No fatalities

11 Jul 2014: AIR TRACTOR INC AT 502B — Hinkle Aviation — Cavalier, ND

Cavalier, ND, United States

On 11 Jul 2014, an AIR TRACTOR INC AT 502B operated by Hinkle Aviation was involved in an aviation accident near Cavalier, ND. No fatalities were reported. Investigators recorded the probable cause as: The pilot's loss of control during the takeoff roll. 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

An agricultural aircraft encountered a turf obstruction during takeoff, resulting in premature liftoff, hard landing, and a ground loop that damaged the left wing. No preimpact anomalies were found.

Accident Overview

An aerial application aircraft was departing from a rough, unimproved turf strip for a spraying mission. During the takeoff roll, the airplane struck a small obstruction in the turf, causing it to become airborne prematurely. As the aircraft settled back toward the ground, the tail wheel contacted the turf with significant force, followed by the main landing gear. This sequence resulted in a porpoising motion and a swerve to the right, with the pilot losing control. The aircraft then ground looped, and the left wing struck the ground, sustaining substantial damage.

Aircraft and Site Conditions

The accident occurred on a natural turf strip that was described as rough and unimproved, typical for remote agricultural operations. The specific type, registration, and operator of the aircraft were not disclosed. No preimpact mechanical anomalies were detected during the post-accident examination, indicating that the aircraft was functioning normally prior to the event. The time of day, weather conditions, and any air traffic control involvement remain unspecified.

Sequence of Events

During the initial takeoff, the aircraft encountered a small turf obstruction. This prompted an early rotation and premature liftoff. Shortly after becoming airborne, the aircraft lost lift and began to descend. The tail wheel struck the ground hard, followed by the main landing gear. The impact induced a porpoise, or repeated bouncing, and the airplane veered to the right. The pilot attempted to regain directional control but was unable to prevent the aircraft from ground looping. As the airplane pivoted, the left wing contacted the ground, causing structural damage.

Damage Assessment

The primary damage was localized to the left wing, which sustained substantial structural harm. The extent of damage to other components, such as the landing gear or fuselage, was not detailed. No injuries were reported in the source material.

Investigation Findings

The investigation did not identify any preexisting mechanical failures or anomalies with the aircraft. The likely cause of the accident was attributed to the pilot's inability to maintain control following the encounter with the obstruction and the subsequent abnormal takeoff profile. However, no official probable cause was stated by the source.

Safety Considerations

While the source does not offer any lessons or recommendations, the circumstances highlight the challenges of operating aircraft from rough, unimproved airstrips, where small surface irregularities can disrupt the takeoff sequence.

Contributing factors

Causes

PilotPerformance/control parameters — Not attained/maintained

Other contributing factors

Contributed to outcome