FAA AC 33.70-1 : 2009
Current
The latest, up-to-date edition.
GUIDANCE MATERIAL FOR AIRCRAFT ENGINE LIFE-LIMITED PARTS REQUIREMENTS
Hardcopy , PDF
English
01-01-2009
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1. PURPOSE
2. APPLICABILITY
3. RELATED REGULATIONS
4. RELATED GUIDANCE
5. DEFINITIONS
6. INTRODUCTION
7. GENERAL
8. GUIDANCE FOR DEFINING AN ENGINEERING PLAN
9. GUIDANCE FOR DEFINING A MANUFACTURING PLAN
10. GUIDANCE FOR DEFINING A SERVICE MANAGEMENT PLAN
11. AIRWORTHINESS LIMITATION SECTION
Gives definitions, guidance, and acceptable methods, but not the only methods, that may be used to demonstrate compliance with the engine life-limited parts integrity requirements of section 33.70 of Title 14 of the Code of Federal Regulations (14 CFR part 33).
| DocumentType |
Standard
|
| Pages |
23
|
| 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 33.70-2 : 2009 | DAMAGE TOLERANCE OF HOLE FEATURES IN HIGH-ENERGY TURBINE ENGINE ROTORS |
| FAA AC 33.4-2 : 0 | INSTRUCTIONS FOR CONTINUED AIRWORTHINESS: IN-SERVICE INSPECTION OF SAFETY CRITICAL TURBINE ENGINE PARTS AT PIECE-PART OPPORTUNITY |
| FAA AC 33-3 : 0 | TURBINE AND COMPRESSOR ROTORS TYPE CERTIFICATION SUBSTANTIATION PROCEDURES |
| FAA AC 33.4-1 : 0 | INSTRUCTIONS FOR CONTINUED AIRWORTHINESS |
| FAA AC 33.14-1 : 0 | DAMAGE TOLERANCE FOR HIGH ENERGY TURBINE ENGINE ROTORS |
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