scope:

INTRODUCTION

This Part states those tests which shall be made to demonstrate that the rotorcraft can be controlled satisfactorily and is adequately stable in the air, and on the ground, in accordance with the requirements of Part 6.

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

Object;

Relevant design requirements;

Applicability;

Equipment;

Loading;

General test conditions;

Tests;

Notes.