N22661

Substantial
None

TAYLORCRAFT BLS/N: 1308

Accident Details

Date
Saturday, March 5, 2016
NTSB Number
ERA16LA123
Location
St. Petersburg, FL
Event ID
20160307X95658
Coordinates
27.723888, -82.665000
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

A partial loss of engine power due to the fatigue fracture of the No. 3 cylinder head stud.

Aircraft Information

Registration
Make
TAYLORCRAFT
Serial Number
1308
Engine Type
Reciprocating
Year Built
1939
Model / ICAO
BLJT1
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
BL-65

Registered Owner (Current)

Name
LAKELAND AREO CLUB INC
Address
3952 JAMES C RAY DR
City
LAKELAND
State / Zip Code
FL 33811-1257
Country
United States

Analysis

On March 5, 2016, about 1345 eastern standard time, a Taylorcraft BL-65, N22661, was substantially damaged during a forced landing near St. Petersburg, Florida. The private pilot and a passenger were not injured. The local personal flight was conducted under the provisions of Title 14 Code of Federal Regulations Part 91.

The pilot reported that after flying for about 1 hour uneventfully, the airplane's engine began to run rough. Shortly thereafter, the engine experienced a 50% power reduction and the pilot subsequently performed a forced landing to a golf course. During the landing, the airplane struck trees and sustained substantial damage to the left wing, which partially separated from the fuselage.

The airplane was manufactured in 1939 and was equipped with a Lycoming O-145-B2, 65-horsepower engine.

Examination of the engine by a Federal Aviation Administration inspector revealed that two nuts were missing from the No. 3 cylinder head studs, three nuts were loose, and a third stud was fractured. The corresponding portion of the fractured stud was located on the cylinder cooling fins with the nut and self-looking washer still attached. The cylinder head and fractured stud were forwarded to the NTSB Materials Laboratory, Washington, DC, for further examination.

Metallurgical examination of the No. 3 cylinder head revealed that the insert that was installed in the hole that contained the fractured stud had been partially pulled out and protruded above the cylinder head face. The mostly flat fracture surface of the stud contained features and striations consistent with fatigue, with a shear lip on one side that displayed features consistent with overstress. A second stud was partially pulled out of the cylinder head. The remaining studs all appeared to still be seated inside their mating cylinder head holes.

Review of maintenance records revealed that airplane's most recent annual inspection was performed on May 15, 2015, about 42 hours before the accident. The engine had been operated for about 18 hours since its most recent inspection, which was performed on October 8, 2015, and included a check of all cylinder head bolts for "tightness."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA16LA123