Qualification testing of turbojet engine thrust reversers.

Bibliographic Details
Corporate Author: United States. Federal Aviation Administration
Format: Government Document Book
Language:English
Published: [Washington, D.C.] : Federal Aviation Administration, [1966]
Series:Advisory circular ; AC no: AC 20-18A
Subjects:
Online Access:https://purl.fdlp.gov/GPO/LPS102945

Internet

https://purl.fdlp.gov/GPO/LPS102945

Available Online

Holdings details from Available Online
Call Number: TD 4.8/5:20-18 A
 
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TD 4.8/5:20-18 A Available