Dispatch with Upper Wing Frost
Latest update
Performance and Operations Conference – Paris 2009
Presented by
Florent PETTENI
Flight Operations Engineer
Performance and Operations Conference - Paris 2009 May 2009 Page 2
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Content
􀃒
Clean WingConcept
􀃒
SurveyResults
􀃒
Airbus Objective
􀃒
Mitigation Means
Performance and Operations Conference - Paris 2009 May 2009 Page 3
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Content
􀃒
Clean WingConcept
􀃒
SurveyResults
􀃒
Airbus Objective
􀃒
Mitigation Means
Performance and Operations Conference - Paris 2009 May 2009 Page 4
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Current Airbus Recommendations
•
Clean wing concept remains applicable
􀀗
Exceptfor:
–
Upper surface of the fuselage
–
Lower wing up to 3mm (1/8 inch)
Performance and Operations Conference - Paris 2009 May 2009 Page 5
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Content
􀃒
Clean WingConcept
􀃒
SurveyResults
􀃒
Airbus Objective
􀃒
Mitigation Means
Performance and Operations Conference - Paris 2009 May 2009 Page 6
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Survey Results (Answers)
•
About 120 answers on all Airbus aircraft type (except A380)
•
8 airlines not affected
AnswersA32077A330/A34032A300/A31010Total119
Performance and Operations Conference - Paris 2009 May 2009 Page 7
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Survey Results (Answers)
•
27 airlines scattered around the world
THANK YOU FOR YOUR CONTRIBUTION
Performance and Operations Conference - Paris 2009 May 2009 Page 8
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Survey Results (Frost Distribution)
•
Inner fuel tank
Performance and Operations Conference - Paris 2009 May 2009 Page 9
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Survey Results (Frost Distribution)
•
Outer fuel tank
Performance and Operations Conference - Paris 2009 May 2009 Page 10
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Survey Results (Frost Distribution)
•
Above landing gear structure
Performance and Operations Conference - Paris 2009 May 2009 Page 11
　
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