Cabin fire involving Airbus A320-232, abeam Cooma, New South Wales, on 18 February 2018

Brief

Occurrence Briefs are concise reports that detail the facts surrounding a transport safety occurrence, as received in the initial notification and any follow-up enquiries. They provide an opportunity to share safety messages in the absence of an investigation.

What happened

On 18 February 2018, an Airbus A320-232 departed Melbourne, Victoria (Vic.) on a scheduled passenger flight to Sydney, New South Wales (NSW). At about 0915 Eastern Daylight-saving Time (EDT), cabin crew were alerted to a fire in the cabin.

The cabin crew traced the source of the fire to three smartphone devices located in a passenger bag at row five. The crew subsequently discharged a fire extinguisher and followed the operator’s procedure for the management of a lithium battery fire. The fire was successfully extinguished, and the devices isolated in a container until the end of the flight.

Safety message

Personal electronic devices (PEDs) such as smartphones contain lithium batteries, which are classed as dangerous goods. The incidence of passenger smartphones resulting in fire on board aircraft has increased. The Civil Aviation Safety Authority (CASA) has published advice on the ‘Least wanted dangerous goods’ carried by passengers. Lost or damaged smartphones were identified as the number one hazardous item on passenger aircraft in 2017. Previous Australian Transport Safety Bureau (ATSB) investigations AO-2016-051 and AO-2016-066 provide further examples of incidents of passenger smartphones causing in-flight fires and smoke events.

This incident highlights the need for passengers to become familiar with the hazards associated with the carriage of personal electronic devices, in particular, the potential for fire if a device is damaged or overheated.

Fire on board aircraft is potentially catastrophic if not managed quickly and appropriately. It is important for operators to ensure crew receive training and are periodically tested in the management of lithium battery fires on board aircraft.

About this report

Decisions regarding whether to conduct an investigation, and the scope of an investigation, are based on many factors, including the level of safety benefit likely to be obtained from an investigation. For this occurrence, no investigation has been conducted and the ATSB did not verify the accuracy of the information. A brief description has been written using information supplied in the notification and any follow-up information in order to produce a short summary report, and allow for greater industry awareness of potential safety issues and possible safety actions.

Occurrence summary

Mode of transport Aviation
Occurrence ID AB-2018-022
Occurrence date 18/02/2018
Location Abeam Cooma
State New South Wales
Occurrence class Incident
Aviation occurrence category Fire
Highest injury level None
Brief release date 28/03/2018

Aircraft details

Manufacturer Airbus
Model A320-222
Sector Jet
Operation type Air Transport High Capacity
Damage Nil

Separation issue involving Aero Commander 500-U and Mooney Aircraft Corp M20J, 28 km south-south-west of Bourke, New South Wales, on 18 January 2018

Brief

Occurrence Briefs are concise reports that detail the facts surrounding a transport safety occurrence, as received in the initial notification and any follow-up enquiries. They provide an opportunity to share safety messages in the absence of an investigation.

What happened

On 18 January 2018, an Aero Commander 500-U departed Cobar, New South Wales (NSW), for Charleville, Queensland (Qld). Another aircraft, Mooney M20J, was also airborne at the same time, flying from Broken Hill, NSW, to Archerfield, Qld.

During cruise at 8,500 ft, the pilot of the 500-U observed traffic on their electronic flight bag (EFB) application in their 10 o’clock position at 10 NM. The EFB application indicated the traffic was within 200 ft of the 500-U’s altitude. The pilot of the 500-U reported that the application displayed the relative positions of the two aircraft remained constant and the distance between them was reducing.

The pilot of the 500-U initiated contact with the crew of the M20J, resulting in the M20J descending to 7,500 ft. Two minutes later, the 500-U pilot observed the M20J passing directly underneath, crossing their track at almost 90 degrees.

Airspace

The aircraft passed each other in Class G airspace. Class G airspace is non-controlled airspace in which IFR[1] and VFR[2] aircraft are permitted to operate without a clearance. There is no air traffic control separation service in Class G airspace.

Weather

The pilot of the 500-U reported that a grey haze prevented sighting the M20J until it passed directly underneath.

