Saab SF-340B, VH-EKN

Summary

A Saab 340B aircraft, registered VH-EKN, was being operated on a scheduled flight from Orange to Sydney, NSW. The crew reported that, shortly after take-off, as they were setting climb power, they heard a `bang' similar to the sound of a compressor stall. The left engine gauges indicated zero torque and excessive inter-turbine temperature (ITT). The left over temperature and ignition lights illuminated, followed by a master warning annunciation. The crew carried out the engine failure procedure and, having shut down the left engine, returned to Orange and landed.

Eight days later, the crew of another Saab 340B, registered VH-OLM, operated by the same company, reported that shortly after take-off from Orange, the right engine displayed characteristics consistent with a compressor stall (ATSB Occurrence 200300078). On that occasion, after the crew carried out the appropriate checklist procedures, normal engine operation and indications were restored and the flight continued to Sydney without further incident.

The affected engines from both aircraft were removed for examination at the manufacturer's overhaul facility. The engine manufacturer, after reviewing the recorded engine data, identified that a number of similar conditions, that may have affected the engines, had existed during both flights. Both events had occurred on the first flight of the day. On both occasions a significant temperature inversion existed at approximately 1,000 ft above ground level, and the compressor stalls occurred when the crews were adjusting the power setting from take-off power to climb power. The engine manufacturer's assessment concluded that a combination of environmental conditions and engine operating procedures had led to both events and made several recommendations to the operator.

Those recommendations included changes to both the maintenance program and to the operation of the engines. They called for compressor washes to be conducted every 200 hours, or more frequently as determined by the operating environment. In the weeks prior to the occurrences there had been significant airborne particles in smoke from bushfires. That may have contributed to contamination of the compressor blades and consequently the engine's susceptibility to compressor stalling. The engine manufacturer also recommended that the operator consider amending the take-off configuration to include selecting the Environmental Control System (ECS) to ON for the first flight of the day. Use of the ECS opens the bleed air valves and reduces the likelihood of compressor stalls. Its use on the first flight of the day would counteract the conditions of temperature inversions that were usually more pronounced in the early morning.

Additionally, the engine manufacturer issued an alert service bulletin, SB CT7-TP S/B 72-A0328, Revision 1, dated 8 April 2003, which required checking that the correct rigging schedule of the engine variable inlet guide vanes (VIGV) had been implemented. Rigging of the VIGV to the specified schedule was used to reduce engine susceptibility to compressor stalls in the range of environmental conditions encountered during routine operations. The operator reported that, although the requirements of the service bulletin had been incorporated into its engine maintenance program, the rigging schedule check had not been completed on the occurrence engines. The service bulletin was subsequently incorporated into the USA Federal Aviation Administration Emergency Airworthiness Directive 2003-08-52, dated 15 April 2003 and subsequently mandated in Australia by the Civil Aviation Safety Authority as Airworthiness Directive AD/CT7/9 on 16 April 2003.

The operator reported that its maintenance program and standard operating procedures had been changed in accordance with the engine manufacturer's recommendations and that all engines in its fleet had been inspected in accordance with the requirements of the engine manufacturers service bulletin. Subsequently, there have been no further reports of compressor stalls in the climb after take-off.

Occurrence summary

Investigation number 200300040
Occurrence date 16/01/2003
Location Orange, Aero.
State New South Wales
Report release date 20/07/2004
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Saab Aircraft Co.
Model 340
Registration VH-EKN
Serial number 340B-257
Sector Turboprop
Operation type Air Transport Low Capacity
Departure point Orange, NSW
Destination Sydney, NSW
Damage Nil

Boeing 737-7BX, VH-VBS

Summary

On 16 January 2003, while conducting pre-flight checks during passenger boarding, the flight crew of a Boeing 737-700 aircraft, registered VH-VBS, detected a pungent burning smell. The pilot in command contacted the company by radio and requested that an aircraft engineer attend the aircraft.

The cabin supervisor advised the pilot in command that she could smell fumes near the forward door. The pilot in command then instructed her to disembark the passengers.

The first officer reported feeling faint and the pilot in command felt dizzy and weak at the knees as he stood to leave the flight deck. The pilot in command also reported experiencing shaking hands, watering eyes and tingling fingers. He opened the windows in the flight deck for ventilation and contacted air traffic control to request paramedic assistance. The cabin supervisor administered oxygen to the pilot in command and the first officer, but when the pilot in command attempted to stand, his legs collapsed from under him.

Airport Rescue and Fire Fighting services attended the aircraft to assist the pilot in command and requested an ambulance. The pilot in command was transported to hospital for observation and was advised by medical personnel that he showed signs similar to mild carbon dioxide poisoning.

A subsequent engineering examination of the aircraft found a burned diode on the master dim and test module circuit board on the P6 panel, located behind the first officer's seat. The plastic cased diode was the only component damaged on the circuit board. Failure analysis conducted by the aircraft manufacturer determined that the diode failure mode was due to excessive heating while under electrical load.

An examination of the circuit board conducted by the ATSB determined that the diode used on the master dim and test module circuit board was a plastic cased component which differed from the diode outlined by silk screening on the circuit board of the master dim and test module. The original diode specified for use was a hermetically sealed, metal cased, glass diode with heat dissipation properties superior to the plastic cased diode, however both diodes were approved by the aircraft manufacturer for use in this application.

The aircraft manufacturer conducted further testing on a diode with the same part number from the event master dim and test module to identify major components of combustion and reported the following:

`The plastic cased diode was manufactured of Bisphenol-A epoxy resin, which decomposed to form Phenol (C6H5OH) and variations of Phenol, eg. Methyl phenol (C6H4CH3OH). The mass loss at 427 degrees C was approximately 12 percent, as measured by thermal gravimetric analysis (TGA).'

The flight crew were physically affected as a result of exposure to the fumes produced from the combustion of the failed diode on the master dim and test module.

