2040 servos do NOT go at the tail.! 3121 the main spar goes at THIRTY PERCENT of chord. the main spar should be Contiguous and should SPAN the width of the fuselage.! 3200 the design of a dihedral wing should include a CENTER section and dihedral BRACE. 3308 aileron servos should be located forward-of thirty percent of chord and as far inboard as is practical.
0544 where a pusher thrust system is used, THE PARTS of the model located in front of the prop BLOCK air flow to the prop.! design of the fuselage should, therefore, be INFORMED by this fact.!
0015 servos do NOT go at the tail.!!!!!! ailerons and elevator Should Extend to the wingtips/stab tips. 0026 the nose SHOULD be tapered/contoured in BOTH axes.!!! it is not recommended that the rudder/elevator be Directly in the prop wash.! googletranslate
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2040 servos do NOT go at the tail.!
3121 the main spar goes at THIRTY PERCENT of chord. the main spar should be Contiguous and should SPAN the width of the fuselage.!
3200 the design of a dihedral wing should include a CENTER section and dihedral BRACE.
3308 aileron servos should be located forward-of thirty percent of chord and as far inboard as is practical.
0544 where a pusher thrust system is used, THE PARTS of the model located in front of the prop BLOCK air flow to the prop.! design of the fuselage should, therefore, be INFORMED by this fact.!
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3356 aileron control horns have NOT been correctly installed.
3608 main landing gear not correctly located.
0015 servos do NOT go at the tail.!!!!!! ailerons and elevator Should Extend to the wingtips/stab tips.
0026 the nose SHOULD be tapered/contoured in BOTH axes.!!! it is not recommended that the rudder/elevator be Directly in the prop wash.! googletranslate
an aircraft that has a propulsion system is NOT a glider.!