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FAA AC 33.65-1 : 0

Current

Current

The latest, up-to-date edition.

SURGE AND STALL CHARACTERISTICS OF AIRCRAFT TURBINE ENGINES

Available format(s)

Hardcopy , PDF

Language(s)

English

€17.95
Excluding VAT

1 PURPOSE
2 RELATED FAR SECTIONS
3 BACKGROUND
4 DEFINITIONS
5 RELATIONSHIP TO AIRCRAFT CERTIFICATION PROCEDURES
6 APPROACH

Gives guidance material for acceptable means of demonstrating compliance with the requirements of Part 33 of the Federal Aviation Regulations (FAR) relative to surge and stall characteristics and thrust response of turbine engines.

DocumentType
Standard
Pages
6
PublisherName
Federal Aviation Administration
Status
Current

FAA AC 43-207 : 2002 CORRELATION, OPERATION, DESIGN, AND MODIFICATION OF TURBOFAN/JET ENGINE TEST CELLS

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