2840-21-914-6270

Aircraft Gas Turbine Engine

2840219146270 219146270 PT6A-112 F300 0T 009 2064

A continuous combustion type engine. Consists primarily of a COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE, CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE and a TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. It may have an AFTERBURNER, TURBINE ENGINE and/or a fan section. Air is compressed and heated by a combustible fuel and expanded through the turbine. It is designed to furnish a source of rotary shaft, pneumatic power or thrust power. The pneumatic power is obtained by a bleedoff of the engine compressor. For a complete operating power unit, mounted on a base, see POWER UNIT, GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine

2840-21-914-6270 ENGINE,GAS TURBINE,AIRCRAFT 2840219146270 219146270

Managed by Canada
NSN Created on 15 May 1998
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-21-914-6270 ENGINE,GAS TURBINE,AIRCRAFT 2840219146270 219146270 1/1
NSN 2840-21-914-6270 (Generic Image) 1/1

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2840-21-914-6270 Related Documents Related Documents 2840-21-914-6270 3+ Documents (More...)

https//www.nsnlookup.com
/fsg-28/fsc-2840/kr
2840-37-520-5277 Aircraft Gas Turbine Engine 2840375205277
Documents 2840-37-520-5277 5+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ca 2840-21-914-6270
Aircraft Gas Turbine Engine 2840219146270 https//www.nsnlookup.com /nato/nato-stock-numbers/inc
2840-37-520-5277 Aircraft Gas Turbine Engine A80611002-01RNCC: 5 | RNVC: 2 | DAC: 3 13 Dec 2010 2840-21-914-6270
https//www.nsnlookup.com
/nato/nato-stock-numbers/inc
Aircraft Gas Turbine Engine (INC 50488)
2840-37-520-5277 Aircraft Gas Turbine Engine A80611002-01RNCC: 5 | RNVC: 2 | DAC: 3 13 Dec 2010 2840-21-914-6270
https//www.nsnlookup.com
/fsg-28/fsc-2840/au
2840-66-133-3428 Aircraft Gas Turbine Engine 2840661333428
2840-66-133-3428 2840661333428 661333428 is a continuous combustion type engine. consists primarily of a compressor, aircraft gas turbine engine, chamber, combustion, aircraft gas turbine engine and a turbine assembly, aircraft gas turbine engine. it may have an afterburner, turbine engine and/or a fan section. air is compressed and heated by a combustible fuel and expanded through the turbine. it is designed to furnish a source of rotary shaft, pneumatic power or thrust power. the pneumatic power is obtained by a bleedoff of the engine compressor. for a complete operating power unit, mounted on a base, see power unit, gas turbine engine.

2840-21-914-6270 Demil Restrictions 2840-21-914-6270

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

2840-21-914-6270 is a Aircraft Gas Turbine Engine

2840-21-914-6270 End Users End Users 2840-21-914-6270

France (ZF)

2840-21-914-6270 Manufacturers Approved Sources 2840-21-914-6270

Part Number
Manufacturer
Status
PT6A-112
00198 - Pratt & Whitney Canada Cie (Active)
Primary Buy
RNCC 3 RNVC 2 DAC 4
F300 0T 009 2064
F6647 - Service Central Des Achats De La (Active)
NATO Reference
RNCC 6 RNVC 9 DAC 9

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