N9877Z

Substantial
None

Bell 206L-1S/N: 45339

Accident Details

Date
Wednesday, May 4, 2005
NTSB Number
DFW05CA121
Location
Georgetown, TX
Event ID
20050622X00838
Coordinates
30.673889, -97.674163
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
6
Total Aboard
6

Probable Cause and Findings

The pilot's improper flare resulting in a hard landing.

Aircraft Information

Registration
N9877Z
Make
BELL
Serial Number
45339
Engine Type
Turbo-shaft
Year Built
1973
Model / ICAO
206L-1B06T
Aircraft Type
Rotorcraft
No. of Engines
2

Registered Owner (Historical)

Name
BDB AVIATION
Address
5910 BOLD RULER WAY
Status
Deregistered
City
AUSTIN
State / Zip Code
TX 78746-1841
Country
United States

Analysis

On May 4, 2005, approximately 1030 central daylight time, a single-engine Bell 206L-1 helicopter, N9877Z, was substantially damaged during a hard landing during a precautionary landing near Georgetown, Texas. The airline transport rated pilot and five passengers were uninjured. The helicopter was owned and operated by Crystal Fingers Corporation of Georgetown, Texas. Visual meteorological conditions prevailed, and a flight plan was not filed for the training flight conducted under the provisions of 14 Code of Federal Regulations Part 91. The local flight departed the Georgetown Municipal Airport (GTU), near Georgetown, Texas, at 1415.

According to a written statement submitted by the 5,600-hour pilot, while in cruise flight at an estimated 500 feet AGL and while holding an airspeed of 90 knots, the helicopter experienced an "uncontrolled 40-degree yaw to the right, following a shutter and vibration in the fuselage and tail section." The pilot elected to execute a precautionary landing on a highway. During the landing flare, the helicopter landed hard with a slight running landing.

In a follow-up interview with a Federal Aviation Administration (FAA) inspector, who inspected the helicopter, the pilot added that the helicopter bounced back into the air after the hard landing on the road, coming to rest on the edge of the road.

Post-accident examination of the helicopter revealed damage to the outter portions of each main rotor blade, the tail rotor drive, the bearing journals, tail rotor drive shaft fairing, vertical fin, and the tail boom assembly,

At 1455, the automated weather observing system at GTU, approximately 2 miles from the accident site, reported wind from 190 degrees at 4 knots, 10 statute miles visibility, few clouds at 4,800 feet, temperature 73 degrees Fahrenheit, dew point 48 degrees Fahrenheit, and an altimeter setting of 30.19 inches of Mercury.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DFW05CA121