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5306-00-514-7105

Internally Relieved Body Bolt

5306005147105 005147105 7435-70 3-10-6 2412

An externally threaded fastener whose external threaded portion is of one nominal diameter. It has a concentric hole along the longitudinal centerline which may extend a part or the full length of the bolt. The concentric hole along the centerline may be counterbored and/or internally threaded at the head end or the bolt end. The head is designed to be held or driven by an external and/or internal driver. For items having a hole(s) perpendicular to the axis which meet the concentric hole along the longitudinal centerline, see BOLT, FLUID PASSAGE. View more Internally Relieved Body Bolt

5306-00-514-7105 BOLT,INTERNALLY RELIEVED BODY 5306005147105 005147105

Managed by United States
NSN Created on 1 Jan 1963
Data Last Changed
January 2023
NATO Update Count
10
NATO Data Quality
AASK Style C1 for 5306-00-514-7105 1/2
NSN 5306-00-514-7105 (Identification) 1/2
STYL Style B40 for 5306-00-514-7105 2/2
NSN 5306-00-514-7105 (Identification) 2/2

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5306-00-514-7105 Related Documents Related Documents 5306-00-514-7105 5+ Documents (More...)

5998-01-097-2468 5998010972468 010972468 is a grouping of two or more physically connected or related electrical an/or electronic parts capable of dissassemblage. each component of the assemblage must be capable of functioning in accordance with its own item name. consists of a single printed circuit board or terminal board upon which are mounted separately manufactured electronic components such as capacitors, inductors, resistors, and the like. it may also include printed electronic components. the item is generally part of a subassembly and cannot be assigned a more definite item name. for items having a complete individual electrical/electronic function, use applicable item name such as amplifier (as modified); power supply; or the like. for items not having a complete individual electrical/electronic function, see applicable subassembly name, such as amplifier subassembly; power supply subassembly; or the like. for an assembly of electrical/electronic components mounted on other than a single printed wiring board, see electronic components assembly. excludes printed circuit boar
5340-33-145-5681 5340331455681 331455681 is a forked part, having transverse hole(s) or slot(s) in each arm (prong) to accommodate a bolt, pin, or the like, and having a connection facility opposite the fork. it is designed to be attached to a shaft, rod, turnbuckle or the like by welding, threading, and/or pinning. may include provisions for locking. see also yoke, universal joint and connector, rod end. for items specifically designed for aviation, see clevis, rod end, aviation.
DAC: X 1 Jan 1963 5315-00-482-1586 Spring Pin 7-12-31RNCC: 5 | RNVC: 2 | DAC: 5 16 Sep 1970 5306-00-514-7105
Account Upgrade 5310-00-060-9810Gang Channel Self-Locking Nut Assembly5310000609810 000609810 G1000-3-10-6
Approved Sources 5310-00-060-9810 Part NumberManufacturerStatusG1000-3-10-6 15653 - Howmet Global Fastening
2 DAC 2 3M150N3-10-6 76301 - The Boeing Company (Active) Secondary Buy RNCC 5 RNVC 2 DAC 2 G1000-3-10-6

5306-00-514-7105 Demil Restrictions 5306-00-514-7105

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

5306-00-514-7105 is a Internally Relieved Body Bolt that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. 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. The precious metals content of this item is unknown.

5306-00-514-7105 HTS and ScheduleB Import and Export 5306-00-514-7105

5306-00-514-7105 End Users End Users 5306-00-514-7105

Portugal (ZP01)
Effective Date:
1 Apr 1991
Greece (ZU01)
Effective Date:
1 Apr 1991

5306-00-514-7105 Manufacturers Approved Sources 5306-00-514-7105

5306-00-514-7105 Technical Data Datasheet 5306-00-514-7105

Characteristic
Specifications
FIIG
A003B0
Distance From Head Largest Bearing Surface To Shank Hole Center [CRZS]
1.969 Inches Nominal First Hole
Concentric Hole Depth [AAWX]
2.062 Inches Nominal
Concentric Hole Diameter [AAXC]
0.250 Inches Nominal
Fastener Length [AASB]
3.375 Inches Nominal
Hardness Rating [CQFM]
25.0 Rockwell C Minimum Overall And 32.0 Rockwell C Maximum Overall
Head Height [AASU]
0.312 Inches Nominal
Head Style [AASK]
Hexagon
Material [MATT]
Steel Overall
Nominal Thread Size [CQJX]
0.250 Inches Concentric Hole
Nominal Thread Diameter [AHYM]
0.750 Inches
Nonstandard Thread Pitch Diameter [CFSG]
+0.6960/+0.7010 Inches
Shank Unthreaded Hole Diameter [AAWB]
0.125 Inches Nominal First Hole
Special Features [FEAT]
Equally Spaced Radial Serrations On Head Bearing Surface
Width Between Flats [AATB]
1.062 Inches Nominal
Style Designator [STYL]
Concentric Hole Unthreaded
Thread Direction [AAJF]
Right-Hand
Thread Length [AASA]
3.375 Inches Maximum
Thread Quantity Per Inch [CMLP]
11
Thread Series Designator [THSD]
Uns
Thread Series [BZRR]
Unf Concentric Hole
Threads Per Inch [AAEL]
11 Concentric Hole

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5306-00-514-7105 Freight Data Freight Information 5306-00-514-7105

5306-00-514-7105 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 093486. A Sub NMFC of Z. It has a NMFC Description of BOLTS,NUTS OR SCREWS, NOI (SUB 3). 5306-00-514-7105 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 5306-00-514-7105 is rated as class 50 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 48950 which rates the freight between FCL and LCL. 5306-00-514-7105 has a variance between NMFC and UFC when transported by rail and the description should be consulted. It has a Water Commodity Code (WCC) of 573 for ocean manifesting and military sealift. 5306-00-514-7105 is not classified as a special type of cargo when transported by water. 5306-00-514-7105 is not a consolidation and does not exceed 84" in any dimension. It should be compatible with a standard 72" Aircraft Cargo Door when transported by air.