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2015-09-03
Standard
AMS3914A
This specification establishes the requirements for a nominal 250 °F cure epoxy preimpregnated carbon fiber plain weave fabric product. The prepreg is a plain weave fabric with 12K tows, a nominal fiber areal weight of 193 gsm, and nominal resin content of 42%.
2015-09-03
Standard
AS5506/1A
This document contains three annexes to the SAE AS5506B Standard - the SAE Architecture Analysis and Description Language. The first annex, the Error-Model Language extends the AADL core language with a state machine-based notation. This notation allows for specification of different types of faults, fault behavior of individual system components, fault propagation affecting related components in terms of peer to peer interactions and deployment relationship between software components and their execution platform, aggregation of fault behavior and propagation in terms of the component hierarchy. The notation also allows for specification fault mitigation strategies expected to be implemented in the health monitoring and fault management component of the actual system – also known as Fault Detection, Isolation, and Recovery (FDIR). The actual design of this component is expressed in the AADL core model.
2015-09-03
Standard
AMS2770N
This specification specifies the engineering requirements for heat treatment, by part fabricators (users) or their vendors or subcontractors, of parts (see 8.8.1). It also covers heat treatment by warehouses or distributors converting raw material from one temper to another temper (see 1.3 and 8.5). It covers the following aluminum alloys: 1100, 2004, 2014, 2017, 2024, 2098, 2117, 2124, 2219, 2224, 3003, 5052, 6013, 6061, 6063, 6066, 6951, 7049, 7050, 7075, 7149, 7178, 7249, 7475
2015-09-03
WIP Standard
AIR4922A
This SAE Aerospace Information Report (AIR) provides a description of the interfacesand their requirements for generic and specific hydraulic actuation systems used in the flight control systems of manned aircraft. Included are the basic control system characteristics and functional requirements, and the essential interfaces (structural, mechanical, hydraulic power, control input, status monitoring, and environment). Major design issues, requirements, and other considerations are presented and discussed. The primary purpose of this document is to describe the interfaces to aid in the development of Interface Control Documents (ICDs) for primary flight control servoactuation systems in future applications. Due to the variety of applications, the number of, and type of, ICDs required for a particular application is left up to the user of this document. The lessons learned from previously developed production aircraft are discussed.
2015-09-02
Standard
AMS6342K
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
2015-09-01
Standard
AMS4229G
This specification covers an aluminum alloy in the form of sand, permanent mold, and composite mold castings.
2015-09-01
Standard
AMS4242C
This specification covers an aluminum alloy in the form of castings.
2015-08-31
Standard
AMS4223E
This specification covers an aluminum alloy in the form of castings.
2015-08-31
Standard
AMS6517A
This specification covers a premium aircraft-quality alloy steel in the form of bars, forgings, and forging stock.
2015-08-30
WIP Standard
AS1701F
This document covers the performance requirements for solid dry film lubricants, air dried, or heat cured for use in aerospace applications. These lubricants are intended to prevent galling, and may be capable of remaining effective for extended periods of time after exposure to extreme environmental conditions.
2015-08-28
Standard
ARP4249A
This SAE Aerospace Recommended Practice (ARP) is intended to evaluate corrosion inhibiting properties of synthetic gas turbine lubricants and gearbox oils. This ARP is a modified form of a method developed in the United Kingdom as DERD Test Method/1, Method No. 18, Issue 1 of January 1984.
2015-08-28
Standard
ARP5873A
This document presents minimum criteria for the design and installation of LED passenger reading light assemblies in commercial aircraft. The use of “shall” in this specification expresses provisions that are binding. Non-mandatory provisions use the term “should.”
2015-08-28
Standard
AS5355/1A
SCOPE IS UNAVAILABLE.
2015-08-28
Standard
AS5355/2A
SCOPE IS UNAVAILABLE.
2015-08-28
Standard
ARP1532B
This SAE Aerospace Recommended Practice (ARP) covers procedures or methods to be used for fabricating, handling, testing, and installation of oxygen lines in an aircraft oxygen system.
2015-08-28
Standard
AIR6185
This SAE Aerospace Information Report (AIR) describes hydraulic system design and installation to minimize the effects of lightning, especially when the aircraft structure is composite. Techniques for effective electrical bonding, hydraulic system lightning protection, and lightning protection verification techniques are discussed.
2015-08-28
Standard
AS22073B
SCOPE IS UNAVAILABLE.
2015-08-28
Standard
AS5355/3A
SCOPE IS UNAVAILABLE.
Viewing 1 to 30 of 29724