No fatalities

21 Jun 2019: Robinson R44 II (N445AP) — Farm & Ranch Helicopter Service Inc — La Ward, TX

La Ward, TX, United States

On 21 Jun 2019, a Robinson R44 II (registration N445AP) operated by Farm & Ranch Helicopter Service Inc was involved in an aviation accident near La Ward, TX. No fatalities were reported. Investigators recorded the probable cause as: The pilot’s failure to maintain helicopter control during a course reversal, which resulted in 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

A Robinson R44 helicopter (N445AP) conducting aerial application was substantially damaged after impacting a field near La Ward, Texas. The pilot was not injured. No mechanical malfunctions were identified.

Accident Details

On June 21, 2019, at approximately 1215 central daylight time, a Robinson R44 helicopter, registration N445AP, sustained substantial damage when it struck a field near La Ward, Texas. The commercial pilot, who was the sole occupant, was not injured. The flight was conducted under 14 Code of Federal Regulations Part 137 for aerial application. Visual meteorological conditions prevailed, and no Federal Aviation Administration flight plan had been filed.

Pilot Account

According to the pilot, during an aerial application pass, he had just reversed his course and was preparing for the next pass when he perceived the helicopter beginning to descend. He added engine power, but the descent continued. The pilot then rolled the throttle fully on and increased collective pitch, yet the rate of descent did not change. As the helicopter neared the field, it began to shake. The pilot executed a flare, and just before ground contact, the helicopter rolled before coming to rest in the field.

Damage and Inspection

An FAA inspector who responded to the accident site reported that the tail boom had separated from the helicopter. Additionally, the fuselage was wrinkled, the landing skids had collapsed, and the main rotor blades were impact-damaged. The inspector stated that no mechanical malfunctions or failures were found that would have precluded normal operations.

Contributing factors

Causes

Descent rate — Not attained/maintained

Other contributing factors

Pilot