Text in force at CAR3R-8: from CAR3R-0, effective 15 May 1956. OCR text
In determining the limit airplane inertia load factor n from the free drop test described above, the following formula shall be used: = Ww, n=, W +L where: nj;= the load factor developed in the drop test, i. e., the acceleration (d,/dt) in g's recorded in the drop test, Plus 1.0. The value of 2 so determined shall not be greater than the limit inertia load factor used in the landing conditions, § 3.243.