N7969C

Destroyed
None

North American SNJS/N: 43974

Accident Details

Date
Tuesday, October 23, 2018
NTSB Number
WPR19LA014
Location
Agoura Hills, CA
Event ID
20181023X82752
Coordinates
34.138053, -118.724441
Aircraft Damage
Destroyed
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The failure of the No. 5 piston rod end due to fatigue, which resulted in a total loss of engine power.

Aircraft Information

Registration
Make
NORTH AMERICAN
Serial Number
43974
Engine Type
Reciprocating
Model / ICAO
SNJT2
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
SNJ-5

Registered Owner (Current)

Name
CONDOR SQUADRON OFFICERS & AIRMENS ASSOC INC
Address
7800 HAYVENHURST AVE
City
VAN NUYS
State / Zip Code
CA 91406-1734
Country
United States

Analysis

On October 23, 2018, about 1344 Pacific daylight time, a North American SNJ-5 airplane, N7969C, was destroyed when it was involved in an accident near Agoura Hills, California. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 personal flight.

The pilot reported that, shortly after departure, he heard two loud bangs, followed by total loss of engine power, and he performed a forced landing to a highway. After touchdown, the airplane swerved to the left, the left wing impacted a concrete divider, and a postimpact fire ensued.

The airplane was equipped with an R-1340-AN1 nine-cylinder, radial engine. Examination of the engine showed that the No. 2 cylinder was cracked between the 10th and 11th (from bottom of head) cylinder head cooling fin. Another crack on the No. 2 cylinder extended from the sparkplug to the base of the head. Additional damage was noted at the base between the Nos. 4 and 5 cylinders, and on the No. 1 cylinder. Disassembly showed that the No. 5 master cylinder rod end had failed on the piston side. Examination of the master rod end by the NTSB Materials Laboratory showed a fracture initiation region on the I-beam shaft, based on fine chevron and river pattern markings. The fracture surface in the immediate origin region was damaged due to mechanical contact during the failure sequence. A higher magnification image of the fracture surface adjacent to the origin region exhibited striation features typical of fatigue crack growth in hardened steel.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR19LA014