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AIRBUS Aircraft Overview/R&D Needs Presented by Cyril FABRE / Head of Airfield Pavement Federal Aviation Administration Airport Pavement Working Group Meeting

AIRBUS Aircraft Overview/R&D Needs Presented by Cyril FABRE / Head of Airfield Pavement Federal Aviation Administration Airport Pavement Working Group

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AIRBUS Aircraft Overview/R&D Needs

Presented byCyril FABRE / Head of Airfield Pavement

Federal Aviation AdministrationAirport Pavement Working Group Meeting

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

Contents

• Air travel market status

• Airbus orders & deliveries

• Family concept

• Product update: • Single Aisle - A320neo

• Long Range

• A380

• A350

• New Airport challenges

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

Air travel has proved to be resilient to external shocks

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

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1970 1980 1990 2000 2010 2020 2030

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1970 1980 1990 2000 2010 2020 2030

Air travel remains a growth market

World annual traffic (RPKs - trillions)

20-year world annual traffic growth

4.8%ICAO

total trafficAirbus

GMF 2011

Air traffichas doubled

every 15 years

Air trafficwill doublein the next15 years

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Airbus firm orders & deliveries

A300 A310

A318 A319 A320 A321

A330 A340 A350

A380 Total

Firm orders 816 8,251 2,128 243 11,438

Customers 86 242 119 18 334

Aircraft delivered 816 4,903 1,203 63 6,985

Firm order backlog 3,348 925 180 4,453

To end November 2011

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

Airbus products catalogue today ...

• The world’s most modern airliner family

A380 Family

A330 Family

A350 Family

A320 Family

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Commonality brings benefits

11days

7 days

7 days8 days

8 days*

8 days*

2 days

3 days

13 days11 days

2 days*

3 days*

12 days

7 days

7 days9 days*

8 days*

8 days*

2 days

3 days

13 days12 days

2 days*

3 days*

* Projected CCQ durations and subject to approval by the Authorities

“A single qualification to fly aircraft of different size and/or

weight which share theSame Type Certificate”

Same Type Rating

“Qualifying from one aircraft type to another by doing

Difference Training rather than a full Type Rating”

Cross Crew Qualification

“One pool of pilots, flying different aircraft types”

Mixed Fleet Flying

X days

Full Transition Training 24 days

A380

A350

A330

A340

A320

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The best keeps getting betterA320neo - new engine option

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A320 Family – 1 aircraft in 4 sizes

A320

A321

A319

A318

Balanced seating capacity

~ +20%

~ +20%

~ +20%

185 to 220 seats*

150 to 180 seats

124 to 156 seats

107 to 132 seats

* Typical two-class/High density

The right sized Family

9

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A320neo: A320 Family efficiency improvement package

Low risk, minimum change aircraft… yet up to 15% overall fuel burn reduction

Sharklets:

Fuel burn saving on long sectors

Improved field performance

New engines:

Bypass ratio 11 to 12

Up to 81 inch fan diameter

Lower SFC

Lower noise levels

First flight-standard Sharklets completed Nov 2011 Increased take-off

capability

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A320neo increases range, increases revenue

15% more range or equivalent extra payloadMost capable aircraft / Typical 2-class layouts

Current Aircraft neo

4,200 nm

3,750 nm

3,750 nm

or 2t additional payload

or 2t additional payload

or 5t additional payload

A31975.5t MTOW

A32078t & 79t MTOW

A32193.5t MTOW

+600 nm

+500 nm

+650 nm

3,600

3,250

3,100

2,500 3,000 4,000nm3,500

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IIWG 59, Miami, 17- 19 January 2012

A320 Family : runway loading comparison - ACN

A320 option for 4 wheel bogie gear (in-services with 1 airline to meet very low PCN airport operations.Reduces ACN’s by ~ 50%.

