Shelter Cove - Willits

Prior to departure the pilot believed that his airplane contained between 30 and 40 gallons of fuel, adequate for a 15-minute-long flight to another airport where he could purchase additional fuel. The pilot reported the fuel gauge registered 40 gallons, so he departed. During initial climb upon reaching an altitude of about 400 feet above the ocean, both engines simultaneously lost power. The pilot rocked the airplane's wings and experienced a 'short surge of power.' However, it lasted only a brief moment and all engine power was again totally lost. The pilot turned toward the shoreline, reduced airspeed, and ditched about 0.25 miles off shore. The overnight tide/wave action subsequently beached most of the airplane. In the pilot's report, he did not indicate having experienced any mechanical malfunctions. The Federal Aviation Administration (FAA) coordinator examined recovered portions of the airframe and engines. In pertinent part, the FAA reported finding no physical evidence of any mechanical malfunction with the examined components. However, because of the airframe damage sustained during immersion in the salt water and the subsequent destruction to components, the Safety Board was unable to document the integrity of the fuel quantity indicator system.

Flight / Schedule

Shelter Cove - Willits

Registration

C-FBCR

MSN

500-1376-135

Year of Manufacture

1963

Date

March 18, 1999 at 06:35 PM

Type

CRASH

Flight Type

Private

Flight Phase

Takeoff (climb)

Crash Site

Lake, Sea, Ocean, River

Crash Location

Shelter Cove California

Region

North America • United States of America

Coordinates

40.0380°, -124.0557°

Crash Cause

Technical failure

Narrative Report

On March 18, 1999 at 06:35 PM, Shelter Cove - Willits experienced a crash involving Rockwell Aero Commander 500, operated by Thomas M. Fisher, with the event recorded near Shelter Cove California.

The flight was categorized as private and the reported phase was takeoff (climb) at a lake, sea, ocean, river crash site.

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

The listed crash cause is technical failure. Prior to departure the pilot believed that his airplane contained between 30 and 40 gallons of fuel, adequate for a 15-minute-long flight to another airport where he could purchase additional fuel. The pilot reported the fuel gauge registered 40 gallons, so he departed. During initial climb upon reaching an altitude of about 400 feet above the ocean, both engines simultaneously lost power. The pilot rocked the airplane's wings and experienced a 'short surge of power.' However, it lasted only a brief moment and all engine power was again totally lost. The pilot turned toward the shoreline, reduced airspeed, and ditched about 0.25 miles off shore. The overnight tide/wave action subsequently beached most of the airplane. In the pilot's report, he did not indicate having experienced any mechanical malfunctions. The Federal Aviation Administration (FAA) coordinator examined recovered portions of the airframe and engines. In pertinent part, the FAA reported finding no physical evidence of any mechanical malfunction with the examined components. However, because of the airframe damage sustained during immersion in the salt water and the subsequent destruction to components, the Safety Board was unable to document the integrity of the fuel quantity indicator system.

Aircraft reference details include registration C-FBCR, MSN 500-1376-135, year of manufacture 1963.

Geospatial coordinates for this crash are approximately 40.0380°, -124.0557°.

Fatalities

Total

0

Crew

0

Passengers

0

Other

0

Crash Summary

Prior to departure the pilot believed that his airplane contained between 30 and 40 gallons of fuel, adequate for a 15-minute-long flight to another airport where he could purchase additional fuel. The pilot reported the fuel gauge registered 40 gallons, so he departed. During initial climb upon reaching an altitude of about 400 feet above the ocean, both engines simultaneously lost power. The pilot rocked the airplane's wings and experienced a 'short surge of power.' However, it lasted only a brief moment and all engine power was again totally lost. The pilot turned toward the shoreline, reduced airspeed, and ditched about 0.25 miles off shore. The overnight tide/wave action subsequently beached most of the airplane. In the pilot's report, he did not indicate having experienced any mechanical malfunctions. The Federal Aviation Administration (FAA) coordinator examined recovered portions of the airframe and engines. In pertinent part, the FAA reported finding no physical evidence of any mechanical malfunction with the examined components. However, because of the airframe damage sustained during immersion in the salt water and the subsequent destruction to components, the Safety Board was unable to document the integrity of the fuel quantity indicator system.

Cause: Technical failure

Occupants & Outcome

Crew On Board

1

Passengers On Board

1

Estimated Survivors

2

Fatality Rate

0.0%

Known people on board: 2

Operational Details

Schedule / Flight

Shelter Cove - Willits

Flight Type

Private

Flight Phase

Takeoff (climb)

Crash Site

Lake, Sea, Ocean, River

Region / Country

North America • United States of America

Aircraft Details

Registration

C-FBCR

MSN

500-1376-135

Year of Manufacture

1963