Search Results

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

RING, WELD, 21,000 KPA, CRES, METRIC

2015-04-24

CURRENT

MA2062A

Standard

RING - BACK UP, BOSS CONNECTION, POLYTETRAFLUORETHYLENE

2022-05-09

CURRENT

AS3076A

Standard

RING - BACK-UP, BOSS CONNECTION POLYTETRAFLUORETHYLENE

2012-11-01

HISTORICAL

AS3076

Standard

Hose, Rubber, Wire-Wound, Synthetic, Ice Eliminating System

2013-01-09

CURRENT

AS6399

This document establishes the requirements for a lightweight, nonkink, flexible elastomeric hose. This hose is typically used with air-operated aircraft ice-preventive systems.

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

Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Metric

2015-08-21

CURRENT

MA2241

This document defines the requirements for a threadless, flexible, self-bonding coupling assembly, which, when installed on machined fixed cavity ferrules, provides a flexible connection for joining tubing and components in aircraft fuel, vent, or other systems. This assembled coupling, hereafter referred to as the assembly, is designed for use from -54 to 204 °C and at 862 kPa operating pressure. AS coupling components referenced herein have been qualified to AS1650. Ferrules referenced herein are inch ferrules adapted to metric tubing.

Standard

Coupling Fuel, Flexible Variable Cavity, Threaded Type with Ferrules, Metric

2015-08-21

CURRENT

MA2250

This Aerospace Specification establishes the requirements for a threaded flexible coupling assembly, hereafter referred to as the assembly, which utilizes ferrules or machined tube end fittings to join tubing and components in aircraft fuel, vent, or other systems. This coupling assembly is designed for use from -54 to 93 °C and at 862 kPa peak working pressure. AS coupling components referenced herein have been qualified to AS1710. Ferrule referenced herein are inch ferrules adapted to metric tubing.

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

GASKET, FITTING END, 24° CONE

2015-04-21

CURRENT

AS4825

Standard

Valve; Air Relief, Low Pressure

2013-01-09

CURRENT

AS8712

This specification covers the requirements for one type of low-pressure relief valve for use in pressurized shipping containers.

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.