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This AIR provides information about the specific requirements for missile hydraulic pumps and their associated power sources.
A-6C4 Power Sources Committee
This document covers external lighting for Electric Vertical Takeoff and Landing (E-VTOL) and Urban Air Mobility (UAM) vehicles. It discusses lights that may be installed both to meet regulatory requirements as well as for customer comfort and aircraft recognition. It also discusses the differences between UAM vehicles and other aircraft and how those differences impact the lighting.
A-20B Exterior Lighting Committee
This specification covers an aluminum alloy in the form of rolled or forged rings up to 6 inches (152 mm), inclusive, in thickness (see 3.3.1.1.1) and an OD to wall thickness ratio of 10 or greater (see 8.5).
AMS D Nonferrous Alloys Committee
This specification covers a magnesium alloy in the form of investment castings (see 8.6).
AMS D Nonferrous Alloys Committee
This specification covers a nitriding grade of premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. AMS6496 and AMS6497 cover UNS K23280 with other quality levels.
AMS E Carbon and Low Alloy Steels Committee
This SAE Standard describes snowmobile and snowmobile cutter requirements for the installation of lamps, reflective devices, and associated equipment.
Snowmobile Technical Committee
This SAE Recommended Practice provides definitions of common terms used in SAE Documents pertaining to motor vehicle lighting. It covers not only basic lighting terms but also terms which identify major segments of technical reports.
Lighting Standard Practices Committee
This SAE Standard establishes the test procedure, environment, and instrumentation for determining the exhaust sound pressure levels of motorcycles under stationary conditions. Since initial publication, it has been successfully applied to regulation and monitoring of sound pressure levels of off-highway vehicles, and that remains its recommended application. Users of SAE J1287 for the purpose of roadside enforcement of sound pressure levels for on-highway motorcycles have reported difficulties with its implementation in that application. In response, SAE J2825 was developed, and is recommended for measurement of exhaust sound pressure levels of stationary on-highway motorcycles. Care must be taken not to confuse stationary sound pressure levels with total motorcycle sound pressure levels. This test does not evaluate total motorcycle sound during operation. For this purpose, SAE J331 or SAE J47 is recommended. Any allowable sound limits (dBA) set in relation to SAE J1287 for exhaust
Motorcycle Technical Steering Committee
This SAE Recommended Practice has been adopted by SAE to specify: a A basis for net engine retarder power rating b Reference inlet air test conditions c A method for correcting observed engine retarder power to reference conditions d A method for determining net engine retarder power with a dynamometer
Truck and Bus Powertrain Committee
This document describes the 2-D computer-aided design (CAD) template for the HPM-1 H-point machine or HPD available from SAE. The elements of the HPD include the curve shapes, datum points and lines, and calibration references. The intended purpose for this information is to provide a master CAD reference for design and benchmarking. The content and format of the data files that are available are also described.
Human Accom and Design Devices Stds Comm
This SAE Standard provides general design performance requirements and related test procedures for composite lighting unit assemblies, other than signaling and marking devices, used on earthmoving and road building and maintenance off-road work machines as defined in SAE J1116.
OPTC3, Lighting and Sound Committee
AE-8C2 Terminating Devices and Tooling Committee
This specification establishes process controls for the repeatable production of preforms by Wire Fed Plasma Arc Directed Energy Deposition (PA-DED). It is intended to be used for aerospace parts manufactured using Additive Manufacturing (AM) metal alloys, but usage is not limited to such applications.
AMS AM Additive Manufacturing Metals
AE-8C2 Terminating Devices and Tooling 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
AE-8C2 Terminating Devices and Tooling Committee
This specification covers an alloy steel in the form of investment castings.
AMS E Carbon and Low Alloy Steels Committee
This specification covers a corrosion-resistant steel product 12 inches (305 mm) and under in nominal diameter, thickness or for hexagons, least distance between parallel sides, and having a maximum cross-sectional area of 144 square inches (930 cm2) in the solution and precipitation heat treated (H1075) condition.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a copper-beryllium alloy in the form of bars and rods (see 8.5).
AMS D Nonferrous Alloys Committee
This specification covers a copper-nickel-tin alloy in the form of bars and rods up to 8.500 inches (216 mm), inclusive, in nominal thickness. When tube is ordered to AMS4596, it shall be supplied to AMS4598 (see 8.8).
AMS D Nonferrous Alloys Committee
This specification covers a tin bronze in the form of sand and centrifugal castings (see 8.5).
AMS D Nonferrous Alloys Committee
This specification covers a copper-nickel-tin alloy in the form of plate over 0.188 to 4.50 inches (4.77 to 114.3 mm) in nominal thickness (see 8.8).
AMS D Nonferrous Alloys Committee
This specification establishes requirements for an interior decorative clear coating for wear protection of metal substrates.
AMS G8 Aerospace Organic Coatings Committee
This specification covers the specific requirements for aluminum alloy 7075 plate and sheet for applications requiring improved exfoliation resistance.
AMS D Nonferrous Alloys Committee
This specification covers a corrosion- and heat-resistant nickel-iron alloy in the form of bars and forgings 5 inches (127 mm) and under in nominal diameter or least distance between parallel sides and forging stock of any size.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a silicone (PVMQ) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
AMS CE Elastomers Committee
This specification covers a titanium alloy in the form of wire, forgings, flash-welded rings 4.000 inches (101.60 mm), inclusive, and under in nominal diameter or distance between parallel sides, bars up through 10.000 inches (254 mm), inclusive, and under in nominal diameter with a maximum cross-sectional area for bars over 4.000 to 10.000 inches (101.60 to 254 mm) in diameter of 79 square inches (509.7 cm2), and stock for forging or flash-welded rings of any size (see 8.6).
AMS G Titanium and Refractory Metals Committee
This Purchasing Specification, AMS6885/4, specifies the batch release and delivery requirements for film adhesive used for repair. This specification is applicable only when the film adhesive is used as part of the repair system defined in AMS6885 and AMS6885/1. This specification also defines the procedure and requirements for storage life extension of materials purchased against this specification. It is only applicable for materials qualified against AMS6885 (refer to PRI-QPL-AMS6885), and shall be carried out within the responsibility of the purchaser and under control of its Quality organisation.
AMS CACRC Commercial Aircraft Composite Repair Committee
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