DEN84FTM01

NTSB accident investigation · Keith A Smith KR-2 · Salt Lake City, UT · February 26, 1984

Accident · FatalFinal report
Date
February 26, 1984, 00:00 local (07:00 UTC)
Place
Salt Lake City, UT
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N54KSKeith A Smith KR-2
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19840226004789A
Case key
16254

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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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/malfManeuvering
Mixture control - incorrectCause
Maintenance,adjustment - improperOther maintenance personnelCause
Lack of total experienceOther maintenance personnelFactor
Engine assembly,piston - overtemperatureCause
Engine assembly,valve,intake - overtemperatureCause
Forced landingManeuvering - turn to landing area (emergency)
Terrain condition - high terrainFactor
Terrain condition - none suitableFactor
Loss of control - in flightManeuvering - turn to landing area (emergency)
Weather condition - high density altitudeFactor
Airspeed - not maintainedPilot in commandCause
Stall/spin - inadvertentPilot in command
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - mountainous/hillyFactor

Analysis

The acft collided with a mountain ridge in a flat'pancake'attitude,no evidence of foward motion was apparent and all thewreckage was confined to the immediate area. The wooden prop was intact with the exception of 2 inches missing from the end of one blade, and no rotational damage WA noted. The fuselage was twisted to the right and detached from the wings. Rock under the wreckage were pressed straight down into the surface. The accident location was about 1/2 way up a 6500 ft ridge which formed a box canyon know as deadman's wash. The engine log was noted for all flts & indicated the engine had an overheat problem. This engine was built as'new'by the plt from parts and plans as obtained from hapi engines. The plt had limited experience with powerplants. Post accident inspection showed that the mixture control metering rod was noted to have only half of the metering orfice open at full rich mixture. This would cause a lean mixture at full rich. The pistons and valves showed evidence of operating at excessive temperatures with excessive wear.

Aircraft

Registration
N54KS
Reported as
Keith A Smith KR-2
Category
Airplane, amateur-built
Serial number
3923
Airframe hours
15
Engine
Volkswagen 1835, 60 horsepower, reciprocating
Damage
Destroyed
Flight
Personal · Part 91
Registered owner
Keith A Smith
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Unknown · November 3, 1983 · 15 hours before
Departed
U42 · West Jordan, UT

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
29
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Left
Toxicology
Performed
Flight hours
221 total · 5 in this make and model · 189 as pilot in command · 4 in the last 90 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
10° at 8 knots
Visibility
20 statute miles
Lowest ceiling
None
Temperature
37 °F, dew point 27 °F
Altimeter
30.00 inHg
Observed at
SLC, 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.