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Accidents · NTSB SEA05LA137 · Final report

Scheibe SF-28A Tandem-Falke accident near North Plains, Oregon, July 3, 2005

On July 3, 2005 at about 11:15 pm local time, a Scheibe SF-28A Tandem-Falke (glider), registered N12HS, was substantially damaged in an accident near North Plains, Oregon (North Plains Glider Port airport). It was a personal flight under general aviation rules (Part 91). No one was hurt; 2 people were on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot's failure to maintain airspeed during landing. Inadequate emergency procedures training and high vegetation were factors.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
July 3, 2005 · about 11:15 pm local time
Place
North Plains, Oregon · North Plains Glider Port · map
Type
Accident
Injuries
No one was hurt; 2 people were on board or involved.
Weather
visual conditions (good weather)
Aircraft
Scheibe SF-28A Tandem-Falke
Registration
N12HS · registry record · serial 5757
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The pilot reported that he was performing an engine off landing to the west, with a three to four knot tailwind. The pilot stated that the approach was normal until final approach when the airspeed indicator suddenly indicated a drop in airspeed to 20 mph. The pilot initially thought that it was wind shear or a stall and pushed the nose down and closed the spoilers. The airspeed indicator then indicated 70 mph and the glider's descent rate decreased. Because of the decrease in descent rate, the pilot now determined that his airspeed and altitude were too high for a safe landing on the airstrip. The pilot opted to land in an open field with tall grass adjacent to the airstrip. After making the decision to land in the field, the pilot, in an attempt to stay aloft longer, tried to start the engine even though he was aware that operating procedures did not recommend it. The pilot stated that he left the cowl flaps closed, left the fuel off because he believed that there was enough fuel in the system to start the engine, and he left the propeller feathered so as not to increase drag. The engine did not start and the pilot continued with the off airstrip landing. After flying over another glider and tow plane on the ground at about 10 feet above ground level, the glider suddenly stalled, dragging a wing and impacting the ground hard in a field next to the airstrip. The glider completed about a 120 degree turn before coming to rest. The field was covered with about three foot tall grass. In a subsequent written statement, the pilot reported that in May 2005, during stall testing, the airspeed indicator dropped to 20 mph and then jumped to 70 mph. After this event, the pilot had the line and airspeed indicator inspected. During this inspection, a couple of drops of water was found at the bottom of the drain plug. The line was cleared and there were no further problems. The pilot reported that the glider is kept outside and under a tarp. The pilot reported no anomalies with the airspeed indicator during the hour flight prior to the accident. The pilot also reported a lack of training in certain emergency procedures that might have helped him in preventing this accident.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

Pilot

  • Certificate: private
  • Ratings: single-engine land; rotorcraft: glider
  • Flight time: 260 hours in all; 5 in this make and model; 21 in the last 90 days; 4 in the last 30 days
  • Last flight review: June 1, 2004
  • Medical certificate: Class 3
  • Seat: frt
  • Injury: no injuries

The aircraft

  • Airframe total time: 545 hours
  • Last inspection: annual inspection, March 1, 2005
  • Maximum gross weight: 1,350 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Limbach 1700EA (piston); 0 hours total

The flight

  • Departed from: North Plains OR at 10:15 pm
  • Flight plan: none
  • Runway 270, 2,000 ft by 50 ft

Weather at the time

  • Light: daylight
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 81°F (27°C), dew point 0°F (-18°C)

Injuries

FatalSeriousMinorNone
Crew1
Passengers1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.