Flap Hinge Mounts: Tack Weld At First

Source: 1999 Beartracks, Bob Barrows

Refer to drawing #13. When making the flap hinge mounts it is best to just tack weld the pieces together first and not finish weld until the wing is finished and the flaps are in place. This will allow you to cut the tack welds and realign the hinge mounts if needed in order to achieve the best fit up between the flaps and wing. Once the fits are established then remove the fittings from the wing and finish welding.


Flap hinge mount as removed from welding jig, tack welded together only!

Engineering Notice Concerning Flap and Aileron Nose Skin Rivet Size (395 and Below)

Source: 1999 Beartracks, Bob Barrows

Reference plans number 395 and below, Drawings #9 and #10. The 3/32" stainless steel pull rivets holding the nose skins to the nose ribs have been changed to 1/8" aluminum pull rivets. The cost and availability of 3/32" S.S. rivets has become a problem. If you have already assembled the ailerons and flaps with the S.S. you can leave them in, they do a good job.

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1998 Wing Strut Material Update

Source: 1998 Beartracks, Bob Barrows

As mentioned in past issues of the newsletter, we have been involved in obtaining new strut material for use on your BEARHAWK project. This endeavor was initiated due to many builders request.

We have designed and purchased an extrusion die so as to produce the strut shown.

The struts are made from aluminum alloy 6061-T6 and heat treated per. spec. Our supplier has provided us with chemical and mechanical certifications for each lot ordered.

We have also designed new aluminum strut end fittings that can be bolted to the strut material. We can supply this NEW strut material and the drawings for the end fittings for shipment inside and outside the U.S.A. Contact R&B Aircraft for details.

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1998 Inboard Flap Lever Engineering Notice (280 and below)

Source: 1998 Beartracks, Bob Barrows

Reference drawings #12 and #14 for plans serial numbers 280 or below.

Inboard Flap Lever

The inboard flap lever arm was shortened from 4-1/8" to 4" for clearance with the aileron cable. If you have completed this assembly you may remove up to 1/16" from the tip of the flap lever arm for clearance.

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