What happened
The incident involved a student pilot operating an aircraft during a training flight. During the initial approach for landing, the airplane bounced twice upon touchdown. In response to this unstable landing, the pilot executed a go-around and attempted a second landing. The second attempt was successful, and the pilot proceeded to taxi the aircraft toward its parking position.
While taxiing, the student pilot noticed an immediate loss of directional control authority. Specifically, the pilot reported that steering using the left rudder pedal was impossible. This mechanical failure prevented normal ground maneuvering. Subsequent physical inspection of the airframe revealed significant structural deformation. The firewall within the engine compartment had been buckled and bent, likely resulting from the forces experienced during the bounced landing.
The investigation
A post-incident examination of the aircraft confirmed the pilot's observations regarding control failure. Investigators found that the firewall was severely deformed. This structural damage compromised the integrity of the control linkages or space required for proper operation, directly correlating with the reported inability to steer via the left rudder pedal.
Findings
The primary finding relates to the structural damage sustained during the landing phase. The buckled and bent firewall is a critical mechanical failure point. This damage occurred as a direct consequence of the airplane bouncing twice on the runway during the first landing attempt. The subsequent go-around and successful second landing did not mitigate the initial structural impact.