Date |
Occurrence # |
Location |
State |
Aircraft |
Model |
Engine |
Model |
Summary |
17/7/2016 |
OCC0717 |
Fort Courage |
NSW |
Jabiru |
J120c |
Jabiru |
2200B |
The pilot and passenger were 8 nm from their destination of Wentworth and were conducting a circuit ...
|
The pilot and passenger were 8 nm from their destination of Wentworth and were conducting a circuit over Fort Courage at 2200ft when an unknown aircraft was noticed overhead within a very close proximity to them. The pilot continued the circuit and then continued to Wentworth.
OUTCOME: Pilots are reminded to maintain good situational awareness through effective scanning and where possible fly at published hemispherical headings even below 5000 AMSL. |
17/7/2016 |
OCC0710 |
Wudinna |
SA |
Jabiru |
J230-D |
Jabiru |
3300-A |
At about 1730 local time the pilot was landing in a paddock on private property and flew into a Mall...
|
At about 1730 local time the pilot was landing in a paddock on private property and flew into a Mallee tree. The pilot had already completed a low pass to confirm where they would land, however landing into the sun distorted their perception of height.
OUTCOME: Loss of control event on landing due to environmental factors. |
16/7/2016 |
OCC0706 |
Dapto |
NSW |
Foxbat |
A22LS Amphibian |
Rotax |
912ULS |
An amphibian aircraft landed in Lake Illawarra with one port side main wheel not fully retracted.
O...
|
An amphibian aircraft landed in Lake Illawarra with one port side main wheel not fully retracted.
OUTCOME: Technical Manager reviewed the report. It was identified that a small stick had punctured the air line for the undercarriage in the floats. The pilot conducted an emergency landing without any major issues. After the incident the owner spoke with the factory and was able to modify the area of concern and no further issues to date. |
14/7/2016 |
OCC0704 |
Private strip, Emu Bore |
WA |
Savannah |
VG |
Rotax |
912 |
During the flight all electrical gauges went to zero. The pilot elected to make a precautionary land...
|
During the flight all electrical gauges went to zero. The pilot elected to make a precautionary landing to check the problem. There was 70nm of rough country to cross before they reached the private strip. There were strong winds gusty winds from the NE. The pilot elected to land on a clay pan. There was no problem with the approach, touch down or holding the line, however the pilot underestimated the extra stopping distance due to the gusting cross wind and clipped a tree.
OUTCOME: Aircraft electrical issues were investigated and the issue was identified as a faulty electrical plug that has since been rectified with no further problems. |
10/7/2016 |
OCC0707 |
Indented Head |
VIC |
Jabiru |
LSA |
Jabiru |
2200A |
All run up and system check were OK and temperature and pressures all in the green. The engine devel...
|
All run up and system check were OK and temperature and pressures all in the green. The engine developed full power on take off with no apparent issues. The aircraft climbed to 1000 ft. and was at cruise power when about 3-5 minutes into the flight the engine suddenly lost all power. The pilot located a suitable paddock and positioned the aircraft for an emergency landing. The pilot briefed the passenger and asked them for assistance to identify power lines and fences. The landing was uneventful with no damage to aircraft or passenger.
OUTCOME: Technical Manager spoke with maintainer who indicated that the engine was a factory rebuilt engine. The engine overheated on number 4 cylinder with the valve seat separating from the cylinder head, which then caused the valve brake. There were indications that the engine overheating may have been pilot induced with a high power high angle of attack climb out rate. Engine has been re-built and has been operating normally since incident. |
2/7/2016 |
OCC0697 |
Palmyra |
QLD |
Tecnam |
P92 Eaglet LSA |
Rotax |
912ULS |
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: The propeller bolts had been re-torqued in the in mor...
|
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: The propeller bolts had been re-torqued in the in morning and completed a flight of 1h with no problems. Shortly after take-off felt a slight vibration in the aircraft that seemed to change with engine rpm. The pilot returned to Palmyra at reduced rpm. After landing, the pilot inspected the spinner and prop and found a small section of the fibreglass cover had lifted off the wood core, approx. 15mm back from the leading edge and near the tip. A small piece of the fibreglass was missing, accounting for the slight vibration. On probing the fibreglass cover, a large section measuring about 120mm from the tip towards the blade root and the full width of the blade was easily peeled off. Inspection of the bond shows no wood fibres attached to the fibreglass part, suggesting a poor bond between the wood core and the fibreglass sheeting. Prop removed and awaiting repair instructions.
