N73182

Substantial
Serious

CESSNA 172MS/N: 17267309

Accident Details

Date
Sunday, July 1, 2012
NTSB Number
CEN12LA408
Location
Griswold, IA
Event ID
20120702X04958
Coordinates
41.333332, -95.083335
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
1
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The pilot’s failure to maintain adequate airspeed during an attempted go-around, resulting in an aerodynamic stall.

Aircraft Information

Registration
Make
CESSNA
Serial Number
17267309
Engine Type
Reciprocating
Year Built
1973
Model / ICAO
172MC172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
182

Registered Owner (Current)

Name
SAVANNAH AIRPLANES VENTURE LLC
Address
PO BOX 1191
City
MYRTLE BEACH
State / Zip Code
SC 29578-1191
Country
United States

Analysis

On June 30, 2012, about 2030 central daylight time, a Cessna 172 airplane, N73182, impacted a field shortly after departure from a private airfield near Griswold, Iowa. The private rated pilot and passenger received serious injuries and the airplane sustained substantial damage. The airplane was registered to and operated by a private individual. Day visual meteorological conditions prevailed and no flight plan was filed for the 14 Code of Federal Regulations Part 91 flight.

The pilot departed from a 2,500 foot airstrip, with several other airplanes to perform a water balloon drop. The airplane made two passes over the airstrip for the balloon drop before returning to land. The pilot reported that during the landing, the setting sun, shadows from the crops, and the barn affected his vision, and he landed long and fast. As the end of the airstrip approached, he applied power for a go-around. The pilot added that the engine did not produce power; the airplane went airborne, he turned left, but could not hold altitude. The airplane impacted a field just south of the airstrip. Witnesses reported that the airplane pulled up and then stalled, or got slow and then stalled in the turn.

A Federal Aviation Administration inspector and a technical representative from the airframe manufacturer responded to the accident site. The airplane’s control continuity and the presence of fuel were confirmed on-site. The FAA inspector added that a witness reported that the engine maintained power throughout the accident sequence. An examination of the engine by the inspector and technical representative did not reveal any preimpact abnormalities. The inspector added that both blades of the fixed pitch propeller had leading edge polishing with one blade twisted back, towards the airframe. During the crash, the airplane sustained heavy impact damage including nearly severing the fuselage just aft of the cabin area.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN12LA408