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Aviation safety reports, made easier to study

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September 9, 2016 · Hughes 369 D · N500TN

Peach Orchard, MO

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 9, 2016
Injury Outcomes
No injuries (2 uninjured)
Location
Peach Orchard, MO
Aircraft
Hughes 369 D (1979)
Tail Number
N500TN
Operator
Air2
Injuries
None
Aircraft Damage
Substantial
NTSB Number
GAA16CA480

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.

NTSB 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.

Full 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.

Flight

Event TypeAccident
Event Time13:00 CDT
Nearest Airport0nm
Flight Plan FiledCvfr
Flight Plan ActivatedUnknown
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHughes 369 D
Tail NumberN500TN
Aircraft CategoryHeli
DamageSubstantial
OperatorAir2
Operating RulePart 133
Engines1
Engine TypeTurboshaft
Engine DetailsRolls Royce · 250-C20R · Turboshaft · 450
Seats5

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 49 · Second Class · None
Crew 2None

Conditions

ConditionsVMC
LightDaylight
Wind230° @ 8 kt, gusting 17 kt
Visibility10 sm
CeilingBroken clouds 3700 ft
Altimeter29.95 inHg
Observation Time17:50
Weather SourceWFAC

Appendix: Source Data