Standard
CLEANER FOR AIRCRAFT EXTERIOR METALLIC SURFACES WIPE SOLVENT, COLD OPERATIONS
1995-01-01
HISTORICAL
AMS1525D
Search Results
Standard
CLEANER FOR EXTERIOR AIRCRAFT SURFACES Thickened or Gel-Type, Water-Base
1996-09-01
HISTORICAL
AMS1523
This specification covers a thickened, water-base, non-solvent type cleaner in the form of a gel.
Standard
Cleaner for Exterior Aircraft Surfaces Gel-Type, Solvent-Base
2004-02-25
HISTORICAL
AMS1533A
This specification covers a solvent-base cleaner in the form of a gel.
Standard
Cleaner for Exterior Aircraft Surfaces Gel-Type, Solvent-Base
2008-03-05
HISTORICAL
AMS1533B
This specification covers a solvent-base cleaner in the form of a gel.
Standard
Cleaner for Exterior Aircraft Surfaces Gel-Type, Solvent-Base
2019-01-08
CURRENT
AMS1533C
This specification covers a solvent-base cleaner in the form of a gel.
Standard
Cleaner for Exterior Aircraft Surfaces Thickened or Gel-Type, Water-Base
2000-01-01
HISTORICAL
AMS1523A
This specification covers a thickened, water-base, type cleaner in the form of a gel.
Standard
Cleaner for Exterior Aircraft Surfaces Thickened or Gel-Type, Water-Base
2019-06-03
CURRENT
AMS1523B
This specification covers a thickened, water-base, type cleaner in the form of a gel.
Standard
Cleaning Compound, Precoating Surface, Aircraft and Aerospace Ground Equipment (AGE)
2010-12-13
CURRENT
AMSC83873A
This specification establishes the requirements for biodegradable, enzyme based, precoating surface cleaners.
Standard
Cleaning/Scale Removing Compound Aircraft Vacuum Toilet Systems
2023-07-06
CURRENT
AMS1454A
This specification covers a cleaning/scale removing compound in the form of a liquid concentrate or gel.
Standard
Compound, Cleaning Gel for Aircraft Surfaces
2017-12-15
CURRENT
AMS79_015
This SAE Standard specifies requirements for a gelled compound for cleaning the soiled exterior of service aircraft. The cleaning gel may be applied by pressure pump as a thixotropic liquid, by brushing or by swabbing. The surfaces to be cleaned may be unpainted metal or surfaces painted with glossy or matt schemes, including strippable acrylic paint complying with DTD 5599. This Standard includes tests to limit specific forms of corrosion that affect aircraft structural materials.
Standard
Corrosion Removing Compound for Aircraft Surfaces
2024-02-12
CURRENT
AMS1640D
This specification establishes requirements for a corrosion-removing compound in the form of a liquid concentrate.
Standard
Corrosion of Aluminum Alloys By Aircraft Maintenance Chemicals, Sandwich Test
1991-10-01
CURRENT
ARP1512B
Standard
Corrosion of Low-Embrittling Cadmium Plate By Aircraft Maintenance Chemicals
1991-10-01
CURRENT
ARP1511B
Standard
Deodorant, Aircraft Toilet, Formaldehyde Base
2001-08-01
CURRENT
AMS1475C
This specification covers a biodegradable, formaldehyde-base material, containing additives, in the form of a concentrated liquid.
Standard
Disinfectant Cleaner for Aircraft Interior General Purpose Liquid
2023-07-24
CURRENT
AMS1453A
This specification covers a general purpose disinfectant in the form of a concentrated liquid to be used diluted in accordance with label instructions.
Standard
Disinfectant, Aircraft General Purpose
2023-07-24
CURRENT
AMS1452C
This specification covers a general-purpose disinfectant in the form of a concentrated liquid.
Standard
Hydrogen Embrittlement Effect on Metals By Aircraft Maintenance Chemicals, Mechanical Test Methods
1977-07-01
CURRENT
ARP1525
The Test Procedure of ARP 1525 is Embodied in ASTM F519, Hydrogen Embrittlement Testing of Aerospace Materials. The requirements of the latest issue of ASTM F519 shall be fulfilled whenever reference is made to ARP1525.)
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.
