Incident Overview

Date: Saturday 15 June 2002
Aircraft Type: de Havilland Canada DHC-8-311
Owner/operator: Schreiner Airways
Registration Number: PH-SDU
Location: Maastricht/Aachen Airport (MST) – ÿ Netherlands
Phase of Flight: Landing
Status: Substantial, repaired
Casualties: Fatalities: 0 / Occupants: 5
Component Affected: Right-hand main gearRight-hand main gear
Investigating Agency: Dutch Safety BoardDutch Safety Board
Category: Accident
During maintenance at Maastricht (MST), a right-hand main undercarriage was replaced. Following retraction and deployment of the landing gear, the right-hand main gear failed to lock down, resulting in its collapse during landing. An instrument approach was initiated with the landing gear selected down, but the gear did not lock, necessitating a gear recycle. An alternate gear extension procedure was attempted but also failed. Investigation revealed a hydraulic swivel assembly was connected upside down, causing bending and preventing locking.During maintenance at Maastricht (MST), a right-hand main undercarriage was replaced. Following retraction and deployment of the landing gear, the right-hand main gear failed to lock down, resulting in its collapse during landing. An instrument approach was initiated with the landing gear selected down, but the gear did not lock, necessitating a gear recycle. An alternate gear extension procedure was attempted but also failed. Investigation revealed a hydraulic swivel assembly was connected upside down, causing bending and preventing locking.

Description

During maintenance at Maastricht (MST) the right hand main undercarriage was replaced. The landing gear was retracted and deployed several times and performed satisfactory. Prior to being released to the leasing company a test flight was made. During an instrument approach the landing gear was selected down, but the right hand undercarriage did not lock down. The crew recycled the gear and again the right hand main gear came down but failed to lock. The ‘alternate gear extension’ procedure was followed but it again failed to lock. Upon landing the right had undercarriage collapsed. The final report of the investigation did not conform to ICAO Annex 13 standards and did not contain a Probable cause. It was noted that the hydraulic swivel assembly was connected upside down. This caused the swivel to bend when the landing gear was lowered, preventing it from locking down.

Primary Cause

Hydraulic swivel assembly connection orientation.Hydraulic swivel assembly connection orientation.

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