Probable cause
The pilot’s failure to lock the collective pitch control after landing, and the mechanic’s failure to properly balance the collective pitch control after converting the helicopter to a single-pilot configuration, which resulted in an uncommanded collective movement and subsequent hard landing.
NTSB analysis
The pilot of the helicopter air ambulance performed an approach and landing to a rooftop heliport in gusting wind conditions, during which he reduced collective pitch control friction to more readily apply collective control inputs. After landing, he started the after-landing portion of the checklist and turned the throttle twist grip on the collective from FLIGHT to IDLE, believing that he had engaged the collective lock. Shortly thereafter, the collective "popped up," and the helicopter became airborne. He immediately grabbed the cyclic with his right hand, the collective with his left hand, and twisted the twist grip to FLIGHT. The helicopter then landed hard, resulting in minor damage. Review of onboard video revealed a sequence of events consistent with the pilot’s statement, and recorded data indicated that the collective rose up consistent with it not locked in the down position and resulted in the engine transitioning from IDLE to FLIGHT. This confirmed the pilot’s observation that the collective rose uncommanded.
The helicopter was designed to be convertible from a dual-pilot configuration (for activities such as training), to single-pilot configuration (for activities such as air ambulance). Two days before the incident, the helicopter had been converted to the single-pilot configuration by a mechanic. This conversion required that the collective be balanced to avoid uncommanded movement; however, post-incident examination of the helicopter revealed that the collective would rise unassisted, indicating that the collective was improperly balanced after the helicopter was converted to the single-pilot configuration.
Text from the NTSB. Open the NTSB docket for ERA18IA078 for the full record.
Event
- Date
- Jan 28, 2018
- Type
- Incident
- Place
- Memphis, Tennessee
- Nearest airport
- Helipad (PVT)
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Day
Airbus Helicopters EC 130
- N-number
- N894GT
- Category
- Helicopter
- Year built
- 2015
- Damage
- Minor
- Operating rule
- Part 135 (charter and commuter)
- Purpose of flight
- Other work use
From the NTSB aviation accident database: N-registered aircraft, events since 2008, data through Oct 28, 2026. The file is published monthly, so the latest weeks are incomplete and recent records can change. The official source is the NTSB aviation investigation search. CheckAero is independent and not affiliated with the NTSB.