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Standard
2013-11-06
This document establishes the minimum criteria for effective training of air carrier and contractor personnel to deice/anti-ice aircraft to ensure the safe operation of aircraft during ground icing conditions. Appendix D specifies guidelines for particular airplane models.
Standard
2013-11-06
This specification covers two types of cleaner in the form of a ready-to-use liquid. Primarily for removing soils, contaminants, and residues from aircraft glass windows by manual application. The cleaners covered by this specification shall be of the following types as ordered: Type I - Regular; and Type II - Antifogging.
WIP Standard
2013-11-01
This standard is applicable to all phases of system acquisition. It is intended for use on all programs with manufacturing content. It requires proven manufacturing management practices to promote delivery of affordable and capable systems to the extent that it is invoked contractually.
Standard
2013-11-01
The focus of this SAE Aerospace Standard (AS) is the integration of thermally actuated pressure release devices, hereafter referred to as fuse plugs, with the wheel and brake assembly. It does not address the manufacturing, quality or acceptance test requirements pertaining to the production of these fuse plugs. It establishes minimum design, installation, qualification, and operational requirements for fuse plugs which are used only in tubeless tire type aircraft braked wheels. Fuse plugs are designed to completely release the contained inflation pressure from a tubeless tire and wheel assembly when brake generated heat causes the tire or wheel to exceed a safe temperature level. The objective is to prevent tire or wheel rupture due to brake generated heat that could cause an unsafe condition for personnel or the aircraft. (Reference: U.S. Department of Transportation FAA Advisory Circular No. 23-17C; Title 14, Code of Federal Regulations (14 CFR) Part 25.735 (j); U.S. Department of Transportation FAA Advisory Circular No. 25.735-1 and U.S.
Standard
2013-11-01
This SAE Aerospace Standard (AS) defines the requirements for brake systems used on military aircraft equipped with wheel-type landing gears.
Standard
2013-11-01
This document covers military aircraft wheel and hydraulically actuated brake equipment.
Book
2013-11-01
Ian K. Jennions
Although the concept of Integrated Vehicle Health Management (IVHM) can be complex in its implementation, it is essentially based upon a simple idea: the more you know about a particular machine’s ability to function, the quicker you can act to prevent malfunctioning. This rapidly developing area of engineering seeks to enable better management of both the vehicle and vehicle fleet health. Use of IVHM can improve vehicle reliability, safety, and reduce unnecessary, unscheduled maintenance through the use of diagnostic and prognosis systems that monitor data and overall vehicle health. From an initial idea by the SAE IVHM Steering Group, these books have been collaboratively written by experts from academia, research and industry, and represent the collective voice of the most qualified authorities in the field. This groundbreaking set addresses both basic and advanced concepts critical for the understanding of IVHM, along with the commercial justification for the adoption of a new modus operandi in asset health management, and its impact on business strategy and technology.
WIP Standard
2013-10-31
This material establishes the minimum criteria for effective training of air carrier and contractor personnel to deice/anti-ice aircraft and to ensure the safe operation of aircraft during ground icing conditions. This program will provide guidelines for the proper procedures to deice and anti-ice aircraft on the ground. It is for training Ground, Flight and Dispatch personnel. Background information to support this training program is provided to make the material a better tool for the preparation and execution of the training and qualification process. A Standard Teaching Plan and the Practical Assessment are included. This material was compiled using various international documents with support from SAE documents and individually contributed editorial comments. Its purpose is to serve as a “Universal Deicing Training Manual”.
WIP Standard
2013-10-31
The purpose of this document is to provide industry recommennded proceduresguidelines for the methods and procedures used in performing the operations and services necessary for proper deicing and anti-icing of aircraft on the ground.
WIP Standard
2013-10-31
The purpose of this SAE Aerospace Information Report (AIR) is to provide information regarding the basic requirements for environmental effects of composite materials used in ULDs. Material variances related to raw materials and manufacturing processes is not part of this information, nor is damage tolerance.
WIP Standard
2013-10-30
This document contains guidelines for establishing clear concise standardized communication and phraseology between aircraft Flight and Ground crews during aircraft deicing operations. It is very important that both parties communicate fully about contact requirements, aircraft configuration, de/anti-icing treatment needed and post deicing reporting requirements
WIP Standard
2013-10-30
This SAE Aerospace Information Resource Document (AIR) covers Forced Air technology including: reference material, equipment, safety, operation, and methodology. This resource document is intended to provide information and minimum safety guidelines regarding use of forced air or forced air/fluid equipment to remove frozen contaminants.. During the effective period of this document relevant sections herein should be considered and included in all/any relevant SAE documents.
Standard
2013-10-29
This Recommended Practice applies to technical publications which present instructions for the proper unloading, set-up, installations, pre-delivery inspection, operation, and servicing of off-road self-propelled work machines as categorized in SAE J1116. Advertising/marketing and other pre-purchase publications are not included.
Standard
2013-10-22
This Recommended Practice outlines the electrical performance characteristics for a continuous duty, diesel or gasoline engine driven brushless alternator unit for supplying 400-Hertz electrical power to commercial transport aircraft. It is intended to assist the airlines in standardizing recommendations for various sizes and configurations of equipment and it is a guide for the preparation of detailed specifications. The unit is primarily intended to supply power to the aircraft during passenger loading and unloading, and during servicing operations. The combination of the equipment specified herein and the interconnecting cables(s) between the 400-Hertz alternator and the aircraft shall provide power characteristics at the aircraft receptacle which meet MIL-STD-704 requirements for Category "B" equipment. Other limits which are necessary to meet specific conditions must be specified by the purchaser.
