787 Dream Liner

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787 Dream Liner
Sola Aviation Conference Sept 18-20,2006 Thor
G. Johansen Technical Director Boeing - Europe
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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
Breakthrough passenger cabin
Enhanced flight deck
Overhead crew rests
Advanced wing design
Advanced engines and nacelles
Large cargo capacity
Composite primary structure
Innovative systems technologies
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Compatible with Todays Infrastructure
787-9 A330/340
787-8 767
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Advanced Technology Contributions to 787
Operational EfficienciesDesigned with Extensive
Airline Input for Optimum Operability,
Reliability, Flexibility, Testability,
Maintainability and Repairability
Systems
Engines
Materials
Aerodynamics
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Composite Solutions Applied Throughout the 787
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Composite 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

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Propulsion Systems FeatureKey Technologies

• Engine and nacelle features
• Higher bypass ratio
• No-engine-bleed systems architecture
• Low-noise nacelles with chevrons
• Laminar flow nacelles
• Interchangeable (at the wing)

GEnx
Trent 1000
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Advanced Systems Technologies Provide Value
More Electric Systems Architecture
Common Core Open Systems Architecture
Advanced Flight Controls
Integrated Health Management
Wireless IFE
e-Enabled Systems
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Cargo Capacity for More Revenue
45 more revenue cargo volume
787 Crew Rest isoverhead (forward/aft)
787-8
Bulk
12 LD-3s
5 Pallets
A330-200
A330-200 uses bulk cargo attendant rest or
lower deckmobile crew rest
Passenger Baggage
Revenue Cargo
Bulk Cargo
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A New Standard in Performance
275 SEATS
200 SEATS
300 SEATS
225 SEATS
350 SEATS
400 SEATS
450 SEATS
250 SEATS
500 SEATS
Fuel consumption per seat (lb/seat)
Current Quads
550 SEATS
Current Twins
787
Fuel consumption per trip (lb/trip)

• Tri-class seating
• 3,000 nmi mission

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Quiet for Airport Communities85 dB Noise
Contours at Heathrow
London Heathrow
60 less area affected than the A330 and A340
787 noise footprint stays in the airport property
767-300

• 85 dBA contours
• 3,000 nmi mission

Source MS Mappoint, (c) Microsoft, Inc.
4001041404
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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

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Escalated Scheduled Maintenance Intervals
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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

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Maintenance Works Both Sides of the Value
Equation
Maintenance Program Fully MPD based or CMP/CMMP
(80-20), GoldCare? Key Considerations
Operators 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
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Standardization 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

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BOEING RESEARCH TECHNOLOGY EUROPE (BRTE), 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
• RD 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

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BOEING RESEARCH TECHNOLOGY EUROPE (BRTE), SPAIN
The Fuel Cell Airplane

• Project Objectives Rationale
• Schedule
• Complete on-board installation Oct 2006
• Bench tests Jan 2007
• Ground tests first flight March 2007
• Approach Work with European Partners Spanish
  CAA
• Size weight reduction
• Systems integration
• On-board installation