20240901017219A

Accident · Destroyed

FAA accident report · Let L 33 SOLO · Kingman, KS · September 1, 2024

Date
September 1, 2024 · 16:20 local
Place
Kingman, KS
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N133LB
NTSB investigation
NTSBCEN24LA331
Reported as
Let L 33 Solo
Reported engine
NONE NONE
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
67 total23 in this make and model13 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

The pilot reported that during the local glider flight, he was unable to find sufficient lift to

Remain airborne. He selected a field that was within gliding distance and setup for landing.

However, on short final, he became fixated on a small tree in the glide path. The airspeed

Decreased, and the glider entered an inadvertent aerodynamic stall. The subsequent impact

With the terrain resulted in damage to the left wing spar and aft fuselage. The pilot stated there

Were no mechanical malfunctions or failures which precluded normal operation of the glider.

As the FAA filed it

THE PILOT REPORTED THAT DURING THE LOCAL GLIDER FLIGHT, HE WAS UNABLE TO FIND SUFFICIENT LIFT TO

REMAIN AIRBORNE. HE SELECTED A FIELD THAT WAS WITHIN GLIDING DISTANCE AND SETUP FOR LANDING.

HOWEVER, ON SHORT FINAL, HE BECAME FIXATED ON A SMALL TREE IN THE GLIDE PATH. THE AIRSPEED

DECREASED, AND THE GLIDER ENTERED AN INADVERTENT AERODYNAMIC STALL. THE SUBSEQUENT IMPACT

WITH THE TERRAIN RESULTED IN DAMAGE TO THE LEFT WING SPAR AND AFT FUSELAGE. THE PILOT STATED THERE

WERE NO MECHANICAL MALFUNCTIONS OR FAILURES WHICH PRECLUDED NORMAL OPERATION OF THE GLIDER.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.