N9284U

Substantial
None

CESSNA 150 S/N: 15078234

Accident Details

Date
Friday, July 8, 1994
NTSB Number
CHI94LA224
Location
ANDOVER, MN
Event ID
20001206X01692
Coordinates
45.249900, -93.329895
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

the flight instructor's improper procedures and directives by electing to pull the mixture control to the 'off' position during simulated emergency procedures. A factor associated with the accident is the existence of weather conditions conducive to carburetor icing.

Aircraft Information

Registration
N9284U
Make
CESSNA
Serial Number
15078234
Engine Type
Reciprocating
Model / ICAO
150 C150
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
FLYWELL FLYING CLUB INC
Address
2119 VIOLET LANE
Status
Deregistered
City
NEW BRIGHTON
State / Zip Code
MN 55112
Country
United States

Analysis

On July 8, 1994, at 0815 central daylight time, a Cessna 150, N9284U, sustained substantial damage following a loss of engine power and subsequent off-airport forced landing near Andover, Minnesota. The certificated flight instructor and private pilot aboard reported no injuries. The 14 CFR Part 91 instructional flight originated in Anoka, Minnesota, at 0800. No flight plan was filed, and visual meteorological conditions prevailed at the time.

According to the instructor's statement, he reduced the engine power to simulate a rough running engine, and than pulled the mixture control out to simulate an engine failure. He said the private pilot did an excellent job of remedial emergency procedures, including pulling the carburetor heat "on" promptly. The instructor wrote that he was satisfied with the private pilot's actions, and told him to restore power. When the private pilot pushed the mixture in to full rich, the engine would not restart. The instructor took control of the airplane and made a forced landing on a nearby field. He was unable to stop the airplane prior to colliding with obstructions.

The reported surface temperature in the area at the time of the accident was 61 degrees and the dew point was 59 degrees. The attached Carburetor Icing Probability Chart places this temperature and dewpoint combination in the severe icing category.

Postaccident inspection of the airplane and its systems discovered no preimpact mechanical anomalies. The engine was started and run at the site with no observed mechanical deficiencies.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI94LA224