Clarksville – Danbury

The pilot was on a personal trip that he had flown many times. On the day of the accident, additional fuel was not available at the departure airport. As he neared his destination, the pilot left one of his engines in a fuel crossfeed configuration causing a partial power loss. The airplane has the capability to climb at more than 500 feet per minute using only one engine. After declaring his emergency to the control tower, radio contact was lost. The aircraft was observed flying 90° to the ILS final approach course at very low altitude banking side to side. The airplane crashed in a 70° nose down position. Heavy snow had started falling just before the accident. A post crash fire destroyed much of the airplane. Both occupants were killed.

Flight / Schedule

Clarksville – Danbury

Registration

N36362

MSN

60-0787-8063400

Year of Manufacture

1980

Date

December 30, 1991 at 07:48 AM

Type

CRASH

Flight Type

Private

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Crash Location

North Salem New York

Region

North America • United States of America

Coordinates

41.3348°, -73.5712°

Crash Cause

Human factor

Narrative Report

On December 30, 1991 at 07:48 AM, Clarksville – Danbury experienced a crash involving Piper PA-60 Aerostar (Ted Smith 600), operated by English Aero Services, with the event recorded near North Salem New York.

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.

2 people were known to be on board, 2 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: 1, passenger fatalities: 1, other fatalities: 0.

The listed crash cause is human factor. The pilot was on a personal trip that he had flown many times. On the day of the accident, additional fuel was not available at the departure airport. As he neared his destination, the pilot left one of his engines in a fuel crossfeed configuration causing a partial power loss. The airplane has the capability to climb at more than 500 feet per minute using only one engine. After declaring his emergency to the control tower, radio contact was lost. The aircraft was observed flying 90° to the ILS final approach course at very low altitude banking side to side. The airplane crashed in a 70° nose down position. Heavy snow had started falling just before the accident. A post crash fire destroyed much of the airplane. Both occupants were killed.

Aircraft reference details include registration N36362, MSN 60-0787-8063400, year of manufacture 1980.

Geospatial coordinates for this crash are approximately 41.3348°, -73.5712°.

Fatalities

Total

2

Crew

1

Passengers

1

Other

0

Crash Summary

The pilot was on a personal trip that he had flown many times. On the day of the accident, additional fuel was not available at the departure airport. As he neared his destination, the pilot left one of his engines in a fuel crossfeed configuration causing a partial power loss. The airplane has the capability to climb at more than 500 feet per minute using only one engine. After declaring his emergency to the control tower, radio contact was lost. The aircraft was observed flying 90° to the ILS final approach course at very low altitude banking side to side. The airplane crashed in a 70° nose down position. Heavy snow had started falling just before the accident. A post crash fire destroyed much of the airplane. Both occupants were killed.

Cause: Human factor

Occupants & Outcome

Crew On Board

1

Passengers On Board

1

Estimated Survivors

0

Fatality Rate

100.0%

Known people on board: 2

Operational Details

Schedule / Flight

Clarksville – Danbury

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

N36362

MSN

60-0787-8063400

Year of Manufacture

1980