SEA96LA196

NTSB accident investigation · Westcott Glasair I-FT · Puyallup, WA · August 21, 1996

Accident · Serious injuriesLimited investigationFinal report
Date
August 20, 1996, 17:15 local (Aug 21, 1996, 00:15 UTC)
Place
Puyallup, WA
Injuries
1 serious, 1 uninjured; on the ground: 1 serious
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N289WWestcott Glasair I-FT
Weather
Visual (VMC) · Day
Status
Completed · report May 23, 1997
Report
Approved by Office Director
FAA report
19960821023409A
Case key
42449

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

failure of the air inlet screen, and subsequent ingestion of the foam air filter. An inadequate maintenance modification by the amateur builder and no suitable landing area were related factors.

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 power(total) - mech failure/malfTakeoff - initial climb
Induction air control,air filter/screen - failureCause
Maintenance,modification - inadequateOwner/builderFactor
Induction air control,air filter/screen - ingestedCause
Ram/induction air - blocked(total)Cause
Forced landingEmergency descent/landing
On ground/water collision with objectEmergency landing
Terrain condition - none suitableFactor
Object - vehicle

Analysis

The pilot reported that during climb-out after completing a touch-and-go, the engine lost power at 300 to 400 feet above ground level. The pilot stated that there was not a suitable landing site, and he opted to make a forced landing to a roadway. During touchdown, the airplane collided with two occupied vehicles. An engine inspection revealed that the inlet screen to the carburetor air box had been fabricated with an approximate half-inch square metal meshing. The wire on the screen had broken and had allowed the foam air filter to be sucked into the throat of the carburetor.

Factual narrative

On August 20, 1996, at 1715 Pacific daylight time, a homebuilt Westcott Glasair I-FT, N289W, operated by and registered to the pilot as a 14 CFR Part 91 personal flight, experienced a loss of engine power shortly after takeoff from Pierce County-Thun Field, Puyallup, Washington. The pilot initiated a forced landing to a city road where, during the landing roll, the airplane collided with two vehicles. Visual meteorological conditions prevailed at the time and no flight plan was filed for the local flight. The airplane was substantially damaged and the commercial pilot was not injured. One person in one vehicle was seriously injured, the other person in another vehicle was not injured. The flight departed from Pierce County approximately one-half hour prior to the accident.

During a telephone interview and subsequent written statement, the pilot stated that the purpose of the flight was to test a newly installed accelerometer. The pilot spent some time performing various maneuvers before returning to the airport to practice touch-and-go landings. After the second takeoff, the pilot stated that at approximately 300-400 feet above ground level, the engine lost power. The pilot was unable to restart the engine and initiated a forced landing. The pilot stated that an open field was unattainable and there were no other suitable landing sites so he elected to aim for and land on a roadway. During the touchdown, the airplane collided with two occupied vehicles.

An inspection of the engine revealed that the inlet screen to the carburetor air box had been fabricated with an approximate half-inch square metal meshing. The wire on the screen broke, allowing the foam air filter to be sucked into the throat of the carburetor.

Aircraft

Registration
N289W
Reported as
Westcott Glasair I-FT (GLASAIR I-)
Category
Airplane, amateur-built
Serial number
289
Airframe hours
106
Engine
Lycoming O-360-A1A, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Robert B. Goodman
Airworthiness certificate
Special, Experimental (Special)
Last inspection
100 hour · May 17, 1996 · 21 hours before

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
62
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
4,982 total · 26 in this make and model · 3,270 as pilot in command · 25 in the last 90 days · 13 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
Variable at 6 knots
Visibility
7 statute miles
Lowest ceiling
6,500 ft broken
Temperature
70 °F, dew point 50 °F
Altimeter
30.00 inHg
Observed at
TCM, 15 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.