2840-21-921-4427

Aircraft Gas Turbine Engine Augmentor Nozzle Section Seal

2840219214427 219214427 3116820-01

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

2840-21-921-4427 SEAL,AUGMENTOR NOZZLE SECTION,AIRCRAFT GAS TURBINE ENGINE 2840219214427 219214427

Managed by Canada
NSN Created on 13 Nov 2001
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-21-921-4427 SEAL,AUGMENTOR NOZZLE SECTION,AIRCRAFT GAS TURBINE ENGINE 2840219214427 219214427 1/1
NSN 2840-21-921-4427 (Generic Image) 1/1

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2840-21-921-4427 DEMIL: | DEMILI : | CRITICALITY : | HMIC : | PMIC : | EDC: | ADPEC : 2840-21-921-4427
2840-01-443-7426 2840-01-708-1429 2840-01-708-1427 https//www.nsnlookup.com /fsg-28/fsc-2840/ca 2840-21-921-4427
2840219214427 219214427,3116820-01 190-6884 2840-01-708-1712 2840-01-443-7426 2840-01-471-6752
2840-01-471-6752 2840-01-708-1724 2840-01-708-1429 https//www.nsnlookup.com /fsg-28/fsc-2840/ca 2840-21-921-4427
2840219214427 219214427,3116820-01 708-1431 2840-01-190-6884 2840-01-708-1712 2840-01-443-7426

2840-21-921-4427 Demil Restrictions 2840-21-921-4427

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

2840-21-921-4427 is a Aircraft Gas Turbine Engine Augmentor Nozzle Section Seal

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