Summary
On June 30, 2011, a Leatherman Karl L ZODIAC CH 601 HDS (N67KL) was involved in an incident near Gray Court, SC. All 1 person aboard were uninjured. The aircraft sustained substantial damage.
The National Transportation Safety Board determined the probable cause of this incident to be: The total loss of engine power due to the failure of the radiator coolant supply fitting.
After climbing to about 1,500 feet and 30 minutes of uneventful flight, the pilot noticed an increase in engine coolant temperature. Shortly thereafter, water sprayed over the windscreen and the engine started to lose power. At that time, the pilot suspected a radiator water hose failed. He started a decent and landed the airplane in a field. During the rollout, the airplane struck several small pine trees and high vegetation resulting in substantial damage to the wings. During and examination of the airplane after the accident, an FAA inspector and the pilot discovered that the water hose fitting going into the radiator was fractured, and that the hose clamp and hose were still attached to the broken fitting. The reason for the failure of the fitting could not be determined.
This incident is documented in NTSB report ERA11CA373. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N67KL.
Accident Details
Probable Cause and Findings
The total loss of engine power due to the failure of the radiator coolant supply fitting.
Aircraft Information
Registered Owner (Historical)
Analysis
After climbing to about 1,500 feet and 30 minutes of uneventful flight, the pilot noticed an increase in engine coolant temperature. Shortly thereafter, water sprayed over the windscreen and the engine started to lose power. At that time, the pilot suspected a radiator water hose failed. He started a decent and landed the airplane in a field. During the rollout, the airplane struck several small pine trees and high vegetation resulting in substantial damage to the wings. During and examination of the airplane after the accident, an FAA inspector and the pilot discovered that the water hose fitting going into the radiator was fractured, and that the hose clamp and hose were still attached to the broken fitting. The reason for the failure of the fitting could not be determined.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA11CA373