737 MAX Limitations

What’s the maximum runway slope. +/- 2%. +/- 2.5%. +/- 1.5%.

What’s Maximum Takeoff and Landing Tailwind Component?.

What’s Maximum Operating Altitude.

What’s Maximum Takeoff and Landing Altitude.

What’s Severe Turbulent Air Penetration speed for climb and descend?.

How can we determine the Severe Turbulent Air Penetration speed during cruise?.

Do not operate HF radios during refueling operations. True. False.

What’s The maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operations. 200 feet. 50 feet. 75 feet.

What’s the Max Difference Between Captain & F/O, allowable on-the-ground altitude display differences for RVSM operations from Sea Level to 5,000 feet. 60 feet. 75 feet. 50 feet.

What’s the Max Difference Between Captain or F/O & Field Elevation, allowable on-the-ground altitude display differences for RVSM operations from sea level to 10,000 feet. 60 feet. 75 feet. 50 feet.

What’s The maximum cabin differential pressure (relief valves).

Use of aileron trim with the autopilot engaged is prohibited. True. False.

For single channel operation during approach, the autopilot shall not remain engaged below 50 feet AGL. True. False.

Airplanes operating with FAA Rules: Maximum allowable wind speeds when landing weather minima are predicated on autoland operations: Headwind. 25. 20. 15.

Do not engage the autopilot for takeoff below 400 feet AGL. True. False.

Airplanes operating with FAA Rules: Maximum allowable wind speeds when landing weather minima are predicated on autoland operations: Crosswind. 25. 20. 15.

Airplanes operating with FAA Rules: Maximum allowable wind speeds when landing weather minima are predicated on autoland operations: Tailwind. 25. 20. 15.

Maximum glideslope angle for autoland is. 3.25 degrees. 2.5 degrees.

Minimum glideslope angle for autoland is. 3.25 degrees. 2.5 degrees.

Autoland capability may only be used with Flaps 30 or 40 and both engines operative. True. False.

Do not use LVL CHG on final approach below 1000 feet AFE. True. False.

Engine ignition must be on for: Take off. Landing. Operation in heavy rain. Anti-ice operation.

Intentional selection of reverse thrust in flight is prohibited. True. False.

APU bleed: Maximum altitude. 10,000 feet. 15,000 feet. 17,000 feet. 41,000 feet.

Airplanes operating under FAA Rules: Inflight - APU bleed + electrical load: 10,000 feet. 15,000 feet. 17,000 feet. 41,000.

Airplanes operating under FAA Rules: Ground only - APU bleed + electrical load. 10,000 feet. 15,000 feet. 17,000 feet. 41,000 feet.

APU electrical load: Maximum altitude. 10,000 feet. 15,000 feet. 17,000 feet. 41,000 feet.

The maximum altitude with flaps extended is 20,000 feet. True. False.

Holding in icing conditions with flaps extended is prohibited. True. False.

In flight, do not extend the speed brake lever beyond the FLIGHT detent. True. False.

Do not use speed brakes below 1000 feet above the surface. True. False.

In flight, do not extend the speedbrake lever beyond the ARMED detent with flaps 40 selected. True. False.

Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g., large side slip angles) as they may result in structural failure at any speed, including below VA. True. False.

Do not use the terrain display for navigation. True. False.

Avoid weather radar operation in a hangar. True. False.

Maximum tank fuel temperature is. 49. 50. 48.

Minimum tank fuel temperature prior to takeoff and inflight is.

Fuel imbalance between main wing tanks for taxi, takeoff, flight or landing must not exceed.

Main tanks 1 and 2 must be full if center tank contains more than.