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This SAE Recommended Practice establishes a method of evaluating the structural integrity of the parking brake system of all new trucks, buses, and combination vehicles designed for roadway use in the following classifications: TRACTOR, TRAILER, TRUCK, AND BUS: over 4500 kg (10 000 lb) GVWR
Truck and Bus Foundation Brake Committee
This AIR was prepared to inform the aerospace industry about the electromagnetic interference measurement capability of spectrum analyzers. The spectrum analyzers considered are of the wide dispersion type which are electronically tuned over an octave or wider frequency range. The reason for limiting the AIR to this type of spectrum analyzer is that several manufacturers produce them as general-purpose instruments, and their use for EMI measurement will give significant time and cost savings. The objective of the AIR is to give a description of the spectrum analyzers, consider the analyzer parameters, and describe how the analyzers are usable for collection of EMI data. The operator of a spectrum analyzer should be thoroughly familiar with the analyzer and the technical concepts reviewed in this AIR before performing EMI measurements
AE-4 Electromagnetic Compatibility (EMC) Committee
This SAE Recommended Practice establishes methods to determine grade parking performance with respect to: a Ability of the parking brake system to lock the braked wheels. b The trailer holding or sliding on the grade, fully loaded, or unloaded. c Applied manual effort. d Unburnished or burnished brake lining friction conditions. e Down and upgrade directions
Truck and Bus Brake Systems Committee
This Aerospace Information Report (AIR) is intended to provide information relating to the construction, calibration, and usage of parallel plate transmission lines in electromagnetic compatibility susceptibility testing
AE-4 Electromagnetic Compatibility (EMC) Committee
This specification covers an aluminum alloy in the form of rolled or cold finished bars and rods of the sizes specified in 3.3.1.1 (see 8.5
AMS D Nonferrous Alloys Committee
This specification covers one type of copper alloy (brass) in the form of bars and rods up to 4.000 inches (101.60 mm) in nominal diameter, thickness between parallel sides, or width as defined in Tables 3 through 6 (see 8.6
AMS D Nonferrous Alloys Committee
This specification covers a polysulfide sealing compound with low adhesive strength, supplied as a two-component system that cures at room temperature
AMS G9 Aerospace Sealing Committee
This recommended practice establishes the requirements and procedures for Barkhausen Noise (BN) inspection of ferromagnetic steel components. See Appendix B for a list of common materials for BN inspection. Applications of the method are listed in 1.2 through 1.5
AMS K Non Destructive Methods and Processes Committee
This SAE Recommended Practice provides test methods and criteria for evaluating the internal cleanliness and air leakage for engine charge air coolers. This SAE Recommended Practice also provides nomenclature and terminology in common use for engine charge air coolers, related charge air cooling system components, and charge air cooling system operational performance parameters
Cooling Systems Standards Committee
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 specification covers the engineering requirements for electrodeposition of nickel and the properties of the deposit
AMS B Finishes Processes and Fluids 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 one grade of commercially pure titanium in the form of bars, wire, forgings, flash welded rings, up to 4.000 inches (101.60 mm), inclusive, in nominal diameter or least distance between parallel sides, and stock for forging or flash welded rings
AMS G Titanium and Refractory Metals Committee
This specification covers an aluminum alloy in the form of welding wire
AMS D Nonferrous Alloys Committee
This specification covers one type of aluminum bronze in the form of bars, rods, forgings, and forging stock
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of sheet, clad on one side
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of honeycomb core in a non-hexagonal, flexible cell configuration, the core being treated for increased corrosion resistance and furnished only in the expanded form
AMS D Nonferrous Alloys Committee
This specification covers established inch/pound manufacturing tolerances applicable to low-alloy steel sheet, strip, and plate ordered to inch/pound dimensions. 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 E Carbon and Low Alloy Steels Committee
AMS2980/1 gives information about the technical requirements and qualification procedure for carbon fiber fabric and epoxy resin systems used for wet lay-up repair of carbon fiber reinforced epoxy structures
AMS CACRC Commercial Aircraft Composite Repair Committee
AMS2980/2 gives specific information about the qualification program for carbon fiber fabric, epoxy systems and the material combination used for wet lay-up repair of carbon fiber reinforced epoxy structures
