N37888

Destroyed
Fatal

SUPERIOR CULVER LFAS/N: 204

Accident Details

Date
Thursday, April 28, 2022
NTSB Number
CEN22LA185
Location
Syracuse, KS
Event ID
20220428105013
Coordinates
37.998580, -101.747600
Aircraft Damage
Destroyed
Highest Injury
Fatal
Fatalities
1
Serious Injuries
0
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The pilot’s exceedance of the airplane’s critical angle of attack, which resulted in an inadvertent aerodynamic stall while returning to the airport following a partial loss of engine power for reasons that could not be determined.

Aircraft Information

Registration
N37888
Make
SUPERIOR
Serial Number
204
Engine Type
Reciprocating
Model / ICAO
CULVER LFABPAT
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
GEIPEL WILLIAM R
Address
2584 42ND AVE
Status
Deregistered
City
WOODVILLE
State / Zip Code
WI 54028-7210
Country
United States

Analysis

On April 28, 2022, about 1040 central daylight time, a Superior Culver LFA, N37888, was destroyed when it was involved in an accident near Syracuse, Kansas. The pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The airplane had recently been rebuilt and the engine had been overhauled. The purpose of the flight was to transport the airplane from the maintenance facility to its owner in another state.

Witnesses reported that after takeoff, and about 150 ft above ground level, the engine began to run rough. The pilot made a steep left turn in a nose-high attitude as if he were attempting to return to the runway. The engine continued to run rough as the left wing dropped and the airplane entered a rapid descent before impacting the ground in a nose-low attitude. The airplane was largely consumed by a post-crash fire.

During a postaccident examination, flight control continuity was established to all control surfaces. The magnetos remained attached to the engine and were thermally damaged along with both ignition harnesses. The carburetor sustained impact and thermal damage. The spark plugs were removed and found to be unremarkable. No evidence of a catastrophic engine failure was present.

When the temperature (66°F) and dewpoint (55°F) were plotted on a carburetor icing probability chart, the result was that the airplane was being operated in an area conducive to serious carburetor icing at glide power. (See figure 1)

Figure 1: Carburetor Icing Probability Chart. Reference: Special Airworthiness Information Bulletin CE-09-35

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN22LA185