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DOT/FAA RIN: 2120-AJ52 Publication ID: Fall 2010 
Title: Damage Tolerance and Fatigue Evaluation of Composite Rotorcraft Structures 
Abstract: This rulemaking would address advances in composite structures technology. The intended effects are increased safety requirements as well as harmonization with international standards. 
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 
CFR Citation: 14 CFR 27   
Legal Authority: 49 USC 106(g)    49 USC 40113    49 USC 44701    49 USC 44702    49 USC 44704   
Legal Deadline:  None
Timetable:
Action Date FR Cite
NPRM  01/06/2010  75 FR 793   
NPRM Comment Period End  04/06/2010    
NPRM Comment Period Reopened  05/05/2010  75 FR 24502   
Reopening of Comment Period End  07/16/2010    
Final Action  11/00/2011    
Additional Information: An Aviation Rulemaking Advisory Committee (ARAC) working group (WG) recommended changes to rotorcraft composite structure safety standards to address advances in technology.
Regulatory Flexibility Analysis Required: No  Government Levels Affected: None 
Small Entities Affected: No  Federalism: No 
Included in the Regulatory Plan: No 
RIN Information URL: www.regulations.gov   Public Comment URL: www.regulations.gov  
RIN Data Printed in the FR: No 
Agency Contact:
Sharon Miles
Regulations and Policy Group
Department of Transportation
Federal Aviation Administration
2601 Meacham Blvd.,
Fort Worth, TX 76137
Phone:817-222-5122
Email: sharon.y.miles@faa.gov