OUTCOME: Technical Manager received a response from the factory which refers owners/ operators to the service manual for the propeller. In this case the issue identified with the propeller was to contact the factory (which the owner did in the first case). The owner/ operator has since had a response back from the manufacturer who has had another approved propeller installed with no further issues. Tecnam now use and have approved Bolly propellers. |
2/7/2016 |
OCC0696 |
10 - 08 nautical miles to the South South west of Bendigo Aerodrome |
VIC |
Jabiru |
TBA |
|
|
Numerous attempts were made to contact the pilot of an aircraft (who was also inbound from a similar...
|
Numerous attempts were made to contact the pilot of an aircraft (who was also inbound from a similar direction, at the same height, tracking towards Bendigo aerodrome). No response was heard from the aircraft.
OUTCOME: No further action can be undertaken based on provided information as the registration number is not registered with RAAus. No further investigation possible. Members are advised to ensure they are compliant with CAAP 166-3 or CAR 166-3 regarding pilot responsibly whilst operating in non-controlled aerodrome/CTAF. |
2/7/2016 |
OCC0694 |
Jacobs Well |
QLD |
Slipstream Engineering |
Genesis |
Verner |
V133VM MK |
After finishing a 1.5 hour uneventful flight the pilot landed and then returned to the runway entry ...
|
After finishing a 1.5 hour uneventful flight the pilot landed and then returned to the runway entry to do a circuit. On take off, at 150 ft, the pilot felt a strong engine vibration and experienced complete loss of power. The pilot attempted to land on the remainder of the runway however it was too short. The pilot performed an emergency landing on an extension cane land clearing (slightly longer area and to the left). On touch down the aircraft wing contacted the cane and swung the aircraft 180 degrees The aircraft stopped before entering a creek.
OUTCOME: The engine temperatures showed normal for take-off and the pilot had taxied the length of the runway (700 meters) after the first landing. Maintainer/ owner suggests that a cylinder may have seized due to the cold morning and had not normalized until after the first landing. This is an experimental aircraft with only 90.2 hours on the engine since its last rebuild. |
1/7/2016 |
OCC0695 |
Ballarat Airport |
VIC |
Esqual |
VM-1c |
Rotax |
912 |
Structural modifications were carried out on the aircraft due to a manufacturing flaw (causing signi...
|
Structural modifications were carried out on the aircraft due to a manufacturing flaw (causing significant forward and aft movement of the wings when manipulated by hand). The maintainer arrived at Ballarat to inspect the aircraft and test fly it on behalf of the owner. A thorough pre-flight inspection was carried out, and static engine run ups and taxi tests were conducted over a period of 2 hours. All systems were working as normal and pilot/maintainer taxied to RWY23 to line up for a circuit. Full power was applied, the ground roll and lift off was normal. On downwind a strong smell of petrol was noticed, so the pilot opened the vent in the window and proceeded to turn base. When on base (with a lower nose attitude) the pilot noticed a significant amount of fuel building up at their feet, estimated to be about 10 L. The pilot immediately turned all electrical switches off and pointed the aircraft to the runway. When the pilot was satisfied they could glide in on RWY23 they shut the engine down, unlatched the canopy hatch, and made an uneventful landing.
OUTCOME: Cause of the fuel leak were the fuel vents (this aircraft is a amateur built). The fuel vents on the original Esqual design were located inside the cabin. During the structural modifications, new fuel vent lines were routed to a position under the outboard section of each wing. The new fuel vents were made out of soft PVC tubing cut at a 45 degree angle. This was to give the tanks a slight positive pressure in flight. The fuel vents inside the cabin were never removed or plugged. When the aircraft gained sufficient airspeed after take off, the fuel tanks were pressurised from the airflow coming into the new vents. This in turn caused fuel to flow out of the original vents in the cabin. Fuel continued to flow through the old vents until the airspeed dropped to a level where the pressure was not great enough to continue the flow of fuel into the cabin. |
29/6/2016 |
OCC0693 |
Caloundra |
QLD |
Tecnam |
P92 Echo |
Rotax |
912ULS |
On landing and taxing to an area where the instructor could safely get out of aircraft for the stude...
|
On landing and taxing to an area where the instructor could safely get out of aircraft for the student to continue solo, the instructor noticed fuel coming from the lower engine cowling. The student shut the aircraft down, the fuel was shut off and aircraft pushed away from fuel on tarmac. Upon investigation the aircraft fuel filter in the engine cowling area was found to be stripped of its internal thread and was leaking.
