Advisory Circular Federal Aviation （咨询通告联邦航空）.pdf

© Advisory US Department of Transportation Circular Federal Aviation Administration Subject: General Type Certification Date : 06/25/2013 AC No: 33-2C Guidelines for Turbine Engines Initiated By: ANE-111 Change: 1. Purpose. This advisory circular (AC) provides general guidance concerning type certification projects for aircraft turbine engines. This AC applies to certain sections of Title 14 of the Code of Federal Regulations (14 CFR) parts 21 , 33, and 45, and describes or references methods of compliance that may be acceptable for engine type certification work. This guidance is general in nature, and where necessary, further reference is made to other documents, which may be the primary source for information on a particular subject. 2. Applicability. a. The guidance provided in this document is directed to engine manufacturers, modifiers, foreign regulatory authorities, and Federal Aviation Administration (FAA) engine type certification designees. b . This material is neither mandatory nor regulatory in nature and does not constitute a regulation. It describes acceptable means, but not the only means, for demonstrating compliance with the applicable regulations. We (the FAA) will still consider other methods an applicant may present to demonstrate compliance. Terms such as should, may, and must are used only in the sense of ensuring applicability of this particular method of compliance when the method in this document is used. While these guidelines are not mandatory, they are derived from extensive FAA and industry experience in determining compliance with relevant regulations. If we find that following this AC would not result in compliance with the applicable regulations, we will not be bound by this AC, and we may requi