Loss of Control in Flight · NTSB LAX08FA115
CESSNA 150J — Sonora, CA
| Date | April 18, 2008 |
| Location | Sonora, CA |
| Aircraft | CESSNA 150J |
| Purpose of flight | Instructional |
| Conditions | Day · Visual Meteorological Cond |
| Phase / occurrence | Maneuvering Loss of control in flight |
| Pilot age | 56 |
| Pilot total time | 1,500 hrs · Experienced |
| Time in type | 25 hrs |
| Fatalities | 2 |
Probable cause
NTSB findings
- Environmental issues-Physical environment-Terrain-High elevation-Effect on operation - F
- Environmental issues-Conditions/weather/phenomena-Temp/humidity/pressure-High density altitude-Effect on operation - F
- Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained - C
- Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
What happened
A flight instructor and a commercial pilot receiving instruction departed from a pond (at an elevation of approximately 1,100 feet) in the float-equipped airplane. A camera recovered from the wreckage disclosed images indicating that the flight went to a mountain lake where a touch-and-go landing was made. The images indicated that the airplane accomplished this landing with an estimated 10-knot, gusting to 20-knot, headwind. After liftoff from the water, the airplane reversed course toward rising mountainous terrain. The wreckage was located at 5,200-feet, and the terrain in the immediate area of the accident site was level. The airplane came to rest on its nose, with the wreckage evididence indicating a stall/loss of control and vertical descent to the ground. The empennage remained nearly vertical to the terrain and bent down slightly. Both floats were also vertical to the terrain. Postaccident inspection of the airplane found no evidence of any preimpact mechanical discrepancies with the airframe or engine that would have prevented normal operation. The density altitude at the time was estimated as 6,907 feet.