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2840-01-444-7693

Aircraft Gas Turbine Engine Turbine Nozzle

2840014447693 014447693 1864M32G02

A single stationary item designed for the purpose of directing air at the proper angle and velocity to a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud. View more Aircraft Gas Turbine Engine Turbine Nozzle

2840-01-444-7693 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840014447693 014447693

Managed by United States
NSN Created on 15 May 1997
Data Last Changed
May 2023
NATO Update Count
1
NATO Data Quality
2840-01-444-7693 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840014447693 014447693 1/1
NSN 2840-01-444-7693 (Generic Image) 1/1

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1864M32G02 A single stationary item designed for the purpose of directing air at the proper angle and
United States (US) 4. 2840-01-444-7693 Marketplace Restrictions Approved Sources Datasheet Management
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2840-01-444-7693 Demil Restrictions 2840-01-444-7693

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

IUID Required

2840-01-444-7693 is a Aircraft Gas Turbine Engine Turbine Nozzle 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.

2840-01-444-7693 HTS and ScheduleB Import and Export 2840-01-444-7693

2840-01-444-7693 End Users End Users 2840-01-444-7693

US Air Force (FXX4)
Effective Date:
1 Sep 2000
Former MOE Rule:
FEE4

2840-01-444-7693 Manufacturers Approved Sources 2840-01-444-7693

2840-01-444-7693 Technical Data Datasheet 2840-01-444-7693

Characteristic
Specifications
FIIG
A10700
Criticality Code Justification [CRTL]
Abhp And Abkw And Abmz And Feat
Design Type [APGF]
Axial Compressor
Diameter [ABMZ]
34.568 Inches Nominal
End Item Identification [AGAV]
Tf-39 Aircraft Gas Turbine Engine
Engine Section Location [CZBJ]
High Pressure Turbine
Material [MATT]
Nickel Alloy Overall
Overall Height [ABKW]
4.482 Inches Minimum And 4.505 Inches Maximum
Overall Length [ABHP]
2.013 Inches Minimum And 2.087 Inches Maximum
Special Features [FEAT]
T.O. 2J-Tf39-4, Fig 62 Ind 22; Boroscope Location; Repl P/N 9022M16g26; Whole New Config Based On Ecp 369, Dcn 97-37; New Matl And Design Changes; Not To Be Grpd To Old Config; When Old Config Comes In And Repl By Tcto Kits With New Parts, Old Config Is Thrown Away, Not Modified, Not I&Sable; Qty 1 Per Assy
Stage Number [CZCJ]
2

2840-01-444-7693 Management Data Management Data 2840-01-444-7693

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 840.13
NET PRICE 840.13

Air Force Air Force

Fund:
RO
Major Repair
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:
NY
GENERAL ELECTRIC ENGINES & COMPONENTS, TF-39
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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2840-01-444-7693 Freight Data Freight Information 2840-01-444-7693

2840-01-444-7693 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 133320. A Sub NMFC of X. It has a NMFC Description of MACHINERY PARTS OIL/FUEL FILTER. 2840-01-444-7693 is rated as class 70 when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 64100 which rates the freight between FCL and LCL. 2840-01-444-7693 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. 2840-01-444-7693 is not classified as a special type of cargo when transported by water. 2840-01-444-7693 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.