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CURRENT
2017-05-08
Standard
AS5385D
This SAE Aerospace Standard (AS) aims at identifying the design criteria and testing methods adequate to guarantee the ultimate load and operational dependability of cargo restraint strap assemblies with a typical 22250 N (5000 lbf) rated ultimate tension load capability, as used by the airline industry in order to restrain cargo on board civil transport aircraft during flight: cargo loaded and tied down onto airworthiness certified air cargo pallets, themselves restrained into aircraft lower deck or main/upper deck cargo systems and meeting the requirements of NAS 3610 or AS36100, or non-unitized individual pieces of cargo, or pieces of, cargo placed onto an unrestrained (“floating”) pallet into either lower deck or main deck containerized cargo compartments of an aircraft.
CURRENT
2017-05-04
Standard
ARP1328C
This SAE Aerospace Recommended Practice (ARP) is intended to recommend: uniform criteria for determination of wind loads that aircraft ground support equipment can encounter and yet allow personnel to work safely, uniform systems for maintaining stability (i.e., stabilizers, outriggers, spring lockout devices), standardization of specific types of interlock systems and actuation systems, a standard formula with its associated design criteria for calculating the steady-state wind stability (i.e., tip point) for aircraft ground support equipment, a standard method for testing these systems.
CURRENT
2017-05-04
Standard
ARP378D
This document presents criteria for design and location of passenger reading lights in commercial aircraft. For LED reading light requirements, see ARP5873, titled: LED Passenger Reading Light Assembly.
CURRENT
2017-05-04
Standard
AS5166B
CURRENT
2017-05-04
Standard
AS21922C
CURRENT
2017-05-02
Standard
AS5356B
This specification covers flexible couplings for joining tubing with AS5131 Type A beaded ends for use in aircraft fuel and vent systems (see 6.1).
HISTORICAL
2017-05-02
Standard
AS5188B
CURRENT
2017-05-01
Standard
AS35051A
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.
HISTORICAL
2017-04-27
Standard
AS1895/7E
CURRENT
2017-04-26
Standard
AS7460C
This procurement specification covers aircraft-quality bolts and screws made of 6.0Al - 4.0V titanium alloy and of 160 ksi tensile strength at room temperature.
CURRENT
2017-04-26
Standard
AS9146
This standard defines FOD Prevention Program requirements for organizations that design, develop, and provide aviation, space, and defense products and services; and by organizations providing post-delivery support, including the provision of maintenance, spare parts, or materials for their own products and services. It is emphasized that the requirements specified in this standard are complementary (not alternative) to customer, and applicable statutory and regulatory requirements. Should there be a conflict between the requirements of this standard and applicable statutory or regulatory requirements, the latter shall take precedence.
CURRENT
2017-04-21
Standard
AIR6162
This document provides an orientation to fusion splicing technology for optical fibers and fiber optic cable. It is intended for managers, designers, installers, and repair and maintenance personnel who need to understand the process of fusion splicing. This technology is widely used in telecommunications and industrial applications, and is finding acceptance in aerospace applications.
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
2017-04-20
Standard
AS20708/78B
CURRENT
2017-04-20
Standard
AS20708/76B
CURRENT
2017-04-20
Standard
AS20708/68B
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