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2840-01-630-0270

Aircraft Gas Turbine Engine Turbine Hub

2840016300270 016300270 23075212

A component of a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It is designed to attach to the front and/or rear of the rotor providing support, alignment, and a means of attachment for a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have provisions for installing bearings, and/or oil and air seals. See also DISK AND HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Turbine Hub

2840-01-630-0270 HUB,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840016300270 016300270

Managed by United States
NSN Created on 23 Jul 2014
Data Last Changed
January 2023
NATO Update Count
3
NATO Data Quality
2840-01-630-0270 HUB,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840016300270 016300270 1/1
NSN 2840-01-630-0270 (Generic Image) 1/1

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2840-01-630-0270 Related Documents Related Documents 2840-01-630-0270 5+ Documents (More...)

RQST NE Updated Every Day 2840-01-630-0270 RQST Updated Every Day 2840-01-630-0270 RQST NE Related Documents
2840-01-630-0270 5+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-630-0270
RQST NE Updated Every Day 2840-01-630-0270 RQST Updated Every Day 2840-01-630-0270 RQST NE Related Documents
2840-01-348-2312 Engine Turbine Hub 670-0606 2840-01-146-9475 2835-22-252-8149 2840-14-484-7972 2840-01-630-0270
Hub 670 -0606 2840-01-146-9475 2835-22-252-8149 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-630-0270
2835 2840-01-348-2312 2840-00-402-6136 670-0606 2840-01-146-9475 2835-22-252-8149 Turbine Hub 2840-01-630-0270
Aircraft Gas Turbine Engine Turbine Hub 2840-01-630-0270 2840-01-348-2312 2840-01-146-9475 2835
2840-01-348-2312 2840-00-402-6136 670-0606 2840-01-146-9475 2835-22-252-8149 2840-14-484-7972 2840-01-630-0270
2840-01-348-2312 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-630-0270 Aircraft Gas Turbine
-28/fsc-2840/us 2840-00-402-6136 670-0606 2840-01-146-9475 2835-22-252-8149 2840-14-484-7972 2840-01-630-0270
-28/fsc-2840/us 2840-00-402-6136 670-0606 2840-01-146-9475 2835-22-252-8149 2840-14-484-7972 2840-01-630-0270
2840-01-348-2312 2840-00-402-6136 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-630-0270
Every Day 2840-01-205-6530 RQST NE Restrictions https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-630-0270
Aircraft Gas Turbine Engine Turbine Hub 2835-22-252-8149 2840-14-484-7972 2840-01-630-0270 https
fsg-28/fsc-2840/us 2840-01-348-2312 Aircraft Gas Turbine Engine Turbine Hub 2840-14-484-7972 2840-01-630-0270

2840-01-630-0270 Demil Restrictions 2840-01-630-0270

DEMIL: Q | DEMILI: 3 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

2840-01-630-0270 is a Aircraft Gas Turbine Engine Turbine Hub that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a confirmed Commerce Control List Item (CCLI). This item is not suspected to be hazardous. This item does not contain a precious metal.

2840-01-630-0270 HTS and ScheduleB Import and Export 2840-01-630-0270

2840-01-630-0270 End Users End Users 2840-01-630-0270

France (ZF01)
Effective Date:
1 Jul 2014

2840-01-630-0270 Manufacturers Approved Sources 2840-01-630-0270

2840-01-630-0270 Technical Data Datasheet 2840-01-630-0270

Characteristic
Specifications
FIIG
A10700
End Item Identification [AGAV]
T56-A-427 Turboprop Engine
Part Name Assigned By Controlling Agency [CXCY]
Wheel Assembly,Turbine First Stage Bladed.

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2840-01-630-0270 Freight Data Freight Information 2840-01-630-0270

2840-01-630-0270 has freight characteristics.. 2840-01-630-0270 has a variance between NMFC and UFC when transported by rail and the description should be consulted.