Casualties unknown

1995-05-21: Grumman G-164A (N35RA) — Night Hawk Aerial Adv. Inc. — Zellwood, FL

Zellwood, FL, US

On May 21, 1995, a Grumman G-164A (registration N35RA) operated by Night Hawk Aerial Adv. Inc. was involved in an aviation accident near Zellwood, FL. Investigators recorded the probable cause as: A LOSS OF AIRCRAFT CLIMB CAPABILITY AFTER THE BANNER PICKUP FOR AN UNDETERMINED REASON. A FACTOR RELATED TO THE ACCIDENT WAS: SOFT TERRAIN IN THE EMERGENCY LANDING AREA. 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 1781061362Data APIEditorial standards

After picking up an advertising banner, the aircraft climbed to 300 feet but then lost airspeed and altitude. Despite increasing power and dropping the banner, the pilot could not maintain altitude and performed a forced landing in a soft field, causing the aircraft to nose over.

Incident Overview

A pilot engaged in aerial advertising operations reported that shortly after picking up a banner, the aircraft experienced difficulties maintaining flight. The incident occurred when the aircraft, which had been towing a banner, encountered performance issues after reaching an altitude of 300 feet.

Sequence of Events

According to the pilot's account, after successfully retrieving the advertising banner, the aircraft climbed to 300 feet above ground level. At that point, the aircraft ceased climbing and the airspeed began to decrease. In response, the pilot increased engine power, but this action did not halt the loss of airspeed; instead, the airspeed continued to drop and the aircraft started to descend. The pilot then lowered the aircraft's nose and released the banner in an attempt to regain performance. However, the aircraft still could not maintain altitude. Consequently, the pilot executed a forced landing in a soft field. During the landing, the aircraft nosed over.

Postcrash Examination

Following the incident, a detailed examination of the engine, its accessories, and the propeller was conducted. The inspection revealed no evidence of any mechanical failure or malfunction that occurred before the crash. All components were found to be within normal operating parameters, with no signs of pre-impact defects.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001207X03510. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.