787 Limitations Flashcards
1
MAXIMUM OPERATING PRESSURE ALTITUDE
787-8, 787-9
43,100
MAXIMUM OPERATING PRESSURE ALTITUDE
787-10
41,100
MAXIMUM TAKEOFF AND LANDING TAILWIND COMPONENT
15 knots
TURBULENT AIR PENETRATION SPEED
At and above FL250
310/.84
TURBULENT AIR PENETRATION SPEED
Below FL250
290
MAX TAKEOFF LANDING CROSSWIND COMPONENT
40knots
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
***feet AGL after takeoff
200
Autoland capability may only be used for operations to runways at or
below ***feet airport field elevation
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 glideslope angles greater than
3.25°, the autopilot must be disengaged below *** feet AGL.
100
Do not use FLCH on final approach below ** feet AFE.
1000
LOW VISIBILITY (HUD) TAKEOFF (RVR <500)
HW
TW
XW
25
15
15
ILS AUTOMATIC LANDING
HW
TW
XW
25
15/10 CATIII
25/15 CATIII
ILS AUTOMATIC LANDING
GLIDE -SLOPE ANGLE
MAX
MIN
- 25
2. 50
Oil Quantity
Minimum prior to start
18 quarts
Oil temperature must be greater than -**C for engine start.
-40°
�Intentional selection of reverse thrust in flight is prohibited.
�Backing the aircraft with use of reverse thrust is prohibited.
�Intentional selection of reverse thrust in flight is prohibited.
�Backing the aircraft with use of reverse thrust 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.
�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.
TIRE – MAXIMUM SPEED
Takeoff
Landing
204
226
