Occurrences

Date	Occurrence #	Location	State	Aircraft	Model	Engine	Model	Summary
5/12/2015	OCC0507	Sunshine Coast	QLD	Piper	Sport Cruiser	Rotax	ULS 912	This flight was conducted for an owner of a leased aircraft online with the flying school. Pilot was...
This flight was conducted for an owner of a leased aircraft online with the flying school. Pilot was given the instruction "RWY 12, cleared for take-off, climb straight ahead". On upwind the pilot flying initiated a left turn onto crosswind to track northbound over water not above 1500' as per our airways clearance, forgetting the conditional clearance previously provided. Co-pilot immediately took over control and returned the aircraft back to the original runway heading. During this correction the tower controller instructed "Aircraft, the instruction was to climb straight ahead, maintain Easterly heading until advised". Pilots continued as per this clearance, to shortly track north over water. OUTCOME: Occurrence reviewed by Operations. Satisfactory action to rectify contravention with ATC instruction by instructor.
4/12/2015	OCC0511	Busselton Regional	WA	Evektor	Sportstar	Rotax	912 ULS	OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: Rudder Hinge Bearings - Both bearings seized with inn...
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: Rudder Hinge Bearings - Both bearings seized with inner spherical part rotating on shank of fixture. That is upper bearing inner part relies on friction of bullet nosed in pin attached to rudder spar, and the lower bearing inner part us secured by castellated nut on retention in lower part of rudder. Apart from being shiny where inner part of bearing was rotating on shanks, no wear step was evident. Due to being located in a recess no measurement for wear could be ascertained on the top pin. The lower beating centre however can be nipped by tightening the castellated nut. Bearings were cleaned of dried grease, readily freed, followed by application of a light grease and rudder reinstalled. Duplicated inspection of rudder control system will be carried out on completion of maintenance to rudder cables. OUTCOME: Evektor are aware that some Nicopress clamps were not sufficiently pressed during manufacture. They have released a Safety Alert Mandatory Bulletin SportStar – 017a SR to cover this anomaly and require a report back to them if additional defects are identified (refer Appendix 2 Item 7).
4/12/2015	OCC0501	Bathurst	NSW	BRM	Bristell	Rotax	912ULS	A current GA PPL holder converting to RA registered BRM Bristell held off on landing too long with a...
A current GA PPL holder converting to RA registered BRM Bristell held off on landing too long with an overly high angle of attack, resulting in portside wing drop and contact with the runway. This was his first solo after 2.5 hours of dual instruction with above average judgment displayed when dual. OUTCOME: CFI has provided an appropriate response to attempt to minimize another occurrence which includes spending more time in dual training irrespective of pilot experience and apparent talent.
2/12/2015	OCC0496	Merimbula	NSW	Airbourne	XT-912	Rotax	912	OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: As per AWB 02-006 the MIL spec 6000 hose swelled to t...
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: As per AWB 02-006 the MIL spec 6000 hose swelled to the point that it restricted the fuel flow to the engine resulting in total engine failure. This hose was factory fitted when the aircraft was new. OUTCOME: Tech spoke with the factory, who were sent the hoses for further investigation. During incident aircraft engine was seen to be not performing at an acceptable rev range however this was overlooked during the incident. Pilot followed correct process and landed straight forward. RAAus have also listed relevant information regarding Flexible Hose Assemblies AWB 02-006 Issue: 2, Date : 8 May 2015, which can be found at the following link https://members.raa.asn.au/announcements/article/?id=awb-flexible-hose-assemblies-maintenance-practices
30/11/2015	OCC0499	Frogs Hollow Airfield Bega	NSW	Airborne Windsports	XT912	Rotax	912	Departed from Frogs Hollow Airstrip Bega. At 300 ft at the end of RWY18, engine lost power, was runn...
