No fatalities

19 Sep 2020: VANS RV4 (N250LB) — Bishop Ag Air LLC — Clovis, NM

Clovis, NM, United States

On 19 Sep 2020, a VANS RV4 (registration N250LB) operated by Bishop Ag Air LLC was involved in an aviation accident near Clovis, NM. No fatalities were reported. Investigators recorded the probable cause as: The pilot’s failure to maintain lateral control during initial climb due to distraction, which resulted in an in-flight upset and impact with terrain. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On September 19, 2020, an experimental Vans RV-4 (N250LB) was substantially damaged near Clovis, NM, after the pilot became distracted by a phone call during initial climb, causing the airplane to become inverted and impact terrain. The pilot was seriously injured.

Accident Details

On September 19, 2020, at 0945 mountain daylight time, an experimental amateur-built Vans RV-4 airplane, registration N250LB, was substantially damaged when it crashed near Clovis, New Mexico. The pilot sustained serious injuries. The flight was conducted under 14 CFR Part 91 as a personal flight.

Pilot Account

The pilot, interviewed about a month after the accident due to his injuries, stated that he planned a normal departure from an airport he frequently used. Shortly after takeoff, during the initial climb, he received a phone call on his mobile phone, which was on the floor by his feet. He was momentarily distracted as he looked down to see the caller's name on the phone. About two seconds later, he looked outside the cockpit and found the airplane inverted. He immediately rolled the airplane upright and level just before the wheels touched the ground. He could not recall any further events. The pilot reported no preimpact mechanical malfunctions.

Witness Account

A witness observed the airplane begin a ground roll to the south, into the wind. The airplane lifted off about midfield and immediately transitioned to a climb. At about 100 ft above ground level, the airplane rolled to the right until it was inverted, then disappeared from the witness's view. The witness reported that the engine sounded smooth and continuous during the flight.

Damage

The airplane came to rest inverted about 800 ft beyond the departure runway end. Photographs provided by the witness showed substantial damage to the fuselage and wings.

Contributing factors

PilotLateral/bank control — Not attained/maintained