2840-21-869-4980

Turbo-Prop Aircraft Engine

2840218694980 218694980 T56A15

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

2840-21-869-4980 ENGINE,AIRCRAFT,TURBO-PROP 2840218694980 218694980

Managed by Canada
NSN Created on 12 Jun 1974
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-21-869-4980 ENGINE,AIRCRAFT,TURBO-PROP 2840218694980 218694980 1/1
NSN 2840-21-869-4980 (Generic Image) 1/1

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2840-21-869-4980 Related Documents Related Documents 2840-21-869-4980 5+ Documents (More...)

Documents 2840-14-243-7731 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ca 2840-21-869-4980
Turbo-Prop Aircraft Engine 2840218694980 //www.nsnlookup.com /nato/nato-stock-numbers/inc Turbo-Prop
2003 2840-14-243-7731 Turbo-Prop Aircraft Engine 160-60009RNCC: 3 | RNVC: 2 | DAC: 2 1 Jan 1968 2840-21-869-4980
Account Upgrade 2840-01-271-8961Turbo-Prop Aircraft Engine2840012718961 012718961 6875452 T56-A-15LFE T56A15
T56-A15 ENGINE,AIRCRAFT,TURBO-PROP 8 EA NS Request Quotation T56A15 ENGINE,AIRCRAFT,TURBO-PROP 8 EA NS
5 RNVC 2 DAC 6 6842601 63005 - Rolls-Royce Corporation (Active) Secondary Buy RNCC 5 RNVC 2 DAC 4 T56A15
5975-01-567-9475 5975015679475 015679475 is a box, frame, or plate fabricated of electrically conductive material designed to mount, but which does not include, electronic components and their associated circuitry. it may have facilities for attachment to a rack or cabinet or to accommodate specially designed components. it may include a shielding function, integral wiring, and mounting hardware as part of the item. excludes mounting base, electrical equipment.

2840-21-869-4980 Demil Restrictions 2840-21-869-4980

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

2840-21-869-4980 is a Turbo-Prop Aircraft Engine

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