N443MW

Substantial
Minor

WONDER VAN'S ACFT RV-6 S/N: 21057

Accident Details

Date
Tuesday, December 7, 1993
NTSB Number
ATL94LA027
Location
RIDGELAND, SC
Event ID
20001211X13821
Coordinates
32.480213, -80.980613
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

IMPROPER INSTALLATION OF THE MAGNETOS BY MAINTENANCE PERSONNEL, WHICH ALLOWED THE RIGHT MAGNETO TO COME LOOSE, OIL TO ESCAPE FROM THE ENGINE, AND SUBSEQUENT OIL STARVATION.

Aircraft Information

Registration
Make
WONDER
Serial Number
21057
Engine Type
Reciprocating
Model / ICAO
VAN'S ACFT RV-6 DH60
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
RV-6

Registered Owner (Current)

Name
KOWALSKI LOIS D
Address
6013 CASTLEGATE DR W APT D24
City
CASTLE ROCK
State / Zip Code
CO 80108-3472
Country
United States

Analysis

On December 7, 1993, at 1310 eastern standard time, a home built Wonder Van's Aircraft RV-6, N443MW, was substantially damaged following a collision with terrain during an emergency landing near Ridgeland, South Carolina. The airline transport pilot received minor injuries in the accident. The aircraft was being operated under 14 CFR Part 91 by the pilot. Visual meteorological conditions existed at the time, and no flight plan had been filed for the personal flight. The flight departed Lawrenceville, Georgia at 1200.

The pilot reported that prior to his initial descent, the engine developed a slight vibration of increasing intensity. The pilot then noted that during the descent, the vibration increased and the electronic tachometer on the right magneto went to zero. The pilot then reported that blue smoke entered the cockpit and oil began spilling onto the windscreen, followed by an engine failure. The pilot executed an emergency landing in a cotton field approximately 7 miles west of the Ridgeland airport. During landing roll, the landing gear hit an area of soft dirt and the airplane flipped over, causing damage to the vertical and horizontal stabilizers, rudder, and left wing.

Post accident investigation of the aircraft engine revealed that the right magneto had separated from the engine. There was a large hole in the top of the crankcase where the magneto had been mounted. The left magneto was also found in the early stages of separation. Both magnetos had been installed on the engine approximately 16 hours before the accident by a certified repair facility.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL94LA027