NSN 5306-00-754-1788
Machine Bolt
Datasheet
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Product description
Machine Bolt NSN 5306-00-754-1788.
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MPN or Model
A2-1342-18
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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.)
1 lb
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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 5306-00-754-1788 machine boltManufacturer Part Numbers and Alternates
| MPN manufacturer part number | Registrant or Supplier |
|---|---|
| A2-1342-18 | Parker Hannifin Corporation |
| 8170157 | U S Army Aviation And Missile |
| MILB6812 | National Aerospace Standards |
| AN74A5 | Aeronautical Standards Group |
| 145-540-96405 | Honeywell International Inc. |
| MS20074-04-05 | National Aerospace Standards |
| A2-1342-18 | Parker-hannifin Corporation |
| MS20074-04-05 | Military Standards |
| MILB6812 | Military Specifications |
| 88 | Triumph Engine Control Systems, Llc |
| A123 | Triumph Engine Control Systems, Llc |
| 173-19 | Hamilton Sundstrand Corporation |
| 145-540-96405 | Honeywell International Inc. |
| A2-1342-18 | Parker Hannifin Corporation |
| 8170157 | U S Army Aviation And Missile |
| AN74A5 | Aeronautical Standards Group |
| MILB6812 | National Aerospace Standards |
| MS20074-04-05 | National Aerospace Standards |
| MILB6812 | Military Specifications |
| A2-1342-18 | Parker-hannifin Corporation |
| 88 | Triumph Engine Control Systems, Llc |
| A123 | Triumph Engine Control Systems, Llc |
| 173-19 | Hamilton Sundstrand Corporation |
| MS20074-04-05 | Military Standards |
| 145-540-96405 | Honeywell International Inc. |
| A2-1342-18 | Parker Hannifin Corporation |
| 8170157 | U S Army Aviation And Missile |
| AN74A5 | Aeronautical Standards Group |
| MILB6812 | National Aerospace Standards |
| MS20074-04-05 | National Aerospace Standards |
| MILB6812 | Military Specifications |
| A2-1342-18 | Parker-hannifin Corporation |
| 88 | Triumph Engine Control Systems, Llc |
| A123 | Triumph Engine Control Systems, Llc |
| 173-19 | Hamilton Sundstrand Corporation |
| MS20074-04-05 | Military Standards |
| 145-540-96405 | Honeywell International Inc. |
| A2-1342-18 | Parker Hannifin Corporation |
| 8170157 | U S Army Aviation And Missile |
| AN74A5 | Aeronautical Standards Group |
| MILB6812 | National Aerospace Standards |
| MS20074-04-05 | National Aerospace Standards |
| MILB6812 | Military Specifications |
| A2-1342-18 | Parker-hannifin Corporation |
| 88 | Triumph Engine Control Systems, Llc |
| A123 | Triumph Engine Control Systems, Llc |
| 173-19 | Hamilton Sundstrand Corporation |
| MS20074-04-05 | Military Standards |
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