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Standard

When and How Shall Oxygen be Used on Aircraft”

2015-09-22
WIP
AIR6256
The aim of this document is to provide a comprehensive synopsis of regulations applicable to aircraft oxygen systems. The context of physiological requirements, international regulations, operational requirements and airworthiness standards is shown to understand the role of aircraft oxygen systems and to demonstrate under which circumstances is needed on aircraft. With regards to National Aviation Regulations States are committed to the Convention on International Aviation (Chicago Convention). The majority of states have adopted, with some deviations, FAA and EASA systems including operational and airworthiness requirements. Accordingly the extent of this document is primarily focused on FAA/EASA requirements.
Standard

FITTING END, BULKHEAD, CONE, DESIGN STANDARD

2020-12-03
WIP
AS6847
This SAE Aerospace Standard defines a bulkhead coupling (with different fitting end styles), which is used in bulkhead cone connection fittings installed in high pressure (3000 psi) oxygen systems for the purpose of mating to applicable oxygen equipment. Dimensions developed from AND10089, Detail Specification Sheet for Fitting End, Design Standard, For Cone Connection.
Standard

FITTING, TEE, BULKHEAD ON SIDE, CONE, DESIGN STANDARD

2020-11-02
WIP
AS6844
This SAE Aerospace Standard (AS) establishes the requirements for bulkhead-on-side-tee cone connection fittings, for use in aircraft oxygen systems at nominal operating pressures up to and including 3000 psi.
Standard

FITTING, UNION, BULKHEAD, CONE, DESIGN STANDARD

2020-11-02
WIP
AS6845
This SAE Aerospace Standard (AS) establishes the requirements for bulkhead-union cone connection fittings, for use in aircraft oxygen systems at nominal operating pressures up to and including 3000 psi.
Standard

FITTING, TEE, BULKHEAD ON RUN, CONE, DESIGN STANDARD

2020-11-02
WIP
AS6843
This SAE Aerospace Standard (AS) establishes the requirements for bulkhead-on-run-tee cone connection fittings, for use in aircraft oxygen systems at nominal operating pressures up to and including 3000 psi.
Standard

Passenger Hypoxia Protection Utilizing Oxygen Enriched Gas Mixtures

2018-10-18
CURRENT
AIR6036
Currently, existing civil aviation standards address the design and certification of oxygen dispensing devices that utilize oxygen sources supplying at least 99.5% oxygen. This Aerospace Information Report discusses issues relating to the use in the passenger cabin of oxygen enriched breathing gas mixtures having an oxygen content of less than 99.5% and describes one method of showing that passenger oxygen dispensing devices provide suitable hypoxia protection when used with such mixtures.
Standard

METABOLIC SIMULATOR TESTING SYSTEMS FOR AVIATION BREATHING EQUIPMENT

1991-04-01
HISTORICAL
ARP4259
This Aerospace Recommended Practice (ARP) describes test equipment and methods used for testing closed cycle or semi closed cycle breathing devices of short duration that are designed to operate with a high partial pressure of oxygen in the breathing circuit. It is intended to supplement ARP1109 and ARP1398 for applications involving closed cycle or semiclosed cycle breathing equipment which may be evaluated to the requirements of AS8031 and/or AS8047.
Standard

Regulator Oxygen Diluter Demand, Automatic Pressure Breathing

1997-10-01
CURRENT
AS1194
To define optimum standards of design, construction and performance for Diluter Demand, Automatic Pressure Breathing, Oxygen Regulators. AS 861, 'Minimum General Standards for Oxygen Systems,' is applicable as supplemented by this specification. This document supersedes in part AS 463, 12-15-56, which is cancelled. This specification covers two types of Diluter Demand, Automatic Pressure Breathing, Oxygen Regulators for use in civil type aircraft. The intent is that the regulators be of two configurations, operable at inlet pressures of 40 to 90 psig and 50 to 150 psig.
Standard

Oxygen Considerations for High Elevation Airport Operations (HEAO)

2021-08-26
CURRENT
AIR6829
This document covers information concerning the use of oxygen when flying into and out of high elevation airports for both pressurized and non-pressurized aircraft. Oxygen requirements for pressurized aircraft operating at high altitudes have for decades emphasized the potential failures that could lead to a loss of cabin pressurization coupled with the potential severe hypoxic hazard that decompressions represent. This document is intended to address the case where the relationship between cabin and ambient pressures are complicated by operations at high terrestrial altitudes. Operators who fly into these high-altitude airports should address the issues related to this environment because it carries the potential for insidious hypoxia and other conditions which can affect safety. It provides information to consider in developing operational procedures to address hypoxia concerns consistent with regulatory mandates.
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