19960528012069A

Accident · Substantial damage

FAA accident report · Schler ASW-20 · Sparks, NV · May 28, 1996

Date
May 28, 1996 · 15:15 local
Place
Sparks, NV
Airport
Air Sailing Gliderport
Phase of flight
Takeoff Ground Roll
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N204Q
NTSB investigation
NTSBLAX96LA212
Reported as
Schler ASW20
Fatal injuries
0
Pilot’s flight hours
622 total254 in this make and model19 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.

Glider encountered a dust devil on takeoff, lost control of aircraft and crashed at end of runway. (.4)the pilot said he was in full control of the glider during the ground roll portion of an aero tow, with the wings level as the glider accelerated through an airspeed between 20 and 30 knots. He reported that 'without warning, the right wing was (then) slammed to the ground.' He applied full opposite aileron which had no effect, and the glider became airborne. The pilot then released from the tow plane, but during touchdown, the glider's nose collapsed, the canopy broke, and the left wing was damaged. When the takeoff was initiated, the local wind was between 5 and 10 knots, with gusts to 12 knots. Following the accident, the wind speed was between 2 and 7 knots. The pilot stated that he believed his glider was 'hit by a freak high velocity wind gust.'

As the FAA filed it

GLIDER ENCOUNTERED A DUST DEVIL ON TAKEOFF, LOST CONTROL OF AIRCRAFT AND CRASHED AT END OF RUNWAY. (.4)THE PILOT SAID HE WAS IN FULL CONTROL OF THE GLIDER DURING THE GROUND ROLL PORTION OF AN AERO TOW, WITH THE WINGS LEVEL AS THE GLIDER ACCELERATED THROUGH AN AIRSPEED BETWEEN 20 AND 30 KNOTS. HE REPORTED THAT 'WITHOUT WARNING, THE RIGHT WING WAS (THEN) SLAMMED TO THE GROUND.' HE APPLIED FULL OPPOSITE AILERON WHICH HAD NO EFFECT, AND THE GLIDER BECAME AIRBORNE. THE PILOT THEN RELEASED FROM THE TOW PLANE, BUT DURING TOUCHDOWN, THE GLIDER'S NOSE COLLAPSED, THE CANOPY BROKE, AND THE LEFT WING WAS DAMAGED. WHEN THE TAKEOFF WAS INITIATED, THE LOCAL WIND WAS BETWEEN 5 AND 10 KNOTS, WITH GUSTS TO 12 KNOTS. FOLLOWING THE ACCIDENT, THE WIND SPEED WAS BETWEEN 2 AND 7 KNOTS. THE PILOT STATED THAT HE BELIEVED HIS GLIDER WAS 'HIT BY A FREAK HIGH VELOCITY WIND GUST.'

NTSB investigation

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