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Aviation safety reports, made easier to study

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February 26, 1984 · Keith A Smith KR-2 · N54KS

Salt Lake City, UT

Overview

Report Status
Preliminary report
Event Type
Accident
Date
February 26, 1984
Injury Outcomes
1 injury (1 fatality)
Location
Salt Lake City, UT
Aircraft
Keith A Smith KR-2
Tail Number
N54KS
Injuries
Fatal
Aircraft Damage
Destroyed
NTSB Number
DEN84FTM01

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.

Full Narrative

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.

Flight

Event TypeAccident
Event Time00:00 MST
Nearest Airport0nm N
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftKeith A Smith KR-2
Tail NumberN54KS
Aircraft CategoryAir
DamageDestroyed
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsVolkswagen · 1835 · Reciprocating · 60
Seats2

People & Injuries

Injury Summary1 injury (1 fatality)
Fatal1
Serious0
Minor0
Uninjured0
Total1
Crew 1Age 29 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind10° @ 8 kt
Visibility20 sm
CeilingNone
Temperature / Dew Point37 C / 27 C
Altimeter30.00 inHg
Observation Time20:50
Weather SourceWFAC

Appendix: Source Data