The 638811 nut for the KC-46 is crafted from a robust iron alloy with a silver finish, featuring a floating nut design for easy installation. It has a nominal thread size of 0.190 inches, 32 threads/inch, and a hardness of 28.0 Rockwell C, ensuring durability. FAA certified for safety!
The 638811 nut is engineered for the KC-46 aircraft, featuring a robust iron alloy 660 shell with a silver surface treatment. This component incorporates a floating nut design, allowing for flexibility during installation. With a nominal thread size of 0.190 inches and a thread quantity of 32 per inch, it ensures compatibility with several applications. The hardness rating of 28.0 Rockwell C minimum guarantees durability under operational conditions. The mounting hole diameter ranges from 0.098 inches to 0.103 inches, while the counterbore diameter is a minimum of 0.194 inches. This nut is FAA certified, ensuring compliance with aviation standards.
Features & Benefits
Features
Floating nut design for excellent installation flexibility.
Durable iron alloy 660 shell with a silver surface treatment.
FAA certified for use in aviation applications.
Benefits
Ensures reliable performance in demanding environments.
Facilitates easy installation with precise mounting specifications.
Meets stringent aviation standards for safety and reliability.
Technical Information
ATA Number
72,
73,
74,
75,
77,
79,
80
ATA Chapter
Engine Turbine / Turbo Prop Ducted Fan / Unducted Fan
Product information provided "as is", and Boeing may add, change, discontinue or remove product information at any time. Product photos may not be exact match to product delivered. Seeterms & conditions.
