Date |
Occurrence # |
Location |
State |
Aircraft |
Model |
Engine |
Model |
Summary |
4/5/2016 |
OCC0637 |
Condobolin |
NSW |
Bristell LSA |
NG5 |
Rotax 912 |
ULS2 |
Pilot (with passenger) conducted five 5 touch and goes and were on final for the sixth and final lan...
|
Pilot (with passenger) conducted five 5 touch and goes and were on final for the sixth and final landing for the day. The wind sock was facing South for the first five landings and swung around to the East just before final. A gust of wind hit the plane and drove it into a clump of small trees. The pilot and passenger no time to do anything before the plane came in contact with the soft top branches causing the plane to flip upside down and crash to the ground. Both pilot and passenger managed to escape from the plane before a fire completely burnt the plane. Aircraft is destroyed with minor injuries to both personnel on board.
OUTCOME: Pilot lost control of the aircraft when the starboard wing grazed branches of a tree on final approach near the landing area threshold of a private landing Area.(R-LOC). Contributing factors included high wing primacy of this experienced Cessna 182 pilot with the low wing aircraft configuration and the lack of understanding of reduced inertia of light sport aircraft at low airspeed. Subsequent actions undertaken include substantial removal of trees on this approach by the owner and Operations request for pilot to undertake specialist revision training in unimproved landing area operations with local CFI as part of new aircraft handover process in the coming months. These actions have been agreed too and will be coordinated by the delivering dealer in the coming months. |
4/5/2016 |
OCC0641 |
Wardell |
NSW |
Paradise |
P1 |
Rotax |
912 U L S |
Pilot was operating out of "Saltwater" ALA in the designated Ballina Southern Training Area (R638 is...
|
Pilot was operating out of "Saltwater" ALA in the designated Ballina Southern Training Area (R638 is just 2 nm miles South of this ALA). On checking EVX notams NAIPS reported "No Current NOTAMs". The pilot's usual procedure was to check with Brisbane Centre on 120.3 to confirm status of the Evans Head Airspace if the intention was to penetrate R683. The pilot had a high workload in the cockpit due to a technical issue and was delayed in the normal turn on to North as well as the call to Brisbane Centre. Pilot was squawking Mode C and immediately contacted Bribane Centre when requested by an overflying RPT aircraft.
OUTCOME: Pilot and landing area operator has amended his flight planning process using appropriate AirServices information in NAIPs via the restricted area briefing tab to confirm status of this RA1 restricted area. This site is a training airfield and the CFI has incorporated the amended planning into all student flight briefings as well. Pilots should be aware that traditional inactive restricted areas are increasingly being activated for a range of extended military activities and historical inactivity cannot be assumed as operations may be H24 by NOTAM. |
26/4/2016 |
OCC0633 |
Northam Station |
QLD |
Tecnam g5 Eaglet |
P96 |
Rotax |
912 |
Aircraft experienced a wire strike on the propeller. The reporter believes that a piece of wire may ...
|
Aircraft experienced a wire strike on the propeller. The reporter believes that a piece of wire may have been dragged onto private strip and picked up by propeller causing propeller and spat damage.
OUTCOME: Pilot stated that it may have been possible that an animal dragged wire onto the runway or picked up in a hangar environment. It is recommended that an inspection of runways and hangars occurs on a regular basis as a sensible precaution to avoid FOD hazards to aircraft. |
23/4/2016 |
OCC0648 |
Adelaide |
SA |
Jabiru |
SP 500 |
Jabiru |
2200A |
Airspace Infringement near Mount Bold Reservoir: Description:- PC12 PIL inbound to Adelaide from DRI...
|
Airspace Infringement near Mount Bold Reservoir: Description:- PC12 PIL inbound to Adelaide from DRINA on descent to A030 visual was given traffic on a 1200 squawk with no mode C indication crossing right to left about 14 miles south east of Adelaide. As traffic was passed, a mode C readout of A029 was received from the 1200 squawk, and PIL's descent was stopped at A040. The aircraft passed each other with no less than 1000 ft separation. The 1200 squawk was identified as Jabiru, the altitude verified, and the aircraft instructed to leave class C descending to A025.
OUTCOME: Loss of situational awareness due to inattention and distraction in close proximity to control area boundary. The experienced pilot has self evaluated his planning and in flight management errors to protect against any further occurrences
SAFETY MESSAGE: RAAus pilots are reminded to ensure adequate planning and consideration of all environmental factors when conducting flights in proximity to known controlled airspace boundaries. High work loads and distraction, due to unexpected flight conditions, can be mitigated by pilots applying generous buffers in their pre-flight planning, and vigilance to in flight navigation, and decision making. |
22/4/2016 |
OCC0639 |
Bundaberg Airport |
QLD |
Homebuilt |
Nova |
Jabiru |
3.3 |
After successfully landing the tail wheel aircraft went into a right hand ground loop and the applic...
|
After successfully landing the tail wheel aircraft went into a right hand ground loop and the application of left rudder was insufficient to correct. The pilot's application of power caused the aircraft to over correct to the left. This caused the right hand main wheel leg to fold in and collapse.
