Wsk Pzl Mielec M 18A accident near Brunswick, NC

On June 10, 2016, a Wsk Pzl Mielec M 18A (airplane) was involved in an accident near Brunswick, NC. 1 person died. Damage to the aircraft: destroyed.

Date
June 10, 2016
Place
Brunswick, NC
Aircraft
Wsk Pzl Mielec M 18A · Airplane
Injuries
1 fatal, 0 serious, 0 minor
Damage
Destroyed
Position
34.127°N, 78.340°W
NTSB ID
20160612X02159

Official records · ERA16LA209

NTSB summary

HISTORY OF FLIGHT On June 10, 2016, about 0900 eastern daylight time, an experimental WSK PZL MIELEC M-18A, N2283M, was destroyed following an inflight separation of the right wing while maneuvering near Brunswick, North Carolina. The commercial pilot was fatally injured. Visual meteorological conditions prevailed, and no flight plan was filed for the aerial application flight, which was operated by Canam Aviators Inc., under the provisions of Title 14 Code of Federal Regulations Part 137. The flight originated from Bear Pen Airstrip (NC43), Supply, North Carolina, around 0845. According to ground personnel, the airplane departed with a full load of fertilizer and 45 minutes of fuel with 30 minutes of reserve fuel. After 1 hour passed and the airplane did not return to the airport, ground personnel called 911 to report the airplane missing. The airplane was subsequently located in a wooded area. PERSONNEL INFORMATION According to Federal Aviation Administration (FAA) records, the pilot held a commercial pilot certificate with ratings for airplane single-engine land, airplane multiengine land, instrument airplane, and rotorcraft-helicopter. He also held an FAA second-class medical certificate, which was issued on May 13, 2016. At the time of the medical examination, the pilot reported 30,576 total hours of flight experience. The pilot's logbook was not recovered. AIRCRAFT INFORMATION The airplane was manufactured in 1994 and imported to the US, where it was issued a special airworthiness certificate in the restricted category. The accident operator purchased the airplane in

Probable cause

The failure of the right wing due to a fatigue fracture of the right outboard wing forward spar lower fitting. Contributing to the accident was the routine operation of the airplane over its certificated maximum gross weight and the operator's improper or inadequate maintenance practices, which failed to apply a service life factor to the airplane to account for its overweight operation and also f

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