Thu Jul 01, 2010 10:07 am
Coyote Ugly hit the nail on the head. Put a set of big tires on an airplane, and the airplane is very apt to go places it would never have gone before.
Also, remember that MASS is largely what counts here as well. So, even on takeoff from a smooth surface, the gear rebounds. Hang more mass out there, and you get more rebound force. Now, do the same thing in an off airport, rough environment, and the forces can be huge, both in extension and in rebound.
Now, put a set of skis on that airplane, or better yet a set of retractable wheel skis, which weigh well over 60 pounds a side. And, take that plane into some rough snow conditions.
An example is the rebound forces in the Husky gear. Aviat built a longer gear to adapt the wheel skis, and the combination of ski weight and a slightly longer arm started bending cabanes, not in extension (impact) but in rebound.
The failure mode in Cessnas that the FAA is describing here has been known by the FAA for decades. I know of at least one VERY conciencious commercial operator who had a failure of this type on a 185. That plane got worked hard on big tires and skis. The operator had the gear legs tested annually, but they still broke.
As others have noted, pilots tend to be pretty hard on these things, even without the additional mass out there, but adding a lot of mass on the end of those spindly little legs DOES increase the forces involved.
Fortunately, at least so far, the FAA hasn't decided to go with an AD requiring NDT of the gear every year. THAT would be a MAJOR PITA, and I doubt it would alleviate the problem in any case.
By the way, the failure point here is between the bolt holes that hold the axle to the gear leg. They crack between bolt holes. It's not real common, but as someone also noted, these gear legs are pretty darn old in general, and have been subjected to a LOT of stress.
MTV