Safety message

This occurrence highlights the importance of following the altitude requirements for VFR flight (see Figure 1) in uncontrolled airspace. This is especially significant when considering the limitations discussed in the ATSB research report Limitations of the See-and-Avoid Principle.

Figure 1: Table of VFR cruising levels

Table of VFR cruising levels.  Source: Aeronautical Information Publication Australia

Source: Aeronautical Information Publication Australia

It also highlights the importance of monitoring area frequency for potential traffic and that electronic aids can be used as a supplementary tool that may enhance maintaining situational awareness.

About this report

Decisions regarding whether to conduct an investigation, and the scope of an investigation, are based on many factors, including the level of safety benefit likely to be obtained from an investigation. For this occurrence, no investigation has been conducted and the ATSB did not verify the accuracy of the information. A brief description has been written using information supplied in the notification and any follow-up information in order to produce a short summary report, and allow for greater industry awareness of potential safety issues and possible safety actions.

__________

  1. Instrument flight rules (IFR): a set of regulations that permit the pilot to operate an aircraft in instrument meteorological conditions (IMC), which have much lower weather minimums than visual flight rules (VFR). Procedures and training are significantly more complex as a pilot must demonstrate competency in IMC conditions while controlling the aircraft solely by reference to instruments. IFR-capable aircraft have greater equipment and maintenance requirements.
  2. Visual flight rules (VFR): a set of regulations that permit a pilot to operate an aircraft only in weather conditions generally clear enough to allow the pilot to see where the aircraft is going.

Occurrence summary

Mode of transport Aviation
Occurrence ID AB-2018-010
Occurrence date 18/01/2018
Location 28 km SSW Bourke
State New South Wales
Occurrence class Incident
Aviation occurrence category Separation issue
Highest injury level None
Brief release date 28/03/2018

Aircraft details

Manufacturer Aero Commander
Model 500-U
Sector Piston
Operation type Private
Damage Nil

Aircraft details

Manufacturer Mooney Aircraft Corp
Model M20J
Sector Piston
Operation type Private
Damage Nil

In-flight engine fire involving Fairchild Industries SA227-DC, Ballina, New South Wales, on 7 January 2018

Brief

Occurrence Briefs are concise reports that detail the facts surrounding a transport safety occurrence, as received in the initial notification and any follow-up enquiries. They provide an opportunity to share safety messages in the absence of an investigation.

What happened

On 7 January 2018, at about 1327 Eastern Daylight-saving Time (EDT), a Fairchild Industries Inc. SA227-DC was conducting training exercises in the circuit area at Ballina, New South Wales, with two crew on board. While on the downwind leg of the circuit, the crew noticed the right engine fire warning light had illuminated on the warning panel. The warning light went out as the crew were about to commence the memory items required for an engine fire warning, and the approach and landing were completed normally.

After parking and shutting the aircraft down, the crew identified smoke stains on the cowls of the right engine. Further inspection revealed evidence of a fire on the upper rear section of the engine. The aircraft was subsequently grounded pending a maintenance inspection.

Maintenance engineers identified a fuel leak from the manifold had ignited resulting in damage to the fuel lines and associated fittings and controls in the immediate vicinity (Figure 1). All damaged parts were replaced and tested prior to the aircraft being returned to service.

Figure 1: Pictures of fire damaged components within the right engine bay

Pictures of fire damaged components within the right engine bay. Source: Operator

Source: Operator

Safety action

As a result of this occurrence, the operator has advised the ATSB that they have taken the following safety action.

Inspections have been completed on all aircraft in the fleet with no other potential fuel system faults identified.

Safety message

This incident highlights the importance of flight crews maintaining awareness of all system states and being prepared to act at the first sign of trouble. A fire during flight has the potential to rapidly propagate unless it is quickly identified and managed, and the aircraft landed at the earliest opportunity.

