N31MH

Substantial
None

Aerospatiale AS350BS/N: 2141

Accident Details

Date
Tuesday, October 4, 2005
NTSB Number
LAX06CA003
Location
Grand Canyon, AZ
Event ID
20051114X01834
Coordinates
33.629310, -112.090744
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
7
Total Aboard
7

Probable Cause and Findings

the pilot's failure to maintain control of the helicopter during landing in gusty wind conditions, which resulted in a hard landing and ground resonance.

Aircraft Information

Registration
N31MH
Make
AEROSPATIALE
Serial Number
2141
Engine Type
Turbo-shaft
Year Built
1988
Model / ICAO
AS350BAS50
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
DUNN TRACY SCOTT
Address
PO BOX 276
Status
Deregistered
City
PHOENIX
State / Zip Code
OR 97535-0276
Country
United States

Analysis

On October 3, 2005, at 1710 Pacific daylight time, an Aerospatiale AS350B, N31MH, encountered a ground resonance event following a hard landing at the Grand Canyon Airport (GCN), Grand Canyon, Arizona. The commercial rotorcraft pilot and six passengers were not injured; the helicopter sustained substantial damage. The helicopter was registered to, and operated by, Maverick Helicopters, Las Vegas, Nevada, as a sightseeing flight under the provisions of 14 CFR Part 135. The tour flight originated from GCN at 1647, and was terminating at the time of the accident. Visual meteorological conditions prevailed, and a company visual flight rules flight plan had been filed.

According to the pilot's written statement, he established the helicopter in a 3-foot hover and taxied to the helipad. As the helicopter neared the helipad, a "gust of wind lifted the aircraft into a 5- to 6-foot hover." The pilot regained control and reestablished the helicopter in a 3-foot hover and began lowering the collective to land. At 1.5 feet above the ground, another gust of wind "slammed" the helicopter onto the ground, impacting the terrain with the right front skid. A "violent vibration" began, and the pilot pulled the helicopter up in the air after realizing he was in a ground resonance situation. The vibrations dissipated, and the pilot set the helicopter down and shut off the engine.

The helicopter sustained substantial damage to its tail boom. Post accident examination of the landing skid system revealed that the spring-steel extensions were within limits and the dampers were in serviceable condition. The pilot did not report any anomalies with the helicopter prior to the event.

The pilot reported that the winds were from the south at 18 knots with gusts to 36 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# LAX06CA003