N9364L

Destroyed
Minor

Gulfstream American AA-1A S/N: A414-0064

Accident Details

Date
Sunday, August 16, 1998
NTSB Number
NYC98LA168
Location
ERIAL, NJ
Event ID
20001211X10940
Aircraft Damage
Destroyed
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

Catastrophic failure of the number 2 engine cylinder, emanating from a corrosion pit on the outside cylinder wall. A factor was the pilot's diminished forward visibility due to oil on the windshield.

Aircraft Information

Registration
N9364L
Make
GULFSTREAM AMERICAN
Serial Number
A414-0064
Engine Type
Reciprocating
Model / ICAO
AA-1A AEA1
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SHAW AVIATION INC
Address
657 BELMONT AVE
Status
Deregistered
City
SOUTHAMPTON
State / Zip Code
PA 18966-3703
Country
United States

Analysis

On August 16, 1998, at 1942 Eastern Daylight Time, a Gulfstream American AA-1A, N9364L, was destroyed during a forced landing near Erial, New Jersey. The certificated commercial pilot received minor injuries. Visual meteorological conditions prevailed at the time of the accident. No flight plan was filed for the flight that departed Ocean City Municipal Airport (26N), New Jersey, about 1800, for Northeast Philadelphia Airport (PNE), Philadelphia, Pennsylvania. The aerial observation (traffic reporting) flight was conducted under 14 CFR Part 91.

The pilot stated that while at 1,500 feet, the airplane's engine developed a slight vibration. He checked the fuel pump on, the mixture rich, and changed fuel tanks. The vibrations increased, and were accompanied by smoke. The pilot heard an explosive "bang" and the cowling came up into his line of vision. Oil covered the pilot's side of the windscreen, and the engine was unable to maintain altitude.

According to a Federal Aviation Administration (FAA) Inspector, the airplane struck a telephone pole during the forced landing. Post-flight inspection revealed a catastrophic failure of the engine's number 2 cylinder.

The cylinder barrel was subsequently examined at the Textron-Lycoming facility in Williamsport, Pennsylvania. It was reported as manufactured in July 1996, with 1,780 hours of service. Inspection revealed a fracture between the first and second cooling fins, which had completely broken through the flange, and spiraled around the barrel. The outside surface of the cylinder, in the vicinity of the fracture, was heavily corroded in areas where paint had flaked off, as well as in areas under the remaining paint. Corrosion pitting was found in some areas up to .004 inches in depth.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC98LA168