MIA98LA018

NTSB accident investigation · Saldairiaga Buccaneer II · Clermont, FL · November 1, 1997

Accident · FatalLimited investigationFinal report
Date
November 1, 1997, 15:48 local (20:48 UTC)
Place
Clermont, FL
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N813LJSaldairiaga Buccaneer II
Weather
Visual (VMC) · Day
Status
Completed · report June 26, 1998
Report
Approved by Office Director
FAA report
19971101031609A
Case key
38422

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The NTSB’s determination of the probable cause, and any contributing factors.

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.

Analysis

Witnesses stated they observed the airplane start a steep left turn, estimated more than a 45 degree angle of bank, between 150 to 300 feet 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 and flight control assembly revealed no evidence of a precrash mechanical failure or malfunction.

Factual narrative

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.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of control - in flightManeuvering
Maneuver - initiatedPilot in command
Airspeed - inadequatePilot in commandCause
Stall - inadvertentPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled

Aircraft

Registration
N813LJ
Reported as
Saldairiaga Buccaneer II (BUCCANEER)
Category
Ultralight, amateur-built
Serial number
B2B-KO22
Engine
Rotax, reciprocating
Damage
Destroyed
Flight
Personal · Part 91
Registered owner
Gerald M. Crouch
Airworthiness certificate
Special, Experimental (Special)
Departed
3WF4

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
54
Certificate
Student
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Left
Toxicology
Performed
Flight hours
500 total

Weather

Conditions
Visual (VMC) · Day
Wind
Variable at 4 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
84 °F, dew point 70 °F
Observed at
LEE, 20 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.