Turbine engine rotor blade containment/durability.
Saved in:
| Corporate author / creator: | United States. Federal Aviation Administration. |
|---|---|
| Imprint: | Washington, D.C. : U.S. Dept. of Transportation, Federal Aviation Administration, [1990] |
| Description: | 5 pages : digital, PDF file. |
| Language: | English |
| Series: | Advisory circular ; AC no. 33-5 United States. Federal Aviation Administration. Advisory circular ; AC 33-5. |
| Subject: | |
| Format: | E-Resource U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/7526979 |
MARC
| LEADER | 00000cam a2200000Ia 4500 | ||
|---|---|---|---|
| 001 | 7526979 | ||
| 005 | 20081209144316.0 | ||
| 006 | m d f | ||
| 007 | cr m|||||||||| | ||
| 008 | 081209s1990 dcua o f000 0 eng d | ||
| 003 | ICU | ||
| 035 | |a (OCoLC)277237601 | ||
| 040 | |a GPO |b eng |c GPO |d MvI | ||
| 074 | |a 0431-A-27 (online) | ||
| 086 | 0 | |a TD 4.8/5:33-5 | |
| 110 | 1 | |a United States. |b Federal Aviation Administration. |0 http://id.loc.gov/authorities/names/n79034443 |1 http://viaf.org/viaf/136855410 | |
| 245 | 1 | 0 | |a Turbine engine rotor blade containment/durability. |
| 264 | 1 | |a Washington, D.C. : |b U.S. Dept. of Transportation, Federal Aviation Administration, |c [1990] | |
| 300 | |a 5 pages : |b digital, PDF file. | ||
| 336 | |a text |b txt |2 rdacontent |0 http://id.loc.gov/vocabulary/contentTypes/txt | ||
| 337 | |a computer |b c |2 rdamedia | ||
| 338 | |a online resource |b cr |2 rdacarrier |0 http://id.loc.gov/vocabulary/carriers/cr | ||
| 490 | 1 | |a Advisory circular ; |v AC no. 33-5 | |
| 500 | |a "06/18/90." | ||
| 538 | |a Mode of access: Internet at the FAA web site. Address as of 12/9/08: http://www.airweb.faa.gov/Regulatory%5Fand%5FGuidance%5FLibrary/rgAdvisoryCircular.nsf/0/eab0330a3c7a22eb862569b3005d6ace/$FILE/ac33-5.pdf; current access available via PURL. | ||
| 500 | |a Title from PDF file caption (viewed Dec. 9, 2008). | ||
| 650 | 0 | |a Airplanes |x Turbine-propeller engines |x Design and construction. | |
| 650 | 0 | |a Airplanes |x Turbojet engines |x Blades. | |
| 776 | 0 | |a United States. Federal Aviation Administration. |t Turbine engine rotor blade containment/durability |h 5 p. |w (OCoLC)29643011 | |
| 810 | 1 | |a United States. |b Federal Aviation Administration. |t Advisory circular ; |v AC 33-5. | |
| 856 | 4 | 0 | |u https://purl.fdlp.gov/GPO/LPS106292 |y Government Publishing Office |
| 903 | |a HeVa | ||
| 929 | |a eresource | ||
| 999 | f | f | |i 056d1d34-d536-5e76-bc4a-23f4dce40c59 |s 941d99cc-c226-5117-9685-6b780ca323a1 |
| 928 | |t Library of Congress classification |l Online |c UC-FullText |u https://purl.fdlp.gov/GPO/LPS106292 |z Government Publishing Office |g ebooks |i 12800713 | ||