N131EH

Substantial
Minor

MESSERSCHMITT-BOELKOW-BLOHM BO-105SS/N: S-595

Accident Details

Date
Sunday, September 6, 2009
NTSB Number
CEN09LA571
Location
Thibodaux, LA
Event ID
20090908X64934
Coordinates
29.747777, -90.832778
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The pilot's inability to maintain control due to the mechanic's inadvertent switching of two cyclic control tubes of different lengths during maintenance.

Aircraft Information

Registration
N131EH
Make
MESSERSCHMITT-BOELKOW-BLOHM
Serial Number
S-595
Engine Type
Reciprocating
Year Built
1982
Model / ICAO
BO-105SSA05
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
9 JIMMY VORHOFF DR
Status
Deregistered
City
ABBEVILLE
State / Zip Code
LA 70510
Country
United States

Analysis

On September 6, 2009, about 1400 central daylight time, a Messerschmitt-Boelkow-Blohm BO-105S helicopter, N131EH, was substantially damaged during a post maintenance flight near Thibodaux, Louisiana. The pilot, the sole occupant, sustained minor injuries. The helicopter was registered to and operated by ERA Helicopters LLC., of Lake Charles, Louisiana. Visual meteorological conditions prevailed and a company flight plan was filed for the 14 Code of Federal Regulations Part 91 local flight.

According to the pilot, while in a 3-foot hover, the helicopter began an uncommanded roll to the right. The pilot attempted to arrest the roll by applying full left cyclic; however, the helicopter's roll could not be arrested. Moments later the right landing skid made contact with the ground followed by the main rotor blades. The helicopter came to rest in a right side low upright position and the pilot was able to exit unassisted.

According to a Federal Aviation Administration (FAA) inspector who responded to the accident site, the purpose of the flight was to perform an operational flight check of maintenance performed to the cyclic control system. Prior to the accident flight, a company mechanic had removed both the lower lateral and longitudinal cyclic control tubes to replace the rod ends on both of the tubes. Although the lateral and longitudinal control tubes have the same part number, they are adjusted to different lengths. The rod ends were replaced with new ones and reinstalled in the helicopter; however, the investigation revealed that the mechanic had inadvertently switched the two control tubes during reassembly. This resulted in an out of rig condition in the cyclic control system.

In addition, a bench check and a teardown were performed on the hydraulic control pack. There were no anomalies noted with the hydraulic system. Continuity was established in the "non-boosted" cyclic control system, and no anomalies were noted. The cyclic system above the hydraulic pack was damaged as result of the accident, but was functional. There also were no anomalies noted with the swashplate system or the main rotor system.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN09LA571