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This recommended practice establishes a procedure for the application of long string abrasive monofilaments to machined aircraft structures for the purpose of removing burrs produced during the machining operations. This procedure is typically applicable to aluminum, titanium, and steel, but usage is not limited to such applications
AMS B Finishes Processes and Fluids Committee
SCOPE IS UNAVAILABLE
E-25 General Standards for Aerospace and Propulsion Systems
To define optimum standards of design, construction and performance for Diluter Demand, Automatic Pressure Breathing, Oxygen Regulators. AS 861, 'Minimum General Standards for Oxygen Systems,' is applicable as supplemented by this specification. This document supersedes in part AS 463, 12-15-56, which is cancelled. This specification covers two types of Diluter Demand, Automatic Pressure Breathing, Oxygen Regulators for use in civil type aircraft. The intent is that the regulators be of two configurations, operable at inlet pressures of 40 to 90 psig and 50 to 150 psig
A-10 Aircraft Oxygen Equipment Committee
This Aerospace Recommended Practice (ARP) provides criteria for operational characteristics to be considered in the design of individual, inflatable life preservers intended for air transport safety
S-9A Safety Equipment and Survival Systems Committee
E-25 General Standards for Aerospace and Propulsion Systems
This specification establishes the requirements for the following types of self-locking nuts: a Wrenching nuts: that is, hex, double hex, spline drive b Anchor nuts: that is, plate nuts, gang channel nuts, shank nuts The wrenching nuts and shank nuts are made of low alloy steels, and the nut elements of plate and gang channel nuts are made of carbon steels or low alloy steels and having MJ threads to ISO 5855/2. Nuts have 1100 MPa tensile strength class at room temperature. Maximum test temperature of parts at 235 °C
E-25 General Standards for Aerospace and Propulsion Systems
This SAE Aerospace Recommended Practice (ARP) describes the multi-pass method for evaluating the filtration performance of fine lube filter elements, commonly utilized in aerospace power and propulsion lubrication systems: gas turbine engines, auxiliary power units (APUs), helicopter transmissions, constant speed drives (CSDs), and integrated drive generators (IDGs
AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
AS81714 covers Terminal Junction System (TJS) components which are used for interconnection of wiring and incorporation of passive components (see 6.1). These environment resistant components have in common the use of crimp type external pin contacts in accordance with AS39029/1 for Series I or crimp type external socket contacts in accordance with AS39029/22 for Series II. This family of TJS components is designed to operate continuously over a temperature range of -65 to 200 °C, using any combination of temperatures generated by the electrical load and ambient temperature so that the maximum internal hot spot, combined temperature, will not exceed the maximum specified for the class of TJS component, unless otherwise specified (1.2, 3.1). The maximum continuous temperature established by the electronic components in a component module (block) shall be limited to the block maximum continuous temperature. The components making up the system and covered by AS81714 include: a Terminal
AE-8C2 Terminating Devices and Tooling Committee
This SAE Aerospace Information Report (AIR) has been prepared by a panel of the SAE A-5A Committee and is presented to document unique design approaches used for aircraft wheels and brakes
A-5A Wheels, Brakes and Skid Controls Committee
This document establishes age limit and guidance for acceptance of hose and hose assemblies containing elastomeric materials for use in aircraft, space vehicles, missiles and component assemblies thereof at time of delivery to the contractor, procuring activity, or contracting officer. This document does not establish limitations on storage times for military/civil activities nor operating life
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This slash document collects general reference material related to gaseous oxygen system flow requirements and sizing calculations. This document will assist oxygen system equipment designers and operators to establish systems and equipment requirements. The document consists of charts, tables, system schematics, system requirements, and sample calculations for system sizing
A-10 Aircraft Oxygen Equipment Committee
This SAE Aerospace Information Report (AIR) provides an orientation regarding the general technology of chemical oxygen generators to aircraft engineers for assistance in determining whether chemical oxygen generators are an appropriate oxygen supply source for hypoxia protection in a given application and as an aid in specifying such generators. Information regarding the details of design and manufacture of chemical oxygen generators is generally beyond the scope of this document
A-10 Aircraft Oxygen Equipment Committee
Engine charging of aircraft has been observed for many years. This SAE Aerospace Information Report (AIR) reviews the history of observations, physical characteristics, and possible techniques for minimizing the effects
AE-4 Electromagnetic Compatibility (EMC) Committee
This document contains general criteria for the planning, design, and construction of military and commercial ground based aviation fueling facilities that receive, store, distribute, and dispense liquid aviation turbine fuels at airports to both fixed and rotary wing aircraft
AE-5C Aviation Ground Fueling Systems Committee
This specification covers environment resistant, heat-shrinkable solder type shield terminations. They may be used on data-bus, RF, and shielded cables in applications. Operating temperature of each product are as indicated on detail specifications
AE-8C2 Terminating Devices and Tooling Committee
This SAE Aerospace Standard (AS) establishes minimum design and performance requirements for galley insert equipment with an electrical and/or pressure system, as well as associated components intended for installation in galleys and other areas (e.g., bars) of transport category airplanes
S-9B Cabin Interiors and Furnishings Committee
This document describes the initial development, evolution, and use of reticulated polyurethane foam as an explosion suppression material in fuel tanks and dry bays. It provides historical data, design practice guidelines, references, laboratory test data, and service data gained from past experience. The products discussed in this document may be referred to as "Safety Foam," "Reticulated Polyurethane Foam," "Baffle and Inerting Material," or "Electrostatic Suppression Material." These generic terms for the products discussed in this document are not meant to imply any safety warranty. Each individual design application should be thoroughly proof tested prior to production installation
AE-5D Fuel Tank Flammability Reduction Systems Committee
This specification covers an aluminum alloy in the form of sheet, procured to inch/pound dimensions and properties. Primarily for parts requiring a high degree of formability (superplasticity) and response to heat treatment
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of hand forgings and rolled rings procured to metric (SI) dimensions. These products have been used typically for complex shaped parts requiring moderate strength and good forgeability of the alloy and where stability is required during machining, but usage is not limited to such applications. Corrosion resistance of this alloy is superior to that of aluminum alloys having copper as the principal alloying element
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of sheet procured in metric units. Primarily for parts requiring a high degree of formability (superplasticity) and response to heat treatment
AMS D Nonferrous Alloys Committee
This specification provides requirements and procedures for air-pressure leak testing of parts
AMS B Finishes Processes and Fluids Committee
This specification covers established metric manufacturing tolerances applicable to seamless and welded thin-walls aircraft tubing of nickel, nickel alloys, and cobalt alloys ordered to metric dimensions. These tolerances apply to all conditions and are based on individual measurements, unless otherwise noted. The term 'excl' is used to apply only to the higher figure of a specified range
AMS F Corrosion and Heat Resistant Alloys Committee
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This SAE Aerospace Information Report (AIR) provides information on air quality and some of the factors affecting the perception of cabin air quality in commercial aircraft cabin air. Also a typical safety analysis process utilizing a Functional Hazard Assessment approach is discussed
AC-9 Aircraft Environmental Systems Committee
This document recommends general gland design criteria for static and dynamic O-ring seal applications specifically for engines and engine control systems
A-6C2 Seals Committee
This standard covers the requirements for non-separable, airframe anti-friction needle bearings, corrosion resistant and traditional materials, intended for use in flight vehicle control systems, with radial loads
ACBG Rolling Element Bearing Committee
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