Date |
Occurrence # |
Location |
State |
Aircraft |
Model |
Engine |
Model |
Summary |
5/3/2016 |
OCC0589 |
Coffs Harbour |
NSW |
Jabiru |
J170-C |
Jabiru |
2200 |
Instructor briefed student pilot in the plane before exiting and confirmed that they were ok with an...
|
Instructor briefed student pilot in the plane before exiting and confirmed that they were ok with another flight to Bundagen and to establish in the training area for 30 minutes. Student pilot taxied from the Aeroclub (via HOTEL ECHO to holding point ALPHA for RWY03 as the instructor insisted they use the main wider runway that the student was used to). Student pilot was given a conditional clearance at holding point ALPHA to line up behind the Foxbat on final. Student pilot read back his clearance with line up behind however the student pilot crossed the holding point in front of the Foxbat. The Foxbat was asked to make a full stop (which they did) and the student pilot was cleared for take off and a right turn in front of the Foxbat. After the student pilot was airborne the Foxbat was cleared for take off doing circuit RWY03. Instructor and CFI questioned the student pilot on their return who explained that they did not see the Foxbat on final and through they were right to enter runway for take-off.
OUTCOME: Non compliance with ATC instruction has been dealt with by the students' CFI. Operations remind all pilots, even those under ATC control, that situational awareness and lookout remain as highest priorities for avoidance of collisions in any circuit area. |
3/3/2016 |
OCC0578 |
Finley Airport |
NSW |
Rand Robinson |
KR2 |
Jabiru |
2200 |
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: Aircraft required possible repair to damaged tail whe...
|
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: Aircraft required possible repair to damaged tail wheel block as well as the right main landing gear (collapsed). On inspection, two mounting bolts holding the main landing gear to the main timber spar were broken with the other two remaining bolts being bent. LAME inspected damage to aircraft and other concerns have been raised during inspection including the main spar needing replacing, concern about the Ballistic chute and the workmanship on the aircraft. A structural engineer is reviewing the aircraft and will provide a report.
OUTCOME: Technical reviewed report and has been notified that this aircraft is beyond repair. The owner has decided to scrap the entire aircraft with the engine/ instrument will be on-sold. |
2/3/2016 |
OCC0577 |
Sunshine Coast |
QLD |
Alpi |
Pioneer Hawk |
Rotax |
912 ULS |
On what was to be the last of six uneventful circuits: At flare, an unexpected gust of wind caused t...
|
On what was to be the last of six uneventful circuits: At flare, an unexpected gust of wind caused the aircraft to balloon and descend heavily onto the nose wheel. Full power was applied immediately and a further circuit flown. Pilot reported to the tower there was extreme difficulty moving the rudder pedals and nose wheel damage was suspected while in flight.
OUTCOME: A fly past and visual inspection was conducted from the ground with no obvious evidence of any damage. An uneventful landing followed. |
29/2/2016 |
OCC0584 |
Kapunda |
SA |
Flight Design |
Ct-sw |
Rotax |
912 ULS |
At 2315z a 1200 squawk was observed entering R265B at 4500ft without an airways clearance in the vic...
|
At 2315z a 1200 squawk was observed entering R265B at 4500ft without an airways clearance in the vicinity of Kapunda, SA. Broadcasts were made on relevant frequencies prior to the aircraft entering R265B without success and were continued until 2320 when CT4511 answered. The aircraft was identified, the Mode C verified and the pilot informed of the infringement. By the time communications had been established, CT4511 had descended to 3500ft and was established outside CTA.
OUTCOME; Experienced pilot used NOTAM information provided by EFB program that was misread and resulted in loss of situational awareness in regards to active status of R625B within the Edinburgh restricted airspace. Pilot has revised planning and flight management practices to use formal NOTAM services for appropriate awareness and has been educated further on limitations of EFB software.
COMMENT: Operations continue to remind pilots of the limitations in the use of electronic navigation programs and the effect they can have in reducing situational awareness both in flight and in prior flight planning |
29/2/2016 |
OCC0583 |
Moorabbin Airport |
VIC |
Fly Synthesis |
Texan 550 |
Rotax |
912 ULS |
An aircraft was observed (TSAD and visually) entering the control zone tracking south-bound via the ...
|
An aircraft was observed (TSAD and visually) entering the control zone tracking south-bound via the coastal route. A number of unreadable transmissions were received on frequency 118.1. Attempts to contact the aircraft were made on both 118.1 and 123.0.
