BELLANCA 17-30A near Albany, OH — 2014-04-05
- Date
- 2014-04-05
- Location
- Albany, OH, USA
- Airport
- UNI
- Aircraft
- BELLANCA 17-30A
- Registration
- N8259R
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 1
- Phase of flight
- Approach
Probable cause
The pilot’s loss of airplane control during the approach to landing.
NTSB narrative
The pilot was using flight following services from air traffic control during the return leg of the cross-country flight, and, about 12 miles from the destination, the pilot reported to the approach controller that he had the airport in sight. Two witnesses reported seeing the airplane traveling toward the airport and then "nose dive" to a nearby quarry's property. One of the witnesses indicated that the back of the airplane hit a tree and that the airplane subsequently impacted the ground. The other witness said that the airplane engine was making a "buzzing" noise after the airplane crashed but that he did not hear anything before the crash. The main airplane wreckage came to rest inverted near a tree line about 2,300 feet northwest of the runway's displaced threshold. Trees in the tree line exhibited broken and cut branches along about a 300-foot-long path, and the airplane was found fragmented and signs of a ground fire were observed along the path. The crankshaft propeller flange had separated from the crankshaft. A family member who flew with the pilot during an earlier leg of the cross-country flight reported that the airplane's engine seemed harder to start than usual and that, during cruise, a distinct engine vibration occurred when the fuel mixture was leaned. However, examinations revealed no preimpact airframe or engine anomalies that would have precluded normal operation. Further, during an engine test run conducted after engine items that had sustained impact damage were replaced and a centering pilot shaft and the propeller flange were welded to the engine's crankshaft separation point, the engine ran normally, and no preimpact engine anomalies were detected. On the basis of the evidence, it is likely that the pilot lost control of the airplane during the approach to landing.
Analysis
- Primary failure mode
- Loss of control
- First missed decision gate
- Pilot could have requested a weather briefing before approach.
NTSB coding
Evidence available
- Photos
- 33 docket documents
Docket documents33
- Evidence Control Formsform
- Party Formsform
- Witness Statementsinterview
- Communication Summary - Becky Sheetsother
- Communication Summary - Fire Chief Waren Keirnsother
- Communication Summary - Leslie Nicholsonother
- Maintenance Logbook Excerptsother
- Pilot Logbook Excerptother
- Pilots 72-Hour History supplied by family memberother
- Photo 1 - Front of Airplanephotos
- Photo 10 - Auxilliary and Fuselage Fuel Tank Selectorphotos
- Photo 11 - Fuel Tank Selectorphotos
- Photo 12 - Flap Jack Screw Extensionphotos
- Photo 13 - Engine Driven Fuel Pump Drive Gear and its Shear Shaftphotos
- Photo 14 - Propeller Flangephotos
- Photo 15 - Sparkplugsphotos
- Photo 16 - Fluid Draining From The Fuel Hose Between Firewall and Engine Driven Fuel Pumpphotos
- Photo 17 - Fuel Manifoldphotos
- Photo 18 - Separated Propeller Flange Welded to Crankshaftphotos
- Photo 19 - Engine on Test Stand with Test Clubphotos
- Photo 2 - Right Side of Airplanephotos
- Photo 20 - Swaged Cable Connection on Governor Control Cablephotos
- Photo 21 - Swaged Cable Connections on Mixture and Throttle Control Cablesphotos
- Photo 3 - Ground Scar and Path of Broken Branchesphotos
- Photo 4 - Aerial View of Accident Locationphotos
- Photo 5 - Tree Branch With Dark Paint Transferphotos
- Photo 6 - Tree Trunk with Charred Barkphotos
- Photo 7 - Separated Tree Branchphotos
- Photo 8 - Tree Branches Not Consistent With Recent Separationsphotos
- Photo 9 - Shattered Glass Near Left Wing Tipphotos
- GPS Factual Reportreport
- Toxicology Reportreport
- Release of Wreckagewreckage
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