Flight Testing of Fixed-Wing Aircraft

Part 2: Stability and Control Flight Testing

Chapter List

Chapter 19: Introduction to Stability and Control Flight Testing
Chapter 20: Static Longitudinal Stability Theory
Chapter 21: Static Longitudinal Stability Flight Test Methods
Chapter 22: Dynamic Longitudinal Stability Theory
Chapter 23: Dynamic Longitudinal Stability Flight Test Methods and Data Reduction
Chapter 24: Longitudinal Maneuvering Stability Theory
Chapter 25: Maneuvering Stability Methods and Data Reduction
Chapter 26: Longitudinal Control and Trim Theory and Flight Test Methods
Chapter 27: Methods for Improving Longitudinal Stability and Control
Chapter 28: Lateral-Directional Stability Theory and Flight Test Methods
Chapter 29: Dynamic Lateral-directional Stability Theory and Flight Test Methods
Chapter 30: Lateral Control Power (Rolling Performance)
Chapter 31: Directional Control
Chapter 32: Flying Qualities

19.1 Introduction

In order to perform its intended mission an aircraft must have adequate stability and control. The quantity of each of these items will depend on the mission or purpose of the aircraft. For instance, a transport aircraft is interested in a high stability level in order to give the passengers a smooth ride through turbulence, while at the other end of the spectrum, the fighter aircraft needs a high level of controllability for air combat maneuvering. So, like aircraft performance, the stability and control is a function of the aircraft mission. As a result, the applicable regulations that govern the levels of stability and control are somewhat different depending on the aircraft's mission.

19.2 Regulations

For civilian airplanes, FAR Part 23 specifies the requirements for light aircraft under 12,500 lb gross weight.

For transport aircraft or aircraft over...

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