NSN 5306-01-546-2288
Coaxial Connector
4.696 inches fastener length, dished hexagon head style, between 0.438 inches and 0.453 inches head height, width between flats: between 1.239 inches and 1.252 inches .
Manufacturer part number NAS6214-63 for national stock number 5306015462288.
Datasheet
-
Product description
Shear Bolt NSN 5306-01-546-2288.
-
MPN or Model
NAS6214-63
-
Schedule B
7318.15.2000 (Bolts and bolts and their nuts or washers exported in the same shipment) -
NMF (National Motor Freight)
093486 - Bolts, Nuts Or Screws, NOI (sub 3) -
Thread Class
3a -
Thread Direction
Right-hand -
Thread Length
Between 0.734 inches and 0.784 inches -
Fastener Length
4.696 inches -
Head Style
Dished hexagon -
Head Height
Between 0.438 inches and 0.453 inches -
Width Between Flats
Between 1.239 inches and 1.252 inches -
Grip Diameter
Between 0.8730 inches and 0.8740 inches -
Thread Diameter
0.875 inches -
Grip Length
0.938 inches -
Thready Qty Per Inch (tpi)
14 -
Min. Tensile Strength (psi)
160000 pounds per square inch -
Hardness Rating
36.0 rockwell c and 40.0 rockwell c -
Surface Finish
32.0 microinches threads -
Material
Steel comp e4340 or steel comp 8740 -
Material Specification
Mil-s-5000 military specification 1st material response or mil-s-6049 military specification 2nd material response or ams 6322 assn standard 2nd material response -
Surface Treatment
Cadmium and chromate -
Surface Treatment Specification
Qq-p-416, type2, class 2 federal specification single treatment response -
Thread Series Designator
Unjf -
Specification Data
80205-nas6214 professional/industrial association standard
More from these suppliers
- 1560-00-340-9204 MPN 5-84471-3Aircraft Door
- 1680-00-345-2294 MPN 30-2221Trim Tab M Retainer
- 4820-00-577-4362 MPN 10-60528-1Safety Relief Valve
- 1560-00-630-4217 MPN 69-2217-2Shield Support Bracket
- 1680-00-645-6975 MPN 5-85679-1Aircraft Gearbox Assembly
- 1560-00-651-3630 MPN 35-5943-4Nose Radome Plunger
- 1560-00-652-7521 MPN 9-67557-9Aircraft Structural Plate
- 1560-00-733-4138 MPN 24-1101-505Aircraft Door
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 5306-01-546-2288 shear boltManufacturer Part Numbers and Alternates
MPN manufacturer part number | Registrant or Supplier |
---|---|
NAS6214-63 | The Boeing Company |