3040-01-555-6332

Straight Shaft

3040015556332 015556332 965B412PC1 66E715PC13 965B412PC1(SE)

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

3040-01-555-6332 SHAFT,STRAIGHT 3040015556332 015556332

Managed by United States
NSN Created on 10 Sep 2007
Data Last Changed
November 2023
NATO Update Count
4
NATO Data Quality
3040-01-555-6332 SHAFT,STRAIGHT 3040015556332 015556332 1/1
NSN 3040-01-555-6332 (Generic Image) 1/1

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3040-01-555-6332 Related Documents Related Documents 3040-01-555-6332 5+ Documents (More...)

Account Upgrade 3040-01-421-8125Straight Shaft3040014218125 014218125 965B412-1 662E715 PIECE 13 965B412PC1
Straight Shaft 3040015556332 015556332 to enable JavaScript in your web browser . 3040-01-555-6332Straight
Shaft3040015556332 015556332 965B412PC1 66E715PC13 965B412PC1(SE) A straight shaft having two or more
-15-142-3783 5905151423783 151423783 RESISTENZA https//www.nsnlookup.com /fsg-30/fsc-3040/us 3040-01-555-6332
Straight Shaft 3040015556332 015556332 3040-01-555-6332 3040015556332 015556332 is a straight shaft
2835-01-037-3375 2835010373375 010373375 is a single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the rotor, compressor, nonaircraft gas turbine engine and/or the rotor, fan, nonaircraft gas turbine engine through a shaft, turbine, nonaircraft gas turbine engine. it consists of disks, blades, hubs, and the like. it is the moving part of a turbine assembly, nonaircraft gas turbine engine. it has facilities for attaching to a shaft, turbine, nonaircraft gas turbine engine.
| DAC: E50110-0445RNCC: 3 | RNVC: 9 | DAC: E01070-0445RNCC: D | RNVC: 9 | DAC: A 12 Mar 1993 3040-01-555-6332
Straight Shaft 965B412PC1(SE)RNCC: 5 | RNVC: 2 | DAC: 5 10 Sep 2007 5330-00-472-3082 Gasket 60-
30 Jul 1974 2010-00-368-8800 Reduction Ge Pinion 5594461RNCC: 3 | RNVC: 2 | DAC: 6 1 Jan 1963 3040-01-555-6332

3040-01-555-6332 Demil Restrictions 3040-01-555-6332

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

3040-01-555-6332 is a Straight Shaft that does not have a nuclear hardened feature, but does have another critical feature or features 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.

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