20101231054309I

Incident · Minor damage

FAA incident report · Mcdonnell D 369E · Eugene, OR · December 31, 2010

Date
December 31, 2010 · 13:15 local
Place
Eugene, OR
Phase of flight
Descent
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N438RC
Reported as
Mcdonnell D 369E
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
1,500 total450 in this make and model10 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 helicopter was descending out of 2400 feet, seven miles from the airport of intended landing. Suddenly the aicraft rolled to the right (starboard) approximately between 110 and 130 degrees of roll (inverted). The aircraft shuddered with a severe vibration. The caution panel and engine out lights illuminated and the engine out horn sounded. The pilot nutralized the pedals and applied left cylic to right the aircraft and it responded slowly at first. The pilot entered autorotation to a small field and touched down with no further damage. The engine was at idle, but running. The pilot then did a normal shutdown. Upon post flight inspection it was discovered there had been a bird strike. There were two minor dents in the lower vertical fin and a thumb size dent about .0030 deep in one of the four tail rotor blades.

As the FAA filed it

THE HELICOPTER WAS DESCENDING OUT OF 2400 FEET, SEVEN MILES FROM THE AIRPORT OF INTENDED LANDING. SUDDENLY THE AICRAFT ROLLED TO THE RIGHT (STARBOARD) APPROXIMATELY BETWEEN 110 AND 130 DEGREES OF ROLL (INVERTED). THE AIRCRAFT SHUDDERED WITH A SEVERE VIBRATION. THE CAUTION PANEL AND ENGINE OUT LIGHTS ILLUMINATED AND THE ENGINE OUT HORN SOUNDED. THE PILOT NUTRALIZED THE PEDALS AND APPLIED LEFT CYLIC TO RIGHT THE AIRCRAFT AND IT RESPONDED SLOWLY AT FIRST. THE PILOT ENTERED AUTOROTATION TO A SMALL FIELD AND TOUCHED DOWN WITH NO FURTHER DAMAGE. THE ENGINE WAS AT IDLE, BUT RUNNING. THE PILOT THEN DID A NORMAL SHUTDOWN. UPON POST FLIGHT INSPECTION IT WAS DISCOVERED THERE HAD BEEN A BIRD STRIKE. THERE WERE TWO MINOR DENTS IN THE LOWER VERTICAL FIN AND A THUMB SIZE DENT ABOUT .0030 DEEP IN ONE OF THE FOUR TAIL ROTOR BLADES.

Other reports on N438RC · 1

Matched to the same aircraft by N-number and date.