N5519K

Substantial
Minor

Bellanca 8KCABS/N: 384-78

Accident Details

Date
Thursday, October 30, 2003
NTSB Number
MIA04LA015
Location
Ocala, FL
Event ID
20031105X01869
Coordinates
29.166666, -82.216667
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
1
Total Aboard
2

Probable Cause and Findings

The failure of the dual student to maintain airspeed (VS) and the CFI's improper supervision while turning to reverse direction resulting in an inadvertent stall/spin and collision with trees and the ground during the resultant uncontrolled descent.

Aircraft Information

Registration
N5519K
Make
BELLANCA
Serial Number
384-78
Engine Type
Reciprocating
Year Built
1978
Model / ICAO
8KCABBL8
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
ROCKY TOP AERO INC
Address
9451 SE 72ND AVE
Status
Deregistered
City
OCALA
State / Zip Code
FL 34472-9200
Country
United States

Analysis

On October 30, 2003, about 1120 eastern standard time, a Bellanca 8KCAB, N5519K, registered to and operated by Rocky Top Aero Inc., impacted a tree while on approach to the Leeward Air Ranch, Ocala, Florida. Visual meteorological conditions prevailed at the time and no flight plan was filed for the Title14 CFR Part 91 instructional flight. The commercial-rated pilot/certified flight instructor (CFI) reported minor injuries and the private-rated pilot/student reported no injuries, and the aircraft incurred substantial damage. The flight had originated about 20 minutes earlier from the same airport.

The CFI stated that he was instructing the student in a maneuver that called for a return to the departing runway after an engine failure. The CFI stated that he closed the throttle on the student as they crossed the departure end of runway 36, about 700 feet above the ground. The student started a left hand turn back to the runway at a bank angle of about 60 degrees, in order to make the runway. At some point during the turn the student applied an excessive rudder input, stalling and causing the aircraft to enter a spin. The CFI took the controls and recovered the airplane. During the recovery, the airplane struck an 8-inch diameter oak tree.

The FAA inspector who responded to the accident stated that there was insufficient distance for the airplane to clear the oak tree grove from the altitude at which the CFI recovered. The aircraft struck the tree in a climbing attitude causing the fuselage to break and bend the left landing gear. The airplane rotated counterclockwise as it fell tail first through the remaining trees before impacting the ground tail first, which it then fell over coming to rest on its back.

The pilot stated there were no mechanical failures or malfunctions to the airplane or any of its systems prior to the accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA04LA015