ATL84FU003

NTSB accident investigation · Pterodactyl Ascender II · Lawrenceville, GA · January 8, 1984

Accident · FatalFinal report
Date
January 8, 1984, 15:10 local (20:10 UTC)
Place
Lawrenceville, GA
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
UNREGPterodactyl Ascender II
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Case key
6338

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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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/malfunctionManeuvering
Flight/nav instruments,airspeed indicator - lack ofFactor
Maintenance,installation - not performedFactor
Operation with known deficiencies in equipment - performedPilot in commandFactor
Weather condition - unfavorable windFactor
Weather condition - turbulenceFactor
Design stress limits of aircraft - exceededPilot in commandCause
Flight control surfaces/attachments - overload
Wing - overload
In flight collision with terrain/waterDescent - uncontrolled
In flight collision with terrain/waterDescent - uncontrolled

Analysis

The plt took off in conditions of turbulence & gusty winds. Witnesses reported the ultralight vehicle pitched & rolled erratically after lift-off. The plt then made a right climbing turn to a downwind heading & proceeded over a tall tree line toward a field where he ultimately crashed. One witness heard a 'pop', then looked & saw the acft descending with the wings folded. Others said the wings flexed upward 1st, then the acft flipped over & the wings reversed & folded around the airframe. An exam revealed upward deformation of the carard, but it had no significant evidence of ground impact. The wings had evidence of both upward & downward bending. The kingpost was bent rearward & its top cap was found 175 ft from the main wreckage. No airspeed indicator was installed. The manufacturer reported that an airspeed indicator was required to judge the speed with the engine running, that the max speed (vne) was easily exceeded & that the flight controls became extremely sensitive at higher airspeeds.

Aircraft

Registration
UNREG
Reported as
Pterodactyl Ascender II (ASCENDER I)
Category
Ultralight, amateur-built
Serial number
1210
Airframe hours
8
Engine
Cuyuna 430D, 30 horsepower, reciprocating
Damage
Destroyed
Flight
Personal · Part 103
Registered owner
Mary B. Mussner
Destination
Snellville, GA

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
39
Airplane ratings
Single-engine land
Medical
Unknown
Seat
Front
Toxicology
Performed
Flight hours
350 total · 4 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
310° at 10 knots
Visibility
20 statute miles
Lowest ceiling
None
Temperature
61 °F, dew point 30 °F
Altimeter
30.00 inHg
Observed at
PDK, 15 nm away