N214GP

Substantial
None

Pietsch ITS/N: ZIA-0016

Accident Details

Date
Wednesday, March 14, 2007
NTSB Number
LAX07CA107
Location
Douglas, AZ
Event ID
20070403X00370
Coordinates
31.342777, -109.506385
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

a loss of directional control during landing due to separation of the rudder cable. A factor was the soft dirt terrain.

Aircraft Information

Registration
Make
PIETSCH
Serial Number
ZIA-0016
Engine Type
Reciprocating
Year Built
1994
Model / ICAO
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
IT

Registered Owner (Current)

Name
PIETSCH WARREN A
Address
2216 N BROADWAY
City
MINOT
State / Zip Code
ND 58703-1011
Country
United States

Analysis

On March 14, 2007, about 1207 mountain standard time, an experimental amateur-built Pietsch IT airplane, N214GP, experienced the disconnection of its right rudder cable control while the pilot was maneuvering near Douglas, Arizona. The airline transport certificated pilot had built the airplane. He operated it as a local flight under the provisions of 14 CFR Part 91, and it originated from Douglas about 1200. The pilot was not injured; the airplane sustained substantial damage during landing.

The pilot reported to the National Transportation Safety Board investigator that he was practicing for an air show. Following the disconnect, he proceeded to land on runway 21 at the Douglas Municipal Airport. When he was unable to maintain directional control during rollout, the airplane swerved off the south side of the runway whereupon it entered an adjacent soft dirt area, and nosed over. The airplane's canopy broke, and the top of the rudder bent, substantially damaging the airplane.

The pilot reported that an examination of his airplane revealed that the right rudder cable separated where two sections had been connected with a turnbuckle. The separation probably resulted from safety wire in the cable's turnbuckle chaffing against the rudder pedal until the wire broke. Thereafter, the turnbuckle unthreaded from the cable ends, and the cable separated. The safety wire's total time since installation was about 240 hours.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX07CA107