The Bolt,clevis, cataloged under National Stock Number 5306-00-151-0531, 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 20 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 6 commercial cross-references from 5 manufacturers, enabling identification through both NSN and commercial part number lookups. 5 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 5306-00-151-0531 |
| Primary Part Number | AN24-29 |
| Item Name | Bolt,clevis |
| 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 | ACTIVE |
| Nominal Thread Diameter | 0.250 INCHES IN |
| Hardness Rating | 26.0 ROCKWELL C MINIMUM AND 32.0 ROCKWELL C MAXIMUM OVERALL |
| Distance From Head Largest Bearing Surface to Shank Hole Center | 1.672 INCHES MINIMUM AND 1.703 INCHES MAXIMUM FIRST HOLE IN |
| Internal Drive Style | SLOT |
| Minimum Tensile Strength | 125000 POUNDS PER SQUARE INCH LBS |
| Thread Length | 0.636 INCHES MINIMUM AND 0.676 INCHES MAXIMUM IN |
| Thread Series Designator | UNF |
| 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 |
| 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 ALL TREATMENT RESPONSES OVERALL |
| Thread Quantity Per Inch | 28 |
| Thread Direction | RIGHT-HAND |
| Head Diameter | 0.500 INCHES NOMINAL IN |
| Shank Unthreaded Hole Diameter | 0.076 INCHES MINIMUM AND 0.086 INCHES MAXIMUM FIRST HOLE IN |
| Thread Class | 3A A |
| Head Height | 0.125 INCHES NOMINAL IN |
| Surface Treatment | CADMIUM AND CHROMATE OVERALL |
| Head Style | BUTTON |
| Groove Diameter | 0.191 INCHES MINIMUM AND 0.201 INCHES MAXIMUM IN |
| Fastener Length | 1.490 INCHES MINIMUM AND 1.510 INCHES MAXIMUM IN |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| 278-22 | Ontic Engineering & Manufacturing, Inc Dba Ontic Us (USA) |
| AN24-29 | Aeronautical Standards Group Dept of Navy and Air Force (USA) |
| AN24-29 PRIMARY | National Aerospace Standards Committee Aerospace Industries Association of America Inc Not for Rfq or Solicitation Use (USA) |
| 278-22 | Donallco Inc (USA) |
| 5306PL1494441 | Jednolity Indeks Materialowy - Uniform Material Index (POL) |
| NASM21 THRU NASM37 | National Aerospace Standards Committee Aerospace Industries Association of America Inc Not for Rfq or Solicitation Use (USA) |
NSN 5306-00-151-0531 is a Bolt,clevis, 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: active.
NSN 5306-00-151-0531 has 6 cross-referenced part numbers: 278-22 (Ontic Engineering & Manufacturing, Inc Dba Ontic Us), AN24-29 (Aeronautical Standards Group Dept of Navy and Air Force), AN24-29 (National Aerospace Standards Committee Aerospace Industries Association of America Inc Not for Rfq or Solicitation Use), 278-22 (Donallco Inc), 5306PL1494441 (Jednolity Indeks Materialowy - Uniform Material Index) and 1 more.
There are 5 known substitutes for 5306-00-151-0531: 5306-00-156-2292, 5306-00-206-1332, 5120-00-293-1796 and 2 more. Verify interchangeability with system specifications before substitution.
Key specifications for AN24-29: Nominal Thread Diameter: 0.250 INCHES IN; Hardness Rating: 26.0 ROCKWELL C MINIMUM AND 32.0 ROCKWELL C MAXIMUM OVERALL; Distance From Head Largest Bearing Surface to Shank Hole Center: 1.672 INCHES MINIMUM AND 1.703 INCHES MAXIMUM FIRST HOLE IN; Internal Drive Style: SLOT. 20 total characteristics are documented in the Federal Logistics Information System.