GAA16CA480

NTSB accident investigation · Hughes 369 · Peach Orchard, MO · September 9, 2016

Accident · No injuriesData collectionFinal report
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.