The Bolt,machine, cataloged under National Stock Number 5306-00-182-2016, 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 16 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 12 commercial cross-references from 11 manufacturers, enabling identification through both NSN and commercial part number lookups. 2 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Cancelled.
| Parameter | Value |
|---|---|
| NSN | 5306-00-182-2016 |
| Primary Part Number | AN4H5A |
| 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 |
| Head Height | 0.140 INCHES MINIMUM AND 0.172 INCHES MAXIMUM IN |
| Minimum Tensile Strength | 125000 POUNDS PER SQUARE INCH LBS |
| Thread Direction | RIGHT-HAND |
| Fastener Length | 0.656 INCHES NOMINAL IN |
| Features Provided | FINISHED HEAD |
| Thread Series Designator | UNF |
| Thread Length | 0.468 INCHES MINIMUM IN |
| Width Between Flats | 0.428 INCHES MINIMUM AND 0.440 INCHES MAXIMUM IN |
| Thread Quantity Per Inch | 28 |
| Material | STEEL COMP 4037 OR STEEL COMP 4130 OR STEEL COMP 8630 OR STEEL COMP 8735 OR STEEL COMP 8740 OR STEEL COMP 4140 OVERALL |
| Thread Class | 3A A |
| Hardness Rating | 26.0 ROCKWELL C MINIMUM AND 32.0 ROCKWELL C MAXIMUM OVERALL |
| Material Document and Classification | MIL-B-6812 MIL SPEC ALL MATERIAL RESPONSES OVERALL |
| Nominal Thread Diameter | 0.250 INCHES IN |
| Head Style | HEXAGON |
| Grip Length | 0.188 INCHES NOMINAL IN |
| Acquisition Status | CANCELLED |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| 5305PL0138837 | Jednolity Indeks Materialowy - Uniform Material Index (POL) |
| 116096 | Bendix Corp the (USA) |
| AN4H5A | Aeronautical Standards Group Dept of Navy and Air Force (USA) |
| 116096 | Honeywell International Inc Div Aerospace-South Bend (bendix Dr) (USA) |
| 080A50600 | Thales Nederland, Huizen (NLD) |
| AN4H5A PRIMARY | National Aerospace Standards Committee Aerospace Industries Association of America Inc Not for Rfq or Solicitation Use (USA) |
| NASM3 THRU NASM20-AN4H5A | National Aerospace Standards Committee Aerospace Industries Association of America Inc Not for Rfq or Solicitation Use (USA) |
| 080A50600 | Thales Optronics B.v. (NLD) |
| Z00.N5108301105 | Daher Aerospace - Ex Socata (FRA) |
| 116096 | Bendix Corp the Brake and Steering Div (USA) |
| 932.19.21.151 | Pilatus Aircraft Ltd (CHE) |
| AN4H5A | Leonardo Spa Helicopters Division - Production Site (ITA) |
NSN 5306-00-182-2016 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 5306-00-182-2016 has 12 cross-referenced part numbers: 5305PL0138837 (Jednolity Indeks Materialowy - Uniform Material Index), 116096 (Bendix Corp the), AN4H5A (Aeronautical Standards Group Dept of Navy and Air Force), 116096 (Honeywell International Inc Div Aerospace-South Bend (bendix Dr)), 080A50600 (Thales Nederland, Huizen) and 7 more.
There are 2 known substitutes for 5306-00-182-2016: 5306-00-568-4455, 2540-01-699-6838. Verify interchangeability with system specifications before substitution.
Key specifications for AN4H5A: Head Height: 0.140 INCHES MINIMUM AND 0.172 INCHES MAXIMUM IN; Minimum Tensile Strength: 125000 POUNDS PER SQUARE INCH LBS; Thread Direction: RIGHT-HAND; Fastener Length: 0.656 INCHES NOMINAL IN. 16 total characteristics are documented in the Federal Logistics Information System.
NSN 5306-00-182-2016 is currently cancelled. Check with the Defense Logistics Agency for current availability and authorized substitutes.