SAE International WHEEL ROLL ON RIM CRITERIA FOR AIRCRAFT APPLICATION ARP1786

Description
This document sets forth minimum roll performance capability for main landing gear wheel to be rolled without tire. The recommended test requirements establish a laboratory demonstration level to equate satisfactory experience on aircraft.
Description
This document sets forth minimum roll performance capability for main landing gear wheel to be rolled without tire. The recommended test requirements establish a laboratory demonstration level to equate satisfactory experience on aircraft.

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WHEEL ROLL ON RIM CRITERIA FOR AIRCRAFT APPLICATION - ARP1786 - SAE International
Warrendale, PA, United States
WHEEL ROLL ON RIM CRITERIA FOR AIRCRAFT APPLICATION
ARP1786
WHEEL ROLL ON RIM CRITERIA FOR AIRCRAFT APPLICATION ARP1786
This document sets forth minimum roll performance capability for main landing gear wheel to be rolled without tire. The recommended test requirements establish a laboratory demonstration level to equate satisfactory experience on aircraft.

This document sets forth minimum roll performance capability for main landing gear wheel to be rolled without tire. The recommended test requirements establish a laboratory demonstration level to equate satisfactory experience on aircraft.

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Technical Specifications

  SAE International
Product Category Standards and Technical Documents
Product Number ARP1786
Product Name WHEEL ROLL ON RIM CRITERIA FOR AIRCRAFT APPLICATION
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