FAA AC 33.65-1 : 0
Current
The latest, up-to-date edition.
SURGE AND STALL CHARACTERISTICS OF AIRCRAFT TURBINE ENGINES
Hardcopy , PDF
English
Important note : All end users must be registered with an Account prior to user licenses being assigned.
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 |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.