No fatalities

18 Aug 2011: GRUMMAN G-164A (N6567) — AERO AG SERVICES INC — El Campo, TX

El Campo, TX, United States

On 18 Aug 2011, a GRUMMAN G-164A (registration N6567) operated by AERO AG SERVICES INC was involved in an aviation accident near El Campo, TX. No fatalities were reported. Investigators recorded the probable cause as: A crack radiating from the exhaust valve rocker box on the number 3 cylinder where the rocker arm bolt attaches, leading to separation of the rocker box top and rocker arm failure. This summary draws on records from NTSB; 13 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

A Grumman G-164A agricultural aircraft, N6567, sustained substantial damage after nosing over during an emergency landing in a flooded rice field following an engine power loss. The pilot was uninjured.

Accident Overview

On August 18, 2011, at 0936 central daylight time, a Grumman G-164A (tail number N6567), operated by Aero Ag Services, Inc., impacted a rice field shortly after takeoff from a grass airstrip near El Campo, Texas. The commercial pilot was not injured. The aircraft sustained substantial damage to its top wing, vertical stabilizer, and rudder.

Flight Details

The flight was conducted under 14 Code of Federal Regulations Part 137 as an aerial application operation. Visual meteorological conditions prevailed, and no flight plan was filed. The local flight had departed from El Campo moments before the accident.

Pilot Report

According to the pilot-operator's accident report, after takeoff and while approximately 2 miles from the airstrip, the engine lost power. The pilot initiated an emergency procedure by dumping the fertilizer load and executed a straight-ahead landing in a flooded rice field. Upon touchdown, the aircraft nosed over.

Post-Accident Examination

A post-accident examination of the engine revealed a crack radiating from the exhaust valve rocker box on the number 3 cylinder at the attachment point of the rocker arm bolt. The top of the rocker box had separated, leading to failure of the rocker arm. Examination of the remaining systems found no preimpact failures or anomalies.

Probable cause

A crack radiating from the exhaust valve rocker box on the number 3 cylinder where the rocker arm bolt attaches, leading to separation of the rocker box top and rocker arm failure.

Contributing factors

Recip eng cyl section — Failure