NSN 5306-01-649-1101
Shear Bolt
Datasheet
-
Product description
Shear Bolt NSN 5306-01-649-1101.
-
MPN or Model
A111-8E
More from these suppliers
- 1560-00-034-5960 MPN 50-810142-10Main Land Universal Arm Assembly
- 1680-01-014-2081 MPN 50-534527-3Arm Rest Cap
- 1560-01-421-0705 MPN 33-630000-17Aircraft Spar
- 1560-01-482-5860 MPN 133-510054-1Aircraft Latch Assembly
- 1680-01-526-2644 MPN ESD4CAircraft Static Discharger
- 1560-01-649-0903 MPN HZ010H8000-062Aircraft Cover Rod Assembly
A high strength, 160,000 pounds per square inch (1100 megapascals) minimum tensile strength externally threaded fastener designed for use in applications involving great shear stress. The head is designed to accommodate an external wrench or driver. The head is not designed to be held or driven with an inserted driver, nor is it designed for rotation by the thumb and fingers. The unthreaded portion is of specific grip length, plated or unplated, and is machined to a tolerance of one thousandth (0.001) of an inch (0.025 mm) or less of a specific diameter for items one inch (25 mm) or less in diameter. Items over one inch (25 mm) in diameter shall have a tolerance of fifteen ten thousandths (0.0015) of an inch (0.038 mm) or less. The nominal major diameter of the threads shall be at least one thousandth (0.001) of an inch (0.025 mm) below the minimum shank diameter, but not below the minimum major diameter for applicable class of fit, as shown in the screw thread standards, fed std h28 and/or other nationally recognized standards. A locking feature may be incorporated in the design of the head or threads. See bolt, machine and bolt, clevis.
Pricing and Availability
Get a quote for 5306-01-649-1101 shear boltManufacturer Part Numbers and Alternates
| MPN manufacturer part number | Registrant or Supplier |
|---|---|
| A111-8E | Beechcraft Corporation |
Stock Check
