DEN01LA020

NTSB accident investigation · Thomas VP-1 · West Jordan, UT · December 8, 2000

Accident · Serious injuriesLimited investigationFinal report
Date
December 8, 2000, 12:45 local (19:45 UTC)
Place
West Jordan, UT
Injuries
1 serious
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N89KDThomas VP-1
Weather
Visual (VMC) · Day
Status
Completed · report November 1, 2001
Report
Approved by Office Director
FAA report
20001208028739A
Case key
50749

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 lack of suitable terrain for a forced landing. Contributing factors were the total loss of engine power due to the failure of the pilot to adjust the manual propeller pitch to permit the engine to achieve sufficient rpm for sustained flight, and the subsequent fouling of the spark plugs due to the over rich fuel condition.

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) - nonmechanicalTakeoff - initial climb
Propeller system/accessories,pitch change mechFactor
Maintenance,adjustment - improperOwner/builderFactor
Powerplant - underspeedFactor
Ignition system,spark plug - fouledFactor
Forced landingEmergency descent/landing
In flight collision with objectEmergency landing after takeoff
Object - building(nonresidential)
Terrain condition - none suitableCause

Analysis

The pilot said he was flight-testing the newly finished homebuilt airplane. The original plans called for a fixed pitch propeller. The pilot said that he had put a manually adjustable pitch propeller on the airplane, and he had adjusted it for cruise flight. He said that once he was airborne, the engine began "lugging" and quickly lost power. He started a right turn to crosswind, and simultaneously began to perform a forced landing. Subsequently, the airplane struck a building and some transmission wires before coming to rest. Postaccident examination of the engine by an FAA inspector revealed that the spark plugs were wet with fuel. The inspector also found heavy carbon deposits in the exhaust stack.

Factual narrative

On December 8, 2000, at approximately 1245 mountain standard time, a Thomas VP-1 homebuilt airplane, N89KD, was destroyed when it impacted the ground during a forced landing near Salt Lake City Municipal 2 Airport, West Jordan, Utah. The pilot received serious injuries. The pilot/builder was operating the airplane under Title 14 CFR Part 91. Visual meteorological conditions prevailed. No flight plan had been filed for this local personal flight that was originating at the time of the accident.

The pilot said he was flight-testing the newly finished homebuilt airplane. The original plans called for a fixed pitch propeller. The pilot said that he had put a manually adjustable pitch propeller on the airplane, and he had adjusted it for cruise flight. He said that once he was airborne, the engine began "lugging," and it quickly lost power. He started a right turn to crosswind, and simultaneously began to perform a forced landing. Subsequently, the airplane struck a building and some transmission wires. The airplane came to rest upright.

Postaccident examination of the engine by an FAA inspector revealed that the spark plugs were wet with fuel. The inspector also found heavy carbon deposits in the exhaust stack.

Aircraft

Registration
N89KD
Reported as
Thomas VP-1
Category
Airplane, amateur-built
Serial number
1
Engine
Volkswagen 1600 CC, 57 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Robert R. Thomas
Airworthiness certificate
Special, Experimental (Special)
Departed
U42

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
48
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Front
Flight hours
486 total · 1 in this make and model · 2 in the last 90 days · 1 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
320° at 6 knots
Visibility
6 statute miles
Lowest ceiling
15,000 ft broken
Temperature
102 °F, dew point 86 °F
Altimeter
29.00 inHg
Observed at
SLC, 10 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.