N10BR

Substantial
Serious

LET L-23 SUPER BLANIKS/N: 917826

Accident Details

Date
Wednesday, June 21, 2023
NTSB Number
CEN23LA254
Location
Gregory, MI
Event ID
20230623192425
Coordinates
42.442080, -84.064360
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
1
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The flight instructor’s failure to maintain adequate airspeed and his exceedance of the glider’s critical angle of attack, leading to an aerodynamic stall during the off-field landing.

Aircraft Information

Registration
Make
LET
Serial Number
917826
Engine Type
None
Year Built
1991
Model / ICAO
L-23 SUPER BLANIK
Aircraft Type
Glider
No. of Engines
0
Seats
2
FAA Model
L-23 SUPER BLANIK

Registered Owner (Current)

Name
SANDHILL SOARING CLUB INC
Address
PO BOX 1891
City
BRIGHTON
State / Zip Code
MI 48116-5691
Country
United States

Analysis

On June 21, 2023, about 1530 eastern daylight time, a Let L-23 Super Blanik, N10BR, was substantially damaged when it was involved in an accident near Richmond Field Airport (69G), Gregory, Michigan. The flight instructor was seriously injured, and the student pilot received minor injuries. The glider was operated as a Title 14 Code of Federal Regulations Part 91 instructional flight.

The glider came to rest about 3,500 ft northwest of the north end of the runway at 69G.

The student pilot reported that he was flying the glider until about 10 minutes before the accident when the flight instructor took over control and started looking for thermals to gain altitude. He said the flight instructor was mostly quiet until he said they were going to perform an off-field landing. The glider flew across a tree line about 150 ft above ground level and turned to land in a bean field. The student had no further recollection of the accident. The flight instructor also reported that he had no recollection of the flight.

The glider sustained substantial damage to the fuselage and both wings.

Postaccident examination showed that the forward fuselage was crushed upward, and rearward and the outboard 6 ft of the left wing was separated. The separation point had signatures indicating upward bending of the tip. The damage to the glider was consistent with a nose-low, left-wing -ow impact. Flight control continuity was verified from the cockpit to all control surfaces. No preimpact anomalies were detected.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN23LA254