N53AS

Substantial
None

LET Blanik L-13S/N: 027057

Accident Details

Date
Monday, May 24, 2004
NTSB Number
LAX04CA220
Location
Sparks, NV
Event ID
20040616X00823
Coordinates
39.871944, -119.700836
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

the student pilot's misjudged altitude, distance, and speed, and failure to attain the proper touchdown point, resulting in an overshoot of the runway.

Aircraft Information

Registration
N53AS
Make
LET
Serial Number
027057
Engine Type
None
Year Built
1977
Model / ICAO
Blanik L-13L13M
No. of Engines
0

Registered Owner (Historical)

Name
NORTHERN CALIFORNIA SOARING ASSOC
Address
PO BOX 26
Status
Deregistered
City
BYRON
State / Zip Code
CA 94514-0026
Country
United States

Analysis

On May 23, 2004, about 1905 Pacific daylight time, a Let Blanik L-13 glider, N53AS, landed long and collided with terrain and high vegetation at the Air Sailing Gliderport, Sparks, Nevada. Northern California Soaring Association was operating the glider under the provisions of 14 CFR Part 91. The student pilot, the sole occupant, was not injured; the glider sustained substantial damage. The local instructional flight originated Sparks about 1635. Day visual meteorological conditions prevailed, and a flight plan had not been filed.

In a written statement, the pilot reported that he was attempting to land on runway 03. While on the downwind leg of the left traffic pattern, he noted that he was close to the runway. During his left turn to base leg, he realized he had become so close to the runway that he had to immediately make his turn to final approach. The glider was above the glide slope, and the pilot elected to deploy full spoilers and configure the glider in a forward slip. Despite his efforts to reduce altitude and airspeed, the pilot could not make the runway, and the glider collided with sagebrush located past the end of the runway. The glider incurred damage to the horizontal stabilizer, right elevator, and tail cone assembly.

The pilot thought the accident could have been prevented if he had established the glider on the downwind leg. He further added that, while on base leg, he could have maneuvered the glider in abbreviated figure eights, in an effort to reduce altitude. The pilot reported no preimpact mechanical malfunctions or failures with the aircraft.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX04CA220