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ASTM-F2317:2009 Edition

ASTM-F2317:2009 Edition

$40.63

F2317/F2317M-05(2009) Standard Specification for Design of Weight-Shift-Control Aircraft

Published By Publication Date Number of Pages
ASTM 2009 10
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1.1 This specification covers the minimum airworthiness standards a manufacturer shall meet in the designing, testing, and labeling of weight-shift-control aircraft.

1.2 This specification covers only weight-shift-control aircraft in which flight control systems do not use hinged surfaces controlled by the pilot.

Note 1This section is intended to preclude hinged surfaces such as typically found on conventional airplanes such as rudders and elevators. Flexible sail surfaces typically found on weight-shift aircraft are not considered hinged surfaces for the purposes of this specification.

1.3 Weight-shift-control aircraft means a powered aircraft with a framed pivoting wing and a fuselage (trike carriage) controllable only in pitch and roll by the pilot’s ability to change the aircraft’s center of gravity with respect to the wing. Flight control of the aircraft depends on the wing’s ability to flexibly deform rather than the use of control surfaces.

1.4 This specification is organized and numbered in accordance with the bylaws established for Committee F37. The main sections are:

1.5 The values stated in either SI units or inch-pound units are to be regarded separately as standard. The values stated in each system may not be exact equivalents; therefore, each system shall be used independently of the other. Combining values from the two systems may result in non-conformance with the standard.

1.6 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory requirements prior to use.

PDF Catalog

PDF Pages PDF Title
1 Scope
Referenced Documents
Terminology
2 Flight Requirements
3 Structural Requirements
4 TABLE 1
5 Design and Construction Requirements
6 Powerplant
Equipment Requirements
Operating Limitations
Keywords
7 A1. DESIGN AND PERFORMANCE STANDARDS FOR LIGHT SPORT AIRCRAFT USED TO AERO-TOW GLIDERS
A1.1 Applicability
A1.2 Controllability and Maneuverability
A1.3 Stability
A1.4 Structure and Strength Requirements
A1.5 Design and Construction
A1.6 Operating Limitations
8 X1. STATIC TEST PROTOCOL WING STRENGTH TESTS
X1.1 Load Tests Required
X1.2 Calculation Of Total Test Loads To Be Applied
X1.3 Positive Load
X1.4 Negative Load
FIG. X1.1
9 TABLE X1.1
FIG. X1.2
TABLE X1.2

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