PartsTable TECHNICAL DATA SHEET
JULY 2026Technical Data Sheet

AN16-31ABolt,machine

Aeronautical Standards Group Dept of Navy and Air Force · NSN 5306-00-274-1527 · FSC 5306 · No Item Name Available
Verified by PartsTable
NSN 5306-00-274-1527 — this item is cataloged by the U.S. Government under National Stock Number 5306-00-274-1527. Primary manufacturer part number: AN16-31A.
Features
  • Bolt,machine — FSC 5306
  • Minimum Tensile Strength: 125000 POUNDS PER SQUARE INCH LBS
  • Grip Length: 2.000 INCHES NOMINAL IN
  • Fastener Length: 3.375 INCHES NOMINAL IN
  • Thread Quantity Per Inch: 14
  • Thread Length: 1.375 INCHES MAXIMUM IN
  • Thread Class: 3A A
  • Features Provided: FINISHED HEAD
Applications
  • Structural fastening and assembly
  • Equipment mounting
  • Panel and housing attachment
  • Applications requiring Steel Comp 4037 or Steel Comp 4130 or Steel Comp 8630 or Steel Comp 8735 or Steel Comp 8740 or Steel Comp 4140 Overall construction
General Description

The Bolt,machine, cataloged under National Stock Number 5306-00-274-1527, 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 18 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 2 commercial cross-references from 2 manufacturers, 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
NSN5306-00-274-1527
Primary Part NumberAN16-31A
Item NameBolt,machine
FSC / FSG5306 / 53 — No Item Name Available
ManufacturerAeronautical Standards Group Dept of Navy and Air Force
StatusACTIVE
Minimum Tensile Strength125000 POUNDS PER SQUARE INCH LBS
Grip Length2.000 INCHES NOMINAL IN
Fastener Length3.375 INCHES NOMINAL IN
Thread Quantity Per Inch14
Thread Length1.375 INCHES MAXIMUM IN
Thread Class3A A
Features ProvidedFINISHED HEAD
Head StyleHEXAGON
Head Height0.515 INCHES MINIMUM AND 0.547 INCHES MAXIMUM IN
Width Between Flats1.428 INCHES MINIMUM AND 1.441 INCHES MAXIMUM IN
Thread Series DesignatorUNS
Nominal Thread Diameter1.000 INCHES IN
Hardness Rating26.0 ROCKWELL C MINIMUM AND 32.0 ROCKWELL C MAXIMUM OVERALL
Surface TreatmentCADMIUM OVERALL
Thread DirectionRIGHT-HAND
MaterialSTEEL COMP 4037 OR STEEL COMP 4130 OR STEEL COMP 8630 OR STEEL COMP 8735 OR STEEL COMP 8740 OR STEEL COMP 4140 OVERALL
Material Document and ClassificationMIL-B-6812 MIL SPEC ALL MATERIAL RESPONSES OVERALL
Surface Treatment Document and ClassificationQQ-P-416,TY 1,CL 3 FED SPEC SINGLE TREATMENT RESPONSE OVERALL
Lifecycle & Compliance
Acquisition StatusACTIVE
HAZMATNo
Verified Substitutes 1
5310-00-167-1726 INTERCHANGEABLE
Washer,flat
Cross-Reference Index
Part NumberManufacturer
AN16-31A Aeronautical Standards Group Dept of Navy and Air Force (USA)
907379 Scandinavian Manufacturing Scama Ab (SWE)
Related Parts
5310-00-167-1726INTERCHANGEABLE
WASHER,FLAT

Frequently Asked Questions

What is NSN 5306-00-274-1527?

NSN 5306-00-274-1527 is a Bolt,machine, 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 5306-00-274-1527?

NSN 5306-00-274-1527 has 2 cross-referenced part numbers: AN16-31A (Aeronautical Standards Group Dept of Navy and Air Force), 907379 (Scandinavian Manufacturing Scama Ab).

What NSN replaces 5306-00-274-1527?

There is 1 known substitute for 5306-00-274-1527: 5310-00-167-1726. Verify interchangeability with system specifications before substitution.

What are the specifications of AN16-31A?

Key specifications for AN16-31A: Minimum Tensile Strength: 125000 POUNDS PER SQUARE INCH LBS; Grip Length: 2.000 INCHES NOMINAL IN; Fastener Length: 3.375 INCHES NOMINAL IN; Thread Quantity Per Inch: 14. 18 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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