xmlns:atom="http://www.w3.org/2005/Atom" xmlns:atom="http://www.w3.org/2005/Atom"
not more than the power or thrust that is available eight seconds after initiation of movement of the power controls from the minimum flight idle position;
the landing gear extended;
the wing flaps in the landing position; and
a climb speed equal to VREF (reference landing speed).
the critical engine inoperative and its propeller in the minimum drag position;
the remaining engine at not more than maximum continuous power;
the landing gear retracted;
the wing flaps retracted; and
a climb speed not less than 1,2 VS1.