Starter duty cycle

A

NG - 2 min on
MAX - 3 min on

10 seconds off for second and subsequent attempts

42
Q

*Wing anti-ice

A

Do not use on the ground when OAT > 10C

Do not using on the ground AFTER deicing

43
Q

*Minimum in-flight temperature

A

-72C at FL350 (-73C at 410)

NEW Alaska B737 Systems (16 decks)

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