Max operating pressure altitude
41,000 feet
Max takeoff/landing tailwind component
15 knots
Recommended Severe Turbulence Penetration Speed:
Cruise
Turb N1 setting from VNAV Cruise Page
Recommended Severe Turbulence Penetration Speed:
Climb and Descent
280 kts / .76 Mach
- Note: If severe turbulence is encountered at altitudes below 15,000 ft and the airplane’s gross weight is less than the maximum landing weight, the airplane may be slowed to 250 knots in the clean configuration.
Takeoff Crosswind Component (knots) split scimitar winglet:
Dry Runway (RCC 6)
33 knots
- Assumes an engine failure RTO
Takeoff Crosswind Component (knots) split scimitar winglet:
Wet Runway (RCC 5, 1/8” less RW containtment of water, snow, slush)
25 knots
- Assumes an engine failure RTO
Landing Crosswind Component (knots) split scimitar winglet:
Dry Runway
37 knots
Landing Crosswind Component (knots) split scimitar winglet:
Wet Runway (RCC 5, 1/8” less RW containtment of water, snow, slush)
37 knots
- Reduce landing crosswind guidelines by 5 knots on wet or contaminated runways when asymmetric reverse thrust is used
Icing conditions exist on the ground and for takeoff when:
OAT 10°C or below
&
- visible moisture in any forms present (I.e. Clouds, fog with visibility of 1 mile or less, rain, snow, sleet, or ice crystals) OR
- while operating on ramps,taxiways, or runways where snow, standing water or slush may be ingested by the engines or freeze on the engines, nacelles, or engine sensor probes.
Icing conditions exist in flight when:
Total Air Temp is 10°C or below
&
- visible moisture in any form is present ( i e clouds, fog with visibility of 1 mile or less, rain, snow, sleet, or ice crystals)
On takeoff or missed approach, do not engage autopilot below:
- 400 ft AGL (* per OpSpec C071)
- 800 ft AGL (old answer)
Autoland max headwind:
25 knots
Autoland max crosswind:
15 knots
Auto land max tailwind (flaps 30 and 40):
10 knots
————————————-
-900 Flaps 30:
Field elevation 4000 ft or less: 10 kts
Field elevation 4001-6000 ft: 5 kts
Field elevation 6000 ft and above: 0 kts
Minimum altitude for use of autopilot on approach
ILS/GPS coupled approach (no autoland):
50 ft AGL
Minimum altitude for use of autopilot on approach
Non-precision approaches:
50 feet below MDA/DA
Maximum flap extension altitude:
20,000 ft
Do not use LVL CHG on final approach below:
1000 ft AFE
