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Viewing 1711 to 1740 of 1746
HISTORICAL
1960-03-01
Standard
AS407B
This Aeronautical Standard covers two basic types of instruments, or combinations thereof, intended for use in indicating fuel consumption of aircraft engines as follows: Type I - Measure rate of flow of fuel used Type II - Totalize amount of fuel consumed or remaining
HISTORICAL
1959-06-15
Standard
AMS3326
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of February 1995. The requirements of this specification are embodied in the latest issue of AMS 3325.
HISTORICAL
1959-02-01
Standard
ARP575
These recommendations are written to cover the subject of obtaining filter patch test samples from aircraft hydraulic pumps of the categories shown below. The same procedure shall apply regardless of the pump drive category.
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specification has been declared "CANCELLED " by the Aerospace Materials Division, SAE, as of December 2008 and has been superseded by AMS2644.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will remain listed in the Numerical Section of the Index of Aerospace Material Specifications, noting that it has been superseded by AMS2644.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
AS405B
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. This Aeronautical Standard covers two basic types of instruments as follows: Type I - Float Instruments, Type II - Capacitance Instruments.
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
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.
CURRENT
1955-03-01
Standard
AIR42
Certain techniques involved in determining the dirt or abrasive content of aircraft greases are considered inadequate. It is desirable to develop a method of analysis which will definitely identify the quantity, size, and degree of abrasiveness of foreign substances in lubricating greases.
CURRENT
1955-03-01
Standard
AIR41
The purpose of this information report is to summarize and document data regarding possible alternatives to the use of cadmium plating on hardware typical of the aerospace hose and fitting industry. To document and provide access to information obtained by an industry survey.
CURRENT
1955-03-01
Standard
AIR44
The objective of this work was to develop a relatively simple bench test or performance test, or a combination of tests, which would be valid for evaluating greases in respect to load support characteristics, when the greases were used in journal bearings or in actuator-type mechanisms.
CURRENT
1955-03-01
Standard
AIR43
The objective of this investigation was to develop a test method for measuring the resistance to rotation of a ball bearing, caused by the grease in that bearing, as a function of temperature. Low temperatures were of particular interest, and it was desired that the test results be expressed in terms which could be used in mechanism design by proper correction for bearing size, etc. It was also desired that the method be capable of measuring 'break away' as well as the running torque of a bearing filled with grease.
CURRENT
1955-03-01
Standard
AIR39
CURRENT
1955-03-01
Standard
AIR40
The objective of this work was to develop a relatively simple screening or bench test, or a combination of such tests, which would evaluate aircraft greases in respect to corrosion protection under the operating conditions described above.
HISTORICAL
1955-01-01
Standard
J313_195501
Automotive and railroad diesel fuels, in general, are derived from petroleum refinery products which are commonly referred to as middle distillates. Middle distillates represent products which have a higher boiling range than gasoline and are obtained from fractional distillation of the crude oil or from streams from other refining processes. Finished diesel fuels represent blends of middle distillates. The properties of commercial distillate diesel fuels depend on the refinery practices employed and the nature of the crude oils from which they are derived. Thus, they may differ both with and within the region in which they are manufactured. Such fuels generally boil over a range between 163 and 371C degrees (325-700F degrees). Their makeup can represent various combinations of volatility, ignition quality, viscosity, sulfur level, gravity, and other characteristics. Additives may be used to impart special properties to the finished diesel fuel.
HISTORICAL
1954-12-15
Standard
AS407A
To specify minimum requirements for Fuel Flowmeters for use primarily in reciprocating engine powered civil transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aeronautical Standard covers two basic types of instruments, or combinations thereof, intended for use in indicating fuel consumption of aircraft engines as follows: TYPE I - Measure rate of flow of fuel used. TYPE II - Totalize amount of fuel consumed or remaining.
HISTORICAL
1952-02-01
Standard
AMS3028B
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE as of March 1990.
HISTORICAL
1952-02-01
Standard
AMS3032B
This specification has been "SUPERSEDED" by the Aerospace Materials Division, SAE, as of 2 November 1990.
HISTORICAL
1952-02-01
Standard
AMS3034
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE.
HISTORICAL
1952-02-01
Standard
AMS3036B
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE.
HISTORICAL
1951-06-01
Standard
AMS3500B
This specification covers leather tanned with chromium salts and retanned with vegetable tanning material.
HISTORICAL
1950-06-01
Standard
AMS3110C
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
HISTORICAL
1949-03-01
Standard
AMS3110B
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
HISTORICAL
1948-11-01
Standard
AS407
To specify minimum requirements for Fuel Flowmeters for use primarily in reciprocating engine powered civil transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aeronautical Standard covers two basic types of instruments, or combinations thereof, intended for use in indicating fuel consumption of aircraft engines as follows: TYPE I - Measure rate of flow of fuel used. TYPE II - Totalize amount of fuel consumed or remaining.
HISTORICAL
1948-11-01
Standard
AS405
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
1948-07-01
Standard
AMS3028A
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE as of March 1990.
HISTORICAL
1948-07-01
Standard
AMS3032A
This specification has been "SUPERSEDED" by the Aerospace Materials Division, SAE, as of 2 November 1990.
HISTORICAL
1948-07-01
Standard
AMS3036A
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE.
CURRENT
1948-03-01
Standard
AS214
HISTORICAL
1947-12-01
Standard
AMS3110A
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
HISTORICAL
1946-11-01
Standard
AMS3032
This specification has been "SUPERSEDED" by the Aerospace Materials Division, SAE, as of 2 November 1990.
Viewing 1711 to 1740 of 1746