N96MB

Destroyed
None

Bell 47G2S/N: 2443

Accident Details

Date
Saturday, August 14, 2004
NTSB Number
CHI04CA229
Location
Muncie, IN
Event ID
20040917X01458
Coordinates
40.154998, -85.316665
Aircraft Damage
Destroyed
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The engine failure for an undetermined reason, and the pilot's inability to properly level-off for landing due to the low rotor speed, which resulted in the hard landing. The low altitude where the engine failure occurred was a factor.

Aircraft Information

Registration
N96MB
Make
BELL
Serial Number
2443
Engine Type
Reciprocating
Year Built
1958
Model / ICAO
47G2B47G
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
6425 S DENNING AVE
Status
Deregistered
City
OKLAHOMA CITY
State / Zip Code
OK 73169-6937
Country
United States

Analysis

On August 14, 2004, about 1500 eastern standard time, a Bell 47G2 helicopter, N96MB, piloted by a private pilot, was destroyed when it impacted the ground during an attempted forced landing. The helicopter was on initial climb after takeoff when it experienced a loss of engine power. The 14 CFR Part 91 personal flight was operating in visual meteorological conditions without a flight plan. The pilot and his one passenger were not injured. The helicopter had just departed the Reese Airport, Muncie, Indiana, for a local flight.

The pilot reported that he had taken off from the Reese Airport and had made a turn to parallel the runway when he heard two loud "bangs" from the engine after which the engine stopped producing power. The pilot stated that he was at 50 feet and 45 miles per hour when the power loss occurred. The pilot stated that he performed an autorotation to a flat area near the airport. He stated that as he "approached touchdown [he] raised collective to cushion the impact but with so little altitude an autorotation gave very little rotor speed." He stated that the helicopter struck the ground in a level attitude while moving forward, the skids collapsed and the helicopter broke apart.

A postaccident examination of the helicopter was conducted. During the examination, the engine was found to rotate. The engine produced compression on all cylinders when rotated by hand. No further components of the engine were tested.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI04CA229