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2840-01-335-9653

Aircraft Gas Turbine Engine Air Seal

2840013359653 013359653 3002123-2

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

2840-01-335-9653 SEAL,AIR,AIRCRAFT GAS TURBINE ENGINE 2840013359653 013359653

Managed by United States
NSN Created on 17 Mar 1991
Data Last Changed
January 2023
NATO Update Count
9
NATO Data Quality
2840-01-335-9653 SEAL,AIR,AIRCRAFT GAS TURBINE ENGINE 2840013359653 013359653 1/1
NSN 2840-01-335-9653 (Generic Image) 1/1

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3002123-2 A rigid metallic item, generally circular.
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2840-01-335-9653 Demil Restrictions 2840-01-335-9653

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

2840-01-335-9653 is a Aircraft Gas Turbine Engine Air Seal that does not have a nuclear hardened feature or any other critical feature 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.

2840-01-335-9653 HTS and ScheduleB Import and Export 2840-01-335-9653

2840-01-335-9653 End Users End Users 2840-01-335-9653

US Coast Guard (C057)
Effective Date:
1 Apr 1991

2840-01-335-9653 Manufacturers Approved Sources 2840-01-335-9653

2840-01-335-9653 Technical Data Datasheet 2840-01-335-9653

Characteristic
Specifications
FIIG
A10700
End Item Identification [AGAV]
Engine Core Assy/Low Pressure Compressor Module/Crossover Duct And No.3 Sump Module Interface;Hu-25A Falcon Jet Aircraft
Diameter [ABMZ]
5.074 Inches Nominal
Engine Section Location [CZBJ]
Low Pressure Compressor
Material [MATT]
Steel Overall
Part Name Assigned By Controlling Agency [CXCY]
Seal,Air,Gas Turbine Engine
Special Features [FEAT]
Material Thickness Of Body 0.012 In.;Flange Thickness 0.246; I.D. 4.131
Stage Number [CZCJ]
5

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2840-01-335-9653 Freight Data Freight Information 2840-01-335-9653

2840-01-335-9653 has freight characteristics.. 2840-01-335-9653 has a variance between NMFC and UFC when transported by rail and the description should be consulted.