Operational Limitations

Question 1

Maximum Takeoff and Landing Tailwind Component

Answer 1

10 knots

Question 2

Maximum Operating Altitude

Answer 2

43,100 feet pressure altitude

Question 3

Maximum Takeoff and Landing Altitude

Answer 3

8,400 feet pressure altitude

Question 4

Turbulent Air Penetration Speed: (in severe turbulence) is defined as:

Answer 4

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 5

The maximum demonstrated takeoff and landing crosswind is?

Answer 5

38 knots

Question 6

Do not operate HF radios during?

Answer 6

Refuelling operations.

Question 7

Do not operate the weather radar in?

Answer 7

a hangar or within 50 feet of any fuel spill.

Question 8

Runway slope

Answer 8

+/- 2%

Question 9

For ground operation (exclusive of takeoff) in tailwinds and crosswinds between 30 and 45 knots, engine power

Answer 9

should be limited to a maximum of 70% N1.

Question 10

Avoid thrust levels above that required for normal taxi operation

Answer 10

in all tailwinds and crosswinds greater than 45 knots.

Question 11

The APU’s starter motors duty cycle for the electric starter motor and air turbine starter is 3 starts attempts in a 60 minute period each. APU start cycle restrictions are:

Answer 11

Electric Starter Motor Wait
Between Startd1 and 2
1 minute
Between Starts 2 and 3
1 minute

Air Turbine Starter Wait
Between Starts 1 and 2
1 minute
Between 2 and 3
1 minute

Question 12

ADIRU alignment must not be attempted

Answer 12

at latitudes greater than 78 degrees, 14.75 minutes.

Question 13

A QFE altitude reference for the primary flight displays must be

Answer 13

selected in the flight management system whenever QFE is used instead of QNH.