N8897F

Substantial
None

HUGHES 269AS/N: 83-0274

Summary

On June 01, 2010, a Hughes 269A (N8897F) was involved in an incident near Cannon Falls, MN. All 1 person aboard were uninjured. The aircraft sustained substantial damage.

The National Transportation Safety Board determined the probable cause of this incident to be: The pilot's failure to maintain rotor speed during the autorotation, which resulted in an excessive sink rate and a hard landing.

The pilot reported that shortly after liftoff he noticed a “disturbing vibration” in the helicopter. He initiated an autorotation to an open agricultural field. The pilot stated that he executed a 180-degree turn in order to avoid a tree line. He noted that the rotor speed got too low and he was unable to reduce the sink rate, which resulted in a hard landing. The main rotor contacted and separated the tail boom, and the right landing skid collapsed during the accident sequence. The pilot noted that additional practice in autorotation descents and landings might have prevented the accident.

This incident is documented in NTSB report CEN10CA280. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N8897F.

Accident Details

Date
Tuesday, June 1, 2010
NTSB Number
CEN10CA280
Location
Cannon Falls, MN
Event ID
20100601X64459
Coordinates
44.481109, -92.761108
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's failure to maintain rotor speed during the autorotation, which resulted in an excessive sink rate and a hard landing.

Aircraft Information

Registration
Make
HUGHES
Serial Number
83-0274
Year Built
1963
Model / ICAO
269A

Registered Owner (Historical)

Name
PARKER ELLEN R
Address
76 CONGRESS ST W
Status
Deregistered
City
SAINT PAUL
State / Zip Code
MN 55107-1106
Country
United States

Analysis

The pilot reported that shortly after liftoff he noticed a “disturbing vibration” in the helicopter. He initiated an autorotation to an open agricultural field. The pilot stated that he executed a 180-degree turn in order to avoid a tree line. He noted that the rotor speed got too low and he was unable to reduce the sink rate, which resulted in a hard landing. The main rotor contacted and separated the tail boom, and the right landing skid collapsed during the accident sequence. The pilot noted that additional practice in autorotation descents and landings might have prevented the accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN10CA280