CRJ900 Product Overview

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Proprietary August 2009 1 This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change. Program Planning, Development & Customer Requirements Bombardier Commercial Aircraft CRJ900 NextGen Product Overview August 2009 W1522308 7/23/2009

description

CRJ900

Transcript of CRJ900 Product Overview

  • Proprietary August 2009 1

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Program Planning, Development & Customer Requirements Bombardier Commercial Aircraft

    CRJ900 NextGen Product OverviewAugust 2009

    W1522308

    7/23/2009

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    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Forward-looking statements

    This presentation includes forward-looking statements. Forward-looking statements generally can be identified by the use of forward-looking terminology such as may, will, expect, intend, anticipate, plan, foresee, believe or continue or the negatives of these terms or variations of them or similar terminology. By their nature, forward-looking statements require Bombardier Inc. (the Corporation) to make assumptions and are subject to important known and unknown risks and uncertainties, which may cause the Corporations actual results in future periods to differ materially from forecasted results. While the Corporation considers its assumptions to be reasonable and appropriate based on current information available, there is a risk that they may not be accurate. For additional information with respect to the assumptions underlying the forward-looking statements made in this presentation, please refer to the respective sections of the Corporations aerospace segment and the Corporations transportation segment in the Management's Discussion and Analysis ("MD&A") section of the Corporation's annual report for fiscal year 2008 available on the Corporations Web site at www.bombardier.com.

    Certain factors that could cause actual results to differ materially from those anticipated in the forward-looking statements include risks associated with general economic conditions, risks associated with the Corporations business environment (such as the financial condition of the airline industry), operational risks (such as risks associated with doing business with partners, risks involved in developing new products and services, product performance warranty, casualty claim losses, risks from regulatory and legal proceedings, environmental risks, risks relating to the Corporations dependence on certain customers and suppliers, human resource risks and risks resulting from fixed-term commitments), financing risks (such as risks resulting from reliance on government support, risks relating to financing support provided on behalf of certain customers, risks relating to liquidity and access to capital markets, risks relating to the terms of certain restrictive debt covenants) and market risks (including foreign currency fluctuations, changing interest rate and commodity pricing risk). For more details, see the Risks and Uncertainties section of the MD&A of the Corporations annual report for fiscal year 2008 available on the Corporations Web site at www.bombardier.com. Readers are cautioned that the foregoing list of factors that may affect future growth, results and performance is not exhaustive and undue reliance should not be placed on forward-looking statements. The forward-looking statements set forth herein reflect the Corporations expectations as at the date of this presentation and are subject to change after such date. Unless otherwise required by applicable securities laws, the Corporation expressly disclaims any intention, and assumes no obligation to update or revise any forward-looking statements, whether as a result of new information, future events or otherwise.

    All amounts are expressed in U.S. dollars unless otherwise indicated.C2520063

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    The Broadest Customer Base for the CRJ Series

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    Introducing the CRJ Extended Family

    CRJ700 Up to 78 seats

    CRJ900up to 90 seats

    CRJ1000up to 100 seats

    CRJ200 50 seats

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    The CRJ Family

    Provides regional airlines with new opportunities for growth: Replacement of existing jet services Increased frequency on existing jet markets

    Replacement of long-haul turboprop services Growth at hubs through:

    Hub extension to smaller markets New non-stop service

    The CRJ family builds businessB1707167

    7/20/2009

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    Benefits of a Family of Aircraft

    Optimize seat capacity to market from 50 to 100 seats Demand-driven dispatch flexibility Common crew qualification (same type rating) Common maintenance and training procedures Common spares Common ground support equipment Common product support

    Reduces fleet costs for increased profitabilityO9411302

    7/24/2009

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    Evolution of the CRJ Family

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    Evolution of the CRJ Family

    CRJ700

    CRJ900

    CRJ1000

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    Change Summary - Family-Driven Concept CRJ700 - CRJ900

    New Winglets for CRJ900

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    ATA Description # of # ofParts in Common %

    ISPL Parts Commonality22 Auto Flight 7 6 8623 Communications 17 17 10024 Electrical Power 7 7 10025 Equipment/Furnishings 2 2 100 26 Fire Protection 7 4 5727 Flight Controls 52 50 96 28 Fuel 38 38 10029 Hydraulic Power 17 17 100 30 Ice and Rain Protection 3 3 10031 Indicating/Recording Systems 13 11 85 32 Landing Gear 44 36 8233 Lights 24 20 83 34 Navigation 20 17 85 35 Oxygen 3 3 100 38 Water/Waste 9 9 100 49 Airborne Auxiliary Power 11 11 100 54 Nacelles/Pylons 93 93 100 76 Engine Controls 3 3 100 79 Oil 3 3 100 80 Starting 2 2 100

    Parts Count Commonality Total 375 352 94

    Parts Commonality CRJ900 - CRJ700

    97% commonality based on initial provisioning costH8682390

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    Introduction of the CRJ NextGen

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    Build On Success The Best RJ Family in the World Just Gets Bigger and Better

    EIS Dec 2000

    EIS Sept 2002

    EIS Oct 2008

    Certification 4Q2009

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    Economics

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    CRJ NextGen Benefits: Fuel Savings - up to 4% Reduction

    The CRJ family offers exceptionally low fuel consumption

    Continued flight testing and service experience, plus technical improvements, are yielding lower fuel burn

    Next Generation improvements reduce fuel consumption by up to 4%

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    $20

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    All by Airline Line - Airline, Heavy- R&O

    Line & Heavy TSP

    CRJ900

    CRJ900 NextGen

    Labour Savings based on DMC Forecast500nm / 78 min flight

    Improved Economics Maintenance - up to 9% Lower Airframe Maintenance Costs

    Longer Times Between Maintenance Checks A Check: 600 Flight Hours C Check: 6,000 Flight Hours Calendar Inspections: 3 years

    Up to 1.4 Days Less Shop Time Per Year = $ Savings Optimized maintenance

    scheduling Refined task procedures to

    reduce labour costs and time Reduced Out-of-Phase

    Maintenance Intervals meaning fewer shop visits

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    Environmentally Friendly Less Fuel Burn = Less CO2 Emissions

