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2840-01-459-1286

Aircraft Gas Turbine Engine Compressor Disk And Hub

2840014591286 014591286 1559M63G04-118 1559M63

An item that consists of a DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and a HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Compressor Disk And Hub

Managed by United States

NSN Created on 21 Sep 1998

Data Last Changed
May 2023

NATO Update Count
3

NATO Data Quality

2840-01-459-1286 DISK AND HUB,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840014591286 014591286 1/1 — NSN 2840-01-459-1286 (Generic Image) 1/1

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Restrictions 2840-01-459-1286

IUID Required

2840-01-459-1286 is a Aircraft Gas Turbine Engine Compressor Disk And Hub 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.

Import and Export 2840-01-459-1286

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End Users 2840-01-459-1286

US Air Force (FXX4)
Effective Date:: 1 Sep 1998; AMC 0 AMSC 0 AMSC F IMC E DSOR FT

Approved Sources 2840-01-459-1286

Part Number
Manufacturer
Status
1559M63G04-118: 98748 - Air Force United States Department (Active); Primary Buy; RNCC 3 RNVC 2 DAC 5
1559M63: 07482 - General Electric Company (Active); Informational Drawing; RNCC D RNVC 9 DAC 2

Datasheet 2840-01-459-1286

Characteristic
Specifications
FIIG: A10700
End Item Identification [AGAV]: F118-Ge-100 Aircraft Gas Turbine Engine
Criticality Code Justification [CRTL]: Abhp And Abmz And Feat
Design Type [APGF]: Axial Compressor
Diameter [ABMZ]: 17.225 Inches Minimum And 17.229 Inches Maximum
Engine Section Location [CZBJ]: Compressor
Material [MATT]: Titanium Alloy Overall
Overall Length [ABHP]: 6.425 Inches Minimum And 6.455 Inches Maximum
Part Name Assigned By Controlling Agency [CXCY]: Original Name Hpc Compressor Spool
Special Features [FEAT]: Pt.O. 2J-F110-4, Fig 67, Ind 5; Hpcr Stg 1-2, Spool Oil Drain Holes Are Enlarged 1.48 Larger Than The Current Elliptical Holes To Allow Better Drainage; Can Only Be Used On The F118-Ge-100 Aircraft Jet Turbine Engine

Management Data 2840-01-459-1286

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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 Afto 95; AFTO 95
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:

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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Freight Information 2840-01-459-1286

2840-01-459-1286 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. 2840-01-459-1286 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. 2840-01-459-1286 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. 2840-01-459-1286 is not classified as a special type of cargo when transported by water. 2840-01-459-1286 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 2840-01-459-1286

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