Brenham – Telluride

During a visual approach, the pilot said he encountered 2,000 fpm downdrafts. The pilot stated he added power and executed a normal approach at 120 knots, compensating for downdrafts/crosswinds. After touchdown, the pilot said he did not get a beta light on the right engine. He stated he brought the power levers 'behind the gate into reverse.' The aircraft drifted left. The pilot said he corrected with brakes and nosewheel steering. He applied takeoff power and the aircraft veered right, and ran off the right side of the runway. The aircraft collided with a dirt bank and then trees. Three tire skid marks were observed on the right side of the runway. A pilot-witness said winds were gusting 22-25 knots, variable from 130-220°. He said the aircraft landed fast and long. Examination of the engines and props revealed no evidence of malfunction. The engine manufacturer recommends prop reverse not be used on icy runway or when beta light on one engine does not illuminate. The aircraft manufacturer advises that nosewheel steering should not be used at speeds below 40 knots. All six occupants were injured, two seriously.

Flight / Schedule

Brenham – Telluride

Registration

N4468M

MSN

T26-119

Year of Manufacture

1969

Date

December 29, 1987 at 05:07 PM

Type

CRASH

Flight Type

Private

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Crash Location

Telluride Colorado

Region

North America • United States of America

Coordinates

37.9375°, -107.8123°

Crash Cause

Human factor

Narrative Report

On December 29, 1987 at 05:07 PM, Brenham – Telluride experienced a crash involving Swearingen SA26T Merlin II, operated by Chemical Financial Corporation, with the event recorded near Telluride Colorado.

The flight was categorized as private and the reported phase was landing (descent or approach) at a airport (less than 10 km from airport) crash site.

6 people were known to be on board, 0 fatalities were recorded, 6 survivors were identified or estimated. This corresponds to an estimated fatality rate of 0.0%.

Crew on board: 1, crew fatalities: 0, passengers on board: 5, passenger fatalities: 0, other fatalities: 0.

The listed crash cause is human factor. During a visual approach, the pilot said he encountered 2,000 fpm downdrafts. The pilot stated he added power and executed a normal approach at 120 knots, compensating for downdrafts/crosswinds. After touchdown, the pilot said he did not get a beta light on the right engine. He stated he brought the power levers 'behind the gate into reverse.' The aircraft drifted left. The pilot said he corrected with brakes and nosewheel steering. He applied takeoff power and the aircraft veered right, and ran off the right side of the runway. The aircraft collided with a dirt bank and then trees. Three tire skid marks were observed on the right side of the runway. A pilot-witness said winds were gusting 22-25 knots, variable from 130-220°. He said the aircraft landed fast and long. Examination of the engines and props revealed no evidence of malfunction. The engine manufacturer recommends prop reverse not be used on icy runway or when beta light on one engine does not illuminate. The aircraft manufacturer advises that nosewheel steering should not be used at speeds below 40 knots. All six occupants were injured, two seriously.

Aircraft reference details include registration N4468M, MSN T26-119, year of manufacture 1969.

Geospatial coordinates for this crash are approximately 37.9375°, -107.8123°.

Fatalities

Total

0

Crew

0

Passengers

0

Other

0

Crash Summary

During a visual approach, the pilot said he encountered 2,000 fpm downdrafts. The pilot stated he added power and executed a normal approach at 120 knots, compensating for downdrafts/crosswinds. After touchdown, the pilot said he did not get a beta light on the right engine. He stated he brought the power levers 'behind the gate into reverse.' The aircraft drifted left. The pilot said he corrected with brakes and nosewheel steering. He applied takeoff power and the aircraft veered right, and ran off the right side of the runway. The aircraft collided with a dirt bank and then trees. Three tire skid marks were observed on the right side of the runway. A pilot-witness said winds were gusting 22-25 knots, variable from 130-220°. He said the aircraft landed fast and long. Examination of the engines and props revealed no evidence of malfunction. The engine manufacturer recommends prop reverse not be used on icy runway or when beta light on one engine does not illuminate. The aircraft manufacturer advises that nosewheel steering should not be used at speeds below 40 knots. All six occupants were injured, two seriously.

Cause: Human factor

Occupants & Outcome

Crew On Board

1

Passengers On Board

5

Estimated Survivors

6

Fatality Rate

0.0%

Known people on board: 6

Operational Details

Schedule / Flight

Brenham – Telluride

Flight Type

Private

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Region / Country

North America • United States of America

Aircraft Details

Registration

N4468M

MSN

T26-119

Year of Manufacture

1969