Conroe - Conroe

During initial takeoff climb the copilot who was manipulating the controls called for METO (maximum except takeoff) power. After the pilot-in-command set METO power, the left engine lost power. The PIC took the controls from the copilot and called for him to feather the left propeller. The copilot did not hear the call to feather the left propeller. Maintaining an indicated airspeed of 90 knots and wings level attitude, the airplane descended into trees and impacted a rural residential paved street. The cockpit area and main fuselage were consumed by a post crash fire. Examination of the throttle quadrant revealed the propeller control levers were forward, the mixture control levers were autorich, the throttle for the right engine was forward, and the throttle for the left engine was at idle. According to a FAA operations inspector maintaining 90 knots with the propeller not feathered would result in the aircraft descending. The pilot and copilot had not completed a proficiency check or flight check for the DC3 type aircraft within the previous 24 months. Examination of the left engine did not disclose any preexisting anomalies.

Flight / Schedule

Conroe - Conroe

Aircraft

Douglas DC-3

Registration

N23WT

MSN

11650

Year of Manufacture

1943

Date

June 20, 1996 at 02:08 PM

Type

CRASH

Flight Type

Training

Flight Phase

Takeoff (climb)

Crash Site

Airport (less than 10 km from airport)

Crash Location

Conroe Texas

Region

North America • United States of America

Coordinates

30.3119°, -95.4561°

Crash Cause

Human factor

Narrative Report

On June 20, 1996 at 02:08 PM, Conroe - Conroe experienced a crash involving Douglas DC-3, operated by Loren Davis Ministries, with the event recorded near Conroe Texas.

The flight was categorized as training and the reported phase was takeoff (climb) 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: 3, crew fatalities: 0, passengers on board: 0, passenger fatalities: 0, other fatalities: 0.

The listed crash cause is human factor. During initial takeoff climb the copilot who was manipulating the controls called for METO (maximum except takeoff) power. After the pilot-in-command set METO power, the left engine lost power. The PIC took the controls from the copilot and called for him to feather the left propeller. The copilot did not hear the call to feather the left propeller. Maintaining an indicated airspeed of 90 knots and wings level attitude, the airplane descended into trees and impacted a rural residential paved street. The cockpit area and main fuselage were consumed by a post crash fire. Examination of the throttle quadrant revealed the propeller control levers were forward, the mixture control levers were autorich, the throttle for the right engine was forward, and the throttle for the left engine was at idle. According to a FAA operations inspector maintaining 90 knots with the propeller not feathered would result in the aircraft descending. The pilot and copilot had not completed a proficiency check or flight check for the DC3 type aircraft within the previous 24 months. Examination of the left engine did not disclose any preexisting anomalies.

Aircraft reference details include registration N23WT, MSN 11650, year of manufacture 1943.

Geospatial coordinates for this crash are approximately 30.3119°, -95.4561°.

Fatalities

Total

0

Crew

0

Passengers

0

Other

0

Crash Summary

During initial takeoff climb the copilot who was manipulating the controls called for METO (maximum except takeoff) power. After the pilot-in-command set METO power, the left engine lost power. The PIC took the controls from the copilot and called for him to feather the left propeller. The copilot did not hear the call to feather the left propeller. Maintaining an indicated airspeed of 90 knots and wings level attitude, the airplane descended into trees and impacted a rural residential paved street. The cockpit area and main fuselage were consumed by a post crash fire. Examination of the throttle quadrant revealed the propeller control levers were forward, the mixture control levers were autorich, the throttle for the right engine was forward, and the throttle for the left engine was at idle. According to a FAA operations inspector maintaining 90 knots with the propeller not feathered would result in the aircraft descending. The pilot and copilot had not completed a proficiency check or flight check for the DC3 type aircraft within the previous 24 months. Examination of the left engine did not disclose any preexisting anomalies.

Cause: Human factor

Occupants & Outcome

Crew On Board

3

Passengers On Board

0

Estimated Survivors

3

Fatality Rate

0.0%

Known people on board: 3

Operational Details

Schedule / Flight

Conroe - Conroe

Flight Type

Training

Flight Phase

Takeoff (climb)

Crash Site

Airport (less than 10 km from airport)

Region / Country

North America • United States of America

Aircraft Details

Aircraft

Douglas DC-3

Registration

N23WT

MSN

11650

Year of Manufacture

1943