- Date
- September 9, 2016, 13:00 local (18:00 UTC)
- Place
- Peach Orchard, MO
- Injuries
- 2 uninjured
- Damage
- Substantial damage
- Phase of flight
- Maneuvering
- Aircraft
- N500TNHughes 369
- Defining event
- Maneuvering-hover: Miscellaneous/other
- Weather
- Visual (VMC) · Day
- Status
- Completed · report March 13, 2017
- Report
- Approved by Office Director
- NTSB office
- General Aviation Accidents
- Parties
- FAA
- FAA report
- 20160909017019A
- Case key
- 94002
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 helicopter pilot’s failure to maintain sufficient separation between the main rotor blade and a power line during line guard installation, which resulted in an electrical arc to the main rotor.
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 helicopter pilot reported that he was flying in support of a utility company crew that was installing line guards for a conductor damper on an energized 161 kilovolts (Kv) electrical transmission line. The transmission line had three phases (power lines) that were separated vertically and staggered horizontally from one another and ran parallel to the ground. The lower phase power line was about 9.5 ft (horizontally) further out from the middle phase power line. While the helicopter was approaching the lines, its main rotor blade clearance from the middle phase line was about 2.5 ft, which resulted in an electrical arc to the main rotor. The pilot landed the helicopter away from the transmission line without further incident. A postaccident examination revealed substantial damage to the main rotor hub and two main rotor blades. The pilot reported no preaccident mechanical malfunctions or failures with the helicopter that would have precluded normal operation. According to Occupational Safety & Health Administration 1910.269(I)(10), the minimum approach distance (MAD) is to "ensure that workers do not approach or take any conductive object closer to the energized parts as set forth in the table below (excerpt)." For a voltage of 161 Kv, the MAD for this operation was equal to or greater than 4.00625 ft.
Factual narrative
The helicopter pilot reported that he was flying in support of a utility company crew that was installing line guards for a conductor damper on an energized 161 kilovolts (Kv) electrical transmission line. The transmission line had three phases (power lines) that were separated vertically and staggered horizontally from one another and ran parallel to the ground. The lower phase power line was about 9.5 feet (horizontally) further out from the middle phase power line. During approach to the lines, the main rotor blade clearance from the middle phase line was about 2.5 feet, which resulted in an electrical arc to the main rotor. The pilot landed the helicopter away from the transmission line without further incident. A postaccident examination revealed substantial damage to the main rotor hub and two main rotor blades. The pilot reported no preaccident mechanical malfunctions or failures with the helicopter that would have precluded normal operation. According to the Occupational Safety & Health Administration (OSHA) 1910.269(I)(10) the Minimum Approach Distances (MAD) is to "ensure that workers do not approach or take any conductive object closer to the energized parts as set forth in the table below (excerpt). " Nominal voltage in kilovolts Distance: Phase to ground exposure (feet) 161 to 169 4.00625 The MAD for this operation was a distance equal to or greater than 4.00625 feet.
Aircraft
- Registration
- N500TN
- Reported as
- Hughes 369 (D)
- Category
- Helicopter
- Serial number
- 590521D
- Built
- 1979
- Airframe hours
- 17,622.7
- Engine
- Rolls Royce 250-C20R, 450 horsepower, turbo shaft
- Damage
- Substantial damage
- Flight
- External load · Part 133
- Operator
- Air2 LLC.
- Registered owner
- Axis Capital
- Airworthiness certificate
- Standard, Normal
- Last inspection
- 100 hour · September 5, 2016
- Flight plan
- Company VFR
- Equipment
- Electronic flight bag or handheld device, Satellite tracking device, Onboard weather
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
- 49
- Injuries
- None
- Certificate
- Commercial
- Medical
- Class 2, Without waivers/limitations
- Last flight review
- March 10, 2015
- Seat
- Left
- Flight hours
- 5,750 total · 3,585 in this make and model · 5,475 as pilot in command · 75 in the last 90 days · 37 in the last 30 days
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 230° at 8 knots, gusting 17
- Visibility
- 10 statute miles
- Lowest ceiling
- 3,700 ft broken
- Temperature
- 93 °F, dew point 73 °F
- Altimeter
- 29.95 inHg
- Observed at
- KTKX, 10 nm away
Docket · 4
The files NTSB released with the investigation on January 25, 2017, on NTSB’s docket system: statements, records, photos and specialists’ reports. 956 KB 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.
Other investigations on N500TN · 1
Matched to the same aircraft by N-number and date.