SAE AIR5648A
Current
The latest, up-to-date edition.
Fuel Versus Oxygen: Evaluations and Considerations
18-10-2018
1. SCOPE
2. REFERENCES
3. BACKGROUND AND PROBLEM DEFINITION
4. AIRCRAFT PERFORMANCE
5. OXYGEN DURATION
6. HOW TO USE THE FIGURES
7. AUTOMATED OXYGEN PLANNING ANALYSIS
8. ANALYSIS
9. INSTRUMENTATION
10. PRODUCT COMMONALITY
11. OXYGEN MANAGEMENT
12. NOTES
Describes oxygen system requirements for an in-flight decompression incident.
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Standard
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| ProductNote |
THIS STANDARD ALSO REFERS TO : CFR.25.1441,CFR23.1441,ESEACS23,ESEACS25,FAA 120-42A,FAA120-92A,FARPart91.167,JAR-OPS 1.245,RIN2120-AI03
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| PublisherName |
SAE International
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| Status |
Current
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| Supersedes |
Specific federal aviation regulations (Titled 14 of the United States Code of Federal Regulations, or 14 CFR) define oxygen system requirements for an in-flight decompression incident. This AIR addresses the operational oxygen system requirements for a decompression incident that may occur at any point during a long-range flight, with an emphasis for a decompression at the equal time point (ETP). This AIR identifies fuel and oxygen management contingencies, and presents possible solutions for the efficient, safe, and optimum fuel/oxygen flight continuation. Oxygen management is a concern to all aircraft, such as single engine types that fly above 10 000 feet and use supplemental oxygen. This document provides a method which can help guide users in developing an oxygen solution for their aircraft.
| FAA AC 120-92 : 2015 | SAFETY MANAGEMENT SYSTEMS FOR AVIATION SERVICE PROVIDERS |
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