About this report

Decisions regarding whether to conduct an investigation, and the scope of an investigation, are based on many factors, including the level of safety benefit likely to be obtained from an investigation. For this occurrence, no investigation has been conducted and the ATSB did not verify the accuracy of the information. A brief description has been written using information supplied in the notification and any follow-up information in order to produce a short summary report, and allow for greater industry awareness of potential safety issues and possible safety actions.

Occurrence summary

Mode of transport Aviation
Occurrence ID AB-2018-004
Occurrence date 07/01/2018
Location Ballina
State New South Wales
Occurrence class Serious Incident
Aviation occurrence category Fire
Highest injury level None
Brief release date 28/03/2018

Aircraft details

Manufacturer Fairchild Industries Inc
Model SA227-DC
Sector Turboprop
Operation type Flying Training
Damage Minor

VFR into IMC involving Piper, PA-28R, near Sunshine Coast Airport, Queensland, on 22 February 2018

Brief

Occurrence Briefs are concise reports that detail the facts surrounding a transport safety occurrence, as received in the initial notification and any follow-up enquiries. They provide an opportunity to share safety messages in the absence of an investigation.

What happened

On 22 February 2018, a Piper PA-28R departed from a local aerodrome to travel to Sunshine Coast Airport, Queensland (Qld). The weather at the time included rain showers, low cloud and reduced visibility. Approaching the airport, the pilot progressively descended the aircraft to remain clear of cloud.

Air traffic control (ATC) advised the pilot that further adverse weather was approaching the airport and provided options to divert to a suitable landing area. The pilot elected to continue, arriving into the circuit at low level in deteriorating weather conditions.

ATC issued a ‘check gear down’ warning to the aircraft shortly before being unable to maintain visual contact with the aircraft in the circuit.[1] Air traffic controllers further issued a ‘Safety Alert, Terrain’[2] call as the aircraft manoeuvred to the north of the airport in the proximity of Mt Coolum (682ft). Air traffic control regained visual contact with the aircraft on short final.

The pilot reported that approaching the airport in the reduced visibility, he relied upon vertical visual contact with the ground to maintain his situational awareness when the horizontal visibility deteriorated. The pilot also stated that he was familiar with the local area and carried two Garmin GPS[3] and two iPads with planning and navigation software.

Figure 1: Sunshine Coast Airport proximity to Mt Coolum, Qld

Figure 1: Sunshine Coast Airport proximity to Mt Coolum, Qld

Source: Google Earth Pro Image 31 October 2017 with ATSB annotations

Visual Meteorological Conditions (VMC) requirements

Table 1: VMC criteria for aeroplanes below 3,000ft above mean sea level

Class of AirspaceFlight VisibilityVertical and Horizontal distance from cloudConditions
Class G (Uncontrolled) or within 1,000 ft of ground5,000MClear of cloud and in sight of ground or waterRadio must be carried and used on the appropriate frequency
Class D (Controlled)5,000M

600M horizontal 1,000FT vertically above cloud

Or 500FT vertically below cloud

ATC may permit operations in weather conditions that do not meet these criteria

(Special VFR).

Source: Aeronautical Information Publication (AIP) Australia: ENR 1.2-4 10 November 2016

Safety message

Pilots are encouraged to make conservative decisions when considering how forecast weather may affect their flight. If poor weather is encountered en-route, timely and conservative decision making may be critical to a safe outcome.

VFR[4] pilots are also encouraged to familiarise themselves with the definition of VMC criteria, and carefully consider available options where forecast or actual conditions are such that continued flight in VMC cannot be assured.

The ATSB SafetyWatch highlights the broad safety concerns that come out of our investigation findings and from the occurrence data reported to us by industry.

The ATSB SafetyWatch highlights the broad safety concerns that come out of our investigation findings and from the occurrence data reported to us by industry.

Flying with reduced visual cues and Inflight decision making such as in this occurrence remains one of the ATSB’s major safety concerns.

