N686Q

The certificated airline transport pilot was departing on a 14 CFR Part 91 personal flight. The purpose of the flight was to deliver a load of wooden roofing shakes to a friend's remote lodge. Witnesses reported that just after takeoff, as the airplane climbed to about 200 to 300 feet above the ground, the airplane abruptly pitched up about 70 degrees, and drifted to the right. The airplane continued to turn to the right as the nose of the airplane lowered momentarily. As the airplane flew very slowly the landing gear was extended. The nose of the airplane pitched up again, the right wing dropped, and the airplane descended. One witness described the descent as: "The wings rocked back and forth as it descended, like a card in the wind, with the nose of the airplane slightly higher." The airplane impacted shallow water in an area of tidal mud flats. A postaccident investigation revealed that the estimated gross weight of the airplane at takeoff was 11,500.8 pounds, 1,400.8 pounds in excess of the airplane's maximum takeoff gross weight. The airplane's center of gravity could not be calculated due to the fact that the exact location/station of the cargo could not be determined. Examination of the airplane revealed no evidence of any preimpact mechanical anomalies.

Flight / Schedule

N686Q

Aircraft

Beechcraft E18

Registration

N686Q

MSN

BA-400

Year of Manufacture

1959

Operator

Aleutian Air

Date

April 10, 2002 at 04:25 PM

Type

CRASH

Flight Type

Cargo

Flight Phase

Takeoff (climb)

Crash Site

Airport (less than 10 km from airport)

Crash Location

Juneau Alaska

Region

North America • United States of America

Coordinates

58.3020°, -134.4197°

Crash Cause

Other causes

Narrative Report

On April 10, 2002 at 04:25 PM, N686Q experienced a crash involving Beechcraft E18, operated by Aleutian Air, with the event recorded near Juneau Alaska.

The flight was categorized as cargo 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 other causes. The certificated airline transport pilot was departing on a 14 CFR Part 91 personal flight. The purpose of the flight was to deliver a load of wooden roofing shakes to a friend's remote lodge. Witnesses reported that just after takeoff, as the airplane climbed to about 200 to 300 feet above the ground, the airplane abruptly pitched up about 70 degrees, and drifted to the right. The airplane continued to turn to the right as the nose of the airplane lowered momentarily. As the airplane flew very slowly the landing gear was extended. The nose of the airplane pitched up again, the right wing dropped, and the airplane descended. One witness described the descent as: "The wings rocked back and forth as it descended, like a card in the wind, with the nose of the airplane slightly higher." The airplane impacted shallow water in an area of tidal mud flats. A postaccident investigation revealed that the estimated gross weight of the airplane at takeoff was 11,500.8 pounds, 1,400.8 pounds in excess of the airplane's maximum takeoff gross weight. The airplane's center of gravity could not be calculated due to the fact that the exact location/station of the cargo could not be determined. Examination of the airplane revealed no evidence of any preimpact mechanical anomalies.

Aircraft reference details include registration N686Q, MSN BA-400, year of manufacture 1959.

Geospatial coordinates for this crash are approximately 58.3020°, -134.4197°.

Fatalities

Total

1

Crew

1

Passengers

0

Other

0

Crash Summary

The certificated airline transport pilot was departing on a 14 CFR Part 91 personal flight. The purpose of the flight was to deliver a load of wooden roofing shakes to a friend's remote lodge. Witnesses reported that just after takeoff, as the airplane climbed to about 200 to 300 feet above the ground, the airplane abruptly pitched up about 70 degrees, and drifted to the right. The airplane continued to turn to the right as the nose of the airplane lowered momentarily. As the airplane flew very slowly the landing gear was extended. The nose of the airplane pitched up again, the right wing dropped, and the airplane descended. One witness described the descent as: "The wings rocked back and forth as it descended, like a card in the wind, with the nose of the airplane slightly higher." The airplane impacted shallow water in an area of tidal mud flats. A postaccident investigation revealed that the estimated gross weight of the airplane at takeoff was 11,500.8 pounds, 1,400.8 pounds in excess of the airplane's maximum takeoff gross weight. The airplane's center of gravity could not be calculated due to the fact that the exact location/station of the cargo could not be determined. Examination of the airplane revealed no evidence of any preimpact mechanical anomalies.

Cause: Other causes

Occupants & Outcome

Crew On Board

1

Passengers On Board

0

Estimated Survivors

0

Fatality Rate

100.0%

Known people on board: 1

Operational Details

Operator

Aleutian Air

Flight Type

Cargo

Flight Phase

Takeoff (climb)

Crash Site

Airport (less than 10 km from airport)

Region / Country

North America • United States of America

Aircraft Details

Aircraft

Beechcraft E18

Registration

N686Q

MSN

BA-400

Year of Manufacture

1959