N5038E

Substantial
Serious

BELLANCA 8KCABS/N: 481-79

Accident Details

Date
Monday, May 29, 2023
NTSB Number
CEN23LA205
Location
Larchwood, IA
Event ID
20230530192252
Coordinates
43.449950, -96.403169
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 proper airspeed and his exceedance of the airplane’s critical angle of attack during initial climb after takeoff, which resulted in an aerodynamic stall and impact with the ground.

Aircraft Information

Registration
Make
BELLANCA
Serial Number
481-79
Engine Type
Reciprocating
Year Built
1979
Model / ICAO
8KCABBL8
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
8KCAB

Registered Owner (Current)

Name
HOHMAN BRENT A
Address
PO BOX 47
City
FULTON
State / Zip Code
SD 57340-0047
Country
United States

Analysis

On May 29, 2023, about 1330 central daylight time, a Bellanca 8KCAB airplane, N5038E, sustained substantial damage when it was involved in an accident near Larchwood, Iowa. The pilot sustained serious injuries and the passenger had minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that he did not recall anything about the accident. The passenger reported that his memory was vague but did recall taking off from the taxiway of a private airstrip (Larchwood-Zangger Vintage Airpark, 2VA). He recalled that he felt a little bit of a roller coaster sensation on the climb out. The airplane seemed to pitch up higher than normal, and then seemed to stall. He recalled that he heard the pilot say that they were stalling. He did not recall seeing the ground or impact with the ground. The pilot reported on the NTSB Form 6120 that there were no mechanical malfunctions or failures of the airplane.

Examination of the accident site showed that the airplane impacted the ground about 700 ft to the left of the departure end of the paved taxiway. The front of the fuselage and both wings sustained substantial damage. Impact damage and low energy signatures were consistent with a stall. Examination of the flight controls revealed continuity from the cockpit to the rudder, ailerons, elevator, and elevator trim surfaces. Interruptions in the flight control continuity were attributed to impact damage.

Fuel was present in the fuel lines and the carburetor bowl. The fuel tanks were breached, but first responders noted that fuel was leaking and the grass around the wreckage showed blight from fuel leakage. Examination of the engine revealed continuity throughout the drivetrain. Thumb compression was verified on all valves and cylinders. No pre-impact anomalies were found with the airframe, fuel, system, flight controls, or the engine.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN23LA205