787 Limitations

Question 1

MAXIMUM OPERATING PRESSURE ALTITUDE

787-8, 787-9

Answer 1

43,100

Question 2

MAXIMUM OPERATING PRESSURE ALTITUDE

787-10

Answer 2

41,100

Question 3

MAXIMUM TAKEOFF AND LANDING TAILWIND COMPONENT

Answer 3

15 knots

Question 4

TURBULENT AIR PENETRATION SPEED

At and above FL250

Answer 4

310/.84

Question 5

TURBULENT AIR PENETRATION SPEED

Below FL250

Answer 5

290

Question 6

MAX TAKEOFF LANDING CROSSWIND COMPONENT

Answer 6

40knots

Question 7

ICING CONDITIONS DEFINITION

Answer 7

Icing conditions exist when OAT (ground) or TAT (flight) is 10°C or below.

Question 8

Do not engage the autopilot below a minimum engagement altitude of
***feet AGL after takeoff

Answer 8

200

Question 9

Autoland capability may only be used for operations to runways at or
below ***feet airport field elevation

Answer 9

8400

Question 10

Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged
below *** feet AGL.

Answer 10

135

Question 11

With LAND 2 or LAND 3 annunciated and glideslope angles greater than
3.25°, the autopilot must be disengaged below *** feet AGL.

Answer 11

100

Question 12

Do not use FLCH on final approach below ** feet AFE.

Answer 12

1000

Question 13

LOW VISIBILITY (HUD) TAKEOFF (RVR <500)
HW
TW
XW

Answer 13

25
15
15

Question 14

ILS AUTOMATIC LANDING
HW
TW
XW

Answer 14

25
15/10 CATIII
25/15 CATIII

Question 15

ILS AUTOMATIC LANDING
GLIDE -SLOPE ANGLE
MAX
MIN

Answer 15

3. 25

2. 50

Question 16

Oil Quantity

Minimum prior to start

Answer 16

18 quarts

Question 17

Oil temperature must be greater than -**C for engine start.

Answer 17

-40°

Question 18

�Intentional selection of reverse thrust in flight is prohibited.
�Backing the aircraft with use of reverse thrust is prohibited.

Answer 18

�Intentional selection of reverse thrust in flight is prohibited.
�Backing the aircraft with use of reverse thrust is prohibited.

Question 19

�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.

Answer 19

�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.

Question 20

TIRE – MAXIMUM SPEED
Takeoff
Landing

Answer 20

204

226