The initial cause of the accident happened eleven hours earlier, during an attempt by operators to fix a blockage in one of the eight condensate polishersthe sophisticated filters cleaning the secondary loop water. These filters are designed to stop minerals and impurities in the water from accumulating in the steam generators and increasing corrosion rates in the secondary side. Blockages are common with these resin filters and are usually fixed easily, but in this case the usual method of forcing the stuck resin out with compressed air did not succeed. The operators decided to blow the compressed air into the water and let the force of the water clear the resin.
Any additional information about any of these incidents would be gratefully received. All on board died. Initial reports are that the aircraft had an unreliable airspeed and the investigation is looking into the new MAX Maneuvering Characteristics Augmentation System.
Reverse thrust was not deployed until Aircraft written off approximately fatalities and 3 survivors. The aircraft veered to the left m down the runway and went over a steep hillside stopping short of the sea.
Aircraft written off but no fatalities. The aircraft suffered a collapse of The accident MLG landing gear then veered off the right hand side of the runway causing the remaining landing gear to collapse.
The right wing of the aircraft went through the perimeter fence causing a fire. Media reporting 29 occupants have been taken to hospital with injuries but no fatalities. The aircraft touched down with 3. The aircraft broke through the airport perimeter fence, car park and dual carriageway before coming to a stop meters beyond the end of the runway.
The aircraft was extensively damaged but there were no reported injuries.
The Italian ANSV has determined that the aircraft crossed the threshold at kt and floated for 14 seconds at a height of ft before touching down m beyond the threshold of Runway 28 LDA 2,m 9,ft which was also wet. It went through the airport perimeter fence at kt.
It then took up the hold for almost 2 hours until commencing its next approach. The aircraft went around from the second approach and crashed shortly after at The preiminary report showed the following inputs: Flap was retracted to 15 as normal by the crew At ft the control column was pushed forward causing the speed to increase to kts and the flap to auto-retract from 15 to 10 SFP aircraft feature.
The thrust reduced for 3 secs causing a deceleration and auto-flap extension back to At ft n the control column was pushed forward and nose down stab trim which lasted 12 secs, both of which resulted in-1g dive to impact.
The strut separated and the left engine contacted the ground. The aircraft stopped on the runway and although there was no fire, fire services sprayed the aircraft with foam. The passengers disembarked via mobile stairs on the runway.
There are no reported injuries to the passengers or crew. The incident was in darkness but the weather was fine. The report issued by the MAK in Russian describes how the crew should have commenced the go-around at a height of 60m but was belatedly initiated at 45m.
This lead to the aircraft descending towards the runway. The gear was retracted before a positive rate of climb had been confirmed.
The inactivity of the first officer prevented rectification of the captain's error.
The aircraft became airborne and the Captain initially elected to divert to Bishkek because of the weather but as the engine and hydraulics failed he elected to return to Osh. On the second landing the landing gear failed on touchdown.The Accident is about a man in his 30's whose life is shattered when his wife dies in a DUI/car accident.
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This page is a complete list of all Boeing write-offs. It should be said that there have been other accidents with more serious damage than some of these listed here, but if the aircraft was repaired they do not appear.
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