Occurrence summary

Investigation number 200300029
Occurrence date 16/01/2003
Location Sydney, Aero.
State New South Wales
Report release date 02/11/2004
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Occurrence class Serious Incident
Highest injury level Minor

Aircraft details

Manufacturer The Boeing Company
Model 737
Registration VH-VBS
Serial number 30746
Sector Jet
Operation type Air Transport High Capacity
Departure point Sydney, NSW
Destination Melbourne, VIC
Damage Nil

Bell 206B (III), VH-AZH, collision with water, Bendora Dam, Australian Capital Territory, on 13 January 2003

Safety Action

Local safety action

The operator has amended the company's operations manual to correctly reflect the types of fire buckets used on the company's individual helicopter types.

The operator has standardised the position of the external load jettison switch on the different helicopter types used by the company in fire fighting operations.

The company's operations manual now details the type of safety clothing to be worn by pilots when engaged in water-bombing operations in company helicopters. The clothing specified includes the wearing of cotton or better, flying suits, approved helmets and comfortable fitting life jackets. Inflatable life jackets have been positioned in each helicopter for that purpose.

The operator has introduced a system for tracking the fitment and maintenance history of cargo hooks fitted to company helicopters.

ATSB safety action

In a briefing to the Civil Aviation Safety Authority, the ATSB drew attention to the fact that the occurrence bucket was not of standard manufacture, and highlighted the possible effects of the use of non-standard buckets by helicopters during fire fighting operations.

As a result of this occurrence, the Australian Transport Safety Bureau issues the following safety recommendations:

Recommendation R20030219

The Australian Transport Safety Bureau recommends that the Civil Aviation Safety Authority, in conjunction with the relevant industry associations, highlight the safety benefits to helicopter pilots and crew of the wearing of personal protective equipment, such as helmets and personal flotation devices when carrying out water-bombing in support of fire fighting operations, through safety promotion initiatives.

Recommendation R20030220

The Australian Transport Safety Bureau recommends that the Civil Aviation Safety Authority, in conjunction with the relevant industry associations, assess the desirability of a requirement for Helicopter Underwater Escape Training for specialist aerial work operations, such as water-bombing in support of fire fighting operations.

Recommendation R20030221

The Australian Transport Safety Bureau recommends that the Civil Aviation Safety Authority, in conjunction with the relevant industry associations, consider advising Australian helicopter operators involved in water-bombing in support of fire fighting operations, of the need to review the type of fire-buckets used to ensure that they comply with the bucket manufacturer's guidance for use on helicopter types and to ensure that the fire-buckets are appropriately maintained.

1 Issue Date: January 2003.
2 Issue Date: May 2002.

Related Documents: | Media Alert |

Analysis

The pilot was qualified and authorised and had recent experience for the operation.

The helicopter had sufficient fuel of the correct type on board for the flight. Rotational damage to the main rotor system and engine was consistent with engine operation at the time of impact.

The helicopter was at high all up weight and operating close to maximum predicted performance in an area with reported variable winds. While those conditions would have increased the risk of encountering LTE, the pilot was highly experienced in long-line and water-bombing operations and had been operating in the area of Bendora Dam for most of the day. That experience should have mitigated the risk that LTE was a factor in this occurrence.

Although of a non-standard construction, the occurrence bucket was assessed as being capable of normal operation, and was able to be carried by the helicopter at its post-accident assessed capacity. There was no evidence that it contributed to the accident.

While the manufacturer of the 'Bambi Bucket' warns of the possibility of dynamic rollover when conducting water-bombing operations, the use of a 24m long-line by the pilot, and vertical water pick-up would have diminished the likelihood for that to have occurred in this occurrence.

The investigation could not confirm the position of the cargo hook release circuit breaker prior to the accident. Had the circuit breaker been in the open-circuit position the rapid release of the bucket by the pilot, such as in an emergency situation requiring jettison of the load, would not have been possible.

The nature of the helicopter's impact with the water, and the resulting damage sustained by the pilot's helmet, reinforced the protective benefits of the use of flightcrew helmets.

It is possible that, during the water pick-up, the pilot may have been at a distance from the shoreline from which, had an engine failure occurred, the helicopter would not have been able to reach land. In that case, the provisions of CAO 20.11 would have applied, requiring the pilot to wear a PFD. That would have greatly eased the difficulty experienced by the helicopter crewman and others performing the rescue and, potentially, lessened the severity of the pilot's injuries.

Given the absence of pilot recollection and witness reports of the accident, and the lack of detailed indications of operation of the helicopter at impact, the reason(s) for the accident could not be established.

While recognising that, in this accident, the pilot was rendered unconscious and therefore unable to exit the helicopter without assistance, the ATSB draws attention to the benefits of HUET. Studies have shown that escape from helicopters involved in water accidents can take longer than the average time that a person can hold their breath. HUET has been shown to decrease exit times from an immersed helicopter, and increase the likelihood of a successful exit by an uninjured occupant. The provision of HUET to pilots, aircrew and passengers regularly operating over significant expanses of water would maximise the possibility for the successful exit of occupants from an immersed helicopter.

Summary

The Bell Helicopter Company, JetRanger III helicopter was engaged in water-bombing in support of fire fighting operations in the vicinity of Bendora Dam, about 37 km southwest of Canberra. A Bell 412 helicopter, with a pilot and crewman on board, was conducting water-bombing operations in conjunction with the JetRanger. An Aerospatiale A350 Squirrel helicopter had recently returned to the area of operations and was conducting a survey of the Bendora fire zone.

The pilots of the two water-bombing helicopters had seen each other as they passed on opposite legs of a racetrack pattern between the fire and the dam. As the Bell 412 returned to the dam for water pick-up, the pilot noted the absence of the JetRanger during that pattern. At about 1238 Eastern Standard Time, the Bell 412 pilot unsuccessfully attempted to contact the JetRanger pilot on the radio. A short time later, the pilot of the Bell 412 noticed the upturned fuselage of the JetRanger in the water. He immediately broadcast a PAN call, and contacted the Squirrel pilot to advise that the JetRanger was in the water.

