§3.354 Limit load factor determination.

In determining the limit airplane inertia load factor n from the free drop test described above, the following formula shall be used: where nj = the load factor developed in the drop test, i.e., the acceleration (dv/dt) in g’s recorded in the drop test, plus 1.0. The value of n so determined shall not be greater than the limit inertia load factor used in the landing conditions, § 3.243. —_A_ Wer Wed