    1 2 3 4 5 6 7 8 9 10 11

    Up to

    +27%

    Up to

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    +30%

    Competitor CompetitorCompetitorOlder

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    70-80SEATS

    80-90SEATS

    90-110SEATS

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    Environmentally Friendly Less Exterior Noise

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    70-80SEATS

    80-90SEATS

    90-110SEATS

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    Note: TOC (Top of Climb) requires Predicted Performance

    T O C

    T O C

    VALTV

    VFLC

    VALTS T O D T

    O D

    VALTVVPATH

    VPATH

    VGP

    3.68o

    SEQRYRW06L

    9000

    12700A

    10100A

    9500A

    6000ARWY

    GABRE AWUDE AXFAL FAF526A

    Technological Innovation Available on the CRJ NextGen Family

    Coupled VNAV Allows Flight Plans on the FMS to include altitudes reducing pilot workload

    Allows for constant descent approaches providing opportunity for fuel savings

    Positions the CRJs to take full advantage of WAAS and LPV Approaches

    First major step for an airline moving toward a paperless cockpit EFBs in general, provides flexibility to display a wide variety of information from Jep

    Charts, airline policies/procedures, airport charts, weather, etc.

    FAA - allows own ships position on a Class II EFB, provides pilot situational awareness while on the ground at airports with a moving map of the airport

    CMC EFB

    Audio Video on Demand (AVOD) system provides passengers with latest in entertainment

    IFE Thales 4500i

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    Composite Technology

    The CRJ NextGen features advanced materials technology, such as composite flight control structures.

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    Composite Technology Resin Transfer Molding (RTM)

    Bombardiers RTM process creates a stiff, strong and lightweight structure with integrated members for lower overall parts count.

    RTM Vane

    RTM Flap

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    General Characteristics

    K2818067

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    Standard 4-abreast 88 seat cabin at 31 pitch Forward and aft lavatories standard Flexible cabin service zones Enhanced cabin comfort 80,000 cycle economic operational life Same Type Rating for family from 50 - 100 pax Environmentally friendly Range of 1,517 nm (2,809 km) High speed cruise up to Mach 0.83 (MMO 0.84) Best in class operating costs Exceptional commonality benefits with CRJ700

    CRJ900 General Characteristics

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    General Arrangement CRJ900

    Gross wing area = 760 ft2 (70.61 m2)Wing sweep = 26.62oFuel capacity = 2,903 US gal. (10 989 litres)

    Q2997501

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    Aircraft Design Weights CRJ900

    Lightweight derivative minimizes landing fees and cash DOCs

    * 6.7 lb per U.S. Gallon

    Standard EE ER LE LR

    Max Take-off Weight (MTOW) lb / kg 80,500 / 36,514 81,560 / 36,995 82,500 / 37,421 83,764 / 37,995 84,500 / 38,329

    Max Landing Weight (MLW) lb / kg

    Max Zero Fuel Weight(MZFW) lb / kg

    Operating Weight Empty (OWE) lb / kg

    Max Usable Fuel* lb / kg

    Max Payload lb / kg

    CRJ 900 NextGen

    73,500 / 33,339

    70,000 / 31,751

    48,160 / 21,845

    75,100 / 34,065

    19,450 / 8,822

    21,840 / 9,906 22,590 / 10,247

    70,750 / 32,092

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    Turnaround Servicing CRJ900

    * Based upon 75% load factor, 1.5 bags per pax North American Servicing guidelines

    1. Baggage2. Galley Catering3. Refueling4. Toilet Servicing5. Potable Water

    Optimized layout to allow 20 min. turnaround time

    Turnaround time 20 min*En-route stop 20 min*

    U4627711

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    0 5 10 15 20 25 30

    START UPLAVATORY SERVICE

    WATER SERVICE

    FUEL SERVICE

    READY TO SERVICE

    CLOSE UP

    LOAD BAGGAGE

    UNLOAD BAGGAGE

    READY TO UNLOADCLOSE DOORS

    EMPLANE PAXGALLEY CLEANING & SERVICE

    PASSENGER CABIN CLEANING

    DEPLANE PAXPOS'N A/C, OPEN DOOR

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    Competitive Turnaround Time CRJ900

    Total turnaround time 20 minutesBased upon 75% load factor, 1.5 bags/pax. North American Servicing guidelines

    Q7260174

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    Jetway / Airbridge Compatibility CRJ900

    The CRJ Series design features ensure compatibility with current jetways and airbridges

    A6154410

    7/23/2009

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    Door Locations CRJ900

    * Sill height 68 (1.73 m)I8100862

    7/23/2009

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    Cargo Compartment Characteristics CRJ900

    Ample cargo volume (6.90 ft3/pax [0.20 m3/pax]) satisfies baggage requirements for connection to long haul flights

    Aft Fwd UnderfloorCompartment Compartment

    Class C C

    Standard volume 437.5 ft3 (12.4 m3) 156 ft3 (4.4 m3)

    Maximum capacity 4,375 lb (1,985 kg) 1,700 lb (771 kg)

    Door size (W x H) 43 x 33 2 @ 42 x 20(1.09 m x 0.84 m) (1.07 m x 0.51 m)

    Sill height 91 (2.31 m) 51 (1.28 m)

    Z2089513

    7/23/2009

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    Main Baggage Compartment CRJ900

    Full standing-headroom main baggage compartment allows fast efficient baggage loading minimizing wasted space

    I1012477

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    Secondary Under-Floor Baggage Compartment CRJ900

    Under-floor baggage location facilitates easy, fast ramp check capability

    Compared to the CRJ700 Increased volume by 47 cu. ft. (1.3 m3) Added second under-floor baggage door

    A9924905

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    Interiors

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    Passenger Experience - New Interior Bigger. Brighter. Better.

