N910U

Substantial
None

Eurocopter France EC-130 B4S/N: 3470

Accident Details

Date
Monday, August 9, 2004
NTSB Number
DEN04CA122
Location
Englewood, CO
Event ID
20040908X01358
Coordinates
39.567222, -104.849998
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

the pilot's failure to perform a preflight inspection. Contributing to the accident was the transmission cowling that disconnected during the landing.

Aircraft Information

Registration
Make
EUROCOPTER FRANCE
Serial Number
3470
Engine Type
Turbo-shaft
Year Built
2001
Model / ICAO
EC-130 B4
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
6
FAA Model
EC 130 B4

Registered Owner (Current)

Name
AIR METHODS LLC
Address
5500 S QUEBEC ST STE 300
City
GREENWOOD VILLAGE
State / Zip Code
CO 80111-1914
Country
United States

Analysis

On August 9, 2004, at approximately 1700 mountain daylight time, a Eurocopter EC 130 B4, N910U, operated by Air Methods and piloted by a commercial pilot, was substantially damaged during ground hover operations at Centennial Airport, Englewood, Colorado. Visual meteorological conditions prevailed at the time of the accident. The test flight was being conducted under the provisions of Title 14 CFR Part 91 without a flight plan. The pilot reported no injuries. The local flight was originating at the time of the accident.

According to the accident report submitted by the pilot, the helicopter had just undergone maintenance and was preparing for a second test flight. The helicopter had departed approximately 15 minutes prior to the accident and returned due to an inoperative HSI. A thorough preflight had been conducted for the first test flight. While the HSI was being repaired, another maintenance technician opened the transmission cowling. The pilot and two avionics technicians boarded the helicopter from the left side, without performing an additional preflight or walk around. The pilot performed a run-up and lifted the helicopter to a hover when an individual on the ground noticed that the cowling was open. The lead mechanic then signaled to the pilot for him to land. As the helicopter set back down, the transmission cowling detached and impacted a main rotor blade and the tail boom. The main rotor blade was damaged at the root and the tail boom was creased and punctured. After the accident, the mechanic reported that it was hot inside and he decided to leave the cowling open.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN04CA122