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Chapter 9 - Pre-Flight TestsPre-flight testing is critical to the success of any flight test program. Pre-flight tests are performed to measure and evaluate the characteristics of an aircraft in a non-flying environment and to verify that these characteristics are as desired. Since aircraft systems are becoming more and more complex, conducting proper pre-flight testing to help identify system characteristics and deficiencies prior to flight is more important now than ever before. Much flight test time has been lost fixing problems that should have been found and corrected prior to flight. Accidents have occurred because pre-flight tests and verification procedures were not conducted thoroughly enough to identify the aircraft's characteristics properly or to find system discrepancies. Proper pre-flight testing helps ensure that the aircraft is ready to fly and contributes toward an efficient, productive, and safe flight test program. The reader should be aware that this Section is dedicated to the testing that should take place prior to the first flight. There are other "pre-flight" tests that take place prior to each individual flight. These latter tests are not discussed in this Section. The following paragraphs of this Section describe significant tests that are usually accomplished prior to flying a new or highly modified aircraft. Test objectives, descriptions, products, and requirements are provided in the following subsections:

9.1 Wind tunnel tests
9.2 Simulation tests
9.3 Propulsion tests
9.4 Weight and balance tests
9.5 Ground vibration tests
9.6 Structural loads tests
9.7 Gain margin tests
9.8 Verification and calibration tests
9.9 Taxi tests

The specific examples given and the test facilities mentioned in this Section will illustrate the approach taken and the techniques used by the US Air Force; however, they are typical of those used by other test organizations.
Document ID
20050209992
Acquisition Source
Legacy CDMS
Document Type
Other - Technical Report
Authors
Paul W Kirsten
(U.S. Air Force Test Center Edwards Air Force Base, United States)
Date Acquired
August 23, 2013
Publication Date
July 1, 2005
Publication Information
Publication: Introduction to Flight Test Engineering [Introduction Aux Techniques Des Essais En Vol]
Publisher: North Atlantic Treaty Organization
Volume: 14
ISBN: 9283711262
Subject Category
Aircraft Design, Testing and Performance
Report/Patent Number
RTO-AG-300-V14
Distribution Limits
Public
Copyright
Other
Technical Review
Single Expert
Document Inquiry

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