N52728Cessna 206H2006-07-22 NTSB Accident Report

Substantial
None

Cessna 206HS/N: 20608185

Summary

On July 22, 2006, a Cessna 206H (N52728) was involved in an incident near Lutsen, MN. All 3 people aboard were uninjured. The aircraft sustained substantial damage.

The National Transportation Safety Board determined the probable cause of this incident to be: The unsuitable terrain the pilot encountered during takeoff in rough water. A factor was the wave in the rough water.

The amphibian airplane sustained substantial damage during takeoff when its float encountered a wave. The pilot stated, "As airspeed increased, the aircraft encountered slightly larger waves and as airspeed approached rotation speed, began hitting the crests of the waves. Just before rotation, a snap was heard and takeoff was immediately aborted. As the aircraft quickly decelerated, the front pilot side float strut pierced through the fuselage by pilot rudder pedals and the whole float assembly collapsed."

This incident is documented in NTSB report CHI06CA197. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N52728.

Accident Details

Date
Saturday, July 22, 2006
NTSB Number
CHI06CA197
Location
Lutsen, MN
Event ID
20060818X01212
Coordinates
47.816387, -90.383331
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

The unsuitable terrain the pilot encountered during takeoff in rough water. A factor was the wave in the rough water.

Aircraft Information

Registration
Make
CESSNA
Serial Number
20608185
Engine Type
Reciprocating
Year Built
2002
Model / ICAO
206HC206
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
WIPAIRE INC
Address
1700 HENRY AVE
Status
Deregistered
City
SOUTH SAINT PAUL
State / Zip Code
MN 55075-3500
Country
United States

Analysis

The amphibian airplane sustained substantial damage during takeoff when its float encountered a wave. The pilot stated, "As airspeed increased, the aircraft encountered slightly larger waves and as airspeed approached rotation speed, began hitting the crests of the waves. Just before rotation, a snap was heard and takeoff was immediately aborted. As the aircraft quickly decelerated, the front pilot side float strut pierced through the fuselage by pilot rudder pedals and the whole float assembly collapsed."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI06CA197