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Accidents · NTSB SEA05FA023 · Final report

Cirrus Design Corp. SR22 accident near Belgrade, Montana, December 4, 2004

On December 4, 2004 at about 10:30 pm local time, a Cirrus Design Corp. SR22, registered N1159C, was destroyed in an accident near Belgrade, Montana (Gallatin Field). It was a personal flight under general aviation rules (Part 91). 3 people were killed and 1 person was seriously injured. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot's failure to maintain altitude/clearance while maneuvering in mountainous terrain, which resulted in an inflight collision with trees and terrain. Contributing factors were the mountainous terrain and the downdraft.

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

What the record shows

Date
December 4, 2004 · about 10:30 pm local time
Place
Belgrade, Montana · Gallatin Field · map
Type
Accident
Injuries
3 people were killed and 1 person was seriously injured.
Weather
visual conditions (good weather)
Aircraft
Cirrus Design Corp. SR22
Registration
N1159C · no longer on the register · serial 0490
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)

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

The airplane, flown by a commercial pilot and carrying three passengers, departed in day visual meteorological conditions for a local flight over rugged mountainous terrain. The purpose of the flight was to meet up with a motor glider and make some "flybys" of the glider. The glider pilot was giving a ride to the airplane pilot's friend. The glider pilot reported that the airplane made two passes by the glider. When the airplane passed by the glider for the second time, it was "in coordinated flight," with the flaps up, and it was either flying level or descending slightly. At the time, the glider was at an altitude of about 8,900 feet and had a ground speed of about 57 knots. The glider pilot lost sight of the airplane as it proceeded north into a cirque or bowl formed by a mountain range (peak elevation about 9,600 feet) running north to south and a transverse range (peak elevation 8,916 feet) running west and then hooking south. The glider pilot and passenger did not witness the accident. However, the glider did enter the bowl about 90 seconds after the airplane had passed the glider. The glider pilot executed a left 180 degree turn in the bowl. During the turn, the glider was at altitudes of 9,100 to 9,200 feet and encountered an air mass that was sinking about 100 to 200 feet per minute. The surviving passenger, who was seated in the left rear seat, reported that as the airplane made the second pass on the glider, the stall warning indicator sounded. The pilot dropped the nose to level out, and the stall warning indicator stopped sounding. The passenger heard a high-pitched whine that sounded like a noise he had heard during the preflight check. He thought it was the sound of the flap motor, but when he looked out, he saw that the flaps were not moving. He could not see the pilot moving the flap control, and neither the pilot, nor the other passengers made any comments about the flaps. The pilot then initiated a descending left turn. During this turn, the pilot looked over his shoulder and, in a normal tone of voice, said, "hang on, we might get a couple of trees on this one." It was about 10 to 15 seconds from the time the stall warning horn stopped sounding until they hit the trees. Distribution of the wreckage at the accident site indicated the airplane impacted trees on the transverse ridge at an elevation of 8,553 feet on a southwesterly heading and traveled about 360 feet before coming to rest. Examination of the airframe and engine revealed no evidence of any discrepancies that would have prevented normal operation of the airplane. The flaps were found in the retracted position. Functional testing of the flaps was precluded by impact and fire damage. The pilot who flew the airplane just prior to the accident flight stated that she experienced no problems with the airplane and that the flaps worked normally during her flight. When interviewed 11 days after the accident, the surviving passenger reported that there were no problems with the airplane during the runup or takeoff. About 8 weeks after the accident, he told his attorney that he recalled that the pilot mentioned before takeoff that the flaps were not working.

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, flight engineer
  • Ratings: multi-engine land; single-engine land; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
  • Flight time: 1,561 hours in all; 105 in this make and model; 1,478 as pilot in command; 362 on instruments
  • Medical certificate: Class 1 (valid medical--w/ waivers/lim.)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 388 hours
  • Last inspection: annual inspection, November 24, 2004
  • Maximum gross weight: 3,400 lb
  • Seats: 4
  • Landing gear: fixed
  • Engine: Teledyne Continental IO550N7B (piston); 0 hours total
  • Fire on the ground

The flight

  • Departed from: BZN Belgrade MT at 10:18 pm
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Visibility: 10 statute miles
  • Sky: scat at 12,000 ft
  • Temperature: 36°F (2°C), dew point 21°F (-6°C)
  • Altimeter: 29.68 inHg
  • Observation at 10:56 pm from BZN, 10 miles away

Injuries

FatalSeriousMinorNone
Crew1
Passengers21

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.

Other NTSB records under N1159C the same tail number, which may have belonged to a different aircraft at the time

1996-06-16SEA96LA124 · accident near Gardiner, WA · substantial damage · serious injuries

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.