Kota Wajar’s safety management system procedures with regard to posting a dedicated lookout were not effectively implemented.
Over the past 26 years, investigations into 41 collisions between trading ships and small vessels on the Australian coast have identified that not maintaining a proper lookout and taking early avoiding action, in accordance with the collision regulations, has been a consistent and continuing contributor to such collisions.
The presentation of the runway 34 visual approach in the operator's Route and Airport Information Manual increased the risk of the runway threshold crossing altitude being entered into the runway extension waypoint.
Qantas provided limited guidance on the conduct of a visual approach and the associated briefing required to enable the flight crew to have a shared understanding of the intended approach.
The ARTC communication protocols did not provide the NCO adequate guidance with respect to standardised phraseology to ensure messages are clear and unambiguous.
The procedures in the ARTC CoP for the use and verification of a conditional proceed authority were ineffective in mitigating the risk to the effectiveness of that authority arising from human error.
SBR’s fatigue-management processes were ineffective in identifying the fatigue impairment experienced by the driver leading up to, and at the time of the occurrence.
Accidents involving Robinson R44 helicopters without bladder-type tanks fitted result in a significantly higher proportion of post-impact fires than for other similar helicopter types. In addition, the existing United States regulatory arrangements are not sufficient to ensure all R44 operators and owners comply with the manufacturer's Service Bulletin SB-78B and fit these tanks to improve resistance to post-impact fuel leaks.
Although certification requirements for helicopters to include a crash-resistant fuel system (CRFS) were introduced in 1994, several helicopter types certified before these requirements became applicable are still being manufactured without a CRFS.
Many of the existing civil helicopter fleet are not fitted with a crash-resistant fuel system, or do not have an equivalent level of safety associated with post-impact fire prevention.
There was no Track Stability Management Plan in place for the section of track where the buckle developed – as was required by the ARTC’s CoP.
V/Line’s organisational processes for responding to and rectifying rail creep defects did not ensure that all such defects were addressed in a timely way.
The manufacturer’s calculations did not take into account the shock load imposed on the simulation wires or the lifeboat and launching frame mounting points.
The Recognized Organization’s process for the approval of the simulation wires for ‘maintenance and testing’ had not taken into account the shock loading that would be experienced during testing.
While the design of the on-load release system allowed the reset position of the hook to be visually confirmed, it did not allow for visual confirmation that the release segment and mechanism had been correctly reset. Consequently, the hook device could appear to be properly reset when it was not.
An equivalent, alternative arrangement to the safety pin had not been provided to prevent inadvertent tripping of the freefall lifeboat’s on-load release during routine operations, such as inspections and maintenance.
The design of the VCA type 37 mixed gauge turnouts (MYD882 and MYD887) was such that they were not suitable for use by rolling stock with a 127 mm rimmed wheel.
Inherent to the design of many dual gauge turnouts, is a region of reduced wheel rim contact on the broad gauge switch blade (rail head) through the transfer area. In circumstances where the switch blade is insufficiently restrained, and where the passing train has a narrow (127 mm) wheel rim width, there is an increased risk of derailment.
The physical testing and commissioning regime for the VCA type 37 turnout did not require the use of standard gauge trains with 127 mm rimmed wheels.
The VCA type 37 turnout design and V/Line’s provisional type approval process did not fully identify the subtle design changes inherent with the VCA type 37 turnout in determining testing, commissioning and validation needs.
