Occurrences

Date	Location	State	Aircraft	Model	Engine	Model	Summary
16/10/2015	Latrobe Valley	VIC	Tecnam	P92 Eaglet	Rotax	912ULS	DEFECT: Nose wheel steering bell crank detached from forward rudder bar (right rudder). Inspection r...
DEFECT: Nose wheel steering bell crank detached from forward rudder bar (right rudder). Inspection revealed that it appears to be torn away at the undercut of the weld. Parts sent to licensed Aviation welder for repair. OUTCOME: Manufacturer released Service Bulletin Tecnam No14-LSA (5 May 2010) for the inspection point requirements that refer to this defect.
14/10/2015	Myrup	WA	Rand Kar	Kr2-s	Aeropower	DL122	Pilot test flew aircraft after instillation of a new prop. After having no problem with taxiing arou...
Pilot test flew aircraft after instillation of a new prop. After having no problem with taxiing around Pilot lined up and rolled on RWY 14. After remaining straight for 200m and up to 50kts, a whirring bang was heard under the port wing. The aircraft slewed to the left in spite of full right rudder, decelerated, the tail came up even with full back stick, then the prop struck and came to stop on the nose. OUTCOME: The KR2 is being rectified by the new owner of the aircraft who has been repairing it and fitting it with a Jabiru engine (as the original engine crankshaft was damaged in the accident) The owner/ maintainer indicated that the incident occurred due to the port disc brake assembly distorting at speed which tangled with the spat, causing the wheel lockup. Additionally it appears that the seat cushioning also hindered some up deflection. Owner/ maintainer is modifying the cushion to get full up elevator, rebuilding a more rigid brake assembly and will be adjusting the weight and balance after the engine refit to ensure that there is no nose heavy tendency.
14/10/2015	Blackwater	QLD	Jabiru	J230	Camit	33SLR	Failure of fuel to feed from right hand wing to surge tank due to blockage in the vent. OUTCOME: T...
Failure of fuel to feed from right hand wing to surge tank due to blockage in the vent. OUTCOME: The pilot/ maintainer inspected the engine and the breather/vent was cleaned out. The pilot/ maintainer waited for fuel to cross feed as the breather/vent was not operating correctly due to contamination. RAAus Technical review. This is a 19 amateur built - previous reports have identified that the fuel vent is susceptible to small particles and grit becoming lodged and then preventing the vent from working (for example, in coastal conditions, salt crystals have formed which has then prevented the vent from operating correctly). The inspection identified that there was no cross feeding and in removing and cleaning the fuel vent the pilot was able to continue on without any other further issues.
12/10/2015	Boonah	QLD	Tecnam	P-96 Golf	Rotax	912 ULS	DEFECT: Both Engine Bearer Plates were found to be cracked on 100 hourly inspection. OUTCOME: Techn...
DEFECT: Both Engine Bearer Plates were found to be cracked on 100 hourly inspection. OUTCOME: Technical Manager contacted manufacturer to reported this issue with engine bearer plates. This is the first report of this type identified to RAAus and the manufacturer. No further action this time however if other maintainers identify similar defects RAAus will contact the factory immediately for further action.
10/10/2015	Bairnsdale	VIC	Alpi Aviation	Pioneer	Jabiru	3300	DEFECT: Right wing rear spar had no attachment and had nil support, this allowed over 1" of up & dow...
DEFECT: Right wing rear spar had no attachment and had nil support, this allowed over 1" of up & down movement at the trailing edge. LH wing had wedge bashed in to eliminate movement. Severe corrosion on bolts holding tail plane. OUTCOME: This is an amateur built aircraft. Maintenance errors will be addressed with training and the release of Technical Manual Issue 4. The L2 has rectified the current issue.
6/10/2015	Port Macquarie	NSW	Aeroprakt	A22 LS Foxbat	Rotax	912 U L S	The aircraft landed hard, resulting in a collapsed nose landing gear. OUTCOME: CFI followed up with...
The aircraft landed hard, resulting in a collapsed nose landing gear. OUTCOME: CFI followed up with pilot the control issues that occurred during this incident.
5/10/2015	Oakey	QLD	Austflight ULA	Drifter A-582	Rotax	582	The aircraft had been refuelled by Jerry-can and fuel drain carried out with no visible contaminatio...
The aircraft had been refuelled by Jerry-can and fuel drain carried out with no visible contamination. Departure was from a private strip and after traveling east to another private strip an approach was made from the west and a go around conducted, followed by an approach from the east, no attempt to land was made. On climb out to the West at approximately 300 feet AGL, the engine stopped. The aircraft was turned into wind and lined up with furrows in an open paddock, a brief attempt to restart was made during the turn. An uneventful landing was carried out. OUTCOME: Appropriate emergency actions were taken following engine failure to land aircraft safely. Appropriate fuel practices were carried out operationally. Aircraft is normally trailered at YBOK. The aircraft had been parked assembled outside one week earlier, Normal fuel drains were conducted pre-flight. Technical - Following the accident the carburettor bowls and fuel cells showed evidence of water that was not detected in the pre-flight. Complete fuel system was cleaned and flushed. The no1 cylinder showed signs of seizure and was repaired accordingly. A subsequent test flight was conducted and was successful and all engine operations normal. All pilots must ensure appropriate fuel sampling is conducted pre-flight based on the design of the fuel system and its likelihood to ingest water when secured in open environments. Poor sealing and open venting systems are common causes of water ingress in flight fuel systems.
