2840-21-896-1268

Turbine Engine Axial-Centrifugal Compressor Rotor

2840218961268 218961268

A single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. It consists of disks, blades, hubs, and the like. It is the moving part of COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Compressor Rotor

2840-21-896-1268 COMPRESSOR ROTOR,AXIAL-CENTRIFUGAL,TURBINE ENGINE 2840218961268 218961268

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Data Last Changed
January 2024
NATO Update Count
1
NATO Data Quality
2840-21-896-1268 COMPRESSOR ROTOR,AXIAL-CENTRIFUGAL,TURBINE ENGINE 2840218961268 218961268 1/1
NSN 2840-21-896-1268 (Generic Image) 1/1

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2840-21-896-1268 2840218961268 218961268
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: | DEMILI : | CRITICALITY : | HMIC : | PMIC : | EDC: | ADPEC : 2840-21-896-1268 is a Turbine Engine
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2840-12-360-3747 2840123603747 123603747,NN31483G01
Day 2840-12-360-3747 RQST NE Related Documents https//www.nsnlookup.com /fsg-28/fsc-2840/ca 2840-21-896-1268
2840218961268 218961268 293-3858 2840-99-103-3965 2840-14-577-8223 2840-14-399-3241 2840-14-493
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2840-14-329-8277 2840143298277 143298277,0283250020
2840-99-799-3352 2840-20-007-3291 2840-14-329-8277 https//www.nsnlookup.com /fsg-28/fsc-2840/ca 2840-21-896-1268
2840218961268 218961268 784-0212 2840-99-779-8636 2840-14-316-2667 2840-14-493-7243 2840-99-799

2840-21-896-1268 Demil Restrictions 2840-21-896-1268

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2840-21-896-1268 is a Turbine Engine Axial-Centrifugal Compressor Rotor

2840-21-896-1268 Related Items NATO Stock Numbers Related to 2840-21-896-1268

2840-14-293-3858 2840-99-103-3965 2840-14-577-8223 2840-14-399-3241 2840-14-493-7246 2840-14-408-3348 2840-12-360-3747 2840-12-300-1225 2840-14-383-7778 2840-14-511-0611 2840-14-493-7214 2840-99-784-0212 2840-99-779-8636 2840-14-316-2667 2840-14-493-7243 2840-99-799-3352 2840-20-007-3291 2840-14-329-8277