Standard
Silicone Rubber Compound Room Temperature Vulcanizing, 55,000 Centipoise Viscosity Durometer 55 - 70
2012-01-17
CURRENT
AMS3366C
Search Results
Standard
Silicone Rubber Compound Room Temperature Vulcanizing, 50,000 Centipoise Viscosity Short Application Life, Durometer 35 - 55
2001-04-01
HISTORICAL
AMS3364C
This specification covers a silicone rubber in the form of a two-component liquid compound.
Standard
Silicone Rubber Compound Room Temperature Vulcanizing, 50,000 Centipoise Viscosity Short Application Life, Durometer 35 - 55
2012-01-17
CURRENT
AMS3364D
This specification covers a silicone rubber in the form of a two-component liquid compound.
Standard
Silicone Rubber Compound Room Temperature Vulcanizing, 50,000 Centipoise Viscosity Durometer 30 - 45
2012-01-17
CURRENT
AMS3363E
This specification covers a silicone rubber in the form of a two-component liquid compound.
Standard
Silicone Rubber Compound Room Temperature Vulcanizing, 50,000 Centipoise Viscosity Durometer 30 - 45
2001-04-01
HISTORICAL
AMS3363D
This specification covers a silicone rubber in the form of a two-component liquid compound.
Standard
Silicone Rubber Compound Room Temperature Vulcanizing, 15,000 Centipoise Viscosity Durometer 35 - 55
2001-04-09
HISTORICAL
AMS3362C
This specification covers a silicone rubber in the form of a two-component liquid compound.
Standard
Silicone Rubber Compound Room Temperature Vulcanizing, 15,000 Centipoise Viscosity Durometer 35 - 55
2012-01-17
CURRENT
AMS3362D
This specification covers a silicone rubber in the form of a two-component liquid compound.
Standard
Sealing of Integral Fuel Tanks
1998-05-01
HISTORICAL
AIR4069A
This SAE Aerospace Information Report (AIR) presents preferred practices for sealing of aircraft integral fuel tanks, including rework of applied fuel tank seals. It addresses engineering designs for integral fuel tanks as they are currently found in practice; and this document discusses the most practical and conservative methods for producing a reliable, sealed system. Design preferences for optimum sealing are not within the scope of this document. Such discussions can be found in the Air Force sponsored handbook, entitled Aircraft Integral Fuel Tank Design Handbook, AFWAL-TR-87-3078. Key objectives of the fuel tank sealing process are to produce a sealing plane that is leak-free and corrosion resistant, especially at fastener locations, at environmental and operational conditions expected for the life of each air vehicle.
Standard
Sealing and Coating Compound: Polyurethane (PUR) Fuel Resistant High Tensile Strength / Elongation For Integral Fuel Tanks / Fuel Cavities / General Purpose
2008-01-03
HISTORICAL
AMS3278A
This specification covers polyurethane (PUR) in the form of two-component sealing compounds.
Standard
Sealing and Coating Compound, Polyurethane (PUR) Fuel Resistant High Tensile Strength / Elongation For Integral Fuel Tanks / Fuel Cavities / General Purpose
2016-10-24
HISTORICAL
AMS3278B
This specification covers polyurethane (PUR) in the form of two-component sealing compounds.
Standard
Sealing Tape, Sheet, or Gasket, Polytetrafluoroethylene, Expanded (EPTFE) Oil and Water Resistant
2010-08-18
HISTORICAL
AMS3255A
This specification establishes the requirements for an expanded polytetrafluoroethylene (EPTFE) in the form of sealing tape, gaskets, or sheets requiring no mixing or curing.
Standard
Sealing Tape, Sheet, or Gasket, Polytetrafluoroethylene, Expanded (EPTFE) Oil and Water Resistant
2017-07-17
CURRENT
AMS3255B
This specification establishes the requirements for an expanded polytetrafluoroethylene (EPTFE) in the form of sealing tape, gaskets, or sheets requiring no mixing or curing.
Standard
Sealing Compounds, Quick Repair, Low Temperature Curing Polysulfide, for Aircraft Structures
2001-06-01
HISTORICAL
AMSS85420
This specification establishes requirements for two types and classes of a two component, low temperature curing, polysulfide, sealing compound for use as a quick-repair material for aircraft structure.
Standard
Sealing Compounds, Quick Repair, Low Temperature Curing Polysulfide, for Aircraft Structures
2011-09-23
CURRENT
AMSS85420A
This specification establishes requirements for two types and classes of a two component, low temperature curing, polysulfide, sealing compound for use as a quick-repair material for aircraft structure.
Standard
Sealing Compound, Thread and Gasket, Fuel, Oil, and Water Resistant
2001-05-01
HISTORICAL
AMSS7916A
This specification establishes the requirements for sealing compounds used on threads and gaskets.
Standard
Sealing Compound, Temperature Resistant, Integral Fuel Tanks and Fuel Cell Cavities, High Adhesion
2005-03-03
HISTORICAL
AMSS8802B
This specification covers temperature resistant, two-component synthetic rubber compounds of the polysulfide type for sealing and repairing integral fuel tanks and fuel cell cavities, for continuous service use from −65 to +250 °F (−54 to 121 °C).
Standard
Sealing Compound, Temperature Resistant, Integral Fuel Tanks and Fuel Cell Cavities, High Adhesion
2011-03-28
HISTORICAL
AMSS8802C
This specification covers temperature resistant, two-component synthetic rubber compounds of the polysulfide type for sealing and repairing integral fuel tanks and fuel cell cavities, for continuous service use from -65 to +250 °F (-54 to 121 °C).
Standard
Sealing Compound, Polythioether, for Aircraft Structures, Fuel and High Temperature Resistant, Fast Curing at Ambient and Low Temperatures
2011-02-18
CURRENT
AMSS29574A
This specification establishes the requirements for two types and three classes of a two component, fast curing at low and ambient temperature, polythioether sealing compound for use in sealing integral fuel tanks and other aircraft structures. Temperature capabilities are identified in 1.2.1.
Standard
Sealing Compound, Polythioether, for Aircraft Structures, Fuel and High Temperature Resistant, Fast Curing At Ambient and Low Temperatures
2001-07-01
HISTORICAL
AMSS29574
This specification establishes the requirements for two types and three classes of a two component, fast curing at low and ambient temperature, polythioether sealing compound for use in sealing integral fuel tanks and other aircraft structures. Temperature capabilities are identified in 1.2.1.
Standard
Sealing Compound, Polythioether Rubber, Light-Cured, for Integral Fuel Tanks and General Purpose, Intermittent use to 360 °F (182 °C)
2022-04-25
CURRENT
AMS1389
This specification covers polythioether rubber fuel resistant sealing compounds, supplied as a two-component system, which cure rapidly when exposed to a cure on demand (CoD) light source used to initiate a reaction that generates crosslinking of sealant polymers. Type 2 compounds also cure at ambient conditions, without light exposure.
