2840-99-340-5265

Turbo-Prop Aircraft Engine

2840993405265 993405265 23061937 1152H-001

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

2840-99-340-5265 ENGINE,AIRCRAFT,TURBO-PROP 2840993405265 993405265

Managed by United Kingdom
NSN Created on 20 Oct 2011
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-99-340-5265 ENGINE,AIRCRAFT,TURBO-PROP 2840993405265 993405265 1/1
NSN 2840-99-340-5265 (Generic Image) 1/1

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23061937 1152H-001 A combustion type power unit, may be with or without container, designed to use superheated
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2840-99-340-5265 Demil Restrictions 2840-99-340-5265

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

2840-99-340-5265 is a Turbo-Prop Aircraft Engine

2840-99-340-5265 End Users End Users 2840-99-340-5265

United Kingdom (ZK)

2840-99-340-5265 Manufacturers Approved Sources 2840-99-340-5265

Part Number
Manufacturer
Status
23061937
K0378 - Rolls-Royce Plc (Active)
Primary Buy
RNCC 3 RNVC 2 DAC 4
1152H-001
U9124 - Ministry Of Defence, Code Reserved (Active)
NATO Reference
RNCC 6 RNVC 9 DAC 9

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