Aborted Engine Start L, R
Airspeed Unreliable
[] CABIN ALTITUDE
Dual Eng Fail / Stall
[] ENG AUTOSTART L, R
Eng Lim / Surge / Stall L, R
Eng Svr Damage / Sep L, R
[] FIRE ENG L, R
[] STABILIZER
Maximum Takeoff and Landing Tailwind Component
15 knots
Severe Turbulent Air Penetration Speed
HF Radio
Do not operate HF radios during refueling operations.
Weather radar
Avoid weather radar operation in a hangar.
Autopilot minimum engage altitude
200 feet AGL after takeoff
Autopilot must be disengaged…
Below 200 feet AGL, without LAND 2 or LAND 3 annunciated.
Maximum allowable wind speeds (including gusts) on autoland operations
Maximum and minimum glideslope angle for Automatic Landing:
Maximum - 3.25° degrees
Minimum - 2.5° degrees
FLCH on final approach
Do not use it below 1,000 feet AFE
Reverse Thrust limitations…
Control inputs (AFM Limitations)
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.
Maximum altitude with flaps extended
20,000 feet
Minimum oil quantity limit
No minimum (FCTM Chapter 8)
Condition statement for Eng Lim/Surge/Stall non-normal checklist
One or more of these occur: