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Accidents · NTSB SEA03LA180 · Final report

Lancair LC41 accident near Bend, Oregon, August 27, 2003

On August 27, 2003 at about 5:45 pm local time, a Lancair LC41, registered N166PD, was destroyed in an accident near Bend, Oregon. It was a flight test under general aviation rules (Part 91). No one was hurt; 1 person was on board or involved. The weather was visual conditions (good weather).

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The NTSB's probable cause their words, unchanged

The inadequate design of the drogue chute mechanical jettison system, which resulted in its failure to separate from the aircraft during in-flight spin recovery tests, and the incorrectly wired drogue chute cable cutter activation unit, which resulted in the inability of the pilot to activate the backup chute separation system after any failure of the primary system.

Source: NTSB aviation accident database, copy made October 4, 2026. Docket and reports at the NTSB.

What the record shows

Date
August 27, 2003 · about 5:45 pm local time
Place
Bend, Oregon · map
Type
Accident
Injuries
No one was hurt; 1 person was on board or involved.
Weather
visual conditions (good weather)
Aircraft
Lancair LC41
Registration
N166PD · registry record · serial 41001
Damage
Destroyed
Flight
Flight test · general aviation rules (Part 91)

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

The pilot, who had been conducting a series of spin entry and recovery tests, had intentionally entered a spin while applying left rudder and left aft stick. Because his flight control inputs did not result in recovery from the spin after three and one-half turns, he deployed the spin recovery/stabilization drogue parachute. Once the aircraft was established in an attitude from which the pilot could maintain controlled flight once the parachute was released, he pulled the drogue chute manual jettison handle. At that point, because the chute did not release, the pilot activated the electrical backup jettison system. When that action did not release the parachute, the pilot tried the electrical system a second time, and finding that this action did not release the chute, he tried the manual release a second time. At that point, because the parachute still remained attached, the pilot applied engine power in an attempt to establish controlled flight with the parachute in trail. Once he determined that the aircraft could not be satisfactorily flown in that configuration, he exited the aircraft and deployed his emergency parachute. During the investigation it was determined that the drogue chute either became entangled in the drogue chute tail boom after release from the tow hook mechanism, or it did not release from the tow hook mechanism when the pilot tried to activate it, but instead was released by the forces created by the impact with the terrain. It was also determined that the chute release system was not flight-load tested on this specific aircraft prior to the in-flight activation. Furthermore it was determined that the backup electrically activated cable guillotine system was wired incorrectly, and could not have been activated by the pilot in flight.

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: commercial pilot, military
  • Ratings: multi-engine land; single-engine land; single-engine sea; instrument: airplane
  • Flight time: 8,700 hours in all; 175 in this make and model; 50 in the last 90 days; 18 in the last 30 days; 8,000 as pilot in command
  • Last flight review: August 10, 2002
  • Medical certificate: Class 1 (valid medical--no waivers/lim.)
  • Seat: left
  • Injury: no injuries

The aircraft

  • Airframe total time: 91.5 hours
  • Last inspection: condition inspection, February 18, 2003; 12 hours since
  • Maximum gross weight: 3,600 lb
  • Seats: 4
  • Landing gear: fixed
  • Engine: Continental TSIOF-550C1B (piston); 0 hours total
  • Fire on the ground

The flight

  • Departed from: S07 Bend OR at 5:17 pm
  • Destination: S07 Bend OR
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Visibility: 30 statute miles
  • Sky: clear
  • Temperature: 79°F (26°C), dew point 0°F (-18°C)
  • Altimeter: 30.14 inHg

Injuries

FatalSeriousMinorNone
Crew1

About this page

Everything above comes from the NTSB's public accident database: the narrative, probable cause and findings are the NTSB's own words, and the coded tables behind its report (pilot, aircraft, flight, weather, injuries, sequence of events) are written out in plain English. Pilots' ages, home towns and medical details are left out on purpose. The docket at the NTSB holds the report as a PDF and the investigation's photographs and documents. This site never names pilots, passengers or anyone else involved. A preliminary report describes what is known soon after the event and can change; the final report, with the probable cause, usually follows one to two years later and this page is refreshed when it does. Case number SEA03LA180.