Standard
History of the SAE A-10 Aircraft Oxygen Equipment Committee
2016-08-19
CURRENT
AIR5354A
The following is the history of SAE Committee A-10.
Search Results
Standard
BIBLIOGRAPHY OF REFERENCES PERTAINING TO THE EFFECTS OF OXYGEN ON IGNITION AND COMBUSTION OF MATERIALS
1970-11-01
HISTORICAL
AIR1169
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
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.
Standard
Aerospace Information Report for Continuous Flow Oxygen Hose Disconnect Fittings
2009-08-27
HISTORICAL
AIR1358B
This Aerospace Information Report (AIR) indicates those dimensions, deemed critical by the manufacturer to assure proper mating of disconnect hose fittings. The dimensions are critical, but not necessarily complete, in defining these fittings since there are other criteria which must also be met.
Standard
Aerospace Information Report for Continuous Flow Oxygen Hose Disconnect Fittings
2000-10-01
HISTORICAL
AIR1358A
This AIR indicates those dimensions, deemed critical by the manufacturer, which are required to be adhered to so that proper mating of the disconnect hose fitting with the correct disconnect be accomplished. The dimensions are critical, but not necessarily complete, in defining these fittings since there are other criteria which must also be met.
Standard
AEROSPACE INFORMATION REPORT FOR CONTINUOUS FLOW OXYGEN HOSE DISCONNECT FITTINGS
1991-09-01
HISTORICAL
AIR1358
This AIR indicates those dimensions, deemed critical by the manufacturer, which are required to be adhered to so that proper mating of the disconnect hose fitting with the correct disconnect be accomplished. The dimensions are critical, but not necessarily complete, in defining these fittings since there are other criteria which must also be met.
Standard
Useful Life Determination for Chemical Oxygen Generators
2013-12-13
HISTORICAL
ARP1894A
The scope of this document is to provide a guideline for the preparation of a plan for testing of inservice chemical oxygen generators to confirm their design useful life. The test program should also allow determination with a sufficient level of confidence, whether generators are suitable for further use (i.e., life extension, or if the useful life limit has been reached).
Standard
USEFUL LIFE DETERMINATION CHEMICAL OXYGEN GENERATORS
1987-02-01
HISTORICAL
ARP1894
This document provides recommended guidelines for a comprehensive program to determine the useful life of chemical oxygen generators where useful life is defined as the sum of shelf and service life. Further, this document provides for a test program to determine with a sufficient level of confidence if the generators are suitable for further use and/or if the life limit has been reached. This program should include testing of generators of a representative sampling of a given year's production, of a particular part number, to provide a level of confidence sufficient to permit the units to be used for an additional specified time period.
Standard
Useful Life Determination for Chemical Oxygen Generators
2014-02-13
CURRENT
ARP1894B
The scope of this document is to provide a guideline for the preparation of a plan for testing of inservice chemical oxygen generators to confirm their design useful life. The test program should also allow determination with a sufficient level of confidence, whether generators are suitable for further use (i.e., life extension, or if the useful life limit has been reached).
Standard
STANDARD FOR OXYGEN FLOW INDICATORS
1966-07-01
HISTORICAL
AS916
This standard is intended to establish general material and design requirements for oxygen flow indicating devices. Flow indicators considered are for diluter-demand and continuous flow systems.
Standard
Oxygen Flow Indication
2019-01-10
CURRENT
AS916C
This SAE Aerospace Standard (AS) defines the overall requirements applicable to oxygen flow indication as required by Airworthiness Requirements of CS/FAR 25.1449 to show that oxygen is being delivered to the dispensing equipment. Requirements of this document shall be applicable to any type of oxygen system technology and encompass “traditional” pneumatic devices, as well electric/electronic indication.
Standard
Reducers, Oxygen Pressure
2023-01-26
CURRENT
AS17852A
This specification covers the requirements for two types of oxygen pressure reducers.
Standard
Reducers, Oxygen Pressure
2009-11-30
HISTORICAL
AS17852
This specification covers the requirements for two types of oxygen pressure reducers.
Standard
Convenient Location of Oxygen Masks for Both the Crew and Passengers of Aircraft
2023-05-01
CURRENT
AIR1390B
There are four basic conditions requiring the dispensing of oxygen through oxygen masks to aircraft occupants in turbine powered aircraft during flight. The following conditions are derived from the Federal Aviation Regulations (FAR) as listed in Section 2.
Standard
Continuous Flow Aviation Oxygen Masks (For Non-Transport Category Aircraft)
2021-08-10
CURRENT
AS1224B
This standard defines the minimum requirement for the design, construction and performance of continuous flow oxygen masks for crew and passengers of general aviation civil aircraft.
Standard
Aircraft Oxygen Replenishment Coupling for Civil Transport Aircraft (Design Standard)
2021-03-09
WIP
AS1219B
This SAE Aerospace Design Standard defines a coupling, which is installed in a high pressure (1850 to 2000 psig) oxygen system of a civil transport aircraft for the purpose of mating to ground oxygen replenishment facilities. Dimensions developed from AND10089, Detail Specification Sheet for Fitting End, Design Standard, For Cone Connection.
Standard
Aircraft Oxygen Replenishment Coupling for Civil Transport Aircraft (Design Standard)
2020-02-28
CURRENT
AS1219A
This SAE Aerospace Design Standard defines a coupling, which is installed in a high pressure (1850 to 2000 psig) oxygen system of a civil transport aircraft for the purpose of mating to ground oxygen replenishment facilities. Dimensions developed from AND10089, Detail Specification Sheet for Fitting End, Design Standard, For Cone Connection.
Standard
FAA REGULATIONS COVERING THE USE OF OXYGEN IN AIRCRAFT
1991-05-01
HISTORICAL
AIR1389
Standard
DYNAMIC TESTING SYSTEMS FOR OXYGEN BREATHING EQUIPMENT
1987-04-01
HISTORICAL
ARP1109A
This ARP describes test equipment and methods used for testing continuous flow, demand and pressure demand regulators and their associated masks as well as filtered protective breathing devices; such articles of oxygen breathing or protective breathing equipment may be tested as individual components or as a complete system.
