CEN11CA282

NTSB accident investigation · Delf Tim Zenith CH-701 · Davenport, IA · April 12, 2011

Accident · No injuriesData collectionFinal report
Date
April 12, 2011, 17:30 local (22:30 UTC)
Place
Davenport, IA
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N701YBDelf Tim Zenith CH-701
Defining event
Takeoff: Flight control sys malf/fail
Weather
Visual (VMC) · Day
Status
Completed · report July 12, 2011
Report
Approved by Office Director
NTSB office
Central Region
Parties
Federal Aviation Administration
FAA report
20110412004929A
Case key
78848

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

On this page

Probable cause

The improper installation of the rudder cable to rudder pedal attachment hardware.

Findings · 2

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Flight control system: rudder control systemAircraft › Aircraft systems · Incorrect service/maintenanceDelf Tim ZENITH CH-701: 1 caseAll aircraft: 93 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

Prior to the flight, the pilot performed a preflight inspection, but he did not inspect the rudder pedals and rudder cable attachments. During takeoff, approximately 50 feet above ground level, the pilot felt something unusual with the left rudder pedal. The airplane immediately veered to the right, and the pilot initiated a climb in an attempt to troubleshoot the problem. Unable to determine what happened, the pilot maneuvered the airplane back to the airport. The airplane was difficult to control to the left and he determined he had to make a landing on the grass adjacent to the runway. During the landing, the airplane impacted a drainage ditch. The airplane sustained substantial damage to the firewall. Postaccident examination of the airplane revealed the bolt/nut hardware that connected the left rudder cable to the rudder pedal had separated, and the cable became disconnected from the pedal. The nut, which is to be secured by a cotter pin, backed off of the bolt. The bolt and nut were found within the airplane. The experimental amateur-built airplane had accumulated approximately 19 hours of flight time, at the time of the accident.

Factual narrative

Prior to the flight, the pilot performed a preflight inspection, but he did not inspect the rudder pedals and rudder cable attachments. During takeoff, approximately 50 feet above ground level, the pilot felt something unusual with the left rudder pedal. The airplane immediately veered to the right, and the pilot initiated a climb in an attempt to troubleshoot the problem. Unable to determine what happened, the pilot maneuvered the airplane back to the airport. The airplane was difficult to control to the left and he determined he had to make a landing on the grass adjacent to the runway. During the landing, the airplane impacted a drainage ditch. The airplane sustained substantial damage to the firewall. Postaccident examination of the airplane revealed the bolt/nut hardware that connected the left rudder cable to the rudder pedal had separated, and the cable became disconnected from the pedal. The nut, which is to be secured by a cotter pin, backed off of the bolt. The bolt and nut were found within the airplane. The experimental amateur-built airplane had accumulated approximately 19 hours during Phase 1 at the time of the accident.

Aircraft

Registration
N701YB
Reported as
Delf Tim Zenith CH-701
Category
Airplane, amateur-built
Serial number
74495
Airframe hours
19
Engine
Continental O-200, 100 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Delf Tim
Registered owner
Delf Tim
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Condition · March 11, 2011
Departed
DVN · Davenport, IA
Destination
DVN · Davenport, IA
Airport
DVN · Davenport Municipal Airport

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
53
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 3, With waivers/limitations
Last flight review
June 15, 2009
Seat
Left
Flight hours
1,200 total · 24 in this make and model · 1,090 as pilot in command · 30 in the last 90 days · 19 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
100° at 4 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
64 °F

Docket · 1

The files NTSB released with the investigation on May 9, 2011, on NTSB’s docket system: statements, records, photos and specialists’ reports. 354 KB in all.

FAA reports on this event · 1

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