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5306-00-757-7157

Machine Bolt

5306007577157 007577157 2380-5

An externally threaded fastener designed for insertion through holes in assembled parts and normally intended to be tightened or released by torquing a nut. The threaded and unthreaded portions are both of one nominal diameter of 0.190 inch (5 mm) or larger. The head is not designed to be held or driven with an inserted driver or by the thumb and fingers. A locking feature may be incorporated in the design of the head or threads. Head dimensions and sizes of threaded and unthreaded portions shall conform to internationally recognized fastener standards. For items having a grip length portion machined to a tolerance of 0.0015 inch (0.038 mm) or less, BOLT, SHEAR. See also SCREW, CAP, HEXAGON HEAD and SCREW, MACHINE. View more Machine Bolt

5306-00-757-7157 BOLT,MACHINE 5306007577157 007577157

Managed by United States
NSN Created on 1 Jan 1960
Data Last Changed
January 2023
NATO Update Count
11
NATO Data Quality
AASK Style C10 for 5306-00-757-7157 1/2
NSN 5306-00-757-7157 (Identification) 1/2
CRHC Style E2 for 5306-00-757-7157 2/2
NSN 5306-00-757-7157 (Identification) 2/2

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5306-00-757-7157 Related Documents Related Documents 5306-00-757-7157 5+ Documents (More...)

browser . 9150-17-056-5396Synthetic Aircraft Turbine Engine Lubricating Oil9150170565396 170565396 BPTO 2380-5
US GAL ETO 2380-5 US GAL Managed by Netherlands NSN Created on 17 Jan 1995 Data Last Changed January
-17-056-5396 Netherlands (ZN) Approved Sources 9150-17-056-5396 Part NumberManufacturerStatusBPTO 2380-5
Upgrade 9150-01-471-0090Synthetic Aircraft Turbine Engine Lubricating Oil9150014710090 014710090 ETO 2380 5
More... ) https//www.nsnlookup.com /fsg-91/fsc-9150/us 9150-01-471-0090 9150014710090014710090,ETO 2380 5
More... ) https//www.nsnlookup.com /fsg-91/fsc-9150/us 9150-01-471-0090 9150014710090014710090,ETO 2380 5
9150-17-055-7410 9150170557410 170557410 is a thermally stable synthetic oil which may contain additives to improve load-carrying oxidation stability and antifoaming properties. this lubricating oil is intended for use in specific models of aircraft turboprop and turboshaft engines. excludes lubricating oil, aircraft turbine engine, synthetic.
Turbine Engine Lubricating Oil9150121950996 121950996 TURBO OIL 2380 TURBINE OIL 205 EXXON TURBO OIL 2380/5
205 D1961 - Deutsche Veedol Gmbh (Active) Incomplete Reference RNCC 3 RNVC 1 DAC 3 EXXON TURBO OIL 2380/5

5306-00-757-7157 Demil Restrictions 5306-00-757-7157

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

5306-00-757-7157 is a Machine 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. This item does not contain a precious metal.

5306-00-757-7157 HTS and ScheduleB Import and Export 5306-00-757-7157

5306-00-757-7157 End Users End Users 5306-00-757-7157

Brazil (YA01)
Effective Date:
1 Sep 2000
Turkey (ZW01)
Effective Date:
1 Nov 2005

5306-00-757-7157 Manufacturers Approved Sources 5306-00-757-7157

5306-00-757-7157 Technical Data Datasheet 5306-00-757-7157

Characteristic
Specifications
FIIG
A003B0
Extended Washer Diameter [AATC]
0.438 Inches Nominal
Extended Washer Thickness [AATD]
0.060 Inches Minimum And 0.070 Inches Maximum
Fastener Length [AASB]
1.595 Inches Minimum And 1.625 Inches Maximum
Hardness Rating [CQFM]
26.0 Rockwell C Minimum Overall And 32.0 Rockwell C Maximum Overall
Head Height [AASU]
0.330 Inches Nominal
Head Style [AASK]
Double Hexagon W/Hole
Hole Diameter [AAUB]
0.070 Inches Nominal
Hole Configuration Style [CRHC]
Double Hexagon Longitudinal Hole
Hole Quantity [ASXK]
4
Hole Type [BQDM]
Drilled
Material [MATT]
Steel Overall
Nominal Thread Diameter [AHYM]
0.250 Inches
Material Document And Classification [MDCL]
Ams6322 Assn Std Single Material Response Overall
Width Between Flats [AATB]
0.304 Inches Minimum And 0.313 Inches Maximum
Surface Treatment Document And Classification [STDC]
Ams2400 Assn Std Single Treatment Response Overall
Surface Treatment [SFTT]
Cadmium Overall
Thread Direction [AAJF]
Right-Hand
Thread Length [AASA]
0.910 Inches Nominal
Thread Series Designator [THSD]
Unf
Thread Quantity Per Inch [CMLP]
28

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5306-00-757-7157 Freight Data Freight Information 5306-00-757-7157

5306-00-757-7157 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). 5306-00-757-7157 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 5306-00-757-7157 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. 5306-00-757-7157 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. 5306-00-757-7157 is not classified as a special type of cargo when transported by water. 5306-00-757-7157 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.