No fatalities

Landing Gear Collapse During Landing Roll Following Scissor Link Disconnection (N402ET)

Cordova, AK, US

On February 20, 2007, a Cessna 402C (registration N402ET) was involved in an aviation accident near Cordova, AK. No fatalities were reported. Investigators recorded the probable cause as: The disconnection of the right main landing gear scissor link/strut due to the bolt pulling through the washer and bushing, leading to loss of directional control and gear collapse. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-07-04Data APIEditorial standards

A retractable gear airplane veered right during landing roll after the right main landing gear scissor link disconnected, causing the gear to collapse and substantial wing spar damage.

Incident Summary

An air taxi cargo flight concluded with a landing on a hard surfaced runway when the pilot reported a right veer during the landing roll, resulting in a loss of directional control. The right main landing gear subsequently collapsed, causing substantial damage to the right wing spar.

Investigation Findings

Examination by the NTSB investigator-in-charge and company maintenance personnel revealed that the right main landing gear scissor link/strut had become disconnected. This disconnection allowed the right main wheel assembly to turn sideways, overloading the gear leg. Further inspection of the linkage showed that the bolt securing the scissors/linkage had pulled through the washer adjacent to the scissor bushing opening, and subsequently through the bushing itself, disconnecting the linkage.

Manufacturer Recommendation

The airplane manufacturer had issued Service Letter ME-83-37 on November 23, 1983, recommending replacement of the original equipment outer main landing gear scissors link washers with larger, more robust washers for improved service life and main landing gear alignment retention. The operator had not complied with this nonmandatory service letter, and the airplane continued to operate with the smaller washers.

Probable cause

The disconnection of the right main landing gear scissor link/strut due to the bolt pulling through the washer and bushing, leading to loss of directional control and gear collapse.

Frequently asked questions

What happened in the 20 Feb 2007 Cessna 402C accident near Cordova, AK?

A retractable gear airplane veered right during landing roll after the right main landing gear scissor link disconnected, causing the gear to collapse and substantial wing spar damage.

Were there any fatalities in the 20 Feb 2007 Cessna 402C accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 20 Feb 2007 involved a Cessna 402C, registration N402ET, at Cordova, AK.

What was the probable cause of the accident?

The disconnection of the right main landing gear scissor link/strut due to the bolt pulling through the washer and bushing, leading to loss of directional control and gear collapse.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20070308X00264. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.