N911LF

Destroyed
Fatal

Bölkow BO-105S S/N: S-740

Accident Details

Date
Friday, November 4, 1994
NTSB Number
MIA95FA018
Location
PERRY, FL
Event ID
20001206X02622
Coordinates
30.170600, -83.609802
Aircraft Damage
Destroyed
Highest Injury
Fatal
Fatalities
2
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
3

Probable Cause and Findings

FAILURE OF THE PILOT TO MAINTAIN SUFFICIENT CLEARANCE FROM THE POWER LINE, WHILE BUZZING (AT LOW ALTITUDE).

Aircraft Information

Registration
N911LF
Make
BÖLKOW
Serial Number
S-740
Engine Type
Reciprocating
Model / ICAO
BO-105S SA05
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
DEUTSCHE CREDIT CORPORATION
Address
2333 WAUKEGAN RD
Status
Deregistered
City
DEERFIELD
State / Zip Code
IL 60015
Country
United States

Analysis

HISTORY OF FLIGHT

On November 4, 1994, about 1107 eastern standard time, N911LF, a Bolkow BO-105S, operated by Omniflight, crashed in Perry, Florida, while on a 14 CFR Part 91 positioning flight. Visual meteorological conditions prevailed at the time and a company VFR flight plan was filed. The helicopter was destroyed and the pilot and one passenger received fatal injuries, and one passenger received serious injuries. The flight originated from a hospital heliport in Tallahassee, Florida, about 1036 the same day.

The survivor and several deer hunters in the area stated the helicopter was flying at a low level, with high speed, when it struck a 69 kilovolt power line, broke the line, flipped and crashed. There was an extensive postcrash fire. The surviving passenger stated that the purpose of the flight was to position the helicopter to another hospital to pick-up a patient. He stated that while in cruise flight the pilot descended rapidly and began to fly at treetop level. The pilot had stated to the other passenger "Now it's time to break Trent in with a real ride". Shortly thereafter, the helicopter dispatcher radioed the helicopter for a position report and the pilot climbed to about 900 feet and radioed the dispatcher with a position report. The pilot then dove the helicopter down to a low altitude and the survivor saw wires in front of the helicopter, and the helicopter struck the wires, then the helicopter lost control, and crashed.

PERSONNEL INFORMATION

Pilot information is located attached to and in this report.

AIRCRAFT INFORMATION

Aircraft records and information is located in, and attached to this report.

METEOROLOGICAL INFORMATION

The closest weather reporting station to the accident site was Tallahassee, Florida. The recorded observation at 1050 EST was sky, 15000 feet scattered clouds, visibility 7 miles, temperature 76 degrees F, dewpoint 62 degrees F, winds from 270 degrees magnetic at 7 knots, altimeter 30.22 in. Hg.

WRECKAGE AND IMPACT INFORMATION The wreckage debris was located along a logging road in Perry, Florida, aligned on a heading of about 120 degrees magnetic. The first evidence of impact was the fallen 69KV power lines on the south side of the road. From the power lines to the main wreckage was a distance of about 360 feet. The main wreckage was mainly burned away. Three of the main rotor blades were located and one main rotor blade was not located. The tailboom was located and both tail rotor blades exhibited cutting failures at about 50 percent of blade span. The failed power line had black paint transfer marks and the left forward skid cross tube had black paint scraped off of it and the right door step also had black paint scraped off. All flight control tubes were failed and exhibited signatures consistent with overload or burning. All rod ends for the control tubes were in place with the associated bolts, nuts, and cotter keys in place. The engines were removed and shipped for examination. Examination of the engines revealed compressor damage consistent with high speed rotation at impact, and the power turbine nozzles exhibited metalization transfer.

MEDICAL AND PATHOLOGICAL INFORMATION

A postmortem examination of the pilot was conducted by Dr. Jerry L. Harris of the District Two Medical Examiner's office Dr. Harris reported the cause of death to be massive trauma. Toxicological testing of the pilot was conducted by the Civil Aeromedical Institute, Oklahoma City, Oklahoma, and was negative for alcohol, carbon monoxide, marijuana, and basic and acetic drugs.

ADDITIONAL DATA

The wreckage and engines were released to Mr. Barrett, representing the insurance carrier on November 7, 1994, and on January 10, 1995.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA95FA018