- Date
- May 2, 2017, 18:15 local (22:15 UTC)
- Place
- Orange Springs, FL
- Injuries
- 1 serious
- Damage
- Substantial damage
- Phase of flight
- Maneuvering
- Aircraft
- N911GEBell 206
- Defining event
- Maneuvering-hover: External load event (Rotorcraft)
- Weather
- Visual (VMC) · Day
- Status
- Completed · report November 15, 2018
- Report
- Approved by Office Director
- NTSB office
- Eastern Region Aviation
- Parties
- FAA FSDO
- FAA report
- 20170502017799A
- Case key
- 95097
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 pilot's failure to maintain adequate clearance between the helicopter's skid and the firefighting bucket and suspension cable, which resulted in the cable becoming entangled on the landing skid and a subsequent loss of helicopter control.
Findings · 2
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 commercial helicopter pilot had completed 25 to 30 water drops in a fire zone using a firefighting bucket on suspension cables. After refueling, he completed three or four additional drops and then filled and pulled the bucket from the water and immediately felt "a severely out of CG [center of gravity] condition to the right." He assumed that the bucket cables were entangled in the right landing skid, so he released the water from the bucket. The condition persisted, so he rocked the helicopter to attempt to free the cable without success. He then released the cable with the cargo release button and heard the "clunk" sound typically heard when the bucket was released, but then he heard another "clunk." The helicopter then began to spin violently and crashed into the water. Examination of the wreckage revealed 6-inch long cable marks on the right rear landing skid tube and a torsional fracture of the tail rotor short shaft. Based on the pilot's statement, the cable marks likely occurred initially when a cable became entangled on the skid tube, followed by the fracture of the tail rotor shaft due to cable or bucket contact with the tail rotor assembly. The pilot reported that there were no preaccident mechanical malfunctions or anomalies with the helicopter that would have precluded normal operation.
Factual narrative
On May 2, 2017, about 1815 eastern daylight time, a Bell 206B helicopter, N911GE, sustained substantial damage during firefighting operations near Orange Springs, Florida. The helicopter was registered to and operated by the Marion County Sheriff's Office as a public-use aircraft. The commercial pilot sustained serious injuries. Visual meteorological conditions prevailed and no flight plan was filed for the local flight that departed Ocala International Airport, Ocala, Florida, about 1500.According to the Aviation Unit Commander and the pilot, the pilot was utilizing a firefighting bucket (Bambi Bucket®) and had completed between 25 and 30 drops on the fire zone. He landed at a nearby landing zone, refueled, and completed 3 or 4 additional drops when the accident occurred. After lowering the bucket into the water and filling it, he pulled the bucket from the water and immediately felt "a severely out of CG condition to the right." He assumed that the bucket cables were entangled in the right landing skid, so he released the water from the bucket. The condition persisted, so he rocked the helicopter to attempt to free the cable; however, this was not successful. He then released the cable with the cargo release button. He heard the "clunk" sound that was typical with releasing the bucket, then he heard another "clunk." The helicopter then began to spin violently and crashed into the water. The pilot freed himself from the cockpit, inflated his personal flotation device, and swam to shore. He utilized his cell phone to call for assistance and was rescued by first responders. The pilot reported there were no preaccident mechanical malfunctions or anomalies that would have precluded normal operation of the helicopter. An examination of the wreckage revealed cable marks on the right rear landing skid tube for about 6 inches in length. There was also a torsional fracture of the tail rotor short shaft.
Aircraft
- Registration
- N911GE
- Reported as
- Bell 206 (B)
- Category
- Helicopter
- Serial number
- 5271
- Built
- 2001
- Airframe hours
- 8,966
- Engine
- Rolls-Royce 250-C20 SER, 400 horsepower, turbo shaft
- Damage
- Substantial damage
- Flight
- Firefighting · Public use
- Operator
- Marion County Sheriff
- Registered owner
- Marion County Sheriff
- Airworthiness certificate
- Standard, Normal
- Last inspection
- 100 hour · December 19, 2016 · 76 hours before
- Departed
- OCF · Ocala, FL
- Destination
- OCF · Ocala, FL
- Equipment
- Electronic flight bag or handheld device, 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
- Pilot
- Age
- 48
- Injuries
- Serious
- Certificate
- Commercial
- Instrument ratings
- Helicopter
- Medical
- Class 2, Without waivers/limitations
- Last flight review
- February 2, 2017
- Seat
- Right
- Restraint
- 4-point
- Flight hours
- 3,494 total · 1,552 in this make and model · 2,510 as pilot in command · 46 in the last 90 days · 17 in the last 30 days · 2 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 360° at 8 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 88 °F, dew point 55 °F
- Altimeter
- 29.95 inHg
- Observed at
- OCF, 25 nm away
Docket · 4
The files NTSB released with the investigation on October 22, 2018, on NTSB’s docket system: statements, records, photos and specialists’ reports. 5.9 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.