CS 29.321 General

• ED Decision 2003/16/RM found in: CS-29 Amdt 11 - Large Rotercraft (Feb 2023)

CS 29.321 General ED Decision 2003/16/RM (a) The flight load factor must be assumed to act normal to the longitudinal axis of the rotorcraft, and to be equal in magnitude and opposite in direction to the rotorcraft inertia load factor at the centre of gravity. (b) Compliance with the flight load requirements of this Subpart must be shown: (1) At each weight from the design minimum weight to the design maximum weight; and (2) With any practical distribution of disposable load within the operating limitations in the rotorcraft flight manual. CS 29.321 General ED Decision 2003/16/RM (a) The flight load factor must be assumed to act normal to the longitudinal axis of the rotorcraft, and to be equal in magnitude and opposite in direction to the rotorcraft inertia load factor at the centre of gravity. (b) Compliance with the flight load requirements of this Subpart must be shown: (1) At each weight from the design minimum weight to the design maximum weight; and (2) With any practical distribution of disposable load within the operating limitations in the rotorcraft flight manual. #### CS 29.321 General *ED Decision 2003/16/RM* (a) The flight load factor must be assumed to act normal to the longitudinal axis of the rotorcraft, and to be equal in magnitude and opposite in direction to the rotorcraft inertia load factor at the centre of gravity. (b) Compliance with the flight load requirements of this Subpart must be shown: (1) At each weight from the design minimum weight to the design maximum weight; and (2) With any practical distribution of disposable load within the operating limitations in the rotorcraft flight manual.