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DOT/FAA RIN: 2120-AH36 Publication ID: Spring 2003 
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: Previously published in the Unified Agenda Agenda Stage of Rulemaking: Final Rule Stage 
Major: No  Unfunded Mandates: No 
EO 13771 Designation: uncollected 
CFR Citation: 14 CFR 25   
Legal Authority: 49 USC 106(g)    49 USC 40113   
Legal Deadline:  None
Timetable:
Action Date FR Cite
NPRM  01/29/2002  67 FR 4318   
NPRM Comment Period End  04/01/2002    
Final Action  09/00/2003    
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