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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 GAS TURBINE ENGINE EXHAUST SMOKE MEASUREMENT
1970-05-01
HISTORICAL
ARP1179
The purpose of this Aerospace Recommended Practice is to standardize test equipment and procedures for the measurement of smoke emission from aircraft gas turbine engines. The procedures included are for determining and reporting the amount of smoke emission. This document is divided into the following sections: 1 Definitions and Terminology 2 Equipment 3 Test Procedures 4 Information and Data to be Recorded 5 Data Reduction and Analysis 6 Presentation of Results
Standard

AIRCRAFT GAS TURBINE ENGINE EXHAUST SMOKE MEASUREMENT
1970-05-04
HISTORICAL
ARP1179A
This Aerospace Recommended Practice (ARP) standardizes test equipment and procedures for the measurement of smoke emission from aircraft gas turbine engines. The procedures included are for determining and reporting the amount of smoke emission. Tests have indicated that the practically achieveable precision of the smoke number is within ±3 when the system is properly used as outlined herein. This procedure is not intended for in-flight testing, nor does it apply to afterburning engines. This ARP is divided into the following sections: 2 Definitions and Terminology 3 Equipment 4 Test Procedures 5 Information and Data to be Recorded 6 Data Reduction and Analysis 7 Presentation of Results 8 Comments
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 VARIABLE DELIVERY HYDRAULIC PUMPS
1959-02-01
HISTORICAL
AS595
This specification establishes the common requirements for variable delivery, hydraulic pumps, suitable for use in aircraft; and the methods to be used for demonstrating compliance with these 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, 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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