OUTCOME: Runway - Loss of Control (R-LOC) on landing. Contributing factors identified were inattention, lack of tail wheel endorsement and braking configuration of aircraft. Pilot requested to undertake authorised endorsement training with an RAAus school and qualified instructor and to consider reversion of brake design to original differential brake configuration. |
20/4/2016 |
OCC0629 |
Yarrawonga |
VIC |
Airborne |
Edge X 582 |
Rotax |
582 |
Aircraft recently experienced abnormal engine indications. Maintainer replaced all fuel lines, fuel ...
|
Aircraft recently experienced abnormal engine indications. Maintainer replaced all fuel lines, fuel filters, cleaned the fuel tank and replacing the fuel pump and other items with the owner. Maintainer had the owner conduct a number of engine runs with a number of RPM settings before conducting a check flight. Maintainer/ pilot conducted the same power run ups to ensure the aircraft was safe to fly which indicated no sign of a problems. Pilot/ maintainer taxied to the beginning of RWY01, ran the engine up to 5000 RPM and held it there for 2 minutes, started take-off roll and rotated as normal. Pilot climbed in a normal climb out to 900 feet and was about to turn down wind when the engine started to lose power. Pilot tried to restart the engine three times without success however had enough power to conduct a landing in a paddock of the end of the runway. No damage sustained to the aircraft or pilot.
OUTCOME: Technical Manager contacted pilot/ maintainer requesting additional information. This was the second incident of its kind regarding engine issues with this specific aircraft. The pilot/ maintainer took appropriate inspections and actions to identify the abnormal engine indications however was unable to identify the source of the problem. The engine has been removed and sent to factory for repair and rectification. The trike manufacturer is assisting with this one off engine issue. |
19/4/2016 |
OCC0661 |
Tamleugh (NW of Violet Town) |
VIC |
Corby |
Corby Starlet CJ-1 |
Jabiru |
2200 |
Before departure the pilot noticed a slight stiffness in the canopy slide function. The canopy locke...
|
Before departure the pilot noticed a slight stiffness in the canopy slide function. The canopy locked securely before flight. Flight from Mt Beauty to Colac, Victoria at 3,500ft at 90 kts. In flight the right hand front corner of the canopy was noticed to be slightly displaced to right (3mm) from normal. This was observed for some time and appeared to be stable. The pilot decided to maintain a reduced speed of 90 kts. After 20 minutes, the canopy suddenly departed the aircraft. The aircraft continued operating normally with no indication of any contact of the canopy with the airframe and with normal engine power and fuel consumption. The pilot elected to continue the flight at reduced speed and the fuel endurance was sufficient for destination with 1 hour reserve.
OUTCOME: Owner/ pilot was aware of concerns with the canopy runners for some time and had planned to change the canopy. Unfortunately due to personal reasons the replacement canopy had not occurred, which lead to the incident. This canopy was converted from side opening to slide in 2003. The canopy is an old style (Gould) normally mounted on a three point slide arrangement. This conversion incorporated two Accuride Ball bearing slides regularly used on Corby Starlets. This Canopy is considerably heavier than the common New Zealand variety generally used these days and consequently side loads may have caused some distortion to the slides when fully extended. The owner/ pilot had opened the canopy when taxiing over undulating grass to get parking instructions. One of the ball bearings may have dislodged from its ball carrier and found its way between two slide elements, forcing the elements apart or imparting considerable side load which could ultimately cause this to happen.
The owner/ pilot has since had a new canopy made and has supplied the appropriate drawings for the new canopy slide. Corby Starlet owners are reminded of the importance of preventative and ongoing maintenance practices. |
19/4/2016 |
OCC0645 |
Caboolture |
QLD |
Aeroprakt |
A22LS Foxbat |
Rotax |
912ULS |
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: The Aircraft was inspected by the maintainer due to a...
|
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: The Aircraft was inspected by the maintainer due to a report of smell of fuel and sign of a leak in the cowling. The maintainer removed the cowlings and on first impressions the leak was detected to be coming from seals around fuel distribution block P/N 851327. After some check tightening of the hoses, and sealing plug, a ground run was conducted and fuel was found to be spraying out of the distribution block. On removal of this block the maintainer found a hairline crack coming from the plug hole and spreading 7mm along to block to the center. The distribution block and seals were all replaced and a ground run was carried out with nil leaks detected and the aircraft re-released to service. The crack was very hard to see due to the machining marks already on the block.