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A318 A319 A320 A321

34

4042

55

2933

40

48

Flexible pavement

Category B

Maximum ramp weightACN

Highest

Basic

34

4042

55

2933

40

48

Flexible pavement

Category B

Maximum ramp weightACN

MTOW

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A320neo: Bringing efficiency to the market

Realistic development schedule

Family Target

Milestones

2010 2012 2013 2014 2015

Entry Into Service

2011

Launch

Design

Development to maturity Ramp-up

End of concept phase

First a/c at the FAL

First flight

• Minimum change aircraft allows for realistic 2015 EIS

• Fuel price anticipated to increase as global economy recovers

• A320neo acts as a natural fuel hedge

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IIWG 59, Miami, 17- 19 January 201214

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A330/A340 programme

A330 A340

Seats 253 - 295 295 - 313 - 380

Range nm 7 250 - 5 850 7 400 - 9 000 - 7 900

PowerplantsCF6-80E/PW4000/

RR Trent 700CFM56-5C/

RR Trent 500

First delivery Dec-93 Jan-93

Firm orders 1,184 377

Customers 90 48

Aircraft delivered 828 375

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A340s no longer on Airbus catalog

News in brief 10 November 2011Twenty years after its maiden flight, Airbus has completed production for the A340 jetliner, reflecting changing market dynamics. While new aircraft are no longer to be built, Airbus will continue to fully support the current global fleet of A340s – which are providing reliable ultra long-haul flight services with customers around the world – as long as they are in operation. Four versions of the A340 were produced by Airbus: the A340-200, A340-300, A340-500 and A340-600. Providing extended operating ranges of up to 9,000 nautical miles, this product line allows operators to eliminate unproductive stops, open new routes and match service standards to targeted market needs on very long-haul segments.

Completion of production marks new chapter in the A340 success story

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A330 is a large Family - A330-200F is part of it

A330-200 Freighter, part of a very succesfull family

A330-200

246 passengers*

A330-300

300 passengers*

A330-200F

70t payload

A330 MRTT

Tanker Transport

ACJ330

VIP

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MTOW 233 t (513.7 klb) 227 t (500.4klb)

MLW 182 t (401.2klb) 187 t (412.3klb)

MZFW 173 t (381.4klb) 178 t (392.4klb)

MFC139,090 litres

(36744 USg)

139,090 litres

(36744 USg)

EnginesPW 4000

RR Trent 700

Engine thrust 68 to 72 klb

Max structural payload (gross) 64 t (141 klb) 69 t (152 klb)

Range capability 4,000 nm 3,200 nm

A330-200F Basic data

RANGE MODE PAYLOAD MODE

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Page 19

TPEKIX

LAXSFO

SEAYVR

CTS

ANC

GDX

SYA

PEK

CAN PVG

A330 MTOW developments

A330-200 238t Maximum Takeoff Weight

+5t = 330nm and/or 3.5t cargo*

A330-300 235t Maximum Takeoff Weight

+2t = 135nm and/or 1.4t cargo*

Increased productivity and higher revenues

240 minute

ETOPS**

**Extended-range Twin-engine Operation Performance Standards

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Page 20

A330 Pavement Loading

-200/-200F/MRTT: 22180mm-300: 25375mm

1068

4mm

All

vers

ions

710mmAll versions

1981mmAll versions

1397mmAll versions

A350 XWB Aircraft Classification Numbers*

Flexible Pavement Rigid Pavement

MTOW Tire Pressur

e

High Medium

Low Very Low

High Medium

Low Ultra Low

Metric ton

(Mpa) A B C D A B C D

A330-200 192 1.42 46 49 56 74 43 48 57 66

A330-300 233 1.45 59 63 74 100 55 63 75 87

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A380 Update

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Market validation

All 3 alliances represented

243 firm orders from 18 Customers

17 A380

10 A380

12 A380

19 A380

1 A380

12 A380

2 A380

6 A380

6 A380

5 A380

6 A380

10 A380

90 A380

10 A380

20 A380

5 A380

6 A380

6 A380

Private Customer

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Qantas

Additional airline-announced routes for 2012 shown dotted

Los Angeles

Auckland

Johannesburg

Jeddah

Manchester

Emirates

Singapore Airlines

Air France

Lufthansa

The A380 network keeps growingFlying 51 routes to 28 destinations

Montreal

Paris

Melbourne

Singapore

Washington DC

New York

Korean Air

Bangkok

Seoul

San Francisco

MiamiShanghai

Tokyo

China Southern

Dubai

BeijingZurichRome

FrankfurtMunichToronto

Hong Kong

Sydney

Malaysia Airlines

GuangzhouHouston

London

Kuala Lumpur

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An airport cycle with the A380

Take off and landing • Take off & Landing performance better than existing aircraft

• Superior noise performance

• No runway extension or widening required (shoulders extension only)

Ground maneuvering• No taxiway widening

• Better manoeuverability than current aircraft

• Better pavement loading than current aircraft

At the gate• Code F stands are flexible

• All ground equipments exists today

• Turn around time better than existing aircraft

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A solution for...

