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2840-01-089-2764

Aircraft Gas Turbine Engine Turbine Rotor Blade

2840010892764 010892764 37E501086P118

An item mounted on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the turbine section of an ENGINE, GAS TURBINE, AIRCRAFT. View more Aircraft Gas Turbine Engine Turbine Rotor Blade

2840-01-089-2764 BLADE,TURBINE ROTOR,AIRCRAFT GAS TURBINE ENGINE 2840010892764 010892764

Managed by United States
NSN Created on 29 Jan 1980
Data Last Changed
January 2023
NATO Update Count
13
NATO Data Quality
2840-01-089-2764 BLADE,TURBINE ROTOR,AIRCRAFT GAS TURBINE ENGINE 2840010892764 010892764 1/1
NSN 2840-01-089-2764 (Generic Image) 1/1

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2840-01-089-2764 Related Documents Related Documents 2840-01-089-2764 1+ Documents (More...)

37E501086P118 An item mounted on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
United States (US) 4. 2840-01-089-2764 Marketplace Restrictions Approved Sources Datasheet Management
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2840-01-089-2764 Demil Restrictions 2840-01-089-2764

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

2840-01-089-2764 is a Aircraft Gas Turbine Engine Turbine Rotor Blade that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. 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.

2840-01-089-2764 HTS and ScheduleB Import and Export 2840-01-089-2764

2840-01-089-2764 End Users End Users 2840-01-089-2764

Republic of Korea (ZH01)
Effective Date:
1 Apr 1991
Greece (ZU01)
Effective Date:
1 Apr 1991

2840-01-089-2764 Manufacturers Approved Sources 2840-01-089-2764

2840-01-089-2764 Technical Data Datasheet 2840-01-089-2764

Characteristic
Specifications
FIIG
A10700
End Item Identification [AGAV]
Acft Eng J85
Design Type [APGF]
Compressor
Engine Section Location [CZBJ]
Low Pressure Compressor
Material [MATT]
Steel Blade
Material Document And Classification [MDCL]
B50t1130m Mfr Ref Single Material Response Blade
Special Features [FEAT]
0.251-0.253 In. Dia Of 1 Hole
Overall Length [ABHP]
4.510 Inches Nominal
Overall Width [ABMK]
1.238 Inches Minimum And 1.242 Inches Maximum
Part Name Assigned By Controlling Agency [CXCY]
Blade,Turbine Engine
Stage Number [CZCJ]
1

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2840-01-089-2764 Freight Data Freight Information 2840-01-089-2764

2840-01-089-2764 has freight characteristics.. 2840-01-089-2764 has a variance between NMFC and UFC when transported by rail and the description should be consulted.