OUTCOME: The pilot failed to plan and apply suitable tracking requirements to remain OCTA and breached YMMB CTA as a result. Lack of understanding and interpretation of ERSA frequency use in relation to YMMB were also contributing factors in this incident. The pilot has been mentored through Operations investigation and has successfully flown the route subsequent to this event, applying better situational awareness and appropriate buffers when transiting this area. |
28/2/2016 |
OCC0573 |
Dayboro - Oakey |
QLD |
ICP SRL |
Savannah |
Rotax |
912ULS |
On track YCAB - Gatton the pilot climbed to clear the D'Arguila Range through scattered cloud until ...
|
On track YCAB - Gatton the pilot climbed to clear the D'Arguila Range through scattered cloud until they were established over the tops at 4,500'. Cloud ahead was seen as 7/8 and rising rapidly, so over Lake Wivenhoe area the decision was made to return YCAB. The pilot commenced climbing to remain above cloud. Over the Dayboro area previously scattered cloud had increased in thickness and was rising rapidly, with no gaps large enough to allow descent below the base or descend to the LL of the BN controlled airspace towards YCAB. The pilot continued climbing to remain above cloud, circling Dayboro - Kilcoy. Passing through 6,000' contact was made with BN Centre to request assistance, initially to return to overhead YCAB via controlled airspace. BN advised to remain below 7,500' and track for Oakey maintaining visual at all times. From Eskvale Vectored by Oakey Approach to their field, which was CAVOK. The pilot landed OK and re-planned for deviation track to the west after a MET briefing at Oakey. The pilot continued flight to home 15 miles south of Tenterfield, remaining in VFR west of the cloud @ 5,000'.
OUTCOME: Pilot has analysed the event and agreed to change focus on use of aircraft for transport and only travel any XC routes based on met conditions with a high probability of continuing VMC. Further enhanced situational awareness and decision making will be incorporated by this pilot. |
28/2/2016 |
OCC0572 |
Wyalla |
QLD |
Aeropup |
TBA |
Aeroconversions Inc |
Aerovee 2.0 |
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: The exhaust tail pipe cracked and separated from the ...
|
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: The exhaust tail pipe cracked and separated from the main exhaust on the left hand side of motor.
OUTCOME: Technical have reviewed report. Defect picked up by owner operator and is a common issue with VW engines. Crack identified which shows care and inspection from operator and defect will be rectified. |
28/2/2016 |
OCC0575 |
Palmyra |
QLD |
Tecnam |
P92 Eaglet LSA |
Rotax |
912ULS |
During the monthly Aero Club spot landing competition, the plane stalled approx 0.5m above the runwa...
|
During the monthly Aero Club spot landing competition, the plane stalled approx 0.5m above the runway and dropped onto the right hand main gear, resulting in a slightly bent right hand main gear leg.
OUTCOME: Identified as Runway-Loss of control (R-LOC). Pilot failed to adequately identify and correct pre- stall condition in the landing phase of flight. Contributing factors may have been HF related due to performance expectations in organised short landing event. |
27/2/2016 |
OCC0580 |
Tyabb |
VIC |
UFO |
5 |
Rotax |
503 |
Aircraft conducting flight testing: all previous flying had been conducted in calm conditions howeve...
|
Aircraft conducting flight testing: all previous flying had been conducted in calm conditions however pilot needed to test how the aircraft handled winds. Pilot flew aircraft in the morning however by mid afternoon Tyabb had a light quartering cross wind from the right. On take-off, circuit and landing the aircraft handled well however, on roll out, the weather changed caused the aircraft to cock off the runway onto the grass and was almost stopped when it hit a small dip and tipped on its nose. Minor damage to aircraft and no injuries.
