Incident Overview

Date: Thursday 26 November 2015
Aircraft Type: Boeing 737-322
Owner/operator: Magnicharters
Registration Number: XA-UNM
Location: Mexico City-Benito Ju rez International Airport (MEX) – ÿ Mexico
Phase of Flight: Landing
Status: Substantial, written off
Casualties: Fatalities: 0 / Occupants: 144
Component Affected: Left-hand main landing gearLeft-hand main landing gear
Investigating Agency: CIDAIA MexicoCIDAIA Mexico
Category: Accident
A Boeing 737-322 experienced a landing gear collapse during a flight from Canc£n to Mexico City-Benito Ju rez International Airport (MEX) due to a structural failure of the left-hand main landing gear. The aircraft was operating at 10 nautical miles out when the crew requested a visual approach for landing on runway 05L. The landing resulted in a strong vibration, leading to the collapse of the left-hand landing gear. The probable cause was a fracture of the shimmy damper piston and subsequent retraction of the left leg assembly, resulting from vibrations during the landing run, which couldn?t be damped due to wear and play between the dynamic parts of the links, fittings, and apex joint.A Boeing 737-322 experienced a landing gear collapse during a flight from Canc£n to Mexico City-Benito Ju rez International Airport (MEX) due to a structural failure of the left-hand main landing gear. The aircraft was operating at 10 nautical miles out when the crew requested a visual approach for landing on runway 05L. The landing resulted in a strong vibration, leading to the collapse of the left-hand landing gear. The probable cause was a fracture of the shimmy damper piston and subsequent retraction of the left leg assembly, resulting from vibrations during the landing run, which couldn?t be damped due to wear and play between the dynamic parts of the links, fittings, and apex joint.

Description

A Boeing 737-322 operating flight GMT779 from Canc£n suffered a landing gear collapsed after landing at Mexico City-Benito Ju rez International Airport (MEX). The aircraft was 10 nautical miles out when the crew requested a visual approach for a landing on runway 05L. Wind was reported as variable 130-160 degrees. The flight was subsequently cleared for their requested approach. After touchdown the aircraft experienced a strong vibration, after which the left-hand main landing gear collapsed. Probable cause: “Fracture of the shimmy damper piston and subsequent retraction of the left leg assembly of the landing gear due to vibrations caused during the landing run, which could not be damped due to wear and play existing between the dynamic parts of the links, fittings and apex joint of the shimmy damper”. CONTRIBUTING FACTORS: – Unstabilized approach – Inadequate service to shimmy damper and shock strut – Landing with a low rate of descent – Wear in the Apex joint due to a play between this and the lower torsion link – Landing with high ground speed and low descent rate

Source of Information

http://www.proceso.com.mx/?p=421814http://www.proceso.com.mx/?p=421814

Primary Cause

Fracture of the shimmy damper piston and subsequent retraction of the left leg assembly due to vibrations during the landing run.Fracture of the shimmy damper piston and subsequent retraction of the left leg assembly due to vibrations during the landing run.

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