14 C.F.R. § 25.531

Current through May 31, 2024

Section 25.531 - Hull and main float takeoff condition

For the wing and its attachment to the hull or main float-

(a) The aerodynamic wing lift is assumed to be zero; and

(b) A downward inertia load, corresponding to a load factor computed from the following formula, must be applied:

where-

n = inertia load factor;

C_TO = empirical seaplane operations factor equal to 0.004;

V_S₁ = seaplane stalling speed (knots) at the design takeoff weight with the flaps extended in the appropriate takeoff position;

[BETA] = angle of dead rise at the main step (degrees); and

W = design water takeoff weight in pounds.

14 C.F.R. §25.531

Doc. No. 5066, 29 FR 18291, Dec. 24, 1964, as amended by Amdt. 25-23, 35 FR 5673, Apr. 8, 1970