OUTCOME: In tail low attitude the fin and rudder are probably blanketed by the large round wing with no amount of rudder stopping it weather cocking. Pilot will be modifying aircraft to a nose wheel as they previous flew UFO2 and UFO3 on nose wheels with no problems. Flight test continues: This is a one off design with no data on how the aircraft will perform. The aircraft handles well in the air however due to being so light it is susceptible to wind sheer on the ground. |
27/2/2016 |
OCC0579 |
Medlow Bath (Katoomba Airfield) |
NSW |
Jabiru |
ST 3 |
Jabiru |
2200A |
Fatal Accident involving RAAus member. RAAus accident consultants are assisting police in determinin...
|
Fatal Accident involving RAAus member. RAAus accident consultants are assisting police in determining the causal factors that led to the accident. A special Enews was published http://www.vision6.com.au/em/message/email/view.php?id=1178971&u=70000 |
27/2/2016 |
OCC0576 |
Drouin South |
VIC |
Evektor |
Sports Star |
Rotax |
912 ULS |
Engine malfunction on takeoff at 300/400 feet. Pilot managed to turn aircraft around however had to ...
|
Engine malfunction on takeoff at 300/400 feet. Pilot managed to turn aircraft around however had to land with a tail wind.
OUTCOME: Engineer conducted an inspection of the aircraft. On review of the aircraft location and fuel it was believed the engine malfunction may have been caused by the use of MOGAS (fuelled from a local service station by jerry can) and contamination by water. Additionally carburettor icing may have also been the casual factor for the malfunction.The engineer spoke with the owner operator and suggested that the aircraft be operated on AVGAS for a period of time as a refinement process is a lot more stringent than decanting fuel from a jerry can purchased at the local service station. |
26/2/2016 |
OCC0591 |
Callington |
SA |
Airborne |
XT912S |
Rotax |
912 |
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: During annual service, fuel filter housing was found ...
|
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: During annual service, fuel filter housing was found broken when approached to change the filter element - aircraft flown 13 days previously with no defect. Appears to be metal failure, poor quality alloy casting in fuel filter. Initially though to have been tampered with but on closer look appears to be metal component failure due to poor quality casting which resulted in a very weak point. Owner has noted on WWW that some aircraft have the two ends safety tied however doubts that would have prevented the failure. The top 12-15 litres of fuel leaked out and evaporated while hangared. In the found state the engine could not have been started.
OUTCOME: Technical have contacted the manufacturer who have said that this defect is the first of its kind reported to the manufacturer. They are currently reviewing this specific fuel filter in regard to the material. |
26/2/2016 |
OCC0568 |
Goulburn |
NSW |
Evektor |
Sportstar Plus |
Rotax |
912 |
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: Hair line cracking around the attachment point of the...
|
OCCURRENCE DETAILS SUBMITTED TO RAAUS: DEFECT: Hair line cracking around the attachment point of the main landing gear to the sub frame of the aircraft was detected during the annual inspection.
OUTCOME: Owner contacted manufacturer and a directive from Evektor engineering was forwarded with drawings, specifications and instructions to complete the repair.
LAME effected the repairs in accordance with the directive and factory repair schedule. |
22/2/2016 |
OCC0571 |
Lincoln Skypark |
SA |
Flight Design |
Ct-sw |
Rotax |
912 ULS |
While on final approach to RWY27 (above Skypark) wind shear was encountered close to the threshold f...
|
While on final approach to RWY27 (above Skypark) wind shear was encountered close to the threshold forcing the aircraft to land heavily 30m short of the threshold on a perimeter road. This had wheel ruts which impacted the nose wheel and forced it upwards resulting in damage to engine frame.
OUTCOME: Pilot reported changing weather at the time which may have been a contributing factor to the identified meteorological event and failed to adequately identify and respond to conditions in the landing phase of flight. |
22/2/2016 |
OCC0567 |
Moorabbin Airport |
VIC |
Aeroprakt |
A22LS |
Rotax |
912ULS |
Student was assessed to a solo standard and sent on a successive solo. Solo student was asked to fol...
|
Student was assessed to a solo standard and sent on a successive solo. Solo student was asked to follow a Decathlon which was flying a wider than normal circuit. Student reported he had the aircraft sighted initially, however approaching late downwind lost sight of the preceding aircraft and student conducted base turn wider than normal. By this time the Decathlon had already taken evasive action with the student realizing he had turned too early. The tower controller then notified the student he had over taken the Decathlon and the controller re-sequenced the aircraft as being ahead of the Decathlon with the student apologising on the radio for over taking the Decathlon.
OUTCOME: CFI counselled Instructor. Student sent early on solo and did not sight aircraft whilst conducting circuit. Additional training provided to student. Incident presented no safety risk and not escalated by ATC. |