I guess I'll go with electrical flaps.
I started making left flap pushrod hole in fuselage. Fits in flap up position.
Is there any reason I should not move the F-445 blocks and actuator as far aft as possible (beyond the 22 1/4" specified in the plans)?
By "as far aft as possible" I mean until the motor end of the flap actuator weldment hits the bulkhead behind it when the arms are in the full up position.
Seems that it would it put the pushrods at less of an angle and make the forward forward slots in the bottom skin/flange less long -- less fuselage skin cutouts?
Finn
I started making left flap pushrod hole in fuselage. Fits in flap up position.
Is there any reason I should not move the F-445 blocks and actuator as far aft as possible (beyond the 22 1/4" specified in the plans)?
By "as far aft as possible" I mean until the motor end of the flap actuator weldment hits the bulkhead behind it when the arms are in the full up position.
Seems that it would it put the pushrods at less of an angle and make the forward forward slots in the bottom skin/flange less long -- less fuselage skin cutouts?
Finn