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Viewing 241 to 270 of 35892
CURRENT
2017-11-30
Standard
AIR1213A
CURRENT
2017-11-30
Standard
AMS4268A
This specification covers an aluminum alloy in the form of sheet and plate 0.010 to 1.500 inch (0.254 to 38.07 mm), inclusive, in thickness, supplied in the −T81/−T851 temper (see 8.5).
2017-11-30
WIP Standard
AMS03_18A
This SAE Standard specifies the properties of chromate conversion coatings on aluminum and aluminum alloys. It details inspection and testing requirements for chromate conversion coatings. Where there are differences in the requirements for the Brushing Grade from the Standard Grade they are highlighted in this Standard.
2017-11-30
WIP Standard
AMS03_14A
This SAE Standard gives guidance for - and specifies the requirements for - the electrodeposition of chromium for engineering purposes. It relates to both new articles and also the reclamation of worn or over-machined components. Chromium electrodeposition undertaken for decorative purposes is not considered herein.
CURRENT
2017-11-30
Standard
ARP497B
This recommendation establishes objectives for high performance control motors to be used with aeronautical and associated equipment in protective enclosures or completely within the shell of the aircraft so that they are subjected only to the internal climatic conditions of heat, cold, shock, vibration, altitude, and humidity. Control motors larger than size #23 are not covered in this document.
CURRENT
2017-11-30
Standard
ARP4729A
This SAE Aerospace Recommended Practice (ARP) provides technical design and application information related to the generation, distribution, control, and utilization of aircraft 270 V DC electrical power systems and support equipment. This document also provides references and definitions to permit comparisons of various electrical systems and components.
CURRENT
2017-11-30
Standard
ARP6539
This SAE Aerospace Recommended Practice (ARP) provides a process for the verification and validation of monitors used in highly-integrated and complex aircraft flight control and related systems.
CURRENT
2017-11-30
Standard
ARP826A
This document covers resolvers which are used to perform coordinate transformations as well as sine and cosine computations, It includes both the categories of compensated and uncompensated resolvers which perform these functions. Linear resolvers are also included because of their similarity to resolvers.
CURRENT
2017-11-30
Standard
AS81099A
This specification gives general requirements for electric devices for which the detail requirements are given by standards only, as the detail requirements for the devices are not complex enough to warrant issuance of detail specifications for them.
2017-11-30
WIP Standard
AMS03_17A
This SAE Standard specifies the requirements for the electro-deposition of gold on ferrous-base materials, copper-base materials, aluminum-base materials, zinc-base materials and nickel-base materials for MOD use. It is primarily intended for use on electrical and electronic items which are to be plated with gold to: a. Increase the electrical conductivity of the surface. b. Provide a solderable surface. This Standard does not cover the gold plating of threaded items.
2017-11-30
WIP Standard
ARP5316E

This SAE Aerospace Recommended Practice (ARP) addresses the general requirements for data recording procedures, packaging, and storing of elastomeric seals and seal assemblies which include an elastomeric element prior to the seal being assembled into hardware components. It applies specifically to those elastomeric seals and seal assemblies packaged shortly after manufacture. The storage period prior to installation of the elastomeric seals and seal assemblies into hardware components is commonly referred to as shelf life.

The information contained in this ARP is intended to be utilized by those organizations who do not have specific requirements or recommendations already in place for the control of elastomeric seals and seal assemblies. This ARP can be specified in control, storage, and procurement documents.

