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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 specification covers a copper alloy in the form of strip (see 8.6).
AMS D Nonferrous Alloys Committee
This specification establishes the engineering requirements for the uphill quenching process of aluminum alloy product. Uphill quenching immerses product in liquid nitrogen followed by exposure to a high-pressure/high-velocity steam blast or boiling water.
AMS D Nonferrous Alloys Committee
This document and the EUROCAE equivalent, ED-107, provides detailed information, guidance, and methods in support of the Federal Aviation Administration (FAA) Advisory Circular (AC) 20-158 and to the European Union Aviation Safety Agency (EASA) AMC 20-158. AC 20-158 provides a means, but not the only means, for demonstrating compliance with Title 14 of the Code of Federal Regulations (14 CFR) 23.1308 (Amendment 57 and lower), 23.2520 (Amendment 64 and higher), 25.1317, 27.1317, 29.1317, and applicable FAA HIRF special conditions addressing HIRF Protection. AMC 20-158 is applicable to Certification Specifications CS 23.1308 (Amendment 4 and lower), 23.2520 (Amendment 5 and higher), 25.1317, 27.1317, and 29.1317. It should be noted that this document is neither mandatory nor regulatory in nature and does not constitute a regulation or legal interpretation of the regulation. Therefore, an applicant may elect to establish an alternative method of compliance that is acceptable to the
AE-4 Electromagnetic Compatibility (EMC) Committee
E-25 General Standards for Aerospace and Propulsion Systems
This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet, strip, and foil 0.100 inch (2.54 mm) and under in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers the requirements for electrodeposited gold plate.
AMS B Finishes Processes and Fluids Committee
This SAE Aerospace Recommended Practice (ARP) is intended to be used for laser systems mounted on aircraft and propagated into navigable airspace. This does not include lasers onboard aircraft where the beam is contained within an enclosure so that the beam cannot enter into airspace, nor does it include lasers from satellites and spacecraft in outer space. It may be used in conjunction with AS4970, ARP5535, ARP5572, ARP5293, and the ANSI Z136 laser safety standards.
G-10T Laser Safety Hazards Committee
SCOPE IS UNAVAILABLE.
E-25 General Standards for Aerospace and Propulsion Systems
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 a titanium alloy in the form of sheet, strip, and plate through 4.000 inches (101.6 mm) nominal thickness.
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of forgings 3.000 inches (76.20 mm) and under in nominal cross-sectional thickness and of stock for forging of any size.
AMS G Titanium and Refractory Metals Committee
This specification covers one type of copper in the form of bars, rods, and shapes. Requirements are provided for bar and rods up to 3.000 inches (mm) in nominal diameter, squares and rectangles with up to 4.000 inches (mm) least distance between parallel sides and shapes of any size (see 8.6).
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of die forgings, hand forgings, and forging stock.
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
This specification covers a copper-beryllium alloy in the form of sand, investment, or centrifugal castings (see 8.7).
AMS D Nonferrous Alloys Committee
AMS P Polymeric Materials Committee
This specification covers a titanium alloy in the form of bars, wire, flash-welded rings up through 4.000 inches (101.60 mm), inclusive, in diameter or least distance between parallel sides, and stock for flash-welded rings or heading of any size (see 8.6).
AMS G Titanium and Refractory Metals Committee
This specification covers a petroleum-base liquid solvent.
AMS B Finishes Processes and Fluids Committee
This specification defines the equipment, procedures, and requirements for joining leads by parallel gap resistance welding.
AMS B Finishes Processes and Fluids Committee
This specification covers a corrosion-resistant nickel-copper alloy in the form of copper-furnace-brazed tubing.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a butyl (IIR) rubber in the form of sheet, strip, extrusions, and molded shapes.
AMS CE Elastomers Committee
This specification covers a carbon steel in the form of wire supplied as coils, spools, or cut lengths (see 8.2).
AMS E Carbon and Low Alloy Steels Committee
This specification covers an alloy steel in the form of investment castings.
AMS E Carbon and Low Alloy Steels Committee
This specification covers optical-quality coatings applied to instrument glasses.
AMS B Finishes Processes and Fluids Committee
This specification covers a chloroprene (CR) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
AMS CE Elastomers Committee
This specification defines the procedures and requirements for fusion welding titanium and titanium alloys and the properties of such weldments.
AMS B Finishes Processes and Fluids Committee
This specification covers established manufacturing tolerances applicable to sheet, strip, and plate of corrosion- and heat-resistant steels, iron alloys, titanium, and titanium alloys. These tolerances apply to all conditions, unless otherwise noted. The term “excl” is used to apply only to the higher figure of the specified range.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification defines limits of variation for determining acceptability of the composition of wrought low-alloy and carbon steel parts and material acquired from a producer.
AMS E Carbon and Low Alloy Steels Committee
This specification covers a copper brazing filler metal in the form of a paste comprising a viscous mixture of powder in a suitable binder.
AMS D Nonferrous Alloys Committee
This specification covers one type of organic (para-aramid) fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.
AMS P17 Polymer Matrix Composites Committee
This specification covers a methyl or methyl vinyl silicone rubber material that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. This specification should not be used for molded rings, compression seals, O-ring cord, and molded in place gaskets for aeronautical and aerospace applications without complete consideration of the end use prior to the selection of this material.
AMS CE Elastomers Committee
This specification covers one type of organic (para-aramid) fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.
AMS P17 Polymer Matrix Composites Committee
This specification covers general requirements for direct current electrically held, environmentally sealed toggle switches for use in alternating current (AC) and direct current (DC) applications. (See 6.1.)
AE-7P Protective and Control Devices
This document covers the general recommendations for Transverse Electromagnetic Mode (TEM) Transmission Lines intended for use in airborne systems (see 6.2.14). For U.S military applications, TEM Transmission Lines shall meet the requirements in accordance with MIL-T-81490. The follow index lists the recommended requirements and methods covered by the Aerospace Recommended Practice (ARP):
AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
This specification covers two series of electrical, rectangular connectors with crimp type removable contacts. These connectors are provided with single, dual, triple, and quadruple insert shell configurations.
AE-8C1 Connectors Committee
This specification covers environment-resisting, quick disconnect, EMI/RFI shielded and non-shielded umbilical, electric connectors and adapter assemblies with removable crimp or nonremovable solder-type contacts and accessories. Connectors are rated for operation from -55 °C (-67 °F) to 200 °C (392 °F). Adapter assemblies are rated for operation from -55 °C (-67 °F) to 125 °C (257 °F). The upper temperature is the maximum internal hot spot temperature resulting from any combination of electrical load and ambient temperature.
AE-8C1 Connectors Committee
This specification covers an aluminum alloy in the form of plate 4.000 to 10.000 inches (101.6 to 254.0 mm), inclusive, in nominal thickness (see 8.5).
AMS D Nonferrous Alloys Committee
This standard establishes definitions, guidelines, and requirements governing materials (e.g., alloy and heat treat condition) allowed for use in chemical process test specimens when requirements call for a generic class of alloy.
AMS B Finishes Processes and Fluids Committee
This specification covers the detail requirements for control transformer synchro, type 16CTB4b, 90 volt, 400 cycle.
AE-7A Generators and Controls Motors and Magnetic Devices
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