ENGINES:
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BRP ROTAX 2-Stroke Ultralight Engines
non certified !
| Engine Type |
| 582 UL DCDI, 65 HP |
Options for 2-Stroke Ultralight Engines
| Options |
| Exhaust for 582 |
| Electric Starter |
| Oil Pump |
| Gearbox B (i=2,58) for 447, 503, 582 |
| Gearbox C (i=2,62/3,0/3,47/4,0) for 503, 582 |
| Gearbox E with electric starter integrated (i=2,62/3,0/3,47/4,0) |
BRP ROTAX 4-Stroke Ultralight Engines
non certified !
| Engine Type |
| 912 UL-2, 85 HP suitable for fixed pitch propeller |
| 912 UL-3, 85 HP suitable for constant speed propeller |
| 912 ULS-2, 100 HP suitable for fixed pitch propeller |
| 912 ULS-3, 100 HP suitable for constant speed propeller |
| 912 iS, 100 HP injected suitable for fixed pitch propeller |
| 914 UL-2, 115 HP turbocharged suitable for fixed pitch propeller |
| 914 UL-3, 115 HP turbocharged suitable for constant speed propeller |
Options for 4-Stroke Ultralight Engines
| Options |
| 912/914 Drive for Cavuum Pump |
| 912/914 Mechanical Tachometer Pick-Up |
| 912/914 Air Guide Buffle |
| 912/914 Electric Starter high duty |
| 912 Fuel Pump Set with threaded fittings and stainless fuel lines |
| 912/914 Screw Connection for Oil Pump |
| 912 Airbox for Preheating with Fittings |
| 912/914 Engine Truss Assembly |
| 912/914 Engine Shock Mount Set |
BRP ROTAX 4-Stroke Aircraft Engines
JAA/FAA certified !
| Engine Type |
| 912 A-2 suitable for fixed pitch propeller |
| 912 A-3 suitable for constant speed propeller |
| 912 F-2 suitable for fixed pitch propeller |
| 912 F-3 suitable for constant speed propeller |
| 914 F-2 suitable for fixed pitch propeller |
| 914 F-2 suitable for constant speed propeller |
Options for 4-Stroke Aircraft Engines
| Options |
| 912/914 Drive for Cavuum Pump |
| 912/914 Mechanical Tachometer Pick-Up |
| 912/914 Air Guide Buffle |
| 912/914 Electric Starter high duty |
| 912/914 Screw Connection for Oil Pump |
| 912 Airbox for Preheating with Fittings |
| 912/914 Engine Truss Assembly |
| 912/914 Shock Mount Set |
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First posted: December 1993 Last Revision: September 2009 |
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Copyright © 2003 AirConsult Aviation Ltd. - All rights reserved |