SEA99LA161

NTSB accident investigation · Wild Goose A1 · Keizer, OR · September 10, 1999

Accident · No injuriesLimited investigationFinal report
Date
September 10, 1999, 15:20 local (22:20 UTC)
Place
Keizer, OR
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N3451Wild Goose A1
Weather
Visual (VMC) · Day
Status
Completed · report November 2, 2000
Report
Approved by Office Director
FAA report
19990910026309A
Case key
47390

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.

A loose fuel line fitting resulted in a loss of engine power. An intentional wheels down landing was a factor.

Analysis

The pilot reported that during the cruise climb, the engine suddenly experienced a short roughness and partial power loss. The engine then regained full power, followed by a complete power loss. The pilot was unable to restart the engine and a forced landing was initiated to an open field. As the aircraft continued to descend, the pilot realized that he would not make the field and diverted to the river. The pilot had been utilizing the amphibian aircraft as a land plane and had not retracted the landing gear after departure. There was not enough time to hand crank the landing gear up. Therefore, the aircraft landed with the gear extended. During the landing on the water, the aircraft nosed over. Post-crash inspection of the engine found a loose fuel line fitting to the fuel pump.

Factual narrative

On September 10, 1999, at 1520 Pacific daylight time, an experimental amphibian Wild Goose A1, N3451, registered to and operated by the pilot as a 14 CFR Part 91 personal flight, experienced a loss of engine power shortly after takeoff from Salem, Oregon. The pilot initiated a forced landing to a river near Keizer, Oregon. During the water landing, the aircraft nosed over. Visual meteorological conditions prevailed at the time and no flight plan was filed. The airplane was substantially damaged. The private pilot and pilot-rated passenger were not injured. The flight had departed from Salem about 20 minutes prior to the accident for a local flight.

During a telephone interview and subsequent written statement, the pilot reported that during the cruise climb with full power applied, the engine suddenly experienced a short roughness and partial power loss. The engine then regained full power, followed by a complete power loss. The second pilot set the aircraft's attitude for best glide, while the first pilot applied carburetor heat and checked the engine gauges and fuel controls. The second pilot turned the aircraft toward an open field, while the first pilot continued to try and restart the engine. The engine would not start. As the aircraft continued to descend, the pilots realized that because of obstructions, the airplane would not make the open field. The pilot then diverted to the river. The pilot stated that he was utilizing this aircraft as a land plane, and had not retracted the landing gear after takeoff. During the emergency descent, there was not enough time to hand crank the landing gear up before touchdown on the water. The aircraft touched down on the water with the landing gear extended. During the landing, the airplane nosed over.

After the aircraft was recovered from the river, a Federal Aviation Administration Inspector from the Hillsboro, Oregon, Flight Standards District Office, inspected the engine. During the inspection, a fuel line fitting to the fuel pump was found loose. The inspector also noted that the fuel lines were of a non-standard aviation quality/size material.

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 powerClimb - to cruise
Fuel system,line fitting - loose part/bolt/nut/clamp/etcCause
Forced landingEmergency descent/landing
Nose overLanding - roll
Wheels down landing in water - intentionalPilot in commandFactor

Aircraft

Registration
N3451
Reported as
Wild Goose A1
Category
Airplane, amateur-built
Serial number
337
Airframe hours
470
Engine
Lycoming O-320, 160 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Gregory A. Lambert
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · June 19, 1999 · 20 hours before
Departed
SLE · Salem, 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
40
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
2,300 total · 20 in this make and model · 2,040 as pilot in command · 39 in the last 90 days

Weather

Conditions
Visual (VMC) · Day
Wind
200° at 8 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
75 °F, dew point 45 °F
Altimeter
30.00 inHg
Observed at
SLE, 5 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.