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NTSB Report

May 3, 2006 · Robinson R44 Raven II · N288RH

Rocky Point, NC

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
May 3, 2006
Injury Outcomes
No injuries (1 uninjured)
Location
Rocky Point, NC
Aircraft
Robinson R44 Raven II
Tail Number
N288RH
Operator
Andrew Weldon Mayes
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ATL06CA073

The pilot stated that during his return flight the tail rotor chip detector light flickered and then came on and stayed on. He said he was familiar with the flight area and knew there was a fire department near his intended landing site. He elected to perform a precautionary landing near the fire department to inspect the helicopter. During the landing he failed to observe a TV transmission line, struck the line, nosed down from about 5-feet AGL, rolled to the left and impacted the ground. The pilot further stated that he was "impacted by a strong lateral wind gust from the east which swung the tail rotor into the low hanging cable. However, the nearest weather reporting facility did not report wind gusts at the time of the accident. The pilot also stated that there was "not a mechanical malfunction".

NTSB Probable Cause

The pilot's inadequate visual lookout during a precautionary landing which resulted in an in-flight collision with a transmission wire.

Full Narrative

On May 2, 2006. at 1945 eastern standard time, a Robinson R44 Ravin II, N288RH, registered to Cape Fear Helicopters, Inc., and operated by an individual as a 14 CFR Part 91 business flight, collided with a transmission line while executing a precautionary landing following a tail rotor chip detector warning light, in Rocky Point, North Carolina. The helicopter received substantial damage. Visual meteorological conditions prevailed and no flight plan was filed. The commercial pilot reported no injuries. The flight originated from the Grand Strand Airport in North Myrtle Beach, South Carolina on May 2, 2006, at 1900. According to the pilot, during his flight to Burgaw, North Carolina, "my tail rotor chip light flickered. Approximately 20 seconds later it flickered again. Less than 1 minute later it came on and stayed on". He stated that he was familiar with the flight area enough to know there was a fire department directly across from his intended landing zone. He performed a precautionary landing in a flat, open field to shut down and inspect the helicopter. He said that on "the west side of 117N has tall pines and obscured the black Time Warner Cable TV Line. Since I could not see the Time Warner Cable line, but did realize there were phone and electric lines, I estimated I was sufficiently far enough away and below them based on my rotor tip/path/plain. I approached highway 117N to be close to a road in case something catastrophic occurred, rotated the helicopter 90 degrees to the north, was impacted by a strong lateral wind gust from the east. This wind abruptly swung my tail rotor into the low hanging Time Warner Cable TV line". He said the helicopter rotated another 90 degrees to an easterly heading, nosed down, from about 5 feet AGL, rolled to the left and impacted the ground. Examination of the tail rotor gearbox chip detector and associated electrical wiring found no evidence of contamination or electrical malfunctions. The closest weather reporting facility to the accident site was from the Wilmington International Airport, Wilmington, North Carolina, located 14 nautical miles north northeast of the accident site. The 1953 surface weather observation was: wind 220-degrees at 7 knots, visibility 10-statute miles, clear of clouds, temperature 18-degrees Celsius, dew point temperature 9-degrees Celsius, and altimeter 30.00 millimeters of mercury. The pilot further stated that there was "not a mechanical malfunction".

Flight

Event TypeAccident
Event Time20:45 EDT
Nearest Airport0nm
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftRobinson R44 Raven II
Tail NumberN288RH
Aircraft CategoryHeli
DamageSubstantial
OperatorAndrew Weldon Mayes
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · IO-540 · Reciprocating · 300
Seats4

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 44 · First Class · None

Conditions

ConditionsVMC
LightDusk
Wind220° @ 7 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point64 F / 48
Altimeter30.00 inHg
Observation Time00:53
Weather SourceWFAC

Appendix: Source Data