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Standard

Hose, Polytetrafluoroethylene TFE Fluorocarbon Resin Wire Braid Reinforced

2019-04-30

CURRENT

AMS3380E

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

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

1965-09-01

HISTORICAL

AMS3380A

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

HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED, HEAVY-DUTY, 275 °F, 3000 psi FLARELESS TITANIUM FITTINGS, INCLUDING JUMP SIZE, 45° TO 90°

2004-06-30

HISTORICAL

AS4628B

Standard

HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED, HEAVY-DUTY, 275 °F, 3000 psi FLARELESS TITANIUM FITTINGS, INCLUDING JUMP SIZE, 45° TO 45°

2004-06-30

HISTORICAL

AS4627B

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

CLAMP, CENTER MOUNT, CUSHIONED, HYDROCARBON FLUID RESISTANT, METRIC

2015-04-27

CURRENT

MA2156/1

Standard

CLAMP, RECTANGULAR LOOP, CUSHIONED, WITH WEDGE, HYDROCARBON FLUID RESISTANT, STAINLESS STEEL, METRIC

2015-04-27

CURRENT

MA2155/2

Standard

CLAMP, RECTANGULAR LOOP, CUSHIONED, WITH WEDGE, HYDROCARBON FLUID RESISTANT, ALUMINUM, METRIC

2015-04-27

CURRENT

MA2155/1

Standard

CLAMP, RECTANGULAR, 2 PIECE, CUSHIONED, WITH WEDGES, HYDROCARBON FLUID RESISTANT, METRIC

2015-04-27

CURRENT

MA2154/1

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

Test Methods for Tube-Fitting Assemblies, Metric (ISO 10583)

2015-08-21

CURRENT

MA2094

This SAE Aerospace Standard (AS) specifies test methods for fitting assemblies used in aircraft fluid systems in the pressure classes B, D, and E, and in temperature Types I, II, and III of MA 2001. This document applies each time that it is referred to in a procurement specification or other definition document. Fluids and materials used for the tests are listed in Section 2.

Standard

HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED, 21 000 KPA, 135 ⁰C, BEAM SEAL, STRAIGHT TO 45⁰, METRIC

2015-04-28

CURRENT

MA5067

Standard

HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED, 21 000 KPA, 135 ⁰C, BEAM SEAL, STRAIGHT TO STRAIGHT, METRIC

2015-04-28

CURRENT

MA5066