    Improved Lighting

    Passenger Amenities

    Larger Overhead Bins

    Larger Windows

    New Look

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    Passenger Experience - Latest Interior Look and Feel

    The contoured smooth lines of the new bins and sidewalls are a key element of the new interior appeal

    Sidewall and Ceiling Wash LED Cool Lighting enhances the spacious, inviting interior

    Maximize natural light into the cabin

    Recessed window blinds maximize viewing area

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    Passenger Experience Proven Passenger Appeal Now Even Better

    High passenger acceptance on flights greater that 2 hours

    Velocity Group survey 2006

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    Passenger Experience Flexible Passenger Cabin Meets Airlines Requirements

    CRJ1000 cabin flexibility easily adapts to 31, 32 or greater seat pitches

    Q6070556

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    Larger window is 2" taller - now 15.8 x 9.8

    Dished sidewalls maximize light entering through the window

    24% more viewing area

    Passenger Experience - Larger Cabin Windows 24% More Viewing Area

    Window blind handles notched into sidewall above

    window to expose the full glass area

    Y5068304

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    Passenger Experience - LED Cabin Lighting Overall Improved Aesthetics

    New ceiling design incorporates accent lighting that illuminates bin handles

    New LED cool lighting system washes along ceiling panel

    LED washes light under bin door Bin interior is illuminated when

    bin doors are open

    LED lighting provides reduced maintenance cost

    T1776990

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    Passenger Experience - Business Class Enhanced Passenger Experience

    S4308301

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    In-flight entertainment systems (seatback IFE or PSU mounted IFE) are Next Generation with passenger-friendly features

    Passenger Experience Optional In-Flight Entertainment Available

    Z9330977

    7/20/2009

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    Passenger Experience Cabin In-Seat Power System Available

    An in-seat power system is available on CRJ aircraft This feature is currently available with BE Spectrum seats Power is available for up to 16 seat pairs

    Outlet is designed to accept all common plug configurations LRU supplier is Astronics

    Z8786064

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    Interior Configurations CRJ900

    Wide range of interior layout options Up to 90 seat variants Mixed seat pitch two-class interiors

    Modular interior design adaptable to meet customer requirements Choice of galley modules Choice of wardrobe modules Fwd/aft cabin flexible zones

    Large choice of interiors to suit Operators requirementsE2555115

    7/23/2009

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    Interior Layouts - Single Class CRJ900

    88 seats @ 31 pitch 593.5 ft3 (16.8 m3) baggage 5 Half-size carts

    86 seats @ 31 pitch 593.5 ft3 (16.8 m3) baggage 8 Half-size carts

    G1882684

    7/23/2009

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    Interior Layouts - Dual Class CRJ900

    9 Seats @ 36 pitch 68 Seats @ 31 pitch 637 ft3 (18.03 m3) baggage 8 Half-size carts

    77 Seat configuration3 Abreast business class

    86 Seat configuration4 Abreast business class

    14 Seats @ 34/36 pitch 72 Seats @ 31 pitch 530 ft3 (15.0 m3) baggage 8 Half-size carts

    A4642665

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    Standard 88 Seat Configuration CRJ900

    88 Seats at 31 pitch593.5 ft3 (16.8 m3) checked baggage15 ft3 (0.41 m3) wardrobe/stowage

    5 cart galley

    Under-floor compartment 156.0 ft3 4.41 m3Aft compartment 437.5 ft3 12.40 m3Total checked baggage vol. 593.5 ft3 or 6.74 ft3/pax 16.81 m3 or 0.19 m3/paxOverhead bin 1.50 ft3/pax 0.04 m3/paxUnder-seat stowage 1.50 ft3/pax 0.04 m3/paxWardrobe and stowage 0.2 ft3/pax 0.00 m3/paxTotal volume: 9.9 ft3/pax 0.28 m3/pax

    A Flight AttendantB BaggageBD Baggage DoorE Type III ExitEC Electronics CabinetG GalleyIA Integrated AirstairL LavatoryS StowageSD Service Door W Wardrobe

    N9333159

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    Optional 86 Seat Configuration CRJ900

    86 Seats at 31 pitch593.5 ft3 (16.8 m3) checked baggage33 ft3 (0.93 m3) wardrobe/stowage

    5 cart galley

    Under-floor compartment 156.0 ft3 4.41 m3Aft compartment 437.5 ft3 12.40 m3Total checked baggage vol. 593.5 ft3 or 6.90 ft3/pax 16.81 m3 or 0.20 m3/paxOverhead bin 1.42 ft3/pax 0.04 m3/paxUnder-seat stowage 1.80 ft3/pax 0.05 m3/paxWardrobe and stowage 0.38 ft3/pax 0.01 m3/paxTotal volume 10.50 ft3/pax 0.30 m3/pax

    J4450999

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    A Flight AttendantB BaggageBD Baggage DoorE Type III ExitEC Electronics CabinetG GalleyIA Integrated AirstairL LavatoryS StowageSD Service Door W Wardrobe

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    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Optional 86 Seat Mixed Class Configuration CRJ900

    86 Seats at 31 pitch593.5 ft3 (16.8 m3) checked baggage39.8 ft3 (1.12 m3) wardrobe/stowage

    8 cart galley

    Under-floor compartment 156.0 ft3 4.41 m3Aft compartment 437.5 ft3 12.38 m3Total checked baggage vol. 593.5 ft3 or 6.90 ft3/pax 16.80 m3 or 0.20 m3/paxOverhead bin 1.50 ft3/pax 0.04 m3/paxUnder-seat stowage 1.50 ft3/pax 0.04 m3/paxWardrobe and stowage 0.4 ft3/pax 0.01 m3/paxTotal volume 10.3 ft3/pax 0.29 m3/pax

    O2139305

    7/23/2009

    A Flight AttendantB BaggageBD Baggage DoorE Type III ExitEC Electronics CabinetG GalleyIA Integrated AirstairL LavatoryS StowageSD Service Door W Wardrobe

  • Proprietary August 2009 47

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Optional 90 Seat Configuration CRJ900

    90 Seats at 31 pitch486.5 ft3 (13.77 m3) checked baggage

    8 cart galley

    Under-floor compartment 156.0 ft3 4.41 m3Aft compartment 330.5 ft3 9.36 m3Total checked baggage vol. 486.5 ft3 or 5.41 ft3/pax 13.77 m3 or 0.15 m3/paxOverhead bin 1.42 ft3/pax 0.04 m3/paxUnder-seat stowage 1.80 ft3/pax 0.05 m3/paxWardrobe/Storage 0.4 ft3/pax 0.01 m3/pax Total volume 9.03 ft3/pax 0.25 m3/pax

    L3233656

    7/23/2009

    A Flight AttendantB BaggageBD Baggage DoorE Type III ExitEC Electronics CabinetG GalleyIA Integrated AirstairL LavatoryS StowageSD Service Door W Wardrobe

