787 Limitations Flashcards
Maximum altitude 787 8/9
43,100 feet
Maximum altitude 787 10
41,100 feet
Maximum Takeoff and Landing Tailwind Component
15 Knots
Turbulent Air Penetration Speed
Severe Turbulence at and above 25,000 ft = 310/.84 Mach whichever is lower
Severe Turbulence below 25,000 feet = 290 knots
Takeoff Crosswind 8/9/10
40 knots
Landing Crosswinds Guideline
40 knots
Slide slip not recommended > 25 knots
Icing Conditions Definition
Icing conditions exist when OAT (ground) or TAT (flight) is 10°C or below.
Do not engage the autopilot below a minimum engagement altitude of_____ft AGL after takeoff
200
Autoland capability may only be used for operations to runways at or below________feet AFE
8400
Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below _____ feet AGL.
135
With LAND 2 or LAND 3 annunciated and glide slope angles greater than 3.25°, the autopilot pilot must be disengaged below _____ feet AGL.
100
Do not use FLCH on final approach below _____ feet AFE
1000
Maximum low visibility HUD takeoff wind components
Headwind 25 knots
Tailwind 15 knots
Crosswind 15 knots
ILS Automatic Landing maximum and minimum glideslope angle is:
Maximum 3.25°
Minimum 2.50°
Communication Limitations
Do not operate HF radio during fueling operations.
Minimum oil quantity prior to start
18 quarts
Minimum oil temperature
Greater than -40° C for engine start
Reverse thrust in flight
Is prohibited
Reverse Thrust for backing the airplane is
Prohibited
Flight Control Inputs
Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g.., large slip angles) as they may result in structural failure at any speed, including below VA.
