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24/07/2026
20/07/2026
14/07/2026

The ATSB has released its final report from its investigation into two separate suspected rotor drive belt failures involving Robinson R22s in northern Australia last November. Both incidents, involving helicopters with different operators and maintainers, resulted in hard landings, but no significant injuries.

https://www.atsb.gov.au/news/2026/r22-drive-belt-failure-accidents

29/06/2026
23/06/2026

The ATSB’s ongoing investigation into the loss of control accident involving a Diamond DA42 aircraft at Adelaide’s Parafield Airport on 29 April has identified that a component in the nose landing gear had failed due to fatigue and that the nose landing gear remained extended during the flight.

https://www.atsb.gov.au/news/2026/da42-nose-landing-gear-actuator-fracture

19/06/2026

Read All Over The Leg - the Yorke Peninsula Country Times is Yorke Peninsula's newspaper.

05/06/2026

The Finke Desert Race 2026 turns 50 this year, bringing thousands of spectators and participants to the Northern Territory’s remote outback.

With many travelling by light plane or helicopter, the skies around Alice Springs and nearby aerodromes will be busier than usual.

Pilots – the Finke Desert Race is classified as a public gathering, meaning increased safety separation requirements apply:

> Stay above 1,000 feet AGL over the racetrack.
> Fixed-wing aircraft: maintain 600m distance.
> Helicopters: maintain 300m distance.

Drone operators – the Finke Desert Race is a declared no-drone zone. Flying drones over the event is strictly prohibited due to serious safety risks, including collisions and potential harm to spectators and competitors. Penalties may apply.

Visit CASA’s info stall on Prologue Day (Saturday 6 June) at the start/finish line to chat with aviation experts about safe flying practices.

Read more on our website: civilaviation.au/finke-2026

Image credit: Finke Desert Race

05/06/2026

An ATSB occurrence brief details an engine failure and collision with terrain involving a Cirrus SR20 at Shellharbour Airport, NSW.

--What happened--
On 3 April 2026, the pilot of a Cirrus SR20 planned a private solo flight from Bankstown to Shellharbour, New South Wales. The pilot was planning to complete circuit practice and then return the aircraft to Bankstown.

During cruise to Shellharbour at 2,400 ft AMSL, while operating in autopilot mode, the fuel mixture was leaned[1] and the pilot observed multiple brief power reductions shortly thereafter. The vibrations lasted 1–2 seconds and did not persist, and the pilot elected to continue to Shellharbour as planned.

Having completed 3 non-eventful circuits on runway 24 at Shellharbour, a fourth circuit was commenced. While the aircraft was established on downwind, the pilot switched fuel tanks to conserve fuel. A landing and subsequent take‑off for a fifth circuit was then commenced. During upwind at approximately 350–450 ft AMSL, the pilot observed several momentary power losses followed by a sustained loss of power and a significant vibration. The engine was fluctuating between the production of power and loss of power.

The pilot was aware of the low altitude and low airspeed and conducted a forced landing in a vacant paddock to the west of the airfield. Prior to landing, the pilot confirmed that the throttle was in the full position with an accompanying rich fuel mixture and the fuel pump in the on position. Just prior to touching down, the aircraft entered an aerodynamic stall and collided with terrain resulting in substantial damage to the left wing and undercarriage. The pilot sustained minor injuries.

The post-flight engineering inspection revealed an induction leak at the no. 1 position induction pipe and a brief rough running magneto. Engineers replaced the no. 2 fuel injector nozzle and 2 of the magneto plugs.

--Cirrus airframe parachute system--
The Cirrus airframe parachute system (CAPS) is designed to safely lower the aircraft and its occupants to the ground, under parachute, in the event of a life-threatening emergency where activation is determined to be safer than continued flight, such as medical incapacitation or airframe failure. In this instance, due to the aircraft’s low altitude, the pilot did not deploy the parachute.

--Safety message--
During emergency operations at low altitude, pilots are encouraged to be decisive when selecting the appropriate landing area, as well as vigilant in maintaining the speed required for a forced landing to avoid a stall prior to touchdown. Should the aircraft enter an aerodynamic stall, execute the stall recovery technique.

[1] The mixture is leaned for stages of flight that would require less fuel to maintain efficient engine operation.

--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.

18/05/2026

An ATSB occurrence brief details an R22 helicopter's collision with terrain in south Queensland.

--What happened--
On the afternoon of 28 March 2026, a Robinson R22 Beta II helicopter with the pilot and a passenger on board was conducting a private, stock monitoring flight around 55 km to the south-east of St George Airport, Queensland. The weather was reported as fine, with 20 km/h (10.8 kt) winds from the south. The pilot reported that while hovering into wind at a height of about 30 ft, they commenced a pedal turn[1] to the right, away from a line of trees. During the turn downwind, the turn rate began to increase and they were unable to arrest or control the rotation – estimating that the helicopter spun through approximately 450 degrees before it descended to heavily contact the ground. The rotating motion during ground contact resulted in the helicopter rolling onto its left side, sustaining substantial damage to the main and tail rotors, tail boom and cabin. Both pilot and passenger were able to egress through the right doorway and were uninjured.

(Photo shows helicopter after being returned upright after the accident.)

--Engineering examination--
The helicopter was recovered and examined by maintenance personnel, with attention to the tail rotor drive train and controls. No evidence of pre-existing mechanical defects was identified, with all damage consistent with being sustained during the accident sequence.

--Safety message: Unanticipated yaw--
Directional (yaw) control of single main rotor helicopters is primarily achieved through the pilot’s manipulation of tail rotor thrust. The torque produced by the drive transmitted through the main rotor is counterbalanced by the tail rotor thrust, with the pilot’s control of that thrust allowing controlled movement of the helicopter about its vertical axis.

In the hover and at low forward airspeeds, several aerodynamic effects can influence the anti-torque effectiveness of the tail rotor system. These can produce yaw motions unanticipated by the pilot, and which, if not immediately arrested, can result in a loss of helicopter control. Collectively known as Loss of Tail Rotor Effectiveness (LTE) phenomena, these include:

- main rotor disk vortex interference
- weathercock stability
- tail rotor vortex ring state
- loss of translational lift.

The United States Federal Aviation Administration (FAA) advisory circular AC 90-95 and the Helicopter Flying Handbook - Chapter 11: Helicopter emergencies and hazards explain these effects and recommend avoiding the following flight conditions when operating at forward airspeeds below 30 kt:

- tailwinds
- out-of-ground effect hovers and high-power demand situations such as low‑speed downwind turns
- hovering in winds above 8–12 kt (especially when out-of-ground effect).

AC 90-95 recommends the following recovery actions if experiencing LTE:

- application of full pedal opposite the direction of rotation
- forward cyclic movement to increase speed
- reduction in power if altitude permits.

https://www.faa.gov/regulations_policies/advisory_circulars/index.cfm/go/document.information/documentid/23136

https://www.faa.gov/sites/faa.gov/files/regulations_policies/handbooks_manuals/aviation/helicopter_flying_handbook/hfh_ch11.pdf

[1] A low-airspeed helicopter turning action initiated solely with the tail rotor controls (pedals).

--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.

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