Net Take Off Flight Path Flashcards
For a two engine aircraft with a critical engine failure, the gross takeoff performance is reduced by .%
0.8
For a three engine aircraft with a critical engine failure, the gross takeoff performance is reduced by .%
0.9
For a four engine aircraft with a critical engine failure, the gross takeoff performance is reduced by _%
1
The first segment begins at ___
screen height. 35ft, 15ft when wet.
The first segment ends at ___
gear up
The speed maintained during the first segment is V_
V2
The first segment requires a ___ climb gradient for 2 engine aircraft
positive
The first segment requires a climb gradient of at least .% for 3 engine aircraft
0.3
The first segment requires a climb gradient of at least .% for 4 engine aircraft
0.5
The second segment starts at ___
Gear retraction
The second segment ends at ___
the altitude the aircraft is levelled off to begin flap retraction
The second segment cannot (and therefore levelling off for flap rectration) cannot be any lower than ___ft AGL
400
By the end of the second segment, the speeds you should have passed through are ___
V2, V3, V4
Below 400ft, the only change in configuration which is allowed is the ___
landing gear retraction
The second segment requires a .% gradient for 2 engine aircraft
2.4
The second segment requires a .% gradient for 3 engine aircraft
2.7
The second segment requires a _% gradient for 4 engine aircraft
3
The second segment climb gradient is defined by ___
- Gear up
- Flaps for takeoff
- Engines at takeoff thrust
- Speed V2
Outline the purpose of the third segment
The aircraft accelerates to flap/slat retraction speed at constant altitude, thereafter accelerating to final takeoff climb speed
During the third segment, flaps are ___ and power is ___ to ___
retracted, reduced, max continuous
The fourth segment involves a climb to ___ft
1500
Outline the aircraft’s configuration in the fourth segment
Flaps retracted, Max Continuous power on one engine, the other secure.
The third and fourth segment require a .% gradient for 2 engine aircraft
1.2
The third and fourth segment require a .% gradient for 3 engine aircraft
1.5
The third and fourth segment require a .% gradient for 4 engine aircraft
1.7
The acceleration from Vfto to final en-route climb speed is done at the end of the ___ segment.
fourth
The Net Takeoff Flight Path should clear all obstacles vertically by __ft and ___ft horizontally (___ft within the airport boundary)
35, 300, 200