4/10/2015	Cessnock	NSW	Tecnam	Sierra P2002JF	Rotax	912 S	DEFECT: Electric elevator trim runaway. During flight the Pilot operated up-trim. After releasing th...
DEFECT: Electric elevator trim runaway. During flight the Pilot operated up-trim. After releasing the up-trim button (located on the head of the control stick) the aircraft continued to change attitude. The trim electric isolation switch was moved to 'off' and control was held with some effort. The stick trim selector was moved to the co-pilot and trim isolator set to 'on'. Retrim was possible by using the buttons on the co-pilot control stick. The fault was later found to be a faulty up-trim switch in the pilots stick. Both up and down switches were replaced and no further trouble has been identified. OUTCOME: Switch was identified as the problem with no actual loss of primary flight control.
3/10/2015	Barwon Heads Airport	VIC	TL Ultralight Co	TL-96 Star	Rotax	912 U L S	A landing approach on RWY26 (grass strip with medium length grass) in turbulent and gusting winds (e...
A landing approach on RWY26 (grass strip with medium length grass) in turbulent and gusting winds (estimated 25 kts) from a NWW direction resulted in a collapsed nose wheel. Hard landing due to windshear. OUTCOME: Hard landing causing a nose wheel collapse due to weather.
2/10/2015	Drysdale River Station	WA	Jabiru	SP 500T	Camit	CAE3300	DEFECT: Pilot attempted to start the engine and the starter engaged and remained engaged after pilot...
DEFECT: Pilot attempted to start the engine and the starter engaged and remained engaged after pilot released the starter button. The stater tuned the engine until the battery was flat. Pilot removed and dismantled the starter solenoid. The solenoid return spring appear to be in perfect condition. after inspections it appeared that the copper contacts welded themselves together causing the starter to remain engaged. OUTCOME: The solenoid and battery were replaced and the starter system now works properly.
1/10/2015	Port Lincoln	SA	Jabiru	J200	Jabiru	3300	Fuel mismanagement. Pilot shut off wrong fuel tap. OUTCOME: Pilot confirmed fuel starvation was the...
Fuel mismanagement. Pilot shut off wrong fuel tap. OUTCOME: Pilot confirmed fuel starvation was the result of incorrect fuel system management. The pilot/owner advised the aircraft has a modified fuel tank system incorporating 3 separate fuel cells. 2 x 50L wing tanks and a centre fuselage 50L tank. All are separately tapped to allow PIC to regulate flow from wing tanks to original; primary tank. Pilot confirmed that having all tanks selected ON can overflow main tank and if wing tanks are empty and in ON position may introduce air into fuel system.
29/9/2015	Alice Springs	NT	Sling	Sling	Rotax	912 U L S	DEFECT: Air intake plug drawn into induction system and found resting on top of the air cleaner elem...
DEFECT: Air intake plug drawn into induction system and found resting on top of the air cleaner element. OUTCOME: Reviewed and actioned by Tech Manager - Manufacturer is aware that plug could be drawn into intake and as such is modifying the plug. Additionally all Sling aircraft owners are being advised of issue with plug.
22/9/2015	Amberley	QLD	Jabiru	J230D	Jabiru	3300A	Airspace Infringement - Pilot did not check NOTAMs or broadcast on the CTAF. OUTCOME: Pilot complet...
Airspace Infringement - Pilot did not check NOTAMs or broadcast on the CTAF. OUTCOME: Pilot completed a ground based review of RAAus CTA avoidance and planning, transponder use and NOTAM revision.
20/9/2015	Pyramid Hill Airport	VIC	Bristell	Bristell	Rotax	912 ULS	A student indicated right brake failure on landing during a training flight. The instructor took ove...
A student indicated right brake failure on landing during a training flight. The instructor took over and completed landing without use of brakes. OUTCOME: The Technical Manager has reviewed this report and has addressed this to the LSA factory. The aircraft is L2-LAME maintained to a high standard.
25/8/2015	Boonah	QLD	Tecnam	P-96 Golf	Rotax	912 ULS	DEFECT: Both nose wheel halves have cracks running through five of the six attachment holes. Could o...
DEFECT: Both nose wheel halves have cracks running through five of the six attachment holes. Could only be seen when wheel halves were apart. OUTCOME: Technical Manager contacted manufacturer to report this issue with nose wheels. This is the first report of this type identified to RAAus and the manufacturer. No further action this time however if other maintainers identify similar defects RAAus will contact the factory immediately for further action.