Number 4 in the Avoidable Accident series published by the ATSB titled ‘Accidents involving pilots in Instrument Meteorological Conditions’ lists three key messages for pilots:

  • Avoiding deteriorating weather or IMC[5] requires thorough pre-flight planning, having alternate plans in case of an unexpected deterioration in the weather, and making timely decisions to turn back or divert.
  • Pressing on into IMC conditions with no instrument rating carries a significant risk of severe spatial disorientation due to powerful and misleading orientation sensations in the absence of visual cues. Disorientation can affect any pilot, no matter what their level of experience.
  • VFR pilots are encouraged to use a ‘personal minimums’ checklist to help control and manage flight risks through identifying risk factors that include marginal weather conditions.

About this report

Decisions regarding whether to conduct an investigation, and the scope of an investigation, are based on many factors, including the level of safety benefit likely to be obtained from an investigation. For this occurrence, no investigation has been conducted and the ATSB did not verify the accuracy of the information. A brief description has been written using information supplied in the notification and any follow-up information in order to produce a short summary report, and allow for greater industry awareness of potential safety issues and possible safety actions.

__________

  1. A standard path normally flown within 3nm (5.5 km) by aircraft when taking off and landing at an airport
  2. Air traffic control will issue a ‘Safety Alert, Terrain’ to aircraft, when they become aware that an aircraft is in a situation that is considered to place it in an unsafe proximity to terrain along its intended flight path
  3. Global Positioning System
  4. Visual Flight Rules
  5. Instrument meteorological conditions (IMC): weather conditions that require pilots to fly primarily by reference to instruments, and therefore under Instrument Flight Rules (IFR), rather than by outside visual reference. Typically, this means flying in cloud or limited visibility.

Occurrence summary

Mode of transport Aviation
Occurrence ID AB-2018-021
Occurrence date 22/02/2018
Location 9 km S Sunshine Coast, Airport
State Queensland
Occurrence class Serious Incident
Aviation occurrence category VFR into IMC
Highest injury level None
Brief release date 28/03/2018

Aircraft details

Manufacturer Piper Aircraft Corp
Model PA-28R
Sector Piston
Operation type General Aviation
Damage Nil

Engine Failure involving Cessna 152, Lake Walyungup, Western Australia, on 7 January 2018

Brief

Occurrence Briefs are concise reports that detail the facts surrounding a transport safety occurrence, as received in the initial notification and any follow-up enquiries. They provide an opportunity to share safety messages in the absence of an investigation.

What happened

On 7 January 2018, the pilot of the Cessna 152 departed Jandakot, Western Australia (WA) to conduct aerobatics. The pilot was the only occupant.

At approximately 1412 Western Standard Time (WST) following an aerobatic-loop, the pilot applied power and the engine failed to accelerate. The pilot completed the emergency checklist, but the engine would not accelerate beyond 1900 RPM. The pilot searched for a suitable landing area, finding Lake Walyungup to be suitable. The pilot then made a PAN-PAN and later a MAYDAY radio transmission. The pilot conducted a successful forced landing on the dry surface of the lake.

The aircraft did not sustain any damage as a result of the landing. The post-flight inspection revealed the carburettor to be the cause of the failure. Metal contamination was detected in the carburettor which was likely disturbed during the aerobatics resulting in the partial engine failure. The source of the contaminants could not be identified.

Safety message

Simulated total loss of power and a subsequent practice forced landing is at the core of a pilot’s emergency training. However, data shows that for light single-engine aircraft a partial power loss is three times more likely to occur than a complete engine failure.

Following the partial engine failure, the pilot in this occurrence had to make important decisions in a short space of time, where to land and how to manage the remaining altitude. The ATSB’s publication and YouTube video ‘Managing partial power loss after take-off in single-engine aircraft’ is available on the ATSB website.

About this report

Decisions regarding whether to conduct an investigation, and the scope of an investigation, are based on many factors, including the level of safety benefit likely to be obtained from an investigation. For this occurrence, no investigation has been conducted and the ATSB did not verify the accuracy of the information. A brief description has been written using information supplied in the notification and any follow-up information in order to produce a short summary report, and allow for greater industry awareness of potential safety issues and possible safety actions.

