2840-21-858-3229

Turbo-Prop Aircraft Engine

2840218583229 218583229 T56A7B S28-025 L14-110-000LC000

A combustion type power unit, may be with or without container, designed to use superheated air to spin a turbine rotor attached to the propeller shaft through reduction gears. View more Turbo-Prop Aircraft Engine

2840-21-858-3229 ENGINE,AIRCRAFT,TURBO-PROP 2840218583229 218583229

Managed by Canada
NSN Created on 14 May 1970
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-21-858-3229 ENGINE,AIRCRAFT,TURBO-PROP 2840218583229 218583229 1/1
NSN 2840-21-858-3229 (Generic Image) 1/1

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2840-21-858-3229 Related Documents Related Documents 2840-21-858-3229 4+ Documents (More...)

T56A7B S28-025 L14-110-000LC000 A combustion type power unit, may be with or without container, designed
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2840-21-858-3229 Demil Restrictions 2840-21-858-3229

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

2840-21-858-3229 is a Turbo-Prop Aircraft Engine

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