N856HA

Substantial
Minor

Robinson R22 MarinerS/N: 1894M

Accident Details

Date
Monday, July 5, 2004
NTSB Number
SEA04CA122
Location
Hillsboro, OR
Event ID
20040803X01137
Coordinates
45.595001, -122.933334
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
1
Total Aboard
2

Probable Cause and Findings

The pilot's failure to maintain aircraft control resulting in an uncontrolled descent and subsequent roll over. Low altitude flight and the pilot's encounter with settling with power were contributing factors.

Aircraft Information

Registration
N856HA
Make
ROBINSON
Serial Number
1894M
Engine Type
Reciprocating
Model / ICAO
R22 MarinerR22
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
HILLSBORO AVIATION INC
Address
3565 NE CORNELL RD
Status
Deregistered
City
HILLSBORO
State / Zip Code
OR 97124-6374
Country
United States

Analysis

On July 5, 2004, at 1500 Pacific daylight time, a Robinson R-22 Mariner, N856HA, registered to and operated by Hillsboro Aviation as a 14 CFR Part 91 instructional flight, experienced a hard landing followed by a rollover at the Portland-Hillsboro Airport, Hillsboro, Oregon. Visual meteorological conditions prevailed at the time and no flight plan was filed for the local instructional flight. The helicopter was substantially damaged and the certified flight instructor was not injured, while the commercial pilot (student) received minor injuries.

In a written statement, the flight instructor reported that they were in the process of practicing "maximum performance takeoff abort - backwards." The student was on the controls during the maximum performance takeoff phase to an altitude of about 150 feet above ground level, and the instructor took over the controls to demonstrate the abort procedures. The instructor took the controls just prior to call for the abort. When the abort phase began, the instructor applied aft cyclic and slightly lowered the collective. The helicopter had been in a tail low attitude and started to descend into "settling with power." The instructor applied forward cyclic and lowered the collective, however the helicopter did not have sufficient altitude to level out or gain airspeed to recover before impacting the ground on the right side skid. The helicopter pivoted around about 180 degrees then rolled over onto its left side.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA04CA122