ERA09CA095

NTSB accident investigation · Beech C23 · Panacea, FL · December 8, 2008

Accident · No injuriesData collectionFinal report
Date
December 8, 2008, 16:15 local (21:15 UTC)
Place
Panacea, FL
Injuries
3 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N60410Beech C23
Defining event
Initial climb: Loss of engine power (partial)
Weather
Visual (VMC) · Day
Status
Completed · report January 29, 2009
Report
Approved by Office Director
NTSB office
Eastern Region Aviation
Parties
FAA/FSDO
Case key
69590

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

A loss of engine power due to a failure of the mixture control cable housing attachment.

Findings · 1

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.

Engine controls: mixture controlAircraft › Aircraft power plant · InoperativeBeech C23: 1 caseAll aircraft: 41 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

During takeoff, the engine lost power. The pilot maneuvered the airplane away from some large trees with rudder and aileron and the airplane touched down near the edge of the runway. The nose gear struck a runway light and broke off. The airplane then spun around approximately 180 degrees before coming to rest, facing north. The underside of the fuselage sustained structural damage. The Federal Aviation Administration inspector who examined the airplane reported that the mixture control cable came loose at the cable housing crimp, resulting in the loss of engine power.

Factual narrative

During takeoff, the engine lost power. The pilot maneuvered the airplane away from some large trees with rudder and aileron and the airplane touched down near the edge of the runway. The nose gear struck a runway light and broke off. The airplane then spun around approximately 180 degrees before coming to rest, facing north. The underside of the fuselage sustained structural damage. The Federal Aviation Administration inspector who examined the airplane reported that the mixture control cable came loose at the cable housing crimp, resulting in the loss of engine power.

Aircraft

Registration
N60410
Reported as
Beech C23
Category
Airplane
Serial number
M-2162
Airframe hours
4,001
Engine
Lycoming O-360-A4K, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
N60410 LLC
Registered owner
N60410 LLC
Airworthiness certificate
Standard, Normal
Last inspection
Annual · December 17, 2007
Departed
PFN · Panama City, FL
Destination
2J0 · Panacea, FL
Airport
2J0 · Wakulla County, runway 18, 2,950 × 70 ft, grass/turf

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
60
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 2, With waivers/limitations
Last flight review
June 20, 2008
Seat
Left
Flight hours
194 total · 194 in this make and model · 120 as pilot in command · 62 in the last 90 days · 38 in the last 30 days · 5 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Lowest ceiling
None
Temperature
64 °F