No fatalities

Landing Gear Separation During Beach Landing Damages Cessna U206F (N441GR)

Pedro Bay, AK, United States

On August 18, 2018, a Cessna U206 F (registration N441GR) operated by K Bay Air LLC was involved in an aviation accident near Pedro Bay, AK. No fatalities were reported. Investigators recorded the probable cause as: The fatigue fracture of both main landing gear legs during the landing roll, which resulted in the collapse and separation of both main landing gear legs. This summary draws on records from NTSB; 13 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 2026-08-03Data APIEditorial standards

On August 18, 2018, a Cessna U206F (N441GR) sustained substantial damage after landing on a remote Alaska beach. Both main landing gear legs separated due to fatigue cracking; no injuries.

Accident Overview

On August 18, 2018, at about 1000 Alaska daylight time, a Cessna U206F airplane, registration N441GR, sustained substantial damage while landing on a remote unimproved tidal beach approximately 36 miles east of Pedro Bay, Alaska. The airplane was registered to AK Air Leasing, LLC and operated by K Bay Air, LLC as a visual flight rules (VFR) on-demand commercial flight under 14 Code of Federal Regulations Part 135. The commercial pilot and five passengers were not injured. Visual meteorological conditions prevailed, and company flight following procedures were in effect. The flight had departed Homer, Alaska, around 0900.

Landing and Damage

According to the pilot, before landing on the tidal beach, he conducted two passes over the landing area to check for debris and determine wind direction. After a stable approach, the left main and uphill tire touched down first, followed by the right main tire. The pilot reported that after touchdown, it "felt like" the airplane had a flat tire and it subsequently veered to the right, coming to rest in a left wing low attitude on a tidal mudflat. The airplane sustained substantial damage to the left wing, left horizontal stabilizer, and left elevator.

Examination Findings

An initial examination by the pilot revealed that both main landing gear legs had separated just above the main axle attach point. Subsequently, an examination by the National Transportation Safety Board (NTSB) Materials Laboratory determined that both main landing gear legs exhibited chevron marks leading to a thumbnail region consistent with fatigue cracking. The NTSB Materials Laboratory examination report is in the public docket for this accident.

Contributing factors

Main landing gear — FailureFatigue/wear/corrosion