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2840-00-798-2480

Aircraft Gas Turbine Engine Air Seal

2840007982480 007982480 336C736P2

A rigid metallic item, generally circular. It may be formed of segmented arcs. It is designed to prevent leakage of air in an ENGINE, GAS TURBINE, AIRCRAFT. It may be of various cross-sectional shapes. It may have mounting facilities. It may act as a spacer but its primary function is as an air seal. View more Aircraft Gas Turbine Engine Air Seal

2840-00-798-2480 SEAL,AIR,AIRCRAFT GAS TURBINE ENGINE 2840007982480 007982480

Managed by United States
NSN Created on 1 Jan 1962
Data Last Changed
January 2023
NATO Update Count
16
NATO Data Quality
2840-00-798-2480 SEAL,AIR,AIRCRAFT GAS TURBINE ENGINE 2840007982480 007982480 1/1
NSN 2840-00-798-2480 (Generic Image) 1/1

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336C736P2 A rigid metallic item, generally circular.
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2840-00-798-2480 Demil Restrictions 2840-00-798-2480

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

2840-00-798-2480 is a Aircraft Gas Turbine Engine Air Seal 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 considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.

2840-00-798-2480 HTS and ScheduleB Import and Export 2840-00-798-2480

2840-00-798-2480 End Users End Users 2840-00-798-2480

Italy (ZR01)
Effective Date:
1 Apr 1991
Greece (ZU01)
Effective Date:
1 Apr 1991
Turkey (ZW01)
Effective Date:
1 Nov 2005

2840-00-798-2480 Manufacturers Approved Sources 2840-00-798-2480

2840-00-798-2480 Technical Data Datasheet 2840-00-798-2480

Characteristic
Specifications
FIIG
A10700
End Item Identification [AGAV]
Acft Eng
Criticality Code Justification [CRTL]
Abhp And Abmz And Feat
Diameter [ABMZ]
2.400 Inches Minimum And 2.440 Inches Maximum
Engine Section Location [CZBJ]
Turbine
Material [MATT]
Steel Overall
Material Document And Classification [MDCL]
Ams6470 Assn Std Single Material Response Overall
Overall Length [ABHP]
0.248 Inches Minimum And 0.252 Inches Maximum
Part Name Assigned By Controlling Agency [CXCY]
Original Name Seal,Gearbox,Front
Special Features [FEAT]
Inner Dia. Bore 1.871-1.875; Counterbore Inner Dia. 1.707-1.709

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2840-00-798-2480 Freight Data Freight Information 2840-00-798-2480

2840-00-798-2480 has freight characteristics.. 2840-00-798-2480 has a variance between NMFC and UFC when transported by rail and the description should be consulted.