Probable cause
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.
NTSB 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, damaging the firewall. 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 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.
Text from the NTSB. Open the NTSB docket for CEN09CA253 for the full record.
Event
- Date
- May 8, 2009
- Type
- Accident
- Place
- Roanoke, Texas
- Nearest airport
- Northwest Regional (52F)
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Day
Cessna 172N
- N-number
- N172SV
- Category
- Airplane
- Damage
- Substantial
- Operating rule
- Part 91 (general aviation)
- Purpose of flight
- Personal
From the NTSB aviation accident database: N-registered aircraft, events since 2008, data through Oct 28, 2026. The file is published monthly, so the latest weeks are incomplete and recent records can change. The official source is the NTSB aviation investigation search. CheckAero is independent and not affiliated with the NTSB.