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Standard

AEROSPACE STANDARD, GLAND DESIGN, O-RING AND OTHER ELASTOMERIC SEALS

1993-06-11
HISTORICAL
AS4716
This SAE Aerospace Standard provides standardized gland (groove) design criteria and dimensions for elastomeric seal glands for static and dynamic applications. The glands have been specifically designed for applications using SAE AS568 size O-rings at pressures exceeding 1500 psi utilizing one or two anti-extrusion (backup) rings and applications at pressures under 1500 psi without backup rings. The glands have been sized to provide sufficient squeeze for effective sealing while at the same time limiting squeeze to allow satisfactory operation in dynamic applications. While specifically designed for standard size O-rings, these glands are also to be used with other elastomeric seals.
Standard

AIRCRAFT DEICING VEHICLE - SELF-PROPELLED, LARGE CAPACITY

1992-12-01
HISTORICAL
ARP1971
This specification covers requirements for a self-propelled, boom type aerial device, equipped with an aircraft deicing fluid spraying system. The unit shall be highly maneuverable for deicing all exterior surfaces of wide-body and intermediate size aircraft, e.g., B-747 and B-737. The vehicle will also be used for aircraft maintenance and inspection. The vehicle shall be suitable for day and night operations.
Standard

AIRCRAFT DEICING VEHICLE SELF-PROPELLED, SMALL CAPACITY

1987-03-01
HISTORICAL
ARP4047
This aerospace recommended practice covers requirements for a self-propelled, boom type aerial device, equipped with an aircraft deicing fluid spraying system. The unit shall be highly maneuverable for deicing all exterior surfaces of intermediate size aircraft, e.g. DC-9, B-727 and B-737. The vehicle will also be used for aircraft maintenance and inspection. The vehicle shall be suitable for day and night operations.
Standard

AIRCRAFT TURBINE ENGINE FUEL SYSTEM COMPONENT ENDURANCE TEST PROCEDURE (ROOM TEMPERATURE CONTAMINATED FUEL)

2007-12-04
HISTORICAL
MAP749B
This recommended practice describes a method for conducting room temperature, contaminated fuel, endurance testing when the applicable specification requires nonrecirculation of the contaminants. The objective of the test is to determine the resistance of engine fuel system components to wear or damage caused by contaminated fuel operation. It is not intended as a test for verification of the component’s filter life. ARP1827 is recommended for filter evaluation.
Standard

ALCOHOL, DENATURED ETHYL

1994-01-01
HISTORICAL
AMS3002E
This specification covers a denatured ethyl alcohol in the form of a liquid.
Standard

ALCOHOL, DENATURED ETHYL

1989-07-01
HISTORICAL
AMS3002D
This specification covers a denatured ethyl alcohol in the form of a liquid.
Standard

ALCOHOL, DENATURED ETHYL

1983-01-01
HISTORICAL
AMS3002C
This specification covers a denatured ethyl alcohol in the form of a liquid.
Standard

ALCOHOL, METHYL

1994-01-01
HISTORICAL
AMS3004E
This specification covers methyl alcohol in the form of a liquid.
Standard

ALCOHOL, METHYL

1989-07-01
HISTORICAL
AMS3004D
This specification covers methyl alcohol 1n the form of a liquid.
Standard

ALCOHOL, METHYL

1983-01-01
HISTORICAL
AMS3004C
This specification covers methyl alcohol in the form of a liquid.
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