OUTCOME: Technical manager reviewed report and on contact with aircraft operator found that the filter has been replaced and the fuel line has been re-positioned and secured by an appropriate L2. Nil defects evident since. |
29/6/2016 |
OCC0883 |
Orange |
NSW |
Aeropakt |
AP22 Foxbat |
Rotax |
912 ULS |
A student was on a solo flight within the circuit. The instructor was maintaining a listening watch ...
|
A student was on a solo flight within the circuit. The instructor was maintaining a listening watch on the radio and had not heard any calls from inbound aircraft nor an aircraft on approach. As such the circuit check had continued on without any knowledge of the second aircraft having to manoeuvre to avoid separation.
OUTCOME: According to the ATSB report there was radio congestion, as such a call from the inbound aircraft may have been missed during a period of high radio congestion whilst the instructor was supervising the student on their solo check. It is recommended that pilots keep a high level of vigilance during initial turn onto base and final. |
28/6/2016 |
OCC0702 |
Barwon Heads Airport |
VIC |
Sirius |
TL-3000 Sirius |
Rotax |
912 ULS |
After landing on RWY 22 (a grass strip, with medium length grass) the pilot exited the RWY however d...
|
After landing on RWY 22 (a grass strip, with medium length grass) the pilot exited the RWY however didn’t see a shallow drain and subsequently hit the propeller (prop strike). The engine was at idle and the pilot was surprised by the very lightweight construction of blades. Long grass contributed to the event (unable to see the drain).
OUTCOME: Taxiing incident - no further action required. |
27/6/2016 |
OCC0692 |
TBA |
NSW |
Jabiru |
J230-D |
Jabiru |
3300A |
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: Maintainer has advised owner that the engine is defec...
|
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: Maintainer has advised owner that the engine is defective and considered no longer airworthy. The engine has previously over heated and maintenance has not been able to assist in the issues. The engine has a total time of 250 hours. Engine heads are warped and loosening therefore needing adjusting every 25 hours. Owner has requested assistance from RAAus.
OUTCOME: Owner advised that another maintainer has reviewed the engine and identified that the defect related to an engine cooling issue. Aircraft defect has been rectified with a manufacturer modification. |
27/6/2016 |
OCC0698 |
Unknown |
NSW |
Jabiru |
J230-D |
Jabiru |
3300A |
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: The aircraft owners’ mechanic has determined that the...
|
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: The aircraft owners’ mechanic has determined that the engine may no longer be airworthy. The engine had a history of overheating, now the heads are warped and loosening therefore needing adjusting every 25 hours.
OUTCOME: Technical Manager reviewed the report and spoke with current maintainer. Maintainer stated that the engine was originally LAME maintained however during that time the LAME did not address issues with the head. The new maintainer conducted an inspection and decided that the engine should be removed prior to failure - a loan engine (Jabiru 3300A) has been fitted. The maintainer has indicated that the engine appears to have been previously run hot which may be have been due to the operator flying the aircraft with a lean mixture. To date nil defects evident since the engine replacement. |
25/6/2016 |
OCC0687 |
Mildura Airport |
VIC |
Morgan |
Cheetah |
Jabiru |
2.2 |
Nose wheel collapsed after landing however not due to a hard landing. Whilst on roll through the wel...
|
Nose wheel collapsed after landing however not due to a hard landing. Whilst on roll through the weld has given way on the nose wheel assembly.
OUTCOME: This is a 19 registered amateur build aircraft. This aircraft type has a history of failure in the nose wheel design and material in which the manufacturer has addressed previously and offered upgradable parts. |