  • Proprietary August 2009 48

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Optional 75 Dual Class Configuration CRJ900

    10 Seats at 37 pitch65 Seats at 34 pitch

    486.5 ft3 (13.77 m3) checked baggage57 ft3 (1.61 m3) wardrobe/stowage

    9 cart galley

    Under-floor compartment 156.0 ft3 4.41 m3Aft compartment 330.5 ft3 9.36 m3Total checked baggage vol. 486.5 ft3 or 6.49 ft3/pax 13.77 m3 or 0.18 m3/paxOverhead bin 1.50 ft3/pax 0.04 m3/paxUnder-seat stowage 1.50 ft3/pax 0.04 m3/paxWardrobe/Storage 0.76 ft3/pax 0.01 m3/pax Total volume 10.25 ft3/pax 0.27 m3/pax

    A6284886

    7/23/2009

    A Flight AttendantB BaggageBD Baggage DoorE Type III ExitEC Electronics CabinetG GalleyIA Integrated AirstairL LavatorySD Service Door W Wardrobe

  • Proprietary August 2009 49

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Optional 77 Dual Class Configuration CRJ900

    9 Seats at 36 pitch68 Seats at 31 pitch

    637.0 ft3 (18.03 m3) checked baggage9.3 ft3 (0.26 m3) wardrobe/stowage

    8 cart galley

    Under-floor compartment 156.0 ft3 4.41 m3Aft compartment 481.0 ft3 13.26 m3Total checked baggage vol. 637.0 ft3 or 8.27 ft3/pax 18.03 m3 or 0.23 m3/paxOverhead bin 1.50 ft3/pax 0.04 m3/paxUnder-seat stowage 1.50 ft3/pax 0.04 m3/paxWardrobe and stowage 0.12 ft3/pax 0.00 m3/paxTotal volume 11.39 ft3/pax 0.32 m3/pax

    Z4303014

    7/23/2009

    A Flight AttendantB BaggageBD Baggage DoorE Type III ExitEC Electronics CabinetG GalleyIA Integrated AirstairL LavatorySD Service Door W Wardrobe

  • Proprietary August 2009 50

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Passenger Experience Cabin Cross Section

    P3717541

    7/20/2009

  • Proprietary August 2009 51

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Passenger Experience - Larger Overhead Bins up to 27% more roller bags stored

    New Enhanced Overhead Bin Design

    40% Increase in Weight Capacity 9% Increase in Overhead Bin Volume Larger Bin Door Opening - 10.5 Accommodating 10.5 x 16 roller bag Optimized Sizing to Maximize Roller Bag Storage

    CRJ700 up to 27% more, CRJ900 up to 21% more roller bags can be storedI8015634

    7/20/2009

  • Proprietary August 2009 52

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    CRJ900 - Interiors

    Forward flight attendant seat Aft flight attendant seatV2448660

    7/23/2009

  • Proprietary August 2009 53

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    G1 Galley Options CRJ900

    Note: Forward potable water system is offered as a separate option (CR 38-21X)

    G1 galley configured for hot meal service

    CR 25-31-401CR 25-31-402CR 25-31-410CR 25-31-438

    G1 galley

    Snack and hot beverage service galley equipped with provisions for:

    5 Atlas half size carts 2 Coffeemakers

    Hot meal service galley equipped with provisions for: 5 Atlas half size carts 2 Ovens

    Hot meal & hot beverage service galley

    Hot meal & beverage service galley

    All four galleys incorporate a number of features that include:

    2 - 5 storage compartments Water/electrical panel 115V/400Hz electrical power outlet Internal galley water system plumbing (where applicable)

    V6390564

    7/23/2009

  • Proprietary August 2009 54

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    G2 Galley Options CRJ900

    G2 galley configured for snack and hot beverage service

    G2 (2 cart)CR 25-32-402CR 25-32-403CR 25-32-404CR 25-32-451CR 25-32-452CR 25-32-453

    G2 (4 cart)

    Snack service galley equipped with provisions for: 2 or 4 Atlas half size service carts

    Snack and hot beverage service galley equipped with provisions for:

    2 or 4 Atlas half size service carts Hot meal & hot beverage service galley equipped with

    provision for 2 or 4 Atlas half size service carts

    All G2 galleys incorporate a number of features that include:

    3 - 4 storage compartments 1 drawer Water/electrical panel (where applicable) Internal galley water system plumbing (where

    applicable)

    C5438686

    7/23/2009

    Note: Forward potable water system is offered as a separate option (CR 38-21X)

  • Proprietary August 2009 55

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    G3 Galley Options CRJ900

    Snack Service with provisions for: 3 Atlas half size service carts 3 Atlas standard containers

    Wardrobe with provisions for Snack Service 2 Atlas half size service carts 2 Atlas standard containers

    Galley incorporates 2 storage compartments

    CR 25-33-403CR 25-33-407

    G3 galleyD1817550

    7/23/2009

  • Proprietary August 2009 56

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Additional Galley Options CRJ900

    G4 Galley Dry storage equipped with provisions for:

    3 Atlas half size service carts 3 Atlas standard containers

    G5 Galley Snacks and hot beverage service galley equipped with

    provisions for: 2 Atlas half size service carts 2 Atlas standard containers

    Hot meal and hot beverage service galley equipped with provisions for:

    1 oven 1 coffeemaker 2 Atlas half size carts 2 Atlas standard containers

    G6 Galley Dry storage galley equipped with provisions for:

    2 Atlas half size service carts 5 Atlas standard containers

    G4 galleyCR 25-33-404CR 25-35-403CR 25-35-402CR 25-36-401

    G5 galleyG5 galley

    D7297566

    7/23/2009

  • Proprietary August 2009 57

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Customized Galley Features CRJ900

    Customers may select from the following options to create customized galley configurations:

    Atlas standard half size beverage/meal/misc. carts (each)

    Atlas standard unit (each) Atlas standard half size waste cart (each) Atlas standard beverage maker - coffee

    (each) Inventum Water Boiler (each) Oven - 32 casserole (TIA, each)

    G1 galley shown with 2 ovens, 4 Atlas half-size beverage/meal/misc. carts

    and 1 Atlas half size waste cartF9600207

    7/23/2009

  • Proprietary August 2009 58

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Systems

    S1723507

    7/15/2009

  • Proprietary August 2009 59

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Maintenance CRJ900

    Specified for high Mean Times Between Failures (MTBFs)

