Search Results

Standard

AERODYNAMIC FAIRING COMPOUND −55° to +85° C −67° to +185° F)

1974-03-01

HISTORICAL

AMS3696

This specification covers a two-component, air-curing, aluminum-powder-filled, epoxy-resin-base material in the form of a paste or putty, suitable for application by spatula or putty-knife.

Standard

SEALING COMPOUND, POLYTHIOETHER, AMBIENT CURE OR IMMEDIATE HEAT CURE For Aircraft Structures, Fuel Resistant With Intermittent Use To 400 °F (204 °C)

1997-03-01

HISTORICAL

AMS3263

This specification covers two classes of a fuel resistant polythioether sealing compound supplied as a two-component system.

Standard

Sealing Compound, Polythioether, Ambient Cure or Immediate Heat Cure For Aircraft Structures, Fuel Resistant with Intermittent Use to 400°CF (204°CC)

2002-12-13

CURRENT

AMS3263A

this specification covers two classes of a guel resistant polythioether sealing compound supplied as a two-component system.

Standard

SEALING COMPOUND, POLYTHIOETHER Nonchromated, Corrosion Inhibiting for Intermittent Use to 360 °F (182 °C)

1996-11-01

HISTORICAL

AMS3259

This specification covers a polythioether sealing compound with nonchromated corrosion inhibitors supplied as a two-component system which cures at room temperature.

Standard

Sealing Compound, Polythioether Nonchromated, Corrosion Inhibiting for Intermittent Use to 360 °F (182 °C)

2004-02-25

HISTORICAL

AMS3259A

This specification covers a polythioether sealing compound with nonchromated corrosion inhibitors supplied as a two-component system which cures at room temperature.

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

COATING MATERIAL, FLUOROCARBON, ELASTOMERIC Rain-Erosion Resistant, Colored

1990-07-01

HISTORICAL

AMS3138/3

This specification covers a fluorocarbon elastomeric coating material for fiber-reinforced-resin composite structures in the form of a two-component brushable or sprayable liquid.

Standard

COATING MATERIAL, FLUOROCARBON, ELASTOMERIC Rain-Erosion and Thermal-Flash Resistant, White

1990-07-01

HISTORICAL

AMS3138/2

This specification covers a fluorocarbon elastomeric coating material for fiber-reinforced-resin composite structures in the form of a two-component, brushable or sprayable liquid.

Standard

COATING MATERIAL, FLUOROCARBON, ELASTOMERIC Rain-Erosion Resistant, Black

1990-07-01

HISTORICAL

AMS3138/1

This specification covers a fluorocarbon elastomeric coating material for fiber-reinforced-resin composite structures in the form of a two-component, brushable or sprayable liquid.

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

AERODYNAMIC FAIRING COMPOUND −55° to +150° C (−67° to +302° F)

1974-03-01

HISTORICAL

AMS3697

This specification covers a two-component, air-curing, aluminum-powder-filled, epoxy- resin-base material in the form of a paste or putty, suitable for application by spatula or putty-knife.

Standard

Sealing Compound, Silicone Rubber, Two-Part, Electrically Conductive and Corrosion Resistant (Nonchromated) for Use from -67 to 500 °F (-55 to 260 °C)

2000-02-01

HISTORICAL

AMS3262

This specification covers a silicone, electrically conductive and corrosion-inhibiting sealing compound.

Standard

Sealing Compound, Silicone Rubber, Two-Part, Electrically Conductive and Corrosion Resistant (Nonchromated) for Use from -67 to 500 °F (-55 to 260 °C)

2011-09-23

CURRENT

AMS3262A

This specification covers a silicone, electrically conductive and corrosion-inhibiting sealing compound.

Standard

SEALING COMPOUND, POLYSULFIDE (T) SYNTHETIC RUBBER for Integral Fuel Tank and Fuel Cell Cavities High Strength, for Intermittent Use to 360°F (182°C)

1993-10-01

HISTORICAL

AMS3269

This specification covers three classes of fuel-resistant polysulfide (T) sealing compound with high strength and temperature characteristics, supplied as a two-component system which cures at room temperature.

Standard

ADHESIVE/SEALANT, FLUOROSILICONE Aromatic Fuel Resistant, One-Part Room Temperature Vulcanizing

1993-07-01

HISTORICAL

AMS3375A

This specification covers a one-part fluorosilicone (FVMQ) adhesive/ sealant, supplied in cartridges, suitable for extrusion and curing to an elastomeric material upon exposure to air. It also covers a compatible primer.

Standard

Adhesive/Sealant, Fluorosilicone Aromatic Fuel Resistant, One-Part Room Temperature Vulcanizing

2001-04-01

HISTORICAL

AMS3375B

This specification covers a one-part fluorosilicone (FVMQ) adhesive/ sealant, supplied in cartridges, suitable for extrusion and curing to an elastomeric material upon exposure to air. It also covers a compatible primer.

Standard

Adhesive/Sealant, Fluorosilicone Aromatic Fuel Resistant, One-Part Room Temperature Vulcanizing

2012-01-17

CURRENT

AMS3375C

This specification covers a one-part fluorosilicone (FVMQ) adhesive/sealant, supplied in cartridges, suitable for extrusion and curing to an elastomeric material upon exposure to air. It also covers a compatible primer.

Standard

Jet Reference Fluid Study for Fuel Tank Sealants

2021-02-03

CURRENT

AIR4275B

This information report covers two distinct projects to formulate Jet Refrence Fluids (JRF) for testing of material compatibility. The first effort began in 1978 and focused on producing a formulation (JRF-2) that simulated JP-4 and included composition with metallic ions that reproduced chalking of fuel tank sealants. This effort resulted in the preparation of AMS2629 that defined the formulation of JRF-2 (Type 1) and the same formulation with metallic ions (Type 2). The second effort began in 2002 and focused on preparing a JRF that simulated Jet A, JP-5 and JP-8. This effort went through multiple iterations, but eventually resulted in a JRF-3 formulation composed of Jet A plus military additives spiked to 25% aromatic content and high levels of sulfur experienced in the global fuel supply. Since the metallic ions added to JRF-2 demonstrated their ability to simulate a chalking reaction, chalking was not tested with the ions added to JRF-3.

Standard

Sealing Compound, Topcoat, Fuel Tank, Buna-N Type

2021-06-29

CURRENT

ARD50102

This specification covers one type of one-component, air-drying protective coating which cures at room temperature.