SEA97LA142

NTSB accident investigation · Glaser-Dirks DG-400 · Weston, OR · June 14, 1997

Accident · No injuriesLimited investigationFinal report
Date
June 14, 1997, 15:20 local (22:20 UTC)
Place
Weston, OR
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N321VGlaser-Dirks DG-400
Weather
Visual (VMC) · Day
Status
Completed · report April 24, 1998
Report
Approved by Office Director
FAA report
19970614018429A
Case key
42633

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

The NTSB’s determination of the probable cause, and any contributing factors.

The pilot's failure to attain a proper descent rate during the forced landing. Factors include: the pilot's failure to use an 'engine start' checklist, failure to turn the ignition switch to the 'on' position, failure to use the landing checklist, failure to lower the wing flaps, and lack of experience in this make and model aircraft.

Analysis

After using the engine to take off and fly to the area where he was going to soar, the pilot retracted the engine into the fuselage. When he was finished soaring, the pilot extended the engine and attempted to restart it. When he could not get it to restart after several attempts, the pilot elected to make a forced landing in an open field. Because the aircraft was low to the ground when the pilot gave up on his attempts to get the engine started, he did not have time to retract the engine, and he forgot to extend the wing flaps. Because the engine was extended and the flaps were in the up position, the aircraft touched down with an excessive rate of descent. The force of the impact caused both wings to flex downward and contact the terrain. One wing became stuck in the soft dirt, and as the aircraft was spun around, its structure received substantial damage. According to the pilot, the reason his engine would not start was because he had forgotten to move the ignition switch to the 'on' position prior to attempting the engine start. He also stated that he had recently purchased the aircraft, and that he did not use a checklist for the engine start, nor did he use a before landing checklist. He further stated that the gliders he was accustomed to flying did not have wing flaps.

Factual narrative

On June 14, 1997, approximately 1520 Pacific daylight time, a Glaser-Dirks DG-400 powered glider, N321V, impacted the terrain during an off-airport forced landing near Weston, Oregon. The commercial pilot, who was the sole occupant, was not injured, but the aircraft, which was owned and operated by the pilot, sustained substantial damage. The local 14 CFR Part 91 personal pleasure flight, which departed Vista Field, Kennewick, Washington about 30 minutes earlier, was being operated in visual meteorological conditions at the time of the accident. No flight plan had been filed, and there was no report of an ELT activation.

According to the pilot, who reported that he had recently purchased the aircraft, he used the aircraft's engine to take off and fly to the area where he was going to soar. Upon reaching that area, he shut down the engine and retracted it into the fuselage. When he finished soaring, the pilot extended the engine and attempted to get it started in order to fly back to the airport of departure. Because it would not start after several attempts, and because he did not have enough altitude to reach an airport, he elected to make a forced landing in a open field. Although he wanted to retract the engine into the fuselage before landing, the aircraft was so low by the time the pilot gave up on getting the engine started that he did not have time to retract it. Just prior to touchdown, the pilot lowered the landing gear, but he forgot to lower the flaps to landing position, and they remained fully retracted during the landing. Because the pilot was attempting to land with the engine extended and the flaps retracted, the aircraft contacted the terrain at an excessive rate of descent. According to the pilot, "The force of the impact drove the cockpit area of the fuselage into the soft dirt and both wings flexed down, striking the soil." The left wing of the glider caught the dirt, and as it was spun around, its structure sustained substantial damage.

The pilot further stated that after the accident he realized that because he was new to the aircraft, he had forgotten to move the ignition switch to the "ON" position before trying to get the engine started. He said that there appeared to be no other problem with the engine. He also said that he did not use a restart or before landing checklist, and that the gliders he was accustomed to flying did not have wing flaps.

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
Checklist - not usedPilot in commandFactor
Electrical system - improper use ofPilot in commandFactor
Lack of total experience in type of aircraftPilot in commandFactor
Forced landingEmergency descent/landing
Hard landingLanding - flare/touchdown
Checklist - not usedPilot in commandFactor
Flaps - not deployedPilot in commandFactor
Lack of total experience in type of aircraftPilot in commandFactor
Proper descent rate - not attainedPilot in commandCause

Aircraft

Registration
N321V
Reported as
Glaser-Dirks DG-400
Category
Airplane
Serial number
4-149
Airframe hours
75
Engine
Rotax 505, 45 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Thomas A. Seim
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · April 4, 1997 · 25 hours before
Departed
S98 · Kennewick, WA

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
49
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Front
Flight hours
1,812 total · 21 in this make and model · 1,734 as pilot in command · 24 in the last 90 days · 12 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
60 statute miles
Lowest ceiling
None
Temperature
81 °F

FAA reports on this event · 1

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