EUROCOPTER AS350BA near Globe, AZ — 2009-11-05
- Date
- 2009-11-05
- Location
- Globe, AZ, USA
- Airport
- P13
- Aircraft
- EUROCOPTER AS350BA
- Registration
- N617LH
- Category
- Helicopter
- Highest injury
- Serious
- Fatalities
- 0
- Phase of flight
- Approach
Probable cause
The pilot receiving instruction’s failure to maintain adequate airspeed or control of the helicopter during a simulated hydraulic failure maneuver, which resulted in a hard landing. Contributing to the accident was the flight instructor’s delayed remedial actions and the lack of a positive exchange of control.
NTSB narrative
During a night vision goggle (NVG) training flight, the flight instructor initiated a simulated hydraulic failure on the downwind leg for landing. The flight instructor stated that during this maneuver, the pilot receiving instruction did not properly adjust the trim and did not maintain sufficient air speed. The helicopter slowed to about 20 knots, which was half the speed the flight instructor expected. When the flight instructor heard what he believed to be the low rotor horn and heard the pilot exclaim “uh-oh,” the flight instructor tried to regain control of the helicopter; however, the helicopter impacted the ground hard. Interviews with the pilot and instructor established that both were manipulating the controls after the initial loss of control and that no positive exchange of control had occurred. The pilot reported that the last time he had performed a simulated hydraulic failure was almost 1 year before the accident and that he had never performed such a procedure or had one demonstrated while operating with NVGs. The pilot and instructor reported no in-flight abnormalities with the helicopter before the initiation of the simulated hydraulic failure, and postaccident examination of the hydraulic system components revealed no abnormalities that would have precluded normal operation.
Analysis
- Primary failure mode
- Human factors
- First missed decision gate
- CFI should have ensured PUI was correcting trim and airspeed before maneuver.
NTSB coding
Evidence available
- Photos
- 16 docket documents
Docket documents16
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- Pilot Interviewsinterview
- Pilot Statement & Diagram- Fiskelinterview
- Pilot Statement & Diagram- McCreadyinterview
- Statement of Party Representatives to NTSB Investigationinterview
- Accredited Representative- BEAother
- Main Rotor Servo Examinationsother
- N617LH Weight & Balance for Accident Flightother
- Servo Inspection & Records SN-EBJ082other
- Servo Inspection & Records- SN AR066other
- Servo Inspection & Records- SN PJ020other
- PHOTO- Main Wreckagephotos
- PHOTO- Main Wreckage Right Sidephotos
- Helicopter Operator Supplemental Reportreport
- Wreckage Diagramwreckage
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