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March 31, 2003 · Hughes 369D · N90431

Tyonek, AK

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
March 31, 2003
Injury Outcomes
No injuries (2 uninjured)
Location
Tyonek, AK
Aircraft
Hughes 369D
Tail Number
N90431
Operator
Prism Helicopters
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ANC03LA038

The commercial certificated helicopter pilot was conducting external load operations in support of seismic operations, and landed a high skid-equipped helicopter in a confined area to pick up a passenger. The landing area had knee to waist level brush. The pilot did not exit the helicopter, but waited until the passenger climbed aboard. The pilot reported that the passenger unknowingly drug a seismic cable over the toe of the left skid as he climbed into the helicopter. As the pilot was lifting the helicopter into a hover, the cable slid aft into the helicopter's external load mirror. The cable severed the mirror from the helicopter, and the mirror was propelled upward, into the main rotor blades. The mirror then struck the vertical stabilizer. A postaccident examination of the rotor system revealed that one rotor blade sustained a dent on the underside of the blade. The director of operations stated that the damaged blade was beyond allowable repair limits, and had to be replaced.

NTSB Probable Cause

The pilot's inadequate visual lookout while lifting into a hover to ensure the helicopter was clear of all objects, which resulted in separation of an external mirror that then struck and damaged a main rotor blade. Factors in the accident were the presence of a seismic cable, and high vegetation around the helicopter's takeoff spot.

Full Narrative

On March 31, 2003, about 1000 Alaska standard time, a Hughes 369D helicopter, N90431, sustained substantial damage when a main rotor blade and the vertical stabilizer were struck by a severed external load mirror as the helicopter was lifting into a hover, about 7 miles southwest of Tyonek, Alaska. The helicopter was being operated as a visual flight rules (VFR) external load operation under Title 14, CFR Part 133, when the accident occurred. The helicopter was operated by Prism Helicopters Inc., Wasilla, Alaska. The commercial certificated pilot, and the sole passenger, were not injured. Visual meteorological conditions prevailed, and VFR company flight following procedures were in effect. During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), on April 4, the director of operations for the operator reported the pilot was lifting the helicopter into a hover in support of seismic operations. The director of operations said that as the pilot lifted off out of a confined area, he was not aware that the seismic cable was caught on the front toe of the left landing gear skid tube. As the helicopter gained altitude, the cable slid aft into the helicopter's external load mirror. The cable severed the mirror from the helicopter, and the mirror was propelled upward, into the main rotor blades. The mirror then struck the vertical stabilizer. In the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1) submitted by the pilot, the pilot indicated that he landed the high skid-equipped helicopter in an area of knee to waist level brush to pick up the passenger. The pilot did not exit the helicopter, but waited until the passenger climbed aboard. The pilot reported that the passenger "apparently drug the seismic cable (black, less than 1 centimeter diameter) over toe of skid, unbeknownst to either the pilot or passenger." A postaccident examination of the rotor system revealed that one rotor blade sustained a dent on the underside of the blade. The director of operations stated that the damaged blade was beyond allowable repair limits, and had to be replaced.

Flight

Event TypeAccident
Event Time05:00 AKST
Nearest Airport0nm
Flight Plan FiledCvfr
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHughes 369D
Tail NumberN90431
Aircraft CategoryHeli
DamageSubstantial
OperatorPrism Helicopters
Operating RulePart 133
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250-C20B · Turboshaft · 420
Seats5

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 44 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
Wind200° @ 5 kt
Visibility30 sm
CeilingNone
Temperature / Dew Point19 C / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data