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Aviation safety reports, made easier to study

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September 10, 1993 · Aerospatiale SA-365-N2 · N818R

Ogden, UT

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 10, 1993
Injury Outcomes
6 injuries (1 fatality, 2 serious injuries, 3 minor injuries)
Location
Ogden, UT
Aircraft
Aerospatiale SA-365-N2
Tail Number
N818R
Operator
American Stores
Injuries
Fatal
Aircraft Damage
Destroyed
NTSB Number
SEA93LA196

DURING A FLIGHT FOR THE PURPOSE OF AERIAL PHOTOGRAPHY, THE HELICOPTER WAS FLYING OVER GLASSY WATER CONDITIONS. THE PILOT HAD SET THE BUG ON THE RADAR ALTIMETER FOR 50 FEET; HOWEVER, WHILE HE WAS LOOKING OUTSIDE FOR REFERENCE, THE HELICOPTER DESCENDED BELOW 50 FEET. THE PILOT STATED THAT HE SUDDENLY HAD A SENSATION OF MOVEMENT OVER THE WATER, AND JUST SECONDS BEFORE IMPACT WITH THE WATER, THE PILOT NOTED TEN FEET ABOVE WATER LEVEL ON THE RADAR ALTIMETER.

NTSB Probable Cause

THE PILOT'S FAILURE TO MAINTAIN PROPER ALTITUDE. A FACTOR TO THE ACCIDENT WAS GLASSY WATER.

Full Narrative

On September 10, 1993, at 1530 mountain daylight time, an Aerospatiale SA365N2, N818R, collided with the water in the Great Salt Lake while maneuvering 10 miles west of Ogden, Utah. Visual meteorological conditions prevailed at the time and no flight plan was filed for the corporate flight. The helicopter was destroyed and the certificated Airline Transport pilot and two passengers suffered minor injuries, two passengers were seriously injured, and one passenger was fatally injured. The flight had departed from the Ogden area on September 19, 1993, at 1330. The pilot reported that the purpose of the flight was to take a camera crew up to produce aerial videography and still photos of the area's mineral extraction facilities. The helicopter had been flying in the area for approximately two hours at varying altitudes from 50 feet to 900 feet. While travelling back to the landing area, the camera director wanted to get one more shot of the water at low level. The pilot noted that the water was calm and glassy and provided no depth perception. The pilot set the decision height "bug" to 50 feet on the radar altimeter then began the descending right turn at 300 feet per minute and 95 knots. At 50 feet above water level, the pilot rolled to level flight and slowed the helicopter to 60 to 70 knots. The pilot was using outside reference while maneuvering and stated that he suddenly turned his attention to the radar altimeter when he felt the sensation of speed over the water and noted that the altitude read 10 feet. Approximately two seconds later the helicopter contacted the water surface. The helicopter pitched over and came to rest on its left side in four feet of water. The pilot reported that there were no mechanical failures or malfunctions with the helicopter at the time of the accident.

Flight

Event TypeAccident
Event Time15:30 MDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftAerospatiale SA-365-N2
Tail NumberN818R
Aircraft CategoryHeli
DamageDestroyed
OperatorAmerican Stores
Operating RulePart 91
Engines2
Engine TypeTurboshaft
Engine DetailsTurbomeca · ARRIEL 1C2 · Turboshaft · 724
Seats10

People & Injuries

Injury Summary6 injuries (1 fatality, 2 serious injuries, 3 minor injuries)
Fatal1
Serious2
Minor3
Uninjured0
Total6
Crew 1Age 43 · First Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility20 sm
CeilingNone
Temperature / Dew Point0 C
Altimeter30.00 inHg
Observation Time21:45
Weather SourceWFAC

Appendix: Source Data