N404LE

Substantial
None

ROBINSON HELICOPTER R22 BETAS/N: 4040

Summary

On August 14, 2010, a Robinson Helicopter R22 BETA (N404LE) was involved in an incident near Mack, CO. All 2 people aboard were uninjured. The aircraft sustained substantial damage.

The National Transportation Safety Board determined the probable cause of this incident to be: The flight instructor's failure to maintain control of the helicopter during a practice autorotation, which resulted in a hard landing.

The certified flight instructor and his student were practicing a 180 degree autorotation with a power recovery to a hover, when the helicopter's sink rate increased dramatically in the flare about 40 feet above the ground. The flight instructor called for a go-around and increased power, raised the collective, and pushed the cyclic forward. The helicopter continued to descend and contacted the runway in a level attitude. After it came to a stop, a vibration was felt and the instructor confirmed that the main rotor blade had struck the tail boom. The instructor reported that there were no mechanical deficiencies with the helicopter.

This incident is documented in NTSB report CEN10CA485. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N404LE.

Accident Details

Date
Saturday, August 14, 2010
NTSB Number
CEN10CA485
Location
Mack, CO
Event ID
20100818X30857
Coordinates
39.267501, -108.858329
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The flight instructor's failure to maintain control of the helicopter during a practice autorotation, which resulted in a hard landing.

Aircraft Information

Registration
Make
ROBINSON HELICOPTER
Serial Number
4040
Engine Type
Reciprocating
Model / ICAO
R22 BETAR22
Aircraft Type
Rotorcraft
No. of Engines
1

Analysis

The certified flight instructor and his student were practicing a 180 degree autorotation with a power recovery to a hover, when the helicopter's sink rate increased dramatically in the flare about 40 feet above the ground. The flight instructor called for a go-around and increased power, raised the collective, and pushed the cyclic forward. The helicopter continued to descend and contacted the runway in a level attitude. After it came to a stop, a vibration was felt and the instructor confirmed that the main rotor blade had struck the tail boom. The instructor reported that there were no mechanical deficiencies with the helicopter.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN10CA485