2840-21-869-3223
Turbo-Shaft Aircraft Engine
2840218693223 218693223 T63A700B L14-112-000LC001 S28-048
A continuous-combustion type engine, may be with or without container, designed to use superheated air to drive a turbine rotor which is connected to the rotorshaft of a helicopter by way of reduction gears. View more Turbo-Shaft Aircraft Engine
Managed by Canada
NSN Created on 19 Nov 1974
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
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Related Documents 2840-21-869-3223 1+ Documents (More...)
T63A700B L14-112-000LC001 S28-048 A continuous-combustion type engine, may be with or without container
RQST NE Updated Every Day 2840-21-869-3223 RQST Updated Every Day 2840-21-869-3223 RQST NE Related Documents
2840-21-869-3223 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ca 2840-21-869-3223
RQST NE Updated Every Day 2840-21-869-3223 RQST Updated Every Day 2840-21-869-3223 RQST NE Related Documents
2840-21-869-3223 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ca 2840-21-869-3223
Restrictions 2840-21-869-3223
End Users 2840-21-869-3223
- Canada (ZC)
Approved Sources 2840-21-869-3223
- Part Number
- Manufacturer
- Status
- T63A700B
- Manufacturer
- 73342 - Allison Transmission Inc (Active)
- Primary Buy
- Primary Buy
- L14-112-000LC001
- 35898 - Department Of National Defence (Active)
- NATO Reference
- NATO Reference
- S28-048
- 35898 - Department Of National Defence (Active)
- NATO Reference
- NATO Reference
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