Originally Posted by
JohnDixson
KJ, the FAA may have changed the rules since I retired, but the test requirement in the advisory circular accompanying Part 29 used to require flight test at a stable point at 1.11 times the twin engine Vne. Losing parts would be considered bad form.
I’d imagine the Part 27 Advisory Circular reflects the same requirement.
I knew you'd have the exact detail, Mr Dixson! Re: "stable point: is that straight and level and without control movements?