N630JL

Substantial
None

Beech 36S/N: E-821

Accident Details

Date
Thursday, July 16, 2020
NTSB Number
CEN20LA288
Location
Independence, MO
Event ID
20200716X94229
Coordinates
39.125278, -94.331947
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

Failure of the No. 5 piston head and ring, which resulted in a total loss of engine power and the pilot’s decision to takeoff with a known mechanical issue.

Aircraft Information

Registration
Make
BEECH
Serial Number
E-821
Engine Type
Reciprocating
Year Built
1976
Model / ICAO
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
6
FAA Model
A36

Registered Owner (Current)

Name
GILDAY AVIATION LLC
Address
2820 BOBMEYER RD HNGR C2
City
HAMILTON
State / Zip Code
OH 45015-1499
Country
United States

Analysis

On July 16, 2020, about 1720 central daylight time, a Beech 36 airplane, N630JL, was substantially damaged when it was involved in an accident near Independence, Missouri. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot recalled that on the previous flight, he was in cruise flight at 8,000 ft when he noted that the airplane began “moving back and forth.” He scanned the instruments and saw the cylinder head temperatures (CHT) for the Nos. 5 and 6 cylinders were “running in the red” along with oil temperature. The pilot diverted to the nearest airport. During the descent for landing, the engine temperatures returned to normal, and he landed uneventfully.

The pilot called the owner and discussed what had occurred. The owner suggested that if the pilot was comfortable, he should return to the home airfield. Since the engine temperatures returned to normal during the descent and landing, the pilot agreed to return if the taxi and engine run-up checked normal. The engine run-up was normal, and the pilot departed the airport without incident.

During the initial climb, about 4 miles from the airport, the No. 4 CHT increased significantly above the rest of the cylinders. The pilot continued the climb, and the airplane began moving back and forth again and began to respond “sluggishly.” The airplane shook and the pilot was unable to maintain altitude, so he set up for a forced landing to a road. During the approach to landing, the engine quit, and the pilot minimized his bank angle to stay out of a stall situation. When the airplane touched down, the pilot lost directional control and the airplane skidded off the road into a grassy area. The airplane sustained substantial damage to the wings and fuselage.

Examination of the engine found that the No. 5 cylinder head and piston ring had failed with signatures of denotation. Additionally, the turbocharger oil seal had failed. The pilot stated that he was not running lean of peak with fuel.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN20LA288