De Havilland DHC-2 accident near Willow, AK

On July 19, 2018, a De Havilland DHC-2 (airplane) was involved in an accident near Willow, AK. 1 person died. Damage to the aircraft: destroyed.

Date
July 19, 2018
Place
Willow, AK
Aircraft
De Havilland DHC-2 · Airplane
Injuries
1 fatal, 3 serious, 0 minor
Damage
Destroyed
Position
61.732°N, 150.048°W
NTSB ID
20180719X32511

Official records · ANC18FA055

NTSB summary

HISTORY OF FLIGHTOn July 18, 2018, about 1900 Alaska daylight time, a float-equipped De Havilland DHC-2 (Beaver) airplane, N9878R, was destroyed when it was involved in an accident near Willow, Alaska. The pilot sustained fatal injuries and the two passengers sustained serious injuries. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 135 on-demand air taxi flight. The director of operations (DO) for Regal Air reported that the flight was chartered by the Alaska Medicaid Travel Office to provide roundtrip transportation for two passengers from a private residence at a remote lake, to the Willow Seaplane Base (2X2) and then return them home 2 days later. A different company pilot flew the passengers (a woman and her 2.5-year-old son) from their home to Willow Seaplane Base on July 16, and the accident flight was the return trip. The accident pilot had not flown out of Willow Lake as a company pilot-in-command or to the destination lake before, so the DO reviewed the lakes, route, and fuel load with him before the flight. The company vice president called the passenger before the flight and obtained an expected cargo load of 600 lbs. A review of Federal Aviation Administration radar and automatic dependent surveillance-broadcast (ADS-B) track data, revealed the airplane departed Lake Hood Seaplane Base (LHD), the operator's home base, about 1755 and arrived at Willow Seaplane Base at 1817. Witnesses reported that after arriving at the Willow Seaplane Base, the pilot loaded the passenger's cargo. According to the passenger, the cargo consisted of

Probable cause

The pilot's exceedance of the airplane's critical angle of attack during departure climb, which resulted in an aerodynamic stall. Contributing to the accident was the pilot's improper decision to load the airplane beyond its allowable gross weight and center of gravity limits, coupled with his lack of operational experience in the airplane make, model, and configuration.

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