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| <span style="font-size:medium; font-weight:normal;">[[E170, en-route, Ishioka Japan, 2014|Separation minima may not always provide adequate protection against wake turbulence in trail]]</span>
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| <span style="font-size:medium; font-weight:normal;">[[B739, Singapore, 2013|The importance of a system for validating that specified ground handling procedures are being followed]]</span>
<span style="color:#AAAAAA;"><sup>posted 24 April 2017 in [[:Category:Accidents and Incidents]]</sup></span>
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<span style="color:#AAAAAA;"><sup>posted 1 May 2017 in [[:Category:Accidents and Incidents]]</sup></span>
  
On 29 April 2014, an aircraft being operated in accordance with ATC instructions in smooth air conditions suddenly encountered an unexpected short period of severe turbulence which led both members of the cabin crew to fall and sustain injury, one a serious injury. The Investigation concluded that the turbulence encountered was due to an encounter with the descending wake vortex of a preceding aircraft.
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On 26 May 2013, about 20 minutes after arrival at Singapore for a turn round, a Boeing 737-900 was suddenly rotated approximately 30 degrees about its main gear by a relatively modest wind gust and damaged by consequent impacts. The Investigation concluded that the movement had been due to the failure to follow manufacturer's guidance on both adequate chocking of the aircraft wheels and the order of hold loading.
  
<div style="text-align:right;">[[E170, en-route, Ishioka Japan, 2014|'''''Read more >>''''']]</div>
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<div style="text-align:right;">[[B739, Singapore, 2013|'''''Read more >>''''']]</div>
 
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Revision as of 09:07, 30 April 2017

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Runway Excursion Runway Incursion Wake Vortex Turbulence Weather Emergency and Contingency
Highlighted Article
The importance of a system for validating that specified ground handling procedures are being followed

posted 1 May 2017 in Category:Accidents and Incidents

On 26 May 2013, about 20 minutes after arrival at Singapore for a turn round, a Boeing 737-900 was suddenly rotated approximately 30 degrees about its main gear by a relatively modest wind gust and damaged by consequent impacts. The Investigation concluded that the movement had been due to the failure to follow manufacturer's guidance on both adequate chocking of the aircraft wheels and the order of hold loading.

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