N623LA

MINR
None

AIR TRACTOR INC AT 402AS/N: 402A-1127

Accident Details

Date
Saturday, April 4, 2015
NTSB Number
CEN15IA200
Location
Brickeys, AR
Event ID
20150420X91520
Coordinates
34.841110, -90.527221
Aircraft Damage
MINR
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The in-flight separation of the attachment hardware at the elevator control pushrod due to maintenance personnel's improper reinstallation of the attachment hardware.

Aircraft Information

Registration
Make
AIR TRACTOR INC
Serial Number
402A-1127
Engine Type
Turbo-prop
Year Built
2000
Model / ICAO
AT 402AF402
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
AT-402A

Registered Owner (Current)

Name
NEAL AIRCRAFT INC
Address
12106 FM 400
City
SLATON
State / Zip Code
TX 79364-7564
Country
United States

Analysis

On April 4, 2015, about 1430 central daylight time, an Air Tractor AT-402A, N623LA, sustained minor damage during a forced landing to a field near Brickeys, Arkansas. The commercial pilot was not injured. The aerial application flight, owned and operated by Taylor Air Service, LLC., was being conducted under the provisions of 14 Code of Federal Regulations Part 137 without a flight plan. Visual meteorological conditions prevailed at the time of the incident. The local flight departed Dawson's Airport (15AR), Brickeys, Arkansas, about 1230.

The pilot reported that during an aerial application pass the elevator control felt abnormal. As he completed the pass he pulled up and detected that the elevator was not responding. The pilot elected to return to the airport and the elevator control continued to be unresponsive. The pilot attempted to maintain pitch control through the use of the elevator trim but turbulence and power changes made this difficult. During an off field landing, the airplane nose pitched down. The pilot countered with nose up trim and the airplane stalled. There was minor damage to the propeller during the impact with the ground.

A post incident examination established that the attachment hardware, including the bolt and nut, was missing from the forward end of the #2 elevator control pushrod. The bolt was located in the airplane in the lower fuselage; however, the nut was not located. About 20 hours prior to the incident flight, maintenance had been performed on the forward rod end bearing on the #2 pushrod. The bolt and nut would have been removed and reinstalled during this maintenance. It is not known if original hardware was used or if the hardware was replaced during this maintenance.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN15IA200