Standard
HIGH CONFORMANCE SEAL, TYPE I AND II STANDARD AND LOW PROFILE
2024-01-16
CURRENT
AS1895/23D
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Standard
SEAL, TYPE I AND II STANDARD AND LOW PROFILE
2024-01-16
CURRENT
AS1895/7J
Standard
RING - BACK-UP, PORT CONNECTION, AMS2660, METRIC
2023-09-01
CURRENT
MA2515A
Standard
Fittings, Tube, Fluid Systems, Separable, High Pressure Beam Seal, 5000/8000 psi, General Specification for
2022-09-30
CURRENT
AS85720C
This specification covers the design requirements and test procedures for separable beam seal fittings which include end fittings (see 2.4.2), connectors (see 2.4.3), and boss fittings for use in aerospace fluid systems. Design requirements are for Class 5000 and 8000 in titanium, and corrosion resistant steel (CRES). Definition of fittings and related terms are defined in 2.4.
Standard
RING - BACK UP, BOSS CONNECTION, POLYTETRAFLUORETHYLENE
2022-05-09
CURRENT
AS3076A
Standard
FITTING END, STANDARD DIMENSIONS FOR, BULKHEAD, DYNAMIC BEAM SEAL, MALE
2022-05-09
CURRENT
AS85421/2C
Standard
FITTING END, BULKHEAD FLARED TUBE, FOR SEAL RING, STANDARD DIMENSIONS FOR, DESIGN STANDARD
2021-12-13
CURRENT
AS1099D
Standard
Preparation for Delivery, General Requirements for Hose Assemblies
2021-10-21
CURRENT
ARP1835A
This Aerospace Recommended Practice covers general requirements for preservation, packaging, and packing of hose assemblies.
Standard
FITTING, TEE, STANDARD AND REDUCER, BULKHEAD ON RUN, INTERNAL PORT ON RUN, FLARED
2021-05-18
CURRENT
AS1032H
Standard
FITTING, TEE, STANDARD AND REDUCER, BULKHEAD ON RUN, INTERNAL PORT ON SIDE, FLARED
2021-05-18
CURRENT
AS1031G
Standard
Fittings, Tube, Fluid Systems, Separable, Beam Seal, 3000/4000 psi, General Specification for
2021-05-18
CURRENT
AS85421C
This specification covers the design requirements and test procedures for separable beam seal fittings which includes end fittings (see 2.3.4), fitting bodies (see 2.3.7), and boss fittings (see 2.3.2) for use in aerospace fluid systems. Design requirements are for class 3000 in corrosion resistant steel (15-5 PH, 17-4 PH CRES) only and for class 4000 in titanium alloy (Ti) and corrosion and heat-resistant steel (nickel alloy 718 CRES) only. Definition of fittings and related terms are defined in 2.3.
Standard
Clamp Loads and Bending Stresses in Aircraft Tubing Installations
2020-10-09
CURRENT
AIR1593A
This SAE Aerospace Information Report (AIR) contains information relative to stresses and loads developed in tubes caused by tube deflections encountered in misaligned installations. Users are advised that when calculating the stresses and loads of a tubing system, the yield strength of existing loop clamp material is significantly lower than the tubing materials specified herein and should be considered.
Standard
HIGH CONFORMANCE SEAL, TYPE I & II STANDARD AND LOW PROFILE
2019-09-27
HISTORICAL
AS1895/23B
Standard
SEAL, TYPE I & II STANDARD AND LOW PROFILE
2019-09-27
HISTORICAL
AS1895/7G
Standard
TEE, BULKHEAD ON RUN, STANDARD AND REDUCER, REDUCED BODY, FLARELESS
2019-07-29
CURRENT
AS4134E
Standard
ELBOW, 90°, BULKHEAD, STANDARD AND REDUCER, REDUCED BODY, FLARELESS
2019-07-29
CURRENT
AS4132C
Standard
TEE, BULKHEAD ON SIDE, STANDARD AND REDUCER, REDUCED BODY, FLARELESS
2019-07-29
CURRENT
AS4135D
Standard
TEE, BULKHEAD ON SIDE, STANDARD AND REDUCER, REDUCED BODY, FLARELESS
2019-01-07
HISTORICAL
AS4135C
Standard
TEE, BULKHEAD ON RUN, STANDARD AND REDUCER, REDUCED BODY, FLARELESS
2019-01-03
HISTORICAL
AS4134D
Standard
Coupling, Fuel, Rigid, Threaded Type
2018-07-12
CURRENT
AS1730E
This specification defines the requirements for a threaded rigid coupling assembly, which utilizes ferrule type machined tube end fittings, to join tubing and components in aircraft fuel, vent, and other systems. This coupling assembly is designed for use from −65 to 200 °F and at 125 psig operating pressure.
