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Viewing 181 to 210 of 8781
CURRENT
2017-04-27
Standard
ARP1420C
The turbine-engine inlet flow distortion methodology addressed in this document applies only to the effects of inlet total-pressure distortion. Practices employed to quantify these effects continue to develop and, therefore, periodic updates are anticipated. The effects of other forms of distortion on flow stability and performance, and of any distortion on aeroelastic stability are not addressed. The guidelines can be used as necessary to create a development method to minimize the risk of inlet/engine compatibility problems. The degree to which guidelines for descriptor use, assessment techniques, and testing outlined in this document are applied to a specific program should be consistent with the expected severity of the compatibility problem.
2017-04-21
WIP Standard
AS153J
Add integral silicone cuff max length and OD to flared parts standards
2017-04-21
WIP Standard
AS155H
Add integral silicone cuff max length and OD to flared parts standards
2017-04-21
WIP Standard
AS154H
Add integral silicone cuff max length and OD to flared parts standards
CURRENT
2017-04-20
Standard
AS976A
NO SCOPE AVAILABLE.
CURRENT
2017-04-20
Standard
AS614D
This SAE Aerospace Standard (AS) defines the requirements for a heavy-duty polytetrafluoroethylene (PTFE) lined, metallic reinforced, hose assembly suitable for use in high temperature, high pressure, 4000 psi, aircraft and missile hydraulic fluid systems.
CURRENT
2017-04-19
Standard
AS20708/79B
No Scope Available
CURRENT
2017-04-19
Standard
AS24334C
SCOPE IS UNAVAILABLE.
CURRENT
2017-04-18
Standard
AS20708/74B
No Scope Available
CURRENT
2017-04-18
Standard
AS20708/67B
No Scope Available
CURRENT
2017-04-18
Standard
MA2112C
NO SCOPE AVAILABLE.
CURRENT
2017-04-18
Standard
MA620SUP1A
This supplement forms a part of Aerosapce Standard MA620, Hose Assemblies, Convoluted Polytetrafluorethylene Metallic Reinforced, High Temperature, Medium Pressure, Aircraft, Metric and shall be used to identify hose assembly standards citing this procurement specification.
CURRENT
2017-04-18
Standard
J1696_201704
This SAE Standard defines the requirements for fluid to be used in the SAE Fuel Filter Test Procedures.
CURRENT
2017-04-14
Standard
J1298_201704
SAE J1298 covers the recommended diagnostic port sizes for use in measuring hydraulic fluid temperature, pressure, flow, and for obtaining fluid samples. See SAE J1502 for the detailed coupling specifications.
2017-04-13
WIP Standard
AIR5875A
This SAE Aerospace Information Report (AIR) outlines comprehensive aircraft flight control system fault isolation methodology that has proven to be effective. The methodology presented in this Information Report has been used in several successful fault isolation efforts on military aircraft.
CURRENT
2017-04-13
Standard
J518/2_201704
This SAE Standard covers general and dimensional specifications for the Code 62 metric (type 1) and inch (type 2) flanged heads, flange clamps (FC and FCM), and split flange clamps (FCS and FCSM) applicable to four-screw flange type tube, pipe, and hose connections. Also included are the recommended port dimensions and port design considerations. Type 2 (inch) flange clamps and split flanges are not for new design.
2017-04-13
WIP Standard
AS4088E
This SAE Aerospace Standard (AS) defines gland details for rod diameters from 1/4 to 15-1/2 in. inclusive corresponding to AS568 O-Ring Dash No. sizes -108/-111, -206/-222, -325/-349 and -425/-460. The gland details herein provide more space than MS33675 and sufficient to fit more efficient and reliable excludion devices. Exclusion device configurations are not specified in this document.
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