The Right Rear Check Cable “Came Loose” From The Fuselage Attach Fitting
Location: Skwentna, AK Accident Number: ANC21LA022
Date & Time: March 4, 2021, 15:00 Local Registration: N1848R
Aircraft: Cessna A185F Injuries: 4 None
Flight Conducted Under: Part 91: General aviation – Personal
On March 4, 2021, about 1500 Alaska standard time, a Cessna 185F, N1848R, was substantially damaged when it was involved in an accident near Skwentna, Alaska. The pilot and three passengers were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.
The pilot reported that, after takeoff from a remote frozen snow-covered lake, with the hydraulic-wheelski-equipped airplane, the right rear check cable “came loose” from the fuselage attach fitting. The right ski then rotated to a nose high position as he maintained control of the airplane. His initial decision was to fly to the Lake Hood Airport (LHD) Anchorage, Alaska, however a “very serious” vibration was noted in the right horizontal stabilizer and he decided to return to the departure lake to land.
During the landing, he decided to land on untracked snow, and as the ski was coming down “into its normal landing position”, the airplane veered hard to the right. Subsequently the right main landing gear separated from the fuselage and the right wing impacted the snow. The fuselage sustained substantial damage.
The airplane was equipped with Airglas LH4000 hydraulic wheel-skis. The pilot reported that the skis equipped on the airplane were manufactured in 2010 or 2011.
The manufacturer issued a service bulletin (SB) on the skis in March 2018. The service bulletin states, in part: “Airglas has received 4 reports of the LH4000 yoke (PN LH3600-5) of the welds shearing off the outboard arm of the yoke. The common thread between all occurrences is a heavy side load is applied to the skis. This sideways load appears to happen in a turn. In three cases, pilot reported to Airglas that they hit an obstruction in a turn.
The yokes Airglas manufactured up until 2014 were manufactured differently than current yoke. The older yokes were welded and then post heat-treated, followed by a mag-particle inspection. We have also seen some evidence that yokes may have been partially cracked, prior to final heavy side load occurrence. The yokes are powder coated, and this may be masking partial cracks.”
The pilot stated that he and his mechanic were unaware of the
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