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2840-01-511-0612
Aircraft Gas Turbine Engine Turbine Shaft
2840015110612 015110612 1863M32P02-101 1863M32P01-101
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. View more Aircraft Gas Turbine Engine Turbine Shaft
May 2023
2
Marketplace 2840-01-511-0612
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Related Documents 2840-01-511-0612 2+ Documents (More...)
United States (US) 4. 2840-01-511-0612 Marketplace Restrictions Approved Sources Datasheet Management
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Turbine Engine Turbine Shaft 2840-01-511-0612Aircraft Gas Turbine Engine Turbine Shaft2840015110612 015110612
1863M32P02-101 1863M32P01 vendors Request Updated Every Day 2840-01-511-0612 https//www.nsnlookup.com
Restrictions 2840-01-511-0612
IUID Required
2840-01-511-0612 is a Aircraft Gas Turbine Engine Turbine Shaft that does not have a nuclear hardened feature, but does have another critical feature or features such as tolerance, fit restriction or application. The DCMO has forced the Demilization requirements for this item as the ICP has not collaborated. This item is a US Munitions List or Commerce Control List Item which must be destroyed to prevent restoration or repair. Only authorized parties may possess this item. This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 2840-01-511-0612
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-511-0612
- US Air Force (FXX4)
- Effective Date:
- 1 Jul 2003
Approved Sources 2840-01-511-0612
- Part Number
- Manufacturer
- Status
- 1863M32P02-101
- Manufacturer
- 07482 - General Electric Company (Active)
- Primary Buy
- Primary Buy
- 1863M32P01-101
- 07482 - General Electric Company (Active)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 2840-01-511-0612
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- Criticality Code Justification [CRTL]
- Agav
- Engine Section Location [CZBJ]
- High Pressure Turbine
- End Item Identification [AGAV]
- F101 Engine
- Part Name Assigned By Controlling Agency [CXCY]
- Shaft,Fwd Hpt Rotor
- Reference Data And Literature [RDAL]
- 2J-F101-4 Fig 56 Ind 3
- Overall Length [ABHP]
- 10.371 Inches Minimum And 10.381 Inches Maximum
Management Data 2840-01-511-0612
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Oct 2022
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
- Oct 2021
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
- Oct 2020
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
- Oct 2019
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
- MOE
- USC
- Code
- Statement
- Order of Use
- Jump To Code
- Qty Per Assy
- UOM
- Technical Document
- Quantative Expression
- Code
- Department of the Air Force (DF)
- L
- R
- Refer To Net Price 5984.45
- NET PRICE 5984.45
- R
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Freight Information 2840-01-511-0612
2840-01-511-0612 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 114215. A Sub NMFC of Z. It has a NMFC Description of ASSEMBLIES JET AIRCRAFT ENGINE. 2840-01-511-0612 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 63220 which rates the freight between FCL and LCL. 2840-01-511-0612 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 671 for ocean manifesting and military sealift. 2840-01-511-0612 is not classified as a special type of cargo when transported by water. 2840-01-511-0612 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.