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Viewing 161941 to 161970 of 182494
1968-12-01
Standard
AIR1064
This SAE Aerospace Information Report (AIR) has been prepared by a panel of the A-5A Subcommittee to present an overview of the landing gear problems associated with aircraft braking system dynamics, and the approaches to the identification, diagnosis, and solution of these problems. All pertinent system modes of vibration are described. In addition, facilities and techniques available for test and evaluation are presented and discussed, and useful references are cited. The terminology used is intended to be consistent with AIR1489, "Aerospace Landing Gear Systems Terminology", but some terminology herein is not yet included in AIR1489. The panel members include representatives from major brake, landing gear, aircraft, and brake control system manufacturers. In addition, drafts of the document were circulated for input beyond the SAE to other experts in the field.
1968-12-01
Standard
AIR1059
This document provides guidance concerning the maintenance and serviceability of oxygen cylinders beginning with the quality of oxygen that is required, supplemental oxygen information, handling and cleaning procedures, transfilling and marking of serviced oxygen assemblies. This document attempts to outline in a logical sequence oxygen quality,serviceability and maintenance of oxygen cylinders.
1968-12-01
Standard
AIR1059A
Recharging of small portable oxygen cylinders by the user is a practice both condemned and discouraged by the Compressed Gas Association (CGA) and the National Fire Protection Association (NFPA). Their condemnation is based on the firm conviction of the majority of the Association members that 'transfilling' and oxygen cylinder by 'unqualified' personnel is basically unsafe and should not be performed. By logic, therefore, it must be deduced that all personnel assigned to transfilling must be qualified. The purpose of this document is to list the best available information and guidelines for the qualification of personnel who are responsible for the filling of fixed or portable aircraft oxygen cylinders. It is a matter of record that the commercial airlines, aircraft manufacturers, and aircraft service stations have been involved in, and will continue to follow, the practice of filling the small portable oxygen units and fixed oxygen cylinders in commercial and general aviation.
1968-12-01
Standard
J587C_196812
This SAE Standard provides test procedures, requirements, and guidelines for vehicular license plate illumination devices.
1968-11-15
Standard
AS1033A
No scope available.
1968-11-15
Standard
AS1037A
No scope available.
1968-11-15
Standard
AS1035A
No scope available.
1968-11-15
Standard
AS1040A
No scope available.
1968-11-15
Standard
AS1038A
No scope available.
1968-11-15
Standard
AS1036A
No scope available.
1968-11-13
Standard
AS26090-2
No scope available.
1968-11-01
Standard
AMS4043A
ABSTRACT
1968-11-01
Magazine
1968-11-01
Standard
J944A_196811
1. SCOPE Evaluation of the energy absorbing properties of the steering wheel assembly of a motor vehicle, or of the relative merit of altemative designs of such assemblies, is a complex problem involving human tolerance, vehicle and occupant dynamics during an accident, and frequency and severity of injuries to various body areas. T\'lO fundamental approaches are being used currently for steering wheel assembly evaluations: laboratory impact tests of varying degrees of complexity, and simulated collision tests. This SAE Recommended Practice describes a simplified laboratory procedure for evaluating the characteristics of steering wheel assemblies under simulated driver impact conditions. Basically, the test procedure employs a torso shaped body block which is impacted against the steering wheel assembly and the transmitted load -time history is measured.
1968-11-01
Standard
AMS4053A
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of March 1995. By this action, subject specification number and title will be deleted from the active specification index of Aerospace Material Specifications.
1968-11-01
Standard
AMS2350L
To establish the issue of specifications, standards, and recommended practices published by standardizing agencies other than divisions and committees of the Aerospace Council of SAE approved for use in determining conformance to requirements of Aerospace Material Specifications (AMS) and other specifications in which this specification is referenced.
1968-11-01
Standard
AMS2503B
This specification covers the engineering requirements for finishing aircraft parts and assemblies with a black enamel.
1968-11-01
Standard
AMS2505B
This specification has been declared "CANCELLED " by the Aerospace Materials Division, SAE, as of December 2008. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been "CANCELLED ".
1968-11-01
Standard
AMS2815G
This specification covers procedures for marking bare wire for welding to provide positive identificaiton of cut lengths, regardless of length, and of spools, and to ensure that the wire is clean and free from foreign materials and corrosion.
1968-11-01
Standard
AMS3165B
This specification covers a petroleum-base liquid solvent.
1968-11-01
Standard
AMS6438A
This specification covers a premium aircraft-quality, low-alloy steel in the form of sheet, strip, and plate. This product has been used typically for heat treated parts, which may be welded during fabrication and which require through-hardening to high strength levels, for use up to 600 degrees F (316 degrees C), but usage is not limited to such applications.
1968-11-01
Standard
AMS6475C
This specification covers a nitriding grade of aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for nitrided parts requiring highest surface hardness, high core hardness, resistance to heat, and less distortion than parts made from steel requiring quenching to case harden, but usage is not limited to such applications.
1968-11-01
Standard
AMS6467A
This specification covers a low-alloy steel in the form of covered welding electrodes.
1968-11-01
Standard
AMS6466A
Primarily for use as filler metal for welding low alloy steels whre response to heat treatment is required in the weld.
1968-11-01
Standard
AMS5799A
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of April 1996 and has been superseded by AWS A5.11 ENiCrMo-2.
1968-11-01
Standard
AMS5555
This specification covers nickel in the form of round wire and rectangular ribbon.
1968-11-01
Standard
AMS5595
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate. These products have been used typically for parts requiring high strength and corrosion resistance from -423 to +1100 °F (-253 to +593 °C), where such parts may require welding during fabrication, but usage is not limited to such applications.

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