Aircraft Accident/Incident Report

Hudson, Kentucky 40143
Saturday, April 14, 2012 13:30 CDT

NTSB Narrative Summary Released at Completion of Accident

About 2 months before the accident, the homebuilt experimental airplane began to experience electrical problems. This was first discovered when the landing gear hesitated before extending. To extend the landing gear during subsequent flights, the pilot shut off all nonessential electrical equipment in the airplane, extended the landing gear, and then turned the electrical equipment back on. On the morning of the accident, while on approach at the destination airport, the electrical system failed and the landing gear would not extend. The pilot reached behind his seat, "jiggled" the airplane's battery cables, and was able to restore electricity and extend the landing gear. He landed the airplane uneventfully and shut the airplane down. After shutdown, the airplane had to be "hand propped" to be restarted; however, the pilot could not adjust the electrically-controlled propeller to the proper pitch for takeoff. The pilot removed the battery from his airplane and returned to his home airport with another pilot. He charged two batteries and returned with the charged batteries to his airplane. The pilot installed one of the batteries in his airplane and stated that if he could get the airplane started, he would fly it back to his home airport with the landing gear down. The airplane started after three attempts, and the pilot taxied to the runway. A witness observed fuel exiting the right wingtip fuel vent during taxi, indicating that there was fuel in the main wing tanks. The pilot departed, and while he was en route, he transmitted that he was experiencing a problem and that he was going to land in a field. A witness observed the airplane at low altitude but did not hear any engine noise as the airplane passed him. The airplane then maneuvered around a barn and touched down in a level attitude in a harvested corn field. The airplane’s landing gear collapsed, and the airplane nosed over. Examination of the airplane and engine revealed no evidence of any preimpact mechanical failure or malfunction; however, examination of the propeller indicated that the engine was not producing power, and the header tank, which supplied fuel to the engine, contained only 8 ounces of fuel. The inline fuel filter and fuel strainer contained only trace amounts of fuel. Further examination revealed that the header tank received its fuel from the wing tanks via electrically-operated transfer pumps. Examination of a connector that connected the positive battery cable to the master relay revealed that the inside of the connector's collar, which had been soldered and crimped onto the battery cable, was moist and heavily corroded, and that not all of the battery cable's wire strands were in contact with the collar of the connector. Further examination revealed that the end of battery cable that had been retained by the connector's collar was also moist and exhibited significant corrosion, indicating that the connector had been exposed to a corrosive environment. Examination of the battery box revealed corrosion and electrolyte (sulfuric acid) residue, which indicated that a release of electrolyte from a previously-installed battery had occurred. Additionally, comparison of the position of the positive battery cable's run from the battery terminal to the master contactor revealed that the master contactor was mounted below the top of the battery and that no precautions had been taken to prevent liquid from running down the cable into the base of the connector. With a failure of the electrical wiring interconnect, the airplane’s battery was unable to power the electrical system. Because the fuel transfer pumps were electrically powered, fuel was not transferred to the header tank to feed the engine, and a loss of engine power occurred. Additionally, without electrical power, the propeller could not be adjusted and the electrically-actuated landing gear could not be retracted to reduce drag and extend the airplane’s glide. Further, because the wing flaps were electrically operated, they could not be extended during the landing, thus the airplane touched down at a higher speed (13 or more knots) than normal touchdown speed, which reduced the survivability of the accident when the airplane nosed over.

NTSB Probable Cause Narrative

The pilot's decision to operate the airplane with known electrical system problems, which resulted in the in-flight failure of the electrical wiring interconnect system, loss of electrical power, and subsequent fuel starvation and loss of engine power.

