No fatalities

15 Oct 2015: Comp Air Inc. (Plambeck) CA8 (N224MS) — Ray, MI

Ray, MI, United States

On 15 Oct 2015, a Comp Air Inc. (Plambeck) CA8 (registration N224MS) was involved in an aviation accident near Ray, MI. No fatalities were reported. Investigators recorded the probable cause as: The pilot's improper use of the trim, which created a cross-controlled situation and resulted in an aerodynamic stall during the attempted go-around. This summary draws on records from NTSB; 6 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On October 15, 2015, a Comp Air CA8 experimental airplane (N224MS) was substantially damaged during landing at Ray Community Airport, Michigan; the pilot sustained minor injuries.

Accident Overview

On October 15, 2015, about 1810 eastern daylight time, a Comp Air Inc. (Plambeck) CA8 experimental airplane, registration N224MS, sustained substantial damage while landing at Ray Community Airport (57D), Ray, Michigan. The private pilot reported minor injuries. Visual meteorological conditions prevailed at the time. The business flight was conducted under 14 CFR Part 91 without a flight plan. The cross-country flight had departed Anniston Regional Airport (KANB), Anniston, Alabama, about 1315 central daylight time.

Pilot Report

The pilot stated that while on a left downwind in the airport traffic pattern for runway 27, he extended 10 degrees of flaps. He completed a left base and extended full flaps while on a short final. Shortly after extending full flaps, the left wing dropped. The pilot attempted to correct the left wing drop with right aileron and rudder, but the airplane did not respond. The pilot elected to go around and increased engine power. The airplane pitched up and the left turn steepened. The pilot subsequently reduced engine power, and with the resulting descent, prepared for an impact with the ground. The airplane struck the ground short of the runway, and the left wing separated from the fuselage. The pilot reported that the engine continued to run for about 15 minutes following the accident.

Post-Accident Examination

A Federal Aviation Administration inspector responded to the accident scene. Examination established that the flight controls were free and correct and that the flaps were completely extended. Further review of the trim system revealed that the right aileron trim and left rudder trim were in positions consistent with a right turn and a left yaw. Examination of the airframe, flight controls, engine, and remaining systems revealed no mechanical anomalies that would have precluded normal operation prior to the accident.

Witness Statement

The inspector interviewed a flight instructor who witnessed the accident. The witness reported that the airplane appeared to be in a cross-controlled attitude, or a skid, while on final approach. The witness confirmed that it sounded as though there were several power changes during the final approach.

Contributing factors

PilotPerformance/control parameters — Not attained/maintained