20060615010819A

Accident · Substantial damage

FAA accident report · Bell 206L-3 · Vernal, UT · June 15, 2006

Date
June 15, 2006 · 17:15 local
Place
Vernal, UT
Phase of flight
To Aborted (Copter/Run Takoff)
Operating rules
Air taxi and commuter (Part 135)
Operator
SVFA
Damage
Substantial damage
Aircraft
N265SH
NTSB investigation
NTSBSEA06LA121
Reported as
Bell 206L3
People aboard
4
Fatal injuries
0
Pilot’s flight hours
1,607 total557 in this make and model134 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) Pilot was operating out of a remote site at 7240 MSL with a density altitude of approx 9700 feet. There were five passengers on board and the aircraft was 40 pounds below max gross weight. The take off area was located in heavy sage brush with some cedar trees and an upslope in the departure path. The flight manual was within the weight limits for a ground effect hover operations but 200 pounds over the limit for out of ground effect hover operations for the existing conditions. The engine was unable to produce sufficient power for take off, the pilot attempted to abort the take-off. The rotor RPM had dropped below the operating limit resulting in loss of control, and aircraft struck the ground and rolled over.

As the FAA filed it

(-23) PILOT WAS OPERATING OUT OF A REMOTE SITE AT 7240 MSL WITH A DENSITY ALTITUDE OF APPROX 9700 FEET. THERE WERE FIVE PASSENGERS ON BOARD AND THE AIRCRAFT WAS 40 POUNDS BELOW MAX GROSS WEIGHT. THE TAKE OFF AREA WAS LOCATED IN HEAVY SAGE BRUSH WITH SOME CEDAR TREES AND AN UPSLOPE IN THE DEPARTURE PATH. THE FLIGHT MANUAL WAS WITHIN THE WEIGHT LIMITS FOR A GROUND EFFECT HOVER OPERATIONS BUT 200 POUNDS OVER THE LIMIT FOR OUT OF GROUND EFFECT HOVER OPERATIONS FOR THE EXISTING CONDITIONS. THE ENGINE WAS UNABLE TO PRODUCE SUFFICIENT POWER FOR TAKE OFF, THE PILOT ATTEMPTED TO ABORT THE TAKE-OFF. THE ROTOR RPM HAD DROPPED BELOW THE OPERATING LIMIT RESULTING IN LOSS OF CONTROL, AND AIRCRAFT STRUCK THE GROUND AND ROLLED OVER.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.