CS-E 30 Assumptions

(See AMC E 30)

(a)In the course of establishing compliance with CS-E certain assumptions have to be made concerning the conditions that may be imposed on the Engine when it is eventually installed in the aircraft. In order that the validity of the conditions assumed in the Engine certification may be assessed for any particular installation, prior to Engine certification, the details of the assumptions made must be submitted. These assumptions must be included in the Engine instructions for installation required under CS-E 20(d).

(b)Where an Engine system relies on components which are not part of the Engine type design, the interface conditions and reliability specifications for those components upon which the Engine certification is based must be specified in the Engine instructions for installation directly or by reference to appropriate documentation.

[Amdt No: E/1]