Cessna R172K N758DH

Summary

On 21 June 2008 at about 17:15 local time, a Cessna R172K registered N758DH, operated by Harold D. Patterson, was involved in an accident near Big Bear City, California, United States. 2 people were on board and nobody was injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

Date

21 June 2008 at 17:15

Classification

Accident

Location

Big Bear City, California, United States

Nearest airport

Big Bear City Airport (L35)

Coordinates

34.2625, -116.8697

Aircraft

Cessna R172K

Registration

N758DH

Category

Airplane

Engines

1

Operator

Harold D. Patterson

Operating rule

Part 91: General Aviation

Purpose of flight

Personal

Phase of flight

Not recorded

Route

Big Bear → San Diego

Aircraft damage

Substantial

Weather

VMC

Light

Day

NTSB number

LAX08LA187

Nobody was injured.

The pilot's failure to attain and maintain an adequate airspeed that led to a stall/mush. Contributing to the accident was the lack of suitable terrain for an off airport landing and a high density altitude.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The pilot reported that after a longer-than-normal takeoff roll, the airplane lifted off the runway with a climb rate of about 300 to 400 feet per minute. As the airplane passed the end of the runway, climb performance suddenly decreased and the airplane started to descend. The pilot verified the throttle and propeller control positions, advanced the mixture to full rich, and applied 20 degrees of flaps as the airplane continued to descend. The pilot stated that due to trees and residential structures within the immediate area, he decided to initiate a controlled landing in a lake as close to the shoreline as possible. Subsequently, the pilot landed the airplane tail first in the water, resulting in substantial damage to both wings. The pilot did not report any mechanical anomalies with the engine or airframe. He added that at the time of the accident, the airplane was about 190 pounds under the maximum gross weight. The density altitude was calculated to be 9,100 feet mean sea level and the pressure altitude was claculated as 6,328 feet msl. Using the calculated pressure altitude, density altitude, aircraft's maximum gross weight, and reported weather conditions, a representative from the airframe manufacturer calculated that the airplane should have attained a climb rate of approximately 500 feet per minute at the time of the accident.

Quoted verbatim from the NTSB record.