No fatalities

2007-01-10: Learjet 35 (N40AN) — AirNet Systems — Columbus-Rickenbacker (Lockbourne AFB), United States of America

Columbus-Rickenbacker (Lockbourne AFB), United States of AmericaLanding (descent or approach)

On January 10, 2007, a Learjet 35 (registration N40AN) operated by AirNet Systems was involved in an aviation accident near Columbus-Rickenbacker (Lockbourne AFB), United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: The pilot's failure to maintain aircraft control during an inflight maneuver which resulted in the design stress limits of the airplane being exceeded. A factor was the excessive airspeed encountered during recovery. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781198354Data APIEditorial standards

A cargo flight captain's intentional aileron roll maneuver during cruise resulted in loss of control, overspeed, and excessive G-loads, causing substantial damage to the left wing and elevator assembly.

Summary

A cargo flight operating under 14 CFR Part 135 experienced substantial damage after the captain intentionally performed an aileron roll maneuver during cruise flight at night. The maneuver led to a loss of control, with the aircraft entering a nose-down unusual attitude and high-speed dive. Recovery efforts resulted in overspeed and excessive G-loads, exceeding the aircraft's design stress limits.

Accident Details

According to the captain, the airplane was functioning normally before the intentional aileron roll. During the maneuver, the roll got out of control while descending through flight level 200. The copilot reported that the captain's roll maneuver caused a nose-down unusual attitude and a high-speed dive. During the subsequent recovery, the aircraft experienced overspeed and excessive G-loads.

Investigation Findings

The official investigation determined that the probable cause was the pilot's failure to maintain aircraft control during an inflight maneuver, which resulted in the design stress limits of the airplane being exceeded. A contributing factor was the excessive airspeed encountered during recovery.

Damage

Inspection of the aircraft revealed substantial damage to the left wing and elevator assembly.