20060618030489A

Accident · Substantial damage

FAA accident report · Scwzer SGS 2-33A · Hood River, OR · June 18, 2006

Date
June 18, 2006 · 16:30 local
Place
Hood River, OR
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N2052T
NTSB investigation
NTSBSEA06CA125
Reported as
Scwzer SGS233A
People aboard
1
Fatal injuries
0
Pilot’s flight hours
2,900 total20 in this make and model4 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.

(-23) Pilot was flying the schweitzer sgs 2-33A glider approximately 5 miles east of the Hood River airport in some ridge soaring conditions. The wind blew the glider downwind of the ridge into some striking conditions. Given the sink and approximately 20 knot headwind the glider did not have enough altitude to return to the lift conditions. An off airport landing was made in a clearing. No one was injured and the aircraft received damage to the leading edge of the right wing, leading edge of the horizontal stabilizer, tears in the fuselage belly fabric, and a bent front skid.

As the FAA filed it

(-23) PILOT WAS FLYING THE SCHWEITZER SGS 2-33A GLIDER APPROXIMATELY 5 MILES EAST OF THE HOOD RIVER AIRPORT IN SOME RIDGE SOARING CONDITIONS. THE WIND BLEW THE GLIDER DOWNWIND OF THE RIDGE INTO SOME STRIKING CONDITIONS. GIVEN THE SINK AND APPROXIMATELY 20 KNOT HEADWIND THE GLIDER DID NOT HAVE ENOUGH ALTITUDE TO RETURN TO THE LIFT CONDITIONS. AN OFF AIRPORT LANDING WAS MADE IN A CLEARING. NO ONE WAS INJURED AND THE AIRCRAFT RECEIVED DAMAGE TO THE LEADING EDGE OF THE RIGHT WING, LEADING EDGE OF THE HORIZONTAL STABILIZER, TEARS IN THE FUSELAGE BELLY FABRIC, AND A BENT FRONT SKID.

NTSB investigation

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

Other reports on N2052T · 1

Matched to the same aircraft by N-number and date.