AMS CACRC Commercial Aircraft Composite Repair Committee
This specification establishes the requirements for brush plating of copper by electrodeposition
AMS B Finishes Processes and Fluids Committee
This specification covers flash welded rings fabricated from carbon and low-alloy steels
AMS E Carbon and Low Alloy Steels Committee
This SAE Aerospace Recommended Practice (ARP) establishes general criteria for the installation (e.g., type, location, accessibility, stowage) and crew member training needed for hand-held fire extinguishers
S-9A Safety Equipment and Survival Systems Committee
This SAE Aerospace Standard (AS) defines the performance requirements for equipment to be used by untrained cabin occupants for protection from toxic and irritant atmospheres while on board and during evacuation of an aircraft
A-10 Aircraft Oxygen Equipment Committee
This document describes particulate filter weigh-room recommended practices to provide guidance in the procedures and processes associated with gravimetric filter weighing of engine or vehicle particulate matter (PM) emissions. This recommended practice provides proper procedures to build and maintain a particulate filter weigh room or enclosure to meet the requirements of EPA's 40 CFR Part 1065 and ISO 14065 for obtaining low measurement uncertainty. The content of this recommended practice addresses the following areas: a Particulate Filter Weigh Room b Microbalance Requirements c Filter Conditioning and Handling Requirements d Weighing Process e Equipment Calibration and Maintenance
Emissions Standards Committee
This SAE Standard describes a reference system architecture based on LTE-V2X technology defined in ETSI Release 14. It also describes cross-cutting features unique to LTE-V2X PC5 sidelink (mode 4) that can be used by current and future application standards. The audience for this document includes the developers of applications and application specifications, as well as those interested in LTE-V2X system architecture, testing, and certification
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The purpose of this SAE Aerospace Information Report (AIR) is to provide guidance for aircraft engine and propeller systems (hereafter referred to as propulsion systems) certification for cybersecurity. Compliance for cybersecurity requires that the engine control, propeller control, monitoring system, and all auxiliary equipment systems and networks associated with the propulsion system (such as nacelle systems, overspeed governors, and thrust reversers) be protected from intentional unauthorized electronic interactions (IUEI) that may result in an adverse effect on the safety of the propulsion system or the airplane. This involves identification of security risks, their mitigation, verification of protections, and their maintenance in service. This document is intended to serve as suitable guidance for propulsion system manufacturers and applicants for propulsion system type certification. It is also intended to provide guidance for subsequent propulsion system integration into
E-36 Electronic Engine Controls Committee
This specification covers the requirements for electrodeposited nanocrystalline cobalt-phosphorus plating
AMS B Finishes Processes and Fluids Committee
This specification covers the requirements for brush plating of non-cyanide silver by electrodeposition
AMS B Finishes Processes and Fluids Committee
This specification covers the requirements for brush plating of medium-hardness, low stress nickel by electrodeposition
AMS B Finishes Processes and Fluids Committee
This specification covers an adhesive compounded from modified epoxy resins in ready-to-use film supplied in rolls or sheets, either supported by mat or by woven monofilaments or unsupported
AMS P17 Polymer Matrix Composites Committee
This specification covers high-purity not less than (99.95%) silica in the form of woven cloth
AMS P17 Polymer Matrix Composites Committee
This SAE Aerospace Standard (AS) covers any protective system that serves the stated purpose
A-10 Aircraft Oxygen Equipment Committee
This standard covers oronasal type masks which use a continuous flow oxygen supply. Each such mask comprises a facepiece with valves as required, a mask suspension device, a reservoir, or rebreather bag (when used), a length of tubing for connection to the oxygen supply source, and a means for allowing the crew to determine if oxygen is being delivered to the mask. The assembly shall be capable of being stowed suitably to meet the requirements of its intended use
A-10 Aircraft Oxygen Equipment Committee
This specification establishes the requirements for undyed thin anodic coatings on aluminum alloys using chemical solutions containing sulfuric acid
AMS B Finishes Processes and Fluids Committee
This specification covers a corrosion-resistant nickel-copper alloy in the form of seamless tubing
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion and heat-resistant steel in the form of bars, wire, tubing, forgings, and forging stock
AMS F Corrosion and Heat Resistant Alloys Committee
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