• The A380 is part of the solution

CongestionDesigned to minimize modificationsMore passenger per flight = growth with no extra flightsThe easiest solution for growth at congested airports around the world

EmissionsState of the art engines for lower emissions and better local air quality

The lowest fuel burn of any large aircraft, reducing CO2 emissions significantly

NoiseA friendly neighbour: half the noise than a 747-400 with 40% more passengersEven quieter than smaller aircraft

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MTOW: 298 tonsTypical two-class layouts: 369 seatsTypical range: 7,600nm

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A350-800

A350 XWB Family

A350-900

A350-1000

MTOW: 268 tonsTypical two-class layouts: 315 seatsTypical range: 7,800nm

MTOW: 248 / 259 tonsTypical two-class layouts: 276 seatsTypical range: 8,250nm

A350 XWB Airport Operations Overview_V00D10019333_v1

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Span 212’ 5’’ 64.75m Fuselage Length 193’ 3’’ 58.91m Height 55’ 11’’ 17.05m

Span 212’ 5’’ 64.75m Fuselage Length 214’ 1’’ 65.26m Height 55’ 11’’ 17.05m

Span 212’ 5’’ 64.75m Fuselage Length 237’ 1’’ 72.25m Height 56’ 0.3’’ 17.08mFuselage height 239’’ 6.09m

Aircraft Dimensions – Code E design

A350-1000

A350-900

A350-800

Fuselage width (constant part) 234’’ 5.96m

Fuselage height 239’’ 6.09mFuselage width (constant part) 234’’ 5.96m

Fuselage height 239’’ 6.09mFuselage width (constant part) 234’’ 5.96m

A350 XWB Airport Operations Overview_V00D10019333_v1

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Aircraft Design Weights

A350-800 A350-900 A350-1000

MTW (Maximum Taxi Weight) [t] 248.9/259.9 268.9 298.9

MTOW (Maximum Take-Off Weight) [t] 248 / 259 268 298

MLW (Maximum Landing Weight) [t] 190 / 193 205 228.5 / 233.5

MZFW (Maximum Zero Fuel Weight) [t] 178 / 181 192 213.5 / 218.5

A350 XWB solution offers a complete family of aircraft

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Ground Maneuvering: Minimum Turning Width

Minimum Turning Width

Design Targets

A350-800 < 46m

A350-900 < 51m

A350-1000 < 56 m

A350 XWB family will be designed to meet or exceed the manoeuvring capabilities of today's existing aircraft which have similar wheel base

Similar ground manoeuvring to current long-range aircraft

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Aircraft Pavement Loading

A350 XWB Aircraft Classification Numbers*

Flexible Pavement Rigid Pavement

High Medium Low Very Low High Medium Low Ultra Low

A B C D A B C D

A350-800 63 67 76 104 60 66 77 90

A350-900 66 70 80 110 64 71 83 96

A350-1000 54 60 73 103 55 69 88 108

Assumptions

A350-800 A350-900 A350-1000

MRW [kg] 259900 268900 308900

MTOW [kg] 259000 268000 308000

Max aft CG % 35 33 34

% Weight on MLG @ max aft CG 92.849 93.683 94.223

Loaded Tyre Pressure Kpa 1590 1660 1500

* VALUES ARE GIVEN FOR A SPECIFIC MTW (max taxi weight), CG (Max aft. CG position) & TIRE PRESSURE (loaded)

** FLEXIBLE PAVEMENT ACN’s ARE BASED ON THE APPROVAL OF ICAO AERODROME PANEL/ DECEMBER 2006

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Continuous adaptation to new aircraft is required

ICAO CAT D ICAO CAT E ICAO CAT F

New aircraft, new challenges for airports

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What Challenges for Pavement ?

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04/18/23High Tire Pressure Tests - Feb.2011

MTOW Increase

Fuselage length increase

Wing-span increase (& shape) for drag reduction

Fewer wheels for:

Weight saving, noise & drag reduction (approach)

Better maneuverability

but, larger wheels and tires (higher load capabilities

higher braking capabilities)

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Need to think about:

• Continuous traffic growth More overload operations ? / Pavement more stressed

• Better aircraft controllability on ground Canalised traffic, reduced lateral wandering width ?

• Climatic changes Material sensitivity to T°

• More precise pavement design & analysis methods

• Combination of PMS with airport traffic simulation tools

• Advanced & innovative material

• Adapted pavement maintenance programme

• Improved pavement construction techniques

• ...

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© 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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