PartsTable TECHNICAL DATA SHEET
JULY 2026Technical Data Sheet

AN24-8Bolt,clevis

Aeronautical Standards Group Dept of Navy and Air Force · NSN 5306-00-156-2692 · FSC 5306 · No Item Name Available
Verified by PartsTable
NSN 5306-00-156-2692 — this item is cataloged by the U.S. Government under National Stock Number 5306-00-156-2692. Primary manufacturer part number: AN24-8.
Features
  • Bolt,clevis — FSC 5306
  • Head Height: 0.125 INCHES NOMINAL IN
  • Thread Quantity Per Inch: 28
  • Hardness Rating: 26.0 ROCKWELL C MINIMUM AND 32.0 ROCKWELL C MAXIMUM OVERALL
  • 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
  • Surface Treatment: CADMIUM AND CHROMATE OVERALL
  • Thread Quantity Per Inch: 28
  • Nominal Thread Diameter: 0.250 INCHES IN
Applications
  • Structural fastening and assembly
  • Equipment mounting
  • Panel and housing attachment
  • Applications requiring Steel Comp 4140 or Steel Comp 8740 or Steel Comp 8630 or Steel Comp 8735 or Steel Comp 4130 or Steel Comp 4037 Overall construction
General Description

The Bolt,clevis, cataloged under National Stock Number 5306-00-156-2692, is classified within Federal Supply Class 5306 (No Item Name Available) of the Hardware and Abrasives group. The primary manufacturer of record is Aeronautical Standards Group Dept of Navy and Air Force. Government technical data includes 30 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 1 commercial cross-reference from 1 manufacturer, enabling identification through both NSN and commercial part number lookups. 1 verified substitute exists in the FLIS interchangeability database. Current acquisition status: Active.

Technical Specifications
ParameterValue
NSN5306-00-156-2692
Primary Part NumberAN24-8
Item NameBolt,clevis
FSC / FSG5306 / 53 — No Item Name Available
ManufacturerAeronautical Standards Group Dept of Navy and Air Force
StatusACTIVE
Head Height0.125 INCHES NOMINAL IN
Thread Quantity Per Inch28
Hardness Rating26.0 ROCKWELL C MINIMUM AND 32.0 ROCKWELL C MAXIMUM OVERALL
Material Document and ClassificationMIL-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
Surface TreatmentCADMIUM AND CHROMATE OVERALL
Thread Quantity Per Inch28
Nominal Thread Diameter0.250 INCHES IN
Single Shear StrengthERR-060
Thread DirectionRIGHT-HAND
Internal Drive StyleSLOT
Minimum Tensile Strength125000 POUNDS PER SQUARE INCH LBS
Thread Length0.323 INCHES MINIMUM AND 0.363 INCHES MAXIMUM IN
Distance From Head Largest Bearing Surface to Shank Hole Center0.359 INCHES MINIMUM AND 0.391 INCHES MAXIMUM FIRST HOLE IN
Thread Series DesignatorUNF
Surface TreatmentCADMIUM AND CHROMATE OVERALL
Surface Treatment Document and ClassificationQQ-P-416 TY 2 CL 3 FED SPEC SINGLE TREATMENT RESPONSE OVERALL
Head StyleBUTTON
MaterialSTEEL COMP 4140 OR STEEL COMP 8740 OR STEEL COMP 8630 OR STEEL COMP 8735 OR STEEL COMP 4130 OR STEEL COMP 4037 OVERALL
Shank Unthreaded Hole Diameter0.076 INCHES MINIMUM AND 0.086 INCHES MAXIMUM FIRST HOLE IN
Thread Class3A A
Head Diameter0.500 INCHES NOMINAL IN
Nominal Thread Diameter0.250 INCHES IN
Thread Series DesignatorUNF
Fastener Length0.521 INCHES MINIMUM AND 0.541 INCHES MAXIMUM IN
Surface Treatment Document and ClassificationQQ-P-416 TY 2 CL 3 FED SPEC SINGLE TREATMENT RESPONSE OVERALL
Minimum Tensile Strength125000 POUNDS PER SQUARE INCH LBS
Material Document and ClassificationMIL-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
Internal Drive StyleSLOT
Groove Diameter0.191 INCHES MINIMUM AND 0.201 INCHES MAXIMUM IN
Hardness Rating26.0 ROCKWELL C MINIMUM AND 32.0 ROCKWELL C MAXIMUM OVERALL
Lifecycle & Compliance
Acquisition StatusACTIVE
HAZMATNo
Verified Substitutes 1
5940-00-754-5440 INTERCHANGEABLE
Terminal,lug
Cross-Reference Index
Part NumberManufacturer
AN24-8 Aeronautical Standards Group Dept of Navy and Air Force (USA)
Related Parts
5940-00-754-5440INTERCHANGEABLE
TERMINAL,LUG

Frequently Asked Questions

What is NSN 5306-00-156-2692?

NSN 5306-00-156-2692 is a Bolt,clevis, manufactured by Aeronautical Standards Group Dept of Navy and Air Force, classified under FSC 5306 (No Item Name Available). Status: active.

What are the part numbers for NSN 5306-00-156-2692?

NSN 5306-00-156-2692 has 1 cross-referenced part number: AN24-8 (Aeronautical Standards Group Dept of Navy and Air Force).

What NSN replaces 5306-00-156-2692?

There is 1 known substitute for 5306-00-156-2692: 5940-00-754-5440. Verify interchangeability with system specifications before substitution.

What are the specifications of AN24-8?

Key specifications for AN24-8: Head Height: 0.125 INCHES NOMINAL IN; Thread Quantity Per Inch: 28; Hardness Rating: 26.0 ROCKWELL C MINIMUM AND 32.0 ROCKWELL C MAXIMUM OVERALL; 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. 30 total characteristics are documented in the Federal Logistics Information System.

Validated with multiple authoritative sources, including Government, OEM, and Certified sources.
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