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Accidents · NTSB WPR10FA388 · Final report

Diamond HK36 accident near Bend, Oregon, August 8, 2010

On August 8, 2010 at about 4:58 pm local time, a Diamond HK36, registered N40440, was substantially damaged in an accident during initial climb near Bend, Oregon (Bend Municipal airport). It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

An condition, which could not be determined because postaccident examination of the airframe and engine did not reveal any anomalies that would have precluded normal operation, that prompted the pilot to discontinue the flight. Contributing to the accident was the pilot's decision to attempt to return to the runway instead of landing straight ahead in the field off the runway end.

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

What the record shows

Date
August 8, 2010 · about 4:58 pm local time
Place
Bend, Oregon · Bend Municipal · map
Type
Accident
Injuries
1 person was killed.
Weather
visual conditions (good weather)
Aircraft
Diamond HK36 TC
Registration
N40440 · no longer on the register · serial 36388
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

Two witnesses observed the motorglider depart from runway 16, appear to have difficulty climbing, and then make a left circling turn in an apparent attempt to return for a landing. The airplane struck an unoccupied factory on the southeast corner of the airport. Damage signatures indicated that the right wing struck the building about 8 feet above the ground while the airplane was in an approximate 30-degree right bank. Ground scars and propeller damage indicated that the engine was running at the time of impact. The pilot had owned the airplane about 9 years, but his experience in the airplane could not be determined. The pilot's autopsy and toxicology results did not reveal any conditions that would have affected the pilot’s operation of the motorglider. Examination of the flight control system and the engine did not reveal any preaccident mechanical conditions or failures that would have precluded normal operation or warranted an immediate turn back for landing. The propeller blade pitch and most cockpit controls were found in their normal or expected positions/settings. However, several conditions that could have contributed to or been indicative of operational difficulties were observed. The circuit breaker for the propeller pitch control was found in the "out" (circuit disabled) position; testing indicated that the breaker was functional, and complied with the manufacturer's specifications. It could not be determined when or how the breaker came to be set to that position. The airplane pitch trim control was found in the full airplane nose-up position instead of the neutral position, but the reasons for this could not be determined. Throughout its range, the tachometer indicated about 15 percent lower than the actual propeller rpm. The nest of a paper wasp, which was likely occupied by a few insects during the attempted flight, was found in the cockpit air inlet, and it is conceivable that the wasps were disturbed and entered the cockpit after takeoff. Since the canopy could not be opened in flight, the presence of the wasps could have prompted the pilot's turn back. Neither the actual climb rate nor the maximum altitude of the airplane could be determined. Therefore, it could not be determined whether the pilot's decision to return for landing was based on the airplane performance, one of the discrepancies noted above, or some combination thereof. Examination of the cockpit indicated that only the takeoff checklist was readily available to the pilot at the time of the accident and that the emergency and other procedures checklists remained inside the flight manual, which was stowed in an undetermined location for the flight. Although an emergency landing on the terrain south of the airport and more closely aligned with the departure heading probably would have damaged the airplane, it also would have likely resulted in a more successful outcome.

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

What happened, in order

  1. Unknown or undetermined during initial climb defining event
  2. Collision with terrain or object (not controlled flight into terrain) during approach

The NTSB's findings

  • cause Not determined › Not determined › (general) › (general) › Unknown/Not determined
  • factor Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
  • Aircraft › Aircraft propeller/rotor › Propeller system › Propeller controlling system › Damaged/degraded
  • Environmental issues › Physical environment › Object/animal/substance › Animal(s)/bird(s) › Effect on personnel

Pilot

  • Certificate: private
  • Ratings: multi-engine land; single-engine land; single-engine sea; instrument: airplane
  • Medical certificate: Class 3
  • Seat: left
  • Injury: fatal

The aircraft

  • Maximum gross weight: 1,698 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Bombardier Rotax 912 (piston); 0 hours total

The flight

  • Departed from: BDN Bend OR at 4:57 pm
  • Destination: BDN Bend OR
  • Flight plan: not recorded
  • Runway 16, 5,200 ft by 75 ft

Weather at the time

  • Light: daylight
  • Wind: from 260° at 3 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 66°F (19°C), dew point 48°F (9°C)
  • Altimeter: 30.00 inHg
  • Observation at 4:55 pm from BDN, 1 miles away

Injuries

FatalSeriousMinorNone
Flight crew1

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.