- Date
- March 23, 2016, 11:00 local (15:00 UTC)
- Place
- Oak Island, NC
- Injuries
- 1 minor
- Damage
- Substantial damage
- Phase of flight
- Maneuvering
- Aircraft
- N843JBRobinson R44
- Defining event
- Maneuvering-hover: Loss of control in flight
- Weather
- Visual (VMC) · Day
- Status
- Completed · report June 1, 2016
- Report
- Approved by Office Director
- NTSB office
- General Aviation Accidents
- Parties
- FAA Greensboro FSDO
- FAA report
- 20160323024319A
- Case key
- 92886
From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.
On this page
Probable cause
The student pilot's failure to maintain a stabilized hover, resulting in a loss of control and an impact with terrain.
Findings · 3
NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.
Sequence of events
The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.
Analysis
The flight instructor reported that the student pilot was asked to conduct several solo "pickups and set downs" on a grass area at the airport. The flight instructor exited the helicopter and observed the student pilot pick the helicopter up to a hover and set the helicopter back on the ground without incident. During the second iteration, the flight instructor observed the helicopter achieve a hover at 5 to 8 feet above ground level for several seconds. She reported that the helicopter then slowly yawed to the right and continued turning to the right until it was 270 degrees from its original heading. The helicopter began to lose altitude, move forward, and the skids impacted the ground. She reported that the helicopter bounced back into the air after impacting the ground and rolled slightly to the left. The helicopter then abruptly rolled to the right, the nose came down, the main rotor blades impacted the ground, and the helicopter came to rest on its right side. After the impact, the flight instructor reported that she crawled inside of the cockpit to turn off the engine. The helicopter sustained substantial damage to the fuselage, main rotor system, tailboom, and horizontal stabilizer. The student pilot reported that he did not recall the accident sequence of events. The flight instructor reported that after the accident, while at the hospital with the student pilot, he reported to her that "I should have been able to control it [the helicopter]." The flight instructor verified that there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The Federal Aviation Administration (FAA) aviation safety inspector who responded to the accident site, reported that he did not notice any mechanical control issues with the helicopter. He also reported that the engine had no signs of any issues and that witnesses stated that after the helicopter impacted the ground, the engine was still running. As a safety recommendation, the flight instructor reported that her organization will increase the time allotment in their training syllabus to allow more emphasis to be placed on the importance of light control inputs and the catastrophic results that can occur from over controlling and abrupt inputs, particularly at a hover. The FAA has published the Helicopter Flying Handbook FAA-H-8083-21 (2012). This handbook discusses techniques for hovering and states in part: To maintain the helicopter in a stabilized hover, make small, smooth, coordinated corrections.
Factual narrative
The flight instructor reported that the student pilot was asked to conduct several solo "pickups and set downs" on a grass area at the airport. The flight instructor exited the helicopter and observed the student pilot pick the helicopter up to a hover and set the helicopter back on the ground without incident. During the second iteration, the flight instructor observed the helicopter achieve a hover at 5 to 8 feet above ground level for several seconds. She reported that the helicopter then slowly yawed to the right and continued turning to the right until it was 270 degrees from its original heading. The helicopter began to lose altitude, move forward, and the skids impacted the ground. She reported that the helicopter bounced back into the air after impacting the ground and rolled slightly to the left. The helicopter then abruptly rolled to the right, the nose came down, the main rotor blades impacted the ground, and the helicopter came to rest on its right side. After the impact, the flight instructor reported that she crawled inside of the cockpit to turn off the engine. The helicopter sustained substantial damage to the fuselage, main rotor system, tailboom, and horizontal stabilizer. The student pilot reported that he did not recall the accident sequence of events. The flight instructor reported that after the accident, while at the hospital with the student pilot, he reported to her that "I should have been able to control it [the helicopter]." The flight instructor verified that there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The Federal Aviation Administration (FAA) aviation safety inspector who responded to the accident site, reported that he did not notice any mechanical control issues with the helicopter. He also reported that the engine had no signs of any issues and that witnesses stated that after the helicopter impacted the ground, the engine was still running. As a safety recommendation, the flight instructor reported that her organization will increase the time allotment in their training syllabus to allow more emphasis to be placed on the importance of light control inputs and the catastrophic results that can occur from over controlling and abrupt inputs, particularly at a hover. The FAA has published the Helicopter Flying Handbook FAA-H-8083-21 (2012). This handbook discusses techniques for hovering and states in part: To maintain the helicopter in a stabilized hover, make small, smooth, coordinated corrections.
Aircraft
- Registration
- N843JB
- Reported as
- Robinson R44 (II)
- Category
- Helicopter
- Serial number
- 13865
- Built
- 2015
- Airframe hours
- 163
- Engine
- Lycoming IO-540-AE1A5, 245 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Instructional · Part 91
- Operator
- High Tide Helicopters, LLC
- Registered owner
- Jaybird Air, LLC
- Airworthiness certificate
- Standard, Normal
- Last inspection
- 100 hour · January 11, 2016
- Departed
- SUT · Oak Island, NC
- Destination
- SUT · Oak Island, NC
- Airport
- SUT · Cape Fear Rgnl Jetport/Howie F
- Equipment
- Electronic primary flight display, ADS-B
Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.
Flight crew
As NTSB recorded them. NTSB leaves out names.
- Role
- Student pilot
- Age
- 65
- Injuries
- Minor
- Certificate
- Student
- Medical
- Class 3, Without waivers/limitations
- Seat
- Right
- Restraint
- 3-point
- Flight hours
- 52 total · 40 in this make and model · 2 as pilot in command · 45 in the last 90 days · 10 in the last 30 days · 2 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 230° at 11 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 64 °F, dew point 55 °F
- Altimeter
- 30.29 inHg
- Observed at
- KSUT
Docket · 4
The files NTSB released with the investigation on May 5, 2016, on NTSB’s docket system: statements, records, photos and specialists’ reports. 4.2 MB in all.
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.