Limitations (Required) (#)

Question 1

Maximum T/O and Landing Tailwind Component

Answer 1

15 Knots

Question 2

HF use when refueling

Answer 2

Do not operate HF radios when refueling.

Question 3

Severe Turbulent Air Penetration Speed

Answer 3

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

Question 4

Wx Radar use

Answer 4

Avoid weather radar operation in a hangar.

Question 5

Autopilot/Flight Director System

Answer 5

• The autopilot must not be engaged below a minimum engage altitude of 200 feet AGL after takeoff
• Autoland capability may only be used for operations into runways at or below 8400 feet airport field elevation
• Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below 100 feet AGL
• With LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25 degrees, the autopilot must be disengaged below 100 feet AGL.

Question 6

Low Visibility (HUD) Takeoff

Answer 6

Headwind - 25 knots
Tailwind - 15 knots
Crosswind - 20 knots

Question 7

Automatic Landing

Answer 7

Headwind - 25 knots
Tailwind - 15 knots
Crosswind - 25 knots

• The maximum glideslope angle is 3.25 degrees
• The minimum glideslope angle is 2.5 degrees

Question 8

Lowest Altitude to use FLCH?

Answer 8

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

Question 9

Engine Oil System

Answer 9

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

Question 10

Reverse Thrust

Answer 10

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

Question 11

Flight Controls

Answer 11

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.