Let L-13 accident near Shelton, WA

On August 11, 1996, a Let L-13 (glider) was involved in an accident near Shelton, WA. 1 person died. Damage to the aircraft: substantial.

Date
August 11, 1996
Place
Shelton, WA
Aircraft
Let L-13 · Glider
Injuries
1 fatal, 0 serious, 0 minor
Damage
Substantial
Position
47.229°N, 123.201°W
NTSB ID
20001208X06614

Official records · SEA96FA186

NTSB summary

HISTORY OF FLIGHT On August 10, 1996, approximately 1915 Pacific daylight time, a Czechoslovakian-manufactured LET L-13 Blanik glider, N90865, being operated by Olympic Air, Inc. of Shelton, Washington, was observed by witnesses to abruptly enter a rapid descent from a right turn, 5 to 10 seconds after releasing from an aero-tow 3 miles southwest of Sanderson Field, Shelton. The aircraft was observed to continue in this rapid descent until it impacted in an area of dense vegetation which according to the towplane pilot was almost directly under the release point. The glider was substantially damaged and the recently certificated private glider pilot, the sole occupant, was fatally injured. According to the towplane pilot, the flight was planned as a local 14 CFR 91 flight from Shelton. Visual meteorological conditions existed and no flight plan had been filed. In an interview with the towplane pilot on the day after the accident, the towplane pilot stated that the accident pilot's planned flight profile was to be an aerotow to traffic pattern altitude, followed by release, entry into the Sanderson Field airport traffic pattern, and landing. He stated that the aerotow and release were uneventful and routine, and that the release occurred at an altitude of 1,850 feet and an airspeed of 80 to 85 MPH (70 to 74 knots.) One ground witness stated that during the rapid descent, he saw the glider turning slowly to the right. Another individual, the pilot of an airplane carrying parachute jump students over Sanderson Field, stated that he observed the release, and that 5 to 10 second

Probable cause

failure of the operator to provide its pilots with information essential for an accurate determination of the glider's weight and balance, the resultant operation of the glider with a center-or-gravity that exceeded the aft limit, and the pilot's inadvertent entry into a stall/spin. Factors relating to the accident were: an incorrect placard concerning the glider's minimum front seat solo weight l

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