The Bell 412 pilot released his water bucket on the shore of the dam and established a hover close to the upturned helicopter. The crewman entered the water and freed the unconscious pilot from the wreckage. The Squirrel arrived at the dam and landed on the shoreline and two of the occupants entered the water to assist the crewman, who was experiencing difficulty keeping the pilot afloat during the rescue. Once on the shore, the pilot was resuscitated before being transported to a Canberra hospital. There were no known witnesses to the accident.

The JetRanger helicopter was substantially damaged in the accident. Examination of the helicopter indicated impact with the water in a slightly right side down, nose-low attitude. Damage to the main and tail rotor systems indicated that both rotors had been under power when the helicopter impacted the water. Rotational damage to the engine compressor and turbine assemblies confirmed engine operation on impact with the water. Advice from the engine manufacturer indicated that the engine was probably producing above flight idle power at that time. There was no evidence of any pre-impact engine or other aircraft abnormality that would have contributed to the development of the occurrence.

A main rotor blade impacted the pilot's upper doorframe, and the right upper overhead window. There was also impact damage evident on the pilot's helmet, consistent with the helmet being struck either by the door frame structure or a main rotor blade.

An estimated 135 L (107 kg) of fuel was on board the helicopter at the time of the occurrence, which was sufficient for the planned flight. A sample of that fuel was sent to a laboratory in Melbourne, Victoria, for analysis. That analysis confirmed that the fuel was free from contamination and of the correct type. Along with a number of other helicopters, the JetRanger had been refuelling from a mobile tanker. None of the pilots of those helicopters reported any fuel-related problems during the day's operation.

The occurrence bucket attached to the JetRanger was placarded as a `Bambi Bucket' model 1012. The company operations manual did not list the 455 L capacity, 1012 model bucket for use and instead described the 545 L capacity, 1214 model bucket for use by company aircraft when conducting water-bombing operations. The bucket manufacturer left the choice of bucket for use when fire-bombing with the operator. However, the bucket manufacturer did not suggest either of the 1012 or 1214 buckets for use with the JetRanger. Instead, the manufacturer recommended use of the 410 L capacity, 9011 model bucket.

The bucket was attached to the JetRanger's cargo hook by a 24 m steel cable. Electrical wiring was fixed to the cable to allow operation of the water release mechanism by the pilot and, when required, to enable the addition of fire retardant foam. The cargo hook unit included a manual and electrical release, to enable pilot-activated release of the bucket and cable. The helicopter's cargo hook electrical release circuit breaker was found in the open-circuit position. As part of the investigation, the circuit breaker was reset and the cargo hook release was tested electrically and manually. While it could not be determined whether the as-found position of the circuit breaker resulted from pilot selection or the accident, both release mechanisms operated normally during subsequent testing.

An internal `cinching strap' controlled the volume of an `as-manufactured' `Bambi Bucket' via a series of metal `D' rings positioned along the length of the strap. That allowed selection of 70%, 80% or 90% of bucket capacity. Nylon webbing loops stitched to the inside of the collapsible synthetic bucket positioned the strap inside the bucket. The bucket strap fitted to the occurrence bucket was non-standard and did not include any `D' rings. Instead, the strap had been tied off with a knot. That was contrary to the bucket manufacturer's Repair Assessment Manual1 that stated that it was not an acceptable practice to tie knots on the strap. The manufacturer cautioned that such actions may result in a false indication of the actual maximum volume of water in the bucket. Following consultation with the bucket manufacturer, it was determined that the bucket was of a non-standard construction.

Examination of the occurrence bucket revealed that several of the nylon webbing loops had been torn from the inside of the bucket. The investigation was unable to determine when the webbing loops failed. The bucket's capacity was 420 L measured in the as-found condition. During that test it was noted that the `cinching' strap exerted no influence on the bucket's volume due to the torn webbing loops. Post accident testing of the bucket's electric water release mechanism was carried out utilising the helicopter's electrical system. That test revealed that the bucket's mechanism operated normally.

The JetRanger pilot held a current Commercial Pilot (Helicopter) License and a valid medical certificate. He had a total of 6,713 hours total flying experience, with in excess of 2,917 hours on type. He was appropriately endorsed for, and very experienced in, fire fighting and long-line operations. The pilot was reported to be medically fit for the flight.

The pilot sustained traumatic head injuries and was submerged for an undetermined period. During subsequent interviews he was unable to recall any details of the accident.

The all up weight for the helicopter, including the 420 L of water carried in the non-standard 1012 model bucket, was estimated to be about 3,309 lbs. The maximum take off all up weight for the ambient conditions was estimated to be about 3,320 lbs.

The helicopter's centre of gravity was estimated to have been within limits.

The Bureau of Meteorology forecast for the Bendora Dam area indicated an east-northeasterly wind at a speed of 15 kts. Other helicopter pilots operating in the area on the day reported winds that varied in direction and strength. Visibility was reported as `good', with some smoke in the area. The investigation was unable to determine the actual wind direction and speed at the time of the accident.

Federal Aviation Administration Advisory Circular AC90-95 described the conditions under which a loss of tail rotor effectiveness (LTE) can occur. Included among those conditions were: high all up weight; out of ground effect hover; low forward airspeed; high power settings; and a wind direction from the left or rear of the helicopter. LTE can result in a loss of control.

The `Bambi Bucket' Manufacturer's Operator's Manual2 warned pilots not to execute 90 degree pedal turns when the helicopter was close to the water and towing the bucket. That warning highlighted the danger of the bucket suspension lines becoming caught on the rear of a landing gear skid, resulting in a dynamic rollover when lifting the bucket. Federal Aviation Administration Advisory Circular AC 90-87 indicated that dynamic rollover normally occurred during slope landings and take-offs, with some degree of bank angle or side drift, with one skid in contact with the ground. In that case, the in-contact skid acted as a pivot point. If an excessive roll rate was permitted to develop around that pivot point, a critical bank angle could be reached where roll could not be corrected, even with full lateral cyclic. The helicopter would then roll over onto its side.

