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Atlas / NTSB / GAA16CA328

NTSB CAROL · Event

Event GAA16CA328

2016-06-17 McAllen, Texas, United States Airport · MFE None 1 aircraft Status: Completed

Registry · N4035W

FAA Aircraft Registry record.

Make / Model

EUROCOPTER AS 350 B2

Year of manufacture

1996 · 20 years old at event

TCDS

H9EU · AIRBUS HELICOPTERS

Engine

TURBOMECA ARRIEL 1SER (681 hp)

Seats / Engines

6 seats · 1 engine

Last airworthiness date

19960927

ADS-B equipped

Yes — Mode-S A4BAE2

Registrant of record

DEPARTMENT OF HOMELAND SECURITY

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's inadvertent input of the right tail rotor pedal, which resulted in a loss of directional control and an impact with service equipment.

Factual narrative

The helicopter pilot reported that during the engine run-up sequence while on a movable helicopter pad attached to a tug, he noticed that the right rear door was not secure. The pilot unhooked his shoulder harness to reach back to secure the door. While attempting to reach the door, the pilot reported that he inadvertently applied right tail rotor pedal, which caused the helicopter to spin to the right multiple times. During the rotation the helicopter departed the movable pad, impacted the tug, and came to rest in an upright position on the ground. The helicopter sustained substantial damage to the vertical stabilizer. The pilot reported there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The helicopter pilot reported that during the engine run-up sequence while on a movable helicopter pad attached to a tug, he noticed that the right rear door was not secure. The pilot unhooked his shoulder harness to reach back to secure the door. While attempting to reach the door, the pilot reported that he inadvertently applied right tail rotor pedal, which caused the helicopter to spin to the right multiple times. During the rotation the helicopter departed the movable pad, impacted the tug, and came to rest in an upright position on the ground. The helicopter sustained substantial damage to the vertical stabilizer. The pilot reported there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).

  • C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
  • Personnel issues-Task performance-Inspection-Preflight inspection-Pilot
  • Environmental issues-Physical environment-Object/animal/substance-Ground vehicle-Contributed to outcome

Verbatim from NTSB's published report. Source file NTSB_2016_GAA16CA328.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.