euroastar350
14th Nov 2010, 07:09
To anyone that operates any of the types in the subject line, I have a few questions:
1.) what is the maximum deflection of the tail rotor blades when either pedal is depressed? I couldn't find this info in the RFM or MM.
2.) when collective is raised fully (engines off), what is the maximum angle of the rotor blades?
3.) Are there any drawings/photo material on the float system?
The reasons I ask these questions and need the material for the floats is that I am making an authentic replica of the B222 series, including the 230 and 430 for Microsoft Flight Simulator 2004/FSX. Here are a couple shots, 1 of the bird in FSX and the other of the newly designed tail rotor:ok:
http://farm5.static.flickr.com/4012/5168451097_2d8f138753_b.jpg
http://farm2.static.flickr.com/1356/5168446889_6a28902b02_b.jpg
Any help is truly appreciated.
1.) what is the maximum deflection of the tail rotor blades when either pedal is depressed? I couldn't find this info in the RFM or MM.
2.) when collective is raised fully (engines off), what is the maximum angle of the rotor blades?
3.) Are there any drawings/photo material on the float system?
The reasons I ask these questions and need the material for the floats is that I am making an authentic replica of the B222 series, including the 230 and 430 for Microsoft Flight Simulator 2004/FSX. Here are a couple shots, 1 of the bird in FSX and the other of the newly designed tail rotor:ok:
http://farm5.static.flickr.com/4012/5168451097_2d8f138753_b.jpg
http://farm2.static.flickr.com/1356/5168446889_6a28902b02_b.jpg
Any help is truly appreciated.