N8654L

Substantial
Fatal

Piper PA-25-235 S/N: 25-5098

Accident Details

Date
Wednesday, August 12, 1998
NTSB Number
MIA98LA222
Location
BAINBRIDGE, GA
Event ID
20001211X10918
Aircraft Damage
Substantial
Highest Injury
Fatal
Fatalities
1
Serious Injuries
0
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The pilot's failure to maintain airspeed resulting in a stall.

Aircraft Information

Registration
N8654L
Make
PIPER
Serial Number
25-5098
Engine Type
Reciprocating
Year Built
1969
Model / ICAO
PA-25-235 PA25
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
HOWELL WILLIAM F
Address
PO BOX 648
Status
Deregistered
City
BAINGRIDGE
State / Zip Code
GA 31717
Country
United States

Analysis

On August 12, 1998, at an unknown time, a Piper PA-25-235, N8654L, registered to a private owner, operating as AG Flight Inc, as a 14 CFR Part 137 aerial application training flight, crashed in the vicinity of Bainbridge, Georgia. Visual meteorological conditions prevailed and no flight plan was filed. The airplane sustained substantial damage. The private pilot was fatally injured. The flight originated from Decatur County Industrial Airpark, Bainbridge, Georgia, at about 1115.

An instructor pilot for the operator stated the pilot did not return from a simulated aerial application run. Attempts to locate the pilot by radio were uneventful. An air search was initiated and the airplane was located at about 1207.

The wreckage of N8654L was located in a wooded area south of Brinson Air Base Road, Bainbridge, Georgia, about 2 miles west of Decatur County Industrial Airpark.

Examination of the crashsite revealed the airplane collided with the ground in a near vertical nose down, right wing low attitude. The leading edge of the right wing sustained sustained "accordion pleats starting just inboard of the lift struts, increasing in magnitude toward the tip which was bent up." The left wing had separated from the fuselage at the trailing edge. Both the hopper and fuel tanks were ruptured. One propeller blade was straight with signs of rotational abrasion on the back. The other propeller blade was bent back with evidence of torsional twisting.

Examination of the flight control system, engine assembly and accessories revealed no evidence of a precrash mechanical failure or malfunction. Continuity of the flight control system was confirmed for pitch, roll, and yaw. (For additional information see FAA Inspector Statement).

Postmortem examination of the pilot was conducted by Dr. Mark A. Koponen, Medical Examiner, Georgia Bureau of Investigation, Decatur, Georgia, on August 14, 1998. The cause of death was multiple blunt force injuries. Postmortem toxicology of specimens from the pilot was performed by the Forensic Toxicology Research Section, 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# MIA98LA222