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Wheels and Brakes, Supplementary Criteria for Design Endurance Civil Transport Aircraft
- Aerospace Standard
Published May 07, 2015 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This document recommends supplementary design criteria to enhance endurance and reliability of transport aircraft wheels and brakes.
This document is being stabilized in recognition by the A-5A committee that the supplemental criteria defined in this document is considered mature technology and has become a part of airframer's technical specifications for current state of the art aircraft. Other SAE documents such as AIR5490 Carbon Brake Contamination and AIR1934 Use of Structural Carbon Heat Sink Brakes on Aircraft offer additional guidance regarding supplemental design criteria such as addressing the damaging effects of alkali metal runway deicers on carbon brakes.
|Aerospace Standard||Maintainability Recommendations for Aircraft Wheel and Hydraulically Actuated Brake Design|
|Aerospace Standard||Mechanical Control Design Guide|
|Aerospace Standard||Aircraft Tire Pressure Monitoring Systems|
Data Sets - Support Documents
|Unnamed Dataset 1|
|TABLE 1||PERCENT RATED LOAD (MAXIMUM STATIC)|
|TABLE 2||STEEL BRAKES|
|Unnamed Dataset 4|
|TABLE 3||CARBON BRAKES|
|Unnamed Dataset 6|
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