NSN 5306-01-180-9103
Coaxial Connector
Between 0.750 inches and 0.780 inches fastener length, double hexagon w/hole head style, 0.196 inches head height, width between flats: between 0.243 inches and 0.251 inches .
Manufacturer part number LD111-0021-0306 for national stock number 5306011809103.
Datasheet
-
Product description
Shear Bolt NSN 5306-01-180-9103.
-
MPN or Model
LD111-0021-0306
-
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 0.365 inches and 0.415 inches -
Fastener Length
Between 0.750 inches and 0.780 inches -
Head Style
Double hexagon w/hole -
Head Height
0.196 inches -
Width Between Flats
Between 0.243 inches and 0.251 inches -
Extended Washer Diameter
Between 0.340 inches and 0.350 inches -
Extended Washer Thickness
0.064 inches -
Grip Diameter
Between 0.1890 inches and 0.1895 inches -
Thread Diameter
0.190 inches -
Grip Length
Between 0.365 inches and 0.385 inches -
Thready Qty Per Inch (tpi)
32 -
Min. Tensile Strength (psi)
220000 pounds per square inch -
Hardness Rating
46.0 rockwell c and 50.0 rockwell c -
Material
Steel comp xm-13 -
Material Specification
Ams 5629 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
- 1560-00-211-0011 MPN 151-31907-5Aircraft Structural Component Support
- 1560-00-572-2709 MPN 187-51098-10Pitot Tube Boom Assembly
- 1560-01-159-0219 MPN 16589-130004-8Fitting
- 4920-01-160-6420 MPN 23A25000Test Program Set
- 1560-01-164-2174 MPN L5341009-001Aircraft Structural Component Support
- 1560-01-175-6169 MPN L1700018-007Aircraft Structural Component Bracket
- 4920-01-179-9586 MPN R-TBD-844Fanshaft Loading Fixture
- 1560-01-189-2617 MPN L1203370-001Aircraft Structural Plate
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 5306-01-180-9103 shear boltManufacturer Part Numbers and Alternates
MPN manufacturer part number | Registrant or Supplier |
---|---|
LD111-0021-0306 | Boeing Company, The |