Summary
On May 08, 2009, a Cessna 172N (N172SV) was involved in an incident near Roanoke, TX. 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 partial loss of engine power due to a failure of the throttle control rod-end to carburetor arm hardware. A contributing factor was the pilot's decision to fly the airplane without a current annual inspection.
During initial climb, the airplane's single engine experienced a partial loss of power. Unable to maintain altitude the pilot performed an emergency landing to a field. During the landing rollout, the airplane impacted a rock and the nose landing gear collapsed. The airplane came to rest in a nose down position and the pilot was able to exit unassisted. Following the accident, an examination of the airplane revealed that the firewall had sustained structural damage, and the throttle control rod-end to carburetor throttle arm hardware was missing. In addition, the airplane had not been inspected in accordance with an annual inspection during the previous year.
This incident is documented in NTSB report CEN09CA253. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N172SV.
Accident Details
Probable Cause and Findings
The partial loss of engine power due to a failure of the throttle control rod-end to carburetor arm hardware. A contributing factor was the pilot's decision to fly the airplane without a current annual inspection.
Aircraft Information
Registered Owner (Historical)
Analysis
During initial climb, the airplane's single engine experienced a partial loss of power. Unable to maintain altitude the pilot performed an emergency landing to a field. During the landing rollout, the airplane impacted a rock and the nose landing gear collapsed. The airplane came to rest in a nose down position and the pilot was able to exit unassisted. Following the accident, an examination of the airplane revealed that the firewall had sustained structural damage, and the throttle control rod-end to carburetor throttle arm hardware was missing. In addition, the airplane had not been inspected in accordance with an annual inspection during the previous year.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN09CA253