LAX07CA107

NTSB accident investigation · Pietsch IT · Douglas, AZ · March 14, 2007

Accident · No injuriesData collectionFinal report
Date
March 14, 2007, 12:07 local (19:07 UTC)
Place
Douglas, AZ
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N214GPPietsch IT
Weather
Visual (VMC) · Day
Status
Completed · report May 29, 2007
Report
Approved by Office Director
Parties
Federal Aviation Administration
FAA report
20070314007479A
Case key
65429

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

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

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Airframe/component/system failure/malfunctionManeuvering
Flt control syst,rudder control cable/rod - chafed
Flt control syst,rudder control cable/rod - disconnectedCause
Loss of control - on ground/waterLanding - roll
Directional control - not possiblePilot in commandCause
Ground loop/swerve - encounteredPilot in command
On ground/water encounter with terrain/waterLanding - roll
Terrain condition - softFactor
Nose overLanding - roll

Analysis

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.

Factual 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.

Aircraft

Registration
N214GP
Reported as
Pietsch IT
Category
Airplane, amateur-built
Serial number
ZIA-0016
Airframe hours
240
Engine
Lycoming IO-360, reciprocating
Damage
Substantial damage
Flight
Air race/show · Part 91
Registered owner
Warren Pietsch
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · May 1, 2006
Departed
DGL · Douglas, AZ
Destination
DGL · Douglas, AZ
Airport
DGL · Douglas Municipal, runway 21, 5,760 × 75 ft, asphalt

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
48
Injuries
None
Certificate
Airline transport
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1
Flight hours
25,000 total · 220 in this make and model · 300 in the last 90 days · 50 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
20 statute miles
Lowest ceiling
None
Temperature
82 °F

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.