20090928049869A

Accident · Substantial damage

FAA accident report · Hughes 369A (OH-6A) · Wasilla, AK · September 28, 2009

Date
September 28, 2009 · 17:00 local
Place
Wasilla, AK
Airport
Wolf Lake
Phase of flight
Other, Specify
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N501SU
NTSB investigation
NTSBANC09LA110
Reported as
Hughes 369A (OH-6A
Reported engine
Rolls Royce 250
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
2,300 total80 in this make and model15 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.

The pilot and owner of the helicopter told investigators that during climb from a hover the aircraft experienced a sudden loss of power at approximately 25 feet AGL and 30 knots of forward airspeed. He said the sudden loss of power caused the rotor RPM to decline and during his attempt to accomplish a low rotor RPM autorotation the aircraft landed hard. The hard landing caused the main rotor blades to strike the tail boom and sever it from the fuselage. There was one passenger onboard at the time of the accident. There were no injuries to the passenger or pilot. The pilot further stated the engine had approximately 100 hours of operation hours remaining until it was scheduled to be removed for overhaul. A review of the aircraft maintenance records by the FAA inspector confirmed the pilot/owner's statement. The records showed that the helicopter was in regulatory compliance of required inspections including airworthiness directives. The records also showed the N2 governor was replaced on July 15, 2009 and 2.3 flight hours prior to the accident.

As the FAA filed it

THE PILOT AND OWNER OF THE HELICOPTER TOLD INVESTIGATORS THAT DURING CLIMB FROM A HOVER THE AIRCRAFT EXPERIENCED A SUDDEN LOSS OF POWER AT APPROXIMATELY 25 FEET AGL AND 30 KNOTS OF FORWARD AIRSPEED. HE SAID THE SUDDEN LOSS OF POWER CAUSED THE ROTOR RPM TO DECLINE AND DURING HIS ATTEMPT TO ACCOMPLISH A LOW ROTOR RPM AUTOROTATION THE AIRCRAFT LANDED HARD. THE HARD LANDING CAUSED THE MAIN ROTOR BLADES TO STRIKE THE TAIL BOOM AND SEVER IT FROM THE FUSELAGE. THERE WAS ONE PASSENGER ONBOARD AT THE TIME OF THE ACCIDENT. THERE WERE NO INJURIES TO THE PASSENGER OR PILOT. THE PILOT FURTHER STATED THE ENGINE HAD APPROXIMATELY 100 HOURS OF OPERATION HOURS REMAINING UNTIL IT WAS SCHEDULED TO BE REMOVED FOR OVERHAUL. A REVIEW OF THE AIRCRAFT MAINTENANCE RECORDS BY THE FAA INSPECTOR CONFIRMED THE PILOT/OWNER'S STATEMENT. THE RECORDS SHOWED THAT THE HELICOPTER WAS IN REGULATORY COMPLIANCE OF REQUIRED INSPECTIONS INCLUDING AIRWORTHINESS DIRECTIVES. THE RECORDS ALSO SHOWED THE N2 GOVERNOR WAS REPLACED ON JULY 15, 2009 AND 2.3 FLIGHT HOURS PRIOR TO THE ACCIDENT.

NTSB investigation

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