Date |
Occurrence # |
Location |
State |
Aircraft |
Model |
Engine |
Model |
Summary |
10/1/2016 |
OCC0539 |
Evans Head |
NSW |
Airborne XT 912 |
SST |
Rotax |
912 UL |
While taxiing across the grass area to parking area the pilot failed to observe an aircraft on take-...
|
While taxiing across the grass area to parking area the pilot failed to observe an aircraft on take-off roll on RWY18 and proceeded to cross this active runway. Evasive action was taken and collision was avoided.
OUTCOME: Pilot failed to stop and effectively scan for traffic prior to crossing an active runway. Ops advise likely blind Myopia exaggerated by reduced situational awareness and contributing overload. A more effective plan was suggested and implemented in relation to crossing of the active runway for subsequent movements. |
10/1/2016 |
OCC0550 |
Gold Coast - Amberley Airspace |
QLD |
Tecnam |
P92 2000 RG |
Rotax |
912 ULS |
Airspace Infringement
OUTCOME: Pilot advised that this was the first time he had used the EFB for a...
|
Airspace Infringement
OUTCOME: Pilot advised that this was the first time he had used the EFB for assisted navigation and, while reasonably familiar with the area, lost situational awareness in relation to fixed features at the northern extent of the R625C restricted airspace boundary. This pilot is returning to active recreational flying after a substantial break and has agreed to review disciplines in relation to pre-flight planning for all future flights. |
9/1/2016 |
OCC0890 |
Archerfield |
QLD |
Sling Aircraft |
Sling 2 |
Rotax |
912 IS |
An aircraft was given instructions and clearance to land by ATC on RWY28L however mistakenly lined u...
|
An aircraft was given instructions and clearance to land by ATC on RWY28L however mistakenly lined up to land and landed on RWY28R.
OUTCOME: The pilot was aware that they were distracted with conversation. During the approach the pilot had landed on the wrong runway and confirmed with Archerfield tower that they were cleared to land on runway left, not right. The pilot was given instruction to contact the tower and gave a rundown of their situation from their perspective. The tower staff informed the pilot that the incident would be reported however stated that no harm had been done and the pilot could take it on board as a lesson, never to be repeated. The pilot has suggested that they will always check clearances and visualize the runways (left and right), mentally assigning the correct runway, then rechecking read back. |
6/1/2016 |
OCC0544 |
Goulburn |
NSW |
Brumby |
LSA R610 Evolution |
Rotax |
912 ULS |
Pilot landed and then after taxiing back to the threshold for RWY07 decided to do a circuit and seco...
|
Pilot landed and then after taxiing back to the threshold for RWY07 decided to do a circuit and second landing. During the takeoff roll for the second take-off, Pilot stalled the aircraft at approximately three metres above the ground, the aircraft impacted the ground heavily and caught on fire.
OUTCOME: Pilot stalled the aircraft which resulted in hard landing. Aircraft has been destroyed due to resulting fire. |
5/1/2016 |
OCC0537 |
Maree |
SA |
Tecnam |
P92 Eaglet |
Rotax |
912 ULS |
On approach to Maree with 15nm to run and cruising at 2000ft the engine began to vibrate severely an...
|
On approach to Maree with 15nm to run and cruising at 2000ft the engine began to vibrate severely and was shut down. A successful forced landing was initiated.
OUTCOME: Engine teardown conducted. Engine report was received and stated that on dismantling the engine they found the lower crankcase through bolt to cylinder #4 was broken and protruding away from the crankcase. It appears that the crankcase through bolt to #4 cylinder has broken, allowing oil and also crankcase pressure to escape. This has not allowed the crankcase pressure to purge the oil back to the oil tank meaning oil level in oil tank became too low to allow adequate lubrication to the engine components resulting in the #1 con rod big end failure. |
3/1/2016 |
OCC0535 |
Moyes tow paddock, Forbes |
NSW |
Moyes-Bailey |
Dragonfly |
Rotax |
582 |
Aircraft was stationary (facing into wind preparing to tow a hang glider). A "dust devil" lifted the...
|
Aircraft was stationary (facing into wind preparing to tow a hang glider). A "dust devil" lifted the tail of the aircraft and overturned it. Engine was immediately shut down and pilot removed from aircraft with no injury. The aircraft was righted and removed to hangar for repair.
OUTCOME: Minor damage occurred to the aircraft with no injuries to the pilot. |
2/1/2016 |
OCC0541 |
Archerfield |
QLD |
The Airplane Factory |
Sling 2 |
Rotax |
912 IS |
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: Coolant hose just below engine developed a leak and c...
|
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: Coolant hose just below engine developed a leak and coolant was noticed dripping onto tarmac after flight. OUTCOME: After inspection of the leak it appeared as though the coolant hose had touched the exhaust and subsequently caused slight burn marks and weakened. The hose was subsequently wrapped in a bit of insulation, (making it hard to see the burn mark) to keep it from the exhaust however eventually the hose developed a hole and leaked behind the wrapping |
31/12/2015 |
OCC0607 |
Portland |
VIC |
Jabiru |
J170-C |
Jabiru |
2200 |
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: Oil leak detected on top if #4 cylinder at crank case...
|
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: Oil leak detected on top if #4 cylinder at crank case interface. Bulk Strip by L2 confirmed crank case fretting on 3 crankshaft bearing.
