Net Take Off Flight Path

Question 1

For a two engine aircraft with a critical engine failure, the gross takeoff performance is reduced by .%

Answer 1

0.8

Question 2

For a three engine aircraft with a critical engine failure, the gross takeoff performance is reduced by .%

Answer 2

0.9

Question 3

For a four engine aircraft with a critical engine failure, the gross takeoff performance is reduced by _%

Answer 3

1

Question 4

The first segment begins at ___

Answer 4

screen height. 35ft, 15ft when wet.

Question 5

The first segment ends at ___

Answer 5

gear up

Question 6

The speed maintained during the first segment is V_

Answer 6

V2

Question 7

The first segment requires a ___ climb gradient for 2 engine aircraft

Answer 7

positive

Question 8

The first segment requires a climb gradient of at least .% for 3 engine aircraft

Answer 8

0.3

Question 9

The first segment requires a climb gradient of at least .% for 4 engine aircraft

Answer 9

0.5

Question 10

The second segment starts at ___

Answer 10

Gear retraction

Question 11

The second segment ends at ___

Answer 11

the altitude the aircraft is levelled off to begin flap retraction

Question 12

The second segment cannot (and therefore levelling off for flap rectration) cannot be any lower than ___ft AGL

Answer 12

400

Question 13

By the end of the second segment, the speeds you should have passed through are ___

Answer 13

V2, V3, V4

Question 14

Below 400ft, the only change in configuration which is allowed is the ___

Answer 14

landing gear retraction

Question 15

The second segment requires a .% gradient for 2 engine aircraft

Answer 15

2.4

Question 16

The second segment requires a .% gradient for 3 engine aircraft

Answer 16

2.7

Question 17

The second segment requires a _% gradient for 4 engine aircraft

Answer 17

3

Question 18

The second segment climb gradient is defined by ___

Answer 18

• Gear up
• Flaps for takeoff
• Engines at takeoff thrust
• Speed V2

Question 19

Outline the purpose of the third segment

Answer 19

The aircraft accelerates to flap/slat retraction speed at constant altitude, thereafter accelerating to final takeoff climb speed

Question 20

During the third segment, flaps are ___ and power is ___ to ___

Answer 20

retracted, reduced, max continuous

Question 21

The fourth segment involves a climb to ___ft

Answer 21

1500

Question 22

Outline the aircraft’s configuration in the fourth segment

Answer 22

Flaps retracted, Max Continuous power on one engine, the other secure.

Question 23

The third and fourth segment require a .% gradient for 2 engine aircraft

Answer 23

1.2

Question 24

The third and fourth segment require a .% gradient for 3 engine aircraft

Answer 24

1.5

Question 25

The third and fourth segment require a .% gradient for 4 engine aircraft

Answer 25

1.7

Question 26

The acceleration from Vfto to final en-route climb speed is done at the end of the ___ segment.

Answer 26

fourth

Question 27

The Net Takeoff Flight Path should clear all obstacles vertically by __ft and ___ft horizontally (___ft within the airport boundary)

Answer 27

35, 300, 200