10 fatalities

2001-10-10: Cessna 208A Caravan (N9530F) — PenAir - Peninsula Airways - Alaska Airlines Commuter — Dillingham, United States of America

Dillingham, United States of AmericaTakeoff (climb)

On October 10, 2001, a Cessna 208A Caravan (registration N9530F) operated by PenAir - Peninsula Airways - Alaska Airlines Commuter was involved in an aviation accident near Dillingham, United States of America during takeoff. 10 people were killed. Investigators recorded the probable cause as: An in-flight loss of control resulting from upper surface ice contamination that the pilot-in-command failed to detect during his preflight inspection of the airplane. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781202347Data APIEditorial standards

A CE-208 crashed shortly after takeoff due to ice contamination on the wing that the pilot failed to detect during preflight. Investigators found no pre-impact failures.

Background

The airplane had been parked outside on the ramp overnight, exposed to rain, snow, and temperatures below 32 degrees Fahrenheit. Other pilots reported that their aircraft, also parked outside, were covered with a layer of ice topped by 1/4 to 1/2 inch of snow or frost. Ramp personnel deiced the accident airplane with a heated glycol-water mixture. The PenAir ramp supervisor who performed the deicing believed the upper wing surface was clear of ice but did not physically touch the wing to verify. It could not be determined whether the pilot visually or physically inspected the wing and tail surfaces after deicing. However, the high-wing configuration would have hampered the pilot's ability to see residual clear ice.

Accident Sequence

The airplane, with the pilot and nine passengers aboard, crashed shortly after takeoff from runway 01. A witness reported a normal flight until the aircraft suddenly pitched up, rolled 90 degrees left, and yawed left. It then descended nose-down until out of view. Engine monitoring data showed a maximum altitude of about 651 feet above mean sea level. The airplane crashed in a level attitude.

Investigation Findings

Investigators found no evidence of pre-impact failures in the structure, flight controls, or instruments. Examination of the engine and propeller revealed no pre-impact anomalies, and the engine was running at impact. Company records indicated the commercial pilot completed initial CE-208 training two months before the accident, with 74 hours in type.

Probable Cause

The official probable cause was determined to be an in-flight loss of control resulting from upper surface ice contamination that the pilot-in-command failed to detect during preflight inspection. Contributing was the lack of a requirement for CE-208 pilots to closely examine the upper wing surface for ice under ground icing conditions.