Premium Information is available for this item - Upgrade for $1 a day

3040-00-402-6146

Straight Shaft

3040004026146 004026146 3017T94P02 3017T94

A straight shaft having two or more of the following conditions: a specified surface finish designation in the range of 1 to 125 microinches (o.o25 to 3.2 micrometers), arithmetical average (aa), machined peripheral flat(s), circular groove (s), keyway(s), splines, threads, or holes. It is not designed for use in aligning by fitting into corresponding holes of another item. It may be drilled for lubricating holes. For items having an integral gear(s) or worm(s), see GEARSHAFT (as modified). For items designed to support rotating members see AXLE(1), STRAIGHT. For items not having the above conditions see PIN, STRAIGHT, HEADLESS. For items having machined ends which constitute steps see SHAFT(1), SHOULDERED; AXLE(1), SHOULDERED; and BOLT, FLUID PASSAGE. View more Straight Shaft

3040-00-402-6146 SHAFT,STRAIGHT 3040004026146 004026146

Managed by United States
NSN Created on 8 Apr 1970
Data Last Changed
January 2023
NATO Update Count
19
NATO Data Quality
AAGZ Style 1 for 3040-00-402-6146 1/1
NSN 3040-00-402-6146 (Identification) 1/1

3040-00-402-6146 Stock and Availability Marketplace 3040-00-402-6146

Need Help?
Request a Quotation from participating marketplace vendors
eBay Updated Every Day
3040-00-402-6146 RQST NE eBay
eBay Updated Every Day
3040-00-402-6146 RQST eBay
Amazon Updated Every Day
3040-00-402-6146 RQST NE Amazon

3040-00-402-6146 Related Documents Related Documents 3040-00-402-6146 3+ Documents (More...)

2840-01-103-5057 2840011035057 011035057 is an item designed to transfer rotary motion from a rotary, turbine, aircraft gas turbine engine to a rotor, compressor, aircraft gas turbine engine and/or a rotor, fan, aircraft gas turbine engine. it may include the hub, turbine, aircraft gas turbine engine. it may include provisions for mounting bearings and/or seals.
2840-01-103-5056 2840011035056 011035056 is an item designed to transfer rotary motion from a rotary, turbine, aircraft gas turbine engine to a rotor, compressor, aircraft gas turbine engine and/or a rotor, fan, aircraft gas turbine engine. it may include the hub, turbine, aircraft gas turbine engine. it may include provisions for mounting bearings and/or seals.
2840-00-003-9568 2840000039568 000039568 SHAFT,TURBINE,AIRCRAFT GAS TURBINE ENGINE

3040-00-402-6146 Demil Restrictions 3040-00-402-6146

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

3040-00-402-6146 is a Straight Shaft that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is a US Munitions List Item and must be mutilated to scrap. This item is not suspected to be hazardous. The precious metals content of this item is unknown.

3040-00-402-6146 HTS and ScheduleB Import and Export 3040-00-402-6146

3040-00-402-6146 End Users End Users 3040-00-402-6146

Brazil (YA01)
Effective Date:
1 Jan 2011
Spain (YB01)
Effective Date:
1 Apr 1991
Malaysia (YW01)
Effective Date:
1 Apr 1991
Canada (ZC01)
Effective Date:
1 Apr 1991
Republic of Korea (ZH01)
Effective Date:
1 Apr 1991
Portugal (ZP01)
Effective Date:
1 Apr 1991
Norway (ZT01)
Effective Date:
1 Apr 1991
Greece (ZU01)
Effective Date:
1 Apr 1991
Turkey (ZW01)
Effective Date:
1 Nov 2005

3040-00-402-6146 Manufacturers Approved Sources 3040-00-402-6146

3040-00-402-6146 Technical Data Datasheet 3040-00-402-6146

Characteristic
Specifications
FIIG
A23200
Material [MATT]
Steel
Surface Finish [CSYM]
8.0 Microinches
First End Style [AAGZ]
Plain
First End Diameter [AMDL]
0.1872 Inches Nominal
End Similarity [AAHN]
Identical
Overall Length [ABHP]
1.465 Inches Nominal

3040-00-402-6146 Related Items NATO Stock Numbers Related to 3040-00-402-6146

3040-00-402-6146 Freight Data Freight Information 3040-00-402-6146

3040-00-402-6146 has freight characteristics.. 3040-00-402-6146 has a variance between NMFC and UFC when transported by rail and the description should be consulted.