N6099E

Substantial
None

Beech K35 S/N: D5986

Accident Details

Date
Wednesday, August 16, 2000
NTSB Number
CHI00LA258
Location
HOLLAND, MI
Event ID
20001212X21680
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

the misjudged glidepath by the pilot. Factors to the accident were the loose throttle cable due to improper installation by maintenance personnel, and the intentional engine shutdown during the precautionary landing by the pilot.

Aircraft Information

Registration
N6099E
Make
BEECH
Serial Number
D5986
Engine Type
Reciprocating
Year Built
1959
Model / ICAO
K35 BE35
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
MICHALKA RALPH
Address
6319 MARLOW ST
Status
Deregistered
City
PORTAGE
State / Zip Code
MI 49024-2615
Country
United States

Analysis

On August 15, 2000, at 2315 eastern daylight time, a Beech K35, N6099E, piloted by a private pilot, was substantially damaged during a precautionary landing on runway 26 (5,000 feet by 100 feet dry asphalt) at the Tulip City Airport (BIV), Holland, Michigan. The personal 14 CFR Part 91 flight was not on a flight plan. Visual meteorological conditions prevailed at the time of the accident. The pilot, who was the sole occupant, reported no injuries. The local flight departed BIV at 2245.

The pilot reported that, while in flight, he found that the throttle control would only operate between 3/4 throttle and full throttle. The pilot elected to land the aircraft. When he believed that he was at a point where a safe landing could be made on the runway, the pilot shut off the engine and attempted to glide the aircraft to landing. The aircraft came to rest about 100 yards short of the runway.

At a postaccident examination of the aircraft, a Federal Aviation Administration Inspector found that the bolt that attaches the clamp for the throttle cable housing in the engine compartment was loose. The inspector found that the position of the throttle cable housing limited the movement of the throttle and that the housing could be moved within the clamp. The inspector also determined that the aircraft engine had been overhauled and reinstalled in the aircraft at the last annual inspection. A logbook entry indicated that the annual inspection was completed on April 15, 2000.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI00LA258