20250419003359A

Accident · Substantial damage

FAA accident report · Schweizer ANM0925013 · Hood River, OR · April 19, 2025

Date
April 19, 2025 · 11:42 local
Place
Hood River, OR
Phase of flight
Unknown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N5786S
NTSB investigation
NTSBWPR25LA138
Reported as
Schweizer ANM0925013
Reported engine
NONE NONE
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor, private pilot, student
Pilot’s flight hours
372 total78 in this make and model78 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.

On 04/19/2025 at 11:42 PDT during an instructional flight for practicing take offs and landings in the pattern, the glider was launched behind the tow aircraft. Using runway 25 for take off they climbed out under tow, made a 270 degree right turn and released over the airport at mid-field at approximately 1400’ AGL. After release the aircraft made the 180° right turn to fly about one mile to the north down wind, to make a u-turn back into the right 45 for landing runway 25 at 1600’ MSL. As the student was going through these steps under the cfi’s verbal direction, he observed that the aircraft had hit a bit of sink, and the altitude was about 1500 feet. The CFI also noticed the airspeed fluctuating indicating gusty winds. So the CFI had the student make the u-turn early and bypass the 45 degree approach normally used, going directly into downwind. This resolved the altitude concern the CFI had. This maneuver had the glider about 300 feet higher than normal and the speed brakes were deployed. The pilot encountered a steeper than normal rate of decent. The CFI realized that due to the rate of decent and low ground speed that they would not be able to land on the runway. The pilot observed the area available to land in, landed the glider in an orchard avoiding structures in the area hitting some trees causing substantial damage to the aircraft.

As the FAA filed it

ON 04/19/2025 AT 11:42 PDT DURING AN INSTRUCTIONAL FLIGHT FOR PRACTICING TAKE OFFS AND LANDINGS IN THE PATTERN, THE GLIDER WAS LAUNCHED BEHIND THE TOW AIRCRAFT. USING RUNWAY 25 FOR TAKE OFF THEY CLIMBED OUT UNDER TOW, MADE A 270 DEGREE RIGHT TURN AND RELEASED OVER THE AIRPORT AT MID-FIELD AT APPROXIMATELY 1400’ AGL. AFTER RELEASE THE AIRCRAFT MADE THE 180° RIGHT TURN TO FLY ABOUT ONE MILE TO THE NORTH DOWN WIND, TO MAKE A U-TURN BACK INTO THE RIGHT 45 FOR LANDING RUNWAY 25 AT 1600’ MSL. AS THE STUDENT WAS GOING THROUGH THESE STEPS UNDER THE CFI’S VERBAL DIRECTION, HE OBSERVED THAT THE AIRCRAFT HAD HIT A BIT OF SINK, AND THE ALTITUDE WAS ABOUT 1500 FEET. THE CFI ALSO NOTICED THE AIRSPEED FLUCTUATING INDICATING GUSTY WINDS. SO THE CFI HAD THE STUDENT MAKE THE U-TURN EARLY AND BYPASS THE 45 DEGREE APPROACH NORMALLY USED, GOING DIRECTLY INTO DOWNWIND. THIS RESOLVED THE ALTITUDE CONCERN THE CFI HAD. THIS MANEUVER HAD THE GLIDER ABOUT 300 FEET HIGHER THAN NORMAL AND THE SPEED BRAKES WERE DEPLOYED. THE PILOT ENCOUNTERED A STEEPER THAN NORMAL RATE OF DECENT. THE CFI REALIZED THAT DUE TO THE RATE OF DECENT AND LOW GROUND SPEED THAT THEY WOULD NOT BE ABLE TO LAND ON THE RUNWAY. THE PILOT OBSERVED THE AREA AVAILABLE TO LAND IN, LANDED THE GLIDER IN AN ORCHARD AVOIDING STRUCTURES IN THE AREA HITTING SOME TREES CAUSING SUBSTANTIAL DAMAGE TO THE AIRCRAFT.

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 N5786S · 1

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