Occurrence summary

Mode of transport Aviation
Occurrence ID AB-2018-003
Occurrence date 07/01/2018
Location 30 km SW from Jandakot
State Western Australia
Highest injury level None
Brief release date 28/03/2018

Aircraft details

Manufacturer Cessna Aircraft Company
Model 152
Sector Piston
Operation type Private
Departure point Jandakot, WA
Damage Nil

Collision with terrain involving Robinson R22 helicopter, 38 km south-west of Tindal Airport, Northern Territory, on 4 January 2018

Brief

Occurrence Briefs are concise reports that detail the facts surrounding a transport safety occurrence, as received in the initial notification and any follow-up enquiries. They provide an opportunity to share safety messages in the absence of an investigation.

What happened

On 4 January 2018, at about 0900 Central Daylight-saving Time (CDT), a Robinson R22 helicopter departed from a private property in Katherine, Northern Territory. The pilot, who was the sole occupant, was conducting a private flight to obtain GPS coordinates of structures on a property 38 km south-west of Tindal, NT.

The pilot landed the helicopter alongside a fence line in long grass. The pilot remained in the helicopter, with the engine running and obtained coordinates as required. The pilot then manoeuvred the helicopter into a low hover and with the breeze coming from the north-east, commenced to move out of the hover and felt the helicopter move to translational lift.[1] The pilot lifted the power to maximum take-off while easing the cyclic[2] forward to take advantage of the headwind.

As the helicopter straightened, about 3 ft above ground level (AGL), it dipped suddenly, pivoting on the front left-hand skid. The pilot attempted to pull the cyclic back but the helicopter rolled to the left and the main rotor blades contacted the ground at full power, almost severing them at the blade roots. The main rotor blades cut the tail boom into three pieces, lodging the tail rotor and assembly into the ground about 5 m in front of the fuselage. The fuselage came to rest on the left side.

Although hanging from his seatbelt, the pilot was able to shut off the master; however, was unable to reach the fuel shut off valve. The pilot’s seat base dislodged and fell off once the pilot released himself from the seatbelt.

Post-accident observation

The pilot observed two old barbed wires leading from the fence line at a 45-degree angle One wire appeared to have broken with impact and the other wire was entangled around the front left-hand skid.

The wires were half buried in the ground and below the grass top level, making them invisible.

Figure 1: Accident site showing fence wire

Figure 1: Accident site showing fence wire

Source: Operator

Safety action

As a result of this occurrence, the pilot has advised the ATSB that they are taking the following safety actions:

  • avoid landing in grass any higher than skid tube height
  • conduct a thorough visual inspection when lifting off around fences.

Safety message

This incident provides a reminder to pilots to conduct a thorough visual inspection to confirm wire locations and other hazards.

This accident highlights the value of restraints and safety helmets for pilots to prevent more serious injury.

ATSB report AO-2014-058 provides an account of a serious head injury to an R22 pilot who was not wearing a helmet. In a later ATSB report, AO-2015-134, the operator commented that the pilot of an R22 accident would have sustained more serious head injuries if he was not wearing a helmet.

About this report

Decisions regarding whether to conduct an investigation, and the scope of an investigation, are based on many factors, including the level of safety benefit likely to be obtained from an investigation. For this occurrence, no investigation has been conducted and the ATSB did not verify the accuracy of the information. A brief description has been written using information supplied in the notification and any follow-up information in order to produce a short summary report, and allow for greater industry awareness of potential safety issues and possible safety actions.

__________

  1. Translational lift occurs when clear, undisturbed air, flows through the rotor system from wind or forward speed.
  2. Cyclic: a primary helicopter flight control that is similar to an aircraft control column. Cyclic input tilts the main rotor disc, varying the attitude of the helicopter and hence the lateral direction.

Occurrence summary

Mode of transport Aviation
Occurrence ID AB-2018-001
Occurrence date 04/01/2018
Location 38 km SW Tindal
State Northern Territory
Occurrence class Accident
Aviation occurrence category Collision with terrain
Highest injury level None
Brief release date 28/03/2018

Aircraft details

Manufacturer Robinson Helicopter Co
Model R22
Sector Helicopter
Damage Substantial

Separation issue involving Aerospatiale AS350, and Robinson R66, 22 km south-west of Aldinga (ALA), South Australia, on 7 January 2018

Brief

Occurrence Briefs are concise reports that detail the facts surrounding a transport safety occurrence, as received in the initial notification and any follow-up enquiries. They provide an opportunity to share safety messages in the absence of an investigation.

