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Standard

HOSE, POLYTETRAFLUOROETHYLENE TFE Fluorocarbon Resin Wire Braid Reinforced

1974-12-01

HISTORICAL

AMS3380B

This specification covers polytetrafluoroethylene resin in the form of extruded and sintered flexible hose reinforced with wire braid.

Standard

Hose, Polytetrafluoroethylene TFE Fluorocarbon Resin Wire Braid Reinforced

2012-12-11

HISTORICAL

AMS3380D

This specification covers a polytetrafluoroethylene resin in the form of extruded and sintered flexible tube reinforced with wire braid.

Standard

HOSE, POLYTETRAFLUOROETHYLENE TFE Fluorocarbon Resin Wire Braid Reinforced

1983-07-01

HISTORICAL

AMS3380C

This specification covers polytetrafluoroethylene resin in the form of extruded and sintered flexible hose reinforced with wire braid.

Standard

Hose Assembly, Convoluted Polytetrafluoroethylene, High Temperature, Medium Pressure, Aircraft, Metric

2015-08-21

CURRENT

MA2079

This Aerospace Standard covers hose assemblies intended for use in aircraft high temperature fluid systems. The specified temperature range is -55°C (-67°F) to +204°C (400°F). Operating pressures are listed in Table I.

Standard

Duct Assembly, Ground, Conditioned Air, Metallic Reinforced, Low Pressure, 350 °F

2013-01-09

CURRENT

AS7365

This Aerospace Standard (AS) defines the requirements for a metallic reinforced, duct assembly suitable for use in low pressure, 350 °F ground heaters.

Standard

Clamp Assemblies, Saddle or Omega Style, Two Point Mount, Multiple Shapes, Metric

2015-08-21

CURRENT

MA2151

This aerospace specification establishes the requirements for metric saddle or omega style clamps used for systems installation in aerospace equipment.

Standard

Clamps, Loop or P Style, Single Point Mount, Multiple Shapes, Metric

2015-08-21

CURRENT

MA2150

This aerospace specification establishes the requirements for metric loop or "P" style clamps used for systems installation in aerospace equipment.

Standard

Fluid Couplings for Spacecraft Servicing, Preparation of Specification for, Metric

2015-08-21

CURRENT

MAP2261

This SAE Metric Aerospace Recommended Practice (MAP) establishes the requirements for preparing a specification for fluid couplings for spacecraft servicing. The objective of this document is to provide design, development, verification, storage, and delivery requirement guidelines for the preparation of specifications for fluid couplings and the ancillary hardware for use with serviceable spacecraft designed for use in the space environment. The couplings shall be capable of resupplying storable propellants, cryogenic liquids, and gases to a variety of spacecrafts.

Standard

Color Coding - Elastomers for Tube Clamp Cushions

2014-10-06

CURRENT

ARP1527B

This SAE Aerospace Recommended Practice (ARP) establishes uniform requirements for color coding of elastomeric cushions on clamps used in aerospace tubing systems, wire bundle retention, and similar applications.

Standard

COLOR CODING - ELASTOMERS FOR TUBE CLAMP CUSHIONS

1991-07-01

HISTORICAL

ARP1527A

This Aerospace Recommended Practice (ARP) establishes uniform requirements for color coding of elastomeric cushions on clamps used in aerospace tubing systems, wire bundle retention, and similar applications.

Standard

COLOR CODING - ELASTOMERS FOR TUBE CLAMP CUSHIONS

1980-03-01

HISTORICAL

ARP1527

This Aerospace Recommended Practice (ARP) establishes uniform requirements for color coding of elastomeric cushions on clamps used in aerospace tubing systems, wire bundle retention, and similar applications.

Standard

Fire Test Equipment for Flexible Hose and Tube Assemblies

2013-01-02

HISTORICAL

AIR1377A

This Aerospace Information Report (AIR) describes equivalent types of equipment that can perform fire tests in accordance with requirements of AS 1055.

Standard

Fire Test Equipment for Flexible Hose and Tube Assemblies

2019-02-06

CURRENT

AIR1377B

This Aerospace Information Report (AIR) describes equivalent types of equipment that can perform fire tests in accordance with requirements of AS 1055.

Standard

FIRE TEST EQUIPMENT FOR FLEXIBLE HOSE AND TUBE ASSEMBLIES

1978-04-01

HISTORICAL

AIR1377

This Aerospace Information Report (AIR) describes equivalent types of equipment that can perform fire tests in accordance with requirements of AS 1055.

Standard

Coupling Assembly, Self-Sealing, Quick Disconnect Fuel and Oil System Components

2013-01-02

CURRENT

AS1969

This specification covers the requirements for self-sealing, quick-disconnect couplings for fuel and oil system components.

Standard

Hose Assembly, Tetrafluoroethylene, Lightweight, 204 °C, 21 000 kPa Hydraulic, Metric

2015-08-21

CURRENT

MA2007A

This specification covers lightweight hose assemblies intended for use in high-temperature, 204 °C, high-pressure, 21 000 kPa (210 bar) aircraft hydraulic systems, also for use in pneumatic systems which allow some gaseous diffusion through the PTFE wall.

Standard

Coupling Assembly, Threadless, Flexible, Fixed Cavity, Current Carrying, Self-Bonding, Procurement Specification

2018-10-12

WIP

AS5830B

Remove unsused (developed / unreleased) part standards. The part standards are AS5840, AS5841, AS5842, and AS5843.

Standard

Coupling Assembly, Threadless, Flexible, Fixed Cavity, Current Carrying, Self-Bonding, Procurement Specification

2013-01-09

HISTORICAL

AS5830

This aerospace specification defines the requirements for a threadless, flexible, conductive, self-bonding coupling assembly which, when installed on fixed cavity ferrules, provides a flexible, current carrying connection for joining tubing and components in aircraft fuel, vent and other systems. The assembled coupling is designed to provide interchangeability of parts and components between qualified manufacturers for the service life of the aircraft system. The assembled coupling is for use from -65 to +200 °F at nominal operating pressures (125 psig for -08 through -64 and 30 psig for -72 through -88). This aerospace specification is a departure from prior qualification practices for assembled couplings. Prior practice sought to validate this type of assembled coupling design by conducting a sequence of tests on sets of coupling assemblies. There were multiple test sequences and each was conducted on a different set of coupling assemblies.

Standard

Coupling Assembly, Threadless, Flexible, Fixed Cavity, Current Carrying, Self-Bonding, Procurement Specification

2017-05-16

CURRENT

AS5830A

This aerospace specification defines the requirements for a threadless, flexible, conductive, self-bonding coupling assembly which, when installed on fixed cavity ferrules, provides a flexible, current carrying connection for joining tubing and components in aircraft fuel, vent and other systems. The assembled coupling is designed to provide interchangeability of parts and components between qualified manufacturers for the service life of the aircraft system. The assembled coupling is for use from -65 to +200 °F at nominal operating pressures (125 psig for -08 through -64 and 30 psig for -72 through -88). This aerospace specification is a departure from prior qualification practices for assembled couplings. Prior practice sought to validate this type of assembled coupling design by conducting a sequence of tests on sets of coupling assemblies. There were multiple test sequences and each was conducted on a different set of coupling assemblies.

Standard

Coupling Assemblies, Quick Disconnect, Automatic Shutoff

2019-04-23

CURRENT

AS7413A

This specification establishes requirements for automatic shutoff, quick-disconnect coupling assemblies for fuel and oil lines.