20050626011369A

Accident · Substantial damage

FAA accident report · Robsin R44RAVENII · Indianola, UT · June 26, 2005

Date
June 26, 2005 · 12:00 local
Place
Indianola, UT
Phase of flight
Pwr On Vertical Ldng/Rtrcrft
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N373DM
NTSB investigation
NTSBDEN05CA097
Reported as
Robsin R44RAVENII
Reported engine
Lycoming O540*
People aboard
3
Fatal injuries
0
Pilot’s flight hours
150 total150 in this make and model55 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 making approach to open field site with three passengers plus himself on board. Temp was approx 55F, pa 6100 MSL, hald tanks of fuel, headed into wind. As pilot attempted to terminate to a hover at 20 feet AGL he noted low rotor RPM and low RPM audio sounded. He attempted to roll on throttle to regain RPM but aircraft settled landing in small revine and rolling over on side. Damage to main fuselage frame, tail boom landing gear and main rotor. Minor injuries to pilot, no other injuries. Based on available information aircraft weight was 2215 lbs, hover oge limit for the conditions is 2340 lbs.

As the FAA filed it

(-23) PILOT WAS MAKING APPROACH TO OPEN FIELD SITE WITH THREE PASSENGERS PLUS HIMSELF ON BOARD. TEMP WAS APPROX 55F, PA 6100 MSL, HALD TANKS OF FUEL, HEADED INTO WIND. AS PILOT ATTEMPTED TO TERMINATE TO A HOVER AT 20 FEET AGL HE NOTED LOW ROTOR RPM AND LOW RPM AUDIO SOUNDED. HE ATTEMPTED TO ROLL ON THROTTLE TO REGAIN RPM BUT AIRCRAFT SETTLED LANDING IN SMALL REVINE AND ROLLING OVER ON SIDE. DAMAGE TO MAIN FUSELAGE FRAME, TAIL BOOM LANDING GEAR AND MAIN ROTOR. MINOR INJURIES TO PILOT, NO OTHER INJURIES. BASED ON AVAILABLE INFORMATION AIRCRAFT WEIGHT WAS 2215 LBS, HOVER OGE LIMIT FOR THE CONDITIONS IS 2340 LBS.

NTSB investigation

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