AAIU Reports
Final Report: Accident, Ozone Delta 3 (Paraglider) Ballinacor, Co. Wicklow 11 May 2019 Report 2019-010
Final Report: Accident, Cessna 750, Citation X+, (N752TX) Cork Airport Co. Cork. Report: 2019-009
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Preliminary Report: Accident, BRM Aero, Bristell NG5, (G-OJCS) Belan, Co. Kildare 13 June 2019. Report: 2019-008
Please see the below Preliminary Report.
NOTE: This Preliminary Report contains information, as known at this time, and does not contain analysis or conclusions. This information is therefore subject to change and may contain errors; any errors in this Report will be corrected in the Final Report.
Final Report: Accident Tecnam P2002-JF, (EI-WAT) Cork Airport, Co. Cork. Report – 2019-007
Final Report: Accident Cessna 140, (EI-AEM) Snug Beag Airfield, Co. Westmeath. Report – 2019-006
SYNOPSIS
Whilst landing at a private airfield, near Delvin, Co. Westmeath, the Cessna '140' aircraft, with one Pilot on board, experienced a bounced landing. Following the bounced landing, the Pilot applied the brakes in an attempt to bring the aircraft to a halt. The aircraft subsequently pitched forward, overturned and came to rest, inverted, on the runway. The Pilot sustained minor bruising. There was no fire.
Interim Statement: Accident involving a CESSNA 208B (G-KNYS). Near Clonbullogue Airfield (EICL) 13 May 2018, Report – 2019-005
INTERIM STATEMENT
Accident involving a CESSNA 208B (G-KNYS) Near Clonbullogue Airfield (EICL) 0n 13 May 2018. Report – 2019-005
A Preliminary Report on this accident was published on 11 June 2018.
EU Regulation 996/2010 requires that, if the Final Report cannot be made public within 12 months, the safety investigation authority shall release an interim statement at least at each anniversary of the accident or serious incident, detailing the progress of the investigation and any safety issues raised.
This Interim Statement should be read in conjunction with the published Preliminary Report.
Final Report: Serious Incident, Airbus A320-214 (EI-GAL). Cork Airport, 11 November 2017. Report – 2019-004
SYNOPSIS
Following a diversion due to fumes in the cockpit, the Airbus A320 aircraft landed at Cork Airport (EICK) at 13.00 hrs on 2 November 2017. Emergency services met the aircraft on the runway and after a short assessment, the aircraft taxied to stand. When the aircraft was parked on stand the Commander directed the passengers to disembark the aircraft immediately. The Commander had intended that an expedited disembarkation be performed. However, some of the passengers opened the emergency overwing exits and disembarked using the escape slides. There were no injuries, but a passenger later became unwell and was taken to hospital.
Final Report: Serious Incident Airbus A330-202, (EI-LAX) On Take-Off, Dublin Airport 28 December 2017 Report – 2019-003
SYNOPSIS
Just after take-off from Runway (RWY) 28 at Dublin Airport (EIDW), on a scheduled passenger flight to Los Angeles International Airport (KLAX), the Flight Crew of the Airbus A330 aircraft received a No. 2 (right-hand) engine fire (ENG 2 FIRE) warning, which required the No. 2 engine to be shut down. Following the shutdown, the fire warning ceased. The Flight Crew declared a MAYDAY (state of emergency) to Dublin Air Traffic Control (ATC) and also pressed the AGENT 1 pushbutton, thereby discharging an engine fire extinguisher into the engine compartment.
Following a review of the situation, the Flight Crew elected to proceed to Shannon Airport (EINN), which had a longer runway than those at EIDW. A holding pattern was entered near EINN to consume fuel and lighten the aircraft for landing. After approximately 20 minutes in the hold, an overweight landing was performed on RWY 06. The aircraft was brought to a stop on the runway, and was inspected by the Airport Fire Service (AFS), who advised that there was no apparent damage. The aircraft then taxied to its parking stand, where all passengers disembarked normally. No injuries were reported.
The ENG 2 FIRE warning was subsequently found to have been caused by hot, high pressure bleed air escaping into the No. 2 engine compartment as a result of the fatigue failure of a short section of No. 2 engine’s high pressure bleed air ducting.
