Jump to Content
Download Final Report
[ Download PDF: 16KB]

The pilot reported that after a normal approach in light wind to runway 14 at Coolangatta, followed by what appeared to be a normal touchdown, the nosegear collapsed. The aircraft came to rest nose down, supported by the propeller, 320 m from the runway threshold. The aircraft was undergoing first of type testing in accordance with CASA Flight Test Format for CAO 101.28 category aeroplanes. On the day of the accident the pilot had been conducting climb and stall tests at close to the maximum takeoff weight (MTOW) at near the most forward centre of gravity. The maximum landing weight (MLW) is 1315 kg and the centre of gravity (CG) limits are between 1930 mm (forward) and 2132mm (aft) from the datum. At the time of landing, the approximate weight and balance was 1240 kg and 1948 mm. Examination of the runway revealed that the nosewheel had scored the surface for about 0.6 m at a point 87 m from the runway threshold (187 m from the runway end).

No further marks occurred until propeller strikes appear 133 m from the runway threshold, 187 m before the aircraft came to rest. Examination ot the damaged nosewheel strut, which is a hollow metal tube, indicated that the fracture occurred at a point on the tube which may indicate defective welding or corrosion. Furthermore, where the strut was attached to the fuselage there was minimal movement or flexibility in the attachment to absorb shock or pressure. During static weight and balance measurements, the static weight on the nosewheel was 182 kg. Consequently when the aircraft was landed at a heavy weight with a forward CG, excessive force may have been exerted on the nosegear the landing, causing it to fail. The pilot has recommended that the structural integrity of the nosewheel strut be further investigated, redesign of the strut attachment, and a check of the elevator control system. He further recommended that the forward CG limit be reduced, and calibration of the airspeed indicator be carried out.

Download Final Report
[ Download PDF: 16KB]
General details
Date: 21 March 1997 Investigation status: Completed 
Time: 15:50 EST  
 Investigation type: Occurrence Investigation 
Release date: 09 May 1997 Occurrence class: Technical 
Report status: Final Occurrence category: Accident 
Aircraft details
Aircraft manufacturer: Amateur Built Aircraft 
Aircraft model: EXPRESS 260 
Aircraft registration: VH-PNK 
Sector: Piston 
Damage to aircraft: Substantial 
Departure point:Coolangatta QLD
Destination:Coolangatta QLD
Share this page Provide feedback on this investigation
Last update 28 October 2014