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Standard

AEROSPACE FUEL SYSTEM SPECIFICATIONS AND STANDARDS

1976-03-01

HISTORICAL

AIR1408

This report lists military and industry specifications and standards which are commonly used in aerospace gas turbine fuel systems. It is intended as a supplement to specifications MIL-F-3863, MIL-F-17874 and MIL-F-8615. Revisions and amendments which are current for these specifications and standards are not listed.

Standard

AGE CONTROL OF AGE SENSITIVE ELASTOMERIC MATERIALS

1975-05-01

HISTORICAL

AIR1364

This report summarizes data and background relative to age control of specific classes of those nitrile type synthetic elastomers used in sealing devices which are resistant to petroleum base hydraulic fluids, lubricating oils and aircraft fuels. This includes, but is not limited to, those nitrile (NBR or BUNA-N) elastomers specifically covered by Section I of MIL-STD-1523.

Standard

AIRCRAFT AND AIRCRAFT ENGINE FUEL PUMP LOW LUBRICITY FLUID ENDURANCE TEST

1991-05-28

HISTORICAL

ARP1797

This procedure is intended to apply to fuel pumps.

Standard

AIRCRAFT BRAKE TEMPERATURE MONITOR SYSTEMS (BTMS)

1992-06-01

HISTORICAL

AS1145A

This specification covers minimum requirements for brake temperature monitoring equipment whenever used on any type and model of civil aircraft. It shall be the responsibility of the purchaser to determine the compatibility of these requirements with the application aircraft and to specify requirements in excess of these minimums as necessary.

Standard

AIRCRAFT ENGINE FUEL PUMP CAVITATION ENDURANCE TEST

1977-08-15

HISTORICAL

ARP492B

This procedure is intended to apply to all pumps downstream of engine inlet.

Standard

AIRCRAFT ENGINE FUEL PUMP CAVITATION ENDURANCE TEST

1963-10-30

HISTORICAL

ARP492A

This procedure is intended to apply to all pumps down stream of engine inlet.

Standard

AIRCRAFT FUEL PUMP CAVITATION ENDURANCE TEST

1957-11-15

HISTORICAL

ARP492

This procedure is intended to apply to any aircraft fuel pump which supplies liquid hydrocarbon fuel either directly to an aircraft engine or to another pump mounted on an aircraft engine, except that it is not intended to apply to a fuel pump mounted in a fuel tank.

Standard

AIRCRAFT FUEL SYSTEM AND COMPONENT ICING TEST

1979-03-15

HISTORICAL

ARP1401

This Aerospace Recommended Practice (ARP) covers a brief discussion of the icing problem in aircraft fuel systems and different means that have been used to test for icing. Fuel preparation procedures and icing tests for aircraft fuel systems and components are proposed herein as a recommended practice to be used in the aircraft industry for fixed wing aircraft and their operational environment only. In the context of this ARP, the engine is not considered to be a component of the aircraft fuel system, for the engine fuel system is subjected to icing tests by the engine manufacturer for commercial and particular military applications.

Standard

AIRCRAFT FUEL SYSTEM VAPOR-LIQUID RATIO PARAMETER

1974-01-01

HISTORICAL

AIR1326

The AIR is limited to a presentation of the historical background, the technical rationale which generated the V/L fuel condition interface requirement in specifications between the aircraft fuel delivery system and the aircraft engine fuel system, and limitations in the usage of the V/L concept.

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

AIRCRAFT TURBINE FUEL CONTAMINATION HISTORY AND ENDURANCE TEST REQUIREMENTS

1994-03-01

HISTORICAL

AIR4023A

This document discusses the history and development of endurance requirements, provides an analysis of test contaminant material and includes a discussion of future requirements.

Standard

AIRCRAFT TURBINE FUEL CONTAMINATION HISTORY AND ENDURANCE TEST REQUIREMENTS

2011-08-10

HISTORICAL

AIR4023

This AIR discusses the history and development of endurance requirements, provides an analysis of test contaminant material and includes a discussion of future requirements.

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, DENATURED ETHYL

1967-11-01

HISTORICAL

AMS3002B

Standard

ALCOHOL, DENATURED ETHYL

1948-11-01

HISTORICAL

AMS3002

Standard

ALCOHOL, DENATURED ETHYL

1951-06-01

HISTORICAL

AMS3002A

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.