Date |
Occurrence # |
Location |
State |
Aircraft |
Model |
Engine |
Model |
Summary |
21/2/2017 |
OCC0929 |
Tooradin Airfield |
VIC |
Airborne |
Edge XT 912 |
Rotax |
912 UL |
The pilot was standing beside the cockpit, with left foot on the brake, left hand on the compression...
|
The pilot was standing beside the cockpit, with left foot on the brake, left hand on the compression strut while pressing the start button with the intention that once the engine started, removing a heat pack from the ignition module, then climbing into the cockpit.
On starting, the plane rolled forward. Pressure on the left brake pedal served only to turn the nosewheel to the right and the brakes to be not applied. The pilot swung into the cockpit but could not regain sufficient control before the plane rolled 15m and the left wing struck a light pole. The power of the engine caused the nose to rise up the light pole, the left landing gear strut contacted the light pole, and the plane came to rest in a nose up position resting on the engine and propeller.
OUTCOME: Loss of Control of aircraft during starting phase due to pilot not being correctly seated and in control of the aircraft braking systems |
20/2/2017 |
OCC0932 |
Yarrawonga |
VIC |
Airborne |
XT 912 |
Rotax |
VL180 |
The aircraft crossed the threshold slightly high but still within the limits of a normal approach an...
|
The aircraft crossed the threshold slightly high but still within the limits of a normal approach and landing. It is unclear if the student then took the power off and put an incorrect input in. The aircraft lurched to the left and descended rapidly to the ground, hitting the left wheel first. The instructor grabbed the controls and told the student to add full power. The aircraft bounced on the left wheel and we were airborne again. The instructor subsequently requested the student select full power as he could not get to the throttle as he had both hands on the controls. The aircraft became airborne again but not lined up on the runway. Again the instructor requested full power however there was no input from the student. On the third bounce the aircraft settled on the runway but it was angled to the left and slowing down. This is when the student added full power. The aircraft then rapidly started moving towards the fence past the flight strip. The instructor had the controls but not the throttle. The aircraft became airborne again and began to climb. The instructor’s intention was to conduct a go-round until the student then put the throttle to flight idle. This caused the aircraft to descend hitting the top of the fence and the aircraft rolled slowly over the fence inverted and settled on its right side.
OUTCOME: A full investigation including a school inspection and CFI renewal was conducted to review training processes and instructional flight management relating to recovery from uncontrolled states both in generic weight shift environments and further into control protocols and risk management in weight shift instructional environments. The investigation outcomes have resulted in adaption by the CFI and school of a more robust application of risk principles in flight operations.
It is further recommended by operations that where shared control environments are required that early intervention of potential uncontrolled states be adopted by all instructors and briefed accordingly in regards to HF elements of pre-flight and operational briefings in relation to crew responsibilities and cockpit resource management (CRM). |
18/2/2017 |
OCC0925 |
Brisbane West Wellcamp |
QLD |
Jabiru |
J160C |
Jabiru |
2200 B |
Conducting touch and go's, the aircraft came to a full stop landing. The pilot then applied full pow...
|
Conducting touch and go's, the aircraft came to a full stop landing. The pilot then applied full power to take off and after 25-40 meters into wind, the Port wing rose suddenly and the aircraft "wheel barrowed" on the front wheel and starboard main wheel, striking propellor and just touching starboard wingtip. The aircraft then righted itself, and came to a stop.OUTCOME: Runway Loss of Control event R-LOC. PIC has undertaken additional training and counseling. |
18/2/2017 |
OCC1069 |
Morton Island |
QLD |
Flysynthesis |
Texan 550 |
Rotax |
912 ULS |
The PAX unlatched one side of the bubble canopy of the aircraft while in flight. A precautionary lan...
|
The PAX unlatched one side of the bubble canopy of the aircraft while in flight. A precautionary landing was safely carried out at local airfield.
OUTCOME: Operations Managers have reviewed this report and no further action or comment is required. Members are reminded to ensure that all passengers have had a pre flight briefed conducted. |
16/2/2017 |
OCC0922 |
Noosa Heads |
QLD |
Alpi |
Pioneer 200 |
Rotax |
912 ULS |
A delayed inbound call owing to unusually high volume of radio traffic resulted in the aircraft to b...
|
A delayed inbound call owing to unusually high volume of radio traffic resulted in the aircraft to be within the airspace prior to being able to contact ATC. The pilot then misunderstood the tower instructions for approach to maintain 1500' and join L downwind 36 and was on track to join R downwind 36 before further contact with the tower for correction.
