FTW90DPA05

NTSB accident investigation · Gyroflug SC01B160 · Mineral Wells, TX · June 10, 1990

Accident · FatalFinal report
Date
June 10, 1990, 08:15 local (13:15 UTC)
Place
Mineral Wells, TX
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Approach
Aircraft
N3412LGyroflug SC01B160
Weather
Visual (VMC) · Day
Status
Completed · report December 14, 1992
Report
Approved by Office Director
FAA report
19900610019339A
Case key
22931

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

Total propeller blade retention failure, the resultant separation of one propeller blade, and the improper installation of the propeller by unknown maintenance personnel.

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 - vfr pattern - base leg/base to final
Propeller system/accessories,prop blade retention - failure,totalCause
Propeller system/accessories,blade - separationCause
Maintenance,installation - improperOther maintenance personnelCause
Remedial action - attemptedPilot in command
In flight collision with terrain/waterDescent - uncontrolled

Analysis

The airplane had been modified to be flown either remotely or by the pilot. Takeoff and initial climb were performed by remote control and control was transferred to the pilot to position for a remote control landing. Angle of bank increased past 90 degrees in a nose high attitude at about 425 feet AGL; the pilot transmitted that he was 'going down' shortly before impact. One of the three wooden propeller blades separated from the hub and was found 1/4 mile from the main wreckage. The blade was attached to the hub primarily by 5 lag screws. Threads in the wood butt of the separated blade were stripped. The 5 screws remained in place. Lag screws in the remaining 2 blades were found undertorqued. Several discrepancies were noted regarding specifications for propeller blade root and size, tolerances, and lag screws.

Aircraft

Registration
N3412L
Reported as
Gyroflug SC01B160
Category
Airplane
Serial number
S-46
Airframe hours
139
Engine
Lycoming O-320-D1A, 160 horsepower, reciprocating
Damage
Destroyed
Flight
Other work use · Part 91
Registered owner
Litton Applied Technology
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · January 30, 1990 · 90 hours before
Airport
MWL · Municipal

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
43
Certificates
Flight engineer, Airline transport, Flight instructor
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Front
Toxicology
Performed
Flight hours
5,354 total · 20 in this make and model · 4,699 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
20 statute miles
Lowest ceiling
None
Temperature
75 °F, dew point 70 °F
Observed at
MWL, 4 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.