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

Routine Inspection and Test Procedures for Aircraft Refueling Hoses

2002-12-16

CURRENT

ARP605

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

GASKET, FITTING END, 24° CONE

2015-04-21

CURRENT

AS4825

Standard

Hose, Aircraft Fueling, Acrylonitrile Butadiene (NBR) Rubber Single Wire Braid Reinforced, Chloroprene Covered, Noncollapsing

2019-04-30

CURRENT

AMS3388E

This specification covers a synthetic rubber in the form of a non-rigid, smooth bore, noncollapsing-type hose.

Standard

Hose, Aircraft Fueling, Acrylonitrile Butadiene (NBR) Rubber Double Wire Braid Reinforced, Chloroprene Covered, Noncollapsing

2019-04-30

CURRENT

AMS3389E

This specification covers a synthetic rubber in the form of a nonrigid, smooth bore, noncollapsing-type hose.

Standard

Hose, Aircraft Fueling, Acrylonitrile Butadiene (NBR) Rubber, Textile Reinforced, Chloroprene Covered, Collapsing

2019-04-30

CURRENT

AMS3386E

This specification covers a synthetic rubber in the form of a soft wall, smooth bore, collapsing-type hose.

Standard

Titles, SAE Subcommittee G-3E Aerospace Tubing Installation Documents, Selection Of

2013-01-02

CURRENT

ARP1987/3

The scope of this SAE Aerospace Recommended Practice (ARP) is to establish the procedure for creating titles of aerospace tubing and clamp installation documents generated by SAE Subcommittee G-3E.

Standard

FERRULE END, COUPLING, FLEXIBLE, VARIABLE CAVITY, THREADED, FERRULE TYPE, DESIGN STANDARD

1984-01-01

HISTORICAL

AS1720A

Standard

FITTING END, COUPLING, FLEXIBLE VARIABLE CAVITY THREADED, FERRULE TYPE DESIGN STANDARD

2013-01-02

CURRENT

AS1720B

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

Adapter - Port Connection, Ring Locked Installation and Removal of

2017-03-01

CURRENT

MA2114B

This SAE Aerospace Standard provides the essential minimum design, installation and removal standard for MA2111, MA2112, MA2113, and MA2119 adapters, and is applicable when specified on engineering drawings or in procurement documents.

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.