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Standard
2013-11-01
This document covers military aircraft wheel and hydraulically actuated brake equipment.
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
It is the purpose of this document to present design recommendations that will provide a basis for satisfactory and safe electrical installations in transport aircraft. This document is not intended to be a complete electrical installation design handbook. However, the requirements for safety extend so thoroughly throughout the electric systems that few areas of the installation are untouched by the document. It is recognized that individual circumstances may alter the details of any design. It is, therefore, important that this document not be considered mandatory but be used as a guide to good electrical application and installation design. Transport aircraft electric systems have rapidly increased in importance over a number of years until they are now used for many functions necessary to the successful operation of the aircraft. An ever increasing number of these functions are critical to the safety of the aircraft and its occupants. The greatly increased power available in electric systems is another factor in aircraft safety.
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
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
2013-10-30
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.
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
Standard
2013-10-29
Dynamic simulation sled testing can represent various automotive collision conditions. Acceleration conditions during sled testing are readily reproducible and can be tuned to simulate collision events that occur during vehicle impacts with a fixed barrier or vehicle. Sled tests are conducted on automotive vehicle bodies or other structures to obtain valuable information. This information can be used to evaluate the dynamic performance of, but not limited to, vehicle restraint systems, vehicle seating systems, and body closure systems.
Standard
2013-10-28
This specification established (1) the common requirements for hydraulic units capable of functioning as starters and as pumps suitable for use in aircraft and missiles and (2) the methods to be used for demonstrating compliance with these requirements.
WIP Standard
2013-10-25
Develop a test procedure for the small female ball slider low speed test similar to J2876 for the 50th male.
Standard
2013-10-25
This SAE Aerospace Standard (AS) covers the requirements for a flexible, lightweight, low pressure, self-extinguishing, silicone hose assembly. The hose has a fully fluorinated fluoropolymer inner liner and is primarily intended for use in aircraft potable water systems.
Standard
2013-10-25
This SAE Aerospace Standard (AS) covers the requirements for a flexible, lightweight, low pressure, self-extinguishing, integrally heated silicone hose assembly. The hose has a fully fluorinated fluoropolymer inner liner and is primarily intended for use in aircraft potable water systems with an environmental operating temperature range of -65 °F (-54 °C) to +160 °F (+71 °C).
WIP Standard
2013-10-22
Scope unavailable.
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
2013-10-21
This SAE Standard specifies minimum performance and test criteria for brake systems to enable uniform assessment of the braking capability of walk-along self-propelled work machines with a mass greater than 115 kg. Service and parking brake systems are covered by this document.
Standard
2013-10-20
Scope is unavailable.
Standard
2013-10-20
Scope is unavailable.
Standard
2013-10-20
Scope is unavailable.
Standard
2013-10-20
Scope is unavailable.
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