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This specification covers accelerated curing synthetic rubber compounds with corrosion inhibitors and low adhesive strength supplied as a two-component system
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of June 1996, and has been superseded by AMS 3731 & /1
This drawing specifies parts AS54712, AS54713, AS54714, AS54715, AS54716, AS54717, AS54718, AS54719, AS54720, AS54721, AS54722, AS54723, AS54724, AS54725, AS54726, AS54727, AS54728, AS54729, AS54730, AS54731, AS54732, AS54734, AS54736, AS54738, AS54740, AS54742, AS54744, AS54746, AS54748, AS54750, AS54752, AS54754, AS54756, AS54758, AS54760, AS54762, AS54764, AS54766, AS54768, AS54770, AS54772, AS54774, AS54776, AS54778, AS54780, AS54782, AS54784, AS54786, AS54788, AS54790, AS54792, AS54794, and AS54796. To view suppliers qualified to manufacture this part, visit https://ts200.sae-itc.org
No Scope available
This specification covers epoxy-resin-impregnated glass fabric laminates in the form of sheet clad on one or both sides with electrolytically-deposited copper foil
This SAE Aerospace Recommended Practice (ARP) presents two BASIC language computer programs to promote and standardize the computation of installed O-ring cross-section deflection hereafter referred to as "squeeze" and the computation of gland volume. The two programs were written with line numbers and without use of any system specific BASIC commands to allow usage with as many systems as possible with a minimum of editing. The programs support entry of customary U.S. or metric dimensions. The squeeze program, called SQ.BAS, has the following features: a allows selection of either piston or rod gland b allows entry of cap strip seal thickness c computes minimum and maximum squeeze d allows checking and correction of entries before execution e allows viewing of output on screen before printing f gives advisory messages for excessive stretch or inadequate squeeze g allows on-line review of essential input and output variables prior to running program h computes clearance between minimum
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995
No scope available
This technical specification document describes tests that certain parts may be required to meet. For example, this tech spec applies to All parts to TS147. To view suppliers qualified against this standard, visit https://ts200.sae-itc.org
This drawing specifies parts AS55018, AS55019, AS55020, AS55021, AS55022, AS55023, AS55024, AS55025, AS55026, AS55027, AS55028, AS55029, AS55030, AS55031, AS55032, AS55034, AS55036, AS55038, AS55040, AS55042, AS55044, AS55046, AS55048, AS55050, AS55052, AS55054, AS55056, AS55058, AS55060, AS55062, AS55064, AS55066, AS55068, AS55070, AS55072, AS55074, AS55076, AS55078, AS55080, AS55082, AS55084, AS55086, AS55088, AS55090, AS55092, AS55094, and AS55096. To view suppliers qualified to manufacture this part, visit https://ts200.sae-itc.org
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of June, 1996, and has been supersed by AMS 3731 & /7
It is intended that this SAE Aerospace Recommended Practice (ARP) will set down guidelines for the development and test of gas motors to provide a practical and reliable hot gas rotary actuation mechanism. Specific operational and test requirements shall be specified in a detail specification
These recommendations are written to cover the subject of engine exhaust gas to air type heat exchangers under the following classifications
This document describes guidelines and methods of performing the safety assessment for certification of civil aircraft. It is primarily associated with showing compliance with FAR/JAR 25.1309. The methods outlined here identify a systematic means, but not the only means, to show compliance. A subset of this material may be applicable to non-25.1309 equipment. The concept of Aircraft Level Safety Assessment is introduced and the tools to accomplish this task are outlined. The overall aircraft operating environment is considered. When aircraft derivatives or system changes are certified, the processes described herein are usually applicable only to the new designs or to existing designs that are affected by the changes. In the case of the implementation of existing designs in a new derivation, alternate means such as service experience may be used to show compliance
The purpose of this SAE Aerospace Recommended Practice (ARP) is to standardize locations of aircraft ground service connections to accommodate the trend toward fixed systems, which use the passenger boarding bridge and/or underground “pop-up” or pit systems as a source of utilities. It must be recognized that, in standardizing the locations of the aircraft service connections, they must continue to be served efficiently in those instances where mobile ground support equipment is used. There is an ever increasing number of fixed installations for aircraft servicing. The objectives to be met by standardizing the locations of the aircraft service connections are the following
This standard covers three basic types of total-temperature-measuring instruments used as a means of determining the total temperature developed by adiabatic heating of the air due to motion of the aircraft through the air. Type I - Flush-type total-temperature sensor Type II - Probe-type total-temperature sensor (electrically heated) Type III - probe-type total-temperature sensor (unheated
This SAE Information Report identifies some enhancements that may be applied to V2X standards, addressing new use cases that require or benefit from high levels of position precision and integrity
Vehicle electrical/electronic systems may be affected when immersed in an electromagnetic field generated by sources such as radio and TV broadcast stations, radar and communication sites, mobile transmitters, cellular phones, etc. The reverberation method is used to evaluate the immunity of electronic devices in the frequency range of 500 MHz to 2.0 GHz, with possible extensions to 200 MHz and 10 GHz, depending upon chamber size and construction. Optional pulse modulation testing at HIRF (High Intensity Radiated Fields) test levels, based upon currently known environmental threats, has been added to this revision of the standard. This document addresses the Mode Stir (Continuous Stirring) Reverberation testing method which has been successfully utilized as a design and production stage development tool for many years. The Mode Tuned (Stepped Tuner) Reverberation testing method is covered in the SAE J1113-28 document
A general method for the preliminary design of a single, straight-sided, low subsonic ejector is presented. The method is based on the information presented in References 1, 2, 3, and 4, and utilizes analytical and empirical data for the sizing of the ejector mixing duct diameter and flow length. The low subsonic restriction applies because compressibility effects were not included in the development of the basic design equations. The equations are restricted to applications where Mach numbers within the ejector primary or secondary flow paths are equal to or less than 0.3
This SAE Aerospace Standard (AS) prescribes requirements for the various types of nozzles that are used for the refueling and defueling of aircraft fitted with pressure fuel servicing systems. It is to be used as a replacement for MIL-N-5877, MS29520 and for all commercial applications
This specification covers a two-component adhesive compound, an epoxy resin base and a hardener, in the form of a paste
This specification covers molded or extruded bar, rod, and shapes produced from a polyamide-imide (PAI) polymer filled with 20% graphite and 3% polytetrafluoroethylene (PTFE). This is designated as Grade 2 material per AMS3670
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
This document describes a manufacturing method for processing unidirectional carbon fiber/epoxy resin impregnated sheet and tape into multi-ply broadgoods and tape produced on an automated cross-plying machine. Broadgoods or tape of two or more ply configurations may be processed, where ply orientations of 0°, 45°, 90°, and 135° (as examples) may be automatically layed in a programmed sequence. In all configurations, the 0° ply direction is parallel to the length of the broadgoods roll or sheet, or tape
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