N5136C

Substantial
None

Beech B35 S/N: D-2421

Accident Details

Date
Saturday, June 29, 1996
NTSB Number
MIA96LA171
Location
KISSIMMEE, FL
Event ID
20001208X06073
Coordinates
28.300111, -81.409408
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

the pilot was operating the airplane at an indicated airspeed that exceeded the design speed for maximum gust intensity (VB), when clear air turbulence was encountered.

Aircraft Information

Registration
N5136C
Make
BEECH
Serial Number
D-2421
Engine Type
Reciprocating
Model / ICAO
B35 BE35
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
WESTFAIR INC
Address
8806 AIRPORT BLVD
Status
Deregistered
City
LEESBURG
State / Zip Code
FL 34788-4002
Country
United States

Analysis

On June 29, 1996, about 0930 eastern daylight time, a Beech B35, N5136C, registered to West Fair, Inc., encountered clear air turbulence while descending near Kissimmee, Florida. Visual meteorological conditions prevailed at the time and no flight plan was filed for the 14 CFR Part 91 personal flight. The airplane was substantially damaged and the commercial-rated pilot, the sole occupant, was not injured. The flight originated about 0830 from the Fort Lauderdale-Hollywood International Airport, Fort Lauderdale, Florida.

The pilot stated that while descending from 2,000 to 1,500 feet in an area of unstable air with the power set to 24 inches manifold pressure, and at an indicated airspeed of 170 miles per hour, the flight encountered "moderate to severe turbulence." He then felt a vibration through the airframe and immediately reduced power. The vibration only lasted "a couple of seconds" and he elected to continue and landed uneventfully at his planned destination. Post landing inspection of the airplane revealed that the rear bulkhead was cracked and both stabilators and both rudders/elevators were damaged. The flight manual for the airplane indicates that the beginning of the caution range is 164 miles-per-hour.

Both rudders/elevators with attach hardware were removed from the airplane and found to be within prescribed limits for static balance tests.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA96LA171