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Viewing 1 to 30 of 7153
CURRENT
2017-05-25
Standard
AIR805D
The purpose of this information report is to present the factors that affect the design and development of aircraft jet blast windshield rain removal systems. Rain removal system design will generally be unique to specific aircraft. Design of these systems typically requires a preliminary design for the system based on available empirical data to be followed with a laboratory development program and a flight test validation program. Published windshield rain removal performance test data is available only for limited windshield configurations.
CURRENT
2017-05-25
Standard
AS20708/131B
Scope is unavailable.
CURRENT
2017-05-25
Standard
AS39029/90B
No scope available.
CURRENT
2017-05-25
Standard
AS21926C
SCOPE IS UNAVAILABLE.
CURRENT
2017-05-25
Standard
AS1043G
SCOPE IS UNAVAILABLE.
2017-05-24
WIP Standard
J2087
This SAE Standard provides test procedures, requirements, and guidelines for a daytime running light (DRL) function.
2017-05-23
WIP Standard
AS85598
This document defines the requirements for spherical, radial-journal, conical and thrust bearings which are of laminated elastomeric construction. These bearings are for use in an environment having a temperature spectrum within a maximum ambient temperature range of -65 degrees F to +160 degrees F while reacting oscillating loads and motions.
2017-05-23
WIP Standard
AS4764A
This document establishes techniques for validating that an aircraft station complies with the interface requirements delineated in MIL-STD-1760.
2017-05-23
WIP Standard
AS4270A
This document establishes techniques for validating that a mission store comples with the interface requirements delineated in MIL-STD-1760.
2017-05-22
WIP Standard
AIR6540
The scope of this report is to capture the fundamental principles of selecting a wire size for an aerospace application using the method prescribed in SAE AS50881 standard. Also, provided in this report are additional calculations to ensure the wire selection will adequately perform in a particular design function including meeting environment constraints. Some of the calculations in this report have been simplified to demonstrate the process for validating the wire size selections for a particular design application. More precise calculations should be investigated and evaluated to ensure proper assessment of each individual calculation in this report.
CURRENT
2017-05-22
Standard
AS39029/91B
SCOPE IS UNAVAILABLE.
CURRENT
2017-05-19
Standard
AMS2355M
This specification covers quality assurance sampling and testing procedures used to determine conformance to applicable specification requirements of wrought aluminum alloy and wrought magnesium alloy mill products (except forging stock), and includes quality assurance and testing procedures for rolled, forged, and flash welded rings (see 8.3). Requirements are specified in inch/pound units.
2017-05-18
WIP Standard
AS81714/29A
No scope available.
2017-05-18
WIP Standard
AS85848/1A
SCOPE IS UNAVAILABLE.
2017-05-18
WIP Standard
J1979
SAE J1979/ISO 15031-5 set includes the communication between the vehicle's OBD systems and test equipment implemented across vehicles within the scope of the legislated emissions-related OBD.
2017-05-18
WIP Standard
AS85720B
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.
CURRENT
2017-05-18
Standard
AIR6130A
14-day material test to determine the cyclic effects of runway deicing compounds on cadmium plated parts.
CURRENT
2017-05-18
Standard
ARP6157
The lubricant performance capability for aero propulsion drive systems is derived from the physical properties of the oil and performance attributes associated with the chemical properties of the oil. Physical properties, such as viscosity, pressure-viscosity coefficient and full-film traction coefficient are inherent properties of the lubricating fluid. Chemical attributes are critical for the formation of protective boundary lubricating films on the surfaces to prevent wear and scuffing. These attributes are also associated with surface initiated fatigue (micropitting). To assure performance and to provide required information for engineering design, methodology for at least five oil properties are being studied: (1) pressure-viscosity coefficient, (2) full-film traction coefficient, (3) scuffing resistance, (4) wear resistance; and (5) micropitting propensity.
CURRENT
2017-05-18
Standard
AS20708/81B
No Scope Available
CURRENT
2017-05-18
Standard
AS20708/94C
This specification covers the detail requirements for 115 volt, 60 and 400 Hz, size 23 synchros (see 6.1).
Viewing 1 to 30 of 7153