CURRENT
2017-11-30
Standard
AMSS6758B
This specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality.
CURRENT
2017-11-30
Standard
AMS6457E
This specification covers a low-alloy steel in the form of welding wire.
CURRENT
2017-11-29
Standard
AIR5301A
This SAE Aerospace Information Report (AIR) was written because of the growing interest in aircraft installed outdoor engine testing by the Federal Aviation Administration, airlines, charter/commercial operators, cargo carriers, engine manufacturers and overhaul and repair stations. This document was developed by a broad cross section of personnel from the aviation industry and government agencies and includes information obtained from a survey of a variety of operators of fixed and rotary wing aircraft and research of aircraft and engine maintenance manuals.
CURRENT
2017-11-29
Standard
AIR6364
The paper discusses in general terms the activities required to be undertaken or demonstrated during the establishment of the facility such as: the assessment checks prior to forwarding to the end users site for embodiment into the facility system the establishment of the facility such as trial installations of hardware, functionality checking of lifting transportation and access systems, centerline pull checks, pressure testing of fuel and air start systems, flushing of wet systems and electrical continuity checking. the commissioning of the facility such as instrumentation calibrations, engine starts, engine running, assessment of command and control system, assessment of DAS system, aerodynamic and acoustic surveys. The paper will concentrate on the main engineering engine related aspects of the facility and will not necessarily contain information on the construction validation activities such as HVAC, electrical, facility fire system, waste water etc.
CURRENT
2017-11-29
Standard
AMS2545
This specification covers the requirements for saturation peening, straightening and forming metal parts using controlled pneumatic activated needles.
2017-11-29
WIP Standard
AIR6504A
This SAE Aerospace Information Report (AIR) provides a method for assessing particle losses that occur in a sampling system of specified geometry based on the nvPM mass and number measured at the end of the sampling system. Both size dependent diffusion loss and size independent thermophoretic loss mechanisms are included in the method. The penetration function of that system must be determined by measurement and/or by computation using an analytical method as described within this report. The outcome of this line loss assessment provides estimated correction factors for nvPM mass and number concentration with associated uncertainties based upon nvPM measurement uncertainties and method assumptions. These correction factors give an estimation of nvPM mass and number values at the inlet to the sampling system.
CURRENT
2017-11-29
Standard
ARIR605
This guide has been written as an applications manual for writing avionics test specifications that conform to ARINC Specification 616. It provides advice for converting ATLAS test specifications into ATLAS test programs and implementing them on Automatic Test Equipment (ATE).This guide has been written as an applications manual for writing avionics test specifications that conform to ARINC Specification 616. It provides advice for converting ATLAS test specifications into ATLAS test programs and implementing them on Automatic Test Equipment (ATE).
CURRENT
2017-11-29
Standard
ARIS619-5
The purpose of this document is to delineate, in an organized fashion, the protocols used by Aircraft Communication Addressing and Reporting System (ACARS) Management Units (MU) defined in ARINC Characteristic 724B and Communications Management Unit (CMU) defined in ARINC Characteristic 758, in their interactions with other onboard avionics equipment. The purpose of this document is to delineate, in an organized fashion, the protocols used by Aircraft Communication Addressing and Reporting System (ACARS) Management Units (MU) defined in ARINC Characteristic 724B and Communications Management Unit (CMU) defined in ARINC Characteristic 758, in their interactions with other onboard avionics equipment.
CURRENT
2017-11-29
Standard
AMS3731/10C
This specification covers an unfilled, room-temperature-polymerizing epoxy resin formulation with a polyamide hardener, supplied as a two-component system.
CURRENT
2017-11-29
Standard
AS5443B
CURRENT
2017-11-28
Standard
AMS3056C
This specification covers the requirements for a refined paraffinic petroleum-base lubricant.
2017-11-27
WIP Standard
AMS6952
This specification covers a titnaium alloy in the form of forgings 4.4 inches (111.76 mm) and under in nominal diameter or least distance between parallel sides and forging stock of any size.
CURRENT
2017-11-21
Standard
AMS2451/3C
This specification covers the requirements for brush plating of low-hardness, low-stress nickel by electrodeposition.
CURRENT
2017-11-21
Standard
ARP1210E
This SAE Aerospace Recommended Practice (ARP) describes a class of digital computer programs for use by organizations other than the engine supplier for reduction of engine test data relating to the interface of the engine in the airframe or test facility. This ARP also is intended as a guide for the preparation of such computer programs.
Viewing 241 to 270 of 35892