scope:

INTRODUCTION 

This Part states those tests which shall be made to demonstrate that the aeroplane can be controlled satisfactorily and is adequately stable in the air, and on the ground, in accordance with the requirements of Part 6. The tests of this Chapter are to be approved by the Aeroplane Project Director in conjunction with A 8 AEE.

Each chapter of this Part contains tests of the aeroplane under a specific fiight condition and is arranged in accordance with a standard layout, the paragraphs being grouped under headings in the following sequence :

(i) Object;

(ii) Relevant design requirements;

(iii) Applicability ;

(iv) Equipment; (VI Loading;

(vi) General test conditions;

viii) Tests;