PartsTable TECHNICAL DATA SHEET
JULY 2026Technical Data Sheet

AN177-20Bolt,close Tolerance

Aeronautical Standards Group Dept of Navy and Air Force · NSN 5306-00-167-3925 · FSC 5306 · No Item Name Available
Verified by PartsTable
NSN 5306-00-167-3925 — this item is cataloged by the U.S. Government under National Stock Number 5306-00-167-3925. Primary manufacturer part number: AN177-20.
Features
  • Bolt,close Tolerance — FSC 5306
  • Shank Unthreaded Hole Diameter: 0.106 INCHES MINIMUM FIRST HOLE IN
  • Fastener Length: 2.078 INCHES MINIMUM AND 2.125 INCHES MAXIMUM IN
  • Hole Diameter: 0.070 INCHES NOMINAL IN
  • Head Height: 0.234 INCHES MINIMUM AND 0.266 INCHES MAXIMUM IN
  • Thread Quantity Per Inch: 20
  • Thread Direction: RIGHT-HAND
  • Hole Type: DRILLED
Applications
  • Structural fastening and assembly
  • Equipment mounting
  • Panel and housing attachment
  • Applications requiring Steel Comp 4130 or Steel Comp 8740 or Steel Comp 8640 or Steel Comp 8735 or Steel Comp 4037 or Steel Comp 4140 Overall construction
General Description

The Bolt,close Tolerance, cataloged under National Stock Number 5306-00-167-3925, 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 24 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 3 commercial cross-references from 2 manufacturers, enabling identification through both NSN and commercial part number lookups. 12 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Cancelled.

Technical Specifications
ParameterValue
NSN5306-00-167-3925
Primary Part NumberAN177-20
Item NameBolt,close Tolerance
FSC / FSG5306 / 53 — No Item Name Available
ManufacturerAeronautical Standards Group Dept of Navy and Air Force
StatusCANCELLED
Shank Unthreaded Hole Diameter0.106 INCHES MINIMUM FIRST HOLE IN
Fastener Length2.078 INCHES MINIMUM AND 2.125 INCHES MAXIMUM IN
Hole Diameter0.070 INCHES NOMINAL IN
Head Height0.234 INCHES MINIMUM AND 0.266 INCHES MAXIMUM IN
Thread Quantity Per Inch20
Thread DirectionRIGHT-HAND
Hole TypeDRILLED
Thread Series DesignatorUNF
Nominal Thread Diameter0.437 INCHES IN
Head StyleHEXAGON
Minimum Tensile Strength125000 POUNDS PER SQUARE INCH LBS
Head Length0.615 INCHES MINIMUM AND 0.627 INCHES MAXIMUM IN
Thread Class3A A
Hardness Rating26.0 ROCKWELL C MINIMUM AND 32.0 ROCKWELL C MAXIMUM OVERALL
Grip Diameter0.4362 INCHES MINIMUM AND 0.4367 INCHES MAXIMUM IN
Thread Length0.624 INCHES MINIMUM AND 0.703 INCHES MAXIMUM IN
Hole Configuration StyleHEXAGON FLATS
Surface TreatmentCADMIUM AND CHROMATE OVERALL
Grip Length1.422 INCHES MINIMUM AND 1.454 INCHES MAXIMUM IN
Shank Unthreaded Hole Diameter0.116 INCHES MAXIMUM SECOND HOLE IN
Distance From Head Largest Bearing Surface to Shank Hole Center1.906 INCHES MINIMUM AND 1.938 INCHES MAXIMUM FIRST HOLE IN
Hole Quantity1
MaterialSTEEL COMP 4130 OR STEEL COMP 8740 OR STEEL COMP 8640 OR STEEL COMP 8735 OR STEEL COMP 4037 OR STEEL COMP 4140 OVERALL
Width Between Flats0.615 INCHES MINIMUM AND 0.627 INCHES MAXIMUM IN
Lifecycle & Compliance
Acquisition StatusCANCELLED
Successor5306-00-051-2338
HAZMATNo
Verified Substitutes 12
No Item Name Available
Bolt,machine
Bolt,machine
5306-00-051-2344NASM20074-05-40 SUCCESSOR
Bolt,machine
National Aerospace Standards Committee Aerospace Industries Association of America Inc Not for Rfq or Solicitation Use
Bolt,machine
Bolt,close Tolerance
Bolt,machine
Bolt,machine
5306-00-144-3686AN3-55 SUCCESSOR
Bolt,machine
National Aerospace Standards Committee Aerospace Industries Association of America Inc Not for Rfq or Solicitation Use
Bolt,machine
Cross-Reference Index
Part NumberManufacturer
AN177-20 Aeronautical Standards Group Dept of Navy and Air Force (USA)
AN177H20 Aeronautical Standards Group Dept of Navy and Air Force (USA)
B6812 Military Specifications Promulgated by Military Departments/agencies Under Authority of Defense Standardization Manual 4120 3-M
Related Parts
SUCCESSOR 5306-00-051-2338 Bolt,machine
5306-00-297-0047SUCCESSOR
NO ITEM NAME AVAILABLE
5306-00-051-2343SUCCESSOR
BOLT,MACHINE
5306-00-051-2344SUCCESSOR
BOLT,MACHINE
NASM20074-05-40
5306-00-051-2349SUCCESSOR
BOLT,MACHINE
5306-00-141-4519SUCCESSOR
BOLT,CLOSE TOLERANCE
5306-00-141-4712SUCCESSOR
BOLT,MACHINE
5306-00-141-4716SUCCESSOR
BOLT,MACHINE
5306-00-144-3686SUCCESSOR
BOLT,MACHINE
AN3-55
5306-00-144-3692SUCCESSOR
BOLT,MACHINE
5306-00-144-3700SUCCESSOR
BOLT,MACHINE
5306-00-144-3711SUCCESSOR
BOLT,CLOSE TOLERANCE

Frequently Asked Questions

What is NSN 5306-00-167-3925?

NSN 5306-00-167-3925 is a Bolt,close Tolerance, manufactured by Aeronautical Standards Group Dept of Navy and Air Force, classified under FSC 5306 (No Item Name Available). Status: cancelled.

What are the part numbers for NSN 5306-00-167-3925?

NSN 5306-00-167-3925 has 3 cross-referenced part numbers: AN177-20 (Aeronautical Standards Group Dept of Navy and Air Force), AN177H20 (Aeronautical Standards Group Dept of Navy and Air Force), B6812 (Military Specifications Promulgated by Military Departments/agencies Under Authority of Defense Standardization Manual 4120 3-M).

What NSN replaces 5306-00-167-3925?

There are 12 known substitutes for 5306-00-167-3925: 5306-00-297-0047, 5306-00-051-2338, 5306-00-051-2343 and 9 more. Verify interchangeability with system specifications before substitution.

What are the specifications of AN177-20?

Key specifications for AN177-20: Shank Unthreaded Hole Diameter: 0.106 INCHES MINIMUM FIRST HOLE IN; Fastener Length: 2.078 INCHES MINIMUM AND 2.125 INCHES MAXIMUM IN; Hole Diameter: 0.070 INCHES NOMINAL IN; Head Height: 0.234 INCHES MINIMUM AND 0.266 INCHES MAXIMUM IN. 24 total characteristics are documented in the Federal Logistics Information System.

Is NSN 5306-00-167-3925 still in active supply?

NSN 5306-00-167-3925 is currently cancelled. Check with the Defense Logistics Agency for current availability and authorized substitutes.

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