This build log is like a Tarantino movie...out of actual sequence. First thing I did (sometime last fall) was the stab servo, then the retract, then paused a while before moving to the wings where I spent about six weeks off and on, then the rudder pushrod, and finally to the forward fuse area and wiring for the most recent month or so. Now, onward (or back to) the stab.
The servo mounts right beneath the stab, so the linkage is short and direct. The airframe is supplied with two ball joints, one of which is unnecessary if the arrangement is tweaked just a bit. There's all kinds of room in there, so used a Servorahmen bearing frame with an MKS HV747 servo. If I had it to do over again, would have just put in a couple of ply rails and the same HV747R side-mount servo as on the rudder. Simpler for spares, and the bearing frame is probably unnecessary for the stab. But, here we are.
Since the elevator is top-hinged, the actuator rod moves slightly forward with "down" travel. So, the slot in the fin must be cut accordingly, and if the servo is canted to align with the movement plane, the lower linkage ball joint becomes unnecessary. The other consideration, as my pal Mike Smith found out through flight tests with his own ASW-17, is the upper ball joint engaging the actuator rod can move side-to-side if not secured, and thus change the stab trim. Placing a wheel collar on both sides of the ball joint solves this problem, although to be completely effective the actuator rod must be cut to exactly the right length, so as not to move when the stab halves are mounted. Not a big deal and the only negative is the actuator rod hanging out both sides of the fin during transport/storage, unless you want to disassemble every time, which would be a complete PITA as the rudder has to come off as well.
Consideration must also be given to the tail wheel, situated directly beneath the servo. The servo wiring and pitot tube plumbing pass through the area.
The servo mounts right beneath the stab, so the linkage is short and direct. The airframe is supplied with two ball joints, one of which is unnecessary if the arrangement is tweaked just a bit. There's all kinds of room in there, so used a Servorahmen bearing frame with an MKS HV747 servo. If I had it to do over again, would have just put in a couple of ply rails and the same HV747R side-mount servo as on the rudder. Simpler for spares, and the bearing frame is probably unnecessary for the stab. But, here we are.
Since the elevator is top-hinged, the actuator rod moves slightly forward with "down" travel. So, the slot in the fin must be cut accordingly, and if the servo is canted to align with the movement plane, the lower linkage ball joint becomes unnecessary. The other consideration, as my pal Mike Smith found out through flight tests with his own ASW-17, is the upper ball joint engaging the actuator rod can move side-to-side if not secured, and thus change the stab trim. Placing a wheel collar on both sides of the ball joint solves this problem, although to be completely effective the actuator rod must be cut to exactly the right length, so as not to move when the stab halves are mounted. Not a big deal and the only negative is the actuator rod hanging out both sides of the fin during transport/storage, unless you want to disassemble every time, which would be a complete PITA as the rudder has to come off as well.
Consideration must also be given to the tail wheel, situated directly beneath the servo. The servo wiring and pitot tube plumbing pass through the area.
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