Engine failure and loss of control during approach at Mobile Downtown

1 fatality • Mobile, United States of America • Landing (descent or approach)

An aircraft experienced an engine runaway and subsequent loss of power lever control during its approach to runway 18, resulting in a collision with a utility pole.

What happened

During the final approach to runway 18 at Mobile Downtown, the pilot notified air traffic control of an ongoing mechanical issue. While the ground controller confirmed visual contact and provided clearance to land, the pilot reported a runaway engine and indicated the necessity of shutting down the engine to manage the situation. As the flight continued its approach, the pilot expressed concern regarding the ability to reach the runway.

Shortly before reaching the threshold, the aircraft type struck a utility pole and impacted the ground, which subsequently triggered a post-impact fire. There were no specific casualty counts provided in the report, but the impact occurred short of the intended runway.

Findings

An inspection of the engine following the accident identified a mechanical failure within the fuel control unit. Specifically, the arm connecting to the fuel control unit interconnect rod end had separated from the rod end swivel ball assembly. The investigation revealed that the assembly had been improperly installed; the bolt head was positioned on the inboard side of the arm, while the washer and nut were located on the outboard side. This configuration caused the rod separation, leading to a loss of power lever control.

Although emergency procedures for a loss of power lever control were established—including specific airspeed, flap, and engine lever settings—the pilot did not follow the published instructions. Consequently, the aircraft was unable to complete the landing on the designated runway.

Probable cause

The separation of the fuel control unit interconnect rod due to improper assembly led to a loss of power lever control, and the failure to follow established emergency procedures prevented the aircraft from reaching the runway.

All Daher TBM 700 accidents →

Frequently asked questions

What happened in the 2003-04-24 Socata TBM-700 accident near Mobile, United States of America?

An aircraft experienced an engine runaway and subsequent loss of power lever control during its approach to runway 18, resulting in a collision with a utility pole.

Were there any fatalities in the 2003-04-24 Socata TBM-700 accident?

The accident was fatal, resulting in 1 fatality.

What aircraft was involved and where did it happen?

The accident on 2003-04-24 involved a Socata TBM-700, registration N705QD, operated by Quest Diagnostics, at Mobile, United States of America.

What was the probable cause of the accident?

The separation of the fuel control unit interconnect rod due to improper assembly led to a loss of power lever control, and the failure to follow established emergency procedures prevented the aircraft from reaching the runway.

Loading the flight search…