N813LJ

Destroyed
Fatal

Saldairiaga BUCCANEER II S/N: B2B-KO22

Accident Details

Date
Saturday, November 1, 1997
NTSB Number
MIA98LA018
Location
CLERMONT, FL
Event ID
20001208X09217
Coordinates
28.550008, -81.750434
Aircraft Damage
Destroyed
Highest Injury
Fatal
Fatalities
1
Serious Injuries
0
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

failure of the pilot to maintain adequate airspeed, while maneuvering at a low altitude, which resulted in an inadvertent stall and subsequent in-flight collision with terrain.

Aircraft Information

Registration
N813LJ
Make
SALDAIRIAGA
Serial Number
B2B-KO22
Engine Type
Reciprocating
Model / ICAO
BUCCANEER II AT2P
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
CROUCH GERALD H
Address
340 BAYWEST NEIGHBORS CIRCLE
Status
Deregistered
City
ORLANDO
State / Zip Code
FL 32835
Country
United States

Analysis

On November 1, 1997, about 1548 eastern standard time, a Saldairiaga, Buccaneer II, N813LJ, operated by a private owner as a 14 CFR Part 91 personal flight, crashed in the vicinity of Clermont, Florida. Visual meteorological conditions prevailed and no flight plan was filed. The airplane was destroyed. The student pilot was fatally injured. The flight originated from Flying Gator Airpark, Clermont, Florida, about 1 hour 18 minutes before the accident.

Witnesses who knew the pilot stated they observed the airplane between 150 to 300 feet southwest of the airpark. The airplane entered a steep left turn, estimated more than a 45-degree angle of bank at a slow airspeed. The airplane appeared to enter an accelerated stall. The nose pitched down and the airplane collided with the ground in a left wing low nose-down attitude. Before the airplane collided with the ground the engine was heard to increase to full power.

Examination of the airframe, flight control system and engine assembly revealed no evidence of a precrash mechanical failure or malfunction. All components necessary for flight were present at the crash site. Continuity of the flight control system was confirmed for pitch, roll, and yaw. An examination of the engine assembly and accessories was not conducted based on statements provided by eyewitnesses indicating the engine was operating at time of impact with the terrain.

Postmortem examination of the pilot was conducted by Dr. Susan M. Rendon, Associate Medical Examiner District Five, Leesburg, Florida, on November 2, 1997. The cause of death was injuries related to the aircraft accident. Postmortem toxicology studies of specimens from the pilot was performed by the Forensic Toxicology Research Section, Federal Aviation Administration, Oklahoma City, Oklahoma. These studies were negative for alcohol, basic, acidic and neutral drugs.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA98LA018