No fatalities

7 Jun 2012: GRUMMAN G164 B (N779EF) — J P Freppon Flying Service, LLC — Higginson, AR

Higginson, AR, United States

On 7 Jun 2012, a GRUMMAN G164 B (registration N779EF) operated by J P Freppon Flying Service, LLC was involved in an aviation accident near Higginson, AR. No fatalities were reported. Investigators recorded the probable cause as: The partial loss of engine power for reasons that could not be determined due to impact and fire damage. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On June 7, 2012, a Grumman G-164B agricultural airplane, N779EF, sustained substantial damage during a forced landing following a partial loss of engine power near Higginson, Arkansas. The pilot was not injured. The cause of the power loss was not determined.

Introduction

On June 7, 2012, a Grumman G-164B agricultural airplane, registration N779EF, experienced a partial loss of engine power shortly after takeoff, leading to a forced landing near Higginson, Arkansas. The aircraft, operated by J.P. Freppon Flying Service, LLC, of Bald Knob, Arkansas, was conducting an aerial application flight under 14 Code of Federal Regulations Part 137. The commercial pilot, the sole occupant, was not injured.

Accident Details

The flight originated from a local airstrip for an aerial application mission. At approximately 1315 central daylight time, while climbing through about 50 feet above ground level, the pilot noticed a partial loss of engine power accompanied by vibrations. He initiated a fertilizer dump and executed a forced landing to a field. The airplane came to rest upright in a wheat field, after which a postimpact fire consumed the aircraft. Visual flight rules (VFR) conditions prevailed, and no VFR flight plan was filed.

Post-Accident Examination

A Federal Aviation Administration inspector examined the airplane. A small crack was found in the number five cylinder of the Pratt & Whitney R-1340 engine. The engine was not disassembled for further examination; therefore, it could not be determined whether the crack resulted from impact or preexisted. The pilot speculated that a magneto might have failed, but due to fire damage, the magnetos and accessories could not be tested. The specific reason for the partial loss of engine power remained undetermined.

Conclusion

The investigation did not identify a definitive cause for the partial loss of engine power. The aircraft was substantially damaged by the crash and subsequent fire, with the pilot escaping uninjured.