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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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NTSB Report

May 6, 1993 · Witts & Church Worloch · N3201K

Lucerne, CO

Overview

Report Status
Probable Cause
Event Type
Accident
Date
May 6, 1993
Injury Outcomes
1 injury (1 fatality)
Location
Lucerne, CO
Aircraft
Witts & Church Worloch
Tail Number
N3201K
Operator
Witts P & Church L
Injuries
Fatal
Aircraft Damage
Destroyed
NTSB Number
DEN93FA054

The airplane required considerable left rudder in most flight attitudes, so the pilot fabricated a part to increase the angle on incidence by offsetting the leading edge of the vertical stabilizer. After installing the part, he took off on a test flight and his partner followed in a chase airplane. The airplane was observed to enter a shallow descent and yaw slightly about its vertical axis, also described as shallow Dutch rolls. The pilot said he had a problem and the airplane impacted terrain shortly thereafter. The fabricated part was never found. A small hole had been drilled through the tube where the leading edge of the vertical stabilizer attaches, but no hole had been drilled through the mating tube. There was evidence that a pin had previously been safetied through this hole. It could not be determined if the pilot had inserted the pin prior to taking off. Load carrying brace wires beneath the horizontal stabilizers were found stretched in tension.

NTSB Probable Cause

LOSS OF CONTROL IN FLIGHT. A FACTOR WAS: THE PILOT'S LACK OF EXPERIENCE IN THE AIRPLANE.

Full Narrative

THE AIRPLANE REQUIRED CONSIDERABLE LEFT RUDDER IN MOST FLIGHT ATTITUDES, SO THE PILOT FABRICATED A PART TO INCREASE THE ANGLE ON INCIDENCE BY OFFSETTING THE LEADING EDGE OF THE VERTICAL STABILIZER. AFTER INSTALLING THE PART, HE TOOK OFF ON A TEST FLIGHT AND HIS PARTNER FOLLOWED IN A CHASE AIRPLANE. THE AIRPLANE WAS OBSERVED TO ENTER A SHALLOW DESCENT AND YAW SLIGHTLY ABOUT ITS VERTICAL AXIS, ALSO DESCRIBED AS SHALLOW DUTCH ROLLS. THE PILOT SAID HE HAD A PROBLEM AND THE AIRPLANE IMPACTED TERRAIN SHORTLY THEREAFTER. THE FABRICATED PART WAS NEVER FOUND. A SMALL HOLE HAD BEEN DRILLED THROUGH THE TUBE WHERE THE LEADING EDGE OF THE VERTICAL STABILIZER ATTACHES, BUT NO HOLE HAD BEEN DRILLED THROUGH THE MATING TUBE. THERE WAS EVIDENCE THAT A PIN HAD PREVIOUSLY BEEN SAFETIED THROUGH THIS HOLE. IF COULD NOT BE DETERMINED IF THE PILOT HAD INSERTED THE PIN PRIOR TO TAKING OFF. LOAD CARRYING BRACE WIRES BENEATH THE HORIZONTAL STABILIZERS WERE FOUND STRETCHED IN TENSION.

Flight

Event TypeAccident
Event Time17:50 MDT
Nearest Airport0nm N
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftWitts & Church Worloch
Tail NumberN3201K
Aircraft CategoryAir
DamageDestroyed
OperatorWitts P & Church L
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsRotax · 582 · Reciprocating · 67
Seats2

People & Injuries

Injury Summary1 injury (1 fatality)
Fatal1
Serious0
Minor0
Uninjured0
Total1
Crew 1Age 30 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind170° @ 11 kt, gusting 14 kt
Visibility10 sm
CeilingBroken clouds 9000 ft
Temperature / Dew Point64 F / 27 C
Altimeter29.00 inHg
Observation Time00:15
Weather SourceWFAC

Appendix: Source Data