Limitations - Memorize

Question 1

Operational Limitations

Maximum Takeoff and Landing Tailwind Component

Answer 1

15 knots

Question 2

Operational Limitations

Maximum Operating Altitude

Answer 2

43,100 ft pressure altitude

Question 3

Operational Limitations

Turbulent Air Penetration Speed

Answer 3

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

290 KIAS below 25,000 feet

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

Question 4

Operational Limitations

Do not operate HF radios when

Answer 4

refueling

Question 5

Operational Limitations

Non-AFM Operational Information

Answer 5

Do not operate the weather radar in a hangar or when personnel are within the area normally enclosed by the aircraft nose radome. Do not operate the weather radar within 50 feet of fueling operations or fuel spills.Note:.

Note: The hangar restriction does not apply to the weather radar test mode.

Question 6

Autopilot/Flight Director System

The autopilot must not be engaged below a minimum engage altitude of

Answer 6

200 feet AGL after takeoff.

Question 7

Autopilot/Flight Director System

Autoland capability may only be used for operations into runways at or below ______

Answer 7

8400 feet airport field elevation.

Question 8

Autopilot/Flight Director System

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

Answer 8

100 feet AGL.

Question 9

Maximum wind component speeds when takeoff weather minima are predicated on HUD takeoff operations:

Headwind

Answer 9

25 knots

Question 10

Maximum wind component speeds when takeoff weather minima are predicated on HUD takeoff operations:

Tailwind

Answer 10

15 knots

Question 11

Maximum wind component speeds when takeoff weather minima are predicated on HUD takeoff operations:

Crosswind

Answer 11

15 knots

Question 12

Maximum wind component speeds when performing autoland operations (may be limited by visibility or runway condition):

Headwind

Answer 12

25 knots

Question 13

Maximum wind component speeds when performing autoland operations (may be limited by visibility or runway condition):

Tailwind

Answer 13

15 knots

Question 14

Maximum wind component speeds when performing autoland operations (may be limited by visibility or runway condition):

Crosswind

Answer 14

25 knots

Question 15

The maximum glide slope angle is _______.

The minimum glide slope angle is _______.

Answer 15

3. 25 degrees
4. 5 degrees

Question 16

Oil temperature must be greater than _______ for engine start.

Answer 16

-40° C

Question 17

Intentional selection of reverse thrust in flight is ________.

Backing the airplane with use of reverse thrust is _________.

Answer 17

prohibited

prohibited

Question 18

Avoid rapid and large _______ _______ _______, 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 18

alternating control inputs

Question 19

Do not extend flaps above ________ .

Answer 19

20,000 feet