Other water-bombing pilots reported that, on previous sorties, the JetRanger pilot had been lowering the bucket vertically into the water to fill from an out of ground effect (OGE) hover, and then lifting it clear vertically before transitioning to forward flight. Underwater photographs of the helicopter showed that the bucket cable was not positioned over the rear of the skid assembly. Examination of the helicopter's landing gear skids did not reveal any damage from the bucket cable.

There was no system in place to track the fitment and maintenance of the company's cargo hooks.

Civil Aviation Order (CAO), 20.11, 5.1.1(a), stated that:

`Aircraft shall be equipped with one life jacket for each occupant when the aircraft is over water at a distance from land:
(a) in the case of a single engine aircraft - greater that that which would allow the aircraft to reach land with the engine inoperative...'

Para 5.1.7 of the CAO stated, in part:

`Where life jackets are required to be carried in accordance with subparagraph 5.1.1(a) each occupant shall wear a life jacket during flight over water...'

The pilot was reported to have been conducting his water pick-ups from close to the shoreline of the dam. The pilot was not wearing a personal flotation device (PFD) at the time of the accident.

A Flight Safety Foundation report - External Loads, Powerplant Problems and Obstacles Challenge Pilots During Aerial Fire Fighting Operations, based on USA accident reports from 1974 to 1998, stated in part:

`Research has shown that the average person, when immersed in cold water, can hold [their] breath for 17.2 seconds, plus or minus 3.7 seconds. Studies of water accidents involving military helicopters and civilian helicopters, however, show that successful underwater escape requires 40 seconds to 60 seconds'.

Helicopter underwater escape training (HUET) teaches pilots, other aircrew and passengers an instinctive escape procedure providing them with an improved chance of survival in the event of a helicopter ditching into water. The pilot reported that he had not undertaken HUET.

Occurrence summary

Investigation number 200300011
Occurrence date 13/01/2003
Location Bendora Dam
State Australian Capital Territory
Report release date 16/12/2003
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Collision with terrain
Occurrence class Accident
Highest injury level Serious

Aircraft details

Manufacturer Bell Helicopter Co
Model 206
Registration VH-AZH
Serial number 3075
Sector Helicopter
Operation type Aerial Work
Departure point Canberra, ACT
Destination Canberra, ACT
Damage Substantial

Fokker F27 MK 50, VH-FNA, Southern Cross (ALA), on 9 January 2003

Safety Action

Local safety action

As a result of its investigation, the operator has:

  • increased the frequency of maintenance inspections of the wiring on the main landing gear, including the junction boxes, and introduced a detailed inspection that includes removal of the junction box cover, inspection of the connections and resealing of the cover, and
  • amended the 'Loss of Cabin Pressure (Decompression)' section of the flight operations manual to require cabin crew to use portable oxygen for at least 30 seconds to one minute after flight crew advise that an aircraft has reached a safe altitude.

Analysis

When the seat belt sign illuminated, the cabin crew were unaware that the aircraft was in an emergency descent due to a loss of cabin pressure and continued cabin duties until the flight crew advised the reason for the descent. When advised that the aircraft had levelled out and it was safe to move about the cabin, the cabin crew continued duties without breathing the supplemental oxygen.

Oxygen deprivation can be insidious and cabin crew may not be the best judges of their own oxygen intake following decompression. Factors that may have contributed to the effects of mild hypoxia reported by the cabin crew include the continued physical activity during the initial descent, lack of intake of supplemental oxygen after the aircraft had levelled out and activity in the cabin during the remainder of the unpressurised flight.

Cabin crew performance can be critical during emergencies. If the cabin crew had used oxygen after the descent had been completed, it would have assisted in recovery from the effects of hypoxia. That use, in turn, would have provided some assurance that cabin crew were able to perform their duties appropriately in any subsequent emergency situation during the remainder of the flight.

Summary

The Fokker B.V. F27 MK 50 was maintaining flight level 250 (FL250), when the flight crew was alerted to a pressurisation problem by a triple chime, master caution and cabin altitude annunciation that indicated that the cabin altitude was climbing above 10,000ft. The normal cabin altitude for flight at FL250 was 8,000 ft. The flight crew donned oxygen masks and initiated the procedure for an emergency descent. That procedure included activation of the cabin fasten seat belt sign, broadcasting their intentions to air traffic control and commencing a descent at maximum speed with the engines at flight idle.

Cabin crew were alerted to a problem by the illumination of the fasten seat belt sign and a change in aircraft attitude. They advised passengers by the public address (PA) system to fasten their seat belts, then walked through the cabin to check compliance with the instruction. Shortly after, the flight crew used the interphone to advise the cabin crew of the loss of cabin pressure. The cabin crew made another PA to advise passengers of the situation and secured the galley before sitting in their crew seats.

The maximum altitude that the cabin attained during the descent, or how long the cabin was at that altitude, could not be determined. The pilot reported that the decompression was not rapid and the descent to a safe altitude was carried out with minimum delay.

The flight crew advised the cabin crew by interphone when a safe altitude had been reached. The cabin crew then checked the cabin safety and security for landing. The remainder of the flight was of short duration and was continued, with the aircraft unpressurised, at an altitude of 10,000 ft. None of the passengers or crew reported any injury or ear distress and supplemental bottled oxygen was not used during the flight. The cabin crew subsequently reported symptoms of mild hypoxia including the tingling of hands, feet and lips.

Emergency descent

The operator's operations manual states that if time permits, the captain should make a broadcast on the PA about the emergency descent.

The pilot reported that he alerted the cabin crew to the emergency descent by interphone instead of the PA, as he considered that the quality of PA transmissions could be affected by the wearing of a crew oxygen mask. As the passenger cabin was not equipped with drop down oxygen masks, he also considered that the flight crew's priority was to manage the descent to a safe altitude as quickly as possible.

