Airport Compatibility

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1 Presented by Dan COHEN-NIR Programs Director Airbus Americas Holdings Inc. Airport Compatibility Opportunities and Challenges

2 Airport Challenges & Aircraft Design Challenge: Prepare airport infrastructure for wave of replacement of Boeing /300/400, /300, Airbus A /300, A /300 by 787-8/9 and A /900/1000 aircraft Risk of significant shortage of full-width and full-length ADG-V gates Challenge: Prepare airport infrastructure for upcoming replacement of DC-9, MD-80 and early 737 models by A320 and 737 NG (most equipped with blended winglets) Risk of significant shortage of ADG-III gates Challenge: Prepare airport infrastructure for the ADG-VI aircraft (A380/747-8) Challenge: Catch-up airport infrastructure for the early generation replacements (A and ER) in terms of pavement strengthening and taxiway fillet widening

3 Aircraft Wing Span Evolution SOURCE: Adapted from IIWG Commercial Aircraft Design Characteristics Trends and growth projections, 2007 A A A

4 Narrow-Body Aircraft Airport Challenge: Prepare airport infrastructure for upcoming replacement of DC- 9, MD-80 and early 737 models by A320 and 737 NG (most equipped with blended winglets) Terminal/apron Airfield Risk of significant shortage of full-width DG-III/Code C gates

5 Narrow-body Family Looking Ahead Several studies under way at Airbus Short-term improvements Long-term improvements Require a STEP-CHANGE in engine performance (fuel burn, emissions and noise) Either provided by current technology New technology (gear turbo fan, open rotor, else?) May or may not lead to a change in the aircraft footprint

6 New Wide-Body / Long-Range Aircraft Airport Challenge: Prepare airport infrastructure for wave of replacement of Boeing /300/400, /300, Airbus A /300, A /300 by 787-8/9 and A /900/1000 aircraft Terminal/apron Airfield Runway, taxiway system, separations, pavement strength, tire pressure Risk of operational restrictions and shortage of full-width and full-length ADG-V gates

7 Aircraft Wing Span (R)Evolution SOURCE: Adapted from IIWG Commercial Aircraft Design Characteristics Trends and growth projections, 2007 A A A Design for higher fuel efficiency drives the next generation aircraft wingspan closer to the DG-V upper limit Review of the airfield compliance and readiness may be required for aircraft operations replacing those of older generation DG-V and DG-IV aircraft

8 More span but less weight for the same mission SOURCE: Adapted from IIWG Commercial Aircraft Design Characteristics Trends and growth projections, 2007 A A A

9 Focus on A350 XWB Airport Compatibility

10 Airport Categories and Indices A A A A A A Wingspan (ft/m) / / / / / /63.5 ICAO Code letter E E E E E E FAA Design Group V V V V V V Overall Length (ft/m) 198.5/ / / / / /75.4 RFF Category (ICAO) ARFF Index (FAA) 8 D 8 D 9 E 8 D 9 E 9 E

11 Dimensions of the A m (212 ft 5.2 in) m (63 ft 2.6 in) m (218 ft 6.5 in) m (55 ft 11 in) m (219 ft 5.5 in)

12 Dimensions of the A m (198 ft 7.5 in) m (212 ft 5.2 in) m (63 ft 2.6 in) m (197 ft 8.4 in) m (55 ft 11 in)

13 Dimensions of the A m (212 ft 5.2 in) m (242 ft 4.7 in) m (63 m (63 ft 2.6 ft 2.6 in) in) 73.59m (241 ft 5.2 in) m (55 ft 11 in)

14 Aircraft Design Weights Model Maximum Taxi Weight (MTW) Maximum Take- Off Weight (MTOW) Maximum Landing Weight (MLW) Maximum Zero Fuel Weight (MZFW) A kg kg kg kg A kg kg kg kg A kg kg kg kg A kg kg kg kg A kg kg kg kg

15 Aircraft Landing Gear Dimensions wheel track wheel base wheel track wheel base A A A /200LR 12.5m 12.6m 12.6m 12.9m 24.9m 22.2m 25.4m 25.9m A MD-11 A A A /-300ER A m 12.6m 12.6m 12.6m 12.9m 12.9m 12.6m 28.7m 24.6m 25.4m 28.0m 33.1m 31.2m 33.3m

16 Minimum Turning Width A /A A A A /200LR Minimum Turning Width 46.1m 44.2m 47.5m 48m A MD-11 A A m 49m 49.5m 50.5m

17 Rigid Pavement ACN

18 Flexible Pavement ACN

19 Tire Pressure Code Tire Pressure Category W High (No limit) X Medium 15 bar (217 psi) ) Y Low 10 bar (145 psi) Z Very low 5 bar (73 psi) Code Evaluation Method T Technical U Using aircraft (26,200) A Prelim(31,300) (25,200) ER (27,200) A (27,400) ER (24,200) A (26,700) A F (28,100) Aircraft (SWL-kg) (19,300) (13,700) ER (21,600) A300-C4 (19,300) (19,300) (16,100) A (18,000)

20 AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of AIRBUS S.A.S.. 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 S.A.S. 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 S.A.S. will be pleased to explain the basis thereof. AIRBUS, its logo, A300, A310, A318, A319, A320, A321, A330, A340, A350, A380, A400M are registered trademarks.

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