OUTCOME: As detailed above the fuel leak source was identified by an appropriate workshop (where the standard maintenance practices for the identification of an issue were conducted). The area of concern was identified as the hairline crack and is being addressed by a replacement part purchased from an approved factory agent. |
17/4/2016 |
OCC0624 |
Yarrawonga |
VIC |
Airborne |
Edge X 582 |
Rotax |
582 |
Pilot conducted a test flight for the owner of the aircraft. Pilot had completed engine runs and the...
|
Pilot conducted a test flight for the owner of the aircraft. Pilot had completed engine runs and then a pre-flight check. The aircraft was running well with no sign of any problems. As the pilot entered the runway they checked the aircraft systems and then applied power. The aircraft responded well and pilot was airborne at the right speed with the aircraft climbing as expected. When the aircraft was three quarters of the way down the runway the engine slowly shut down. Pilot did not try to restart the aircraft and made a forced landing on the runway and rolled to a stop. Pilot restarted the engine on the ground and conducted a run up through the power band with no problem. A high speed taxi was conducted and the pilot conducted a circuit and landed again with no further problems.
OUTCOME: All appropriate steps were carried out in relation to the flight testing of the new aircraft. The pilot conducted the correct processes and satisfied himself that the aircraft was considered satisfactorily for additional flight. Engine issues may have resulted from some sort of contamination passing through the system, i.e. fuel, due to aircraft proceeding to be retested and found to produce full power, and subsequently flew without any further issue. |
15/4/2016 |
OCC0627 |
Rockingham |
WA |
Morgan Aero Works |
Cheetah |
Jabiru |
2200 |
Morgan pilot was on climb out of Serpentine over Rockingham tracking for Carnac Island at about 1015...
|
Morgan pilot was on climb out of Serpentine over Rockingham tracking for Carnac Island at about 1015 h on radio frequency 135.25 passing through 2800. An aircraft was sighted at approximately the same altitude heading South almost directly towards Morgan aircraft. Morgan pilot was very slightly below and, because the other aircraft was tracking across their flight path from left to right, took evasive action by quickly rolling left and down. When the aircraft was about halfway between the Morgan aircraft and the point when they were first sighted, the Morgan pilot noticed it took evasive action up and to the left.
OUTCOME: Morgan pilot contacted Perth Centre and reported the near miss, they confirmed the likely identity of the aircraft, then reported other traffic in the area in which pilot attended to. ATSB conducted an investigation of this report and the information can be located at https://www.atsb.gov.au/publications/investigation_reports/2016/aair/ao-2016-038/ |
14/4/2016 |
OCC0651 |
Wagga Wagga |
NSW |
DynAero |
MCR-ULC |
Rotax |
912ULS |
Flight from YTMU to YSWG (for the fitment of a new radio) pilot was using an ICOM portable, for the ...
|
Flight from YTMU to YSWG (for the fitment of a new radio) pilot was using an ICOM portable, for the flight, attached to the aircraft aerial (previous flight had good transmit and reception). During the flight the pilot noticed few radio calls on the area frequency. On 126.95 the pilot gave a 10 NM call 'West at 4,500 ft descending to 3,000 ft, with an expected overhead in 5 minutes' while listening for calls indicating an established runway direction. When over the field at 3,000 ft the pilot was not able to determine the wind direction and noticed a twin taxiing slowly and a Qantas Dash-8 at the apron. The pilot decided to use RWY23 and descended to 1,700 ft entering mid-downwind for RWY23 (standard radio call) calling 'turning base for RWY23, full stop'. At about 200 ft above the ground the pilot noticed an aircraft landing in the opposite direction (on RWY05) with another behind it. The pilot immediately turned right to the dead side, clear of the runway, and in the runway direction climbing to 3,000 ft. On reaching 3,000 ft the twin had commenced to take off on RWY05 and the Dash-8 was at the holding point. The pilot called on the radio that they would orbit at 3,000 ft until the Dash-8 had taken off. The pilot then heard the twin confirming it was an IFR flight for Sydney, however the QANTAS kept asking for the aircraft position after even after the pilot had called their position and height. Another aircraft copied the pilot's transmission to the QANTAS. Following the Dash-8's departure the pilot descended to 1700 ft to enter downwind for RWY05. After the pilot's call another aircraft called that they had turned to downwind for RWY05, then asked the pilot to Go-Around as they had priority. The pilot climbed to 3,000 ft to be well clear and wait the landing of this aircraft where they then descended to enter downwind for RWY05, landing satisfactorily.