Event Information

Type of Event Accident
Event Date 4/14/2012
Event Day of the Week Saturday
Time of Event 1330
Event Time Zone Central Daylight Time
Event City Hudson
Event State KENTUCKY
Event Country --
Zipcode of the event site 40143
Event Date Year 2012
Event Date Month 4
MidAir Collision Indicator No
On Ground Collision occurred ? No
Event Location Latitude 374109N
Event Location Longitude 0862008W
Event Location Airport --
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 Weather Observation Facility
Time of the weather observation 1355 Central Daylight Time
Direction of event from weather observation facility (degrees) 90
Weather Observation Facility ID FTK
Elevation of weather observation facility 755
Distance of event from weather observation facility (units?) 21
Time Zone of the weather observation CDT
Lighting Conditions Day
Lowest Ceiling Height 8500
Lowest Non-Ceiling Height --
Sky/Lowest/Cloud Conditions --
Sky Condition for Lowest Ceiling Broken
Visibility Runway Visual Range (Feet) --
Visibility Runway Visual Value (Statute Miles) --
Visibility (Statute Miles) 10
Air Temperature at event time (in degrees celsius) 24
Dew Point at event time (in degress fahrenheit) 11
Wind Direction (degrees magnetic) 180
Variable Wind Indicator Wind direction could be determined
Wind Speed (knots) 15
Wind Velocity Indicator --
Wind Gust Indicator Not Gusting
Wind Gust (knots) --
Altimeter Setting at event time (in. Hg) 30.04
Density Altitude (feet) --
Intensity of Precipitation --
METAR weather report --
Event Highest Injury Fatal
On Ground, Fatal Injuries --
On Ground, Minor Injuries --
On Ground, Serious Injuries --
Injury Total Fatal 1
Injury Total Minor --
Injury Total None --
Injury Total Serious --
Injury Total All 1
Investigating Agency NTSB
NTSB Docket Number (internal use) 31426
NTSB Notification Source FAA Southern Region ROC
NTSB Notification Date --
NTSB Notification Time --
Fiche Number and/or location -used to find docket information --
Date of most recent change to record Jun 13 2013 9:21AM
User who most recently changed record kenj
Basic weather conditions Visual Meteorological Cond
FAA District Office --

Aircraft Involved

Aircraft #1

Aircraft Registration Number N235MW
NTSB Number ERA12FA280
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 MANZITTO MICHAEL A
Aircraft Model MWLANCAIR 235
Aircraft Series Identifier --
Aircraft Serial Number MW06
Certified Max Gross Weight 1400
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 2
Number of Engines 1
Fixed gear or retractable gear Retractable
Aircraft, Type of Last Inspection Conditional
Date of Last Inspection May 11 2011 12:00AM
Airframe hours since last inspection 86
Airframe Hours 324
ELT Installed Yes
ELT Activated Yes
ELT Aided Location of Event Site No
ELT Type Unknown
Aircraft Owner Name KLEIN DONALD E JR
Aircraft Owner Street Address --
Aircraft Owner City LOUISVILLE
Aircraft Owner State KY
Aircraft Owner Country USA
Aircraft Owner Zipcode 40299-3271
Operator is an individual? Yes
Operator Name KLEIN DONALD E JR
Operator Same as Owner? Yes
Operator Is Doing Business As --
Operator Address Same as Owner? Yes
Operator Street Address --
Operator City LOUISVILLE
Operator State KY
Operator Country USA
Operator Zip code 40299-3271
Operator Code --
Owner has at least one certificate None
Other Operator of large aircraft? No
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 2I3
Departure City Falls of Rough
Departure State KY
Departure Country USA
Departure Time 1325
Departure Time Zone CDT
Destination Same as Local Flt --
Destination Airport Code LOU
Destination City Louisville
Destination State KY
Destination Country USA
Specific Phase of Flight --
Report sent to ICAO? --
Evacuation occurred --
Date of most recent change to record Jul 9 2013 3:17PM
User who most recently changed record reej
Since inspection or accident Time of Accident
Event Location Runway Number and Location N/A
Runway Length --
Runway Width --
Sight Seeing flight No
Air Medical Flight No
Medical Flight --