§25.531. Hull and main float takeoff condition.

14 C.F.R. § 25.531

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:

Notes, amendments, and revision history

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

Authority: 49 U.S.C. 106(f), 106(g), 40113, 44701, 44702 and 44704; Pub. L. 115-254, 132 Stat 3281 (49 U.S.C. 44903 note).

Source: Docket No. 5066, 29 FR 18291, Dec. 24, 1964, unless otherwise noted.

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