Little Falls - Little Falls

A witness reported the airplane did not climb above 200 feet and reported seeing the airplane 'wobbling up and down' as it attempted to climb. He reported the airplane went into a sharp left bank and nose dived down. The airplane burned upon impact. The wreckage was located in a wooded area about 3/4 mile from the approach end of runway 30. Numerous open farm fields were located near the airplane's flight path. The winds were reported at 240 degrees at 22 knots gusting to 29 knots. The wreckage path was on a 040 heading and covered about 190 feet from initial tree impact to the location of the main wreckage. The engine inspection did not reveal any anomalies to either engine. The flight was the first maintenance check flight after the airplane had not been flown for 14 months. During maintenance the pilot had put about 100 gallons of water in the left main and left auxiliary fuel tanks to locate a fuel leak. A plug was installed in the left auxiliary fuel drain valve and the fuel tank could not be checked during preflight for fuel contamination without removing the plug.

Flight / Schedule

Little Falls - Little Falls

Registration

N541N

MSN

421A-0161

Year of Manufacture

1968

Date

June 1, 1998 at 06:31 PM

Type

CRASH

Flight Type

Test

Flight Phase

Takeoff (climb)

Crash Site

Airport (less than 10 km from airport)

Crash Location

Little Falls-Morrison County Minnesota

Region

North America • United States of America

Coordinates

45.9764°, -94.3625°

Crash Cause

Human factor

Narrative Report

On June 1, 1998 at 06:31 PM, Little Falls - Little Falls experienced a crash involving Cessna 421A Golden Eagle I, operated by George Fortier III, with the event recorded near Little Falls-Morrison County Minnesota.

The flight was categorized as test and the reported phase was takeoff (climb) at a airport (less than 10 km from airport) crash site.

1 people were known to be on board, 1 fatalities were recorded, 0 survivors were identified or estimated. This corresponds to an estimated fatality rate of 100.0%.

Crew on board: 1, crew fatalities: 1, passengers on board: 0, passenger fatalities: 0, other fatalities: 0.

The listed crash cause is human factor. A witness reported the airplane did not climb above 200 feet and reported seeing the airplane 'wobbling up and down' as it attempted to climb. He reported the airplane went into a sharp left bank and nose dived down. The airplane burned upon impact. The wreckage was located in a wooded area about 3/4 mile from the approach end of runway 30. Numerous open farm fields were located near the airplane's flight path. The winds were reported at 240 degrees at 22 knots gusting to 29 knots. The wreckage path was on a 040 heading and covered about 190 feet from initial tree impact to the location of the main wreckage. The engine inspection did not reveal any anomalies to either engine. The flight was the first maintenance check flight after the airplane had not been flown for 14 months. During maintenance the pilot had put about 100 gallons of water in the left main and left auxiliary fuel tanks to locate a fuel leak. A plug was installed in the left auxiliary fuel drain valve and the fuel tank could not be checked during preflight for fuel contamination without removing the plug.

Aircraft reference details include registration N541N, MSN 421A-0161, year of manufacture 1968.

Geospatial coordinates for this crash are approximately 45.9764°, -94.3625°.

Fatalities

Total

1

Crew

1

Passengers

0

Other

0

Crash Summary

A witness reported the airplane did not climb above 200 feet and reported seeing the airplane 'wobbling up and down' as it attempted to climb. He reported the airplane went into a sharp left bank and nose dived down. The airplane burned upon impact. The wreckage was located in a wooded area about 3/4 mile from the approach end of runway 30. Numerous open farm fields were located near the airplane's flight path. The winds were reported at 240 degrees at 22 knots gusting to 29 knots. The wreckage path was on a 040 heading and covered about 190 feet from initial tree impact to the location of the main wreckage. The engine inspection did not reveal any anomalies to either engine. The flight was the first maintenance check flight after the airplane had not been flown for 14 months. During maintenance the pilot had put about 100 gallons of water in the left main and left auxiliary fuel tanks to locate a fuel leak. A plug was installed in the left auxiliary fuel drain valve and the fuel tank could not be checked during preflight for fuel contamination without removing the plug.

Cause: Human factor

Occupants & Outcome

Crew On Board

1

Passengers On Board

0

Estimated Survivors

0

Fatality Rate

100.0%

Known people on board: 1

Operational Details

Schedule / Flight

Little Falls - Little Falls

Flight Type

Test

Flight Phase

Takeoff (climb)

Crash Site

Airport (less than 10 km from airport)

Region / Country

North America • United States of America

Aircraft Details

Registration

N541N

MSN

421A-0161

Year of Manufacture

1968