    Design for quick access and repair ability Aircraft systems LRU removal within 20 minutes APU removal within 45 minutes Engine change within 1 shift

    Baseline maintenance intervals A Check: 600 Flight Hours C Check: 6,000 Flight Hours Calendar Check: 3 Years

    High MTBFs coupled with easy access = reduced maintenance costsV9997134

    7/23/2009

  • Proprietary August 2009 60

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Advanced Technology Utilization CRJ900

    CRJ900 is an advanced technology aircraft

    Avionics 6 screen glass cockpit with an

    integrated avionics suite Growth capability for CNS/ATM

    Powerplant Latest generation CF34-8 engine Full Authority Digital Electronic

    Control (FADEC)

    Landing Gear and Brakes Dual Electronic Anti-Skid System Electronic Brake Temperature

    Monitor System (BTMS)

    Auxiliary Power Unit Fully automatic control Single push button start

    Flight Controls Hydro-mechanical primary controls Control-by-Wire secondary controls

    Hydraulics 3 Independent systems High Pressure 3000 psi

    P3757116

    7/23/2009

  • Proprietary August 2009 61

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Flight Deck CRJ900

    Collins ProLine 4 avionic system selected for all CRJ aircraft to ensure a high degree of commonality

    R9166665

    7/23/2009

  • Proprietary August 2009 62

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Avionics and Cockpit Systems CRJ900

    Designed for 2 person operation Electronic Flight Instrument System (EFIS) consists of 6 screens:

    2 Primary Flight Display (PFD) for flight performance 2 Multi-Function Displays (MFD) for integrated navigation, weather and traffic

    information 2 Engine Indication and Crew Alerting System (EICAS) displays

    Engine Indication and Crew Alerting System (EICAS) provides: Automated visual and aural indications Synoptic pages for systems Primary status pages for systems operation and status

    Avionics and cockpit systems commonality with CRJ700, facilitating Same Type Rating

    N8850422

    7/23/2009

  • Proprietary August 2009 63

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    APU Assembly CRJ900

    Tailcone mounted APU minimizes ramp sound levels,and is not essential for dispatch

    Forward

    R2025545

    7/23/2009

  • Proprietary August 2009 64

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    APU System CRJ900

    Designed for 41,000 ft. operation (full aircraft envelope) APU start capability up to 37,000 ft.

    Fully contained (hub and blades) Controlled by digital Electronic Control Unit (ECU) with

    BITE capability Removable in less than 1 hour Intended to meet ICAO-16 noise requirements

    70 dBA at forward passenger door (ICAO - 15 dBA) Standard equipment on CRJ Series aircraft Non-essential for dispatch

    Y2559044

    7/23/2009

  • Proprietary August 2009 65

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Cabin Temperature Control System CRJ900

    Efficient airflow patterns = stable temperature controlQ9389904

    7/23/2009

  • Proprietary August 2009 66

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Flight Controls - Flaps and Slats CRJ900

    Flap drive system consists of rugged torque tubes and linear ball screw actuators Slat drive system consists of rack and pinions and rotary gear actuators Skew sensing incorporated on flap system

    Slats on CRJ900 enhance field performanceC4189254

    7/23/2009

  • Proprietary August 2009 67

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Electrical Power CRJ900

    Consists of three (3) 40 KVA generators: Two engine - mounted Integrated Drive Generators (IDG) One APU - mounted generator

    Emergency AC power supplied by Air-Driven Generator (ADG) External AC receptacle provided for ground operations

    Provided by four (4) 120 amp Transformed Rectifier Units (TRUs) in nose compartment

    APU and main battery provide additional DC power sources No external DC power connection required

    CRJ900 is predominately an AC aircraft

    AC System

    DC System

    Z2334900

    7/23/2009

  • Proprietary August 2009 68

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Landing Gear CRJ900

    Rugged, durable steel disk braking

    Main landing gear features two steel disk braked wheels per axle (rugged, durable design) Landing gear design life: 80,000 cycles Brake design life: 1,600 landings tires: 250 - 400 landings

    Y6329539

    7/23/2009

  • Proprietary August 2009 69

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    13

    2 Rudder

    3

    1

    3

    2

    1

    1

    1

    1

    1

    2

    2

    3

    3

    3

    1

    1

    2

    2

    3

    3

    23

    Outbd Brakes

    Nose Landing GearNose Wheel SteeringInbd Brakes

    Main Landing Gear

    #3 AAC Motor Pump

    #3 BAC Motor Pump

    Aileron

    #2Engine Driven Pump

    #2ThrustReverser

    #2AC MotorPump

    Multi FunctionOutbd SpoilerMulti Function

    Inbd Spoiler

    InbdGroundSpoiler

    Outbd GroundSpoiler

    LH Elevator

    RH Elevator

    #1 EngineDriven Pump

    #1 ThrustReverser

    #1BAC MotorPump

    No 1 SystemNo 2 SystemNo 3 SystemNo 3 System

    Hydraulic System CRJ900

    Independent hydraulic systems ensure redundancy for safe operation

    Three independent systems supply hydraulics to various aircraft systems Each system sized to meet demands of flight Complete interface with EICAS for ease of operation

    F9838109

    7/23/2009

  • Proprietary August 2009 70

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    LH Engine RH Engine

    Refuel/DefuelManifold

    Filter

    ScavengeEjector

    APU Pump

    Booster Pump

    PP

    P

    APU

    PTransferEjector

    Primary FeedEjector

    XflowPump

    GravityXflowValve

    Firewall SOV

    Drain Ejector

    Fuel System Schematic CRJ900

    Large fuel capacity ensures long-haul operation capability

    Consists of three fuel tank configuration - one centre and two wing tanks Total fuel capacity is 2,903 USG (10,989 Litres)

    Q1142938

    7/23/2009

  • Proprietary August 2009 71

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Propulsion

    A6331343

    7/15/2009

  • Proprietary August 2009 72

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    General Electric CF34-8C5 Engine

    One engine for the whole NextGen family

    Relative to the GE CF34-3B1 engine

    O7369361

    7/20/2009

  • Proprietary August 2009 73

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Powerplant Commonality CRJ700/900/1000

    CRJ700 provides engine normal take-off power optionsto match operational requirements

