Uploaded by John Benson

B737-NG limitations

NG limitations 10.5.19
These weights are for a “Typical 737-800”
Max Taxi weight: 156,000 lbs.
Max Takeoff weight: 155,500 lbs.
Max Landing weight: 144,000 lbs.
Max Zero Fuel weight: 136,000 lbs.
The maximum takeoff and landing tailwind component is 10 knots.
Use of aileron trim with the autopilot is prohibited.
Do not engage the autopilot for takeoff below 400 feet AGL.
For single channel operation during approach, the autopilot shall not
remain engaged below 50 feet AGL.
Maximum and minimum glideslope angles for autoland are 3.25o and 2.5o respectively.
Autoland may only be used with flaps 30 or 40 and both engines operative.
Do not use LVL CHG on final approach below 1000 feet AFE .
Intentional selection of reverse thrust in flight is prohibited.
APU Inflight – Bleed + electrical load: max alt 10,000 ft.
APU Ground only – Bleed + electrical load: max alt 15,000 ft.
APU Bleed: max alt 17,000 ft.
APU electrical load: max alt 41,000 ft.
The maximum altitude with flaps extended is 20,000 ft.
Holding in icing conditions with flaps extended is prohibited.
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.
Do not deploy the speedbrakes in flight at radio altitudes less than 1,000 feet.
Avoid weather radar operation in a hangar, or within 50 feet (15.25 meters)
of fueling operations or a fuel spill.
Do not operate HF radios during refueling operations.