Plymouth - Plymouth

The airplane was returning from a 3-hour aerial mapping mission and was lined up for a straight-in, 5-mile final approach for landing. About 3 miles out on final approach, and prior to performing the before-landing check, both engines stopped producing power in sequence, one almost immediately after the other. The pilot said that by the time he completed his remedial actions the airplane had descended to about 200 feet above the ground and the engines would not restart. The auxiliary fuel tank gauges were bouncing between 2-5 gallons and the main tanks were bouncing around at 25 gallons per side. The pilot then selected a forced landing site between two large trees and landed the airplane in heavily wooded terrain. A detailed examination of the wreckage revealed no evidence of preimpact mechanical anomalies. According to information contained in the aircraft manufacturer’s owner's manual, the auxiliary fuel tanks are designed for cruising flight and are not equipped with pumps; operation near the ground (below 1000 feet) using auxiliary fuel tanks is not recommended. The first step in the before-landing check was to select the main fuel tanks on both the left and right fuel selectors, respectively. The pilot indicated that he should have selected the main tanks sooner and performed the before-landing check earlier in the approach.
Plymouth - Plymouth — crash photo

Flight / Schedule

Plymouth - Plymouth

Aircraft

Cessna 401

Registration

N401TE

MSN

401-0180

Year of Manufacture

1971

Date

June 19, 2010 at 05:03 PM

Type

CRASH

Flight Type

Topographic

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Crash Location

Plymouth Massachusetts

Region

North America • United States of America

Coordinates

41.9427°, -70.7619°

Crash Cause

Technical failure

Narrative Report

On June 19, 2010 at 05:03 PM, Plymouth - Plymouth experienced a crash involving Cessna 401, operated by Oasis Flight Services, with the event recorded near Plymouth Massachusetts.

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

3 people were known to be on board, 0 fatalities were recorded, 3 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: 2, passenger fatalities: 0, other fatalities: 0.

The listed crash cause is technical failure. The airplane was returning from a 3-hour aerial mapping mission and was lined up for a straight-in, 5-mile final approach for landing. About 3 miles out on final approach, and prior to performing the before-landing check, both engines stopped producing power in sequence, one almost immediately after the other. The pilot said that by the time he completed his remedial actions the airplane had descended to about 200 feet above the ground and the engines would not restart. The auxiliary fuel tank gauges were bouncing between 2-5 gallons and the main tanks were bouncing around at 25 gallons per side. The pilot then selected a forced landing site between two large trees and landed the airplane in heavily wooded terrain. A detailed examination of the wreckage revealed no evidence of preimpact mechanical anomalies. According to information contained in the aircraft manufacturer’s owner's manual, the auxiliary fuel tanks are designed for cruising flight and are not equipped with pumps; operation near the ground (below 1000 feet) using auxiliary fuel tanks is not recommended. The first step in the before-landing check was to select the main fuel tanks on both the left and right fuel selectors, respectively. The pilot indicated that he should have selected the main tanks sooner and performed the before-landing check earlier in the approach.

Aircraft reference details include registration N401TE, MSN 401-0180, year of manufacture 1971.

Geospatial coordinates for this crash are approximately 41.9427°, -70.7619°.

Fatalities

Total

0

Crew

0

Passengers

0

Other

0

Crash Summary

The airplane was returning from a 3-hour aerial mapping mission and was lined up for a straight-in, 5-mile final approach for landing. About 3 miles out on final approach, and prior to performing the before-landing check, both engines stopped producing power in sequence, one almost immediately after the other. The pilot said that by the time he completed his remedial actions the airplane had descended to about 200 feet above the ground and the engines would not restart. The auxiliary fuel tank gauges were bouncing between 2-5 gallons and the main tanks were bouncing around at 25 gallons per side. The pilot then selected a forced landing site between two large trees and landed the airplane in heavily wooded terrain. A detailed examination of the wreckage revealed no evidence of preimpact mechanical anomalies. According to information contained in the aircraft manufacturer’s owner's manual, the auxiliary fuel tanks are designed for cruising flight and are not equipped with pumps; operation near the ground (below 1000 feet) using auxiliary fuel tanks is not recommended. The first step in the before-landing check was to select the main fuel tanks on both the left and right fuel selectors, respectively. The pilot indicated that he should have selected the main tanks sooner and performed the before-landing check earlier in the approach.

Cause: Technical failure

Occupants & Outcome

Crew On Board

1

Passengers On Board

2

Estimated Survivors

3

Fatality Rate

0.0%

Known people on board: 3

Operational Details

Schedule / Flight

Plymouth - Plymouth

Flight Type

Topographic

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

Aircraft

Cessna 401

Registration

N401TE

MSN

401-0180

Year of Manufacture

1971

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