1 fatality

2014-11-18: Rockwell Aero Commander 500 (N30MB) — Central Air Southwest — Chicago-Midway, United States of America

Chicago-Midway, United States of AmericaLanding (descent or approach)

On November 18, 2014, a Rockwell Aero Commander 500 (registration N30MB) operated by Central Air Southwest was involved in an aviation accident near Chicago-Midway, United States of America during landing or approach. One person was killed. Investigators recorded the probable cause as: The pilot's inability to preserve adequate airspeed while maneuvering back toward the airport after reporting engine difficulties caused an aerodynamic stall/spin. 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 1781193300Data APIEditorial standards

A cargo charter flight ended in an accident near the runway threshold after the pilot attempted to return for landing following reports of left engine issues.

What happened

During a scheduled cargo charter operation, the pilot encountered difficulties with the left engine shortly after departing the airport. The pilot notified air traffic control of the situation, expressing an intention to return to the airfield for an emergency landing. To facilitate this, the pilot initiated a left-hand traffic pattern.

Following the initial departure, GPS tracking indicated that the aircraft type (not specified in source) performed a left turn toward a southeasterly direction, reaching a peak altitude of approximately 959 feet. The flight path then transitioned into a subsequent left turn that continued until the aircraft's descent ended near the accident site, located roughly 0.50 miles southeast of the runway's displaced threshold.

Findings

Analysis of GPS data and environmental wind conditions indicated that the airspeed during the turning maneuver had dropped to approximately 45 knots. This speed was significantly lower than the 59-knot stall speed required for level flight with flaps extended, as specified in the airplane's flight manual. While the pilot had reported issues with the left engine, post-accident inspections of the airframe and engines found no mechanical failures that would have prevented standard operation, leaving the exact nature of the engine trouble unconfirmed.

Ultimately, the investigation concluded that the pilot failed to maintain sufficient airspeed during the turn, leading to an aerodynamic stall and subsequent spin.

Probable cause

The pilot's inability to preserve adequate airspeed while maneuvering back toward the airport after reporting engine difficulties caused an aerodynamic stall/spin.