N2190W

Substantial
Minor

Beech C23S/N: M-1560

Accident Details

Date
Tuesday, February 18, 2003
NTSB Number
ATL03LA047
Location
Valdosta, GA
Event ID
20030221X00246
Coordinates
30.782499, -83.276664
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The pilot's failure to maintain adequate airspeed during a go-around resulting in an inadvertent stall and collision with trees.

Aircraft Information

Registration
N2190W
Make
BEECH
Serial Number
M-1560
Engine Type
Reciprocating
Year Built
1974
Model / ICAO
C23BE23
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
A & E AIR LLC
Address
RR 2 BOX 2048
Status
Deregistered
City
MORVEN
State / Zip Code
GA 31638-9733
Country
United States

Analysis

On February 18, 2003, at 1730 eastern standard time, a Beech C23, N2190W, registered to A & E Air LLC and operated by a student pilot collided with terrain during final approach to Valdosta Regional Airport, Valdosta, Georgia. The instructional flight was operated under the provisions of Title 14 CFR part 91 with no flight plan filed. Visual meteorological conditions prevailed at the time of the accident. The student pilot received minor injuries, and the airplane was substantially damaged. The flight departed Valdosta Regional Airport, Valdosta, Georgia, on February 18, 2003 at 1700.

According to the student pilot, the airplane was high on approach to runway 17. The pilot contacted the Valdosta control tower and requested a go-around. The tower controller cleared the flight to make a right turn to enter a left downwind to runway 35. When the student pilot reached down to retract the flaps, the airplane stalled and collided into a stand of trees.

Examination of the wreckage site revealed the airplane came to rest in a stand of trees at the approach end of runway 17. Examination of the right wing revealed it separated from the airframe at the wing root. Approximately four feet of the outboard left wing was separated. The fuselage and empennage sections of the airframe were buckled. No mechanical or flight control malfunctions were reported by the student pilot.

Review of the pilots operating handbook revealed: Power off stall speeds as follows: flaps up, level 61 knots; flaps down (35 degrees), level, 50 knots. Maximum altitude loss during a normal stall recovery is approximately 300 feet.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL03LA047