PartsTable TECHNICAL DATA SHEET
JULY 2026Technical Data Sheet

2018930Bolt,machine

Embraer Aviation International · NSN 5306-00-151-2626 · FSC 5306 · No Item Name Available
Verified by PartsTable
NSN 5306-00-151-2626 — this item is cataloged by the U.S. Government under National Stock Number 5306-00-151-2626. Primary manufacturer part number: 2018930.
Features
  • Bolt,machine — FSC 5306
  • Thread Quantity Per Inch: 24
  • Grip Length: 0.938 INCHES NOMINAL IN
  • Head Style: HEXAGON
  • Surface Treatment: CADMIUM AND CHROMATE OVERALL
  • Fastener Length: 1.469 INCHES NOMINAL IN
  • Thread Class: 3A A
  • Material: STEEL COMP 8740 OR STEEL COMP 8630 OR STEEL COMP 8735 OR STEEL COMP 4037 OR STEEL COMP 4140 OR STEEL COMP 4130 OVERALL
Applications
  • Structural fastening and assembly
  • Equipment mounting
  • Panel and housing attachment
  • Applications requiring Steel Comp 8740 or Steel Comp 8630 or Steel Comp 8735 or Steel Comp 4037 or Steel Comp 4140 or Steel Comp 4130 Overall construction
General Description

The Bolt,machine, cataloged under National Stock Number 5306-00-151-2626, is classified within Federal Supply Class 5306 (No Item Name Available) of the Hardware and Abrasives group. The primary manufacturer of record is Embraer Aviation International. Government technical data includes 18 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 9 commercial cross-references from 8 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
NSN5306-00-151-2626
Primary Part Number2018930
Item NameBolt,machine
FSC / FSG5306 / 53 — No Item Name Available
ManufacturerEmbraer Aviation International
StatusCANCELLED
Thread Quantity Per Inch24
Grip Length0.938 INCHES NOMINAL IN
Head StyleHEXAGON
Surface TreatmentCADMIUM AND CHROMATE OVERALL
Fastener Length1.469 INCHES NOMINAL IN
Thread Class3A A
MaterialSTEEL COMP 8740 OR STEEL COMP 8630 OR STEEL COMP 8735 OR STEEL COMP 4037 OR STEEL COMP 4140 OR STEEL COMP 4130 OVERALL
Thread DirectionRIGHT-HAND
Surface Treatment Document and ClassificationQQ-P-416,TY 2,CLASS 3 FED SPEC ALL TREATMENT RESPONSES OVERALL
Material Document and ClassificationMIL-S-6049 MIL SPEC 1ST MATERIAL RESPONSE OR MIL-S-6050 MIL SPEC 2ND MATERIAL RESPONSE OR MIL-S-6098 MIL SPEC 3RD MATERIAL RESPONSE OR AMS 6300 ASSN STD 4TH MATERIAL RESPONSE OR MIL-S-5626 MIL SPEC 5TH MATERIAL RESPONSE OR MIL-S-6758 MIL SPEC 6TH MATERIAL RESPONSE OVERALL
Thread Series DesignatorUNF
Nominal Thread Diameter0.312 INCHES IN
Width Between Flats0.490 INCHES MINIMUM AND 0.502 INCHES MAXIMUM IN
Hardness Rating26.0 ROCKWELL C MINIMUM AND 32.0 ROCKWELL C MAXIMUM OVERALL
Features ProvidedFINISHED HEAD
Minimum Tensile Strength125000 POUNDS PER SQUARE INCH LBS
Thread Length0.531 INCHES MINIMUM IN
Head Height0.172 INCHES MINIMUM AND 0.204 INCHES MAXIMUM IN
Lifecycle & Compliance
Acquisition StatusCANCELLED
Successor5306-00-063-3268
HAZMATNo
Verified Substitutes 12
No Item Name Available
Bolt,machine
Bolt,machine
Bolt,close Tolerance
Bolt,close Tolerance
5306-00-150-9233AN5-40A SUCCESSOR
Bolt,machine
National Aerospace Standards Committee Aerospace Industries Association of America Inc Not for Rfq or Solicitation Use
Bolt,machine
Bolt,machine
Bolt,machine
Bolt,clevis
Cross-Reference Index
Part NumberManufacturer
2018930 Embraer Aviation International (FRA)
MILB6812 National Aerospace Standards Committee Aerospace Industries Association of America Inc Not for Rfq or Solicitation Use (USA)
AN5-13A Aeronautical Standards Group Dept of Navy and Air Force (USA)
MILB6812 Military Specifications Promulgated by Military Departments/agencies Under Authority of Defense Standardization Manual 4120 3-M
5306001512626 E.c.a Etablissement Central Des Approvisionnements Des Forces Armees Royales
7415117 CAGE 00000
2018930 Embraer S.a. (BRA)
2018930 Embraer Empresa Brasileira De Aeronautica Sa (BRA)
AN5-13A Leonardo Spa Helicopters Division - Production Site (ITA)
Related Parts
SUCCESSOR 5306-00-063-3268 Bolt,machine
5306-00-734-5825SUCCESSOR
NO ITEM NAME AVAILABLE
5306-00-144-3646SUCCESSOR
BOLT,MACHINE
5306-00-144-4058SUCCESSOR
BOLT,CLOSE TOLERANCE
5306-00-150-9097SUCCESSOR
BOLT,CLOSE TOLERANCE
5306-00-150-9233SUCCESSOR
BOLT,MACHINE
AN5-40A
5306-00-150-9866SUCCESSOR
BOLT,MACHINE
5306-00-150-9867SUCCESSOR
BOLT,MACHINE
5306-00-150-9868SUCCESSOR
BOLT,MACHINE
5306-00-151-0656SUCCESSOR
BOLT,CLEVIS
5306-00-151-0709SUCCESSOR
BOLT,MACHINE
5306-00-151-1084SUCCESSOR
BOLT,MACHINE

Frequently Asked Questions

What is NSN 5306-00-151-2626?

NSN 5306-00-151-2626 is a Bolt,machine, manufactured by Embraer Aviation International, classified under FSC 5306 (No Item Name Available). Status: cancelled.

What are the part numbers for NSN 5306-00-151-2626?

NSN 5306-00-151-2626 has 9 cross-referenced part numbers: 2018930 (Embraer Aviation International), MILB6812 (National Aerospace Standards Committee Aerospace Industries Association of America Inc Not for Rfq or Solicitation Use), AN5-13A (Aeronautical Standards Group Dept of Navy and Air Force), MILB6812 (Military Specifications Promulgated by Military Departments/agencies Under Authority of Defense Standardization Manual 4120 3-M), 5306001512626 (E.c.a Etablissement Central Des Approvisionnements Des Forces Armees Royales) and 4 more.

What NSN replaces 5306-00-151-2626?

There are 12 known substitutes for 5306-00-151-2626: 5306-00-734-5825, 5306-00-063-3268, 5306-00-144-3646 and 9 more. Verify interchangeability with system specifications before substitution.

What are the specifications of 2018930?

Key specifications for 2018930: Thread Quantity Per Inch: 24; Grip Length: 0.938 INCHES NOMINAL IN; Head Style: HEXAGON; Surface Treatment: CADMIUM AND CHROMATE OVERALL. 18 total characteristics are documented in the Federal Logistics Information System.

Is NSN 5306-00-151-2626 still in active supply?

NSN 5306-00-151-2626 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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