N2284U Brantly Helicopter B-2B accident

NTSB MIA90LA150 · 1990-07-10 · CHRISTIANSTED

Docket — crew, injuries and powerplant

Factual narrative

HELICOPTER WAS AT NEAR GROSS WEIGHT AND PILOT ESTIMATED TEMPERATURE AT HELIPAD TO BE 90 DEGREES FAHRENHEIT. AS HELICOPTER LIFTED OFF HE PERFORMED LEFT PEDAL TURN WHICH REQUIRES ADDITIONAL ENGINE POWER. HELICOPTER DESENDED DOWN HILL AWAY FROM HELIPAD AND ALTITUDE COULD NOT BE MAINTAINED WITH FULL ENGINE POWER. LEFT SKID CONTACTED TREE STUMP AND HELICOPTER ROLLED OVER.

Probable cause

THE FAILURE OF THE PILOT TO EVALUATE WEIGHT, TEMPERATURE, AND POWER AVAILABLE PRIOR TO TAKEOFF AND THEN PERFORMING A LEFT PEDAL TURN AFTER TAKEOFF RESULTING IN THE HELICOPTER DESENDING EVEN THOUGH FULL POWER WAS APPLIED. The National Transportation Safety Board determined the probable cause of this accident.

Circumstances

Event type
Accident
Highest injury
None
Weather conditions
Visual Meteorological Cond
Light condition
Day
Sky condition
NONE
Ceiling (ft)
0
Visibility (sm)
15
Wind direction
160
Wind speed (kt)
12
Temperature (F)
82
Distance from field
0.0

Aircraft

RegistrationMakeModelDamageFAR part
N2284U Brantly Helicopter B-2B SUBS 091

Sequence of events

#OccurrencePhase
1 250 Cruise
2 230 Cruise
3 380 Descent

Findings

Finding
17310 cause
23203 cause