N525PW

Substantial
Minor

Walker Phil RV-6AS/N: 525

Accident Details

Date
Thursday, April 4, 2013
NTSB Number
CEN13LA220
Location
Spearfish, SD
Event ID
20130405X61906
Coordinates
44.480667, -103.839797
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The coil-distributor wire loosening in flight, which rendered the ignition system inoperative and subsequently caused the loss of engine power.

Aircraft Information

Registration
N525PW
Make
WALKER PHIL
Serial Number
525
Engine Type
Reciprocating
Year Built
2004
Model / ICAO
RV-6ARV6
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
VANSCHOIACK AARON L
Address
PO BOX 403
Status
Deregistered
City
HAYTI
State / Zip Code
SD 57241-0403
Country
United States

Analysis

On April 4, 2013, about 1640 mountain daylight time, an RV-6A airplane, N525PW, experienced a loss of engine power and conducted a forced landing near Spearfish, South Dakota. The private rated pilot and flight instructor received minor injuries and the airplane was substantially damaged. The airplane was registered to and operated by a private individual under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed for the flight that operated without a flight plan. The flight originated from the Black Hills Airport – Clyde Ice Field, Spearfish, South Dakota, about 1630.

According to the pilot, he had recently purchased the airplane and was flying the airplane back to his home airfield. After stopping at an en route airport for fuel, they departed, and were climbing through 6,000 feet when the engine suddenly lost power. The pilot added that he switched on the auxiliary fuel pump and ignition system; however, the engine did not restart. He then selected a pasture for the forced landing. During landing, the nose gear collapsed and the airplane came to rest inverted.

The responding Federal Aviation Administration (FAA) inspector examined the airplane on site and noted that the airplane’s fuselage and vertical stabilizer sustained substantial damage during the accident. The airplane was equipped with an automotive Chevrolet 4.6L engine adapted for aviation use. Further examination of the engine revealed that the carburetor’s air filter was dirty and partly clogged. Additionally, a wire that runs from the coil to the distributor was found disconnected from the coil terminal. The wire and distributor were the automotive type and had the traditional terminal male/female plug arrangement, without an additional locking mechanism.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN13LA220