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July 23, 2004 · Grumman G-164A · N7220

Nyssa, OR

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
July 23, 2004
Injury Outcomes
1 injury (1 minor injury)
Location
Nyssa, OR
Aircraft
Grumman G-164A
Tail Number
N7220
Operator
Donald L Taylor
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
SEA04LA139

During an aerial application run, the pilot heard a loud bang, and the engine suddenly lost a significant amount of power. Because the aircraft did not have enough power to remain airborne, the pilot 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. It was ultimately 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, and the fracture was of such a nature that it kept the cylinder from developing the compression necessary for detonation of the fuel/air mixture.

NTSB Probable Cause

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

Full Narrative

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.

Flight

Event TypeAccident
Event Time19:30 PDT
Nearest Airport0nm
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftGrumman G-164A
Tail NumberN7220
Aircraft CategoryAir
DamageSubstantial
OperatorDonald L Taylor
Operating RulePart 137
Engines1
Engine TypeReciprocating
Engine DetailsPratt & Whitney · R-985 · Reciprocating · 450
Seats1

People & Injuries

Injury Summary1 injury (1 minor injury)
Fatal0
Serious0
Minor1
Uninjured0
Total1
Crew 1Age 70 · Second Class · Minor

Conditions

ConditionsVMC
LightDaylight
Wind270° @ 10 kt
Visibility20 sm
CeilingNone
Temperature / Dew Point0 C
Altimeter0

Appendix: Source Data