OUTCOME: RAAus Operations Managers reviewed this incidents with the Aero Club CFI and noted that the member was exercising the privileges of his CASA RPL not any RAAus exemption privileges. Notwithstanding this the pilot has been debriefed on CTA clearance protocols. |
12/2/2017 |
OCC0915 |
Ball Bay |
QLD |
BRM Aero |
Bristell UL FG |
Rotax |
912 ULS2 |
The aircraft had been flying for approx. 30 minutes at 5,000 RPM and 2,000ft when there was a slight...
|
The aircraft had been flying for approx. 30 minutes at 5,000 RPM and 2,000ft when there was a slight shudder and the revs dropped to 3,800 RPM. The fuel pressure was 4 PSI and all instruments checked okay. The pilot pulled on the carby heat and turned the electric pump on - fuel pressure was at 5 PSI. Revs dropped slightly and as the pilot was close to Ball Bay airstrip carried out a precautionary landing with no incident. On the ground and engine would not rev above 3,800 RPM.
Determined Outcome: This incident has not been able to be replicated on the ground. The carburettor and ignition were replaced with no reoccurrence. The conditions on the day of the incident were; temperature 32 degrees with 60% humidity and may have been a contributing factor. The RAAus Technical Manager has made the LSA importer aware of this issue so that they can monitor any future occurrences. No further action by RAAUs can be taken at this point in time. |
12/2/2017 |
OCC0914 |
Atherton Airport |
QLD |
JABIRU |
J230 |
Jabiru |
3300 |
After completing pre-flight checks the pilot taxied to the runway threshold and lined up for take-of...
|
After completing pre-flight checks the pilot taxied to the runway threshold and lined up for take-off. After giving a rolling call, full power was applied and initial speed pick up was good but as the aircraft went up the hill it didn't pick up in the long wet grass. On the flat it slowly picked up speed in the long wet grass however the pilot felt there was not enough runway left so, closed the throttle and applied the brakes. The brakes locked and skidded so the pilot released them and reapplied several times, not as hard, then started to make a right turn but was still too fast. The pilot was concerned that the left wing would contact the ground so decreased the turn. Then the aircraft slid into a fence hitting a post which caused a prop strike, then bounced back and the tail made contact with a post at the back.
OUTCOME: Pilots are reminded to consider appropriate Take off rejection points as part of their Pre Take-off safety brief with particular consideration to variations in slope of runway and surface conditions. |
12/2/2017 |
OCC0920 |
Walgett |
NSW |
Cessna |
162 |
Continental |
0-200-D |
Birdstrike: The pilot observed a number of birds around the runway however they flew away while the ...
|
Birdstrike: The pilot observed a number of birds around the runway however they flew away while the aircraft was taxied and touch and goes were conducted. When conducing the final landing, a few birds did not fly away and hit the aircraft wing.
OUTCOME: RAAus have checked the ERSA for Walgett to confirm information is available about bird hazards. The ADDITIONAL INFORMATION section states:
1. After rain deep water puddles. ACFT 5,700KG & ABV confine TAX to RWY centre & turn
only on RWY end turning nodes, 05/23.
2. Animal & bird hazard exists.
RAAus will continue to monitor for any additional reporting of additional bird strikes. |
11/2/2017 |
OCC0916 |
Quirindi Airport |
NSW |
Aeroprakt |
A22LS Foxbat |
Rotax |
912 U L S |
The aircraft suffered a heavy landing causing nose wheel leg to be bent.
Determined Outcome: Due ...
|
The aircraft suffered a heavy landing causing nose wheel leg to be bent.
Determined Outcome: Due to the approach speed not being managed appropriately, the aircraft suffered a hard landing and damaged the nose gear. PIC noted HF and inappropriate approach speed and steep angle. Pilots are reminded of the importance of a stabilised approach at the manufacturer's recommended speed according to the POH. |
10/2/2017 |
OCC0985 |
Maroochydoore |
QLD |
AeroPrakt |
A32 |
Rotax |
912 ULS |
The light aircraft did not receive calls from ATC therefore failed to respond. This resulted in an R...
|
The light aircraft did not receive calls from ATC therefore failed to respond. This resulted in an RPT having to cancel an already cleared RNAV-36 (RNP) approach. The RPT subsequently joined a Visual Right CCT. Communications were re-established between ATC and the light aircraft.
