Damage tolerance for high energy turbine engine rotors.
| Author/creator | United States |
| Format | Electronic |
| Publication Info | [Washington, D.C.] : U.S. Dept. of Transportation, Federal Aviation Administration, [2001] |
| Description | 1 v. (various pagings) : digital, PDF file |
| Supplemental Content | https://purl.fdlp.gov/GPO/LPS106376 |
| Subjects |
| Series | Advisory circular ; AC no. 33.14-1 United States. Federal Aviation Administration. Advisory circular ; AC 33.14-1. ^A500611 |
| General note | "1/8/01." |
| General note | Title from PDF file caption (viewed Dec. 10, 2008). |
| General note | GPO Cataloging Record Distribution Program (CRDP). |
| Technical details | Mode of access: Internet at the FAA web site. Address as of 12/10/08: http://www.airweb.faa.gov/Regulatory%5Fand%5FGuidance%5FLibrary/rgAdvisoryCircular.nsf/0/fcb8e6cc06307a3c86256a84005b21ba/$FILE/ac33.14-1.pdf; current access available via PURL. |
| GPO item number | 0431-A-27 (online) |
| Govt. docs number | TD 4.8/5:33.14-1 |
Availability
| Library | Location | Call Number | Status | Item Actions |
|---|---|---|---|---|
| Electronic Resources | Access Content Online | ✔ Available |