N163BH

Substantial
None

BELL 206B S/N: 3027

Accident Details

Date
Tuesday, December 20, 1994
NTSB Number
MIA95LA044
Location
MIAMI, FL
Event ID
20001206X02773
Coordinates
25.650592, -80.409027
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

INADEQUATE SUPERVISION BY THE PILOT-IN-COMMAND (CFI) FOR FAILURE TO NOTE REDUCTION IN CLEARANCE BETWEEN THE TAIL ROTOR AND AN EMBANKMENT.

Aircraft Information

Registration
N163BH
Make
BELL
Serial Number
3027
Engine Type
Turbo-shaft
Year Built
1980
Model / ICAO
206B B06
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
BISCAYNE HELICOPTERS INC
Address
13955 SW 127TH ST BLDG 121
Status
Deregistered
City
MIAMI
State / Zip Code
FL 33186-5324
Country
United States

Analysis

On December 20, 1994, about 1515 eastern standard time, a fixed float-equipped Bell 206B, N163BH, registered to and operated by Biscayne Helicopters, collided with an embankment of a quarry about 4 nautical miles northwest of the Kendall-Tamiami Executive Airport, Miami, Florida, while on a 14 CFR Part 91 instructional flight. Visual meteorological conditions prevailed at the time and no flight plan was filed for the local flight. The helicopter was substantially damaged and the certified flight instructor (CFI), helicopter-rated student, and passenger were not injured. The flight originated about 1500 from the Kendall-Tamiami Executive Airport, Miami, Florida.

Before the flight the student advised the CFI that he did not have any experience operating a helicopter equipped with floats. The flight departed and proceeded direct to the quarry. The student stated that after landing on the water near the south side of the quarry, he performed water maneuvers as directed by the CFI. While facing north, the passenger observed that the helicopter was drifting south and announced this over the intercom. The student lifted to hover during which the tail rotor contacted the embankment and directional control was lost. The CFI stated that he took over the controls, maneuvered the helicopter away from the embankment and performed a hovering autorotation to the water. Postaccident examination of the helicopter revealed tail rotor blade and tail boom damage.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA95LA044