Instrument Check

We were in IMC at 4000 feet, on a vector for the VOR-A approach at the Wichita, Kan., Colonel James Jabara Airport. The airplane was an A36 Bonanza and I was in the instructors seat on the last approach of a day-long training session. This was in the era before GPS, long before iPads and moving-map handhelds, and the owner of this then-well-equipped 36 had ignored the short-lived Loran phase. So we were eastbound on a long downwind, and crabbing into a northerly wind before intercepting the westbound final approach course before circling to Jabaras north/south runway.

Many of todays workplaces seek to create a formalized safety culture, an environment where employees practice behaviors that minimize accidents, look out for their co-workers and where reporting unsafe conditions is encouraged, not subject to retaliation, and frequently rewarded. It can be a great goal, but it often creates an exaggerated sense of safety where people need safety training to use a power strip and posters about how to get out of a car without tripping. The goal of creating a safety culture often ends up a corporate farce, since the best safety cultures are not created by artifice, but happen naturally because people really care.

The pilot later stated he selected the landing gear handle to the down position, but the main landing gear did not lock in the extended position. He then selected the landing gear handle up, but the landing gear did not retract. After maneuvering away from the airport, an attempt to pump down the gear with the emergency hand pump was unsuccessful. An airframe-mounted mirror indicated the left landing gear was down. During the landing, the right main landing gear collapsed and the airplane veered to the right and departed the runway surface, coming to rest on the parallel taxiway.

The landing was normal, and I took a close look at the left landing gear after shutting down but couldnt find anything amiss. The tire and wheel looked good, and there was no hydraulic fluid seeping from the strut. The brake was secure and had tested fine on the landing, and when taxiing in. There was no damage to the wing, the landing gear door or any other part of the airplane. Not finding anything wrong with the airplane I forgot about it, wondering if I had imagined it. Ultimately, I figured Id hit a dog with the landing gear and, sadly, someone had lost their pet.

During a scheduled inspection, technicians encountered corroded and bent control yoke boss attachment hardware that proved difficult to remove. After consulting with the manufacturer, the final recommendation was to remove the boss via cutting the bolts (p/n 2315152-33). Manufacturer was able to repair the yoke assembly using SB 31-27-11 and kit 2381602-801. Aircraft had been parked outside without gust locks.

Recent, similar efforts involving the FAA and the GA community are picking up in tempo. Youve already seen some of the institutional changes: relaxed certification standards for installing advisory angle-of-attack indicators and the new rash of all-electronic attitude indicators, among others, which are designed to help minimize the classic loss-of-control inflight accident. These and other outcomes may be producing tangible results, but its too early to be sure. Regardless, by using a data-driven approach and producing specific safety enhancements, these efforts are creating some useful outcomes for GA pilots. The way this came to be is an example of why you never want to see sausage made.

Beech Model 65 Queen AirFailed Gear Limit SwitchLanding gear limit switch (p/n MS250261) failed to stop motor during retraction, causing landing gear circuit breaker to pop. Aircraft landed without incident. Re-rigged the switch IAW maintenance manual. Retraction test and ops check okay.Part total time: Unknown

1) A Piper PA-32R-300 Lance attempted to take off from a 3200-foot-long grass runway on a June morning with flaps retracted. It lifted off at the end of the runway, then descended into a shallow valley, touched down and lifted off a second time, before settling back to the ground and colliding with a barbed-wire fence. It was later determined to have been 188 pounds over its maximum gross weight with its center of gravity 0.15 inches aft of limits. Density altitude was about 1800 feet above field elevation.

It was a warm, blustery late-spring day in Texas. Visibility was restricted by the haze, and the afternoons updrafts were in full bloom. The whole package made the air hot, bumpy and thick. I had a multi-engine checkride scheduled in a few days, so my instructor and I were aloft in the Piper Seneca I that Id been using and were up to no good, trying to buff out the rough spots. This was for a commercial multi-engine checkride and emphasized instrument work.

My flight instructor also lives in an airpark development, about 40 nm away, an easy hop. When we fly together, I generally taxi directly to her home. Past palm and pine trees, mailboxes, fences and…well, you get the idea. (Her trash gets collected on Fridays.) So Im no stranger to ground operations in close quarters. It could be said that I dont really know what to do with all the expansive, unobstructed pavement available for taxiing at real airports. Thats not to say Ill never taxi into something; thats always a risk.