Maximum Operating Pressure Altitude
787-8, 787-9 43,100 feet
787-10 41,100 feet
Max Takeoff/Landing Tailwind
15 knots
Turbulent Air Penetration Speed for Severe Turbulence
At or above FL250 310kts/.84 (whichever lower)
Below FL250 290 KIAS
Max Takeoff Crosswind Guidelines
CG </= 20 40 knots all models and weights
For CG>20 Reference Limitations
Max Landing Crosswind (Dry)
40 knots (however sideslip only ie: zero crab not recommended in excess of 25 knots)
Icing Conditions Definition
When OAT (ground) or TAT (flight) is 10 degrees C or below
Autopilot / FD limitations
- Do not engage the autopilot below 200’ AGL after takeoff
- Autoland capability only at runways at or below 8400’ field elevation
- Without LAND 2 or LAND 3 annunciated, autopilot must be disengaged by 135’ AGL
- With LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25 degrees, autopilot must be disengaged below 100’ AGL
- Do not use FLCH on final approach below 1000’ AFE
Low Vis (HUD) Takeoff (below 500’ RVR) limits:
Headwind 25 knots
Tailwind 15 knots
Crosswind 15 knots
SA CAT I approaches Max Crosswind
15 knots
ILS automatic landing glideslope angle limits:
Max glideslope angle 3.25 degrees
Minimum angles 2.50 degrees
Communications Limitation (memory items)
Do not operate HF radio during fueling operations
Minimum oil quantity prior to start?
18 quarts
Reverse Thrust limitations
- Intentional selection of reverse thrust in flight is prohibited
- Backing the airplane with use of reverse thrust is prohibited
Minimum oil temp prior to start
Greater than -40 degrees C
Control Inputs Limitation?
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
