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AMS1384B - Acid, Inhibited Phosphoric Aircraft Turbine Engine Components Room Temperature Application

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Document Number: AMS1384B
Project Initiation: 09-04-2013
Project Number:
Revision Number: B
Sponsor Name: Juliana Garcia
Title
Acid, Inhibited Phosphoric Aircraft Turbine Engine Components Room Temperature Application
Scope
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.
Rationale
This document has been determined to contain basic and stable technology which is not dynamic in nature.
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