Accident Cessna 310N N85WT,
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ASN Wikibase Occurrence # 43652
 
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Date:Sunday 7 October 2007
Time:11:48
Type:Silhouette image of generic C310 model; specific model in this crash may look slightly different    
Cessna 310N
Owner/operator:Private
Registration: N85WT
MSN: 310N0106
Year of manufacture:1968
Total airframe hrs:4472 hours
Fatalities:Fatalities: 2 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Ekalaka, MT -   United States of America
Phase: Landing
Nature:Private
Departure airport:Bozeman, MT (BZN)
Destination airport:Baraboo, WI (C85)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The instrument-rated private pilot was on a cross-country flight in instrument meteorological conditions. About 40 minutes after departure the pilot reported to air traffic control (ATC) that he was encountering icing conditions at his cruise altitude of 13,000 feet and requested a lower altitude. The pilot was cleared to descend to 11,000 feet. The pilot continued to encounter icing conditions and was cleared to descend to lower altitudes. About 15 minutes after the pilot's initial report of icing conditions, he transmitted "headed towards the runway" followed by "...going down...troubles with engine." No additional communication from the accident pilot was received. The wreckage was located later that day in an open field about 2 miles west of a private airstrip. Post accident examination of the airframe and engine revealed no evidence of mechanical malfunction or anomaly. Ground scars and wreckage signatures were consistent with a stall/mush into the terrain. Weather forecasts and pilot reports for the pilot's intended route of flight indicated icing and widespread instrument meteorological conditions. The pilot received a weather briefing prior to the flight; however, it was limited by his request to wind, temperature aloft forecasts and METAR observations for his route of flight. FAA Advisory Circular 91-51A states, in part, "The most hazardous aspect of structural icing is its aerodynamic effects. Ice can alter the shape of an airfoil. This can cause control problems, change the angle of attack at which the aircraft stalls, and cause the aircraft to stall at a significantly higher airspeed..." The AC additionally states "Flight into known or potential icing situations without thorough knowledge of icing and its effects and appropriate training and experience in use of deice and anti-ice systems should be avoided." According to the manufacturer, the airplane was not certified or equipped for flight into known icing conditions. It is probable that the airplane was unable to maintain an adequate airspeed during the descent for landing and stalled short of the runway.
Probable Cause: The pilot's improper in-flight planning/decision, his continued flight into adverse weather (icing conditions), and failure to maintain an adequate airspeed during the emergency descent for landing. Contributing to the accident were the forecast icing conditions.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: SEA08FA006
Status: Investigation completed
Duration:
Download report: Final report

Sources:

NTSB: https://www.ntsb.gov/_layouts/ntsb.aviation/brief.aspx?ev_id=20071022X01626&key=1

Location

Revision history:

Date/timeContributorUpdates
28-Oct-2008 00:45 ASN archive Added
21-Dec-2016 19:24 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
04-Dec-2017 18:57 ASN Update Bot Updated [Operator, Other fatalities, Departure airport, Destination airport, Source, Narrative]

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