20140608010449A

Accident · Substantial damage

FAA accident report · Mcdonnell Douglas Helicopter 369E · Gilbert, AZ · June 8, 2014

Date
June 8, 2014 · 01:05 local
Place
Gilbert, AZ
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N504MP
NTSB investigation
NTSBWPR14TA236
Reported as
Mcdonnell Douglas Helicopter 369E
Reported engine
Rolls-Royce 250
People aboard
2
Fatal injuries
0
Other injuries
2
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
825 total825 in this make and model150 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.

On 06/08/2014 at 0105 local time, mesa police dept helicopter N504MP experienced a loss of power during flight. Pilot reports engine began to slowly "spin down" at which point he entered an autorotation to an unlit open field. Pilot reports they were in a cruise configuration at approximately 500-700 feet AGL and 60-70 KIAS at time of power loss. Upon touchdown, the tail of the helicopter impacted the ground which caused the main rotor blades to impact the tail cone. The tail rotor section of the boom separated from the aircraft. The aircraft landed upright and there was no further damage.

As the FAA filed it

ON 06/08/2014 AT 0105 LOCAL TIME, MESA POLICE DEPT HELICOPTER N504MP EXPERIENCED A LOSS OF POWER DURING FLIGHT. PILOT REPORTS ENGINE BEGAN TO SLOWLY "SPIN DOWN" AT WHICH POINT HE ENTERED AN AUTOROTATION TO AN UNLIT OPEN FIELD. PILOT REPORTS THEY WERE IN A CRUISE CONFIGURATION AT APPROXIMATELY 500-700 FEET AGL AND 60-70 KIAS AT TIME OF POWER LOSS. UPON TOUCHDOWN, THE TAIL OF THE HELICOPTER IMPACTED THE GROUND WHICH CAUSED THE MAIN ROTOR BLADES TO IMPACT THE TAIL CONE. THE TAIL ROTOR SECTION OF THE BOOM SEPARATED FROM THE AIRCRAFT. THE AIRCRAFT LANDED UPRIGHT AND THERE WAS NO FURTHER DAMAGE.

NTSB investigation

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