The Bolt,machine, cataloged under National Stock Number 5306-00-754-1788, is classified within Federal Supply Class 5306 (No Item Name Available) of the Hardware and Abrasives group. The primary manufacturer of record is National Aerospace Standards Committee Aerospace Industries Association of America Inc Not for Rfq or Solicitation Use. Government technical data includes 22 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 12 commercial cross-references from 10 manufacturers, enabling identification through both NSN and commercial part number lookups. 12 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Cancelled.
| Parameter | Value |
|---|---|
| NSN | 5306-00-754-1788 |
| Primary Part Number | MS20074-04-05 |
| Item Name | Bolt,machine |
| FSC / FSG | 5306 / 53 — No Item Name Available |
| Manufacturer | National Aerospace Standards Committee Aerospace Industries Association of America Inc Not for Rfq or Solicitation Use |
| Status | CANCELLED |
| Hole Type | DRILLED |
| Hole Quantity | 6 |
| Thread Direction | RIGHT-HAND |
| Head Height | 0.203 INCHES MINIMUM AND 0.234 INCHES MAXIMUM IN |
| Thread Series Designator | UNIFIED NATIONAL COARSE (UNC) |
| Hole Diameter | 0.070 INCHES NOMINAL IN |
| Grip Length | 0.109 INCHES MINIMUM AND 0.141 INCHES MAXIMUM IN |
| Minimum Tensile Strength | 125000 POUNDS PER SQUARE INCH LBS |
| Features Provided | FINISHED HEAD |
| Width Between Flats | 0.430 INCHES MINIMUM AND 0.439 INCHES MAXIMUM IN |
| Material Document and Classification | MIL-S-5626 MIL SPEC 1ST MATERIAL RESPONSE OR MIL-S-6049 MIL SPEC 2ND MATERIAL RESPONSE OR MIL-S-6050 MIL SPEC 3RD MATERIAL RESPONSE OR MIL-S-6098 MIL SPEC 4TH MATERIAL RESPONSE OR MIL-S-6758 MIL SPEC 5TH MATERIAL RESPONSE OR AMS 6300 ASSN STD 6TH MATERIAL RESPONSE OVERALL |
| Thread Quantity Per Inch | 20 |
| Surface Treatment | CADMIUM OVERALL |
| Hardness Rating | 26.0 ROCKWELL C MINIMUM AND 32.0 ROCKWELL C MAXIMUM OVERALL |
| Hole Configuration Style | HEXAGON LONGITUDINAL HOLE |
| Head Style | HEXAGON |
| Material | STEEL COMP 4140 OR STEEL COMP 8740 OR STEEL COMP 8630 OR STEEL COMP 8735 OR STEEL COMP 4130 OR STEEL COMP 4037 OVERALL |
| Surface Treatment Document and Classification | QQ-P-416,TY 2 CL 3 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
| Thread Length | 0.499 INCHES MINIMUM AND 0.578 INCHES MAXIMUM IN |
| Fastener Length | 0.640 INCHES MINIMUM AND 0.687 INCHES MAXIMUM IN |
| Nominal Thread Diameter | 0.250 INCHES IN |
| Thread Class | 3A A |
| Acquisition Status | CANCELLED |
| Successor | 5306-00-063-3268 |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| A123 | Triumph Engine Control Systems Llc (USA) |
| 173-19 | Hamilton Sundstrand Corporation (USA) |
| A2-1342-18 | Parker Hannifin Corporation Div Aerospace Group Headquarters (USA) |
| A2-1342-18 | Parker-Hannifin Corporation Dba Pneutronics Div Corporate Headquarters (USA) |
| 8170157 | Us Army Aviation and Missile Command (USA) |
| MS20074-04-05 | Military Standards Promulgated by Military Departments Under Authority of Defense Standardization Manual 4120 3-M |
| MS20074-04-05 PRIMARY | National Aerospace Standards Committee Aerospace Industries Association of America Inc Not for Rfq or Solicitation Use (USA) |
| 145-540-96405 | Honeywell International Inc. Dba Honeywell International Div Aerospace - Phoenix (USA) |
| MILB6812 | Military Specifications Promulgated by Military Departments/agencies Under Authority of Defense Standardization Manual 4120 3-M |
| MILB6812 | National Aerospace Standards Committee Aerospace Industries Association of America Inc Not for Rfq or Solicitation Use (USA) |
| 88 | Triumph Engine Control Systems Llc (USA) |
| AN74A5 | Aeronautical Standards Group Dept of Navy and Air Force (USA) |
NSN 5306-00-754-1788 is a Bolt,machine, manufactured by National Aerospace Standards Committee Aerospace Industries Association of America Inc Not for Rfq or Solicitation Use, classified under FSC 5306 (No Item Name Available). Status: cancelled.
NSN 5306-00-754-1788 has 12 cross-referenced part numbers: A123 (Triumph Engine Control Systems Llc), 173-19 (Hamilton Sundstrand Corporation), A2-1342-18 (Parker Hannifin Corporation Div Aerospace Group Headquarters), A2-1342-18 (Parker-Hannifin Corporation Dba Pneutronics Div Corporate Headquarters), 8170157 (Us Army Aviation and Missile Command) and 7 more.
There are 12 known substitutes for 5306-00-754-1788: 5306-00-063-3268, 5306-00-144-3646, 5306-00-144-4058 and 9 more. Verify interchangeability with system specifications before substitution.
Key specifications for MS20074-04-05: Hole Type: DRILLED; Hole Quantity: 6; Thread Direction: RIGHT-HAND; Head Height: 0.203 INCHES MINIMUM AND 0.234 INCHES MAXIMUM IN. 22 total characteristics are documented in the Federal Logistics Information System.
NSN 5306-00-754-1788 is currently cancelled. Check with the Defense Logistics Agency for current availability and authorized substitutes.