2840-01-708-1724

Aircraft Gas Turbine Engine Augmentor Nozzle Section Seal

2840017081724 017081724 FK16636

A rigid item designed to complete the circumference when the NOZZLE,AUGMENTER EXHAUST,AIRCRAFT GAS TURBINE ENGINE is in the open position allowing the nozzle to maintain control of the hot exhaust gases. It is situated between the AUGMENTOR NOZZLE SECTION,OUTER,AIRCRAFT GAS TURBINE ENGINE and the AUGMENTOR NOZZLE SECTION,OUTER,AIRCRAFT GAS TURBINE ENGINE and the AUGMENTOR NOZZLE SECTION,CONVERGENT,AIRCRAFT GAS TURBINE ENGINE; AUGMENTOR NOZZLE SECTION,INNER,AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Augmentor Nozzle Section Seal

2840-01-708-1724 SEAL,AUGMENTOR NOZZLE SECTION,AIRCRAFT GAS TURBINE ENGINE 2840017081724 017081724

Managed by United States
NSN Created on 20 Mar 2023
Data Last Changed
November 2023
NATO Update Count
1
NATO Data Quality
2840-01-708-1724 SEAL,AUGMENTOR NOZZLE SECTION,AIRCRAFT GAS TURBINE ENGINE 2840017081724 017081724 1/1
NSN 2840-01-708-1724 (Generic Image) 1/1

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2840-01-708-1724 Related Documents Related Documents 2840-01-708-1724 5+ Documents (More...)

RQST NE Updated Every Day 2840-01-708-1724 RQST Updated Every Day 2840-01-708-1724 RQST NE Related Documents
,FK16636 FK16636 A rigid item designed to complete the circumference when the NOZZLE,AUGMENTER EXHAUST
2840017081724017081724,FK16636 2840014434133 014434133,5103T25P02 708-1712 2840-01-443-7426 2840
-01-673-3848 2840011906884 011906884,9505M12G02 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-708-1724
2840017081724 017081724,FK16636 2840014434133 014434133,5103T25P02 708-1712 2840-01-443-7426 2840
-01-471-6752 2840-01-708-1724 2840-01-673-3848 2840016733848 016733848,4114730 708-1712 2840-01-443-7426
Restrictions 2840-01-682-4781 DEMIL: Q | DEMILI https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-708-1724
2840017081724 017081724,FK16636 Documents 2840-01-708-1724 5+ Documents ( More... ) https//www.nsnlookup.com
-4133 2840014434133 014434133,5103T25P02 708-1712 708-1712 2840-01-443-7426 2840-01-471-6752 2840-01-708-1724
Numbers Related to 2840-01-691-7838 2840-01-682-4781 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-708-1724
2840017081724 017081724,FK16636 2840-01-443-7426 2840-01-471-6752 2840-01-708-1724 https//www.nsnlookup.com
www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-708-1429 2840017081429 017081429,FK16588 2840-01-471-6752 2840-01-708-1724
www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-443-4133 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-708-1724
2840017081724 017081724,FK16636 www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-673-4535 2840016734535
2840-01-443-4133 2840014434133 014434133,5103T25P02 708-1712 2840-01-443-7426 2840-01-471-6752 2840-01-708-1724

2840-01-708-1724 Demil Restrictions 2840-01-708-1724

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

2840-01-708-1724 is a Aircraft Gas Turbine Engine Augmentor Nozzle Section Seal that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. 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.

2840-01-708-1724 HTS and ScheduleB Import and Export 2840-01-708-1724

2840-01-708-1724 Manufacturers Approved Sources 2840-01-708-1724

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