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July 14, 2004 · Hughes 500D · C-GVHG

Iliamna, AK

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
July 14, 2004
Injury Outcomes
No injuries (1 uninjured)
Location
Iliamna, AK
Aircraft
Hughes 500D
Tail Number
C-GVHG
Operator
Prism Helicopters
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ANC04LA079

The commercial helicopter pilot reported the helicopter was sitting and running at flight-idle while he and two helpers prepared a sling load. He said he was climbing into the helicopter, and did not see the activity, but one of the helpers standing near the cargo door threw a rope to the other helper. He said the rope was inadvertently tossed into the main rotor system, and wrapped around the rotor head. The pilot indicated that the main rotor blades and rotor head received structural damage during the encounter with the rope.

NTSB Probable Cause

The ground crew's failure to use proper procedures while securing a sling load to the helicopter, which resulted in foreign object damage to the helicopter's main rotor system while idling.

Full Narrative

On July 14, 2004, about 1100 Alaska daylight time, a Canadian registered Hughes 500D helicopter, C-GVHG, sustained substantial damage when a ground crew member inadvertently threw a rope into the idling main rotor system at a remote mine site, about 20 miles west of Iliamna, Alaska. The helicopter was being operated by Prism Helicopter LTD, of Wasilla, Alaska, as a visual flight rules (VFR) external load flight under Title 14, CFR Part 133, when the accident occurred. The solo commercial pilot was not injured. Visual meteorological conditions prevailed, and company flight following procedures were in effect. During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC) on July 15, the pilot said the helicopter was sitting and running at flight-idle while he and two helpers prepared a sling load. He said he was climbing into the helicopter, and did not see the activity, but one of the helpers standing near the cargo door threw a rope to the other helper. He said the rope was inadvertently tossed into the main rotor system, and wrapped around the rotor head. The pilot said that the main rotor blades and rotor head received structural damage during the encounter with the rope. He noted that there were no known mechanical anomalies with the helicopter prior to the accident. During a telephone conversation with the IIC on July 15, the director of operations for the operator said ground crew members receive specific training for handling ropes and equipment around operating helicopters.

Flight

Event TypeAccident
Event Time11:00 AKDT
Nearest Airport0nm
Flight Plan FiledCvfr
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHughes 500D
Tail NumberC-GVHG
Aircraft CategoryHeli
DamageSubstantial
OperatorPrism Helicopters
Operating RulePart 133
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250-C20B · Turboshaft · 375
Seats4

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 26 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility20 sm
CeilingOvercast 4000 ft
Temperature / Dew Point64 F / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data