Casualties unknown

2001-05-22: Beech 58 (N23AM) — Gaylord, MI

Gaylord, MI, US

On May 22, 2001, a Beech 58 (registration N23AM) was involved in an aviation accident near Gaylord, MI. Investigators recorded the probable cause as: the pilot not maintaining directional control during the reported loss of number one engine power during initial climb and the pilot not following the airplane emergency procedure's corrective action for engine failure after lift-off, and the inadvertent… This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

A Beech 58 was destroyed after an in-flight loss of control following a reported left engine power loss during initial climb. The pilot was uninjured; the passenger sustained minor injuries. Post-crash examination found no anomalies, and the left engine produced rated power when tested.

Accident Overview

A Beech 58 airplane was destroyed when it impacted terrain after an in-flight loss of control. The incident occurred during initial climb after takeoff, following a reported loss of engine power. The pilot stated that within seconds of rotation, he perceived an abrupt hard yaw to the left with near simultaneous rolling of the right wing up and activation of the stall warning horn. He reflexly applied hard right rudder and aileron and pushed the nose down, which partially reduced the yaw and roll. The airplane continued to rotate in a spin, with the left wing tip striking the ground and then spinning tail first into the ground. The entire sequence from perception of yaw to ground strike lasted a matter of one or two seconds.

Pilot and Passenger Injuries

The pilot was uninjured. The passenger sustained minor injuries.

Post-Accident Examination

FAA inspectors performed an on-scene examination of the wreckage. An inspector noted that the grass had not been mowed and was approximately 16 to 18 inches high. The landing gear collapsed during impact. The left and right wings were twisted and bent. The left and right engines broke free from their mounts. The aft fuselage section, including the empennage, completely separated from the forward section just aft of the aft-facing seats and came to rest on the top inboard section of the left wing and engine. The inspector stated that he was unable to determine any anomalies.

The left engine was subsequently test run and produced rated power.

Aircraft Manual Information

The Beech 58 manual's emergency procedures section stated: "Where practicable, the emergencies requiring immediate corrective action are treated in check list form for easy reference and familiarization. Other situations, in which more time is usually permitted to decide on and execute a plan of action, are discussed at some length. ... ENGINE FAILURE AFTER LIFT-OFF AND IN FLIGHT ... The most important aspect of engine failure is the necessity to maintain lateral and directional control. ... An immediate landing is advisable regardless of take-off weight."

Pilot Report

The pilot reported a "power loss [left] engine."

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20010524X01011. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.