Damage tolerance and fatigue evaluation of structure [electronic resource]
- Bib ID:
- 4547277
- Format:
- Book
- Author:
- United States. Federal Aviation Administration
- Online Access:
- http://purl.access.gpo.gov/GPO/LPS105871
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- Description:
-
- [Washington, D.C.] : U.S. Dept. of Transportation, Federal Aviation Administration, [1998]
- 20 p. : digital, PDF file.
- Series:
- United States. Federal Aviation Administration. Advisory circular ; AC 25.571-1 C.
- Technical Details:
- Mode of access: Internet at the FAA web site. Address as of 11/26/08: http://www.airweb.faa.gov/Regulatory%5Fand%5FGuidance%5FLibrary/rgAdvisoryCircular.nsf/0/88f968a77cbb45b6862569d00076b7c3/$FILE/ac25.571-1c.pdf ; current access available via PURL.
- Notes:
-
- "4/29/98."
- Advisory Circular 25.571- lB, dated February 18, 1997, is canceled.
- Title from PDF file caption (viewed Nov. 26, 2008).
- Subject:
- Airframes -- Fatigue
- Other authors/contributors:
- United States. Federal Aviation Administration
- Govt. Doc. Number:
- TD 4.8/5:25.571-1 C
- Copyright:
-
In Copyright
You may copy under some circumstances, for example you may copy a portion for research or study. Order a copy through Copies Direct to the extent allowed under fair dealing. Contact us for further information about copying.
- Reason for copyright status:
- Until 2068 [Created/Published Date + 70 Years]
Copyright status was determined using the following information:
- Material type:
- Literary Dramatic Musical
- Published status:
- Published
- Publication date:
- 1998
Copyright status may not be correct if data in the record is incomplete or inaccurate. Other access conditions may also apply. For more information please see: Copyright in library collections.
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