![]() ![]() Rationale - The Model 40 was a one-off, minimum-change variant of the Bonanza.Merge Beechcraft Model 40 → Beechcraft Bonanza (See Wikipedia:Merging and moving pages for details on performing mergers.) No prejudice to restoring the article if more information, such specs, is forthcoming, thoush discussion first would be good. A summary of the conclusions reached follows. Subsequent comments should be made in a new section. In the landing phase the bungee system must be over-ridden by the pilot when making a cross-wind landing and cross-control inputs are required to keep the airplane aligned with the runway centerline without drifting left or right. On takeoff increased right-foot pressure is still required to overcome torque and P-factor. This system is most useful in cruise flight. It allows the pilot to make coordinated turns with his feet on the floor using the yoke alone. ![]() The rudder/aileron interconnect is a flexible bungee which can be over-ridden by the pilot by use of control input. NOTABLE THAT THE PRESS IN THE WORLD DID NOT AGREE WITH ANY OF THIS RE TYPE OF AIRCRAFT AND RESULTANT CAUSE/ES. ![]() The above mentioned problems in yaw accuracy were simply accepted in that aircraft, and it was engineered towarded that purpose, and with much lower performance than the Bonanza. Think of the bungee interconnect system as "power assist" for the rudders and ailerons and you'd be close.Ĭontrast the Bonanza's system with the true mechanical interconnect on the Ercoupe, which from the factory had no rudder pedals. Indeed, such as system would be nigh impossible, because the amount of rudder necessary is different depending on aircraft attitude, speed and the amount of power the engine is developing. The aileron and rudder systems are interconnected by bungees, as opposed to a mechanical system deflecting aileron and rudder in exactly correct increments. The commentary about the interconnect is misleading. ![]()
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