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Aviation safety reports, made easier to study

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NTSB Report

March 14, 2007 · Pietsch IT · N214GP

Douglas, AZ

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
March 14, 2007
Injury Outcomes
No injuries (1 uninjured)
Location
Douglas, AZ
Aircraft
Pietsch IT
Tail Number
N214GP
Injuries
None
Aircraft Damage
Substantial
NTSB Number
LAX07CA107

During landing rollout, the pilot's experimental amateur-built airplane swerved off the runway and nosed over in soft dirt. The pilot-builder had been practicing maneuvers for an air show when the right rudder control cable became disconnected. Safety wire, which secured a turnbuckle connecting two ends of the rudder cable, had chafed against a rudder pedal until the wire broke. Thereafter, the turn buckle unthreaded from the cable ends and the cables separated. The pilot's ability to maintain directional control during landing was compromised.

NTSB Probable Cause

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

Full Narrative

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.

Flight

Event TypeAccident
Event Time12:07 MST
Nearest AirportDouglas Municipal (0nm)
Runway21
Runway Length5760 ft
Runway Width75 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPietsch IT
Tail NumberN214GP
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · IO-360 · Reciprocating
Seats1

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 48 · First Class · None

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility20 sm
CeilingNone
Temperature / Dew Point0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data