Probable cause
The fracture of the throttle cable in tensile overstress because of wear damage, which resulted in the partial loss of engine power.
NTSB analysis
While climbing out from a private airstrip, the airplane experienced a partial loss of power at 150 feet, and the pilot executed an emergency forced landing in a cotton field. The airplane touched down in the field and subsequently nosed over, coming to rest inverted. The throttle cable was found fractured between the engine and the firewall. Laboratory examination determined that the cable fractured in tensile overstress associated with wear damage. The wear damage is consistent with a sharp bend in the cable trajectory. It is likely that the push-pull operation of the throttle cable may have resulted in further damage to the cable.
Text from the NTSB. Open the NTSB docket for CEN11LA610 for the full record.
Event
- Date
- Aug 29, 2011
- Type
- Accident
- Place
- Monette, Arkansas
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Day
Grumman Acft Eng Cor-Schweizer G-164A
- N-number
- N48378
- Category
- Airplane
- Damage
- Substantial
- Operating rule
- Part 137 (agricultural)
- Purpose of flight
- Aerial application
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.