NSN 5306-00-754-1785
Wheel Bolt
Between 1.265 inches and 1.312 inches fastener length, hexagon head style, between 0.203 inches and 0.234 inches head height, width between flats: between 0.430 inches and 0.439 inches .
Manufacturer part number MS20074-04-12 for national stock number 5306007541785.
Datasheet
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Product description
Machine Bolt NSN 5306-00-754-1785.
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MPN or Model
MS20074-04-12
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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 0.499 inches and 0.578 inches -
Fastener Length
Between 1.265 inches and 1.312 inches -
Head Style
Hexagon -
Head Height
Between 0.203 inches and 0.234 inches -
Width Between Flats
Between 0.430 inches and 0.439 inches -
Hole Diameter
0.070 inches -
Thread Diameter
0.250 inches -
Grip Length
Between 0.734 inches and 0.766 inches -
Hole Quantity
6 -
Hole Type
Drilled -
Features Provided
Finished head -
Thready Qty Per Inch (tpi)
20 -
Min. Tensile Strength (psi)
125000 pounds per square inch -
Hardness Rating
26.0 rockwell c and 32.0 rockwell c -
Minimum Yield Strength
2577 pounds per square inch -
Hole Configuration Style
Hexagon longitudinal hole -
Material
Steel comp 8740 or steel comp 8630 or steel comp 8735 or steel comp 4037 or steel comp 4130 or steel comp 4140 -
Material Specification
Mil-s-6049 military specification 1st material response or mil-s-6050 military specification 2nd material response or mil-s-6098 military specification 3rd material response or ams 6300 assn standard 4th material response or mil-s-6758 military specification 5th material response or mil-s-5626 military specification 6th material response -
Surface Treatment
Cadmium -
Surface Treatment Specification
Qq-p-416, type 2 cl 3 federal specification single treatment response -
Thread Series Designator
Unc
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An externally threaded fastener designed for insertion through holes in assembled parts and normally intended to be tightened or released by torquing a nut. the threaded and unthreaded portions are both of one nominal diameter of 0.190 inch (5 mm) or larger. The head is not designed to be held or driven with an inserted driver or by the thumb and fingers. a locking feature may be incorporated in the design of the head or threads. head dimensions and sizes of threaded and unthreaded portions shall conform to internationally recognized fastener standards. for items having a grip length portion machined to a tolerance of 0.0015 inch (0.038 mm) or less, bolt, shear. See also screw, cap, hexagon head and screw, machine.
Pricing and Availability
Get a quote for 5306-00-754-1785 machine boltManufacturer Part Numbers and Alternates
MPN manufacturer part number | Registrant or Supplier |
---|---|
MS20074-04-12 | Military Standards |
92596-12 | Carleton Life Support Systems Inc. |
MILB6812 | National Aerospace Standards |
187807 | Honeywell International Inc. |
AN74A12 | Aeronautical Standards Group |
MILB6812 | Military Specifications |
92596-12 | Honeywell Intl Inc Defense Avionics |
A459 | Triumph Engine Control Systems, Llc |
MS20074-04-12 | Military Standards |
92596-12 | Carleton Life Support Systems Inc. |
MILB6812 | National Aerospace Standards |
187807 | Honeywell International Inc. |
AN74A12 | Aeronautical Standards Group |
A459 | Triumph Engine Control Systems, Llc |
MILB6812 | Military Specifications |
92596-12 | Honeywell Intl Inc Defense Avionics |
MS20074-04-12 | Military Standards |
92596-12 | Carleton Life Support Systems Inc. |
MILB6812 | National Aerospace Standards |
187807 | Honeywell International Inc. |
AN74A12 | Aeronautical Standards Group |
A459 | Triumph Engine Control Systems, Llc |
MILB6812 | Military Specifications |
92596-12 | Honeywell Intl Inc Defense Avionics |
MS20074-04-12 | Military Standards |
92596-12 | Carleton Life Support Systems Inc. |
MILB6812 | National Aerospace Standards |
187807 | Honeywell International Inc. |
AN74A12 | Aeronautical Standards Group |
A459 | Triumph Engine Control Systems, Llc |
MILB6812 | Military Specifications |
92596-12 | Honeywell Intl Inc Defense Avionics |
MS20074-04-12 | Military Standards |
92596-12 | Carleton Life Support Systems Inc. |
MILB6812 | National Aerospace Standards |
187807 | Honeywell International Inc. |
AN74A12 | Aeronautical Standards Group |
A459 | Triumph Engine Control Systems, Llc |
MILB6812 | Military Specifications |
92596-12 | Honeywell Intl Inc Defense Avionics |
92596-12 | Honeywell Intl Inc Defense Avionics |
MILB6812 | Military Specifications |
A459 | Triumph Engine Control Systems, Llc |
AN74A12 | Aeronautical Standards Group |
187807 | Honeywell International Inc. |
MILB6812 | National Aerospace Standards |
92596-12 | Carleton Life Support Systems Inc. |
MS20074-04-12 | Military Standards |
MS20074-04-12 | Military Standards |
92596-12 | Carleton Life Support Systems Inc. |
MILB6812 | National Aerospace Standards |
187807 | Honeywell International Inc. |
AN74A12 | Aeronautical Standards Group |
A459 | Triumph Engine Control Systems, Llc |
MILB6812 | Military Specifications |
92596-12 | Honeywell Intl Inc Defense Avionics |
MS20074-04-12 | Military Standards |
92596-12 | Carleton Life Support Systems Inc. |
MILB6812 | National Aerospace Standards |
187807 | Honeywell International Inc. |
AN74A12 | Aeronautical Standards Group |
A459 | Triumph Engine Control Systems, Llc |
MILB6812 | Military Specifications |
92596-12 | Honeywell Intl Inc Defense Avionics |
MS20074-04-12 | Military Standards |
92596-12 | Carleton Life Support Systems Inc. |
MILB6812 | National Aerospace Standards |
187807 | Honeywell International Inc. |
AN74A12 | Aeronautical Standards Group |
A459 | Triumph Engine Control Systems, Llc |
MILB6812 | Military Specifications |
92596-12 | Honeywell Intl Inc Defense Avionics |