PIPER PA 46-350P

Full Narrative

On October 2, 2022, about 1600 Mountain daylight time, a Piper PA-46-350P, N987PS, was substantially damaged when it was involved in an accident near Clovis, New Mexico. The pilot and passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that he encountered “a major wind gust” while on a visual approach to runway 4 at Clovis Regional Airport (CVN). In response, he aborted the approach, applied full engine power, and retracted the landing gear and flaps; however, the airplane did not have enough speed and power to maintain flight. The pilot subsequently felt the airplane buffet and lowered the nose. The pilot maneuvered the airplane and initiated a gear-up landing to an open field adjacent to runway 4. During the landing sequence, the right horizontal stabilizer impacted an airport sign, and the airplane came to rest upright. A postaccident fire ensued.

The automated weather observation station located on the airport reported that, about 4 minutes before the accident, the wind was from 180° at 11 knots. The same automated station reported that, about 56 minutes after the accident, the wind was from 160° at 10 knots. The calculated crosswind component at the time of the accident was about 7 knots, with a tailwind of about 8 knots.

Postaccident examination of the airplane revealed that the fuselage undercarriage, right horizontal stabilizer, and the right elevator were substantially damaged. A subsequent examination of the recovered wreckage revealed no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation.

A review of the airplane’s Pilot Operating Handbook (POH), Section 4.33, “GO-AROUND,” states in part, “To initiate a go-around from a landing approach, the mixture should be set to full RICH, the propeller control should be a full INCREASE, and the throttle should be advanced to full power while the pitch attitude is increased to obtain the balked landing climb speed of 80 KIAS. Retract the landing gear and slowly retract the flaps when a positive climb is established. Allow the airplane to accelerate to the best angle of climb (81 KIAS) for obstacle clearance or to the best rate of climb speed (110 KIAS) if obstacles are not a factor.”