Class B Limitations

Question 1

At the planning stage, the minimum climb gradient is assumed to be ___ft/min AEO

Answer 1

300

Question 2

When a stopway/clearway is unavailable, the unfactored takeoff distance x _.__ may not exceed the TORA.

Answer 2

1.25

Question 3

When a stopway/clearway is available, the unfactored takeoff distance x _.__ may not exceed the TORA.

Answer 3

1.00

Question 4

When a stopway/clearway is available, the unfactored takeoff distance x _.__ may not exceed the ASDA.

Answer 4

1.30

Question 5

When a stopway/clearway is available, the unfactored takeoff distance x _.__ may not exceed the TODA.

Answer 5

1.15

Question 6

During the take off climb, you need to vertically avoid obstacles along the takeoff path which cannot be avoided visually by __ft, __ft if you bank more than 15 degrees

Answer 6

35, 50

Question 7

The aeroplane must clear all obstacles vertically by at least __ft

Answer 7

50

Question 8

The aeroplane must clear all obstacles horizontally by at least ___

Answer 8

90m + ( D / 8 )

Question 9

For aircraft with a wingspan of less than 60m, the aeroplane must clear all obstacles horizontally by at least ___

Answer 9

60m + ( wingspan / 2 ) + ( D / 8 )

Question 10

The take off flight path begins at __ft above the end of the TODR, and ends at ___ft above the surface

Answer 10

50, 1500

Question 11

The aeroplane is not banked prior to reaching __ft above the surface, and then not more than __ degrees

Answer 11

50, 15

Question 12

Failure of the critical engine occurs on the AEO takeoff flight path where ___

Answer 12

visual reference for avoiding obstacles is expected to be lost

Question 13

The gradient of the takeoff flight path from 50ft to the assumed engine failure height is equal to the average AEO gradient during the climb and transition to the enroute configuration, multiplied by _.__

Answer 13

0.77

Question 14

With track changes of no more than 15 degrees, you do not need to consider obstacles with a lateral distance of greater than __m if navigational accuracy can be maintained, ___m otherwise

Answer 14

300, 600

Question 15

Multi-engine aeroplanes, with one engine failed, must be able to fly to __ft above a suitable aerodrome, assuming a rate of climb of __fpm.

Answer 15

1000, 300

Question 16

The enroute climb gradient of a multi-engine aeroplane with one engine out must be the gross of descent of climb increased or decreased by _% respectively.

Answer 16

0.5

Question 17

Single engine aeroplanes must always be able to reach a place where a safe forced landing can be made, assuming a ROC of at least ___fpm can be maintained and the enroute gradient is the gross increased by __%

Answer 17

300, 0.5