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DOT/FAA RIN: 2120-AH36 Publication ID: Fall 2001 
Title: ●Material Strength Properties and Design Values 
Abstract: The FAA proposes to revise the material strength properties and material design values requirement for transport category airplanes by incorporating changes developed in cooperation with the Joint Aviation Authorities of Europe and the U.S. and European aviation industry through the Aviation Rulemaking Advisory Committee. This proposal is intended to achieve common requirements and language between the requirements of the U.S. regulations and the Joint Aviation Requirements of Europe, while maintaining at least the level of safety provided by the current regulations. 
Agency: Department of Transportation(DOT)  Priority: Substantive, Nonsignificant 
RIN Status: First time published in the Unified Agenda Agenda Stage of Rulemaking: Proposed Rule Stage 
Major: No  Unfunded Mandates: No 
CFR Citation: 14 CFR 25   
Legal Authority: 49 USC 106(g)    49 USC 40113   
Legal Deadline:  None
Timetable:
Action Date FR Cite
NPRM  12/00/2001    
Additional Information: Project Number: ANM-98-300.
Regulatory Flexibility Analysis Required: No  Government Levels Affected: None 
Small Entities Affected: No  Federalism: No 
Included in the Regulatory Plan: No 
Agency Contact:
Rich Yarges
Airframe and Airworthiness Branch, Aircraft Certification Service
Department of Transportation
Federal Aviation Administration
Northwest Mountain Region, 1601 Lind Avenue SW,
Renton, WA 98055-4056
Phone:425 227-2143