Grum.Man
En-Route
The Venture is nothing like that thankfully. It's praised as an excellent ifr platform with great stability.
The Venture is nothing like that thankfully. It's praised as an excellent ifr platform with great stability.
Get back to us when you can compare horizontal tail volume of a small-tail Lancair to that of a Venture. I've seen no data that suggests the Venture is anywhere close to neutral stability in the flight envelope. The Lancair is quite the opposite.Actually the Lancair probably handles better. Short couple tails have some nasty characteristics.
Great read. Makes it sound like one hell of an airplane!
http://s121.photobucket.com/user/kr...D-4ADB-8971-A44E2ECB606A_zps4mcsocuc.jpg.html
Dad and the owner reunited and working to remove the elevator for transport.
Late to the thread. That must be your Dad supervising (in the middle) ?
Interesting panel layout
Dang is that thing Japan registered? Everything on the wrong side.
Small plane with big engine means sitting on the right for better balance.
Sorry, don't understand that?
Big engine 'P' factor will be about the yaw axis, so seemingly indifferent as to whether one is left or right of the longitudinal centerline. What am I not understanding here please? Less right rudder at TO power?
Torque is about the longitudinal axis, so extra weight on the right side (assuming conventional turning prop) will tend to balance it somewhat.
Sorry, don't understand that?
Big engine 'P' factor will be about the yaw axis, so seemingly indifferent as to whether one is left or right of the longitudinal centerline. What am I not understanding here please? Less right rudder at TO power?
I was waiting for that. In addition to what was mentioned above you have to know the design of the airplane. The nose gear is mounted to the engine. The engine is mounted to the airframe with rubber mounts. Due to the narrow gear any application of power really torques the airplane and drags the nose to the left. The original steering system was to utilize differential braking and there is almost 0 caster on the nose strut. Early models with left hand seating struggled to maneuver in just the right circumstances of power wind and ground slope.
This one has a modified steering system to help overcome that but it still tracks hard left while taxing with a right cross wind or when having to go up hill.
The nose gear is mounted to the engine. The engine is mounted to the airframe with rubber mounts. .
Differential braking and almost zero caster on the nose gear sounds like an interesting combination, regardless of wind or power setting. I assume that was to keep the gear design simple while ensuring the nose gear was centred on retraction (something the GA Grumman's with their fixed gear, free-castoring nosewheels didn't have to deal with)?
Wow - fast little machine! What would be typical cruise speed and fuel burn on a 500 mile trip?