20120922019379I

Incident · Minor damage

FAA incident report · Bell 205A-1 · La Grande, OR · September 22, 2012

Date
September 22, 2012 · 15:48 local
Place
La Grande, OR
Airport
La Grande/Union County
Phase of flight
Climb
Operating rules
Rotorcraft external load (Part 133)
Operator
GFLA
Damage
Minor damage
Aircraft
N689H
Reported as
Bell 205A-1
Reported engine
Alliedsign T5317A-1
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
15,000 total2,000 in this make and model35 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 was dipping water from a remote pond with a bucket on a 100' long line for usfs fire fighting use. During the climb with a full bucket the pilot heard a bang and the aircraft rolled slightly to the rt. The power the engine was developing had been reduced and the rotor RPM was slowing. The pilot assumed he had experienced a compressor stall. The pilot lowered the nose to gain RPM. As the RPM was coming back the pilot tried to increase collective to climb out again but felt the same noise and rotation again. Having no more altitude the pilot saw an opening in the trees, dropped the bucket and line and made a precautionary landing. During the landing flare the aircraft main rotor struck a tree. The main rotor blades suffered a crease and one blade had a hole through it. There was no other damage to the aircraft.

As the FAA filed it

THE PILOT WAS DIPPING WATER FROM A REMOTE POND WITH A BUCKET ON A 100' LONG LINE FOR USFS FIRE FIGHTING USE. DURING THE CLIMB WITH A FULL BUCKET THE PILOT HEARD A BANG AND THE AIRCRAFT ROLLED SLIGHTLY TO THE RT. THE POWER THE ENGINE WAS DEVELOPING HAD BEEN REDUCED AND THE ROTOR RPM WAS SLOWING. THE PILOT ASSUMED HE HAD EXPERIENCED A COMPRESSOR STALL. THE PILOT LOWERED THE NOSE TO GAIN RPM. AS THE RPM WAS COMING BACK THE PILOT TRIED TO INCREASE COLLECTIVE TO CLIMB OUT AGAIN BUT FELT THE SAME NOISE AND ROTATION AGAIN. HAVING NO MORE ALTITUDE THE PILOT SAW AN OPENING IN THE TREES, DROPPED THE BUCKET AND LINE AND MADE A PRECAUTIONARY LANDING. DURING THE LANDING FLARE THE AIRCRAFT MAIN ROTOR STRUCK A TREE. THE MAIN ROTOR BLADES SUFFERED A CREASE AND ONE BLADE HAD A HOLE THROUGH IT. THERE WAS NO OTHER DAMAGE TO THE AIRCRAFT.