DFW08CA159

NTSB accident investigation · Beech E-18 · Guymon, OK · June 1, 2008

Accident · No injuriesData collectionFinal report
Date
June 1, 2008, 15:30 local (20:30 UTC)
Place
Guymon, OK
Injuries
3 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N241XBeech E-18
Defining event
Landing-landing roll: Loss of control on ground
Weather
Visual (VMC) · Day
Status
Completed · report July 30, 2008
Report
Approved by Office Director
FAA report
20080601834219A
Case key
68157

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 pilot's failure to maintain directional control during landing roll out. Contributing to the accident was the crosswind.

Findings · 3

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.

Wind: crosswindEnvironmental issues › Conditions/weather/phenomena · Contributed to outcomeBeech E18S-9700: 1 caseAll aircraft: 1,008 casesProbable cause
Performance/control parameters: directional controlAircraft › Aircraft oper/perf/capability · Not attained/maintainedBeech E18S-9700: 1 caseAll aircraft: 3,958 casesProbable cause
Object/animal/substance: fence/fence postEnvironmental issues › Physical environment · Not specifiedBeech E18S-9700: 1 caseAll aircraft: 313 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

The private pilot used differential power to help land his twin engine, tailwheel-equipped airplane on a paved runway with a left crosswind. During the landing roll out, when the tailwheel touched down on the ground, the airplane turned into the wind and departed the runway to the left. It crossed over a ditch and struck a metal fence. The airplane sustained structural damage to the left engine mount. The left wing tip, left landing gear drag link, right vertical stabilizer and the rudder were also damaged. The pilot stated that the accident could have been prevented if he had kept the tail in the air longer with more differential power carried into the landing roll out. He reported that the wind was from 100 degrees at 15 knots.

Factual narrative

The private pilot used differential power to help land his twin engine, tail wheel-equipped airplane on a paved runway with a left crosswind. During the landing roll out, when the tail wheel touched down on the ground, the airplane turned into the wind and departed the runway to the left. It crossed over a ditch and struck a metal fence. The airplane sustained structural damage to the left engine mount. The left wing tip, left landing gear drag link, right vertical stabilizer and the rudder were also damaged. The pilot stated that the accident could have been prevented if he had kept the tail in the air longer with more differential power carried into the landing roll out. He reported the wind was from 100 degrees at 15 knots.

Aircraft

Registration
N241X
Reported as
Beech E-18
Category
Airplane
Serial number
BA455
Engine
Pratt & Whitney R-985, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Bogie Brothers LLC (Charles Bogie)
Airworthiness certificate
Standard, Normal
Departed
PWA · Oklahoma City, OK
Destination
GUY · Guyon, KS
Airport
GUY · Guymon, runway 18

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
40
Certificate
Private
Airplane ratings
Multi-engine land
Instrument ratings
Airplane
Medical
Class 3
Flight hours
1,100 total · 65 in this make and model · 4 in the last 90 days · 3 in the last 30 days

Weather

Conditions
Visual (VMC) · Day

FAA reports on this event · 1

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