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2840-01-448-4901

Aircraft Gas Turbine Engine Hot Section Module

2840014484901 014484901 4082654-803 4084522-801 4082657-808 4084522-802 4084522-800

A unit consisting of a CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE and TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE with hardware and accessories attached. It may include an AFTERBURNER, TURBINE ENGINE. It is specifically designed for quick replacement of this portion of an ENGINE, GAS TURBINE, AIRCRAFT. View more Aircraft Gas Turbine Engine Hot Section Module

2840-01-448-4901 HOT SECTION MODULE,AIRCRAFT GAS TURBINE ENGINE 2840014484901 014484901

Managed by United States
NSN Created on 29 Aug 1997
Data Last Changed
May 2023
NATO Update Count
11
NATO Data Quality
2840-01-448-4901 HOT SECTION MODULE,AIRCRAFT GAS TURBINE ENGINE 2840014484901 014484901 1/1
NSN 2840-01-448-4901 (Generic Image) 1/1

2840-01-448-4901 Stock and Availability Marketplace 2840-01-448-4901

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2840-01-448-4901 Related Documents Related Documents 2840-01-448-4901 5+ Documents (More...)

4082654-803 4084522-801 4082657-808 4084522-800 4084522-802 A unit consisting of a CHAMBER, COMBUSTION
United States (US) 4. 2840-01-448-4901 Marketplace Restrictions Approved Sources Datasheet Management
Request a Quotation from participating marketplace vendors Request Updated Every Day 2840-01-448-4901
2337Aircraft Gas Turbine Engine Turbine Component https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-448-4901
2840014484901 014484901,4082654-803 Subscribe View Prices Effective DateOrganizationUnit https/
CharacteristicSpecificationsFIIGA521B0Special Features [FEAT]1St Stage Assembly And Use Only On 4082654-803
And 5.813 Inches MaximumSpecial Features [FEAT]Nt.O. 2J-F100-54, Fig 89, Ind 71; Use Only On P/N 4084522-800
, -801, -802, 4082654-803, And 4082657-808; Location Near No. 4 Bearing Front Air Sealing Ring, Front
Stator Assy, 1St Stage Turbine Stator Support, Vanes, Inner Air Sealing Ring; Use Only On P/Ns 4084522-800
, 4082654-803 And 4082657-808 Management Data 2840-01-448-6990 Subscribe View Prices Effective DateOrganizationUnit
Ind 4; Location Near The Rear Compressor Drive Turbine Rotor And Stator Assy; Use Only On P/Ns 4084522-801
And -802, 4082654-803 And 4082657-808Stage Number [CZCJ]1 Management Data 2840-01-448-7032 Subscribe

2840-01-448-4901 Demil Restrictions 2840-01-448-4901

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

IUID Required

2840-01-448-4901 is a Aircraft Gas Turbine Engine Hot Section Module that is an aviation critical safety item or flight safety critical aircraft part. 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.

2840-01-448-4901 HTS and ScheduleB Import and Export 2840-01-448-4901

2840-01-448-4901 End Users End Users 2840-01-448-4901

US Air Force (FXX4)
Effective Date:
1 Sep 2000
Former MOE Rule:
FEE4
Singapore (YJ01)
Effective Date:
1 May 1999
Republic of Korea (ZH01)
Effective Date:
1 Nov 2002
Greece (ZU01)
Effective Date:
1 May 2008

2840-01-448-4901 Manufacturers Approved Sources 2840-01-448-4901

2840-01-448-4901 Technical Data Datasheet 2840-01-448-4901

Characteristic
Specifications
FIIG
A23900
Criticality Code Justification [CRTL]
Agav
End Item Identification [AGAV]
Acft Eng F100pw229
Part Name Assigned By Controlling Agency [CXCY]
Core Engine Module

2840-01-448-4901 Management Data Management Data 2840-01-448-4901

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
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
F
When Exhausted Use 2840-01-582-2797
Department of the Air Force (DF)
L
R
Refer To Net Price 3030515.46
NET PRICE 3030515.46

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:
NZ
PRATT & WHITNEY JET ENGINES & COMPONENTS, F-100–P-100
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).

2840-01-448-4901 Related Items NATO Stock Numbers Related to 2840-01-448-4901

2840-01-448-4901 Freight Data Freight Information 2840-01-448-4901

2840-01-448-4901 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 120800. A Sub NMFC of C. It has a NMFC Description of ENGINES, INTERNAL COMBUSTION,NOI; S. 2840-01-448-4901 is rated as class 100 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. 2840-01-448-4901 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 593 for ocean manifesting and military sealift. 2840-01-448-4901 is classified as Aircraft Engine, Internal Combustion Engine or Fuel Control Device when transported by water. 2840-01-448-4901 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.

2840-01-448-4901 Packaging Data Packaging Data 2840-01-448-4901

Responsible Activity
Packaging Data Source
Primary Inventory Control Activity (PICA)
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Item Pack Level (Unpackaged)

Item Size
Item Weight
Characteristics
Weight/Dimensions Category
Fragility
Item Preservation
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Unit Pack Level (Packaged)

Quantity per Pack
Unit Size
Unit Weight
Unit Cube
Preservation Method
Cleaning/Drying
1
90.0" H x 60.0" W x 65.0" L
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Special Requirements
Preservation Material
Wrapping Material
Cushioning/Dunnage
Cushioning Thickness
Container
Special Marking
Special 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
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