OUTCOME: Operations reviewed report and believe that if the pilot has a similar situation again, another aircraft with working VHF radio fly in company with the aircraft to ensure adequate radio communications are maintained. This is in line with CAAP 166-1 (3) recommendations. |
13/4/2016 |
OCC0622 |
Bathurst |
NSW |
Jabiru |
J170 |
Jabiru |
2200B |
Glider and tug combinations operating on RWY08 conducting Left Hand (LH) circuits. Powered aircraft ...
|
Glider and tug combinations operating on RWY08 conducting Left Hand (LH) circuits. Powered aircraft conducting operations on RWY17. (RWY08 is not considered serviceable for powered aircraft due to high glider and tug activity inside the active RWY.)
Jabiru called inbound from the South and arrived to a busy circuit with other powered aircraft conducting LH circuits on RWY17. Gliders and tug aircraft were in operation on RWY08. Using standard procedures Jabiru announced its intentions and joined an early downwind (Left) for RWY17. Once established on downwind RWY17 Jabiru communicated with Glider and Ground to confirm separation between the gliders that were operating in the vicinity. Glider Ground advised there were two gliders “thermalling 4000’ off the threshold RWY26” and the pilot confirmed that they had them both sighted. Jabiru continued with the circuit calling both Base leg and Final approach, before landing on RWY17 and was maintaining a look-out for other aircraft (including Cessna in front, Diamond behind and the two gliders) with which the pilot had lost sight during turns to Base and Final (Jabiru being a high wing aircraft).
Once Jabiru had touched down on RWY17 the pilot noticed a glider on short final for RWY08 (at the Jabirus' 2 o'clock position) it was then the pilot decided that they did not have sufficient time to stop before RWY08. Jabiru applied full power to cross RWY08 as quickly as possible as it was the pilots best option to keep clear of the glider. Once Jabiru reached flying speed the pilot took-off and announced their intention to conduct another circuit.
OUTCOME: ATSB and RAAF have investigated this occurrence. The ATSB have provided a short bulletin on the investigation which can be read by accessing https://www.atsb.gov.au/publications/investigation_reports/2016/aair/ao-2016-034/ |
13/4/2016 |
OCC1045 |
Bendigo |
VIC |
Tecnam |
P92 Super Echo |
Rotax |
912 ULS |
Check flight carried out for pilots use of disabled control. Subsequent to flight it was found that ...
|
Check flight carried out for pilots use of disabled control. Subsequent to flight it was found that the Modification had not been approved by the aircraft manufacture as required for a LSA aircraft.
OUTCOME: RAAus Technical Manager has reviewed the report. The report has indicated that the aircraft is an LSA however it is actually type certified. The aircraft is currently about to complete the MARAP certification for the fitment, and formal approval, of the modification. |
11/4/2016 |
OCC0634 |
Mallee Highway |
SA |
Airborne |
ST 292 |
Rotax |
582 |
Pilot was flying circuits in the area and landed hard on the highway causing substantial damage to t...
|
Pilot was flying circuits in the area and landed hard on the highway causing substantial damage to the aircraft with the pilot being hospitalised. The pilot had no memory of the accident or shortly prior to the occurrence. Local pilot instructor assessed the scene after the accident and believes the most likely reason would appear a whirly wind struck the aircraft on landing. The pilot was the only person involved.
OUTCOME: Runway-Loss of Control (R-LOC) with environmental contributing factors. Weight shift pilots are reminded that decreased control authority in turbulence can increase risks especially in take off and landing. In this case localised turbulence due to the release of thermal convection was a significant contributor to the accident. These effects are not restricted to the hottest part of the day and can be prevalent as afternoon conditions change particularly if a "trigger" such as a landing aircraft disturbs a parcel of warmer air on landing. |
9/4/2016 |
OCC0652 |
Lancefield |
VIC |
Brumby |
LSA R600 |
Rotax |
912ULS |
The RAAus component of the investigation into the fatal accident near the aerodrome of Penfield, Vic...
|
The RAAus component of the investigation into the fatal accident near the aerodrome of Penfield, Victoria involving RAAus CFI and pilot was completed in accordance with RAAus usual protocols. The Coroner has advised RAAus on 27 April 2018 there were no significant safety outcomes related to recreational aviation activities. RAAus continue to work at the invitation of state and territory police to provide industry and aviation specific subject matter experts to investigate fatalities relating to recreational aircraft accidents. This forms parts of RAAus overall strategy to inform members on safety related matters that may affect them and assist local authorities in determining what occurred. These investigations are conducted to ensure any relevant safety matters are provided to RAAus members and reduce the likelihood of a reoccurrence. |