What happened

On 7 January 2018, a Robinson R66 helicopter departed the north coast of Kangaroo Island on a private flight to Aldinga Airport, South Australia. Upon reaching the mainland, the pilot observed what appeared to be sea fog from the north; however, the pilot then realised it was smoke from a grass fire at Carrickalinga, SA. The pilot advised he was listening on the area frequency and did not hear any notifications regarding a grass fire in the area so continued towards Aldinga at 2,000 ft.

About 10 NM SW of Aldinga Airport as shown in Figure 1, the crew of the Aerospatiale AS350 was conducting and directing fire control services at Carrickalinga and providing periodic transmissions on the Aldinga common traffic advisory frequency (CTAF). The transmissions were for inbound and outbound aircraft in order for them to keep clear of the aircraft conducting fire control below 2,500 ft.

At approximately 1400 Central Daylight-saving Time (CDT), the crew of the AS350 observed the Robinson R66 pass below on an opposite track. The crew of the AS350 turned left and climbed to increase separation. Information from both pilots estimated the distances between the aircraft to be of different clearance heights. The pilot of the R66 advised they were visual with the AS350 at all times. As the R66 passed Carrickalinga, the crew changed to the Aldinga CTAF to provide their 10 NM inbound call, and were notified by the crew of the AS350 of the fire exclusion zone.

Figure 1: Distance from Carrickalinga, SA to Aldinga Airport, SA

Figure 1: Distance from Carrickalinga SA to Aldinga Airport SA

Source: Google Earth, annotated by ATSB.

Airspace

Class G airspace

Class G airspace is non-controlled airspace. IFR and VFR traffic are permitted without a clearance and there is no separation service provided by air traffic control. Aldinga Airport is a non-controlled aerodrome with a discrete CTAF, which is a different frequency from the surrounding Class G airspace area frequency.

Safety action

As a result of this occurrence, the pilot of the AS350 has advised the ATSB that the incident has been shared among their company to highlight the importance of area frequency scans even when monitoring the local CTAF.

Safety message

This incident highlights the importance of monitoring the area frequency and local CTAF when operating nearby the 10 NM radius to successful identify any potential traffic conflict. As bushfire season has commenced in Australia for 2018 this incident has put attention to when bushfires are observed to try and avoid the area if possible or to ask ATC on the area frequency if there is an exclusion zone in place for fire control operations. Further information is available from ATSB research report: Limitations of the See-and-Avoid Principle.

The ATSB SafetyWatch highlights the broad safety concerns that come out of our investigation findings and from the occurrence data reported to us by industry. One of the safety concerns relates to safety around non-controlled aerodromes.

The ATSB SafetyWatch highlights the broad safety concerns that come out of our investigation findings and from the occurrence data reported to us by industry. One of the safety concerns relates to safety around non-controlled aerodromes.

About this report

Decisions regarding whether to conduct an investigation, and the scope of an investigation, are based on many factors, including the level of safety benefit likely to be obtained from an investigation. For this occurrence, no investigation has been conducted and the ATSB did not verify the accuracy of the information. A brief description has been written using information supplied in the notification and any follow-up information in order to produce a short summary report, and allow for greater industry awareness of potential safety issues and possible safety actions.

Occurrence summary

Mode of transport Aviation
Occurrence ID AB-2018-002
Occurrence date 07/01/2018
Location 22 km SW of Aldinga
State South Australia
Occurrence class Incident
Highest injury level None
Brief release date 28/03/2018

Aircraft details

Manufacturer Robinson Helicopter Co
Model R66
Sector Helicopter
Operation type Private
Damage Nil

Aircraft details

Manufacturer Aerospatiale Industries
Model AS350
Sector Helicopter
Operation type Aerial Work
Damage Nil

Know CO: Use an active warning carbon monoxide detector

The Australian Transport Safety Bureau (ATSB) urges operators and owners of piston-engine aircraft to know about the presence of carbon monoxide (CO) by using an active warning detector. 

