FAA AC 33.27-1 : 2011
Current
The latest, up-to-date edition.
ENGINE AND TURBOSUPERCHARGER ROTOR OVERSPEED REQUIREMENTS OF 14 CFR SECTION 33.27
Hardcopy , PDF
English
01-01-2011
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1. Purpose
2. Applicability
3. Related Regulations
4. Related Documents
5. Definitions
6. Objectives
7. General
8. Acceptable Means of Compliance
9. Factors to be Considered when Determining
Test Conditions
10. Failure Cases
Gives guidance and acceptable methods, but not the only methods, for demonstrating compliance with the rotor strength (overspeed) requirements of Title 14 of the Code of Federal Regulations (14 CFR) 33.27.
| DocumentType |
Standard
|
| Pages |
9
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA AC 33-2 : 2013 | GENERAL TYPE CERTIFICATION GUIDELINES FOR TURBINE ENGINES |
| FAA AC 33.70-1 : 2009 | GUIDANCE MATERIAL FOR AIRCRAFT ENGINE LIFE-LIMITED PARTS REQUIREMENTS |
| FAA AC 33-3 : 0 | TURBINE AND COMPRESSOR ROTORS TYPE CERTIFICATION SUBSTANTIATION PROCEDURES |
| FAA AC 33.64-1 : 2010 | GUIDANCE FOR PRESSURIZED ENGINE STATIC PARTS |
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.