Departed from Frogs Hollow Airstrip Bega. At 300 ft at the end of RWY18, engine lost power, was running very rough and aircraft was losing altitude. Aircraft was landed as per forced landing training one mile directly south of airstrip in paddock without incident. OUTCOME: Defect reported from this incident and as per AWB 02-006 the MIL spec 6000 hose swelled to the point that it restricted the fuel flow to the engine resulting in total engine failure. This hose was factory fitted when the aircraft was new. Tech spoke with the factory, who were sent the hoses for further investigation. During incident aircraft engine was seen to be not performing at an acceptable rev range however this was overlooked during the incident. Pilot followed correct process and landed straight forward. RAAus have also listed relevant information regarding Flexible Hose Assemblies AWB 02-006 Issue: 2, Date: 8 May 2015, which can be found at the following link https://members.raa.asn.au/announcements/article/?id=awb-flexible-hose-assemblies-maintenance-practices
29/11/2015	OCC0491	Caboolture	QLD	Tecnam	P92	Rotax	912 ULS	Left wing petrol cap was left off the aircraft after refuelling. OUTCOME: Pilot stated that there ...
Left wing petrol cap was left off the aircraft after refuelling. OUTCOME: Pilot stated that there was a change in where the pre-flight checks were completed and they were doing things slightly different to their normal routine. The aircraft was located in a different position and on grass making it more difficult to manoeuvre the petrol drum trolley. Pilot was aware of the HF involved in how the fuel cap was forgotten. Suggest that during pre-flight checks that a checklist is followed and ensure that petrol caps are secured using visually verification during inspection.
29/11/2015	OCC0494	Southport	QLD	Tecnam	2000R	Rotax	912	Wheels not clicked in resulting in wheels up landing (damage to one tip of propeller, no damage to a...
Wheels not clicked in resulting in wheels up landing (damage to one tip of propeller, no damage to air frame). OUTCOME: Pilot has been advised to upgrade his landing procedure checks and not be distracted while in the circuit.
29/11/2015	OCC0513	Woodstock	QLD	Howard Hughes Engineering	Light Wing GA-912	Rotax	912	Fatal Accident involving RAAus member. RAAus Accident consultants are assisting police in determinin...
Fatal Accident involving RAAus member. RAAus Accident consultants are assisting police in determining the causal factors that led to the accident. See the RAAus Special ENews at the following link for more information http://www.vision6.com.au/em/message/email/view.php?id=1155598&u=70000. Non-inquest findings: The Coroner concluded that the pilot died at about 6.20am on 29 November 2015 while piloting a Hughes Lightwing GA-912 aircraft that took off from Runway 33 at Starke Airfield, suffered a loss of engine power, aerodynamically stalled and impacted the ground causing his death. The cause of the loss of power was unable to be determined due to significant post-impact fire. There have been no recommendations made to RAAus by the Coroner. https://www.courts.qld.gov.au/courts/coroners-court/findings
27/11/2015	OCC0489	Bankstown Airport	NSW	Aeroprakt	Foxbat A22LS	Rotax	912 ULS	Student pilot conducted a solo check in order to complete second solo circuit lesson. Student pilot ...
Student pilot conducted a solo check in order to complete second solo circuit lesson. Student pilot dropped instructor off and taxied back towards RWY11R for this solo flight which authorized him to conduct three circuits followed by a full stop landing. All sequences in the circuit appeared normal until landing. On landing, the aircraft bounced twice and on the final touch down, the nose wheel collapsed, propeller hit the runway and the aircraft ran off the runway onto the grass. Student pilot was uninjured and was escorted back to the flight school. After a brief conversation with the student pilot it was determined they seemed to have encountered pilot induced oscillation for which they failed to go around. The aircraft was then towed to maintenance. OUTCOME: Ops spoken to CFI. CFI stated that all instructors have been briefed to ensure they conduct demonstration PIO and go-around procedures for all students, and include a notation on the student record to show competence. CFI ensuring all students are thoroughly briefed and checked for go-around procedures prior to further solo. The student will be taking a short break from training as a result of this accident, but does intend to return.
26/11/2015	OCC0522	Bundaberg Airport	QLD	Jabiru	J200	Jabiru	3300A	Reported that damage had occurred to a hanger had appeared overnight and a damaged aircraft parked a...
Reported that damage had occurred to a hanger had appeared overnight and a damaged aircraft parked a short distance away. OUTCOME: Investigation found RAAus pilot had run into hangar overnight due to unsafe operation of the aircraft. Damage to hangar has been compensated through third party property damage insurance. Due to the lack of communication with the pilot their pilot certificate has been suspended until further contact has been made.
24/11/2015	OCC0512	Busselton Regional	WA	Evektor	Sportstar	Rotax	912 ULS	OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: Rudder Hinge Bearings - Both bearings seized with inn...
