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Positive Control Check

By Pia Bergqvist / Published: Aug 03, 2012
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There are some in-flight failures that are extremely difficult, if not impossible, to recover from. One such malfunction is the failure of a major control surface. A positive control check is part of the preflight procedures section of the practical test standards for gliders since they are often assembled right before the flight. While a positive control check may not be warranted for each flight in certified airplanes, it’s definitely worth doing every time there has been any type of maintenance done to the airplane or if you’re flying an airplane that is not yours.

Two people are required to conduct a positive control check. One person moves around the outside of the airplane and stops at each control surface to hold it steady while the person inside the cockpit moves the control actuator that manipulates that particular surface. Make sure that the actuator won’t move when pressure is applied while the person outside holds the control surface steady. Also, when the person outside relieves the pressure (still holding for resistance), check that the control surface moves in the appropriate direction with each control input. This ensures that all the linkages are properly connected before you start taxiing out for departure.

You may think this check can be completed in the runup area as part of the control check during the runup. But the runup control check is not fail-proof. A pilot who flew a Piper Cub that was assembled on site at this year’s AirVenture was forced to climb from the rear seat to the front seat to move the CG forward enough to level off his airplane after he realized that his control stick wouldn’t move the elevator down. Only the linkage that brought the elevator up was connected. He performed a control check in the runup area, but didn’t realize gravity brought the elevator down – not the control stick. Fortunately he landed safely in the end, but the type of CG manipulation the pilot accomplished would be impossible in most airplanes and such a control failure would generally not have a happy outcome.

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RHalstead's picture

Weight shift and trim control can save your bacon in quite a few smaller planes and particularly in the 150 and even 172. You can even land a Bonanza using trim, but it takes practice and presence of mind.

For me flying a Bo/Debonair has always included a positive control check of moving the control surfaces during the walk around and watching the yoke movement as I did so. I could see the yoke movement from every control surface and watching the elevator trim tab movement as I moved the elevator let me know if it was hooked up and working. That was a small tab, but sure had a lot of power. As the Deb and Bo have interconnected ailerons and rudder, moving the rudder will at least show some movement in the yoke and with those big windows you can still see from back there although you might have to lean to the side a bit.

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