NSN 5306-01-167-6319
Close Tolerance Hex Head Bolt
1.585 inches fastener length, double hexagon head style, 0.164 inches head height, width between flats: between 0.430 inches and 0.439 inches .
Manufacturer part number LD111-0026-0419 for national stock number 5306011676319.
Datasheet
-
Product description
Close Tolerance Bolt NSN 5306-01-167-6319.
-
MPN or Model
LD111-0026-0419
-
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
0.397 inches -
Fastener Length
1.585 inches -
Head Style
Double hexagon -
Head Height
0.164 inches -
Width Between Flats
Between 0.430 inches and 0.439 inches -
Grip Diameter
Between 0.2490 inches and 0.2495 inches -
Thread Diameter
0.250 inches -
Grip Length
1.188 inches -
Thready Qty Per Inch (tpi)
28 -
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
- 1560-00-784-8247 MPN 265-318204-11Aircraft Window Panel
- 1560-00-863-4474 MPN 265-318354Handle Support
- 1560-01-137-7602 MPN 202-17070Aircraft Structural Component Support
- 1560-01-154-3357 MPN 16589-130004-10Aircraft Structural Component Support
- 1680-01-162-7190 MPN L5234058-011Outed Assemb Sector
- 5930-01-175-2610 MPN L431C2015CFlow Switch
- 4920-01-180-2944 MPN 45A78000-001Aircraft Hydraulic System Components Fixture
- 1680-01-182-9322 MPN L5303305-081Aircraft Seat Frame
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 5306-01-167-6319 close tolerance boltManufacturer Part Numbers and Alternates
MPN manufacturer part number | Registrant or Supplier |
---|---|
LD111-0026-0419 | Boeing Company, The |