Oxygen

Oxygen masks stowed beside their seats provided immediate emergency oxygen for the flight crew. Five portable oxygen bottles located in the cabin were available for use by the cabin crew and passengers, if required, when the aircraft had reached a safe altitude.

Cabin crew use of oxygen

Research conducted by the Civil Aeromedical Institute, Federal Aviation Administration (FAA), found that physical activity such as that performed by cabin crew will significantly shorten the time of useful consciousness during an aircraft decompression. Based on that research, the FAA's recommended procedure for cabin crew during a decompression was for them to immediately don the nearest oxygen mask, sit down or grasp a fixed object, and hold on in order to brace themselves until given clearance to move about the cabin by the flight crew.

The operator's flight operations manual loss of cabin pressure (decompression) procedure, 'Immediate Action for All Cabin Crew', required cabin crew to secure the bar/meal cart, sit down if a seat was available, or hold on securely to a rigid structure and, if near a PA handset, advise passengers to fasten their seat belts. The procedure also advised cabin crew to use portable (supplemental) oxygen themselves, if required, once the aircraft had reached a safe altitude. None of the cabin crew felt the need to use supplemental oxygen.

Electrical junction box

An electrical junction box on the right main landing gear oleo contained electrical wiring and connectors for the right main landing gear weight on wheels microswitch. The microswitch activates 12 different relays that are linked to avionics systems, warning and inhibit systems, the pressurisation system and engine ground controls.

A subsequent inspection by company engineers found that the junction box had been contaminated with moisture through inadequate sealing of the box cover following routine maintenance. The moisture ingestion led to spurious electrical signals being sent to the aircraft's pressurisation system, resulting in erratic cabin altitude control.

Occurrence summary

Investigation number 200300008
Occurrence date 09/01/2003
Location Southern Cross (ALA)
State Western Australia
Report release date 22/12/2003
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Air/pressurisation
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Fokker B.V.
Model F27
Registration VH-FNA
Serial number 20106
Sector Turboprop
Operation type Air Transport High Capacity
Departure point Perth, WA
Destination Kalgoorlie, WA
Damage Nil

Collision between steam passenger Train 8382 & Loaded B-double truck

Final report

Executive summary

The Victorian Minister for Transport, the Hon Peter Batchelor, MP requested the Australian Transport Safety Bureau (ATSB) to undertake an independent investigation into the collision between steam locomotive K183,and its consist, and a loaded 'B-double' truck at the Saleyards Road level crossing, Benalla.

The investigation was conducted in accordance with the provisions of the Transport Act 1983 (Victoria) as amended.

The Terms of Reference for the investigation were:

The Investigation will examine all relevant matters including:

  1. The immediate events leading to the collision, including determination of the relative contribution of rolling stock, infrastructure and operating procedures.
  2. Train maintenance systems.
  3. The track authority.
  4. Qualification,training and re-training procedures for relevant staff.
  5. Scheduling of train staff to heritage and special interest.
  6. Operating procedures and effectiveness of such procedures.
  7. Medical condition of the rail safety workers involved in the collision.
  8. Post collision emergency management arrangements and procedures.
  9. Conspicuity of the engine and tender.
  10. Any specific issues relating to the Saleyards Road crossing and its approaches.
  11. Final report format to follow the model Draft AS Guidelines for rail safety investigations.

At about 1250 on Sunday 13 October 2002 an historic steam passenger train, 8382 carrying a wedding party, collided with a fully loaded B-double flour truck on a railway level crossing at Benalla, Victoria.

The B-double truck did not give way and crossed the level crossing in the path of train 8382. The evidence to the investigation was that the B-double driver did not see the train until he was actually crossing the rail track. The train was so close that he did not have time to accelerate his vehicle clear. The probability is that the train crew had no reason to suppose that the B-double would not stop at the crossing and as the B-double started to cross the train crew could do nothing to avoid or mitigate the collision.

The train driver, fireman, and one footplate1 visitor on the locomotive were fatally injured. Another footplate visitor was seriously injured as a result of the collision. No other injuries were reported.

The collision occurred on the Saleyards Road railway level crossing located approximately 1.1 kilometres from Benalla township on the Benalla - Yarrawonga/Oaklands branch line. The level crossing was a passive crossing protected by 'give way' and other warning signs on the road approaches. As a result of the collision, locomotive K183 and tender, carriage DT319 (power supply van) and the leading bogie of carriage BK712 derailed.

The B-double truck was owned and operated by Greenfreight Pty Ltd based in Wodonga. The train was operated by West Coast Railway. The train locomotive was owned by the Victorian Government and managed by Steam Rail Victoria Inc based in Newport. The carriages from the train were owned and maintained by West Coast Railway.

After impact, the train locomotive left the tracks and ploughed into soft earth next to the railway line. The locomotive was tipped onto its side and the tender was pushed into the locomotive cabin. The tender also distorted the crew compartment roof shearing the bolts holding the boiler safety valve assembly. High pressure steam vented into the atmosphere and into the crew compartment.

In accordance with the Terms of Reference, the investigation was limited to factors directly affecting safe rail operation. Other factors directly involving the B-double truck do not form part of this report.

The train and track infrastructure and maintenance systems were found to be in operational condition and conducted in accordance with accepted procedures. The train was running on an appropriate track authority. The qualifications, training and re-training procedures were appropriate and had been followed. The scheduling of train staff was not a factor in the collision, though the report recommends a review of rostering for special trains by the Rail Tram and Bus Union, particularly crews in secondary employment. The medical condition of the rail safety workers involved met the required standard and no medical factors were implicated in the cause of the collision. Post collision emergency management and response procedures were effective and efficient.

The locomotive was displaying its headlight on high beam. The train was so close to the truck as they both approached the crossing, and was also sounding its whistle, it is not possible to determine what level of conspicuity, if any, would have alerted the B-double driver.

A number of factors were identified as being critical to safe railway operation at Saleyards level crossing. The level of protection at the Saleyards Road level crossing could be improved for heavy goods vehicles accessing Saleyards Road from the east. The sighting distance, based on a train speed of 80 kph, may be insufficient to allow a heavy goods vehicle to cross and clear the level crossing in safety.

