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 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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Safety Update 2015-1: Flap and Aileron Hinge Pocket Cover Plates

ENGINEERING CHANGE NOTICE
Subject: Flap and Aileron Hinge Pocket Cover Plates
Applies to any of the Bearhawk types that have the covers installed.
Recently a Bearhawk 4-place had a flap retraction problem on one flap because the pocket cover plate jammed into the top wing skin, and would not allow the flap to retract. The plane was still flyable, but this problem needs to be addressed.
FLAPS: On the top of the flaps the cover plate should only be deep enough to cover the gap from the flap spar to the back of the wing skin, about 1 ¼ inches, with the flap up.
AILERONS: On the aileron the cover needs to be much deeper, so that with full down aileron, the front of the cover is still under the wing skin.

15q3zbAdditional information:
Bearhawk builder Jonathan Battson experienced a case where his flap hinge pocket cover got stuck under the upper wing skin when he attempted to retract the flaps after takeoff, causing one flap to stay extended at the third notch. He writes “The jam did considerable cosmetic damage to the top skin of the wing. It was the pocket where the skins join which jammed, to the combined thickness of the two sheets of 0.025″ Aluminum, plus stiffener section.”
Jonathan also adds:
“The Bearhawk can easily be controlled with 1 flap fully deployed and the other fully retracted, even as fast as 75 KIAS. The control inputs necessary to remain straight and level (or climbing at full power), are only marginally out of balance – just enough that you would certainly notice something is wrong. You most definitely are not fighting for aileron authority, as many would have you believe, all that is required is just a little rudder and a little opposite aileron to continue in balanced flight.”