Standard
2013-10-21
This document establishes standard graphical symbols and color conventions for use in either still (static) or animated graphics used for communicating service information. This document's purpose is to communicate conventions for using those symbols and colors to accurately and consistently communicate intended information via graphics-based documentation. These practices are intended for use in service procedures, assembly instructions, training materials, and similar applications when trying to minimize the amount of human natural language text used within the document. The still and animated graphical conventions referenced should support effective communication via paper and "traditional" electronic media. The conventions can also extend to documenting via additional electronic delivery paradigms such as Augmented Reality (AR). This document is intended for organizations interested in using graphics-based documentation to record and communicate assembly, adjustment, maintenance, and other service procedures.
WIP Standard
2013-10-21
This Aerospace Information Report will summarize several existing aircraft landing gear shimmy analysis techniques and provide guidance on the synthesis and testing of tire properties, strut properties, and other landing gear mechanical properties that support the various shimmy analysis methods. This AIR is applicable to large and small fixed wing and rotary wing aircraft for military or civilian use.
Standard
2013-10-20
The task of chemical process operator in the parts cleaning area is generally considered unskilled labor and in the past, little or no training had been provided or recommended. Since overhaul cleaning is a critical process step prior to visual and fluorescent penetrant inspection processes, consideration must be given to minimum levels of training for these process operators. It is the responsibility of the department supervisor to ensure that all personnel within the department are trained to acceptable level in all general aspects of health and safety and basic operating procedures. This document is intended to augment the local quality control system which will control the application and frequency of the guidelines stated within.
Standard
2013-10-20
Scope is unavailable.
Standard
2013-10-20
Scope is unavailable.
Standard
2013-10-20
Scope is unavailable.
WIP Standard
2013-10-18
This specification covers nonfluorescent, magnetic particles having black, red, gray, or other color, as specified, supplied in the form of dry powders. This product is used typically as an inspection medium in a dry magnetic particle inspection process in accordance with ASTM E 1444, but usage is not limited to such application.
WIP Standard
2013-10-18
This specification covers nonfluorescent magnetic particles in the form of a mixed, ready-to-use suspension in an odorless inspection oil vehicle. These products have been used typically as the inspection medium in a wet magnetic particle inspection system in accordance with ASTM E 1444, but usage is not limited to such application.
WIP Standard
2013-10-18
This specification covers nonfluorescent, magnetic particles in the form of dry powders intended to be suspended in oil or conditioned water vehicle for use in the wet method, magnetic particle inspection. These particles have been used typically as the inspection medium in a wet magnetic particle inspection system in accordance with ASTM E 1444, using either an oil or a conditioned water vehicle, but usage is not limited to such application.
WIP Standard
2013-10-18
This specification covers nonfluorescent magnetic particles in the form of a mixed, ready to use suspension in an odorless oil vehicle and packaged in aerosol cans. These particles have been used typically as the inspection medium in a wet magnetic particle inspection system in accordance with ASTM E 1444, but usage is not limited to such application.
WIP Standard
2013-10-18
This specification covers fluorescent magnetic particles in the form of a dry powder. These particles have been used typically as the inspection medium in wet, fluorescent magnetic particle inspection system as defined in ASTM E 1444 using either an oil or conditioned-water vehicle, but usage is not limited to such application.
WIP Standard
2013-10-18
This specification covers fluorescent magnetic particles in the form of a mixed, ready to use suspension in an odorless inspection oil vehicle. These particles have been used typically as the inspection medium in a wet method, magnetic inspection system as defined in ASTM E 1444, but usage is not limited to such application.
Standard
2013-10-17
This specification establishes the classification, technical requirements, tests, and test procedures for the qualification, approval, and quality verification of all materials used in the liquid penetrant methods of inspection with the exception of those excluded in the application section.
Technical Paper
2013-10-14
Chao Liu, Changfu Zong, Lei He, Chunshan Li, Minghui Liu
A fault detection and diagnosis (FDD) algorithm of 4WID/4WIS Electric Vehicles has been proposed in this study aiming to find the actuator faults. The 4WID/4WIS EV is one of the promising architectures for electric vehicle designs which is driven independently by four in-wheel motors and steered independently by four steering motors. The 4WID/4WIS EVs have many potential abilities in advanced vehicle control technologies, but diagnosis and accommodation of the actuator faults becomes a significant issue. The proposed FDD approach is an important part of the active fault tolerant control (AFTC) algorithm. The main objective of the FDD approach is to monitor vehicle states, find the faulty driving motor and then feedback fault information to the controller which would adopt appropriate control laws to accommodate the post-fault vehicle control system. The unique character of the proposed FDD approach is that it is a system-level method, namely it tries to locate the faulty motor and motor driver systems, while it does not need to identify which part of the motor and motor driver systems has a failure.
Standard
2013-10-11
This document is offered to provide state-of-the-art information about design factors that must be considered in the design of new or significantly modified engine test cells used to test propeller equipped turboprop engines in either QEC or bare engine configurations. The report does not address design considerations for test cells designed to test turboprop engines with dynamometer type load absorption devices because they are essentially tested as turboshaft engines. Design considerations for those test cells are presented in AIR4989, Reference 2.1.
WIP Standard
2013-10-10
This ARP documents methods and processes that may be utilized by aircraft manufacturers (or type certificate holders, researchers, or others) to evaluate the aerodynamic effects of SAE aircraft ground deicing/anti-icing fluids (“fluids”) when applied to specific aircraft.
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