N3212D

Substantial
None

Raytheon Aircraft Company B36TCS/N: EA-651

Accident Details

Date
Tuesday, September 16, 2003
NTSB Number
NYC03LA201
Location
Batavia, OH
Event ID
20031001X01631
Coordinates
39.078334, -84.210281
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A loss of engine power during an approach for undetermined reasons.

Aircraft Information

Registration
Make
RAYTHEON AIRCRAFT COMPANY
Serial Number
EA-651
Engine Type
Reciprocating
Model / ICAO
B36TCM360
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
6
FAA Model
B36TC

Registered Owner (Current)

Name
HALO AVIATION CORP
Address
5305 LIMESTONE RD STE 200
City
WILMINGTON
State / Zip Code
DE 19808-1247
Country
United States

Analysis

On September 16, 2003, about 1400 eastern daylight time, a Raytheon B36TC, N3212D, was substantially damaged during a forced landing, following a loss of engine power at Clermont County Airport (I69), Batavia, Ohio. The certificated private pilot was not injured. Visual meteorological conditions prevailed for the flight that departed Highland County Airport, Hillsboro, Ohio. No flight plan was filed for the personal flight conducted under 14 CFR Part 91.

The pilot stated that while on the downwind leg for runway 22, a 3,568-foot long runway, the engine lost all power. The pilot activated the electric fuel pump and turned base leg for the runway. The engine regained partial power, but would not develop full power. The pilot intentionally flew a high approach as a precaution, and the airplane touched down hard, about half-way down the runway. It bounced several times, skidded, and traveled off the end of the runway. During the overrun, the left main landing gear collapsed, and the right wing sustained substantial damage. The airplane came to rest upright in a grass area beyond the end of the runway.

A Federal Aviation Administration inspector examined the airplane after the accident. He noted approximately 27 gallons of fuel in each wing tank. The inspector, and a representative from the engine manufacturer, subsequently test ran the engine with no difficulty or discrepancies noted. The engine ran at idle and full power without interruption, and a successful magneto check at 1,700 rpm was completed.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC03LA201