Hood JUNIOR ACE N1012S

Summary

On 30 September 2008 at about 22:37 local time, a Hood JUNIOR ACE registered N1012S was involved in an accident near Ashville, Alabama, United States. One person was on board and nobody was injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

Date

30 September 2008 at 22:37

Classification

Accident

Location

Ashville, Alabama, United States

Nearest airport

Town and Country Airpark (3AL6)

Coordinates

33.7872, -86.3081

Aircraft

Hood JUNIOR ACE

Registration

N1012S

Category

Airplane

Engines

1

Operator

Not recorded

Operating rule

Part 91: General Aviation

Purpose of flight

Personal

Phase of flight

Not recorded

Route

Branchville → Brranchville

Aircraft damage

Substantial

Weather

VMC

Light

Day

NTSB number

NYC08CA328

Nobody was injured.

The pilot's improper flare while landing. Contributing to the accident was the airplane's lack of yaw control as reported by the pilot.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The pilot of the amateur-built Junior Ace stated that the purpose of the personal flight was to fly in the local area for about 1 hour. The airplane was equipped with one centrally-mounted control stick, a two-place bench seat, and two sets of rudder pedals. About 20 minutes into the flight, the pilot turned the airplane to the left. When he attempted to turn to the right, the airplane yawed "uncontrollably" to the left. The pilot said he applied more right rudder in an attempt to control the left yaw, but the yaw increased. The pilot reported that he could not stop the yawing motion. He stated that, "it felt like the airplane was stalling and about to spin." A witness stated that the airplane’s wings rocked back and forth in a smooth, slow rocking motion. The pilot attempted to land in a field, and "flared high" above the ground. The airplane impacted the ground, and nosed over. The right main landing gear, right wing rear strut, and firewall were damaged. The pilot reported that there were no mechanical malfunctions of the airplane prior to the flight. He also stated that for this flight, he sat in the center of the bench seat, straddled the control stick, and was utilizing the "outboard rudder pedals." Examination of the wreckage by a Federal Aviation Administration inspector revealed all flight controls moved free, correct and had full travel.

Quoted verbatim from the NTSB record.