N35134

Substantial
Minor

Bell 47G-3B-1 S/N: 3591

Accident Details

Date
Saturday, July 26, 1997
NTSB Number
IAD97LA104
Location
MT. VERNON, OH
Event ID
20001208X08410
Coordinates
40.390651, -82.469184
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

The pilot's failure to maintain rotor RPM.

Aircraft Information

Registration
Make
BELL
Serial Number
3591
Engine Type
Reciprocating
Model / ICAO
47G-3B-1 B47G
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
3
FAA Model
47G-3B-1

Registered Owner (Current)

Name
SCIBELLI DANIEL A
Address
106 FOSTER RD
City
SOUTHWICK
State / Zip Code
MA 01077-9529
Country
United States

Analysis

On July 26, 1997, about 1710 eastern daylight time, a Bell 47G-3B-1, N35134, was substantially damaged as it impacted the ground during a forced landing at the Knox County Fairground, Mt. Vernon, Ohio. The certificated commercial pilot and two passengers were not injured. Four people on the ground received minor injuries when struck by flying debris. Visual meteorological conditions prevailed and no flight plan was filed for the sightseeing flight conducted under 14 CFR Part 91.

The pilot was taking passengers for 5 minute flights from the County Fairgrounds. The pilot stated that with two passengers onboard, he reached approximately 75 to 100 feet AGL, when the helicopter experienced "an unexplained loss of RPM." Unable to clear obstacles in his departure path, the pilot initiated a 180 degree right pedal turn back to his point of departure. The pilot stated that obstacles near the landing pad required him to stay high and "a tailwind caused the rotor RPM to further decay." Witnesses stated that the helicopter impacted the ground hard, and the main rotor blades severed the tail boom.

On July 28, 1997, a Federal Aviation Administration (FAA) Inspector examined the wreckage. He stated that the fuel sumps were drained and no signs of contamination was found, and the fuel tank vent passages were unobstructed. The helicopter company's chief pilot stated to the FAA Inspector that the helicopter lost rotor blade power shortly after lift off and out of ground effect, but the pilot did not report any engine malfunction. The Inspector monitored two engine operations, but without rotor engagement due to rotor blade damage sustained during the accident. According to the Inspector, the engine was started twice, and magneto functional checks were performed with a "normal" RPM drop observed each time.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# IAD97LA104