2840-01-708-1730

Aircraft Gas Turbine Engine Augmentor Nozzle Section Seal

2840017081730 017081730 FK16635

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

2840-01-708-1730 SEAL,AUGMENTOR NOZZLE SECTION,AIRCRAFT GAS TURBINE ENGINE 2840017081730 017081730

Managed by United States
NSN Created on 20 Mar 2023
Data Last Changed
November 2023
NATO Update Count
1
NATO Data Quality
2840-01-708-1730 SEAL,AUGMENTOR NOZZLE SECTION,AIRCRAFT GAS TURBINE ENGINE 2840017081730 017081730 1/1
NSN 2840-01-708-1730 (Generic Image) 1/1

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2840-01-708-1730 Related Documents Related Documents 2840-01-708-1730 5+ Documents (More...)

Documents 7820-15-112-0154 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-708-1730
2840017081730 017081730,FK16635 015059056,3031T97P38 2840-01-505-9056 fsg-28/fsc-2840/dk 2840-22
-622-6700 2840226226700 226226700,2479-105 673 2840-01-708-1730 www.nsnlookup.com /fsg-28/fsc-2840/dk
2840014437426 014437426,5110T19G02 2840-21-921-4427 2840219214427 219214427,3116820-01 673-3848 2840-01-708-1730
2840-01-505-9056 2840-01-708-1431 2840-22-622-6700 2840226226700 226226700,2479-105 673-3848 2840-01-708-1730
2840-01-505-9056 2840-01-708-1431 2840-01-443-4133 2840014434133 014434133,5103T25P02 673-3848 2840-01-708-1730
fsc-2840/us 2840-01-443-7426 2840014437426 014437426,5110T19G02 219214427,3116820-01 673-3848 2840-01-708-1730
2840-01-505-9056 2840-01-708-1431 2840-01-190-6884 2840-01-708-1712 226226700,2479-105 673-3848 2840-01-708-1730
01-505-9056 2840-01-708-1431 2840-01-190-6884 2840-01-708-1712 014434133,5103T25P02 673-3848 2840-01-708-1730
701-1962 2840017011962 017011962,2410M50P02 2840-01-701-1962 2840-01-686-5641 2840-01-673-3848 2840-01-708-1730
2840016865641 016865641,3031T97P24 226226700,2479-105 701-1962 2840-01-686-5641 2840-01-673-3848 2840-01-708-1730
9056 708-2900 2840-01-708-1715 226226700,2479-105 701-1962 2840-01-686-5641 2840-01-673-3848 2840-01-708-1730
2840-01-505-9056 fsg-28/fsc-2840/dk 2840-22-622-6700 2840226226700 226226700,2479-105 673-3848 2840-01-708-1730
2840-01-505-9056 28/fsc-2840/us 2840-01-443-4133 2840014434133 014434133,5103T25P02 673-3848 2840-01-708-1730
2840-01-505-9056 2840226226700 226226700,2479-105 701-1962 2840-01-686-5641 2840-01-673-3848 2840-01-708-1730

2840-01-708-1730 Demil Restrictions 2840-01-708-1730

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

2840-01-708-1730 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.

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