The highest limit load factor experienced by a civil transport aircraft is in the range
(A) $0.0-2.0$
(B) $2.0-5.0$
(C) $5.0-8.0$
(D) $8.0-10.0$
The highest limit load factor experienced by a civil transport aircraft is in the range
(A) $0.0-2.0$
(B) $2.0-5.0$
(C) $5.0-8.0$
(D) $8.0-10.0$