Additionally, the risk assessment process used by VicRoads and the Benalla Rural City Council to determine the level of protection used at railway level crossings on approved B-double routes could be improved.

The investigation makes several safety recommendations to the Victorian Department of Infrastructure, VicRoads, Benalla Rural City Council, Freight Australia, West Coast Railway, Rail Tram and Bus Union, Standards Association of Australia, and the Victorian Level Crossing Committee. The recommendations relate to reviewing railway level crossings on B-double routes, footplate visitors, fatigue management, and Australian Standards. One review should encompass level crossing protection treatments and include any significant changes such as traffic flow and type, speed and vegetation. The active involvement of the rail industry in level crossing issues is also recommended. A community education programme is recommended to address the dangers of railway level crossings to road and pedestrian users.

Additional recommendations include consideration of the type of road and rail traffic as part of the Australian Standard for level crossing protection.

For copies and enquiries of the report please contact the Victorian Department of Infrastructure, Public Affairs Division. Telephone (03) 9655 6263.

  1. Footplate refers to the locomotive cabin of a steam locomotive.

Occurrence summary

Investigation number 2002003
Occurrence date 13/10/2002
Location Benalla
Report release date 23/02/2006
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Rail
Rail occurrence category Collision
Occurrence class Incident
Highest injury level Fatal

Train details

Train number 8382
Type of operation Passenger
Departure point Yarrawonga
Destination Melbourne
Train damage Substantial

Collision between the passenger train 5AL8 and vehicles at the Salisbury Interchange level crossing, Salisbury, South Australia, on 24 October 2002

Final report

Executive summary

At 15:33:01 on 24 October 2002 passenger train 5AL8 collided with a car and scheduled bus on the Salisbury Interchange controlled level crossing on Park Terrace. As a result of the accident four people were killed and 26 injured. A small sedan car and the bus were effectively destroyed. In addition two other road vehicles were damaged. The locomotive and the first vehicle of the consist sustained minor damage. There was no derailment of any rail vehicles.

The standard gauge track owned and operated by ARTC, runs parallel to two broad gauge tracks operated by TransAdelaide. These three tracks share the northern rail corridor, which runs through Salisbury.

As train 5AL8 approached the level crossing on Park Terrace from Adelaide, the driver and co-driver saw stationary road vehicles across the standard gauge track. The driver of the locomotive acted promptly in sounding a sustained warning on the horn, applying the emergency brakes and putting the throttle to idle. Two cars reversed clear of the track to a position between the standard gauge and the TransAdelaide tracks. The small sedan and the bus were unable to move because of other vehicles, though the driver of the sedan managed to jump out of her car and run clear.

The sighting distance from the train cab to the standard gauge crossing was approximately 250 m. The train could not stop in time to prevent the collision and came to a halt 183 m to the north of the Park Terrace level crossing.

The report concludes that the locomotive, rolling stock, rail, signalling infrastructure and the boom gate barriers at the crossing, up to the time of the collision, were in good condition and operated as designed.

Prima facie the road vehicles stationary on the rail tracks had entered the crossing when the drivers could not drive through the crossing because the crossing, or road beyond the crossing, was blocked. On this view the immediate causal factor was the non-observance of the Australian Road Rules 1999. From a systemic point of view, however, the accident was more complex with a number of causal factors relating to:

  • road design (the number of entry/exit points);
     
  • road traffic lights and the inter-link with the level crossing warning system;
     
  • the width of the crossing;
     
  • probable lack of awareness by road vehicle drivers of the road traffic rules as they relate to level crossings;
     
  • the lack of 'near hit safety' reporting at level crossings;
     
  • the lack of a focused body to oversight and undertake risk based assessments of level crossing safety.

The investigation found little evidence from records that Park Terrace level crossing was of public concern from a rail safety perspective. There were recorded concerns and direct observation that, when the traffic lights at the Salisbury Highway intersection were red, traffic did, on occasions, queue over the Park Terrace crossing. On the basis of direct observation, such an accident at Park Terrace was foreseeable.

The response to the accident by the emergency services and railway companies was timely. The first emergency persons to respond crawled beneath train 5AL8, a dangerous but understandable reaction to reach the injured. Police established tight control at the level crossing, but commuters and onlookers were able to access the adjacent lengths of track although the TransAdelaide passenger service continued running.

The report details 13 key conclusions:

  1. The immediate cause of the collision between train 5AL8, the white Nova Holden WOJ 601 and Serco bus number 246 (VYV 786) was that the drivers of the road vehicles entered the level crossing, in contravention of the Australian Road Rules, at a time when they were unable to drive through the crossing and were blocked by other vehicles.
     
  2. The driver and co-driver of locomotive NR 34, reacted promptly in sounding a warning of train 5AL8, applying emergency brakes and returning the throttle to idle. Neither the driver nor the co-driver could have taken any action that would have prevented the collision with the white Holden Nova or Serco bus number 246 (VYV 786) operating the 401 service.
     
  3. Locomotive NR 34 and the 25 vehicles of the consist comprising train 5AL8 were in working order, were properly maintained and were fit for purpose. There were no deficiencies in the consist that contributed to the collision.
     
  4. The railway infrastructure (track circuitry, signals, level crossing warning signals and the boom barrier) worked as designed within standard time limits.
     
  5. Following the collision, the on train staff servicing the passenger vehicles of train 5AL8 acted promptly to assist the injured at the scene of the accident until they were able to relinquish care to the emergency services.
     
  6. The response of the emergency services was timely.
     
  7. The road traffic lights at the junction of Park Terrace, Gawler Street, North Lane and the Bus Interchange and the link with the level crossing warning signals worked as designed.
     
