GE Aviation H80 (skoršie označenie aj M601H-80) is turbovrtuľový aircraft engine vyrábaný in the Czech republic by GE Aviation Business & General Aviation (BGA) Turboprops. The engine is built on the basis of the engineand M601 modernými technológiami and materiálmi with výkonom on hriadeli 597 kW (800 SHP). Konštrukcia engineand at the same time secures high performance of the aj pri vyššej temperature all others air and vo higher nadmorských výškach. From the engineand H80 is odvodený engine H75 with výkonom 559 kW (750 SHP) and H85 with výkonom 633 kW (850 SHP).
The engine received a certifikáciu FAA 13.03.2012, in októbri 2012 received Russian type osvedčenie, won the aj osvedčenie from európskej EASA, brazílskej and argentínskej the agency of pre civilné the air force.
The engine was certified to drive lietadiel L-410UVP-E20, the Thrush 510G, Technoavia Rysačok and the CAIGA Primus 150.
Type : Turbovrtuľový (Weight Forces)
Dĺžka : 1 670 mm (66")
Height : 580 mm (23")
Width : 560 mm (22")
Dry hmotnosť : 177 kg (390 lb)
Kompresný ratio : 6,7
Fuel: Jet A, Jet A-1
Oil: Mil-L 23699C
TBO : 3600 hours, 6600 cyklov
The basic warranty (under this, what comes before):
- 1000 h
- 1100 cyklov
- 24 mesiacov
Source:
www.geaviation.cz
http://en.wikipedia.org/wiki/General_Electric_H80
the Aviation and aerospace 2013 / 09, str. 9.
The engine received a certifikáciu FAA 13.03.2012, in októbri 2012 received Russian type osvedčenie, won the aj osvedčenie from európskej EASA, brazílskej and argentínskej the agency of pre civilné the air force.
The engine was certified to drive lietadiel L-410UVP-E20, the Thrush 510G, Technoavia Rysačok and the CAIGA Primus 150.
Type : Turbovrtuľový (Weight Forces)
Dĺžka : 1 670 mm (66")
Height : 580 mm (23")
Width : 560 mm (22")
Dry hmotnosť : 177 kg (390 lb)
Kompresný ratio : 6,7
Fuel: Jet A, Jet A-1
Oil: Mil-L 23699C
TBO : 3600 hours, 6600 cyklov
The basic warranty (under this, what comes before):
- 1000 h
- 1100 cyklov
- 24 mesiacov
Source:
www.geaviation.cz
http://en.wikipedia.org/wiki/General_Electric_H80
the Aviation and aerospace 2013 / 09, str. 9.