Incident Overview

Date: Friday 8 December 2017
Aircraft Type: GAF Nomad N.22C
Owner/operator: Bayswater Road Pty Ltd / Australian Aerial Mapping
Registration Number: VH-ATO
Location: Buka Airport (BUA) – ÿ Papua New Guinea
Phase of Flight: Landing
Status: Substantial
Casualties: Fatalities: 0 / Occupants: 1
Component Affected: Landing gear system (specifically the manual pump handle and extension motor).Landing gear system (specifically the manual pump handle and extension motor).
Investigating Agency: AIC PNGAIC PNG
Category: Accident
A GAF Nomad aircraft, owned by Bayswater Road Ltd, experienced a landing failure due to a malfunctioning landing gear system. The pilot-in-command attempted to extend the landing gear manually but failed, resulting in damage to the landing gear pods and nose forward of the nose locker. The pilot deployed the emergency system, but the manual pump broke, hindering the extension process. The landing occurred on a grassy flight strip, causing significant damage to the landing gear and aircraft structure. The electrical wiring to the up-lock switch on the right land gear was fractured, rendering the landing gear extension system inoperable.A GAF Nomad aircraft, owned by Bayswater Road Ltd, experienced a landing failure due to a malfunctioning landing gear system. The pilot-in-command attempted to extend the landing gear manually but failed, resulting in damage to the landing gear pods and nose forward of the nose locker. The pilot deployed the emergency system, but the manual pump broke, hindering the extension process. The landing occurred on a grassy flight strip, causing significant damage to the landing gear and aircraft structure. The electrical wiring to the up-lock switch on the right land gear was fractured, rendering the landing gear extension system inoperable.

Description

The GAF Nomad aircraft, registered VH-ATO, owned and operated by Bayswater Road Ltd, departed Buka Airport, conducting an aerial survey under VFR. The pilot-in-command was the sole occupant. The pilot reported that when doing the pre-landing checks the landing gear failed to extend. He attempted to deploy the landing gear using the emergency system (which consists in a manual pump), but the handle of the manual pump broke after three to four pumps. The pilot decided to perform a landing in the grassy flight strip, which was about 32 metres to the right of the sealed runway centerline. There was significant damage to both landing-gear pods and the nose forward of the nose locker. The landing gear doors had significant skin damage and were not aligned with the pods. The nose cone was punctured and torn on the underside. The lower attachment points of both wings’ struts came into contact with the landing-gear pods and fracturing the pods side skins. The trailing skin on the left lower strut was bent. AIC comment: The landing gear system was examined including the electrical wiring. The wire to the up-lock switch on the right land gear had fractured and separated, rendering the normal landing gear extension system inoperative. Excessive force due to the resistance of the locked-up landing gear extension motor during the pumping to extend the gear manually, likely contributed to the overload failure of the handle.

Primary Cause

Failure of the landing gear system due to a broken manual pump handle and subsequent overload of the extension motor during manual extension.Failure of the landing gear system due to a broken manual pump handle and subsequent overload of the extension motor during manual extension.

Share on:

Leave a Reply

Your email address will not be published. Required fields are marked *