N49588

Substantial
None

Bell 206 B2S/N: 1726

Summary

On January 13, 2008, a Bell 206 B2 (N49588) was involved in an incident near La Verna, CA. 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 pilot's improper preflight planning which resulted in a jammed cyclic control while maneuvering.

The commercial pilot and mechanic were conducting a maintenance test flight to facilitate a dynamic track and balance of the main rotor system when the accident occurred. In a written statement, the pilot reported the helicopter was in a three-foot hover, moving forward, when control was lost. The helicopter subsequently collided with terrain resulting in substantial damage to the fuselage. The pilot reported the left cyclic control was removed prior to the flight; however, the protective cover was not installed. He stated that during the accident flight, the test equipment (used for track and balance) "became entangled" at the left cyclic attach point and prevented full cyclic control.

This incident is documented in NTSB report SEA08CA059. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N49588.

Accident Details

Date
Sunday, January 13, 2008
NTSB Number
SEA08CA059
Location
La Verna, CA
Event ID
20080207X00153
Coordinates
35.091388, -117.781669
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot's improper preflight planning which resulted in a jammed cyclic control while maneuvering.

Aircraft Information

Registration
Make
BELL
Serial Number
1726
Engine Type
Turbo-shaft
Model / ICAO
206 B2B06
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
LESTER CAPLAN
Address
7312 LINDELL
Status
Deregistered
City
UNIVERSITY CITY
State / Zip Code
MO 64601
Country
United States

Analysis

The commercial pilot and mechanic were conducting a maintenance test flight to facilitate a dynamic track and balance of the main rotor system when the accident occurred. In a written statement, the pilot reported the helicopter was in a three-foot hover, moving forward, when control was lost. The helicopter subsequently collided with terrain resulting in substantial damage to the fuselage. The pilot reported the left cyclic control was removed prior to the flight; however, the protective cover was not installed. He stated that during the accident flight, the test equipment (used for track and balance) "became entangled" at the left cyclic attach point and prevented full cyclic control.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA08CA059