1. Southampton 2 P Bradshaw EDXCW

2. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Develop Capabilities for Multiple Challenges The idea is to select the concepts to explore the more relevant capabilities and meet the widest range of challenges Past : one single concept to best meet all requirements Past : one single concept to best meet all requirements Past : one single concept to best meet all requirements Today : a family of concepts tailored to fit specific sets of requirements

3. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Understand the Challenges The key driving factors for the future air transport system have been captured and analysed MARKET REQUIREMENTS 1. High Productivity 2. Low cost of operation 3. Superior reliability/maintainability 4. Comfort / health driven cabin design 5. Low cost of acquisition 6. High flexibility/updatability 7. Family Concept design 8. Market specialisation ENVIRONMENTAL PRESSURE 9. Low noise 10. Reduced emissions 11. Low manufacturing impact INTEGRATION IN THE SYSTEM 12. Solution to airport congestion 13. Good airport compatibility 14. Exploiting new ATM opportunities ENVIRONMENT MARKET SYSTEM

4. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Irrespective of final future product configurations, the champions will act as basic vectors, describing the whole set of future capability development Select the Champions From the foreseen range of requirements, Airbus has selected typical concepts, as most able to drive the innovations in their respective field of difficulty : The Simple Flying Bus The Proactive Green The Payload Driven The Value of Speed The Flying Truck

5. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Extend the Capability Limits Development of the Champion Concepts will extend the capability limits beyond the natural trend of the classic configuration, as shown in the following assessment Classic Configuration (ref.) Simple Flying Bus Proactive Green Payload Driven Value of Speed 1 Value of Speed 2 Flying Truck SystemMarket Environment Classic configuration used as reference (red line)

6. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Wing & High Lift Devices

7. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Weight and Drag Balance Minimising Operating Cost means balancing weight and drag benefits drag MWE datum +5dc -5dc datum -1t -2t +2t +1t

8. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Span vs Area vs Block Fuel Span and Area Trades Mission Efficiency -6 -4 -2 0 2 4 6 DOCM Block Fuel Change [%] -15 -10 -5 0 5 10 15 Area Span Baseline 33.4m 38.7m 125m 2 145m 2 Fuel limit boundary 3500nm Design Mission (500 nm) Vapp limit const. AR TTC limit

9. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Span vs Area vs DOC/ Weight Area Baseline 33.4m 38.7m 125m 2 145m 2 wing weight for iso Vapp Span and Area Trades Operator Cost -0.4 -0.3 -0.2 -0.1 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 EDP Change [%] -4 -2 0 2 4 6 Area Span Baseline 33.4m 38.7m 125m 2 145m 2 CoC Design Mission (500 nm) Fuel Price assumened at 0.7 $/Gal Other key trades include: DOC vs A/C price vs Fuel price Fuel margin vs Area vs Span Aircraft Price vs Area vs Span

10. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Requirements for High Lift Devices V approach = 1.23 x Vs 1g + 5 kts CL approach = f(CL max ) Cl max limit V approach = 1.23 x Vs 1g + 15 (20) kts cruis e Provide sufficient lift to meet Vapp Avoid tail-strike @ touch down Avoid NLG first impact @ touchdown for High speed landing CLCL Alpha C L0 Overspeed cases Max Alpha cases Tailstrike NLG First Impact

11. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. Typical Airbus Description  High lift: Slats, single slotted fowler flaps & aileron  Roll control: o/b aileron & spoilers  Load control: o/b aileron & spoilers  Lift reduction: spoilers  Speed brake: spoilers

12. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of AIRBUS UK LTD. No intellectual property rights are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of AIRBUS UK LTD. This document and its content shall not be used for any purpose other than that for which it is supplied. The statements made herein do not constitute an offer. They are based on the mentioned assumptions and are expressed in good faith. Where the supporting grounds for these statements are not shown, AIRBUS UK LTD will be pleased to explain the basis thereof.