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5306-01-388-6942

Shoulder Bolt

5306013886942 013886942 MIL-B-6812 NAS1297-8-43

An externally threaded fastener whose threaded portion is of one nominal diameter, No. 10 (0.190 IN.) (5 mm) or larger. It has a round unthreaded neck or shank all or part of which is of greater diameter than the threaded portion. The head is not designed to be held or driven with an inserted drivers. A locking feature may be incorporated in the design of the head or threads. For items with a thread diameter smaller than No. 10 (0.190 IN.) (5 mm) and those items with an inserted drive head, use SCREW, SHOULDER. For items which are No. 10 (0.190 IN.) (5 mm) or larger in size and are both shouldered and have an externally relieved body, use BOLT, EXTERNALLY RELIEVED BODY. Excludes THUMBSCREW. View more Shoulder Bolt

5306-01-388-6942 BOLT,SHOULDER 5306013886942 013886942

Managed by United States
NSN Created on 6 Apr 1994
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
AASK Style C1 for 5306-01-388-6942 1/1
NSN 5306-01-388-6942 (Identification) 1/1

5306-01-388-6942 Stock and Availability Marketplace 5306-01-388-6942

5306-01-388-6942 Related Documents Related Documents 5306-01-388-6942 5+ Documents (More...)

MIL-B-6812 NAS1297-8-43 An externally threaded fastener whose threaded portion is of one nominal diameter
Every Day 5306-01-388-6942 RQST Updated Every Day 5306-01-388-6942 RQST NE Related Documents 5306-01
Marketplace Restrictions Approved Sources Datasheet Management MIL-B-6812 BOLT,SHOULDER 63 EA NS
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5306-01-388-6942 Demil Restrictions 5306-01-388-6942

DEMIL: A | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: | ADPEC: 0

5306-01-388-6942 is a Shoulder Bolt that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.

5306-01-388-6942 HTS and ScheduleB Import and Export 5306-01-388-6942

5306-01-388-6942 End Users End Users 5306-01-388-6942

US Air Force (FBB5)
Effective Date:
1 May 2000
Former MOE Rule:
FEKZ

5306-01-388-6942 Manufacturers Approved Sources 5306-01-388-6942

5306-01-388-6942 Technical Data Datasheet 5306-01-388-6942

Characteristic
Specifications
FIIG
A003B0
Fastener Length [AASB]
3.457 Inches Minimum And 3.497 Inches Maximum
Head Height [AASU]
0.328 Inches Minimum And 0.360 Inches Maximum
Head Style [AASK]
Hexagon
Material [MATT]
Steel Comp 4140 Overall And Steel Comp 8740 Overall And Steel Comp 8650 Overall And Steel Comp 8735 Overall And Steel Comp 4130 Overall And Steel Comp 4037 Overall
Nominal Thread Diameter [AHYM]
0.500 Inches
Shoulder Diameter [AATN]
0.620 Inches Minimum First Shoulder And 0.624 Inches Maximum First Shoulder
Shoulder Length [AATX]
2.687 Inches Nominal First Shoulder
Shoulder Shape [CWYB]
Round First Shoulder
Thread Series Designator [THSD]
Unjf
Width Between Flats [AATB]
0.928 Inches Minimum And 0.940 Inches Maximum
Specification/Standard Data [ZZZK]
80205-Nas1297 Professional/Industrial Association Standard
Surface Treatment Document And Classification [STDC]
Qq-P-416 Ty2 Cl2 Fed Spec Single Treatment Response Overall
Surface Treatment [SFTT]
Cadmium Overall And Chromate Overall
Thread Direction [AAJF]
Right-Hand
Thread Class [AAJD]
3A
Thread Length [AASA]
0.770 Inches Nominal
Thread Quantity Per Inch [CMLP]
20

5306-01-388-6942 Management Data Management Data 5306-01-388-6942

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
May 2010
Department of the Air Force (DF)
EA
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5306-01-388-6942 Freight Data Freight Information 5306-01-388-6942

5306-01-388-6942 has freight characteristics.. 5306-01-388-6942 has a variance between NMFC and UFC when transported by rail and the description should be consulted.