N6895Q

Substantial
Minor

GRUMMAN G-164B S/N: 357B

Accident Details

Date
Sunday, May 7, 1995
NTSB Number
SEA95LA094
Location
STAYTON, OR
Event ID
20001207X03560
Coordinates
44.810165, -122.719161
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

A POWER LOSS FOR UNDETERMINED REASON(S). A FACTOR WAS THE SOFT TERRAIN.

Aircraft Information

Registration
Make
GRUMMAN
Serial Number
357B
Engine Type
Reciprocating
Year Built
1977
Model / ICAO
G-164B G64T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
G-164B

Registered Owner (Current)

Name
PETRIK PATTY O
Address
939 11TH ST SW
City
SIDNEY
State / Zip Code
MT 59270-5207
Country
United States

Analysis

On May 7, 1995, approximately 1420 Pacific daylight time, a Grumman G-164B, N6895Q, registered to/operated by Trans Ag, Inc., and being flown by an airline transport pilot, was substantially damaged when it nosed over during the landing roll following a loss of power while initiating an aerial spray run near Stayton, Oregon. The pilot sustained minor injuries. Visual meteorological conditions prevailed and there was no flight plan in effect. The flight, which was to dispense fertilizer, was to have been operated under 14CFR137.

The pilot reported that upon arriving at the destination field and entering the spray pattern at an altitude of approximately 80 feet above ground the engine began to "quit and restart and backfire." The pilot rolled wings level, however, the surging/ backfiring continued and he elected to execute a forced landing due to power lines in his flight path. Upon touchdown in a soft dirt field the aircraft rolled approximately 300 feet after which the wheels sank into the soil and the aircraft nosed over.

The operator reported in a telephone conversation that subsequent to the accident the magnetos were checked and found to operate satisfactorily. Additionally, the air induction system was examined and found to be unobstructed. Uncontaminated fuel was found within both wings following the accident. Fuel is delivered to the engine by a gravity feed system. The Operator also reported that rapid accelerations of throttle may result in backfiring and a tendency for the engine to be slow to "spool up" with the corrective action being to reduce throttle as appropriate.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA95LA094