N234LAROBINSON HELICOPTER R22 BETA2009-02-06 NTSB Accident Report

Substantial
None

ROBINSON HELICOPTER R22 BETAS/N: 3534

Summary

On February 06, 2009, a Robinson Helicopter R22 BETA (N234LA) was involved in an incident near Cypress, TX. 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 student pilot's failure to maintain adequate main rotor rpm and the instructor's delayed remedial action.

While performing a 180-degree autorotation, the student pilot raised the collective in order to maintain the rotor rpms within normal parameters. At approximately 250 feet above ground level, the rotor rpm was allowed to decay to 95% at which time the helicopter began to sink. The lowest observed rpm was 85%. The certified flight instructor took control of the helicopter, but could not recover prior to impact with terrain. The helicopter landed hard and rolled onto its left side. Substantial crushing damage was sustained to the fuselage. Winds at the time of the accident were 190 degrees at 14 knots gusting to 30 knots.

This incident is documented in NTSB report CEN09CA157. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N234LA.

Accident Details

Date
Friday, February 6, 2009
NTSB Number
CEN09CA157
Location
Cypress, TX
Event ID
20090209X44415
Coordinates
30.085832, -95.599166
Nearest Airport
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The student pilot's failure to maintain adequate main rotor rpm and the instructor's delayed remedial action.

Aircraft Information

Registration
Make
ROBINSON HELICOPTER
Serial Number
3534
Engine Type
Reciprocating
Year Built
2004
Model / ICAO
R22 BETAR22
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
HELICOPTER SERVICES INC
Address
19931 STUEBNER AIRLINE RD # A
Status
Deregistered
City
SPRING
State / Zip Code
TX 77379-5472
Country
United States

Analysis

While performing a 180-degree autorotation, the student pilot raised the collective in order to maintain the rotor rpms within normal parameters. At approximately 250 feet above ground level, the rotor rpm was allowed to decay to 95% at which time the helicopter began to sink. The lowest observed rpm was 85%. The certified flight instructor took control of the helicopter, but could not recover prior to impact with terrain. The helicopter landed hard and rolled onto its left side. Substantial crushing damage was sustained to the fuselage. Winds at the time of the accident were 190 degrees at 14 knots gusting to 30 knots.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN09CA157