FAA AC 33.4-2 : 0
Current
The latest, up-to-date edition.
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS: IN-SERVICE INSPECTION OF SAFETY CRITICAL TURBINE ENGINE PARTS AT PIECE-PART OPPORTUNITY
Hardcopy , PDF
English
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1 PURPOSE
2 RELATED REGULATIONS
3 RELATED REFERENCE MATERIAL
4 DEFINITIONS
5 BACKGROUND
6 CRITICAL PARTS AND FEATURES IDENTIFICATION
7 INSPECTION METHODS
8 FREQUENCY OF INSPECTIONS
9 ENGINE INSTRUCTIONS FOR CONTINUED AIRWORTHINESS (ICA)
10 RECORD KEEPING
Gives guidance and acceptable methods, but not the only methods, that may be used to demonstrate compliance with the requirements of section 33.4 of Title 14 of the Code of Federal Regulations, Instructions for Continued Airworthiness.
| DocumentType |
Standard
|
| Pages |
9
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| FAA 8110.54 : 2010 | INSTRUCTIONS FOR CONTINUED AIRWORTHINESS RESPONSIBILITIES, REQUIREMENTS, AND CONTENTS |
| FAA AC 33.70-1 : 2009 | GUIDANCE MATERIAL FOR AIRCRAFT ENGINE LIFE-LIMITED PARTS REQUIREMENTS |
| FAA AC 33-2 : 2013 | GENERAL TYPE CERTIFICATION GUIDELINES FOR TURBINE ENGINES |
| FAA AC 33.4-1 : 0 | INSTRUCTIONS FOR CONTINUED AIRWORTHINESS |
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