N246DB

Substantial
Minor

Bair Helicopters, Inc. SEAREY S/N: MK-013

Accident Details

Date
Sunday, March 26, 2000
NTSB Number
MIA00LA119
Location
KILL DEVIL HILL, NC
Event ID
20001212X20702
Coordinates
36.009986, -75.660110
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The inadvertent stall by the pilot-in-command while on final approach resulting in the uncontrolled descent and in-flight collision with water.

Aircraft Information

Registration
N246DB
Make
BAIR HELICOPTERS, INC.
Serial Number
MK-013
Engine Type
None
Year Built
1994
Model / ICAO
SEAREY FK9
No. of Engines
0

Registered Owner (Historical)

Name
TAIL FEATHER LLC
Address
PO BOX 28
Status
Deregistered
City
KILL DEVIL HILLS
State / Zip Code
NC 27948-0028
Country
United States

Analysis

On March 26, 2000, about 1554 eastern standard time, a homebuilt amphibious SeaRey, N246DB, registered to Tail Feather LLC, experienced an in-flight loss of control and crashed into Roanoke Sound near Kill Devil Hills, North Carolina. Visual meteorological conditions prevailed at the time and no flight plan was filed for the 14 CFR Part 91 personal flight. The airplane was substantially damaged and the commercial-rated pilot and one passenger sustained minor injuries. The flight originated about 1530, from Kill Devil Hills, North Carolina.

The pilot stated that after takeoff he performed one touch-and-go landing on the water where the airplane is based then flew north of there then returned and performed one touch-and-go landing on the water. While turning left base to final for the planned 3rd touch-and-go landing, with 10 degrees of flaps extended, in a 15-20 degree angle of bank, and with the power reduced, the passenger called out that the indicated airspeed was 55 miles per hour. The pilot later reported that he did not monitor the airspeed during the turn. He applied partial power; the engine responded, then lowered the nose. He then applied aft elevator input with no response. The airplane contacted the water while in a left wing low attitude. He further reported that there was no engine or flight control preimpact failure or malfunction and just before impact with the water the flight encountered a wind gust.

According to one of the co-owners of the airplane, he verified aileron, rudder, and elevator flight control continuity from the cockpit to each control surface after the accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA00LA119