No fatalities

21 Aug 2013: CESSNA 180J (N7807K) — Kenneth W Castner III — Palmer, AK

Palmer, AK, United States

On 21 Aug 2013, a CESSNA 180J (registration N7807K) operated by Kenneth W Castner III was involved in an aviation accident near Palmer, AK. No fatalities were reported. Investigators recorded the probable cause as: The pilot’s failure to maintain adequate airspeed during initial climb after takeoff, which resulted in a subsequent aerodynamic stall. Contributing to the accident was the pilot’s decision to take off with a slight tailwind. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On August 21, 2013, a Cessna 180 sustained substantial damage after impacting trees post-takeoff from Walby Lake Seaplane Base. The pilot, sole occupant, reported minor injuries. The airplane was operated under Part 91 with visual conditions prevailing.

Accident Details

On August 21, 2013, about 1356 Alaska daylight time, a Cessna 180 (registration N7807K) sustained substantial damage when it impacted trees after takeoff from Walby Lake Seaplane Base (AA85) in Palmer, Alaska. The airplane was registered to a private individual and operated by the pilot under 14 CFR Part 91. The commercial pilot, the sole occupant, sustained minor injuries. Visual meteorological conditions prevailed, and no flight plan was filed for the local personal flight, which was originating at the time of the accident. The intended destination was Finger Lake Seaplane Base (99Z), near Palmer.

Pilot Statement

During a telephone conversation with the NTSB investigator-in-charge, the pilot reported that during takeoff to the west, the airplane felt sluggish after becoming airborne. As the airplane climbed to about 100 feet above ground level, he decreased the flap setting by one notch, and the airplane started to descend rapidly. Subsequently, the airplane impacted trees about 600 feet west of the lake. The pilot added that he felt he may have retracted the flaps from the third notch to the first notch, and stalled the airplane. He did not recall hearing the stall warning horn.

Examination

Examination by an FAA inspector revealed structural damage to both wings and the fuselage. The airplane was recovered to a secure location for further examination. An NTSB investigator found the flap handle in the second notch (20-degree setting). The stall warning horn was disassembled and produced a sound when suction air pressure was applied to the bell. The reed was intact; however, it could not be determined if the stall warning system was intact and calibrated due to impact damage.

Weather Information

Review of recorded weather data from the Palmer (PAAQ) weather station, located about 4 miles east of the accident site, indicated that at 1353, wind was from 080 degrees at 8 knots.

Contributing factors

Causes

Airspeed — Not attained/maintainedPilot

Other contributing factors

Decision related to condition