N707BD

Substantial
None

Worgull HORNET S/N: 707

Accident Details

Date
Monday, September 11, 2000
NTSB Number
LAX00LA350
Location
CAMP VERDE, AZ
Event ID
20001212X22022
Coordinates
34.480541, -111.779220
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

Separation of the forward spark plug due to wear damage to the cylinder head threads. A factor in the accident was traffic on the highway and the pilot having to maneuver to avoid the traffic.

Aircraft Information

Registration
N707BD
Make
WORGULL
Serial Number
707
Engine Type
Reciprocating
Year Built
1998
Model / ICAO
HORNET BPAT
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
WORGULL ROBERT C
Address
2275 MOONEY LN
Status
Deregistered
City
CAMP VERDE
State / Zip Code
AZ 86322
Country
United States

Analysis

On September 11, 2000, at 0830 hours mountain standard time, an experimental Worgull Hornet, N707BD, experienced a loss of engine power and made a forced landing on Interstate 17 after takeoff from the Montezuma Airport, Camp Verde, Arizona. During the attempted landing, the airplane landed hard as the pilot was maneuvering to avoid obstacles. The airplane, owned and operated by the pilot under the provisions of 14 CFR Part 91, sustained substantial damage. The airline transport pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed for the personal flight. A flight plan had not been filed. The flight was originating at the time of the accident.

In an interview with a Safety Board investigator, the pilot stated that a spark plug was found detached from the forward cylinder. He reported that the spark plug threads in the cylinder heads are made out of aluminum and the threaded portions of the spark plug barrels are made of steel.

In the pilot's written statement to the Safety Board, he indicated that new spark plugs had been installed prior to the last flight, and that they were torqued to the manufacturer's recommendation of 110-inch pounds. He further indicated that there was deterioration of the threads inside of the cylinder head. He recommended a visual inspection of the spark plug threads and cylinder head threads during periodic spark plug removal.

A Federal Aviation Administration inspector examined the airplane at the owner's facilities on September 22, 2000. He noted that the threads on both cylinders showed evidence of wear and appeared flattened.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX00LA350