N7220

Substantial
Minor

Grumman G-164AS/N: 896

Accident Details

Date
Friday, July 23, 2004
NTSB Number
SEA04LA139
Location
Nyssa, OR
Event ID
20040803X01132
Coordinates
43.886943, -117.083610
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The failure (fracture) of the number four cylinder head during an aerial application run. Factors include the soft crop-covered terrain.

Aircraft Information

Registration
Make
GRUMMAN
Serial Number
896
Engine Type
Reciprocating
Year Built
1972
Model / ICAO
G-164AG64T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
G-164A

Registered Owner (Current)

Name
MID CONTINENT AIRCRAFT CORP
Address
1601 HIGHWAY 84 EAST
City
HAYTI
State / Zip Code
MO 63851-1944
Country
United States

Analysis

On July 22, 2004, approximately 2030 mountain daylight time, a Grumman G-164A, nosed over after experiencing a main landing gear collapse during a forced landing in an agricultural field about two miles west of Nyssa, Idaho. The commercial pilot, who was the sole occupant, received minor injuries, and the aircraft, which was owned and operated by the pilot, sustained substantial damage. The 14 CFR Part 137 aerial application flight, which departed a local agricultural airfield, had been airborne for about 10 minutes at the time of the accident. The flight was taking place in visual meteorological conditions. No flight plan had been filed.

According to the pilot, during one of his application runs there was a loud bang, and the engine suddenly lost a significant amount of power. Since it appeared that he did not have enough power to remain airborne, he elected to execute a forced landing in a nearby agricultural field. Although the initial touchdown was uneventful, the main gear of the aircraft dug into the soft terrain, leading to a main gear collapse and a nose-over of the aircraft. According to both the pilot and the FAA Inspector who responded to the accident, it was determined that while the aircraft was in flight, the number four cylinder head had fractured near where the cylinder head was screwed into the cylinder barrel. The FAA Inspector said that the fracture was of such a nature that it kept the cylinder from developing the compression necessary for detonation of the fuel/air mixture.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA04LA139