T/O Engine failure acceleration altitude
Hi folks!
Wondering what is the acceleration altitude in case of engine failure at take off (no contingency procedure due to obstacles) according to your AFM or/and company SOP.
I'd appreciate a brief comment on the pros and cons of different options, especially low altitude (ca. 400 ft) versus high altitude (ca. 1500 ft).
Thanks so much for your kind help, happy landings!!