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RCSD-2012-11 - RC Soaring Digest

RCSD-2012-11 - RC Soaring Digest

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Supplied flap and aileron horns. Two of these escaped during<br />

shipping. Probably would work just fine, but I elected to make<br />

the replacements a bit larger for more substantial attachment.<br />

Final parts ready for installation.<br />

any of the typical aileron servos will fit.<br />

But if you wish to substitute flat covers<br />

you have very little space to work with.<br />

The inside height of the bay is about<br />

15/32" at the forward edge and only<br />

5/16" at the aft edge. Space is of course<br />

more generous in the flap servo bay,<br />

with 13/32" of height at the aft edge.<br />

Airtronics 94761’s fit nicely there.<br />

Unlike most composite sailplanes these<br />

days the ailerons are top hinged and<br />

intended to be driven with an external<br />

linkage. It may be possible to run the<br />

linkage inside but I used the stock setup<br />

and covers. Flaps are bottom hinged.<br />

The wipers are some of the best I’ve<br />

seen with very tight tolerances to the skin<br />

with no interference. Hinge movement is<br />

very good with plenty of range of motion<br />

and no binding at all.<br />

Two fuselages were supplied with the<br />

review package, for F3B and F3F. The<br />

F3B fuselage is very small in cross<br />

section and sets the wing at a positive<br />

angle of incidence. The F3F fuselage<br />

appears to have zero-zero incidence<br />

settings and is sized about 1/10" taller<br />

and wider in order to accommodate<br />

the ballast tube. Only one servo tray<br />

and harness were supplied. We did not<br />

build out the F3F fuselage as of the time<br />

of publication, though other than the<br />

differences noted above it is identical.<br />

The large cross section carbon wing<br />

joiner is typical for a two piece wing. It’s<br />

hollow, with two spaces on each end<br />

that can be used for ballast. It may not<br />

have much practical effect but the depth<br />

of the cavities on the subject joiner vary<br />

by about an inch left to right. Additional<br />

ballast cavities are molded into the wing<br />

roots. It should be possible to tailor the<br />

ballast to load it up without changing the<br />

CG. By my rough calculation there is a<br />

little less than 9 cubic inches of volume<br />

total in all cavities which would give a<br />

maximum possible capacity of about 43<br />

ounces of brass or 59 ounces of lead.<br />

Tailoring for CG will likely reduce the<br />

maximum possible weight.<br />

The wing skins are not pre-cut for flap<br />

pushrod exits or for horn installation.<br />

Supplied horns are glass and seem<br />

rather small for secure attachment.<br />

Two of them were lost in shipment,<br />

however, so I had no choice but to<br />

fabricate new ones. The hardware was<br />

packaged in thin, fragile plastic bags<br />

which had broken open, and the box was<br />

constructed so that small parts could<br />

44 R/C <strong>Soaring</strong> <strong>Digest</strong>

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