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2840-01-340-6506

Aircraft Gas Turbine Engine Compressor Rotor

2840013406506 013406506 1359M16G06-118 1359M16G03-118

A single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. It consists of disks, blades, hubs, and the like. It is the moving part of COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Compressor Rotor

2840-01-340-6506 ROTOR,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840013406506 013406506

Managed by United States
NSN Created on 18 Jun 1991
Data Last Changed
May 2023
NATO Update Count
7
NATO Data Quality
2840-01-340-6506 ROTOR,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840013406506 013406506 1/1
NSN 2840-01-340-6506 (Generic Image) 1/1

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2840-01-340-6506 Related Documents Related Documents 2840-01-340-6506 5+ Documents (More...)

1359M16G06-118 1359M16G03-118 A single or multistage assembly designed to deliver air at the proper
United States (US) 4. 2840-01-340-6506 Marketplace Restrictions Approved Sources Datasheet Management
Request a Quotation from participating marketplace vendors Request Updated Every Day 2840-01-340-6506
vendors Request Updated Every Day 2840-01-240-3518 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-340-6506
2840013406506 013406506,1359M16G06-118 2840-01-340-6506Aircraft Gas Turbine Engine Compressor Rotor2840013406506
013406506 1359M16G06-118 1359M16G03 NumberManufacturerStatus1359M16G06-118 98748 - Air Force United
Compressor Rotor2840014753393 014753393 1359M16G06 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-340-6506
2840013406506 013406506,1359M16G06-118 Account Upgrade 2840-01-340-6506Aircraft Gas Turbine Engine
Compressor Rotor2840013406506 013406506 1359M16G06 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840
https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-340-6506
2840013406506 013406506,1359M16G06-118 28/fsc-2840/us 2840-01-250-6895 2840012506895 012506895,1359M16G06
28/fsc-2840/us 2840-01-250-6895 2840012506895 012506895,1359M16G06 Compressor Rotor2840013406506 013406506

2840-01-340-6506 Demil Restrictions 2840-01-340-6506

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

IUID Required

2840-01-340-6506 is a Aircraft Gas Turbine Engine Compressor Rotor that is an aviation critical safety item or flight safety critical aircraft part. Demilitarization of this item has been confirmed and is not currently subject to changes. 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.

2840-01-340-6506 HTS and ScheduleB Import and Export 2840-01-340-6506

2840-01-340-6506 End Users End Users 2840-01-340-6506

US Air Force (FXX4)
Effective Date:
1 Apr 1991

2840-01-340-6506 Manufacturers Approved Sources 2840-01-340-6506

2840-01-340-6506 Technical Data Datasheet 2840-01-340-6506

Characteristic
Specifications
FIIG
A10700
End Item Identification [AGAV]
Pacer Special
Criticality Code Justification [CRTL]
Agav

2840-01-340-6506 Management Data Management Data 2840-01-340-6506

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Oct 2022
Department of the Air Force (DF)
EA
Subscribe
1
Oct 2021
Department of the Air Force (DF)
EA
Subscribe
1
Oct 2020
Department of the Air Force (DF)
EA
Subscribe
1
Oct 2019
Department of the Air Force (DF)
EA
Subscribe
1
MOE
USC
Code
Statement
Order of Use
Jump To Code
Qty Per Assy
UOM
Technical Document
Quantative Expression
Department of the Air Force (DF)
L
R
Refer To Afto 95 Req
AFTO 95 REQ
Department of the Air Force (DF)
L
R
Refer To Net Price 23196.93
NET PRICE 23196.93

Air Force Air Force

Fund:
SF
Stock fund applicable to items managed for the Air Force by the respective Inventory Control Point
Budget:
8
97X4830.FCL4 - Materiel Support DIV (MSD) - Materiel Support Division (MSD), which includes those Air Force Centrally Managed Investment Items (ERRC XD1=C and XD2=T) except for those still managed in budget programs (BP) 15, 25, 82, 83, and 84 as stock fund exempt. MSD also includes items centrally procured and managed as Expense Items (ERRC XB3=N and XF3=P). Reference AFMAN 23–110, Volume 1, Part 3, Chapter 7, Paragraph 7.3.1
Aggregation Code:
JU
F118-GE-100 ENGINE
Price Validation Code:
N
The current standard price in Catalog Management Data (CMD) has not analyzed or coded for LP/LM.
The price has not been analyzed or reviewed for accuracy.
ZOP or Standard price challenges are permissible but must be supported with adequate justification. However, if coded for Local Purchase (LP) or Fabrication/Manufacture as indicated with an (LM) Acquisition Advice Code of “L” or “F”, then it must be evaluated locally where purchased or fabricated.
Expendability
Recoverability
Repairability:
T
Expendable. Reparable. Condemn at Depot. AF Recoverable Assembly Management System (AFRAMS).

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2840-01-340-6506 Freight Data Freight Information 2840-01-340-6506

2840-01-340-6506 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. 2840-01-340-6506 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 2840-01-340-6506 is rated as class 77.5 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 63220 which rates the freight between FCL and LCL. 2840-01-340-6506 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. 2840-01-340-6506 is not classified as a special type of cargo when transported by water. 2840-01-340-6506 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.