minimum flap retraction height
Minimum Flaps Retraction Height
What would happen if, using take off analysis that states the minimum retraction altitude as being 400 feet above ground level accomplished with SOP Take off- one engine in accordance TO THE SAME ANALYSIS, in case of delay of the retraction altitude until 1000 feet AGL?
In other words, what could happen if the SOP was changed to accelerate at 1000 feet AGL in case of engine failure, but using take off analysis based on a minimum retraction altitude of 400 feet AGL?
Thanks in advance for your help in this topic