FTW83FU002

NTSB accident investigation · Pterodactyl Ascenger II+ · Round Rock, TX · July 30, 1983

Accident · FatalFinal report
Date
July 30, 1983, 15:16 local (20:16 UTC)
Place
Round Rock, TX
Injuries
1 fatal
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
UNREGPterodactyl Ascenger II+
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Case key
20770

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 control - in flightManeuvering
Low pass - performedPilot in command
Weather condition - unfavorable windFactor
Weather condition - gustsFactor
Aircraft handling - not maintainedPilot in commandCause
Lack of familiarity with aircraftPilot in commandFactor
Lack of total experiencePilot in commandFactor
Inadequate initial trainingPilot in commandFactor
Airframe/component/system failure/malfunctionManeuvering
Wing,bracing wire - overload
Design stress limits of aircraft - exceeded
In flight collision with terrain/waterDescent - uncontrolled

Analysis

The ultralight vehicle had been recently built & had been flown once by an experienced ultralight plt. He reported there were no discrepancies in the vehicle's assembly or flt characteristics. The owner & 2 other personnel met at the flying area & assembled the vehicle. The only one with flying experience took off & made several passes over the area. On the last pass, he waved both hands & yelled what 1 witness thought was 'I love it.' Shortly after that, the vehicle turned into the wind & began oscillating in pitch. The nose then pitched up to or beyond a verticle attitude & the vehicle began descending tail 1st, then crashed. Witnesses reported that the wings folded, but they were not sure whether the wings folded before or after the vehicle entered the tail slide. The vehicle was not designed for a tail slide. An exam revealed that 1 landing wire & all 4 canard brace wires had separated from overload. The wind was gustingto 20 KTS, a dust devil was seen in the vicinity & svrl more-experienced plts had stopped flying due to the winds.

Aircraft

Registration
UNREG
Reported as
Pterodactyl Ascenger II+ (ASCENGER I)
Category
Ultralight, amateur-built
Airframe hours
2
Engine
Cuyuna UL 202, 35 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 103
Registered owner
James Kirby
Airport
Edville

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Airplane ratings
Single-engine land
Medical
Unknown
Seat
Center
Flight hours
6 total · 6 in this make and model · 6 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
60° at 10 knots, gusting 20
Visibility
15 statute miles
Lowest ceiling
None
Temperature
93 °F, dew point 66 °F
Altimeter
30.00 inHg