2840-15-207-0113
Turbine Engine Cooling Plate
2840152070113 152070113 4106T80P02 (241)A34604106T80P02
An item of various cross sections used to exhaust heat from the gas generator turbine rotor of a turbine engine. View more Turbine Engine Cooling Plate
Managed by Italy
NSN Created on 8 Aug 2012
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality

Marketplace 2840-15-207-0113
Need Help?
Request a Quotation from participating marketplace vendors
Request a Quotation from participating marketplace vendors
Related Documents 2840-15-207-0113 1+ Documents (More...)
4106T80P02 (241)A34604106T80P02 An item of various cross sections used to exhaust heat from the gas
2840-15-207-0113 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/it 2840-15-207-0113
Turbine Engine Cooling Plate 2840152070113 4106T80P02 (241)A34604106T80P02 An item of various cross
2840-15-207-0113 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/it 2840-15-207-0113
Turbine Engine Cooling Plate 2840152070113 4106T80P02 (241)A34604106T80P02 An item of various cross
Restrictions 2840-15-207-0113
End Users 2840-15-207-0113
- Italy (ZR)
Approved Sources 2840-15-207-0113
- Part Number
- Manufacturer
- Status
- 4106T80P02
- Manufacturer
- A3460 - Ge Avio Srl (Active)
- Primary Buy
- Primary Buy
- (241)A34604106T80P02
- A3460 - Ge Avio Srl (Active)
- Secondary Buy
- Secondary Buy
Similar Supply Items to 2840-15-207-0113

















