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Accidents · NTSB NYC03LA081 · Final report

Amateur-built SD3-30 accident near Du Bois, Pennsylvania, April 9, 2003

On April 9, 2003 at about 11:15 am local time, a amateur-built SD3-30, registered N805SW, was substantially damaged in an accident near Du Bois, Pennsylvania (Du Bois-Jefferson County airport). It was flown under charter and air-taxi rules (Part 135). No one was hurt; 2 people were on board or involved. The weather was instrument conditions (cloud, fog or low visibility).

The NTSB's probable cause their words, unchanged

The captain's failure to maintain the proper glidepath during the instrument approach, and his failure to perform a go-around. Factors were a low ceiling and reduced visibility due to mist.

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

What the record shows

Date
April 9, 2003 · about 11:15 am local time
Place
Du Bois, Pennsylvania · Du Bois-Jefferson County · map
Type
Accident
Injuries
No one was hurt; 2 people were on board or involved.
Weather
instrument conditions (cloud, fog or low visibility)
Aircraft
Amateur-built SD3-30
Registration
N805SW · registry record · serial 3055
Damage
Substantial damage
Flight
Flight · charter and air-taxi rules (Part 135)

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

The airplane was on an instrument landing system (ILS) approach in instrument meteorological conditions. The captain initially stated that the airplane was on the ILS approach with the engine power set at flight idle. About 300 feet above the ground, and 1/4 to 1/2 mile from the threshold, the captain made visual contact with the runway. The captain stated that the left engine then surged, which caused the airplane to yaw right and drift left. At the time, the airplane was in visual conditions, and on glideslope, with the airspeed decreasing through 106 knots. The captain aligned the airplane with the runway and attempted to go-around, but the throttles were difficult to move. The airplane began to stall and the captain lowered the nose. The airplane subsequently struck terrain about 500 feet prior to the runway. After the captain was informed that the engine power should not be at flight idle during the approach, he amended his statement to include the approach power setting at 1,000 lbs. of torque. The co-pilot initially reported that the engine anomaly occurred while at flight idle. However, the co-pilot later amended his statement and reported that the anomaly occurred as power was being reduced toward flight idle, but not at flight idle. Examination of the left engine did not reveal any pre-impact mechanical malfunctions. Examination of the airplane cockpit did not reveal any anomalies with the throttle levers. Review of a flight manual for the make and model accident airplane revealed that during a normal landing, 1,100 lbs of torque should be set prior to turning base leg. The manual further stated to reduce the power levers about 30 feet agl, and initiate a gentle flare. The reported weather at the airport about 5 minutes before the accident included a visibility 3/4 mile in mist, and an overcast ceiling at 100 feet. The reported weather at the airport about 7 minutes after the accident included visibility 1/4 mile in freezing fog and an overcast ceiling at 100 feet. Review of the terminal procedure for the respective ILS approach revealed that the decision height was 200 feet agl, and the required minimum visibility was 1/2 mile.

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: airline transport pilot
  • Ratings: multi-engine land; single-engine land; instrument: airplane
  • Flight time: 3,470 hours in all; 2,100 in this make and model; 76 in the last 90 days; 18 in the last 30 days; 2,665 as pilot in command
  • Last flight review: November 25, 2002
  • Medical certificate: Class 1 (valid medical--no waivers/lim.)
  • Seat: left
  • Injury: no injuries

Co-pilot

  • Certificate: commercial pilot
  • Ratings: multi-engine land; single-engine land; instrument: airplane
  • Flight time: 1,347 hours in all; 431 in this make and model; 82 in the last 90 days; 36 in the last 30 days; 786 as pilot in command
  • Last flight review: January 31, 2003
  • Medical certificate: Class 1 (valid medical--no waivers/lim.)
  • Seat: rgt
  • Injury: no injuries

The aircraft

  • Airframe total time: 24,401 hours
  • Last inspection: approved inspection programme, March 24, 2003; 26 hours since
  • Maximum gross weight: 22,600 lb
  • Seats: 2
  • Landing gear: retractable
  • Engine 1: Pratt & Whitney PT6A-45R (turboprop); 0 hours total
  • Engine 2: Pratt & Whitney PT6A-45R (turboprop); 0 hours total

The flight

  • Departed from: PIT Pittsburgh PA at 10:05 am
  • Destination: DUJ Du Bois PA
  • Flight plan: IFR
  • Runway 25, 5,504 ft by 100 ft
  • A second pilot was aboard

Weather at the time

  • Light: dawn
  • Wind: from 070° at 6 knots
  • Visibility: 0.8 statute miles
  • Sky: overcast at 100 ft
  • Temperature: 32°F (0°C), dew point 30°F (-1°C)
  • Altimeter: 30.10 inHg
  • Observation at 12:10 pm from DUJ

Injuries

FatalSeriousMinorNone
Crew2

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.