Montgomery – Columbus

During the takeoff roll and initial climb both engines were producing normal power. As the airplane climbed through 150 feet, the left engine lost power. The pilot reported that he feathered the left propeller. He further stated that following the securing of the left engine, the right engine began to 'power down.' The pilot reported that he was unable to maintain a climb attitude and was forced to land on the airport in a grassy area. The subsequent examination of the cockpit disclosed that the left engine throttle was in the full forward position, and the right throttle lever was in the mid-range position. Both propeller levers were found full forward. The left engine mixture lever was in the full forward position, and the right mixture lever full aft, or lean, position. The functional check of both engines was conducted. Initially the left engine would not start, but after troubleshooting the fuel system, the left fuel boost pump was determined to have been defective. The 'loss of engine power after liftoff' checklist requires that the pilot identify the inoperative engine and to feather the propeller for the inoperative engine.

Flight / Schedule

Montgomery – Columbus

Registration

N601JS

MSN

60-0553-179

Year of Manufacture

1978

Date

May 29, 1999 at 05:24 PM

Type

CRASH

Flight Type

Private

Flight Phase

Takeoff (climb)

Crash Site

Airport (less than 10 km from airport)

Crash Location

Montgomery Alabama

Region

North America • United States of America

Coordinates

32.3777°, -86.3091°

Crash Cause

Technical failure

Narrative Report

On May 29, 1999 at 05:24 PM, Montgomery – Columbus experienced a crash involving Piper PA-60 Aerostar (Ted Smith 600), operated by Alpha Beta Aviation, with the event recorded near Montgomery Alabama.

The flight was categorized as private and the reported phase was takeoff (climb) 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 technical failure. During the takeoff roll and initial climb both engines were producing normal power. As the airplane climbed through 150 feet, the left engine lost power. The pilot reported that he feathered the left propeller. He further stated that following the securing of the left engine, the right engine began to 'power down.' The pilot reported that he was unable to maintain a climb attitude and was forced to land on the airport in a grassy area. The subsequent examination of the cockpit disclosed that the left engine throttle was in the full forward position, and the right throttle lever was in the mid-range position. Both propeller levers were found full forward. The left engine mixture lever was in the full forward position, and the right mixture lever full aft, or lean, position. The functional check of both engines was conducted. Initially the left engine would not start, but after troubleshooting the fuel system, the left fuel boost pump was determined to have been defective. The 'loss of engine power after liftoff' checklist requires that the pilot identify the inoperative engine and to feather the propeller for the inoperative engine.

Aircraft reference details include registration N601JS, MSN 60-0553-179, year of manufacture 1978.

Geospatial coordinates for this crash are approximately 32.3777°, -86.3091°.

Fatalities

Total

0

Crew

0

Passengers

0

Other

0

Crash Summary

During the takeoff roll and initial climb both engines were producing normal power. As the airplane climbed through 150 feet, the left engine lost power. The pilot reported that he feathered the left propeller. He further stated that following the securing of the left engine, the right engine began to 'power down.' The pilot reported that he was unable to maintain a climb attitude and was forced to land on the airport in a grassy area. The subsequent examination of the cockpit disclosed that the left engine throttle was in the full forward position, and the right throttle lever was in the mid-range position. Both propeller levers were found full forward. The left engine mixture lever was in the full forward position, and the right mixture lever full aft, or lean, position. The functional check of both engines was conducted. Initially the left engine would not start, but after troubleshooting the fuel system, the left fuel boost pump was determined to have been defective. The 'loss of engine power after liftoff' checklist requires that the pilot identify the inoperative engine and to feather the propeller for the inoperative engine.

Cause: Technical failure

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

Montgomery – Columbus

Flight Type

Private

Flight Phase

Takeoff (climb)

Crash Site

Airport (less than 10 km from airport)

Region / Country

North America • United States of America

Aircraft Details

Registration

N601JS

MSN

60-0553-179

Year of Manufacture

1978