1. Limitations

Question 1

What is Maximum Takeoff and Landing Tailwind Component Limit?

Answer 1

10 knots (RX Limitation)

Question 2

What is the limitation regarding HF radios use?

Answer 2

Do not operate HF radios when refueling.

Question 3

What is Severe turbulence air penetration speed?

Answer 3

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

Question 4

What is the limitation regarding weather radar use?

Answer 4

Avoid weather radar operation in a hangar.

Question 5

What is the minimum altitude to engage the autopilot after T/O?

Answer 5

200’ ft.

Question 6

What is the maximum Autoland capability altitude?

Answer 6

8400’ ft.

Question 7

If LAND2 or LAND3 is not displayed, when must the Autopilot be disengaged?

Answer 7

Below 135’ ft. AGL.

Question 8

If the G/S angle is more than 3.25 and LAND2 or LAND3 displayed, when must the
Autopilot be disengaged?

Answer 8

Below 100’ ft. AGL.

Question 9

What are the wind limitations when a Low Visibility HUD T/O is conducted?

Answer 9

o Headwind 25 knots
o Tailwind 10 knots (RX Limitation)
o Crosswind 20 knots

Question 10

What are the Limitations when landing weather minimums are predicted on Autoland
operations?

Answer 10

o Headwind 25 knots
o Tailwind 10 knots (RX Limitation)
o Crosswind 25 knots

Question 11

What is the maximum glideslope angle when landing weather minimums are predicted
on Autoland operations?

Answer 11

The maximum glideslope angle is 3.25 degrees.

Question 12

What is the minimum glideslope angle when landing weather minimums are predicted
on Autoland operations?

Answer 12

The minimum glideslope angle is 2.5 degrees.

Question 13

What is the limitation regarding FLCH use?

Answer 13

Do not use FLCH on final approach below 1,000 feet AFE.

Question 14

What is the minimum Oil temperature for engine start?

Answer 14

Oil temperature must be greater than -40° C for engine start.

Question 15

What are the limitations regarding Reverse Thrust use?

Answer 15

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

Question 16

What are the limitations on alternating control inputs?

Answer 16

o 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.