Limitations -300ER (# items)

Question 1

Maximum Takeoff and Landing Tailwind Component

Answer 1

15 Knots

Note: The capability of the airplane has been satisfactorily demonstrated for takeoff and landings with tailwinds up to 15 knots. This does not constitute operational approval to conduct takeoffs and landings with tailwind components in excess of 10 knots.

Question 2

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

Answer 2

• 270 knots below 25,000 feet;
• 280 knots or 0.82 Mach whichever is lower at 25,000 feet and above.

Maintain a minimum speed of 15 knots above the minimum maneuvering speed at all altitudes when airspeed is below 0.82 Mach.

Question 3

Do not operate ______________ during refueling operations.

Answer 3

HF Radios

Question 4

Avoid ___________________ in a hangar.

Answer 4

weather radar operation

Question 5

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

Answer 5

200ft AGL

Question 6

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

Answer 6

200ft AGL

Question 7

Automatic Landing

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

Answer 7

Headwind: 25 knots
Crosswind: 25 knots
Tailwind: 10 knots

Question 8

Automatic Landing

The maximum glideslope angle is ______ degrees.

Answer 8

3.25

Question 9

Automatic Landing

The minimum glideslope angle is ______ degrees.

Answer 9

2.5

Question 10

Do not use FLCH on final approach below ____________.

Answer 10

1,000 feet AFE

Question 11

What AFM limitations should we observe regarding reverse thrust operations?

Answer 11

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

Question 12

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

Answer 12

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 V A .

Question 13

The maximum altitude with flaps extended is ___________.

Answer 13

20,000 feet