  8. The road traffic signals at the Salisbury Highway/Park terrace intersection did not work as designed or as recommended by Australian Standard AS1742.14, in that the link with the railway crossing had been broken at some time and the special queue-clearing phase was not operational. There was no effective maintenance or checking system in place to monitor the continuing operation of the queuing phase of the lights and the links with the traffic Control Centre. The non-operation of the special queuing phase was probably not a significant factor in the collision of 24 October.
     
  9. The road traffic on the western side of the level crossing for traffic crossing Salisbury Highway or turning onto Salisbury Highway was halted at the traffic signals causing traffic to back-up over the level crossing.
     
  10. The backing up of westbound traffic across some part of the level crossing was not unusual and had become an accepted factor of driving in Park Terrace.
     
  11. The complexity of the Park Terrace road system over a distance of 175 m from the bus interchange turning just east of the level crossing to the stop line at Salisbury Highway, increased the probability of road vehicles backing up to the level crossing in that:

    - Road vehicles exiting or entering the Station car park and crossing or from the outside westbound lane, right turn lane, or attempting to enter the eastbound lane potentially restrict traffic flow.

    - Road vehicles exiting or entering the Eureka Tavern car park across the traffic.

    - Heavy traffic southbound on the Salisbury Highway restricts the opportunity for traffic in the left turn lane to join the Salisbury Highway.
     
  12. Based on observed behaviour of road vehicle drivers, a collision between traffic queued at Park Terrace and a train was foreseeable. However, the absence of any specific reports of near miss incidents or accidents between trains and vehicles at Park Terrace had led to a belief that there was no significant risk.
     
  13. The lack of initial site control following the collision and during the immediate emergency phase increased the risk of pedestrian onlookers being struck by trains, either through any possible movement of train 5AL8 or the TransAdelaide services.

The Salisbury level crossing review report by Mr Vince Graham of January 2003 made a number of recommendations (attachment 2), which are endorsed by this report. Mr Graham also made interim recommendations in early November that the track speed 500 m on either side of Park Terrace should be limited to 50 km/h. This report recommends that train speed restrictions introduced as a safety measure in the vicinity of level crossings should be further reviewed taking into account the new traffic arrangements and safety measures and the different types and characteristics of trains on the standard and broad gauge tracks.

In addition the report recommends:

RR20030001
Road traffic signals adjacent to level crossings be regularly monitored to ensure that all links and functions within the system are operational.

RR20030002
Traffic flows through Park Terrace should be measured to assess the practicality of extending the timing on a link to force westbound traffic from Park Terrace to take account of the worst case timing scenario, while maintaining the existing timing of the boom barrier closing.

RR20030004
The rail industry should attempt to devise a confidential hazard reporting system that embraces the whole industry in the one system.

RR20030005
ARTC and TransAdelaide review their notification and communication procedures when responding to accidents on the shared rail corridor, particularly between the train control centres and the accident site.

RR20030006
The rail companies and emergency services examine ways in which early effective site control and control of public access might be further improved.

RR.20030007
Standards Australia develop a standard for the marking of a 'do not enter unless clear' area across level crossings, with a view to providing appropriate cues to help road vehicle drivers assess the space available on the other side of the crossing.

RR20030008
Transport SA should review the provisions of the Road Traffic Regulations 1996 to determine whether or not any existing penalty
covering the drivers of vehicles that stop or park within the boundary of rail level crossings is appropriate.

Note: This investigation was undertaken by the ATSB on behalf of the State Government of South Australia. Media enquiries should be directed to the SA Government's media contact, Emma Brown (08) 8204 8261.

Occurrence summary

Investigation number 2002/002
Occurrence date 24/10/2002
Location Salisbury
State South Australia
Report release date 11/03/2003
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Rail
Occurrence class Accident
Highest injury level Fatal

Collision between suburban electric passenger train 1648 and suburban electric empty train 1025

Final report

Executive summary

At about 0914 on Tuesday 18 June 2002 a scheduled suburban electric passenger train number 1648, on an up journey, collided with an approaching scheduled suburban electric empty train number 1025, on a down journey, on a section of single line, 772.3 metres south of Epping Railway station. Passenger train 1648 had a driver and 16 passengers on board, while the empty train 1025 had a driver and two other drivers travelling as passengers with the train. Train 1025 was traversing a single line section and crossing into Epping Yard at the time of the collision. The leading cab on train 1025 had just traversed a set of points and passed the fouling point for both the main line and the crossover line into Epping Yard, moments prior to the collision. Train 1648 had departed Epping platform and was advanced into the single line section on a restricted indication, and had subsequently passed signal EPP121 that was indicating stop. Both trains and infrastructure, including signalling and tracks, were operated by Melbourne Transport Enterprises, through Connex Trains Melbourne (CTM) and Alstom Melbourne Transport Limited (AMTL).

Damaged passenger train

Emergency services, including the Police, Fire and Ambulance services attended the scene. The driver of the passenger train suffered bruising to his right upper arm, but was discharged from hospital on the day of the collision. Minor injuries to passengers were reported. No passengers were hospitalised.

The evidence available, including an expert medical assessment, suggests that the driver of train 1648's performance was impaired by his physically 'unwell' condition. He could not recall events between the departure from Epping station on the up journey and the point that the train passed signal EPP121 at stop, a period of about one minute. As a result, signal EPP121 was passed at stop and a collision occurred. Train 1648 was travelling at about 60 km/h and train 1025 at about 12 km/h, at the point of initial impact.

Signal distances at Epping

Diagram showing Epping Yard signal distances

 

There are safeguards or defences to protect against such an accident. On this occasion the defences in place failed to prevent the accident. A number of defences were identified as being inadequate in terms of design or application.

The investigation established that train maintenance was not a factor in the accident. In addition, the signalling system, which incorporates automatic train stops, operated within its design criteria. However, the design criteria of the signalling system was such that it could not maintain a minimum safety margin to prevent the collision, given the speed of the passenger train involved.

Trains are fitted with pilot valves (including a dead man's handle), so that in the event that a driver becomes incapacitated the train should be brought to a halt. On this occasion the driver of train 1648 had become incapacitated but the pilot valve did not activate by applying the train's emergency brakes.

