I had an interesting phone conversation yesterday afternoon with Phil Lockwood, of Lockwood Aviation, about this project. Just a few tidbits I gathered from the conversation...
- They are planning on releasing a full hardware "kit" to builders for their own installation. Their shop and their labor could be made available for the installation, but that's not being looked at yet, the plan is for owner-install of a FWF kit.
- Half-fuel solo climbs of 1800 fpm are being seen into the upper teens at full power - though the Rotax is time-limited for full power.
- Cruise speeds in the low 190's knots true in the 17k-19k altitudes in normal "go-fast" mode with higher fuel burn, and 10 knots slower in eco mode (LOP).
- Good cooling results with the second iteration of the cowl, but they are going to put the 916 in now and test with that to make sure enough cooling is available for the higher takeoff-rated power of the 916. Both the 915 and 916 are rated for 135 continuous.
- 135hp continuous is available to "about 19,000 feet" according to Phil, at which point it starts to taper off as the turbo is doing everything it can, there ain't nothing left.
- Service ceiling will be FL230 due to high bearing rpm on the turbo.
- They expect to be in production by the end of this year. We did not discuss price - I didn't ask and he didn't volunteer.
- The rudder on the test aircraft is different - some readers here have spotted that it was replaced with not-quite-matching paint, including me. Phil said the rudder was replaced due to damage (not related to testing) and is the exact same design. No control surfaces or empennage surfaces were changed for the increase in Vne (approved by Vans). He told me that Vans approved using the IAS of 182 knots for Vne at altitude as a limiting factor rather than true airspeed. I believe EAA reported 205 ktas (which would be about 147 kias at FL190, depending on temperature) being a limitation, so maybe there is more to this story. This indicates to me (my opinion and zero confirmation) that flutter is not the primary concern for the Vne on the 9/9A model, at least at these expected operating altitudes.
- A dorsal fin was added from the aft end of the canopy slide track (for a slider) back to the vertical stabilizer to improved yaw stability, in order to counter the longer cowl on the nose.