Casualties unknown

Aerial Application Aircraft Settles Shortly After Takeoff (N2833J)

Fairfield, NE, US

On July 29, 1987, a Cessna 188B (registration N2833J) was involved in an aviation accident near Fairfield, NE. Investigators recorded the probable cause as: The pilot's failure to ensure the aircraft was within weight and balance limits for the prevailing density altitude conditions, which resulted in an inability to climb after takeoff. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards

An aircraft conducting an aerial application flight began to settle shortly after takeoff, resulting in the left wing striking the ground. The pilot noted that dumping part of the load might have allowed continued flight.

What happened

The incident occurred during an aerial application flight, a phase of operation typically involving the dispensing of agricultural chemicals or similar materials. Shortly after takeoff, the aircraft began to settle rather than climb as expected. As the descent continued, the left wing made contact with the ground. The impact caused the aircraft to turn approximately 180 degrees before coming to rest.

Environmental conditions at the time of the event were noted as being quite warm, with a temperature of 95 degrees Fahrenheit. The density altitude was recorded at 4,000 feet, a factor that can significantly impact aircraft performance by reducing engine power and lift generation capabilities.

The investigation

Following the accident, investigators reviewed the operational context and the pilot's account. The primary focus was on understanding why the aircraft failed to maintain altitude during the critical initial climb phase. No mechanical failures were immediately cited in the narrative provided, pointing instead toward performance limitations or weight issues.

Findings

The pilot provided a statement indicating that the aircraft was likely too heavy for the prevailing conditions. He remarked that he "could have dumped some of the load so the aircraft could have flown out." This suggests that fuel exhaustion or more accurately, excessive weight, was a primary concern. The combination of high temperature and density altitude reduced the aircraft's ability to climb with its current payload.

The pilot survived the incident, though specific injury details were not provided in the source text. The event highlights the critical importance of weight and balance calculations, especially during aerial application operations where fuel burn changes the aircraft's center of gravity and total weight rapidly.

Probable cause

The pilot's failure to ensure the aircraft was within weight and balance limits for the prevailing density altitude conditions, which resulted in an inability to climb after takeoff.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001213X31616. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.