CO is a colourless and odourless gas, and its presence may not be detected until the physical symptoms and cognitive effects present themselves. When inhaled, CO preferentially binds to haemoglobin, the oxygen carrying molecule in red blood cells. This creates carboxyhaemoglobin (COHb) compounds and prevents oxygen from binding to the molecule and being transported, resulting in oxygen starvation.

Symptoms can include breathlessness, confusion, disorientation and incapacitation.

Disposable chemical spot detectors, as commonly used in general aviation, may be effective in warning pilots of the presence of CO, but they have known limitations. Spot detectors are passive devices that relies on the pilot regularly monitoring it for discolouration. In addition, identifying a positive indication is also dependent on the detector being easily visible and accessible. Plus, these detectors do have a limited shelf-life when removed from their original packaging, which may be further affected by factors such as exposure to harsh direct sunlight, cleaning chemicals, and halogens. 

The ATSB highlighted its concerns regarding exposure to CO when it issued two Safety Advisory Notices arising from its investigation into the collision with water of a DHC-2 Beaver aircraft in Jerusalem Bay, north of Sydney, in which the pilot and five passengers were fatally injured. 

Toxicological testing of blood samples found the pilot and two passengers had elevated levels of CO. The levels detected were likely to have adversely affected the pilot’s ability to control the aircraft during the flight. The aircraft was fitted with a disposable chemical CO spot detector.

From the investigation, the ATSB published a Safety Advisory Notice, to piston-engine aircraft owners and pilots, reiterated the importance of the use of an active CO detector in the cabin. A second Safety Advisory Notice, to maintainers of piston-engine aircraft, highlighted the importance of the thorough inspection of exhaust systems and the timely repair or replacement of deteriorated components. 

Additionally, the Civil Aviation Safety Authority (CASA) published an Airworthiness Bulletin(Opens in a new tab/window), which encouraged operators and maintenance organisations to initiate a periodic CO detection check to measure the level of CO in the cabin at each annual or 100 hours-time in service (whichever occurs first), and each time the exhaust system or related components are disturbed.

The CO level entering the cabin must be less than 1 part in 20,000 parts of air (equivalent to 50 parts per million), derived from FAA FAR 23.83.

The ATSB's 'Know CO' campaign, launched in December 2021, encourages the use of CO detectors with an active warning. These inexpensive and widely available devices can provide pilots with the best opportunity to detect CO exposure before it adversely affects their ability to control the aircraft, or they become incapacitated.

It is worth noting that in July 2023, the UK Civil Aviation Authority (CAA) published its report into a study on how low-cost, commercial off-the-shelf, carbon monoxide CO detectors with attention-getting capabilities performed in a variety of general aviation (GA) aircraft and operating conditions.

Following a review in 2020 of accidents and incidents in the UK by the Air Accidents Investigation Board (AAIB) which identified two fatal accidents, each with two fatalities, and fifteen other events where CO may have been a causal factor over a 20-year period,  a was established to qualitatively and quantitatively investigate how low-cost active detectors perform in UK GA aircraft over a full flying season, to better understand pilot’s user experience of flying with these devices and to evaluate CO levels in a cross-section of the fleet.

Findings from the study suggested the risk of CO exposure remains a persistent background threat throughout the year and is somewhat elevated during cold weather operations. Anecdotal test evidence suggested that active CO detectors designed for domestic use can function reasonably at typical recreational GA altitudes (up to 5,000 feet). 

The report highlighted that while effective maintenance remains the first line of defence against CO and is the only way to avoid exposure, choosing to fly with an active CO detector is a decision pilots can make to protect themselves and their passengers from CO should maintenance fail.

With a wide range of active CO detectors on the market it has never been easier for pilots to find a device that suits their needs and budget. Active CO detectors are increasingly being built into other aviation equipment as standard, including ADS-B and headsets, making them ever more prevalent in GA aircraft. Additionally, some active CO detectors can be paired to personal electronic devices such as smartphones and smartwatches, increasing the likelihood of being alerted to elevated CO levels.

