SEA95LA094

NTSB accident investigation · Grumman G-164B · Stayton, OR · May 7, 1995

Accident · Minor injuriesLimited investigationFinal report
Date
May 7, 1995, 14:20 local (21:20 UTC)
Place
Stayton, OR
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N6895QGrumman G-164B
Weather
Visual (VMC) · Day
Status
Completed · report February 14, 1996
Report
Approved by Office Director
FAA report
19950507009779A
Case key
42146

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

A power loss for undetermined reason(s). A factor was the soft terrain.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine powerManeuvering - aerial application
Reason for occurrence undeterminedCause
Forced landingEmergency landing
Nose overLanding - roll
Terrain condition - softFactor

Analysis

While initiating a spray run, the engine began surging and backfiring. The aircraft was 80 feet above ground, and with power lines in the pilot's flight path he elected to execute a forced landing. During the landing rollout in a dirt field the aircraft's wheels sank into the soil and the aircraft nosed over. Postcrash examination revealed no discrepancy with the magnetos or air induction system, and uncontaminated fuel was in the aircraft's fuel tanks.

Factual narrative

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.

Aircraft

Registration
N6895Q
Reported as
Grumman G-164B
Category
Airplane
Serial number
357B
Airframe hours
5,200
Engine
P&W R-985-AN1, 450 horsepower, reciprocating
Damage
Substantial damage
Flight
Aerial application · Part 137
Registered owner
Trans Ag, Inc.
Airworthiness certificate
Special, Restricted (Special)
Last inspection
Annual · October 7, 1994 · 193 hours before
Departed
5OR8 · OR

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
43
Certificate
Airline transport
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Front
Flight hours
7,556 total · 217 in this make and model · 4,170 as pilot in command · 90 in the last 90 days · 48 in the last 30 days · 5 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
360° at 4 knots
Visibility
20 statute miles
Lowest ceiling
4,500 ft overcast
Temperature
61 °F, dew point 46 °F
Altimeter
29.00 inHg
Observed at
SLE, 8 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.