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This specification covers two types of refined hydrocarbon compounds in the form of liquids. This specification only covers newly manufactured materials.
This specification covers an aluminum alloy in the form of sand, permanent mold, composite mold, and investment castings (see 8.6).
This specification covers an aluminum alloy in the form of permanent mold castings (see 8.6).
This SAE Aerospace Information Report (AIR) describes a mathematical model that can be used to analyze particle count data. Particle counts that fit the model can be graphically displayed, converted from one counting size-frequency range to another, and extrapolated to estimate counts beyond the measured range. Derivation, applications, and calculations are described.
This standard gives the dimensional requirements for insert arrangements used in AS81569 Series 1 and 2 electrical connectors.
This standard specifies basic and high performance test methods and requirements for round, screened and unscreened, multi-core sheathed cables intended for use in road vehicle applications. The unscreened, single-core cables shall be in accordance with ISO 6722, SAE J1127, SAE J1128, SAE J1654, SAE J1678, or SAE J2183. Other cores may be used, but in these cases, the construction and tests required to ensure functionality of these cores shall be agreed between customer and supplier. See ISO 6722 for temperature classes. ISO 6722 will be needed to perform some of the tests in this standard.
CLARA identifies four functions: Data Space Generator, Truth Data Generator, Coefficient Generator, and Reconstructor. Together these four functions standardize the solution to the LAR problem.
This method estimates noise for both single and tandem main rotor helicopters except for approach where it applies to single rotor designs only. It does not apply to coaxial rotor designs. Due to lack of available data, application of the method has not been evaluated for application to tiltrotor, or other VTOL configurations, when operating in the helicopter mode. Since there are substantial differences between helicopter rotors included in the data base, and tiltrotor rotors, application to VTOL configurations other than helicopters is not advised. Application is limited to helicopters powered by turboshaft engines and does not apply to helicopters powered by reciprocating engine, tip jets or other types of power plants. It provides noise information using basic operating and geometric information available in the open literature. To keep the method simple, it generates A-weighted sound levels, and Sound Exposure Levels precluding the necessity for spectral details. The method
Satisfactory measurements of noise in personnel-occupied rotorcraft cabins may require test techniques different from those prescribed for other types of aircraft (ARP1323) because rotorcraft operate under significantly different flight conditions. Recommendations of this ARP apply to the recording of acoustical data on magnetic tape and the subsequent processing and analysis of the recorded data.
This Aerospace Recommended Practice (ARP) defines quantities that may be used to describe various attributes of the sound field in the interior of aircraft. For a particular aircraft, or for a specific situation in a particular aircraft, it may not be necessary to utilize all the quantities included here to provide an adequate description of an aircraft's interior acoustical environment.
The primary measurement procedure recommended in this ARP includes the recording of sound pressure signals in the interior of an airplane during steady state cruise conditions with analysis after the flight into octave band (or one-third octave band) sound pressure levels.
The following recommendations and suggestions are made for consideration for procurement of new equipment, or modification to existing equipment where practical. Excluded from this AIR is mobile ground equipment, such as fork lift trucks and front end loaders, that have a functional requirement for simultaneous vehicle motion and accessory operation.
This SAE Recommended Practice provides design guidelines to vehicle manufacturers by establishing the characteristics of top tether anchorage provisions required for securing child restraints so equipped in forward facing rearmost designated passenger seating positions of all passenger cars, multipurpose passenger vehicles, and trucks and buses of 4500 kg (10 000 lb) Gross Vehicle Weight Rating or less, accommodating six occupants or less. Further, it provides interface information to child restraint manufacturers.
This document establishes the minimum requirements for the electrical bonding and grounding of electric, avionic, armament, communication, and electronic equipment installations for aeronautical and aerospace applications. The bonding and grounding requirements specified herein are to ensure that an adequate low resistance return path for electric, avionic, armament, communication and electronic equipment is achieved which can withstand operating conditions and corrosion. This is essential for the reduction of coupling of electromagnetic fields into or out of the equipment as well as for providing electrical stability to control the currents and/or voltages caused by static charges and discharges and for suppressing the hazardous effects thereof.
This SAE Aerospace Standard (AS) defines the parameters that describe the performance of an analog link transported over an optical fiber interconnect system suitable for aerospace applications.
This SAE Aerospace Recommended Practice (ARP) provides design, operation, construction, test and installation recommendations for equipment that automatically presents supplemental oxygen masks to cabin occupants in the event of loss of cabin pressure. It specifically covers automatic presentation for transport category aircraft that operate above 30 000 ft (9144 m) altitude. It also provides guidance for similar equipment used in non-transport category aircraft, or aircraft operated below 30 000 ft (9144 m) altitude.
This SAE Standard establishes basic dimensions for motor vehicle license plates. It is based on data supplied by the American Association of Motor Vehicle Administrators, Motor Vehicle manufacturers Association, and Motorcycle, Scooter and Allied Trades Association. The dimensions established in this document have considered legibility and identification of the license plate.
This specification covers flash welded rings fabricated from carbon and low-alloy steels.
The recommendations cover stowage of all portable cabin emergency equipment, including: a Oxygen bottles/units b Oxygen masks c Fire extinguishers d Protective breathing equipment (PBE) e First aid kits f Emergency/expanded medical kits and pouches g Megaphones h Flashlights i Life rafts j Survival kits k Life preservers l Flotation seat cushions m Emergency locator transmitters (ELT) n Automatic external defibrillators (AED) o Resuscitation/life support equipment
This specification covers the design requirements and all performance requirements for procurement of 1 7/8 inch dial pilot’s standby compasses as specified herein.
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