No fatalities

Practice Aerial Application Flight Ends with Substantial Damage after Engine Power Loss

What Cheer, IA, United States

On July 25, 2016, a CESSNA 188 A was involved in an aviation accident near What Cheer, IA. No fatalities were reported. Investigators recorded the probable cause as: The loss of engine power for undetermined reasons due to the pilot not making the airplane or engine available for examination, which resulted in a forced landing and an impact with terrain. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 2026-08-03Data APIEditorial standards

A pilot performing practice aerial application operations at 30 feet experienced a gradual engine power loss, landed in a bean field, and sustained substantial damage to the right wing and left elevator. Postaccident examination found no anomalies in fuel or carburetor, but weather conditions suggested a risk of carburetor icing.

Incident Overview

A pilot reported that while conducting "practice" aerial application operations at an altitude of approximately 30 feet above ground, the engine gradually lost power. The pilot executed a left turn and subsequently landed in a bean field. The landing resulted in substantial damage to the right wing and left elevator.

Pilot Reports

In postaccident interviews, the pilot stated that just before the power loss, the aircraft was in wings-level flight with the mixture set to full rich and power at a cruise setting. The carburetor heat was off for the entire flight. The pilot described the power loss as gradual, with no visible oil spray on the windscreen. Following the accident, the pilot checked the oil level and found no anomalies.

Examination Findings

An airframe and powerplant mechanic conducted a postaccident examination. They drained 13 gallons of fuel from the single fuel tank. The float carburetor and gascolator were inspected and found to be unremarkable. The propeller could be rotated normally.

Weather and Carburetor Icing Considerations

An automated weather observing system located 13 nautical miles northeast of the accident site, near the time of the incident, reported a temperature of 81°F (27°C) and a dew point of 66°F (19°C). According to a carburetor-icing-probability chart, the engine was at risk of "moderate icing" at cruise power. The Federal Aviation Administration Pilot's Handbook of Aeronautical Knowledge (PHAK) notes that carburetor ice can form when temperatures are below 70°F (21°C) and relative humidity above 80%, but also at higher temperatures due to evaporative cooling. The PHAK states that ice buildup can cause engine cessation. The airplane manufacturer's owner manual advises selecting the minimum amount of carburetor heat to keep ice cleared when conditions are conducive to carburetor icing.

Probable Cause

The investigation suggested that the loss of engine power was likely due to carburetor ice, but the pilot, who was also the airplane owner, did not make the airframe or engine available for examination by the National Transportation Safety Board.

Contributing factors

Contributed to outcomeConducive to carburetor icingNot used/operated