N125MZ

Substantial
None

AVIA STROITEL AC-5MS/N: 005

Accident Details

Date
Saturday, April 12, 2003
NTSB Number
SEA03LA061
Location
Richland, WA
Event ID
20030416X00519
Coordinates
46.305557, -119.304168
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's failure to maintain airspeed and the failure of the propeller drive assembly. A factor contributing to the accident was the inadvertent stall.

Aircraft Information

Registration
Make
AVIA STROITEL
Serial Number
005
Engine Type
2-cycle
Year Built
2001
Model / ICAO
AC-5MAC5M
Aircraft Type
Glider
No. of Engines
1
Seats
1
FAA Model
AC-5M

Registered Owner (Current)

Name
MICKE THOMAS BERND
Address
38 COBBLER RD
City
MANSFIELD
State / Zip Code
MA 02048-2750
Country
United States

Analysis

On April 12, 2003, approximately 1600 Pacific daylight time, an Avia Stroitel AC-5M powered glider, N125MZ, was substantially damaged during a forced landing following a loss of engine power at the Richland Airport (RLD), Richland, Washington. The private pilot, sole occupant and owner of the glider, was not injured. Visual meteorological conditions prevailed and no flight plan was filed for the 14 CFR Part 91 personal flight. The flight was originating at the time of the accident.

According to the Pilot/Operator Aircraft Accident Report (NTSB form 6120.1/2), the pilot reported "the takeoff on runway 1 was normal, but approximately two-thirds of the way down the runway, at approximately 150 feet above ground level, I noticed the engine 'over-revving' and the aircraft no longer climbing." The pilot reported that he failed to lower the nose to ensure proper airspeed in order to land straight ahead on runway 1. The pilot further stated that he made the wrong decision and turned right to land on the intersecting runway [runway 7], and during the turn "the airspeed was allowed to deteriorate until the right wing stalled." The airplane's right wing tip impacted the ground causing it to spin around 180 degrees, skidding backwards across a taxiway, and coming to rest in sandy soil.

The pilot reported that the tension on the propeller drive belts was checked during the aircraft preflight. The pilot also stated that the tension on the propeller drive belts "slipped" and caused a loss of thrust after takeoff. The pilot further reported that the reason for the drive belts slipping was not determined.

The pilot reported the glider had sustained damage to the right wing tip and the main gear. The bottom right front of the fuselage was scraped and cracked, the rear portion of the fuselage where it transitions with the vertical stabilizer was cracked approximately half-way through its circumference, and the tail wheel was crushed.

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Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA03LA061