No fatalities

12 Mar 2016: AMERICAN AA 1 — EGGETT GLADE D. — Brigham City, UT

Brigham City, UT, United States

On 12 Mar 2016, an AMERICAN AA 1 UNDESIGNAT operated by EGGETT GLADE D. was involved in an aviation accident near Brigham City, UT. No fatalities were reported. Investigators recorded the probable cause as: Loss of directional control during landing, due to nose landing gear damage sustained in the prior takeoff, resulting in a runway excursion and nose over. 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

During takeoff roll at about 60 knots, the pilot felt an abrupt right turn and heard a scraping sound. After a strong gust, the nose gear was found bent. On landing, the airplane veered into a ditch and nosed over, sustaining substantial damage.

Event Sequence

The pilot reported that during the takeoff roll at approximately 60 knots with a slight crosswind, he felt an abrupt turn to the right, heard a "huge steady scrape" sound, and noted a vibration. After becoming airborne at 65 knots, he experienced a strong gust of wind from the left, which felt like a quartering tailwind. He stated he did not believe the airplane touched back down on the runway after becoming airborne. Following the takeoff, the pilot flew the airplane over the airport, where a local pilot on the ground reported that the nose landing gear was bent.

Landing and Damage

During the subsequent landing, the pilot executed a soft field type of landing, with the main landing gear touching down first. He held the nose landing gear off the ground as long as possible, but when it made contact, he lost directional control and heard a scraping noise. The airplane departed the runway to the right, entered a ditch, and nosed over. The airplane sustained substantial damage to the fuselage, left wing, and vertical stabilizer.

Wind Conditions

The pilot took off on runway 17 at about 1410. The weather observation facility at the accident airport reported that from 1355 to 1415, the wind velocity varied from 13 knots to 15 knots with occasional gusts to 19 knots, and the wind direction varied from 190 to 240 degrees.

Aircraft Information

According to the Federal Aviation Administration (FAA) Type Certificate Data Sheet, the maximum demonstrated crosswind component for the airplane is 15 miles per hour (13.03 knots). The FAA has published the Airplane Flying Handbook FAA-H-8083-3A (2004), which discusses operations in crosswind conditions. The handbook states that takeoffs and landings in certain crosswind conditions are inadvisable or even dangerous, and that pilots should determine the maximum crosswind component of each airplane they fly and avoid operations exceeding the airplane's capability.

Contributing factors

Causes

PilotAttain/maintain not possible

Other contributing factors

Damaged/degraded