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2840-00-054-1346

Aircraft Gas Turbine Engine Turbine Nozzle Assembly

2840000541346 000541346 730684 617284 704374

A 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. The assembled item forms a complete circle. View more Aircraft Gas Turbine Engine Turbine Nozzle Assembly

2840-00-054-1346 NOZZLE ASSEMBLY,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840000541346 000541346

Managed by United States
NSN Created on 20 May 1968
Data Last Changed
January 2023
NATO Update Count
10
NATO Data Quality
2840-00-054-1346 NOZZLE ASSEMBLY,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840000541346 000541346 1/1
NSN 2840-00-054-1346 (Generic Image) 1/1

2840-00-054-1346 Stock and Availability Marketplace 2840-00-054-1346

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730684 617284 704374 A stationary item designed for the purpose of directing air at the proper angle
United States (US) 4. 2840-00-054-1346 Marketplace Restrictions Approved Sources Datasheet Management
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2840-00-054-1346 Demil Restrictions 2840-00-054-1346

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

2840-00-054-1346 is a Aircraft Gas Turbine Engine Turbine Nozzle Assembly 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.

2840-00-054-1346 HTS and ScheduleB Import and Export 2840-00-054-1346

2840-00-054-1346 End Users End Users 2840-00-054-1346

Turkey (ZW01)
Effective Date:
1 Dec 1995

2840-00-054-1346 Manufacturers Approved Sources 2840-00-054-1346

2840-00-054-1346 Technical Data Datasheet 2840-00-054-1346

Characteristic
Specifications
FIIG
A10700
Criticality Code Justification [CRTL]
Agav
Diameter [ABMZ]
27.680 Inches Nominal
Engine Section Location [CZBJ]
Turbine
End Item Identification [AGAV]
Tf-33 Aircraft Engine
Special Features [FEAT]
19.530 In. Id; 150 Vanes
Overall Length [ABHP]
1.191 Inches Nominal
Stage Number [CZCJ]
14

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2840-00-054-1346 Freight Data Freight Information 2840-00-054-1346

2840-00-054-1346 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 133300. A Sub NMFC of Z. It has a NMFC Description of MACHINERY/MACHINES NOI. 2840-00-054-1346 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. 2840-00-054-1346 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. 2840-00-054-1346 is not classified as a special type of cargo when transported by water. 2840-00-054-1346 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.