787 Dream Liner 787 Dream Liner

Sola AviationConference

Sept 18-20,2006

Thor G. JohansenTechnical DirectorBoeing - Europe

Configured for Success. 787 breaks new ground in Engineering, Materials, Assembly & Passenger Comfort. Features are Designed to Provide Record Low Level Operational Cost in its Class

Configured for Success. 787 breaks new ground in Engineering, Materials, Assembly & Passenger Comfort. Features are Designed to Provide Record Low Level Operational Cost in its Class

Composite primary

structure

Advanced engines and

nacelles

Breakthrough passenger cabin Enhanced

flight deckAdvanced wing design

Innovative systems

technologies

Large cargo capacity

Overhead crew rests

Compatible with Today’s InfrastructureCompatible with Today’s Infrastructure

787-8767

787-9A330/340

Advanced Technology Contributions to 787 Operational Efficiencies

Designed with Extensive Airline Input for Optimum Operability, Reliability, Flexibility, Testability, Maintainability and Repairability

Advanced Technology Contributions to 787 Operational Efficiencies

Designed with Extensive Airline Input for Optimum Operability, Reliability, Flexibility, Testability, Maintainability and Repairability

Systems

Materials

Aerodynamics

Engines

Composite Solutions Applied Throughout the 787Composite Solutions Applied Throughout the 787

Carbon laminate

Carbon sandwich

Fiberglass

Aluminum

Aluminum/steel/titanium pylons

Composites50%

Aluminum20%

Titanium15%

Steel10%

Other5%

Composite is the Smart ChoiceComposite is the Smart Choice

Fatigue and corrosion resistant

Higher strength-to-weight ratio reduces weight

Enables enhanced passenger comfort

Allows larger, more integrated structure

More future growth potential than metals

Propulsion Systems FeatureKey TechnologiesPropulsion Systems FeatureKey Technologies

GEnx

Trent 1000

Engine and nacelle features:

Higher bypass ratio

No-engine-bleed systems architecture

Low-noise nacelles with chevrons

Laminar flow nacelles

Interchangeable (at the wing)

Advanced Systems Technologies Provide ValueAdvanced Systems Technologies Provide Value

Common Core Open Systems Architecture

Advanced Flight Controls

More Electric Systems Architecture

Wireless IFEIntegrated Health

Management e-EnabledSystems

787-8

A330-200

Cargo Capacity for More RevenueCargo Capacity for More Revenue

Passenger Baggage

Revenue Cargo

Bulk Cargo

45% more revenue cargo volume787 Crew Rest isoverhead (forward/aft)

5 Pallets

12 LD-3s

2 LD-3s + 4 Pallets

8 LD-3s

Pallet-mounted Crew Rest

Bulk

A330-200 uses bulk cargo attendant rest or lower deckmobile crew rest

Bulk

A New Standard in PerformanceA New Standard in Performance

300 SEATS

275 SEATS

350 SEATS 400 SEATS 450 SEATS

500 SEATS

550 SEATS

Fuel consumption

per seat (lb/seat)

Fuel consumption per trip (lb/trip)• Tri-class seating

• 3,000 nmi mission

787

Current Twins

Current Quads

225 SEATS

250 SEATS

200 SEATS

4001041404

Feet

Meters

0 5000

0 1500

Quiet for Airport Communities85 dB Noise Contours at HeathrowQuiet for Airport Communities85 dB Noise Contours at Heathrow

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A330-300

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787- 8767-300

• 85 dBA contours• 3,000 nmi mission

60% less area affectedthan the A330 and A340

London Heathrow

787 noise footprint stays in the airport

propertyA340-300 A330-200

The 787 Will Be an Environmental Leader and Subject to Minimum Environmental Taxation

The 787 Will Be an Environmental Leader and Subject to Minimum Environmental Taxation

Focus on life cycle management and -economics

Less fuel used, lower emissions

Quieter for communities, crews, and passengers

Fewer hazardous materials

Less waste in production

Escalated Scheduled Maintenance IntervalsEscalated Scheduled Maintenance Intervals

767 A330 787

Line Maintenance

Interval500 hours 700 hours 1,000 hours

Base Maintenance

Interval18 months 18 months 36 months

Heavy StructuralInspection

6 years 6 years 12 years

Maintenance Works Both Sides of the Value Equation Maintenance Works Both Sides of the Value Equation

Over 12 years the 787 advantage:

113 additional flights

20 fewer line checks

3 fewer base checks

1 less structural check

= Superior Revenue Availability

Maintenance Works Both Sides of the Value Equation Maintenance Works Both Sides of the Value Equation

Maintenance Program: Fully MPD based or CMP/CMMP (80-20), GoldCare?

Key Considerations:

Operator’s Operations, Maintenance and

Reliability Policies and Capabilities

-Fleet Management

-Continuing Improvement Processes

-Non-Mandatory Modifications

-Preventive and Corrective Maintenance

-Maintenance Interval Utilization

-Distribution of HT, CM and OC Components

Operational Environment

Airplane Utilization

Airplane Configuration

Standardization Keeps Overall Costs DownStandardization Keeps Overall Costs Down

Robust catalog Airline designed to easily accommodate

pre-designed offerings Interior configuration can happen later

in the design process

Standard Boeing flt deck philosophy Dual HUD and EFB Common training, Easier transitions

(PQP, STAR) Reduced infrastructure

BOEING RESEARCH & TECHNOLOGY EUROPE (BR&TE), SPAIN

The Fuel Cell Airplane

Project Objectives & Rationale:

Aim: To demonstrate for the first time that a straight level manned flight can be achieved with fuel cells as the only source of power

R&D effort: Hands on integration of novel technology on a prototype • The engine of a motor-glider (Diamond HK36TTC Super-Dimona) has been

substituted by a PEM Fuel Cell/Li ion Battery hybrid power source that will drive an electric motor rotating a variable pitch propeller

• The battery will only be used for take off & climb• The fuel is compressed hydrogen gas (5,000 psi) stored in a light-weight

composite tank

• Current Status:• Glider airframe modified for accommodating new systems• Subsystems manufacturing almost completed and on-board installation on-

going• Post integration functional tests scheduled for Jan 2007

BOEING RESEARCH & TECHNOLOGY EUROPE (BR&TE), SPAIN

The Fuel Cell Airplane

Project Objectives & Rationale:

Schedule: Complete on-board installation – Oct 2006Bench tests – Jan 2007Ground tests & first flight – March 2007

Approach: Work with European Partners & Spanish CAA• Size & weight reduction• Systems integration• On-board installation• Safety requirements• Specifications & tests protocols development for systems acceptance• Post integration tests, experimental airworthiness certificate, ground & flight

tests protocols, flight manuals and public flight demos

Benefits of Work: Develop capability for integration of fuel cell systems in aerospace applications