Jet TakeoffText Box: Our Software is not just another calculator. 
It provides you with a complete solution when it comes to takeoff performance.

 

 

 

 

 

Text Box: Let your computer calculate optimum takeoff and landing performance for not just one airport, but three
You can pick a departure airport, a destination airport, and an alternate.
 

 

 

 

 

  

Text Box: The software will find the maximum weight you can use in every situation. It will check all the pertinent charts such as WAT limit, brake energy limit, tire speed limit, obstacle limit etc.
If your plane cannot take off at the proposed weight, the software will calculate the best weight that will work given the conditions.

 

 

 

 

 

 

 

 

Text Box: Get accurate meaningful answers in just seconds.


 

 

 

 

 

ObstUse011aDuring obstacle clearance calculations, our software simultaneously uses

runway analysis and obstacle analysis, to arrive at an answer that gives you the

best takeoff weight possible under the given conditions. When the weight has to

be reduced, the Accelerate-Go Distance decreases while the available climb gradient

increases. Including the unused runway, the required climb gradient decreases.

Attempting to do such calculations by hand can be overwhelming, but our software

does it accurately in a split second!

 

 

 

 

 

 

Clearing an obstacle:

In this scenario the maximum takeoff weight allowed was determined as follows:

The program searches for the highest possible aircraft weight which allows the aircraft

to clear the obstacle by a minimum of 35 feet. In this example it was determined that this

optimum weight (8922 lbs) will result in an accelerate-go distance of 3200 feet, leaving

1033 feet of unused runway. Add this unused runway distance to the obstacle distance

of 1850 feet and the total distance from the end of accelerate-go portion to the obstacle is

now 2883 feet. Thus, the minimum takeoff gradient required in order to clear this particular

obstacle is 6.9% (height of 200 feet and distance of 2883 feet). This is illustrated in the

diagrams below.

 

Without taking into account the unused runway, the minimum required takeoff

gradient is 10.8% In order to achieve this climb gradient the takeoff weight would

have to be reduced to 7220 lbs. At this low weight one is not fully taking advantage

of this airplane’s capabilities.

Takeoff Gradient

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Taking into account the unused runway, the minimum required takeoff gradient is 6.9%

allowing the aircraft to takeoff with a weight of 8922 pounds and safely clear the obstacle.

 

 

Note that the Takeoff Climb Gradient chart does not provide any information regarding Headwind

Corrections or Tailwind Corrections. The Climb Gradient values used in computations are zero-wind values.

 

 

 

Some screenshots of  Windows versions:

 

ClimbLimitEx

 

Alpine001

 

Pick a color for each page for easy airport identification

Save your data and later retrieve it all with just a click

TripleView

Or if you are working in a low light environment select a Night View Mode to make it easier on your eyes in preserving the night vision

 

NiteView02

 

 

Copyright © 2009-2012 AFM Solutions