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2840-01-414-0605

Aircraft Gas Turbine Engine Turbine Rotor

2840014140605 014140605 9525M19G15 9525M19G16 9525M19G17 9525M19G18 9525M19

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, AIRCRAFT GAS TURBINE ENGINE and/or the ROTOR, FAN, AIRCRAFT GAS TURBINE ENGINE through a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It consists of disks, blades, hubs, and the like. It is the moving part of a TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Turbine Rotor

2840-01-414-0605 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840014140605 014140605

Managed by United States
NSN Created on 30 May 1995
Data Last Changed
May 2023
NATO Update Count
12
NATO Data Quality
2840-01-414-0605 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840014140605 014140605 1/1
NSN 2840-01-414-0605 (Generic Image) 1/1

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2840-01-414-0605 Related Documents Related Documents 2840-01-414-0605 5+ Documents (More...)

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Aircraft Gas Turbine Engine Turbine Rotor 2840-01-414-0605 2840014140605 014140605 is a single
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2840-01-675-7654 2840016757654 016757654 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, aircraft gas turbine engine and/or the rotor, fan, aircraft gas turbine engine through a shaft, turbine, aircraft gas turbine engine. it consists of disks, blades, hubs, and the like. it is the moving part of a turbine assembly, aircraft gas turbine engine. it has facilities for attaching to a shaft, turbine, aircraft gas turbine engine.
9525M19G04 9525M19G06 9525M19G07 9525M19G08 9525M19G09 9525M19G10 9525M19G01 9525M19G02 9525M19G03 9525M19
9525M19G03 07482 - General Electric Company (Active) Canceled/Obsolete RNCC 5 RNVC 9 MEDALS DAC 4 9525M19

2840-01-414-0605 Demil Restrictions 2840-01-414-0605

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

IUID Required

2840-01-414-0605 is a Aircraft Gas Turbine Engine Turbine Rotor 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 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.

2840-01-414-0605 HTS and ScheduleB Import and Export 2840-01-414-0605

2840-01-414-0605 End Users End Users 2840-01-414-0605

US Air Force (FXX4)
Effective Date:
1 May 1995
Greece (ZU01)
Effective Date:
1 May 2008

2840-01-414-0605 Management Data Management Data 2840-01-414-0605

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
Nov 2020
Department of the Air Force (DF)
EA
Subscribe
1
Jan 2020
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
E
Replaced By 2840-01-675-7654
Department of the Air Force (DF)
L
R
Refer To Net Price 235605.08
NET PRICE 235605.08

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:
PR
F11O 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).

2840-01-414-0605 Related Items NATO Stock Numbers Related to 2840-01-414-0605

2840-01-414-0605 Freight Data Freight Information 2840-01-414-0605

2840-01-414-0605 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 120840. A Sub NMFC of X. It has a NMFC Description of ENGINES INTERNAL COMBUSTION NOI. 2840-01-414-0605 is rated as class 150 when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 61410 which rates the freight between FCL and LCL. 2840-01-414-0605 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. 2840-01-414-0605 is not classified as a special type of cargo when transported by water. 2840-01-414-0605 is not a consolidation, but exceeds 84" in at least one dimension. It may not be compatible with a standard 72" Aircraft Cargo Door when transported by air.

2840-01-414-0605 Packaging Data Packaging Data 2840-01-414-0605

Responsible Activity
Packaging Data Source
Primary Inventory Control Activity (PICA)
--

Item Pack Level (Unpackaged)

Item Size
Item Weight
Characteristics
Weight/Dimensions Category
Fragility
Item Preservation
62.0" H x 36.0" W x 36.0" L
--
--
--
--

Unit Pack Level (Packaged)

Quantity per Pack
Unit Size
Unit Weight
Unit Cube
Preservation Method
Cleaning/Drying
1
77.0" H x 46.0" W x 50.0" L
--
--
Physical Protection
Any Suitable Process
Preservation Material
Wrapping Material
Cushioning/Dunnage
Cushioning Thickness
Container
Special Marking
No Requirement
Special Requirements – see Specific Instructions or Drawings provided
Special Requirements. See Specific Instructions or Drawings Provided
Special Requirements. See Specific Instructions or Drawings Provided
Special requirement – See specific instructions or drawings provided
Special requirements

Intermediate Pack Level

Quantity of Unit Packs
Container
--
No Requirement