ERA17TA170

NTSB accident investigation · Bell 206 · Orange Springs, FL · May 2, 2017

Accident · Serious injuriesFinal report
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.

Aircraft capabilityAircraft › Aircraft oper/perf/capability · Not attained/maintainedBell 206B: 2 casesAll aircraft: 57 casesProbable cause

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.