FTW92LA125

NTSB accident investigation · Shewmaker BD5 · Castroville, TX · May 3, 1992

Accident · Serious injuriesLimited investigationFinal report
Date
May 2, 1992, 20:15 local (May 3, 1992, 01:15 UTC)
Place
Castroville, TX
Injuries
1 serious
Damage
Destroyed
Phase of flight
Approach
Aircraft
N68DSShewmaker BD5
Weather
Visual (VMC) · Day
Status
Completed · report July 26, 1993
Report
Approved by Office Director
FAA report
19920502019489A
Case key
18488

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 pilot's failure to maintain aircraft control during the flare. Factors were the engagement of the propeller feathering system and the pilot's total lack of experience in type aircraft and the slipped propeller pitch change system.

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.

Airframe/component/system failure/malfunctionApproach
Propeller system/accessories,pitch change mech - slippedFactor
Propeller system/accessories,feathering system - engagedFactor
Forced landingDescent - emergency
In flight collision with terrain/waterLanding - flare/touchdown
Aircraft control - not maintainedPilot in commandCause
Lack of total experience in type of aircraftPilot in commandFactor

Analysis

The pilot was attempting a high speed taxi test when the airplane became airborne. A normal climb was made to approximately 1,000 feet AGL. The pilot made several left turns while in level flight and proceeded back toward the airport. During the approach, the propeller system's variable control mechanism slipped which allowed the propeller to go to the full feather position. The airplane's airspeed was between 160 to 180 mph when this occurred, according to the pilot. The airspeed then dropped to approximately 100 mph and the pilot initiated a forced landing to an open field. During the flare prior to touchdown, the pilot added power and the airplane yawed. The left wing tip struck the ground and the pilot lost control of the airplane which then impacted the terrain. The pilot stated the propeller control system probably vibrated loose during the flight. This system is controlled by the pilot from the cockpit with a vernier knob. The pilot built the airplane and had not flown it before the accident.

Aircraft

Registration
N68DS
Reported as
Shewmaker BD5
Category
Airplane, amateur-built
Serial number
0014
Airframe hours
1
Engine
Honda EB3, 105 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Part 91
Operator
Shewmaker, Darryl D.
Registered owner
Shewmaker, Darryl D.
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Unknown · January 2, 2000

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
44
Certificates
Flight instructor, Airline transport, Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--w/ waivers/lim
Seat
Center
Flight hours
17,650 total · 1 in this make and model · 17,350 as pilot in command · 145 in the last 90 days · 45 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
130° at 9 knots
Visibility
8 statute miles
Lowest ceiling
4,000 ft broken
Temperature
81 °F, dew point 66 °F
Altimeter
30.00 inHg
Observed at
SAT, 20 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.