FAA AC 33.17-1 : 2009
Current
The latest, up-to-date edition.
ENGINE FIRE PROTECTION SECTION 33.17
Hardcopy , PDF
English
01-01-2009
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1. PURPOSE
2. APPLICABILITY
3. DEFINITIONS
4. GENERAL
5. MATERIALS DESIGN ASSESSMENT
6. CONDUCT OF FIRE TESTS
7. OTHER CONSIDERATIONS
8. TEST PLANS
APPENDIX 1 - REFERENCES
Gives definitions, guidance, and acceptable methods, but not the only methods, that may be used to demonstrate compliance with the engine fire protection requirements of Title 14 Code of Federal Regulations (14 CFR 33.17).
| DocumentType |
Standard
|
| Pages |
12
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| SAE ARP 5757 : 2016 | GUIDELINES FOR ENGINE COMPONENT TESTS |
| FAA AC 21-16 : 2011 | RTCA DOCUMENT DO-160 VERSIONS D, E, F, AND G, "ENVIRONMENTAL CONDITIONS AND TEST PROCEDURES FOR AIRBORNE EQUIPMENT" |
| SAE ARP 986 : 2015 | GUIDE FOR QUALIFICATION TESTING OF AIRCRAFT AIR VALVES |
| FAA AC 33-4 : 0 | DESIGN CONSIDERATIONS CONCERNING THE USE OF TITANIUM IN AIRCRAFT TURBINE ENGINES |
| SAE AIR 1377B : 1980 | FIRE TEST EQUIPMENT FOR FLEXIBLE HOSE AND TUBE ASSEMBLIES |
| SAE AS1055D | FIRE TESTING OF FLEXIBLE HOSE, TUBE ASSEMBLIES, COILS, FITTINGS AND SIMILAR SYSTEM COMPONENTS |
| FAA AC 20-135 : 0 | POWERPLANT INSTALLATION AND PROPULSION SYSTEM COMPONENT FIRE PROTECTION TEST METHODS, STANDARDS AND CRITERIA |
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