19980808030099A

Accident · Substantial damage

FAA accident report · Bell 212 · Juntura, OR · August 8, 1998

Date
August 8, 1998 · 15:07 local
Place
Juntura, OR
Phase of flight
Hovering
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N291B
NTSB investigation
NTSBSEA98GA159
Reported as
Bell 212
People aboard
1
Fatal injuries
0
Pilot’s flight hours
12,000 total500 in this make and model100 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) The scenario began as the helicopter was in a hover just beginning to lower the water bucket into a large pond. The pilot reported losing lift and slipped to the right to gain clean air. As the pilot applied additional collective control, the low rotor speed alarm sounded a glance at the two N1 gauges showed #1 to be "0" and #2 to be in the high 90'S. The pilot then made two attempts to release the bucket (being successful on the second) and then executed an autorotation maneuver resulting in a landing in the soft mud adjacent to the pond. The helicopter recieved damage to the rotor blades as well as substantial damage to the belly of the acft.

As the FAA filed it

(-23) THE SCENARIO BEGAN AS THE HELICOPTER WAS IN A HOVER JUST BEGINNING TO LOWER THE WATER BUCKET INTO A LARGE POND. THE PILOT REPORTED LOSING LIFT AND SLIPPED TO THE RIGHT TO GAIN CLEAN AIR. AS THE PILOT APPLIED ADDITIONAL COLLECTIVE CONTROL, THE LOW ROTOR SPEED ALARM SOUNDED A GLANCE AT THE TWO N1 GAUGES SHOWED #1 TO BE "0" AND #2 TO BE IN THE HIGH 90'S. THE PILOT THEN MADE TWO ATTEMPTS TO RELEASE THE BUCKET (BEING SUCCESSFUL ON THE SECOND) AND THEN EXECUTED AN AUTOROTATION MANEUVER RESULTING IN A LANDING IN THE SOFT MUD ADJACENT TO THE POND. THE HELICOPTER RECIEVED DAMAGE TO THE ROTOR BLADES AS WELL AS SUBSTANTIAL DAMAGE TO THE BELLY OF THE ACFT.

NTSB investigation

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