On Sunday, our new Bearhawk Model 5 took to the skies. Built by Collin Campbell and test flown by Rollie van Dorn.
Some basic specs on this new model. The fuselage is 2" wider than the Bearhawk 4 and uses a C182 windshield (instead of C170). The fuselage is also 9" longer than the Bearhawk 4. The wing is the standard Model B wing with no changes. Bob believes this wing to be a 3,000 lb gross wing.
Engine is a 315 HP Lycoming IO580. Prop is the 3 blade Trailblazer I have used on my 4 place. Projected gross weight of 3,000 lbs. I say "projected" because the flight testing is not finished. Both the final gross weight and fore and aft CG limits are still not 100% determined. We have some idea where these specs will end up but it needs to be confirmed by flight testing.
The plane has close to 4 hours on it after a few days of testing flying, Performance - Rollie was flying final at 60 mph with a little power. He said the plane handled really well with quite light control forces. He said it flies like my 4 place which has very light controls. Rollie had no trouble getting it down and stopped before the mid point (big mud pond after rains) of Collin's 1350 ft runway. Rollie saw a 156 mph TAS at 3,500 ft running 24/2400 - about 72% power I think. For sure higher cruise speeds will happen up at 6,500 -7,000 ft where the sweet spot is for best cruise numbers. 18 GPH on that thirsty engine.
Empty weight was very surprising for everyone. With a heavy angle valve cylinder injected engine and around 15 lbs more tubing weight for the bigger fuselage - I was hoping for a weight less than 1600 lbs. But I thought 1625 or more was likely. Bob was hoping for under 1600 lbs. It came out at 1512 lbs. We were all very happy.
This Model 5 can not use the 4 cylinder engines. The smallest engine that can be used is the Lycoming 540 with parallel valve cylinders. But it was really designed for the 300 HP IO540 with angle valve cylinders. Lycoming made me a great deal on this IO580 which is why it is on the plane instead of a Bob Barrows IO540 of 300 HP. Bob designed an innovative alternate air system which has not really been tested yet.
The brakes will not hold it above 1700 RPM when it starts skipping across the ground. With that big engine and the take off thrust of the Hartzell Trailblazer - it gets with the program quickly on take off and climb out. 0410201250a reduced.jpgModel 5 side view reduced.jpgRollie with Model 5 reduced.jpg
They are beginning work on the tooling for the kit for this one at the kit factory. This is just a heads up about the plane first here on this forum for the "Bearhawk Community".. More details will follow as more test flying is done. Thanks to Collin for building a beautiful plane, and thanks to Rollie for volunteering to do the test flying. They are both outstanding members of the BH community that contribute a lot. Mark
Some basic specs on this new model. The fuselage is 2" wider than the Bearhawk 4 and uses a C182 windshield (instead of C170). The fuselage is also 9" longer than the Bearhawk 4. The wing is the standard Model B wing with no changes. Bob believes this wing to be a 3,000 lb gross wing.
Engine is a 315 HP Lycoming IO580. Prop is the 3 blade Trailblazer I have used on my 4 place. Projected gross weight of 3,000 lbs. I say "projected" because the flight testing is not finished. Both the final gross weight and fore and aft CG limits are still not 100% determined. We have some idea where these specs will end up but it needs to be confirmed by flight testing.
The plane has close to 4 hours on it after a few days of testing flying, Performance - Rollie was flying final at 60 mph with a little power. He said the plane handled really well with quite light control forces. He said it flies like my 4 place which has very light controls. Rollie had no trouble getting it down and stopped before the mid point (big mud pond after rains) of Collin's 1350 ft runway. Rollie saw a 156 mph TAS at 3,500 ft running 24/2400 - about 72% power I think. For sure higher cruise speeds will happen up at 6,500 -7,000 ft where the sweet spot is for best cruise numbers. 18 GPH on that thirsty engine.
Empty weight was very surprising for everyone. With a heavy angle valve cylinder injected engine and around 15 lbs more tubing weight for the bigger fuselage - I was hoping for a weight less than 1600 lbs. But I thought 1625 or more was likely. Bob was hoping for under 1600 lbs. It came out at 1512 lbs. We were all very happy.
This Model 5 can not use the 4 cylinder engines. The smallest engine that can be used is the Lycoming 540 with parallel valve cylinders. But it was really designed for the 300 HP IO540 with angle valve cylinders. Lycoming made me a great deal on this IO580 which is why it is on the plane instead of a Bob Barrows IO540 of 300 HP. Bob designed an innovative alternate air system which has not really been tested yet.
The brakes will not hold it above 1700 RPM when it starts skipping across the ground. With that big engine and the take off thrust of the Hartzell Trailblazer - it gets with the program quickly on take off and climb out. 0410201250a reduced.jpgModel 5 side view reduced.jpgRollie with Model 5 reduced.jpg
They are beginning work on the tooling for the kit for this one at the kit factory. This is just a heads up about the plane first here on this forum for the "Bearhawk Community".. More details will follow as more test flying is done. Thanks to Collin for building a beautiful plane, and thanks to Rollie for volunteering to do the test flying. They are both outstanding members of the BH community that contribute a lot. Mark
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