CHI06LA088

NTSB accident investigation · Irwin Sonex 2180 · Rockford, IL · February 27, 2006

Accident · No injuriesLimited investigationFinal report
Date
February 27, 2006, 16:45 local (22:45 UTC)
Place
Rockford, IL
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N514KPIrwin Sonex 2180
Weather
Visual (VMC) · Day
Status
Completed · report October 3, 2006
Report
Approved by Office Director
Parties
Federal Aviation Administration
FAA report
20060227006149A
Case key
63281

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

The loss of engine power due to the restricted movement of the throttle cable during cruise flight. A factor in the accident was the trees contacted during the forced landing.

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/malfunctionCruise
Throttle/power lever,cable - movement restrictedCause
Forced landingEmergency descent/landing
In flight collision with objectEmergency descent/landing
Object - tree(s)Factor
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - ground

Analysis

The experimental amateur-built airplane sustained substantial damage on impact with trees and terrain during a forced landing. The pilot reported the throttle stuck during cruise flight. The pilot attempted to get the sticking throttle to release and the throttle stuck in idle position. The kit manufacturer's examination of the throttle cable and carburetor concluded: "The throttle cable was not supported/attached to anything from the firewall to the cockpit control knob. There was a large amount of flex in the cable when the control knob was pushed when resistance was applied to the Carb End of the cable. The only anchor on the throttle cable was a "through the firewall" clamp. ... The AeroCarb was disassembled. ... Nothing internally was found that would cause it to stick."

Factual narrative

On February 27, 2006, about 1645 central standard time (cst), an experimental amateur-built Irwin Sonex 2180 airplane, N514KP, piloted by a private pilot, sustained substantial damage on impact with trees and terrain during a forced landing near Rockford, Illinois. The personal flight was operating under 14 Code of Federal Regulations Part 91. No flight plan was on file. The pilot reported that he sustained no injuries. The flight originated from the Poplar Grove Airport (C77), near Poplar Grove, Illinois, at 1615.

The pilot's accident report, in part, stated:

Aircraft departed C77 on a personal, recreational flight at

approximately 415 pm cst. Pilot performed several throttle sticking

tests in the immediate vicinity of C77 and all was o.k. Pilot cruised

north of Rockford, IL at approximately 2200 [feet above mean sea

level] at 2800 rpm. Just north of Cottonwood Airport (IC8) pilot

attempted to increase throttle. It stuck. Pilot attempted to get

sticking to release [and] throttle stuck in idle position. Pilot turned

toward Cottonwood but when he determined it was out of range, he

picked the best available corn field. Upon approach, he pulled up

over electrical wires [and] a wind gust pushed the plane into the top

of a tree about 25 [feet] up. After impacting the tree, the plane

stopped forward movement and fell tail first to the ground. ... The

craft then tipped onto its top. Pilot exited through broken canopy.

A Federal Aviation Administration Inspector and a representative from the kit manufacturer examined the wreckage to include the throttle cable and carburetor. The kit manufacturer stated:

When disconnected from the carb, the Throttle Cable was found to

be quite stiff compared to others Sonex Aircraft, LLC has experience

with. Note that the owner stated it was smoother prior to the

incident. The throttle cable was not supported/attached to anything

from the firewall to the cockpit control knob. There was a large

amount of flex in the cable when the control knob was pushed when

resistance was applied to the Carb End of the cable. The only anchor

on the throttle cable was a "through the firewall" clamp. ...

The AeroCarb was disassembled. No internal flaws or defects were

found other than some very minor scratches. Nothing internally was

found that would cause it to stick. ...

The Sonex website, www.sonexaircraft.com, was reviewed. The site contains links to service bulletins to include bulletins in reference to sticky throttles.

Aircraft

Registration
N514KP
Reported as
Irwin Sonex 2180
Category
Airplane, amateur-built
Serial number
514
Airframe hours
18.5
Engine
Aero Vee 2180, 80 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Ken Irwin
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Condition · February 1, 2006
Departed
C77 · Poplar Grove, IL

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
Minor
Certificate
Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 3, With waivers/limitations
Last flight review
July 1, 2005
Seat
Left
Flight hours
742 total · 18 in this make and model · 667 as pilot in command · 18 in the last 90 days · 13 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
60° at 15 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
36 °F, dew point 21 °F
Altimeter
29.98 inHg
Observed at
RFD, 6 nm away

FAA reports on this event · 1

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