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Standard

Disinfectant (Insecticide), Aircraft

2018-09-28
CURRENT
AMS1450B
This specification covers insecticides for use in disinsection of aircraft as required on international passenger flights.
Standard

Compound, Hot Carbon and Paint Remover Aircraft Turbine Engine Components

2015-05-06
WIP
AMS1385B
This specification covers a solvent-based compound in the form of a liquid. This compound has been used typically for removal of carbonaceous soils and paint from aircraft turbine engine parts by immersion in liquid at elevated temperature, but usage is not limited to such applications. This compound should not be used on steel parts having hardness of 40 HRC or over.
Standard

Training for Quality Control of Overhaul Chemical Process Operators (Parts Cleaners)

2013-10-20
CURRENT
ARP6240
The task of chemical process operator in the parts cleaning area is generally considered unskilled labor and in the past, little or no training had been provided or recommended. Since overhaul cleaning is a critical process step prior to visual and fluorescent penetrant inspection processes, consideration must be given to minimum levels of training for these process operators. It is the responsibility of the department supervisor to ensure that all personnel within the department are trained to acceptable level in all general aspects of health and safety and basic operating procedures. This document is intended to augment the local quality control system which will control the application and frequency of the guidelines stated within.
Standard

Scale Conditioner, Alkaline Aircraft Turbine Engine Components

2013-09-04
WIP
AMS1380B
This specification covers a strongly alkaline scale conditioner in the form of a liquid or a water-soluble powder. This product has been used typically in conditioning heat scale formed on aircraft turbine engine high-temperature alloy part by immersion in a solution of the compound at elevated temperature, but usage is not limited to such applications. These compounds are unsuitable for cleaning aluminum parts.
Standard

Acid, Inhibited Phosphoric Aircraft Turbine Engine Components Room Temperature Application

2013-09-04
WIP
AMS1384B
This specification covers an inhibited phosphoric acid in the form of a liquid concentrate or a water soluble powder for dilution with water. Primarily for derusting of aircraft turbine engine ferrous components and removal of heat scale and other contamination from the surface of nickel alloys by immersion at room temperature. Should not be used on steel parts having hardness of 40 HRC or over.
Standard

Oxide Conditioner, Alkaline Permanganate Aircraft Turbine Engine Components

2013-09-04
WIP
AMS1383B
This specification covers an alkaline permanganate oxide conditioner in the form of a water-soluble powder or a liquid for dilution with water. This product has been used typically for conditioning of oxidation products on aircraft turbine engine components fabricated from steels, nickel alloys, and cobalt alloys by immersion in a solution of the cleaner at elevated temperature, but usage is not limited to such applications.
Standard

Urea Compound, Powder

1994-03-01
CURRENT
AMS1731B
This specification has been designated as "SUPERSEDED" by the Aerospace Materials Division, SAE, as of May 17, 1993. The requirements of this specification are embodied in the latest issue of AMS 1431.
Standard

CLEANING EFFICIENCY OF TURBINE ENGINE GAS PATH CLEANERS Laboratory Test Method

1991-10-01
CURRENT
ARP1862A
This SAE Aerospace Recommended Practice (ARP) covers a laboratory procedure for determining the cleaning efficiency of aircraft turbine engine gas path cleaners. Results are indicative of cleaning compound performance in the compressor sections of installed aircraft turbine engines, when used in a starter crank/soak/rinse application.
Standard

Stress Corrosion of Titanium Alloys, Effect of Cleaning Agents on Aircraft Engine Materials

1990-10-01
CURRENT
ARP1795A
This document establishes a test procedure for determining the propensity of aircraft turbine engine cleaning and maintenance materials for causing stress-corrosion cracking of titanium alloy parts. The evaluation is conducted on representative titanium alloys by determining the effect of contact with cleaning and maintenance materials on tendency of pre-stressed titanium alloys to crack when subsequently heated to elevated temperatures.
Standard

CLEANING EFFICIENCY OF TURBINE ENGINE GAS PATH CLEANERS Laboratory Test Method

1986-10-01
HISTORICAL
ARP1862
This recommended practice covers a laboratory procedure for determining the cleaning efficiency of aircraft turbine engine gas path cleaners. Results are indicative of cleaning compound performance in the compressor sections of installed aircraft turbine engines, when used in a starter crank/soak/rinse application.
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