The performance of the driver of train 1648 was impaired by migraine symptoms, and possibly treatment, and the effect of stressful personal circumstances. The driver's history of migraine had been declared during regular medical assessments but the medical guidelines did not address the symptoms or treatment for a potentially incapacitating illness. The report also addresses factors that contribute to the driver working when he was unwell.

The Investigation Team has also reviewed the factors surrounding the Footscray collision on 5 June 2001 (ATSB rail investigation report no. 11-01) and considers this event to contain some similar safety issues.

A number of safety actions have been taken or are underway through the Victorian Department of Infrastructure.

The report's recommendations on pages 41 and 42 relate to:

  • the design of the signalling system;
  • the train working procedures for trains operating on single line sections of track;
  • the medical fitness/assessment guidelines;
  • the medical conditions that can impair or incapacitate a train driver;
  • driver sign-on procedures;
  • sick leave policy;
  • emergency procedures; and
  • recommendations contained in the ATSB Footscray investigation report.

Copies of the report are available from the Director Public Transport Safety, Victorian Department of Infrastructure, Plaza Level, 80 Collins Street, Melbourne or by telephoning (03) 9655 6402.

Occurrence summary

Investigation number 2002/001
Occurrence date 18/06/2002
Location Epping
State New South Wales
Report release date 25/07/2003
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Rail
Occurrence class Accident
Highest injury level Serious

Wharf contact by Sofrana Magellan

Summary

Investigation discontinued.

Occurrence summary

Investigation number 187
Occurrence date 01/11/2002
Location Brisbane
Report status Final
Investigation type Occurrence Investigation
Investigation status Discontinued
Mode of transport Marine
Marine occurrence category Contact
Occurrence class Incident
Highest injury level None

Ship details

Name Sofrana Magellan
IMO number 8513443
Ship type Container
Flag A & B
Destination Brisbane

Lifeboat incident on board Hong Kong flag bulk carrier Ma Cho

Final report

Summary

On 8 December 2002, Ma Cho arrived in Devonport, Tasmania, to discharge a part cargo of fertiliser at number four berth on the western side of the river.

On 9 December, the master made the decision to conduct an abandon ship drill before the vessel was due to depart for Geelong. The drill commenced at about 1540 and the starboard lifeboat was prepared for lowering to the water.

At approximately 1548 the mate reported that the crew inside the lifeboat were seated and had fastened their safety belts. Lowering of the boat then commenced with one of the crew operating the davit winch brake from the deck. When the boat had been lowered approximately two metres from the davit head the after on-load release hook suddenly opened, releasing the after fall. The lifeboat's stern fell to leave the boat suspended vertically by the remaining forward fall with its stern swinging approximately five metres above the water. The boat crew were shaken by the incident but remained secured in their seats inside the now vertical lifeboat. The second mate had sustained a small cut over his left eye.

After the crew had disembarked, the lifeboat was lowered to the water to allow the on-load release system to be inspected. It was found that the cable operating the after hook was not properly secured by the saddle clamp under the operating unit. Each time the actuating handle was operated, lost motion was induced by the cable sliding through the clamp and this meant that the after hook was not resetting fully. The cable clamp was temporary repaired and then the lifeboat was housed in its davit. Ma Cho was subsequently cleared to complete the voyage to Geelong.

The report conclusions include:

  • The cable clamp securing the aft hook's operating cable adjacent to the operating mechanism had been modified which resulted in lost motion within the cable.
  • As a result of the lost motion in its operating cable, the after hook had not been fully reset when the previous lifeboat drill was conducted on 2 November 2002.
  • The design of the on-load release system was flawed with respect to the hook locking mechanism.
  • The ship's safety management system was deficient with respect to both the operating and maintenance instructions and to crew training on the on-load release system.

The report makes a general recommendation to ISM Code accreditation authorities regarding ship safety management systems as they relate to on-load release systems. The report also recommends that the lifeboat manufacturer and classification societies review the design of the on-load release system.

Occurrence summary

Investigation number 188
Occurrence date 09/12/2002
Location Devonport
State Tasmania
Report release date 30/06/2004
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Marine
Marine occurrence category Lifeboat
Occurrence class Incident
Highest injury level Minor

Ship details

Name Ma Cho
IMO number 9118252
Ship type Bulk Carrier
Flag Hong Kong
Departure point Davenport, Tas

Equipment failure on board Australian registered bulk carrier Goliath

Final report

Executive summary

On 22 September 2002 the catastrophic failure of the main engine turbocharger disabled the cement carrier Goliath in Bass Strait. The replacement turbocharger failed in a similar manner on 12 February 2003, only four and a half months later, when Goliath was off Jervis Bay, again disabling the ship.

At 0107 on 22 September 2002, the Australian flag bulk cement carrier Goliath experienced a main engine turbocharger failure while the vessel was en route from Newcastle to Devonport when the turbocharger 'exploded' and disabled the ship's main engine.

At 1543 on 12 February 2003, while Goliath was en route from Devonport to Sydney, the turbocharger failed again. This time, the failure was witnessed by the second engineer who heard the rapid acceleration of the turbocharger before it exploded. Once again, the turbocharger had been damaged beyond repair and the ship was disabled.

The investigation report concludes that both turbocharger failures were similar and had occurred when the compressor discs burst due to overspeed. While it is not possible to state with certainty, the most likely mechanism leading to both overspeeds was a scavenge fire in the engine.

The ATSB delayed the release of these final investigation reports because of litigation involving the parties and because the investigations preceded and were not protected under the Transport Safety Investigation Act 2003.

Occurrence summary

Investigation number 186
Occurrence date 22/09/2002
Location Bass Strait
State Victoria
Report release date 21/06/2006
Report status Final
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Marine
Marine occurrence category Equipment
Occurrence class Incident
Highest injury level None

Ship details

Name Goliath
IMO number 9036430
Ship type Bulk carrier
Flag Australia
Departure point N/A
Destination N/A