OUTCOME: Temporary loss of 2 -way communications between tower and aircraft. No cause was able to be identified. |
5/2/2017 |
OCC0913 |
Moorabbin Airport |
VIC |
Aeroprakt |
A22LS Foxbat |
Rotax |
912ULS |
On final landing of a circuits session in gusty conditions, the student straightened the nose but di...
|
On final landing of a circuits session in gusty conditions, the student straightened the nose but didn't flare quite enough causing plane to land reasonably gently but flat resulting in a small bounce of approximately 3ft height. The student steadied well initially but the nose then dropped quickly, partly due lack of control by the student and partly sudden lull in wind. When the nose dropped the nose wheel landed firmly first with audible thud. The Instructor went to take over at first sense of nose dropping but was not quick enough to go around before nose landed due to being about to land.
OUTCOME: Instructor has had debrief with CFI and Operations on control management practices, student control limits and instructional policies that have been implemented and reviewed to prevent further re-occurrences of this nature. |
4/2/2017 |
OCC0910 |
Jacobs Well |
QLD |
Bearhawk |
Patrol |
Lycoming |
O-320 |
Whilst landing on an airstrip surrounded by cane fields, a vehicle emerged at the start of the runwa...
|
Whilst landing on an airstrip surrounded by cane fields, a vehicle emerged at the start of the runway. The pilot was able to manoeuvre the aircraft to avoid a collision.
OUTCOME: The airfield has two clubs operating, and one club can access the airfield and hangars via a boom gate, the other club is prevented from this and must access the airfield and hangars via an access road, which cuts across the overrun area of the runway. This has highlighted more of a hazard at this location in which some pilots are required to access the airfield and hangars via aerodrome access road, placing them in potential conflict with aircraft on final. The aircraft can see the car, but due to the surrounding crop of cane, the car cannot see the aircraft. RAAus Operations Manager reviewed the report and spoke with the member operating the vehicle who was prevented from seeing any aircraft on approach due to the cane crop in the vicinity. This information is also highlighted on the Clubs website page as an advisory for those driving into the airfield: http://www.gcsfc.org.au/driving-to-jcw.html RAAus recommends that in a situation such as this the pilot should conduct a go-around as he would have had visibility of the car from the air. |
2/2/2017 |
OCC0924 |
Private Property |
QLD |
Thruster Aircraft |
Thruster T300 |
Rotax |
582 DCDI |
A new propellor was fitted to the aircraft using parts and specifications provided by the manufactur...
|
A new propellor was fitted to the aircraft using parts and specifications provided by the manufacturer, however there was one washer per bolt around the outer hub bolts which secure the pitch blocks and blade route when there were three washers used on original hub. The hub bolts were tensioned to manufacturer specifications. After 50mins of flight the aircraft developed a vibration. Upon inspection after landing it was found that the hub had a crack at one of the outer hub bolts.
OUTCOME: The pilot/ owner identified that the manufacturer did not supply relevant assembly instructions in relation to the aircraft when the parts were supplied. Additionally there was an incorrect number of washers supplied for the installation. The pilot/ owner referenced two sources of assembly instructions, however there was some difference in the information. The RAAus Technical Manager has addressed this with the manufacturer who has now supplied the correct current assembly instructions, including the correct number of washers to be used with the replacement parts. |
1/2/2017 |
OCC0906 |
Colosseum Inlet |
QLD |
Super Petrel |
100 |
Rotax |
912 U L S |
During flight, the PAX side perspex window blew out. This damaged the propeller, however did not cau...
|
During flight, the PAX side perspex window blew out. This damaged the propeller, however did not cause the carbon fibre propeller to disintegrate and did not cause severe vibration. The aircraft returned to the airfield and landed with no issue.
OUTCOME: Technical Manager reviewed this report which is for an amateur built aircraft. After inspection of the aircraft it was determined that there was deterioration of the glue holding in the Perspex window which led to the window blowing out. Owner/ operator is addressing the issue by using:
- epoxy glue to glue in the window (the same way as the manufacturer does).
- the new system used on the LSA Super Petrels (Sicaflex 221 with a layer of fibre glass cloth around the edge). |
1/2/2017 |
OCC0905 |
Whitegum |
WA |
Micro aviation |
Bathawk |
Camit |
3300SLRE |
During flight training the student rounded out too high and the instructor took over too late to pre...
|
During flight training the student rounded out too high and the instructor took over too late to prevent the aircraft landing firmly.
OUTCOME: During landing, the student rounded out too high and the Instructor did not react quickly enough to prevent a hard landing. |