The report also highlighted the risk of CO poisoning may be known and understood by many pilots, the same cannot be said for consumers and third parties generally, who may fly in piston engine aircraft on a commercial or recreational basis. Pilots therefore should consider the significant safety benefits offered by flying with an active CO detector – it could not only save their life, but their passengers’ as well.

Read the report: CODE Trial Summary Report (caa.co.uk)(Opens in a new tab/window)
 

AOPA Real Pilot Story: Hidden Hazard

Flying his Mooney, Dan Bass was overcome by CO poisoning and lost consciousness while airborne. He recounts the dreadful accident and his miraculous survival waking up in a snow-covered field in the bitter north American February cold.

New Zealand Airline Academy sees immediate value of electronic CO detectors

In this CAA NZ article, The value of an electronic CO detector | aviation.govt.nz(Opens in a new tab/window), the Chief Flying Instructor of the New Zealand Airline Academy talks about Installing electronic CO detectors across its entire training fleet almost immediately saved two lives.

Technical assistance to the Civil Aviation Authority of the Philippines – Aircraft Accident Investigation and Inquiry Board investigation of an accident involving an IAI Westwind 1124A aircraft, RP-C5880, Ninoy Aquino International Airport, Manila

Update

On 29 March 2020, an IAI Westwind II 1124A aircraft registered RP-C5880, on an aeromedical flight from Ninoy Aquino International Airport, Manila, Philippines was destroyed following a runway excursion during take-off from RWY 06. The eight occupants received fatal injuries.

The Civil Aviation Authority of the Philippines – Aircraft Accident Investigation and Inquiry Board (AAIIB) requested assistance from the Australian Transport Safety Bureau (ATSB) to download the aircraft’s cockpit voice recorder (CVR) and flight data recorder (FDR) to assist their investigation.

To facilitate this support and to provide the appropriate protections for the information, the ATSB appointed an accredited representative in accordance with paragraph 5.23 of ICAO Annex 13 and commenced an investigation under the Australian Transport Safety Investigation Act 2003.

On 15 October 2020, the fire-damaged recorders from RP-C5880 (Universal Navigation Corporation CVR-30 and Fairchild Model F800 FDR) arrived in Canberra. The CVR and FDR were successfully downloaded at the ATSB data recovery facility. This activity was performed by ATSB recorder specialists in conjunction with AAIIB investigators located in the Philippines. All data recovered from the recorders was provided to the AAIIB to assist with their Annex 13 investigation. A report detailing the results of the download of the recorders was provided to the AAIIB on 18 July 2021.

Figure 1: Universal CVR-30 cockpit voice recorder recovered from RP-C5880 on arrival at ATSB

Side view of the cockpit voice recorder

Source: ATSB

Figure 2: Fairchild Model F800 flight data recorder recovered from RP-C5880 on arrival at ATSB

Side view of the cockpit voice recorder

Source: ATSB

The Philippines AAIIB is responsible for the investigation and release of the final investigation report regarding this accident. Any enquiries regarding the investigation should be addressed to the Philippines Aircraft Accident Investigation and Inquiry Board at the contact details listed below:

Aircraft Accident Investigation and Inquiry Board
Civil Aviation Authority of the Philippines
Email: aaiib@caap.gov.ph
Web: https://caap.gov.ph/2020-accidents/

Occurrence summary

Investigation number AE-2020-052
Occurrence date 29/03/2020
Location Ninoy Aquino International Airport (RPLL), Manila
Report release date 22/07/2021
Report status Final
Investigation level Defined
Investigation type External Investigation
Investigation phase Final report: Dissemination
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Runway excursion
Occurrence class Accident
Highest injury level Fatal

Aircraft details

Manufacturer Israel Aircraft Industries Ltd
Model Westwind 1124A
Registration RP-C5880
Serial number 353
Aircraft operator Lionair Inc.
Sector Jet
Operation type Medical Transport
Departure point Ninoy Aquino International Airport (RPLL), Manila
Destination Haneda Airport (RJTT), Tokyo
Damage Destroyed