This standard practice addresses requirements to be met for establishing a small aeroplane structure as low stress or low strain by design. If the criteria of a low stress airframe structure is met, additional options are available with regards to demonstrating structural durability. See the F3115 Standard Specification for Structural Durability of Small Airplanes for these options.
Airframe; Aeroplane; low stress
None Provided
The title and scope are in draft form and are under development within this ASTM Committee.
Date Initiated: 11-27-2017
Technical Contact: Terry Ercolani
Item: 001
Ballot: F44.30 (17-03)
Status: Will Reballot Item
Item: 002
Ballot: F44 (21-02)
Status: Withdrawn From Balloting
Item: 001
Ballot: F44.30 (21-01)
Status: Will Reballot Item
Item: 002
Ballot: F44 (22-09)
Status: Withdrawn From Balloting