N441GR

Substantial
None

Cessna U206S/N: U20601801

Accident Details

Date
Saturday, August 18, 2018
NTSB Number
ANC18LA067
Location
Pedro Bay, AK
Event ID
20180828X64220
Coordinates
59.796943, -154.129714
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
6
Total Aboard
6

Probable Cause and Findings

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.

Aircraft Information

Registration
N441GR
Make
CESSNA
Serial Number
U20601801
Engine Type
Reciprocating
Year Built
1972
Model / ICAO
U206C206
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
AK AIR LEASING LLC
Address
2282 KACHEMAK DR
Status
Deregistered
City
HOMER
State / Zip Code
AK 99603-8019
Country
United States

Analysis

On August 18, 2018, about 1000 Alaska daylight time, a Cessna U206F airplane, N441GR, sustained substantial damage while landing at a remote unimproved tidal beach about 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 the provisions of 14 Code of Federal Regulations Part 135 when the accident occurred. The commercial pilot and five passengers were not injured. Visual meteorological conditions prevailed, and company flight following procedures were in effect. The flight departed Homer, Alaska, about 0900.

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 stated that after touchdown, it "felt like" the airplane had a flat tire and it subsequently veered to the right and came 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.

An initial examination of the airplane, by the pilot, revealed that both main landing gear legs separated just above the main axle attach point.

An examination by the National Transportation Safety Board (NTSB) Materials Laboratory revealed 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.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC18LA067