NSN 5306-01-348-0795
Close Tolerance Hex Head Bolt
Between 2.356 inches and 2.374 inches fastener length, hexagon head style, between 0.251 inches and 0.256 inches head height, width between flats: between 0.741 inches and 0.752 inches .
Manufacturer part number 03A095-8-27 for national stock number 5306013480795.
Datasheet
-
Product description
Close Tolerance Bolt NSN 5306-01-348-0795.
-
MPN or Model
03A095-8-27
-
Schedule B
7508.90.0000 (Other articles of nickel, nesoi (excluding cloth, grill & netting of nickel wire)) -
NMF (National Motor Freight)
093486 - Bolts, Nuts Or Screws, NOI (sub 3) -
Thread Class
3a -
Thread Direction
Right-hand -
Thread Length
Between 0.375 inches and 0.390 inches -
Fastener Length
Between 2.356 inches and 2.374 inches -
Head Style
Hexagon -
Head Height
Between 0.251 inches and 0.256 inches -
Width Between Flats
Between 0.741 inches and 0.752 inches -
Grip Diameter
Between 0.4986 inches and 0.4991 inches -
Shank Unthreaded Hole Diameter
0.106 inches first hole and 0.116 inches first hole -
Thread Diameter
0.500 inches -
Grip Length
Between 1.686 inches and 1.704 inches -
Thready Qty Per Inch (tpi)
20 -
Min. Tensile Strength (psi)
125000 pounds per square inch -
Distance From Head Largest Bearing Surface To Shank Hole Center
2.226 inches first hole and 2.244 inches first hole -
Material
Nickel alloy 718 -
Material Specification
Ams 5662 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
- 5935-01-327-7490 MPN 05A092N31912CElectrical Connector Backshell
- 1560-01-370-6043 MPN DAA3255D205-011Aircraft Structural Component Support
- 1560-01-380-5969 MPN DAA3150A680-082Aircraft Fairing
- 1560-01-424-1668 MPN DAA3420D129-292Aircraft Thermal Insulation
- 1560-01-453-4050 MPN DAA3420A106-110Aircraft Trailing Edge
- 5935-01-492-4411 MPN 05A107T25B19SAElectrical Plug Connector
- 1560-01-384-4499 MPN DAA3420D129-066Aircraft Thermal Insulation
- 1560-01-423-9300 MPN DAA3420D129-284Aircraft Thermal Insulation
An externally threaded fastener whose unthreaded portion is of a specified 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. 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. A locking feature may be incorporated in the design of the head or threads. For items having close tolerance, and fabricated from material having 160,000 pounds per square inch (1100 megapascals) minimum tensile strength, see bolt, shear. For items fabricated from material having less than 160,000 pounds per square inch (1100 megapascals) minimum tensile strength and not having a close tolerance, see bolt, machine.
Pricing and Availability
Get a quote for 5306-01-348-0795 close tolerance boltManufacturer Part Numbers and Alternates
MPN manufacturer part number | Registrant or Supplier |
---|---|
03A095-8-27 | Hi-shear Corporation |
03A095-8-27 | Lisi Aerospace Canada Corp |
03A095-8-27 | Northrop Grumman Systems Corporation |
AS402-8-27 | Avibank Mfg., Inc. |
LB58-8-27 | Hi-shear Corporation |
LB58-8-27 | Lisi Aerospace Canada Corp |