Standard
CAP, PRESSURE SEAL, FLARELESS TUBE FITTING
2023-11-10
CURRENT
AS21914E
Search Results
Standard
NUT - HEXAGON, BOSS CONNECTION, CRES - UNS S30400, 75 KSI
2023-08-01
CURRENT
AS9553C
Standard
ELBOW, TUBE, 45°, BULKHEAD, FLARELESS TUBE UNIVERSAL TO FLARED TUBE
2023-01-17
CURRENT
AS24654B
Standard
ELBOW, TUBE - 90°, BULKHEAD, FLARELESS TUBE UNIVERSAL TO FLARED TUBE
2023-01-17
CURRENT
AS24651B
Standard
ELBOW, TUBE - 90°, BULKHEAD, FLARED TUBE UNIVERSAL TO FLARELESS TUBE
2023-01-17
CURRENT
AS24652B
Standard
TEE, FLARELESS TUBE WITH BULKHEAD ON RUN
2023-01-17
CURRENT
AS21912E
Standard
ELBOW, 90° UNIVERSAL, FLARELESS TUBE, HIGH PROFILE
2023-01-17
HISTORICAL
AS21925E
Standard
TEE, BULKHEAD, FLARELESS TUBE, INTERNAL THREAD ON RUN
2023-01-17
CURRENT
AS21911E
Standard
BACKPLATE, RETRAINING STRAP, AMS5510
2022-10-13
CURRENT
AS9395A
Standard
NUT, PLAIN, HEXAGON, BOSS CONNECTION, SILVER PLATED, 347 CRES UNS S34700
2022-08-26
CURRENT
AS9201D
Standard
FITTING END, STANDARD DIMENSIONS FOR, BULKHEAD, DYNAMIC BEAM SEAL, MALE
2022-05-09
CURRENT
AS85421/2C
Standard
FITTING END, STANDARD DIMENSIONS FOR DYNAMIC BEAM SEAL, MALE
2022-05-02
CURRENT
AS85421/1A
Standard
UNION, FLARELESS TUBE BULKHEAD AND UNIVERSAL
2021-11-23
CURRENT
AS21924F
Standard
Titles, SAE G-3 Committee Document, Selection of
2021-10-21
CURRENT
ARP1987B
This SAE Aerospace Recommended Practice (ARP) establishes the procedure for creating titles of G-3 Committee documents which will be published by the SAE Aerospace Organization. This standardization will avoid several different names describing the same item and will improve alphabetical listings of documents by subject.
Standard
FITTINGS, TUBE, FLUID SYSTEMS, SEPARABLE, HIGH PRESSURE, DYNAMIC BEAM SEAL, DESIGN STANDARD FOR MALE END
2020-10-19
CURRENT
AS85720/1B
Standard
Clamp Assembly, Saddle Type, Cushioned, General Specification For
2020-04-21
CURRENT
AS85449B
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
Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification
2017-07-10
HISTORICAL
AS1650D
This SAE Aerospace Standard (AS) 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, and is designed for use from −65 to +400 °F and at 125 psig nominal operating pressure.
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
Coupling Assembly, Hydraulic, Self-Sealing, Quick Disconnect
2015-07-27
CURRENT
AS25427
This specification covers the detail requirements for aircraft hydraulic self-sealing quick disconnect couplings, for use in types I and II hydraulic systems (-65°F to +275°F temperature range) as defined by Specification MIL-H-5440.
Standard
CLAMP, LOOP, CUSHIONED, ELONGATED, METRIC
2015-04-23
HISTORICAL
MA14272
