N60859

Substantial
None

Cessna 185F S/N: 18504064

Accident Details

Date
Thursday, June 19, 1997
NTSB Number
ANC97LA086
Location
SITKA, AK
Event ID
20001208X08043
Coordinates
56.729312, -135.000579
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

failure of the pilot(s) to properly flare the airplane during a simulated forced landing. The excessive rate of descent on final approach was a related factor.

Aircraft Information

Registration
N60859
Make
CESSNA
Serial Number
18504064
Engine Type
Reciprocating
Year Built
1980
Model / ICAO
185F C185
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SHUMAN CECIL R
Address
27339 GOLDEN EAGLE CT
Status
Deregistered
City
CHUGIAK
State / Zip Code
AK 99567-5125
Country
United States

Analysis

On June 19, 1997, about 1440 Alaska daylight time, an amphibious float equipped Cessna 185F, N60859, crashed during a simulated forced landing on a remote lake, about 10 miles south of Sitka, Alaska. The airplane was being operated as a visual flight rules (VFR) local area instructional flight under Title 14 CFR Part 91 when the accident occurred. The airplane, operated by Mountain Aviation Inc., Sitka, sustained substantial damage. The certificated commercial pilot (first pilot), a certificated airline transport pilot (second pilot), and the sole passenger, were not injured. Visual meteorological conditions prevailed. A VFR flight plan was filed. The flight originated at the Sitka airport, about 1330.

On June 20, 1997, at 1320, the second pilot reported in a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), he was preparing the first pilot and the passenger for a CFR Part 135 check ride to be conducted in a float equipped airplane. The second pilot is the chief pilot for Mountain Aviation. The second pilot, seated in the right front seat, stated he briefed the first pilot about the planned training maneuver that was a simulated engine failure after takeoff from the water. Following a takeoff with 20 degrees of flaps selected, the second pilot pulled the engine throttle to idle about 60 to 100 feet above the water. The first pilot, seated in the left front seat, lowered the nose of the airplane and descended for landing. The first pilot landed the airplane on the water in a level attitude but with an excessive rate of descent.

The front float strut attach points separated from the fuselage and the front of the fuselage pivoted downward, coming to rest on the front float spreader bar. The airplane received wrinkling damage to the fuselage aft of the float attach points and under the front doors. The propeller struck the front portion of one float.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC97LA086