N138ZX

Substantial
Serious

M-SQUARED AIRCRAFT SPRINT 1000S/N: 000582DT

Accident Details

Date
Tuesday, May 22, 2018
NTSB Number
CEN18LA189
Location
Gurdon, AR
Event ID
20180523X05505
Coordinates
33.923053, -93.157218
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
2
Minor Injuries
0
Uninjured
0
Total Aboard
2

Probable Cause and Findings

Inadequate engine maintenance, which resulted in the failure of the MAG piston ring and the subsequent total loss of engine power due to a piston seizure.

Aircraft Information

Registration
Make
M-SQUARED AIRCRAFT
Serial Number
000582DT
Engine Type
2-cycle
Year Built
2006
Model / ICAO
SPRINT 1000
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
SPRINT 1000

Registered Owner (Current)

Name
SMELTZER PAUL C
Address
152 MC 422
City
TEXARKANA
State / Zip Code
AR 71854
Country
United States

Analysis

On May 21, 2018, about 1915 central daylight time, an M-Squared Sprint 1000 light-sport airplane, N138ZX, was substantially damaged when it was involved in an accident near Gurdon, Arkansas. The pilot and passenger were seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported to the Federal Aviation Administration (FAA) inspector that the airplane had just departed from runway 26 at Gurdon Lowe Field. When the airplane was about 800 ft above ground level (agl), "the engine suddenly stopped." As the pilot looked for a suitable landing site, the "engine seized up", and the airplane began to descend rapidly. The pilot deployed the airplane's ballistic parachute about 200 ft agl. The airplane descended and landing hard in a residential area. The airplane's wings and fuselage were substantially damaged.

The pilot recalled that during the takeoff and climb there were no unusual indications from the instruments, nor any unusual sounds from the engine.

The engine was examined by the FAA inspector with technical assistance from the engine manufacturer. Examination of the engine revealed that the top of the MAG piston ring had failed resulting in damage to the MAG piston and cylinder walls. The examination also noted vertical scoring on the PTO cylinder, and significant vertical scoring on the MAG cylinder. In addition, both rubber PTO and MAG carburetor intake sockets were worn and cracked.

Complete engine records were not available and there was no record that showed that the engine had been overhauled during its 23 years of operation. The manufacturer recommends an engine overhaul be performed every 300 hour or 5 years, whichever occurs first. The rubber carburetor intake sockets should be replaced every 5 years or when signatures of deterioration are detected.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN18LA189