Accident Probes

the fact sheet suggests. Finally

According to the pilot, he was delayed about 10 minutes by traffic before completing the engine run-up and takeoff roll with no anomalies noted. After the pilot lifted off and retracted the landing gear, the engine stopped producing power about 300 feet above the runway. There was no time to perform remedial actions to restore power, so the pilot lowered the landing gear and touched down on the remaining runway. The airplane went off the departure end of the runway, down an embankment and across a road before coming to rest upright 384 feet beyond the runways departure end in low brush.

After a brake master cylinder was installed, the technician was unable to bleed the brake system. Fluid pulled from reservoir would return to reservoir through the same line as the internal bypass was not functioning properly. Master cylinder was disassembled and bypass was found stuck and unable to move. Metal shavings were found inside, and an O-ring was torn, with black specks mixed in with the shavings. Part replaced with new master cylinder.

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• Checkride Paperwork
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UDRI’s test was conducted “at a higher speed than the combined maximum speed of the drone and airplane

My airplane has wingtip-mounted fuel tanks, installed under a supplemental type certificate (STC). In many ways, theyve transformed and improved the machine by adding greater loading flexibility, thanks in part to a gross-weight increase. What drag they produce isnt noticeable, and the additional endurance means the airplane is faster over some trips than it was before. For many of my destinations, I can depart with full tanks, fly to my destination, shoot an approach, miss it and fly home with reserves.

The pilot reported that he and his co-owner had flown the airplane the night before the accident; it flew normally without problems. On the morning of the accident, he had to use the low-pressure boost pump to start the engine, but the pre-takeoff run-up was normal. The airplane ised most of the 4201-foot-long runway before becoming airborne. On reaching about 500 feet agl, the pilot determined the engine was not producing full power. He turned on the low-pressure boost pump and climbed to 1000 feet agl before turning back to the airport. The engine continued losing power, so he conducted a forced landing to a cornfield. A witness reported observing dark exhaust trailing the airplane during the takeoff.

I started my lessons (at 50 years old!) at an airport called Howell-New Lenox in Illinois. On my first solo, I had to go around due to a back taxi by another student with his instructor (my first exposure to being PIC in a two-pilot operation. But I was cool; I also learned that I was pretty calm in an abnormal situation-when Im alone.

Ive owned Cessna T210s since 1977; first a 1969 J model and then a 1979 N model with a TSIO-520-R engine. In the 1980s, there were a number of fuel exhaustion accidents in 210s, all of them attributable to not getting a full fill and resulting in being shorted an hours supply when fueling stops after fuel backs up out of the filler port. The outboard sections of the fuel tanks are slightly higher than the bottom of the filler port. To get the last one-plus gallons in the tanks requires the slowest of fueling until reaching the real full point.

During descent, pilot noted oil streaking back from top engine cowl louvers, then dropping oil pressure. Pilot conducted precautionary shutdown and feathered propeller. Pilot continued descent and landed at destination without issue. Maintenance removed cowling and found oil appearing to come from the turbocharger (p/n 4066109025) area. Further investigation revealed oil bypassing the seals on the turbo.