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2840-00-909-5510

Aircraft Gas Turbine Engine Turbine Nozzle

2840009095510 009095510 6853952

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

2840-00-909-5510 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840009095510 009095510

Managed by United States
NSN Created on 1 Jan 1960
Data Last Changed
January 2023
NATO Update Count
32
NATO Data Quality
2840-00-909-5510 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840009095510 009095510 1/1
NSN 2840-00-909-5510 (Generic Image) 1/1

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2840-00-909-5510 Related Documents Related Documents 2840-00-909-5510 2+ Documents (More...)

5975-01-685-3952 5975016853952 016853952 is an item which facilitates the mounting of electronic/electrical equipment(s) into racks and the like, having holes and/or clamping devices enabling quick replacement of the mounted equipment. does not include the equipment for which designed. may include interconnecting facilities and resilient mountings. excludes drawer, electrical equipment, rack mounted; drawer, electrical equipment cabinet; chassis, electrical equipment and plate, mounting, electrical equipment.

2840-00-909-5510 Demil Restrictions 2840-00-909-5510

DEMIL: B | DEMILI: | CRITICALITY: Y | HMIC: N | PMIC: A | EDC: | ADPEC:

2840-00-909-5510 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. This item is a US Munitions List Item and must be mutilated to scrap. This item is not suspected to be hazardous. This item does not contain a precious metal.

2840-00-909-5510 HTS and ScheduleB Import and Export 2840-00-909-5510

2840-00-909-5510 End Users End Users 2840-00-909-5510

Brazil (YA01)
Effective Date:
1 Oct 2000
Singapore (YJ01)
Effective Date:
1 Apr 1991
New Zealand (ZE01)
Effective Date:
1 Apr 1991
Germany (ZG01)
Effective Date:
1 Mar 2013
Republic of Korea (ZH01)
Effective Date:
1 Aug 1995
Greece (ZU01)
Effective Date:
1 Apr 1991

2840-00-909-5510 Manufacturers Approved Sources 2840-00-909-5510

2840-00-909-5510 Technical Data Datasheet 2840-00-909-5510

Characteristic
Specifications
FIIG
A10700
End Item Identification [AGAV]
Aircraft Engine Model T56
Criticality Code Justification [CRTL]
Agav
Design Type [APGF]
Axial Compressor
Engine Section Location [CZBJ]
Turbine
Material [MATT]
Nickel Overall
Material Document And Classification [MDCL]
Inconel 713 Mfr Ref Single Material Response Overall
Special Features [FEAT]
T.O. 2J-T56-44, Fig 20A, Ind 10; Used On Pos 5, 10, 15, 20, 25 And 30; Weu 6870728; Weu 6896898 U/W 6852237 Or 6856654; Weu 23031747
Stage Number [CZCJ]
1

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2840-00-909-5510 Freight Data Freight Information 2840-00-909-5510

2840-00-909-5510 has freight characteristics.. 2840-00-909-5510 has a variance between NMFC and UFC when transported by rail and the description should be consulted.