No fatalities

27 Nov 2014: PIPER PA 18-150 (N9720P) — Alaska West Air, INC — Nikiski, AK

Nikiski, AK, United States

On 27 Nov 2014, a PIPER PA 18-150 (registration N9720P) operated by Alaska West Air, INC was involved in an aviation accident near Nikiski, AK. No fatalities were reported. Investigators recorded the probable cause as: The total loss of engine power due to carburetor icing, which resulted from the pilot’s failure to use carburetor heat while operating at low-power settings in an area conducive to carburetor icing. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On November 27, 2014, a Piper PA-18-150 (N9720P) experienced total engine power loss while maneuvering for an off-airport landing near Nikiski, Alaska, resulting in collision with terrain. The pilot sustained serious injuries; the passenger minor injuries. The aircraft was operated by Alaska West Air, Inc. under Part 135.

Accident Overview

On November 27, 2014, at 1117 Alaska standard time, a Piper PA-18-150 airplane, registration N9720P, collided with terrain following a total loss of engine power while maneuvering for an off-airport landing near Nikiski, Alaska. The aircraft was registered to Summit Leasing LLC and operated by Alaska West Air, Inc. under 14 CFR Part 135 as an on-demand commercial air taxi flight. Visual meteorological conditions prevailed, and a company flight plan was filed. The flight originated from Kenai, Alaska approximately 1030.

Pilot Actions

The pilot reported that before the accident, he flew 20 to 30 minutes surveying the area for possible landing sites. During this time, he applied carburetor heat three or four times to check for carburetor ice. After selecting a landing site, he completed the pre-landing checklist and placed the carburetor heat in the off position. On short final, the engine lost all power. The pilot then switched fuel tanks and turned the carburetor heat back on, but the engine did not restart. The airplane subsequently collided with rising terrain just short of the intended landing site, sustaining substantial damage to the fuselage and wings.

Post-Accident Examination

On December 1, 2014, NTSB investigators performed an examination of the airframe and engine. Control cable continuity was established from the cockpit controls to the engine for throttle, mixture, carburetor heat, and cabin heat. A follow-up examination on December 11 focused on the engine and fuel system. No anomalies, contamination, or evidence of malfunction were found in any engine accessories. The cylinders, pistons, valve train, crankshaft, and other internal components showed no evidence of anomaly or malfunction that would have precluded normal operation. Both magnetos were tested; when the coupling was rotated, a blue spark was produced from each terminal in rotational order.

Meteorological Conditions

The closest weather reporting facility, Kenai Airport, about 31 miles southeast of the accident site, reported at 1053: wind from 010 degrees at 3 knots, clear sky, visibility 10 statute miles, temperature 10°F, dewpoint 9°F, barometric pressure 30.23 inHg. According to a carburetor icing probability chart, an airplane operating in the ambient conditions at the accident site could expect light carburetor icing while at cruise or glide power.

Other Pilot Observations

Another pilot employed by the same company, who had landed at the same location minutes before the accident aircraft approached, stated that during the descent, his aircraft had accumulated carburetor ice during the approach.

Damage and Injuries

The pilot, a certificated commercial pilot, sustained serious injuries. The sole passenger sustained minor injuries. The aircraft sustained substantial damage to the fuselage and wings.

Contributing factors

Effect on equipmentNot used/operatedPilot