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HISTORICAL
1958-08-01
Standard
AMS3388
This specification covers a synthetic rubber in the form of a non-rigid, smooth bore, noncollapsing-type hose. This hose has been used typically for fueling aircraft, but usage is not limited to such applications. This hose is not intended for flexible connection between tractor and trailer, to be collapsed for drainage, or for operating pressures higher than 185 psi (1276 kPa).
HISTORICAL
1958-08-01
Standard
AMS2635
Primarily for determining the presence of cracks, porosity, blowholes, inclusions, and other imperfections which may or may not be exposed to the surface and which may be detrimental to usage of the parts.
HISTORICAL
1958-08-01
Standard
AMS3155
This specification has been declared "CANCELLED " by the Aerospace Materials Division, SAE, as of December 2008 and has been superseded by AMS2644. The requirements of the latest issue of AMS2644 shall be fulfilled whenever reference is made to the cancelled AMS3155. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications, noting that it has been superseded by AMS2644.
HISTORICAL
1958-08-01
Standard
AMS3156
This specification has been declared "CANCELLED " by the Aerospace Materials Division, SAE, as of December 2008 and has been superseded by AMS2644. The requirements of the latest issue of AMS2644 shall be fulfilled whenever reference is made to the cancelled AMS 3156. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications, noting that it has been superseded by AMS2644.
HISTORICAL
1958-07-15
Standard
ARP433
This Aeronautical Recommended Practice covers Liquid Oxygen Quantity Indicators for use with associated Liquid Oxygen converters.
HISTORICAL
1958-07-15
Standard
AS405B
This Aeronautical Standard covers two basic types of instruments as follows: Type I - Float Instruments Type II - Capacitance Instruments
HISTORICAL
1958-07-15
Standard
AS398A
This Aeronautical Standard covers two basic types of instruments as follows:
CURRENT
1958-07-15
Standard
AS403A
CURRENT
1958-07-01
Standard
AS396B
This Aeronautical Standard covers both direct and repeating type gyroscopically stabilized Bank and Pitch Indicating Instruments.
HISTORICAL
1958-07-01
Standard
AS397A
This Aeronautical Standard covers two basic types as follows: Type I - Air Operated Type II - Electrically Operated
CURRENT
1958-07-01
Standard
AS394A
This Aeronautical Standard covers four (4) basic types of direct indicating instruments as follows: TYPE I - Range 0-2000 feet per minute climb and descent TYPE II - Range 0-3000 feet per minute climb and descent TYPE III - Range 0-4000 feet per minute climb and descent TYPE IV - Range 0-6000 feet per minute climb and descent
HISTORICAL
1958-07-01
Standard
AS399A
This Aeronautical Standard covers minimum requirements for gyroscopically stabilized Magnetic Direction Instruments for use in aircraft.
HISTORICAL
1958-02-15
Standard
ARP427
This Aeronautical Recommended Practice covers two types of two unit Pressure Ratio Instruments each of which consist of a Transducer and an Indicator. The Transducer computes the ratio of two pressures and converts this ratio to a synchro electrical signal which is transmitted to the Indicator.
CURRENT
1958-02-15
Standard
ARP464
HISTORICAL
1958-01-01
Standard
AMS2640F
This specification has been declared 'CANCELLED' by the Aerospace Materials Division SAE, as of April 1996. and has been superseded ASTM E 1444.
HISTORICAL
1957-11-15
Standard
ARP419
These recommendations cover the mechanical and electrical installation and installation test procedures for automatic pilots of the type normally used in transport type aircraft. The material in this ARP does not supercede any airworthiness requirement in the Civil Air Regulations.
HISTORICAL
1957-11-15
Standard
ARP492
This SAE Aerospace Recommended Practice (ARP) defines procedures for testing aircraft engine fuel pumps for th epurpose of determining their resistance to eterioration, during steady state endurance test, while receiving MIL-T-5624 Grade JP-4 fuel as a homogenous mixture of gas and liquid expressed as a ratio of vapor volume to liquid volume (V/L). The procedure recommended herin is based on experience gathered by a number of laboratories conducting component qualification tests to MIL-E-5009, currently MIL-E-5007. It is intendd to produce a uniform reproducible steady state test condition for fuel pump cavitation testing as required by various military engine specifications. This test is NOT intended to establish altitude, climb rate, starting, or other transient performance of the article tested.
HISTORICAL
1957-11-15
Standard
AS524
HISTORICAL
1957-11-15
Standard
AS468
No scope available.
HISTORICAL
1957-11-15
Standard
AS472
No scope available.
HISTORICAL
1957-11-15
Standard
AS471
No scope available.
HISTORICAL
1957-11-15
Standard
AS470
No scope available.
HISTORICAL
1957-11-01
Standard
ARP485
HISTORICAL
1957-11-01
Standard
AS473
No scope available.
HISTORICAL
1957-07-01
Standard
J80_195707
This SAE Recommended Practice covers the requirements for rubber floor mats made from five types of rubber compounds as required by the physical property requirements of the application.
HISTORICAL
1956-12-15
Standard
AS405A
This Aeronautical Standard covers two basic types of instruments as follows: Type I - Float Instruments, Type II - Capacitance Instruments. To specify minimum requirements for Fuel and Oil Quantity Instruments for use in aircraft, the operation of which may subject the instruments to the environmental conditions specified in Paragraph 3.3.
HISTORICAL
1956-12-15
Standard
AS412A
This Aeronautical Standard covers the basic type of carbon monoxide detector instrument used to determine toxic concentrations of carbon monoxide by the measurement of heat changes through catalytic oxidation.
HISTORICAL
1956-12-15
Standard
AS418
This Aeronautical Standard covers the basic type of maximum allowable airspeed indicators used to indicate continuously both the indicated airspeed and the maximum allowable airspeed in the ranges shown below;
HISTORICAL
1956-12-01
Standard
AIR64
This AIR is intended as a status report on the of E.C.S. to date in dealing with the problem of equipment cooling in present and immediate future civil transport aircraft. Subsequent revisions to this AIR will follow as more information is gathered on this subject.
Viewing 7261 to 7290 of 7371