Standard
CLAMP, LOOP TYPE, CUSHIONED SUPPORT
2019-01-16
HISTORICAL
AS21919B
Search Results
Standard
CLAMP, LOOP TYPE, CUSHIONED SUPPORT
2017-08-24
HISTORICAL
AS21919A
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
COUPLING - CLAMP, GROOVE V-BAND 6.400, 9.400, 11.400 FLANGE OD
2006-10-10
HISTORICAL
AS976
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
Clamp Assembly, Loop Type, Cushioned, General Specification For
2015-07-27
HISTORICAL
AS85052A
This SAE Aerospace Standard (AS) defines the requirements for loop type clamps primarily intended for general clamping of tubing for aircraft hydraulic systems.
Standard
Clamp Assembly, Saddle Type, Cushioned, General Specification For
2015-07-27
HISTORICAL
AS85449A
This SAE Aerospace Standard (AS) defines the requirements for saddle-type clamps. Tests and criteria noted do not indicate any specific areas of application or usage. Supplemental testing may be necessary to determine suitability for specific environments and applications.
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
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
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.
Standard
Coupling Assemblies, Quick Disconnect, Automatic Shutoff
2011-06-08
HISTORICAL
AS7413
This specification establishes requirements for automatic shutoff, quick-disconnect coupling assemblies for fuel and oil lines.
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
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
Couplings, Hose, Reattachable Screw-On
2013-01-07
CURRENT
AS38404
This document establishes the requirements for screw-on type reattachable couplings for use in low temperature hose assemblies.
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
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
FLANGE END, SOLID, WIDE DESIGN STANDARD
2013-01-07
CURRENT
AS4751/3
