20040218015129A

Accident · Destroyed

FAA accident report · Bell 206B · Decatur, TX · February 18, 2004

Date
February 18, 2004 · 20:00 local
Place
Decatur, TX
Phase of flight
Hovering
Operating rules
Rotorcraft external load (Part 133)
Operator
H0LA
Damage
Destroyed
Aircraft
N16MV
NTSB investigation
NTSBFTW04TA075
Reported as
Bell 206B
Fatal injuries
0
Pilot’s flight hours
1,760 total140 in this make and model30 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) Aircraft was operating in a large field doing fire bucket operation/training with a U.S. Forest service crew. Pilot was attempting to pick up the canvas water bucket in the unimproved field. It appears that the rear portion of the right skid dug into the soft ground as he attempted to bring the helicopter to a hover, perhaps in an unnoticed drift to the right. The pilot reported that he felt a force pulling his skid down as he attempted to hover. He recognized the problem too late as he applied full left cyclic and lowered the collective after the helicopter exceeded the critical angle of bank into the low skid. At that point the situation was unrecoverable, and the helicopter rolled 90 degrees to the right severing all control surfaces. This appears to be a classic case of dynamic rollover, which is quite common on similar skid equipped helicopters.

As the FAA filed it

(-23) AIRCRAFT WAS OPERATING IN A LARGE FIELD DOING FIRE BUCKET OPERATION/TRAINING WITH A U.S. FOREST SERVICE CREW. PILOT WAS ATTEMPTING TO PICK UP THE CANVAS WATER BUCKET IN THE UNIMPROVED FIELD. IT APPEARS THAT THE REAR PORTION OF THE RIGHT SKID DUG INTO THE SOFT GROUND AS HE ATTEMPTED TO BRING THE HELICOPTER TO A HOVER, PERHAPS IN AN UNNOTICED DRIFT TO THE RIGHT. THE PILOT REPORTED THAT HE FELT A FORCE PULLING HIS SKID DOWN AS HE ATTEMPTED TO HOVER. HE RECOGNIZED THE PROBLEM TOO LATE AS HE APPLIED FULL LEFT CYCLIC AND LOWERED THE COLLECTIVE AFTER THE HELICOPTER EXCEEDED THE CRITICAL ANGLE OF BANK INTO THE LOW SKID. AT THAT POINT THE SITUATION WAS UNRECOVERABLE, AND THE HELICOPTER ROLLED 90 DEGREES TO THE RIGHT SEVERING ALL CONTROL SURFACES. THIS APPEARS TO BE A CLASSIC CASE OF DYNAMIC ROLLOVER, WHICH IS QUITE COMMON ON SIMILAR SKID EQUIPPED HELICOPTERS.

NTSB investigation

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