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: Rudder Hinge Bearings - Both bearings seized with inner spherical part rotating on shank of fixture. That is upper bearing inner part relies on friction of bullet nosed in pin attached to rudder spar, and the lower bearing inner part us secured by castellated nut on retention in lower part of rudder. Apart from being shiny where inner part of bearing was rotating on shanks, no wear step was evident. Due to being located in a recess no measurement for wear could be ascertained on the top pin. The lower beating centre however can be nipped by tightening the castellated nut. Bearings were cleaned of dried grease, readily freed, followed by application of a light grease and rudder reinstalled. Duplicated inspection of rudder control system will be carried out on completion of maintenance to rudder cables. OUTCOME: Evektor are aware that some Nicopress clamps were not sufficiently pressed during manufacture. They have released a Safety Alert Mandatory Bulletin SportStar – 017a SR to cover this anomaly and require a report back to them if additional defects are identified (refer Appendix 2 Item 7).
24/11/2015	OCC0486	Gympie	QLD	Aeroprakt Foxbat	A22LS	Rotax	912 ULS	The student pilot was assigned a training area solo exercise that was to finish with a short session...
The student pilot was assigned a training area solo exercise that was to finish with a short session of circuits. The student had already completed approximately 4hrs solo during his training to date. On returning from the training area the first touch and go landing was uneventful. During the second approach, the student was observed to balloon during the flare to land. The aircraft entered a high rate of sink and yawed slightly to the right. As no attempt to arrest the sink rate with power (and / or) go around was initiated - the supervising instructor made a broadcast on the radio to the student advising him to add power immediately. This was not done and the aircraft impacted the ground heavily on the left main gear and nose gear simultaneously. The force of the impact caused the nose gear to collapse and the left wing to momentarily contact the runway. The aircraft came to rest upright and sitting on it's nose. The pilot exited the aeroplane un-injured. The supervising instructor attended the aeroplane immediately and turned off the fuel and electrics. OUTCOME: CFI has briefed student pilot and conducting further training
23/11/2015	OCC0519	Busselton Regional	WA	Evektor	Sportstar	Rotax	912 ULS	OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: Throttle Control Assembly P/No. E6-06 02 21B; operate...
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: Throttle Control Assembly P/No. E6-06 02 21B; operates two Bowden cables to throttle levers on twin Bing carburettors. Cable to operate LH carburettor kinked in aluminium barrel of throttle assembly preventing LH throttle lever on carburettor from opening to full throttle and while the RH carburettor achieved full throttle against the max stop. OUTCOME: Aircraft grounded until new throttle assembly obtained and fitted. Full mechanical synchronization, followed by pneumatic synchronization to be performed in accordance with the Rotax Maintenance Manual.
22/11/2015	OCC0520	Moorabbin Airport	VIC	Aeroprakt	A22LS Foxbat	Rotax	912 ULS	Pilot had requested RWY22 and stopped on the right place. Pilot made a radio call to request taxi to...
Pilot had requested RWY22 and stopped on the right place. Pilot made a radio call to request taxi to apron. The ground told pilot to hold shark RWY17R and thought RWY17R was further front so started to move forward. At that point ground stated that the aircraft was in the middle of the RWY17R and asked for the aircraft to move faster and taxi to apron. OUTCOME: Instructor sent pilot solo on the day of the event and had conducted a dual flight check with the student in the Moorabbin Airport circuit. This was not the first solo flight for student pilot who has been briefed before on Moorabbin taxiing procedures. Operations has reviewed report and school follow up and assessment satisfactory.
22/11/2015	OCC0485	Moorabbin Airport	VIC	Aeroprakt	AP22	Rotax	912 ULS	Pilot requested to use RWY22 and stopped in the right place and made the radio call. The ground told...
Pilot requested to use RWY22 and stopped in the right place and made the radio call. The ground told the pilot to hold short on RWY17R so the pilot stopped. At that time the pilot was thinking that RWY17R was further front and proceeded forward until they saw the holding point and stopped. The ground made the radio call to the pilot and explained that the aircraft was in the middle of the RWY17R and to move faster and taxi to apron. OUTCOME: CFI has taken appropriate actions to mitigate further risk from this student and retraining in CTA procedures will be undertaken by school for this student.