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ASA B737 Systems > Limitations > Flashcards

Limitations Flashcards

1
Q

Maximum Tailwind for Takeoff and Landing

A

15kts

Gusts are not controlling, however steady state winds near the limits with higher gusts should be considered unacceptable.

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2
Q

Maximum Dry Runway Wind Limits

A

Steady state: 50kts

Gust component: 20kts

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3
Q

Maximum Crosswind for Takeoff (dry runway)

A

40kts (700)
34kts (9MAX)
33kts (800/900)

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4
Q

Maximum Crosswind for Landing (Braking Action Good)

A

40kts (700/9MAX)

37kts (800/900)

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5
Q

Maximum Operating Altitude

A

41,000ft

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6
Q

Maximum Altitude for Takeoff and Landing

A

8,400ft

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7
Q

Minimum Temperature for Takeoff and Landing

A

-54C

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8
Q

Maximum Operating Speed

A

Vmo/Mmo or gear/flap placards as appropriate

Vmo is 340kts, Mmo is 0.82M

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9
Q

Severe Turbulence Penetration Target Speed

A

280 KIAS / .76M

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10
Q

With Either or Both Engine Bleed Air Switches ON, do not operated the Packs in what mode?

A

Do not operate AC Packs in HIGH for Takeoff, Approach, or Landing

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11
Q

Engine Anti-Ice Limitation

A

Must be ON during all ground/flight operations when icing conditions exist or are anticipated.

Exception: climb or cruise below -40C SAT

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12
Q

Wing Anti-Ice Limitation

A

Do not operate on the ground with OAT above 10C

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13
Q

Minimum Height for Autopilot Engagement on Takeoff

A

1,000ft AGL

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14
Q

Minimum Height for Autopilot Use on Approach in Single Channel

A

50ft AGL

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15
Q

Minimum Height for Autopilot Use on Approach for Manually Flown HGS AIII

A

500ft AGL

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16
Q

Aileron Trim with Autopilot Engaged is

A

Prohibited

17
Q

Do Not Operate HF Radios, when?

A

Refueling or either aft door open.

18
Q

Engine Warm up/Cool down Time

A

3 minutes

MAX minimum oil temp for takeoff is 31C

19
Q

Maximum Time for Takeoff Thrust

A

5 minutes

10 minutes if OEI on takeoff

20
Q

Maximum Start EGT

A

NG: 725C

MAX: 753C (883C for air start)

21
Q

Engine Ignition in CONT for

A

Takeoff
Landing
Icing
Hail, sleet, moderate to heavy rain

22
Q

Engine Ignition in Severe Turbulence

A

Flight

23
Q

Starter Duty Cycle

A

First attempt:

NG: 2 minutes

MAX: 3 minutes

Subsequent attempts refer to manual

24
Q

Assumed Temperature Thrust Reduction Limits

A

Wind shear

Contaminated Runway

27k bump thrust (800)

Headwind weight adjustment

MEL

25
Q

Reverse Thrust In-Flight

A

Intentional Selection In Flight Prohibited

26
Q

APU Altitude Limitations

A

41,000ft - Max operating

41,000ft - Electric

17,000ft - Bleed

10,000ft - Bleed and Electric

27
Q

APU Bleed Limitation

A

Closed for 2 minutes after start (ASA) and 1 minute prior to shutdown

(Shutdown limit is met automatically by APU OFF)

APU Bleed must be closed with another Bleed source except for start.

Bleed valve may be open for engine start but avoid engine power above idle

28
Q

Maximum Flap Extension Altitude

A

20,000 ft

29
Q

When is Holding with Flaps Extended Prohibited?

A

Prohibited in Icing Conditions

30
Q

Speed Brake Limitations

A

Do not deploy speed brakes with flaps extended beyond 10*, although avoid if possible (ASA)

Do not deploy speed brakes below 1,000 ft AGL

In fight, do not deploy the SPEED BRAKE lever beyond the FLIGHT DETENT.

31
Q

Load Alleviation System Limitation

A

Manual override is prohibited (700W/900ER)

32
Q

Minimum Fuel Temperature

A

-37C unless the actual fuel freeze point is known. (ASA)

Minimum fuel temperature is the higher of -43C or fuel freeze point + 3C.

33
Q

Fuel Imbalance Limitations

A

Must be scheduled to be zero.

Random fuel imbalance must not exceed 1,000lbs for taxi, takeoff, flight, or landing.

34
Q

Center Tank Fuel Limitations

A

Main wing tanks must be scheduled to be full if the center tank contains more than 1,000lbs, except when defueling or transferring fuel.

Center tank fuel pumps must not be ON unless personnel are available in the flight deck to monitor low pressure lights.

Center tank fuel pump switch must be OFF when the LOW PRESSURE light illuminates. If the center tank is empty, both center tank fuel pump switches must be OFF.

35
Q

Hydraulic Pump Limitation

A

Ground operation of electric hydraulic pump requires a minimum of 1,675lbs of fuel in the respective tank. (does not apply after landing)

36
Q

Minimum Oil Temperature for Takeoff

A

31C (9MAX only)

37
Q

Maximum T/O EGT

A

NG: 950 C

MAX: 1038C

ASA B737 Systems (16 decks)

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