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Wheels and Brakes, Supplementary Criteria for Design Endurance Civil Transport Aircraft
- Aerospace Standard
- ARP597E
- Stabilized
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This document recommends supplementary design criteria to enhance endurance and reliability of transport aircraft wheels and brakes.
Rationale
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.
Recommended Content
Aerospace Standard | Maintainability Recommendations for Aircraft Wheel and Hydraulically Actuated Brake Design |
Aerospace Standard | Mechanical Control Design Guide |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
TABLE 1 | PERCENT RATED LOAD (MAXIMUM STATIC) | |
TABLE 2 | STEEL BRAKES | |
Unnamed Dataset 4 | ||
TABLE 3 | CARBON BRAKES | |
Unnamed Dataset 6 |
Issuing Committee
Reference
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