Results
This SAE lab test procedure should be used when performing the following specialized weathering tests for wheels; Florida Exposure, QUV, Xenon and Carbon Weatherometer. In addition to these procedures, some additional post-weathering tests may be specified. Please refer to customer specifications for these requirements.
This SAE Recommended Practice is intended as a guide toward standard practice and is subject to change to keep pace with experience and technical advances. This document establishes additional performance requirements and provides test methods and requirements to evaluate the suitability of materials intended for optical applications in motor vehicles. The tests are intended to determine physical and optical characteristics of the materials only. Performance expectations of finished assemblies, including plastic components, are to be based on tests for lighting devices, as specified in SAE Standards and Recommended Practices for motor vehicle lighting equipment. Glass and materials inclusive to the light source are not in scope for this method.
This specification covers a corrosion- and heat-resistant steel in the form of welding wire.
This specification covers quality assurance sampling and testing procedures used to determine conformance to applicable specification requirements of carbon and low-alloy steel forgings.
The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide recommendations which will lead to the standardization of interior door design and operation in all transport aircraft. Interior doors are broadly classified into two main categories which include egress path doors and non-egress path doors. The scope of this ARP does not include crew rest doors, secondary barriers to the flight deck, or doors incorporated in furniture surrounding passenger seats as defined in AS6960.
These general guidelines and precautions apply to personnel operating directional drilling tracking equipment when used with horizontal directional drilling (HDD) machines as defined in ISO 21467:2023.
This specification covers an aluminum alloy in the form of Alclad sheet and plate 0.040 to 1.000 inch, inclusive (1.02 to 25.40 mm, inclusive) in nominal thickness (see 8.5).
This specification covers a heat-treatable, corrosion-resistant steel in the form of bars, wire, forgings, mechanical tubing, and stock for forging or heading.
This SAE Aerospace Recommended Practice (ARP) is written for individuals associated with the ground-level testing of large and small gas turbine engines and particularly for those who might be interested in constructing new or adding to existing engine test cell facilities.
This SAE Aerospace Standard (AS) establishes the requirements for AS3504 and AS3505 thin wall self-locking inserts made from a corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07718.
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing.
This specification covers a titanium alloy in the form of forgings 4.400 inches (111.76 mm) and under in nominal diameter or least distance between parallel sides and a maximum cross-sectional area of 63.8 square inches (411.6 cm2) and under and forging stock of any size (see 8.7).
This specification covers a chloroprene (CR) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
This specification covers quality assurance sampling and testing procedures used to determine conformance to applicable material specification requirements of wrought corrosion- and heat-resistant steel and alloy products and of forging stock.
This specification covers an aluminum alloy in the form of sand, permanent mold, and composite mold castings with nominal wall thickness up to 1.0 inch (25 mm) or nominal weight up to 50 pounds (23 kg) (see 8.2 and 8.8).
This specification covers an aluminum alloy in the form of castings (see 8.6).
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).
This specification covers a premium aircraft-quality steel in the form of bars, forgings, mechanical tubing, flash welded rings up through 6.000 inches (152.40 mm), and stock for forging or flash welded rings.
This specification covers one type of aluminum silicon bronze in the form of rods and bars up to 3.00 inches (76.2 mm), inclusive, in nominal diameter or distance between parallel sides, and forgings and forging stock of any size (see 8.5).
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm), inclusive, in nominal diameter or least distance between parallel sides and 32 square inches (206.46 cm2) maximum cross-sectional area and stock for forging of any size (see 8.7).
This specification covers a corrosion- and heat-resistant steel in the form of wire 0.010 inch (0.25 mm), up to and including 0.25 inch (6.35 mm).
This specification covers the requirements for gold deposited on metal surfaces and the properties of the deposit.
This specification covers requirements and recommendations for the heat treatment of wrought aluminum alloy raw materials (see 2.2.1) by producers. It supersedes AMS-H-6088 and replaces MIL-H-6088.
This specification covers a premium aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock.
This specification covers a silver alloy in the form of wire, rod, sheet, strip, foil, pig, powder, shot, and chips, and a viscous mixture (paste) of powder in a suitable binder.
This specification covers an aluminum alloy in the form of sheet and plate 0.008 to 1.000 inch (0.203 to 25.4 mm) thick, supplied in the annealed (O) temper (see 8.5). When specified, product shall be supplied in the “as fabricated” (F) temper (see 8.5).
This specification covers three types of a free-machining, corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.
This specification covers a shampoo type carpet cleaner in the form of a liquid.
This specification covers an aluminum alloy in the form of drawn, round, seamless tubing with wall thickness of 0.018 to 0.500 inch (0.46 to 12.70 mm), inclusive (see 8.6).
This specification covers a corrosion- and heat-resistant nickel alloy in the form of welding wire.
This specification covers non-silicone synthetic rubber sealing compounds supplied as a two-component system that cures at room temperature.
This specification covers an aluminum alloy in the form of seamless drawn round tubing, having a wall thickness of 0.045 to 0.125 inches (1.14 to 3.18 mm) (see 8.6).
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