3 fatalities

Elevator Trim Cable Misrigging Leads to Accident During Post-Maintenance Flight (N587X)

Columbus-Rickenbacker (Lockbourne AFB), United States of AmericaTakeoff (climb)

On September 1, 2008, a Convair CV-580 (registration N587X) operated by Air Tahoma was involved in an aviation accident near Columbus-Rickenbacker (Lockbourne AFB), United States of America during takeoff. 3 people were killed. Investigators recorded the probable cause as: The improper (reverse) rigging of the elevator trim cables by company maintenance personnel, and their subsequent failure to discover the misrigging during required post-maintenance checks. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards
Aircraft registered N587X
Aircraft registered N587X. Photo: Michael Eaton-Aviation / CC BY-SA 4.0, via Wikimedia Commons

A post-maintenance flight ended in a cornfield impact after improperly rigged elevator trim cables caused reversed trim inputs. Maintenance inspection sign-offs were missing. The flight crew briefed on the maintenance did not properly respond to the trim problem.

Flight Details

The accident flight was the first flight after maintenance that included flight control cable rigging. The flight was intended to provide cockpit familiarization for the first officer and the pilot observer, and as a training flight for the first officer. About one minute after takeoff, the first officer contacted the tower and stated that they needed to return to land. The airplane impacted a cornfield about one mile southwest of the approach end of the runway, occurring 2 minutes 40 seconds after the initiation of the takeoff roll.

Cockpit Voice Recorder Evidence

Data from the cockpit voice recorder (CVR) indicated that, during the flight, neither the captain nor the first officer called for the landing gear to be raised, the flaps to be retracted, or the power levers to be reduced from full power. From the time the first officer called "rotate" until the impact, the captain repeated the word "pull" approximately 27 times. When the observer pilot asked, "Come back on the trim?" the captain responded, "There's nothing anymore on the trim."

Maintenance Findings

Inspection of the airplane revealed that the elevator trim cables were rigged improperly, resulting in the trim cables being reversed. As a consequence, when the pilot applied nose-up trim, the elevator trim system actually applied nose-down trim. An examination of the maintenance instruction cards used for the last inspection showed that the inspector's block on numerous checks was not signed off by the Required Inspection Item (RII) inspector. Specifically, the RII inspector did not sign the item that stated: "Connect elevator servo trim tab cables and rig in accordance with Allison Convair [maintenance manual]…" The item had been signed off by the mechanic, but not by the RII inspector. The card also contained a note in bold type stating: "A complete inspection of all elevator controls must be accomplished and signed off by an RII qualified inspector and a logbook entry made to this effect." The RII inspector block was not signed off.

Probable Cause

The official probable cause was stated as: The improper (reverse) rigging of the elevator trim cables by company maintenance personnel, and their subsequent failure to discover the misrigging during required post-maintenance checks. Contributing to the accident was the captain’s inadequate post-maintenance preflight check and the flight crew’s improper response to the trim problem. The flight crew had been briefed on the maintenance work performed on the airplane; therefore, when the captain’s nose-up trim inputs were affecting his ability to control the airplane, at a minimum, he should have stopped making additional inputs and returned the airplane to the configuration it was in before the problem worsened.