Landing / Ground Loss of Control · NTSB CEN15FA119
CESSNA 182L — Owen, WI
| Date | January 26, 2015 |
| Location | Owen, WI |
| Aircraft | CESSNA 182L |
| Purpose of flight | Personal |
| Conditions | Day · Instrument Meteorological Cond |
| Phase / occurrence | Landing-flare/touchdown Collision with terr/obj (non-CFIT) |
| Pilot age | 27 |
| Pilot total time | 1,874 hrs · Experienced |
| Time in type | 65 hrs |
| Fatalities | 1, 1 serious |
Probable cause
NTSB findings
- Aircraft-Aircraft oper/perf/capability-Aircraft capability-(general)-Capability exceeded
- Personnel issues-Task performance-Planning/preparation-Weather planning-Instructor/check pilot - C
What happened
The accident occurred on the third leg of a multi-leg cross-county trip that the flight instructor and the student pilot were making to relocate the airplane, which the student pilot had recently purchased. The flight instructor stated that, before beginning the flight, he obtained a weather briefing indicating icing conditions along the route of flight, but he thought they would be able to get above the weather. Although the airplane was not certified or equipped to fly into icing conditions, the flight instructor elected to initiate the flight. While en route, the airplane accumulated airframe ice despite the flight instructor making several altitude changes in an attempt to reach warmer temperatures. The airplane eventually accumulated enough ice that it was no longer capable of maintaining altitude, which resulted in the flight instructor making an off-airport emergency landing on a country road. The airplane's windshield was iced over restricting the pilot's forward visibility, and during the landing roll, the airplane contacted trees. A postaccident examination of the airplane at the accident site revealed the presence of rime ice on the top and bottom wing surfaces. Additionally, several pieces of concave-shaped ice ranging from 1.5-inches- to 7-inches-long and from 1.5-inches- to 2-inches-wide were located around the accident site. An examination of the airframe and engine did not reveal any anomalies that would have prevented normal operation.