Damage tolerance for high energy turbine engine rotors.

Bibliographic Details
Corporate Author: United States. Federal Aviation Administration
Format: Government Document Book
Language:English
Published: [Washington, D.C.] : U.S. Dept. of Transportation, Federal Aviation Administration, [2001]
Series:Advisory circular ; AC no. 33.14-1
Subjects:
Online Access:https://purl.fdlp.gov/GPO/LPS106376

MARC

Tag First Indicator Second Indicator Subfields
LEADER 00000cam a2200000Ka 4500
001 in00002444729
005 20211202190349.0
006 m d f
008 081210s2001 dcu s f000 0 eng d
035 |a (OCoLC)ocn277629220 
040 |a GPO  |c GPO  |d MvI  |d UtOrBLW 
049 |a WWW 
074 |a 0431-A-27 (online) 
086 0 |a TD 4.8/5:33.14-1 
110 1 |a United States.  |b Federal Aviation Administration. 
245 1 0 |a Damage tolerance for high energy turbine engine rotors. 
264 1 |a [Washington, D.C.] :  |b U.S. Dept. of Transportation, Federal Aviation Administration,  |c [2001] 
300 |a 1 volume (various pagings) :  |b digital, PDF file. 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a unspecified  |b zu  |2 rdacarrier 
490 1 |a Advisory circular ;  |v AC no. 33.14-1 
500 |a "1/8/01." 
538 |a 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. 
500 |a Title from PDF file caption (viewed Dec. 10, 2008). 
500 |a Electronic resource. 
650 0 |a Airplanes  |x Turbine-propeller engines  |x Certification. 
810 1 |a United States.  |b Federal Aviation Administration.  |t Advisory circular ;  |v AC 33.14-1. 
856 4 0 |u https://purl.fdlp.gov/GPO/LPS106376  |t 0 
999 |a MARS 
999 f f |s af3a6cab-f6e0-3be7-9878-0efb81992f7a  |i 6f46b8bc-f8ba-3c48-91ec-4e24e64c2ab2  |t 0 
952 f f |a Texas A&M University  |b College Station  |c Electronic Resources  |d Available Online  |t 0  |e TD 4.8/5:33.14-1  |h Superintendent of Documents classification 
998 f f |a TD 4.8/5:33.14-1  |t 0  |l Available Online