No fatalities

21 Apr 2014: CIRRUS DESIGN CORP SR20 — BOSTON AVIATION LEASING II LLC — Sanford, FL

Sanford, FL, United States

On 21 Apr 2014, a CIRRUS DESIGN CORP SR20 operated by BOSTON AVIATION LEASING II LLC was involved in an aviation accident near Sanford, FL. No fatalities were reported. Investigators recorded the probable cause as: The student pilot's failure to maintain directional control during the aborted landing. Contributing to the accident was his failure to compensate for torque, P-factor, and the reported crosswind conditions. 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

During a supervised solo flight, a student pilot lost control after a go-around initiated due to a crosswind, with the aircraft veering left despite full opposite control input.

Incident Overview

During a supervised solo flight, a student pilot was performing circuits in the traffic pattern. The pilot had completed three previous circuits, with two of the three landing attempts being aborted. On the fourth landing attempt, a 70-degree right crosswind caused the airplane to be blown off the left side of the runway.

Go-Around and Loss of Control

In response to the deviation, the student pilot applied full engine power to conduct a go-around. The airplane then veered left and banked 45 degrees to the left. The student pilot reported that despite pushing the control stick fully to the right, the airplane continued to turn left. The student pilot also stated that there were no mechanical deficiencies with the airplane that would have prevented normal operation.

Relevant Guidance

According to FAA Advisory Circular AC-61-23C (Pilot's Handbook of Aeronautical Knowledge), the effect of torque increases in direct proportion to engine power, airspeed, and airplane attitude. When power is high, airspeed is slow, and angle of attack is high, the effect of torque is greater. During takeoffs and climbs, when torque is most pronounced, sufficient right rudder pressure is required to counteract the left-turning tendency and maintain a straight path.

Contributing factors

Causes

Student/instructed pilotDirectional control — Not attained/maintained

Other contributing factors

Incorrect use/operationResponse/compensation