    P8235042

    7/20/2009

  • Proprietary August 2009 74

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Common Right and Left (CRL) Powerplant Design CRJ900

    CRJ900 features common right and left: Nacelle Fan cowl doors Core cowl doors Thrust reverser Nose cowl

    Engine Build Up Unit (EBU) 80% interchangeability

    CRL powerplant components significantly reduce spares requirementsC8364743

    7/23/2009

  • Proprietary August 2009 75

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Clamshell Design Facilitates Improved CF34-8C5 Core and LRU Access

    Pylon-mounted clamshell doors remain closed between A checks

    G4627486

    7/20/2009

  • Proprietary August 2009 76

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    On-Wing Maintenance for Reduced Costs CRJ900

    Pylon mounted engine, thrust reverser, cowl doors and other components significantly reduce engine change times:

    Hours Crew Neutral engine 6 3 Full Quick Engine Change (QEC) 3 3

    Majority of LRUs changed in 10 to 30 minutes e.g. fuel control 30 min

    lube pump 15 minanti-ice valve 10 min

    C1768536

    7/23/2009

  • Proprietary August 2009 77

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Environmental Compatibility CRJ900 - Certified Emission Levels

    42.8 43

    10.7

    75.2

    19.1

    15.6

    16.6

    0.50

    20

    40

    60

    80

    100

    120

    140

    CO HC NOx Smoke

    g/kNorSN

    ICAO Requirement incl. CAEP/6

    CF34-8C5 Emissions

    Demonstrated ample margin for current and anticipated requirementsG9994953

    7/23/2009

  • Proprietary August 2009 78

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    All CRJ900 weight variants are certified to Chapter IV with good margins

    83.989.1

    92.35.1

    5.2

    6

    75

    80

    85

    90

    95

    100

    Fly-over Lateral Approach

    N

    o

    i

    s

    e

    L

    e

    v

    e

    l

    (

    E

    P

    N

    d

    B

    )

    Margin (ICAO Annex 16 Chapter III )Noise Level (Chapter IV)

    6.3

    265.4

    255

    260

    265

    270

    275

    280

    Cumulative

    N

    o

    i

    s

    e

    L

    e

    v

    e

    l

    (

    E

    P

    N

    d

    B

    )

    Margin (ICAO Ch IV)Acc. Noise Level

    Environmental Compatibility CRJ900 LR - Chapter IV Certified Noise Levels

    Y6879575

    7/23/2009

  • Proprietary August 2009 79

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Performance

    K4039727

    7/15/2009

  • Proprietary August 2009 80

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Performance EFB, CAFM and CIFP

    Electronic Flight Bag (EFB) has been certified by Transport Canada and is available on the CRJ NextGen aircraft

    EFB will provide operators with improved cockpit efficiency

    EFB will enable faster turnaround , optimized flight profile, quicker performance calculations, cost indexing, charting, and flight log management, etc.

    EFB on CRJ NextGen aircraft features note taker, side view, and eDoc browser

    Computerized Aircraft Flight Manual (CAFM) and Computerized In-Flight Planning (CIFP ) have been developed for the CRJ NextGen aircraft

    K9109776

    7/20/2009

  • Proprietary August 2009 81

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    * Type spec aircraft, pax at 225lb, enroute ISA, typical reserve assumptions (100 nm diversion, 45 min hold @ 15000ft, 5% flight fuel contingency)

    Nominal Performance CRJ900

    Standard EE ER LE LRMax Cruise Speed

    (ISA, FL350, 95% MTOW)M / kt

    Take-off Field Length(ISA, SL, MTOW)

    ft / m 5,938 / 1,810 6,099 / 1,859 6,244 / 1,903 6,439 / 1,963 6,553 / 1,997

    Landing Field Length(ISA, SL, MLW)

    ft / m

    Single Engine Ceiling(ISA, 95% MTOW, A/I off)

    ft / m 17,500 / 5,334 17,076 / 5,205 16,700 / 5,090 16,321 / 4,975 16,100 / 4,907

    Range*(88 PAX and M0.78)

    nm / km 1,059 / 1,961 1,172 / 2,171 1,284 / 2,378 1,370 / 2,537 1,517 / 2,809

    0.830 / 478

    5,257 / 1,602 5,349 / 1,630

    CRJ900 NextGen

    W6890627

    7/23/2009

  • Proprietary August 2009 82

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Nominal Performance

    * Type spec aircraft, pax at 225lb, enroute ISA, typical reserve assumptions (100 nm diversion, 45 min hold @ 15000ft, 5% flight fuel contingency) Includes optional NTO+2% Includes optional NTO+5%

    CRJ700 CRJ900 CRJ100070 PAX 88 PAX 100 PAX

    Take-off Field Length(ISA+10, SL) ft / m 4,815 / 1,468 5,457 / 1,663 5,851 / 1,783

    Landing Field Length(ISA+10, SL) ft / m 4,869 / 1,484 5,142 / 1,567 5,514 / 1,681

    Take-off Weight lb / kg 67,286 / 30,520 76,010 / 34,478 82,492 / 37,418

    Landing Weight lb / kg 62,994 / 28,574 71,304 / 32,343 77,251 / 35,040

    500 nm / M0.78*

    X1112642

    7/20/2009

  • Proprietary August 2009 83

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Nominal Performance

    CRJ700 CRJ900 CRJ100070 PAX 88 PAX 100 PAX

    Take-off Field Length(ISA+10, SL) ft / m 5,191 / 1,582 6,066 / 1,849 6,482 / 1,976

    Landing Field Length(ISA+10, SL) ft / m 4,879 / 1,487 5,152 / 1,570 5,527 / 1,685

    Take-off Weight lb / kg 70,958 / 32,186 80,017 / 36,295 86,950 / 39,440

    Landing Weight lb / kg 63,169 / 28,653 71,495 / 32,430 77,463 / 35,137

    1000 nm / M0.78*

    * Type spec aircraft, pax at 225lb, enroute ISA, typical reserve assumptions (100 nm diversion, 45 min hold @ 15000ft, 5% flight fuel contingency) Includes optional NTO+2% Includes optional NTO+5%

    S2334512

    7/20/2009

  • Proprietary August 2009 84

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Payload Range CRJ900 NextGen

