N2186B

Substantial
Minor

Davis/Cleaver RENEGADE 2 S/N: 0022

Accident Details

Date
Sunday, April 11, 1999
NTSB Number
FTW99LA115
Location
PORT ALLEN, LA
Event ID
20001205X00467
Coordinates
30.449195, -91.199943
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The loss of engine power for undetermined reasons. A factor was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
N2186B
Make
DAVIS/CLEAVER
Serial Number
0022
Engine Type
Reciprocating
Year Built
1986
Model / ICAO
RENEGADE 2 DA2
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
CLEAVER BOB
Address
7400 THUNDERBIRD BEACH LANE
Status
Deregistered
City
WATSON
State / Zip Code
LA 70786
Country
United States

Analysis

On April 11, 1999, at 1530 central daylight time, a Davis/Cleaver Renegade 2 homebuilt experimental airplane, N2186B, was substantially damaged when it impacted trees and terrain during a forced landing following a loss of engine power near Port Allen, Louisiana. The private pilot, sole occupant, received minor injuries. The pilot and another private individual were the builders and owners of the biplane. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 local personal flight, which originated 30 minutes prior to the accident.

According to the pilot, the airplane was turning to final approach for a private grass strip, when the engine lost power. The pilot tried to avoid a residential area by flying toward an open area along the final approach path. During the approach, the biplane clipped a pecan tree resulting in the aircraft spinning around and impacting the ground in a nose low attitude. Witnesses to the accident helped the pilot out of the rear seat of the tandem-seat airplane.

According to an FAA inspector, the engine, forward of the firewall, was buried in the ground. The front cockpit area was "heavily" damaged. The left wings were crushed aft approximately 12 inches, and the right wings sustained little damage. The FAA inspector confirmed flight control continuity at the accident site along with the presence of fuel in the tanks.

The other owner of the experimental airplane, who was also the designated repairman for the aircraft, stated that he could not find any problems with the Rotax engine after the accident. The carburetor was destroyed, making it impossible to examine. He had flown the airplane 20 minutes prior to the accident flight and did not note any problems. The repairman completed a condition inspection of the airplane on April 1, 1999.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW99LA115