N316MG

Substantial
Minor

Magni MAGNI M 16S/N: 16-06-3474

Accident Details

Date
Friday, May 29, 2020
NTSB Number
CEN20LA203
Location
Cape Girardeau, MO
Event ID
20200529X00734
Coordinates
37.226943, -89.564720
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The student pilot’s decision to take off with inadequate runway remaining, and his subsequent failure to attain proper airspeed, which resulted in the gyroplane’s descent into terrain.

Aircraft Information

Registration
N316MG
Make
MAGNI
Serial Number
16-06-3474
Engine Type
Reciprocating
Year Built
2006
Model / ICAO
MAGNI M 16MM16
Aircraft Type
Gyroplane
No. of Engines
1

Registered Owner (Historical)

Name
KONZELMANN HENRY J
Address
4046 OAKBROOK RD
Status
Deregistered
City
DE SOTO
State / Zip Code
MO 63020-5293
Country
United States

Analysis

On May 29, 2020, at 1715 central daylight time, a Magni M-16 gyroplane, N316MG, was substantially damaged when it was involved in an accident near Cape Girardeau, Missouri. The student pilot received minor injuries. The aircraft was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 instructional flight.

The student pilot was conducting a supervised solo flight to practice touch-and-go landings and stated that, while on approach for the fourth or fifth landing, the engine warning light illuminated while on the downwind leg. He dismissed the engine light when it extinguished while rolling down the runway and elected to take off again. He then noticed a “weird smell” after he took off and the engine did not seem to be producing power, so he landed again; however, because the aircraft was nearing the end of the runway, he chose to take off again so that the gyroplane did not continue off the end of the runway into the muddy grass. The pilot reported that, after takeoff, he “had no speed” and “fell behind the power curve,” and the gyroplane descended into the grass past the end of the runway. The wheels dug into the soft ground and the aircraft rolled onto its side, substantially damaging the rotor system, the airframe, and the tail assembly.

The flight instructor and owner of the gyroplane watched the pilot land and stated that the pilot remained on the runway too long before taking off again. He stated that he was expecting the pilot to exit the runway and taxi back when he took off again with about 100 to 200 ft of runway remaining. The nose of the gyroplane was “too high,” and the gyroplane settled back to the ground past the departure end of the runway.

He explained that the accident gyroplane was equipped with an engine alarm light that would illuminate for high exhaust gas temperatures (EGT), low oil pressure, low fuel pressure, and low voltage. He believed that the light illuminated on downwind for high EGT due to having the throttle at full power for too long, and that the light went out when the throttle was reduced for landing. He further explained that the light likely illuminated on landing due to low oil pressure when the throttle was reduced to idle.

The engine was examined by a local mechanic and no anomalies were noted that would have precluded normal operation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN20LA203