    Type spec aircraft, pax at 225lb, enroute ISA, typical reserve assumptions (100 nm diversion, 45 min hold @ 15000ft, 5% flight fuel contingency)

    0

    5000

    10000

    15000

    20000

    25000

    0 500 1000 1500 2000 2500 3000Range (nm)

    P

    a

    y

    l

    o

    a

    d

    (

    l

    b

    )

    0

    2000

    4000

    6000

    8000

    10000

    P

    a

    y

    l

    o

    a

    d

    (

    k

    g

    )

    CRJ900 CRJ900 ER CRJ900 LR

    88 pax

    A2795587

    7/23/2009

  • Proprietary August 2009 85

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Block Time CRJ900 NextGen

    Type spec aircraft, pax at 225lb, enroute ISA, typical reserve assumptions (100 nm diversion, 45 min hold @ 15000ft, 5% flight fuel contingency)

    0

    20

    40

    60

    80

    100

    120

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    180

    100 150 200 250 300 350 400 450 500 550 600 650 700 750 800 850 900 950 1000

    Range (nm)

    B

    l

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    i

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    e

    (

    m

    i

    n

    )

    H4867197

    7/23/2009

  • Proprietary August 2009 86

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Block Fuel CRJ900 NextGen

    Type spec aircraft, pax at 225lb, enroute ISA, typical reserve assumptions (100 nm diversion, 45 min hold @ 15000ft, 5% flight fuel contingency)

    0

    1000

    2000

    3000

    4000

    5000

    6000

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    9000

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    100 150 200 250 300 350 400 450 500 550 600 650 700 750 800 850 900 950 1000

    Range (nm)

    B

    l

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    F

    u

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    l

    (

    l

    b

    )

    0

    500

    1000

    1500

    2000

    2500

    3000

    3500

    4000

    4500

    B

    l

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    )

    G4322285

    7/23/2009

  • Proprietary August 2009 87

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Range from Minneapolis CRJ900 NextGen

    Type spec aircraft, pax at 225lb, enroute ISA, typical reserve assumptions (100 nm diversion, 45 min hold @ 15000ft, 5% flight fuel contingency)G3521741

    7/28/2009

    CRJ900 NextGen

    Standard

    Extended Range

    Long Range

  • Proprietary August 2009 88

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Range from Frankfurt CRJ900 NextGen

    Type spec aircraft, pax at 225lb, enroute ISA, typical reserve assumptions (100 nm diversion, 45 min hold @ 15000ft, 5% flight fuel contingency)P6910278

    7/28/2009

    CRJ900 NextGen

    Standard

    Extended Range

    Long Range

  • Proprietary August 2009 89

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Range from Dubai CRJ900 NextGen

    Type spec aircraft, pax at 225lb, enroute ISA, typical reserve assumptions (100 nm diversion, 45 min hold @ 15000ft, 5% flight fuel contingency)D5615969

    7/28/2009

    CRJ900 NextGen

    Standard

    Extended Range

    Long Range

  • Proprietary August 2009 90

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Range from Hong Kong CRJ900 NextGen

    Type spec aircraft, pax at 225lb, enroute ISA, typical reserve assumptions (100 nm diversion, 45 min hold @ 15000ft, 5% flight fuel contingency)M3056319

    7/28/2009

    CRJ900 NextGen

    Standard

    Extended Range

    Long Range

  • Proprietary August 2009 91

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Economics

    L7997750

    7/15/2009

  • Proprietary August 2009 92

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Economics 500 nm, Jan 09US$, North American Environment

    CRJ series provide exceptional economics and the tradition continues with 16% and 17% lower seat costs for the CRJ900 and CRJ1000

    * $1.95 per Gallon

    CRJ700 CRJ900 CRJ1000Block Time min 92 93 93Block Fuel lb 4,357 4,876 5,234Crew $ 462.54 466.55 466.05Fuel* $ 1258.69 1408.62 1512.04Landing & NavAid $ 196.98 216.09 239.61Insurance $ 82.93 84.76 102.21Maintenance $ 572.59 613.32 661.49Cash cost/trip $ 2573.72 2789.34 2981.40Ownership $ 2035.27 2080.27 2508.45DOC/trip $ 4608.99 4869.61 5489.85DOC/SM $ 8.01 8.46 9.54DOC/ASM 11.44 9.62 9.54

    BASE -15.96% -16.62%

    O9009223

    7/20/2009

  • Proprietary August 2009 93

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Economics 500 nm, Jan 09 US$, European Environment

    CRJ series provide exceptional economics and the tradition continues with 16% and 18% lower seat costs for the CRJ900 and CRJ1000

    * $1.95 per Gallon

    CRJ700 CRJ900 CRJ1000Block Time min 92 93 93Block Fuel kg 1,976 2,212 2,374Crew $ 691.50 697.50 696.75Fuel* $ 1258.69 1408.62 1512.04Eurocontrol, Airport & Nav. $ 959.15 1041.97 1104.16Insurance $ 82.93 84.76 102.21Maintenance $ 572.59 613.32 661.49Cash cost/trip $ 3564.85 3846.17 4076.65Ownership $ 2324.85 2376.26 2865.36DOC/trip $ 5889.71 6222.43 6942.01DOC/KM $ 6.36 6.72 7.50DOC/AKM 9.09 7.64 7.50

    BASE -15.96% -17.49%

    D4598565

    7/20/2009

  • Proprietary August 2009 94

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Commonality

    J9808321

    7/20/2009

  • Proprietary August 2009 95

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Commonality Design Philosophy CRJ900 General Requirements

    Maximum commonality with the CRJ200 and 700: Training and support Systems Spares Ground support equipment Maintenance program Maintenance equipment

    Minimize cash operating costs with family of aircraftC9533669

    7/23/2009

  • Proprietary August 2009 96

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Flight Crew Commonality CRJ Series

    All CRJ aircraft are certified with same type rating

    Commonality with CRJ flight deck Commonality with controls and indications Commonality with handling and maneuvering

    Common pilot pool between CRJ200, 700, 900 and 1000 Single pilot pool with mixed fleet flying Reduced flight crew training Significant reduction in training costs

    Y5192655

    7/27/2009

  • Proprietary August 2009 97

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Training Commonality CRJ Series

