Casualties unknown

1996-05-24: Beech A36 (N59WW) — Meriden, CT

Meriden, CT, US

On May 24, 1996, a Beech A36 (registration N59WW) was involved in an aviation accident near Meriden, CT. Investigators recorded the probable cause as: the pilot's improper planning/decision, his failure to use takeoff power, and his premature lift-off of the airplane, which resulted in an inadvertent stall/mush and subsequent collision with terrain. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

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

A pilot initiated a downwind takeoff on runway 18 with two passengers. The airplane climbed about 40 feet then stopped climbing and accelerating. After aborting the climb, the airplane veered off the runway and a fire erupted. The aircraft was estimated 76 pounds over maximum takeoff weight and 2 inches beyond forward CG limit.

Accident Details

The pilot initiated a downwind takeoff on runway 18 with two passengers aboard. According to the pilot, after a ground run of 600 feet, he rotated the airplane for takeoff. The airplane climbed to about 40 feet above the runway, then stopped climbing and stopped accelerating.

Witnesses reported that the airplane entered a steep nose-high attitude during takeoff. After climbing briefly, the wings rocked (or wobbled) to the left and right. The pilot then lowered the nose briefly and stated that he increased engine power '2 ticks into the yellow (arc).' He aborted the climb and attempted to land.

After ground contact, the airplane veered off the runway. After stopping, a fire erupted, which resulted in further damage.

Aircraft Modifications and Weight/CG

The airplane's reciprocating engine had been replaced with an Allison 250-B17C turbine engine per Supplemental Type Certificate (STC) SA3523NM, by Tradewind Turbines, Amarillo, TX.

The Pilot's Operating Handbook indicated that a ground roll of 1,800 feet would have been required for the takeoff conditions. The airplane was estimated to be 76 pounds over its maximum takeoff weight and about 2 inches beyond the forward center of gravity (CG) limit (as listed in the STC). Additionally, the pilot did not use maximum power for takeoff as described in the STC.

Environmental Conditions

The wind was estimated to be from 350 degrees at 15 knots.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001208X05843. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.