Limitations -8 (# items)

Question 1

The Maximum Takeoff and Landing Tailwind
Component for the 787-8 is…

Answer 1

15 knots

Question 2

Are HF radios allowed during refueling?

Answer 2

No. Do not operate HF radios when refueling.

Question 3

Severe turbulent air penetration speed (in severe turbulence) is defined as:

Answer 3

• 290 KIAS below 25,000 feet
• 310 KIAS/.84 Mach (whichever is lower) at and above 25,000 feet.

Question 4

Use of weather radar operation in a hangar…

Answer 4

Avoid weather radar operation in a hangar.

Question 5

The autopilot must not be engaged below a minimum engage altitude of ____ after takeoff.

Answer 5

200 feet AGL

Question 6

Autoland capability may only be used for operations into runways _________ airport field elevation

Answer 6

At or below 8400 feet

Question 7

Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged
below _______.

Answer 7

100 feet AGL

Question 8

With LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25
degrees, the autopilot must be disengaged below _______.

Answer 8

100 feet AGL.

Question 9

Low Visibility HUD Takeoff

Maximum wind component speeds when takeoff weather minima are predicated on HUD takeoff operations (headwind, crosswind, tailwind):

Answer 9

Headwind: 25kt
Crosswind: 20kt
Tailwind: 15kt

Question 10

Automatic Landing

Maximum wind component speeds when landing weather minima are predicated on autoland and CAT II/III operations (headwind, crosswind, tailwind):

Answer 10

Headwind: 25kt
Crosswind: 25kt
Tailwind: 10kt

Question 11

Automatic Landing

The maximum glideslope angle is ____ degrees.

Answer 11

3.25

Question 12

Automatic Landing

The minimum glideslope angle is ____ degrees.

Answer 12

2.5

Question 13

Do not use FLCH on final approach below _____.

Answer 13

1000 feet AFE

Question 14

Oil temperature must be greater than _____ for engine start.

Answer 14

-40° C

Question 15

What AFM limitations should we observe regarding the use of reverse thrust?

Answer 15

*Intentional selection of reverse thrust in flight is prohibited.
*Backing the airplane with use of reverse thrust is prohibited.

Question 16

What AFM limitation should we observe regarding the use of flight controls?

Answer 16

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.