FAA AC 33-3 : 0
Current
TURBINE AND COMPRESSOR ROTORS TYPE CERTIFICATION SUBSTANTIATION PROCEDURES
Hardcopy , PDF
English
1 PURPOSE
2 CANCELLATION
3 CHANGES
4 REFERENCES REGULATIONS
5 SCOPE
6 ACCEPTABLE MEANS OF COMPLIANCE FOR SUBSTANTIATING
TURBINE AND COMPRESSOR ROTORS
Gives guidance and acceptable means, not the sole means, by which compliance may be shown with the turbine and compressor rotor substantiation requirements in Federal Aviation Regulations, Part 33.
| DocumentType |
Standard
|
| Pages |
8
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA AC 33.27-1 : 2011 | ENGINE AND TURBOSUPERCHARGER ROTOR OVERSPEED REQUIREMENTS OF 14 CFR SECTION 33.27 |
| FAA AC 33.64-1 : 2010 | GUIDANCE FOR PRESSURIZED ENGINE STATIC PARTS |
| MIL-HDBK-516 Revision C:2014 | Airworthiness Certification Criteria |
| FAA AC 33.15-1 : 0 | MANUFACTURING PROCESS OF PREMIUM QUALITY TITANIUM ALLOY ROTATING ENGINE COMPONENTS |
| FAA AC 33.15-2 : 2011 | MANUFACTURING PROCESSES FOR PREMIUM QUALITY NICKEL ALLOY FOR ENGINE ROTATING PARTS |
| FAA AC 33.70-2 : 2009 | DAMAGE TOLERANCE OF HOLE FEATURES IN HIGH-ENERGY TURBINE ENGINE ROTORS |
| FAA AC 33.70-1 : 2009 | GUIDANCE MATERIAL FOR AIRCRAFT ENGINE LIFE-LIMITED PARTS REQUIREMENTS |
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