None Airport
Aircraft Accident/Incident Report

Pocahontas, Arkansas 72455
Tuesady, June 6, 2006 8:00 CDT

NTSB Narrative Summary Released at Completion of Accident

The 18,700-hour pilot was piloting his single-engine experimental airplane at an altitude of 4,500 feet mean sea level (msl) when he started to feel a "slight vibration" or "light buzz" from the engine. The vibrations gradually became more severe until there was a loud bang and the engine seized. The pilot made a forced landing to a hay field. Metallurgical examination of the engine revealed the crankshaft had fractured through the crank cheek, between the #5 and #6 cylinder journals as a result of fatigue cracking. Further examination revealed that the crankshaft was susceptible to early subsurface fatigue failure due to the presence of "honeycomb" structure and microcracking. The mechanical damage was from contact of the connecting rod with the crankshaft thrust faces, and the "honeycomb" structure was most likely a result of overheating during the forging process. The crankshaft had been installed new in the engine in 2001,and two years later was modified with 11:1 compression ratio pistons. As a result of this and other modifications, engine power was increased by 30 percent. Due to the fact that these modifications altered the engine's original certification criteria; the engine was re-classified as an experimental. The serial number of the fractured crankshaft was listed in Lycoming's Mandatory Service Bulletin (SB) 569A, titled Crankshaft Retirement for Certain Lycoming Engines, which recommended the crankshafts be replaced at the first instance the engine crankcase was separated or no later than February 21, 2009. The SB was generated as a result of several subsurface fatigue failures of similar crankshafts used on higher horsepower engines (greater than 300 HP). Those crankshafts were subject to Airworthiness Directive (AD) 2002-04-51, which would have required them to be removed before the date of this accident. Since the engine was classified as experimental, the crankshaft did not have to be removed as a result of this guidance. The AD and SB were issued as a result of a slight change in the specified composition of the crankshaft material, which was a small vanadium addition intended to lower the tempering temperature and reduce warpage; however, this change increased the susceptibility to "honeycomb" and microcracking when slightly over-heated during the forging process. The "honeycomb" and microstructure significantly reduced fatigue properties. The loss of fatigue life was most pronounced in the higher HP applications, and the experimental modifications made to this engine would have made the crankshaft more susceptible to fatigue fracture.

NTSB Probable Cause Narrative

The loss of engine power as a result of a fractured crankshaft due to fatigue. A factor was the engine modifications to increase engine horsepower.

Event Information

Type of Event Accident
Event Date 6/6/2006
Event Day of the Week Tuesday
Time of Event 800
Event Time Zone Central Daylight Time
Event City Pocahontas
Event State ARKANSAS
Event Country --
Zipcode of the event site 72455
Event Date Year 2006
Event Date Month 6
MidAir Collision Indicator --
On Ground Collision occurred ? --
Event Location Latitude 361426N
Event Location Longitude 0905711W
Event Location Airport None
Event Location Nearest Airport ID --
Indicates whether the acc/inc occurred off or on an airport Off Airport/Airstrip
Distance from airport in statute miles --
Degrees magnetic from airport --
Airport Elevation --
Weather Briefing Completeness --
Investigator's weather source Pilot
Time of the weather observation
Direction of event from weather observation facility (degrees) --
Weather Observation Facility ID --
Elevation of weather observation facility --
Distance of event from weather observation facility (units?) --
Time Zone of the weather observation --
Lighting Conditions Day
Lowest Ceiling Height --
Lowest Non-Ceiling Height --
Sky/Lowest/Cloud Conditions Clear
Sky Condition for Lowest Ceiling None
Visibility Runway Visual Range (Feet) --
Visibility Runway Visual Value (Statute Miles) --
Visibility (Statute Miles) 10
Air Temperature at event time (in degrees celsius) 19
Dew Point at event time (in degress fahrenheit) 14
Wind Direction (degrees magnetic) 180
Variable Wind Indicator Wind direction could be determined
Wind Speed (knots) 10
Wind Velocity Indicator --
Wind Gust Indicator Not Gusting
Wind Gust (knots) --
Altimeter Setting at event time (in. Hg) 30
Density Altitude (feet) --
Intensity of Precipitation --
METAR weather report --
Event Highest Injury None
On Ground, Fatal Injuries --
On Ground, Minor Injuries --
On Ground, Serious Injuries --
Injury Total Fatal --
Injury Total Minor --
Injury Total None 1
Injury Total Serious --
Injury Total All --
Investigating Agency NTSB
NTSB Docket Number (internal use) 20633
NTSB Notification Source LIT FSDO
NTSB Notification Date Jun 7 2006 12:00AM
NTSB Notification Time --
Fiche Number and/or location -used to find docket information DMS
Date of most recent change to record Nov 29 2006 12:45PM
User who most recently changed record NTSB\johb
Basic weather conditions Visual Meteorological Cond
FAA District Office Little Rock, Arkansas

Aircraft Involved

Aircraft #1

Aircraft Registration Number N181DM
NTSB Number DFW06LA154
Missing Aircraft Indicator --
Federal Aviation Reg. Part Part 91: General Aviation
Type of Flight Plan filed None
Flight plan Was Activated? No
Damage Substantial
Aircraft Fire None
Aircraft Explosion None
Aircraft Manufacturer's Full Name McClung
Aircraft Model Christian Eagle I
Aircraft Series Identifier --
Aircraft Serial Number M002
Certified Max Gross Weight 1650
Aircraft Category Airplane
Aircraft Registration Class --
Aircraft is a homebuilt? Yes
Flight Crew Seats --
Cabin Crew Seats --
Passenger Seats --
Total number of seats on the aircraft 1
Number of Engines 1
Fixed gear or retractable gear Fixed
Aircraft, Type of Last Inspection Conditional
Date of Last Inspection Mar 1 2006 12:00AM
Airframe hours since last inspection --
Airframe Hours 524.5
ELT Installed No
ELT Activated No
ELT Aided Location of Event Site No
ELT Type --
Aircraft Owner Name Red Eagle Aviation Incorporated
Aircraft Owner Street Address --
Aircraft Owner City Peachtree
Aircraft Owner State GA
Aircraft Owner Country USA
Aircraft Owner Zipcode 30269
Operator is an individual? No
Operator Name --
Operator Same as Owner? Yes
Operator Is Doing Business As --
Operator Address Same as Owner? Yes
Operator Street Address --
Operator City --
Operator State --
Operator Country --
Operator Zip code --
Operator Code --
Owner has at least one certificate None
Other Operator of large aircraft? --
Certified for Part 133 or 137 Operation --
Operator Certificate Number --
Indicates whether an air carrier operation was scheduled or not --
Indicates Domestic or International Flight --
Operator carrying Pax/Cargo/Mail --
Type of Flying (Per_Bus / Primary) Personal
Second Pilot on Board No
Departure Point Same as Event No
Departure Airport Code JFX
Departure City Jasper
Departure State AL
Departure Country USA
Departure Time 638
Departure Time Zone CDT
Destination Same as Local Flt --
Destination Airport Code Y76
Destination City Des Plains
Destination State MO
Destination Country USA
Specific Phase of Flight Cruise - normal
Report sent to ICAO? --
Evacuation occurred --
Date of most recent change to record Sep 6 2006 4:08PM
User who most recently changed record CASH
Since inspection or accident Time of Accident
Event Location Runway Number and Location NA
Runway Length --
Runway Width --
Sight Seeing flight No
Air Medical Flight No
Medical Flight --