No fatalities

21 Mar 2013: AVIAT A-1B — howard L. Patton — Dumas, TX

Dumas, TX, United States

On 21 Mar 2013, an AVIAT A-1B operated by howard L. Patton was involved in an aviation accident near Dumas, TX. No fatalities were reported. Investigators recorded the probable cause as: The pilot’s failure to maintain control of the airplane while taking off in gusty crosswind conditions. Contributing to the accident was the pilot’s decision to takeoff instead of waiting to ensure that the wind velocity had decreased. This summary draws on records from NTSB; 6 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

A pilot reported that during takeoff, a strong wind gust caused the airplane to become airborne prematurely, then settle back and veer off the runway, nosing over after contacting a drainage ditch, resulting in substantial damage.

Incident Summary

A pilot stated that after ending a flying lesson early due to increasing wind and turbulence, he waited 5 to 10 minutes for the wind to calm to 10–12 knots before attempting a takeoff in his own airplane. During the takeoff roll on runway 19, a strong gust of wind lifted the airplane off the ground prematurely, with the right wing raised 45 to 50 degrees. The pilot managed to level the wings before the airplane settled back onto the runway. The aircraft then traveled about 100 feet off the side of the runway, where it nosed over after contacting a drainage ditch, sustaining substantial damage to the left wing, vertical stabilizer, rudder, and fuselage.

Pilot Account

The pilot noted that the approach end of the runway was somewhat sheltered by buildings and hangars. He did not specify the aircraft type, registration, or his home airport. No occupants or injuries were mentioned.

Wind Conditions

Local wind reported 13 minutes before the accident was from 230 degrees at 13 knots, gusting to 20 knots. The wind reported 7 minutes after the accident was from 280 degrees at 23 knots, gusting to 28 knots. The pilot had waited for wind speeds to decrease to 10–12 knots before initiating the takeoff.

Damage

The accident resulted in substantial damage to the left wing, vertical stabilizer, rudder, and fuselage. No further details on damage extent were provided.

Contributing factors

Causes

Pilot

Other contributing factors

Effect on operationContributed to outcome