OUTCOME: Rectification via engineering methods and upgrading of components. No issue with this type of engine. |
31/12/2015 |
OCC0534 |
Bundaberg Airport |
QLD |
Jabiru |
SP2200 |
Jabiru |
2200 |
When approaching the airport, to overfly at 1600 feet to join the circuit, the engine began to run r...
|
When approaching the airport, to overfly at 1600 feet to join the circuit, the engine began to run roughly. After approximately 10 seconds there was a loud bang and the engine ran smoothly but with limited power. A successful landing was conducted with no damage to airframe or injuries to crew.
OUTCOME: A later examination of the engine showed that the No.4 piston had disintegrated causing extensive damage to the cylinder and block. |
30/12/2015 |
OCC0532 |
Boonah |
QLD |
FK Lightplanes |
FK9 ELA SW |
Rotax |
912 S |
Routine circuit with intention of touch and go practice in crosswind. On downwind the wind turbulenc...
|
Routine circuit with intention of touch and go practice in crosswind. On downwind the wind turbulence was unpleasant and an aircraft was still back tracking RWY22. Pilot decided to do a full stop on turning downwind the second time and made subsequent radio calls. On final Pilot focused on landing with the left main wheel into the wind and airspeed 65 knots. Pilot rounded out and flared the aircraft which experienced sink and possibly windshear resulting in the aircraft landed firmly and then ballooned. On the second touch the aircraft landed in three points, placing excessive pressure on the nosewheel causing the fork to bend back and wheel spat to break the tail piece (of which penetrated the fibreglass under carriage slightly) immediately above its normal position.
OUTCOME: Damage to aircraft was the result of nose wheel fork bent and wheel spat broken into three pieces. Contributing Factors was the pilot focusing on landing on left main wheel into the crosswind and not 'flying the aircraft', perhaps flared a fraction late. Windshear may have contributed as it was gusting 0 to 15 knots and after ballooning pilot should have maintained more stick back. Pilot conducted additional practice with CFI in crosswind landings. |
27/12/2015 |
OCC0530 |
White Gum Farm Airport |
WA |
Airborne Windsports |
XT-912-B |
Rotax |
912 UL |
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: During a pre-flight inspection it was noticed that #3...
|
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: During a pre-flight inspection it was noticed that #3 exhaust pipe was cracked close to the cylinder head. The crack extended for 3/4 of the diameter of the pipe.
As there has been no impact on the pipe it appears to be a stress crack that appeared during the last flight several days earlier. The pipe is quite long and there is a reasonable amount of torque placed upon it by the weight of the muffler (located on the other side of the engine).
OUTCOME: Uncommon occurrence and seems that the exhaust pipe may have a twist loading on it coupled with vibration from the engine. There was no evidence of 'copper coat' on the junctions. Exhaust pipe was replaced. |
27/12/2015 |
OCC0531 |
Caboolture |
QLD |
Sling |
2 |
Rotax |
912 |
Whilst performing touch and go landings aircraft struck a bird on rotation on the fifth take-off. Pi...
|
Whilst performing touch and go landings aircraft struck a bird on rotation on the fifth take-off. Pilot continued the takeoff as the aircraft was still flying normally and conducted the following circuit, without moving the flaps, and made normal landing.
OUTCOME: On inspection of the aircraft it was found that the bird struck the underside of the fuselage however caused no visible damage to the aircraft. |
26/12/2015 |
OCC0533 |
King Ash Bay |
NT |
Jabiru |
J160 |
Jabiru |
2200A |
Landing on dirt strip 6 to 7 knot crosswind and a gust of wind blew the aircraft to the right side o...
|
Landing on dirt strip 6 to 7 knot crosswind and a gust of wind blew the aircraft to the right side of the strip. As the aircraft touched down the right main wheel sunk on soft dirt which damaged the undercarriage. Pilot tried to steer plane to the left and as the plane came to rest it dipped forward and the right wing tip hit the ground.
OUTCOME: Damage to the undercarriage and the right wing tip of aircraft due to crosswind and hitting soft ground. |
20/12/2015 |
OCC0523 |
Narrabri |
NSW |
Evektor |
Sportstar |
Rotax |
912 |
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: Fuselage mounting structure for right hand undercarri...
|
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: Fuselage mounting structure for right hand undercarriage - yoke assembly cracked and damaged.
OUTCOME: Current LAME liaising with Evektor. Company have sent out new box section to address this failure. Structural failure due to design fault combined with a heavy landing some time in its history. |
20/12/2015 |
OCC0516 |
Private airfield |
QLD |
Savannah |
XL VG |
Rotax |
912 |
On approach landing aircraft encountered a wind-sheer (severe turbulence) losing altitude at 10 mete...
|
On approach landing aircraft encountered a wind-sheer (severe turbulence) losing altitude at 10 meters and contacting ground, aircraft was at full power and elevator applied.
OUTCOME: Pilot was accustomed to conducting flat long approaches and on the day in question the conditions were changing with a developing sea breeze interacting with thermic conditions and exaggerating turbulence. Pilot approach speed was appropriate for zero flap setting. This was the second approach of the flight. Likely cause: Continuation of approach in identified turbulent conditions resulting in Loss of control in landing phase (R-LOC). Contributing factors: Surrounding terrain and cane crop, lack of secondary windsock and configuration in landing. |