N1567Q

Substantial
None

CESSNA 150S/N: 15072867

Accident Details

Date
Wednesday, June 29, 2016
NTSB Number
ERA16LA235
Location
Peachtree City, GA
Event ID
20160630X31108
Coordinates
33.373611, -84.584724
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The fatigue failure of the No. 3 cylinder exhaust valve, which resulted in a total loss of engine power at low altitude after takeoff.

Aircraft Information

Registration
N1567Q
Make
CESSNA
Serial Number
15072867
Engine Type
Reciprocating
Year Built
1971
Model / ICAO
150C150
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
JEFFORD JACK D
Address
106 SAGAMORE LN
Status
Deregistered
City
PEACHTREE CITY
State / Zip Code
GA 30269-3258
Country
United States

Analysis

On June 29, 2016, at 1930 eastern daylight time, a Cessna 150L, N1567Q, experienced a total loss of engine power and was substantially damaged during a forced landing after takeoff from Atlanta Regional Airport (FFC), Peachtree City, Georgia. The student pilot was not injured. Visual meteorological conditions prevailed, and a visual flight rules flight plan was filed for the solo instructional flight, which was conducted under the provisions of 14 Code of Federal Regulations Part 91.In a telephone interview, the pilot stated that she performed the preflight inspection, engine start, run-up, and takeoff from runway 31 with no anomalies noted. At 400 ft above ground level, the engine "sputtered, and then stopped." The pilot selected a golf course for the forced landing, and touched down on a slightly rolling fairway lined with trees. During the rollout, the airplane clipped trees and struck a small berm, which collapsed the nose landing gear.

Examination of the airplane by a Federal Aviation Administration (FAA) inspector revealed substantial damage to the engine firewall. The engine was rotated by hand at the propeller. The magnetos produced spark at all eight spark plugs. A compression check was performed, and thumb compression was confirmed on all but the No. 3 cylinder.

The No. 3 cylinder was removed, and severe impact damage was noted on the dome of the piston and the cylinder head. The exhaust valve was separated at the stem, and the intake valve was fractured, with about 50 percent of the valve head separated. Pieces of the valve were recovered in the exhaust manifold. Both valves and their associated fragments were forwarded to the NTSB Materials Laboratory in Washington, DC for examination.

Fracture analysis of the No. 3 cylinder exhaust valve revealed fatigue failure of the valve stem transition area at the valve head. The remaining fracture surfaces observed on the valves were due to overstress.

The pilot held an FAA student pilot and third-class medical certificate, issued on December 22, 2015. She reported 41 total hours of flight experience, of which 38 were in the accident airplane.

The two-seat, single-engine, high-wing airplane was manufactured in 1971 and was equipped with a Continental O-200 series engine. The airplane had been operated for about 410 hours since its most recent annual inspection was completed on July 5, 2015, at 3,488 total airframe hours.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA16LA235