NSN 5306-01-232-5093
Coaxial Connector
Between 0.968 inches and 0.998 inches fastener length, double hexagon w/hole head style, 0.355 inches head height, width between flats: between 0.492 inches and 0.502 inches .
Manufacturer part number LD111-0020-0704 for national stock number 5306012325093.
Datasheet
-
Product description
Shear Bolt NSN 5306-01-232-5093.
-
MPN or Model
LD111-0020-0704
-
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) -
Unit Weight (Est.)
0.1 lb -
Thread Class
3a -
Thread Direction
Right-hand -
Thread Length
Between 0.718 inches and 0.748 inches -
Fastener Length
Between 0.968 inches and 0.998 inches -
Head Style
Double hexagon w/hole -
Head Height
0.355 inches -
Width Between Flats
Between 0.492 inches and 0.502 inches -
Extended Washer Diameter
Between 0.740 inches and 0.750 inches -
Extended Washer Thickness
0.099 inches -
Hole Diameter
Between 0.050 inches and 0.060 inches -
Grip Diameter
Between 0.4365 inches and 0.4370 inches -
Thread Diameter
0.438 inches -
Grip Length
0.250 inches -
Hole Quantity
4 -
Hole Type
Drilled -
Thready Qty Per Inch (tpi)
20 -
Min. Tensile Strength (psi)
220000 pounds per square inch -
Hole Configuration Style
Double hexagon longitudinal hole -
Material
Steel comp xm-13 -
Material Specification
Ams5629 assn standard single material response -
Surface Treatment
Passivate -
Surface Treatment Specification
Qq-p-35 federal specification single treatment response -
Thread Series Designator
Unjf
More from these suppliers
- 1560-00-120-8870 MPN 88-43804Engine Control Rod
- 1560-00-150-7750 MPN 55-52515-2Elev Wheel Assembly
- 1560-00-185-2135 MPN 36-31834Cockpit Enclo Glass
- 1560-00-340-6556 MPN 192-522181Horizontal Sta Stop
- 1560-00-401-2629 MPN 276-530017-5Center Pedesta Trim
- 1560-00-506-6256 MPN 159-311149Aircraft Structural Component Support
- 1560-01-134-6372 MPN 265-321323-012Aircraft Structural Component Support
- 1560-01-173-8641 MPN L1700008-016Aircraft Structural Component Bracket
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 5306-01-232-5093 shear boltManufacturer Part Numbers and Alternates
MPN manufacturer part number | Registrant or Supplier |
---|---|
LD111-0020-0704 | Boeing Company, The |