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This SAE AIR covers Forced Air technology including: reference material, equipment, safety, operation, and methodology. It is intended to provide pressure and temperature (temps pages 26 & 31) information and minimum safety guidelines regarding use of equipment to remove frozen contaminants related to: i) Forced air ii) Forced air/fluid iii) Deicing fluid
G-12M Methods Committee
This information report covers all known aircraft with respect to deicing operations, especially with regard to OEM pressure and temperature limitations on the airframe. It provides data for airlines/operators on compliance with OEM limits and confirms that OEM limits are not exceeded during deicing operations.
G-12M Methods Committee
This AIR provides information about the specific requirements for missile hydraulic pumps and their associated power sources.
A-6C4 Power Sources Committee
This SAE Aerospace Information Report (AIR) has been written for individuals associated with ground level testing of turbofan and turbojet engines, and particularly for those who might be interested in investigating steady-state performance characteristics of a new test cell design or of proposed modifications to an existing test cell by means of numerical modeling and simulation. It is not the intent of this standard to provide specific test cell design recommendations, which are covered in the reference documentation.
EG-1E Gas Turbine Test Facilities and Equipment
This specification covers an aluminum alloy in the form of bars, rods, and wire, in the sizes shown in 3.3.3, in the “as-fabricated (F) temper.” When specified, product shall be supplied in the annealed (O) condition (see 8.6).
AMS D Nonferrous Alloys Committee
This specification covers a corrosion-resistant nickel-copper alloy in the form of wire 0.002 inch (0.05 mm) in diameter and larger.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers an iron-nickel-cobalt alloy in the form of bars and forgings.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers aluminum and aluminum alloy foil in the form of laminated sheet (see 8.6).
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of sheet and plate 0.008 to 1.000 inch (0.20 to 25.40 mm), inclusive, in thickness, clad on two sides, supplied in the annealed (O) condition. When specified, product shall be supplied in the “as fabricated” (F) temper (see 8.6).
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of die forgings up to 4 inches (102 mm), hand forgings up to 8 inches (203 mm), rolled or forged rings up to 2.5 inches (63.5 mm) in thickness, and forging stock (see 8.6).
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of rolled or cold-finished bars, rods, and wire and of flash-welded rings and stock for flash-welded rings.
AMS D Nonferrous Alloys Committee
This specification covers a series of iron-nickel, iron-nickel-cobalt, and iron-nickel-chromium alloys used for sealing to glasses and ceramics in electronic applications (see 6.1).
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a columbium (niobium) alloy in the form of foil, sheet, strip, or plate.
AMS G Titanium and Refractory Metals Committee
This specification covers a columbium alloy in the form of bars, rods, or wire.
AMS G Titanium and Refractory Metals Committee
This specification covers a corrosion-resistant nickel-copper alloy in the form of seamless tubing.
AMS F Corrosion and Heat Resistant Alloys Committee
Recommendations presented in this document are intended primarily for the acquisition of far-field noise data. The test engine is to be appropriately configured and operated so that the sound pressure levels obtained are consistent with the specific objectives of the test. The principal output of the data reduction system is one-third octave band sound pressure levels. However, when appropriate, data may be recorded for purposes of broader or narrower bandwidth analysis.
A-21 Aircraft Noise Measurement Aviation Emission Modeling
The purpose of this procedure is to establish a technique for reliably and repeatedly measuring the RF shielding characteristics of EMI gasket materials and EMI gaskets against various joint surfaces. The procedure is also used to test the reliability of the gasketed joint combinations after being subjected to hostile environments.
AE-4 Electromagnetic Compatibility (EMC) Committee
Systems shall be classified in terms of type, category and class.
A-6A2 Military Aircraft Committee
This ARP is intended to cover the warning, caution, and advisory indicating system required for commercial and military aerospace vehicles.
A-20A Crew Station Lighting
This specification covers a premium aircraft-quality alloy steel in the form of plate.
AMS E Carbon and Low Alloy Steels Committee
This specification covers an aluminum alloy in the form of sheet and plate 0.020 to 0.499 inch (0.50 to 12.50 mm), inclusive, in nominal thickness, clad on two sides (see 8.6).
AMS D Nonferrous Alloys Committee
This specification covers an arc-cast molybdenum alloy in the form of round bars 0.125 to 4.5 inches (3.00 to 112.50 mm), inclusive (see 8.6).
AMS G Titanium and Refractory Metals Committee
This SAE Aerospace Recommended Practice (ARP) delineates two complementary filter element performance parameters: (1) dirt capacity, and (2) filtration efficiency, and corresponding test procedures. It is intended for non-cleanable (disposable), fine fuel filter elements, rated at 25 µm(c) or finer, used in aviation gas turbine engine fuel systems.
AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
This specification covers the requirements for electrodeposited cadmium plating.
AMS B Finishes Processes and Fluids Committee
This specification covers a cast leaded-tin bronze in the form of sealing rings (see 8.5).
AMS D Nonferrous Alloys Committee
This specification covers the specific requirements for 7178 aluminum alloy alclad plate and sheet; the general requirements are covered in AMS-QQ-A-250. The plate and sheet covered by this specification shall be an integral composite product consisting of a heat-treatable aluminum alloy (7178) core with thin layers of an aluminum alloy (7072) anodic to the core and of approximately equal thickness bonded to both surfaces.
AMS D Nonferrous Alloys Committee
This specification covers a titanium alloy in the form of sheet, strip, and plate up through 4.000 inches (101.60 mm) inclusive in thickness (see 8.6).
AMS G Titanium and Refractory Metals Committee
This specification covers bearings of a leaded bronze cast on one or both faces of a steel backing.
AMS D Nonferrous Alloys Committee
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This specification covers one type of brass in the form of forgings and forging stock.
AMS D Nonferrous Alloys Committee
This specification covers flash welded rings made of aluminum and aluminum alloys.
AMS D Nonferrous Alloys Committee
This specification covers a gold-palladium-nickel alloy in the form of wire, rod, sheet, strip, foil, pig, powder, shot, chips, preforms, and a viscous mixture (paste) of the powder in a suitable binder.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion-resistant nickel-copper alloy in the form of bars, forgings, and forging stock.
AMS F Corrosion and Heat Resistant Alloys Committee
AMS CE Elastomers Committee
AMS CE Elastomers Committee
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