CS-E 700 Excess Operating Conditions

(See AMC E 700) Where any of the operating conditions (e.g. air or gas pressure, thrust, gas temperature) substantiated elsewhere in this subpart could be exceeded in any of the normal and likely emergency conditions within the flight envelope declared by the Engine constructor, it must be established to the satisfaction of the Agency that the most severe conditions likely to occur will have no unacceptable effects on the Engine.

[Amdt. No.: E/1]