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2840-01-438-8397

Aircraft Gas Turbine Engine Compressor Rotor

2840014388397 014388397 1559M63G02-118

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

Managed by United States

NSN Created on 20 Nov 1996

Data Last Changed
May 2023

NATO Update Count
3

NATO Data Quality

2840-01-438-8397 ROTOR,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840014388397 014388397 1/1 — NSN 2840-01-438-8397 (Generic Image) 1/1

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Restrictions 2840-01-438-8397

IUID Required

2840-01-438-8397 is a Aircraft Gas Turbine Engine Compressor Rotor 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 2840-01-438-8397

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End Users 2840-01-438-8397

US Air Force (FXX4)
Effective Date:: 1 Nov 1996; AMC 0 AMSC 0 AMSC F IMC E DSOR FT

Approved Sources 2840-01-438-8397

Part Number
Manufacturer
Status
1559M63G02-118: 98748 - Air Force United States Department (Active); Primary Buy; RNCC 3 RNVC 2 DAC 2

Datasheet 2840-01-438-8397

Characteristic
Specifications
FIIG: A10700
End Item Identification [AGAV]: F118-Ge-100 Aircraft Gas Turbine Engine
Criticality Code Justification [CRTL]: Feat And Abhp And Abmz And Czbj
Design Type [APGF]: Axial Compressor
Diameter [ABMZ]: 17.300 Inches Nominal
Engine Section Location [CZBJ]: High Pressure Compressor
Material Document And Classification [MDCL]: Ti-17 Mfr Ref Single Material Response Overall
Material [MATT]: Titanium Alloy Overall
Overall Length [ABHP]: 6.143 Inches Minimum And 6.163 Inches Maximum
Part Name Assigned By Controlling Agency [CXCY]: Original Name Spool,Compressor Rotor
Special Features [FEAT]: T.O. 2J-F110-14, Fig 67, Ind 5 Under P/N 1559M63g02; Includes Stage 2; Also Consists No. 1 Disk And No. 2 Disk And Forward Shaft That Makes A 1 Piece Construction That Holds Both Stgs; Weights 40.3 Lbs; Basic P/N Can Be Used On All Engine Types, But Once Used On The F118, It Can Only Be Used On An F118 Engine; Reidentification Will Consist Of Adding The Engine Type As A Dash Number Following The P/N
Stage Number [CZCJ]: 1

Management Data 2840-01-438-8397

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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 Net Price 10920.51; NET PRICE 10920.51

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).

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Freight Information 2840-01-438-8397

2840-01-438-8397 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. 2840-01-438-8397 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 2840-01-438-8397 is rated as class 85 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. 2840-01-438-8397 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. 2840-01-438-8397 is not classified as a special type of cargo when transported by water. 2840-01-438-8397 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.

Packaging Data 2840-01-438-8397

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: 15.5" H x 15.5" W x 6.8" L; --; --; --; --

Unit Pack Level (Packaged)

Quantity per Pack
Unit Size
Unit Weight
Unit Cube
Preservation Method
Cleaning/Drying: 1; 21.0" H x 21.0" W x 8.0" 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