FTW83FU003

NTSB accident investigation · Rotec Rally 2B · Keller, TX · August 26, 1983

Accident · FatalFinal report
Date
August 26, 1983, 07:45 local (12:45 UTC)
Place
Keller, TX
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
UNREGRotec Rally 2B
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Case key
20771

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

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) - nonmechanicalCruise
Ignition system - switched offCause
Powerplant controls - improper use ofPilot in commandCause
Lack of total experience in type of aircraftPilot in commandFactor
Inadequate transition/upgrade trainingPilot in commandFactor
Loss of control - in flightOther
Flt control syst,wing spoiler system - incorrectCause
Maintenance,adjustment - improperPilot in commandCause
Flt control syst,wing spoiler system - deployed inadvertentlyCause
Spoiler extension - inadvertentPilot in command
Aircraft handling - uncontrolledPilot in command
In flight collision with terrain/waterDescent - uncontrolled

Analysis

After assembling his ultralight, the plt received dual instruction in a 2 place model. After his 2nd dual flt, he told his instructor (CFI) he had soloed his vehicle. The CFI cautioned him against further solo flts until he was qualified &emphasized the need to wear a helmet. 3 days later, witnesses saw the vehicle cruising at aprx 300 to 500 ft AGL when itsuddenly rolled right & entered a steep nose down attitude & crashed. None of the witnesses could verify the eng status before impact. Neither of the prop blades had rotational damage, but 1 blade broke when it hit the ground. The eng was started with fuel remaining in the fuel tank & operated normally. The ignition switch was mounted on the control stick next to the twist grip throttle & was found in the off position. The eng was equipped with a centrifugal clutch & could not be started by a windmilling prop. The plt was not wearing a helmet & had suffered extensive head injuries. His CFI had warned him that his spoiler lines were too tight & could result in unwanted spoiler action wtih aft stick movement.

Aircraft

Registration
UNREG
Reported as
Rotec Rally 2B
Category
Ultralight, amateur-built
Serial number
64169
Engine
Cuyuna 430R, 35 horsepower, reciprocating
Damage
Destroyed
Flight
Personal · Part 103
Registered owner
Carl W. Locke

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
39
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Expired
Seat
Front
Toxicology
Performed
Flight hours
194 total · 2 in this make and model · 168 as pilot in command · 2 in the last 90 days · 2 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
290° at 2 knots
Visibility
6 statute miles
Lowest ceiling
None
Temperature
81 °F, dew point 72 °F
Altimeter
30.00 inHg
Observed at
FTW, 22 nm away