The Cicaré 7T/B/BT mandatory service bulletin (BSC007) for the general stabiliser support assembly provided limited guidance for disassembly of the manufactured component and did not stipulate a compliance period within which to perform the inspection nor provide consideration for repeat inspections. This potentially reduced the opportunity to detect the presence of crack initiation and growth in the stabiliser support assembly.
The rostering of the driver in the days leading up to the incident was inconsistent with Sydney Trains' rostering principles.
Sydney Trains' risk management procedures did not sufficiently mitigate risk to the safe operation of trains in circumstances where the presence of an intermediate train stop at Richmond may have reduced the risk of trains approaching the station at excessive speed.
Sydney Trains’ risk management procedures did not sufficiently mitigate risk to the safe operation of trains in circumstances when there were deficiencies in the buffer stop design at Richmond and at other locations.
When A42 collided with buffer stop at Richmond station No. 2 platform, the reinforced concrete end stop of the buffer stop withstood the impact of the collision and prevented the train from crossing into a pedestrian and main road precinct. The two hydro-pneumatic rams on the front of the buffer stop did not perform their intended function. They were not aligned with the front of the Waratah train and instead of absorbing energy from the collision, they penetrated the cavity either side of the front-of-train coupler.
The crash energy management system on the Waratah passenger train A42 reduced the impact force of the collision but not all components performed as designed. The performance of the crash energy management system was significantly limited by the buffer stop at Richmond being incompatible with the front of the Waratah train.
The pre-flight safety briefing and safety information card did not include a clear instruction on how to activate the flow of oxygen from the passenger oxygen masks and that the bag may not inflate when oxygen is flowing. This resulted in some passengers not understanding whether or not there was oxygen flowing in the mask.
The Civil Aviation Safety Authority (CASA) did not have an effective framework to approve and oversight air displays, predominantly due to the following factors:
Tugs were to be available to escort the mini cape-size ships until they had entered the South Channel, where they were stood down. However, the tug masters had not been trained in the specifics of escort towage nor in emergency response.
In pre-trial simulations, the risks associated with engine failure during departure were only considered up to when a ship had entered the South Channel. Consequently, the tugs were not in attendance to assist if propulsion was lost.
There were a total of 16 engine malfunction events globally over a 4-year period attributed to modification of the Advantage 70™ engine. The modification increased the engine outer duct gas path temperature, which led to distortion and liberation of the outer transition duct segments.
Response by Pratt and Whitney (P & W)
The fall arrest equipment used was incorrectly attached to the workers on the suspended platform. Consequently, had either of them fallen from the platform the equipment would not have worked correctly, resulting in serious or fatal injuries.
The Civil Aviation Advisory Publication for Aeroplane Landing Areas (92-1(1)) did not have guidance for the inclusion of a safe runway overrun area.
The Civil Aviation Safety Authority’s procedures and guidance for scoping a surveillance event included several important aspects, but it did not formally include the nature of the operator’s activities, the inherent threats or hazards associated with those activities, and the risk controls that were important for managing those threats or hazards.
There was no requirement for operators of passenger transport flights in aircraft with six or less seats to provide passengers with a verbal briefing, or written briefing material, on the brace position for an emergency landing or ditching, even for aircraft without upper torso restraints fitted to all passenger seats.
Upper torso restraints (UTRs) were not required for all passenger seats for small aeroplanes manufactured before December 1986 and helicopters manufactured before September 1992, including for passenger transport operations. Although options for retrofitting UTRs are available for many models of small aircraft, many of these aircraft manufactured before the applicable dates that are being used for passenger transport have not yet been retrofitted.
There were a significant number and variety of problems associated with the operator’s activities that increased safety risk, and the operator’s chief pilot held all the key positions within the operator’s organisation and conducted most of the operator’s flights. Overall, there were no effective mechanisms in place to regularly and independently review the suitability of the operator’s activities, which enabled flight operations to deviate from relevant standards.
The operator’s pilots routinely conducted near-aerobatic manoeuvres during passenger charter flights. However, procedures for these manoeuvres were not specified in the operator’s Operations Manual, and there were limited controls in place to manage the risk of these manoeuvres.
Although the operator’s procedures required that baggage and cargo be secured during flight, this procedure was routinely not followed, and the aircraft were not equipped with cargo nets or other means for securing loads in the baggage compartment.
Although the operator’s procedures required that actual weights be used for passengers, baggage and other cargo, this procedure was routinely not followed, and pilots relied on estimated weights when calculating an aircraft’s weight and balance.