    Initial differences training from CRJ200 to CRJ900 3 days differences training

    4 computer-based training (CBT) sessions (4 hrs. each) 2 fixed training device (FTD) sessions (4 hrs. each)

    Recurrent training As required by local authorities (generally 2 per year)

    Alternating check rides between CRJ200 and CRJ700 are NOT required

    P2200674

    7/23/2009

  • Proprietary August 2009 98

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Maintenance Commonality CRJ Series

    Aircraft maintenance philosophy is designed for maximum commonality:

    Reduced initial and attrition training Reduced non-direct personnel required Reduced requirement for special tools and equipment Reduced indirect overhead

    M3295025

    7/20/2009

  • Proprietary August 2009 99

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Spares Commonality CRJ Series

    CRJ700/900 designed to have highest degree of spares commonality

    Reducing spares inventory

    Certain aircraft systems require increase in loads/capacity Parts commonality kept where feasible

    Operator feedback incorporated for improved reliability and maintainability

    Trade-offs required with parts commonality

    I4516894

    7/23/2009

  • Proprietary August 2009 100

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Total Commonality Savings Sample Fleet* 10 + 10 Aircraft

    Commonality SavingsFlight Crew Non Recurring Recurring Present Value*

    Initial Training $2.23 M $2.23 MRecurrent Training $0.16 M $1.34 M

    Attrition Training $1.13 M $9.70 MCrew Pooling / Scheduling $0.86 M $7.37 M

    $20.63 MMaintenance

    Initial Training $0.88 M $0.88 MAttrition/Recurrent Training $0.05 M $0.44 M

    Direct Labor Wage Costs $0.07 M $0.60 M$1.92 M

    SparesInitial Spares Investment $0.79 M $0.79 MSpares Overhead (8%) $0.06 M $0.54 M

    $1.33 M

    Operations Support $0.45 M $0.58 M $5.41 M $5.41 M

    Total Commonality Savings $29.3 M

    G2535022

    7/23/2009

    Sample fleet 10 CRJ200 + 10 CRJ900 vs 10 CRJ200 + 10 90-seat aircraftDiscount rate 8.0%/year, 15 year term

  • Proprietary August 2009 101

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Large Commonality Savings with CRJ Family

    Sample fleet 10 CRJ200 + 10 CRJ900 vs 10 CRJ200 + 10 90-seat aircraftDiscount rate 8.0%/year, 15 year term

    7%5%

    18%

    70%

    MaintenanceSpares

    Other

    Flight Crew

    Total savings = $2.9 m per CRJ900

    Flight crew $20.63 MMaintenance $1.92 MSpares $1.33 MOperations Support $5.41 MTotal: $29.3 M

    H6435993

    7/23/2009

  • Proprietary August 2009 102

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Commonality Assumptions

    Aircraft Fleet SizeStatus prior to acquistion of larger typeFleet mix used in studyAnnual aircraft utilizationAnnual number of flights per aircraft

    Flight Crew Capt. FO Capt. FO Capt. FOAverage annual salary $52,893 $26,052 $73,897 $36,397 $73,897 $36,397Crew benefits (% of salary)Pilot initial training costNumber of pilots trained via purchase agreementPilot block hours per monthAnnual captain flow through rate to major airlinesAnnual pilot attrition rateRecurrent training cost per pilotRecurrent training interval (months)Pilot upgrade training cost (FO => Captain)

    MaintenanceAverage annual salaryAirline maintenance personnel benefitsNominal number of mechanics per aircraftAnnual attrition rateInitial training cost per mechanicNumber of mechanics trained via purchase agreement

    SparesOverhead cost (annual rate on initial spares provisioning cost)

    Training OperationsNumber of management pilotsNumber of flight instructorsNumber of ground school instructorsNumber of maintenance instructors

    30%

    2 0 1

    $15,850

    3

    Incl'd in CRJ count4

    03

    $5,2006

    $12,200

    $45,000

    4800%15%

    4.05%

    2

    2

    8% 8%

    30%same as CRJ

    5%$7,400

    2

    4.15%

    $15,850

    15%$5,200

    6n/a

    $45,000

    $29,350

    $45,000

    0

    2

    8%

    13

    $29,350 $6,800 $29,350

    6

    15%$5,200

    4480

    10%

    30%

    8010%

    2200

    30% 30% 30%

    2200 2200

    103000 3000 300010 10

    JET9010 nil nil

    CRJ200 CRJ900

    G5891081

    7/23/2009

  • Proprietary August 2009 103

    This [These] document[s] contain[s] financial, commercial, scientific, technical or other proprietary information. This document is for informational purposes only; is not part of any proposal; creates no contractual commitment and is subject to change.

    Information contained in this document is proprietary to Bombardier Inc., Bombardier Aerospace, Commercial Aircraft (Bombardier). This document must not be reproduced or shared with, or distributed to, any third party in whole or in part without Bombardiers prior written consent.

    This document is submitted for informational purposes only; is not part of any proposal; and creates no contractual commitment. Bombardier provides the information contained in this document on an as is, where is basis and makes no representation or warranty of any kind regarding the applicability or reliability of any of such information with respect to any use whatsoever to be made of it by the recipient.

    Any information of a technical nature contained in this document may contain inaccuracies and is subject to change and should never be relied upon for operational use.

    Report Number: CRJ900 NextGen Product OverviewDate: August 1st, 2009Prepared By: PPD&CRContact: [email protected]

    Program Planning Development & Customers RequirementsBOMBARDIER COMMERCIAL AIRCRAFT

    Many Solutions, One Source.

    K1947865

    7/20/2009

    Program Planning, Development & Customer RequirementsBombardier Commercial AircraftForward-looking statementsSlide Number 3Introducing the CRJ Extended FamilyThe CRJ FamilyBenefits of a Family of AircraftEvolution of the CRJ FamilyEvolution of the CRJ FamilyChange Summary - Family-Driven ConceptCRJ700 - CRJ900Parts CommonalityCRJ900 - CRJ700Introduction of the CRJ NextGenBuild On SuccessThe Best RJ Family in the World Just Gets Bigger and Better CRJ NextGen Benefits:Fuel Savings - up to 4% ReductionImproved EconomicsMaintenance - up to 9% Lower Airframe Maintenance CostsSlide Number 15Slide Number 16Technological Innovation Available on the CRJ NextGen FamilyComposite TechnologyComposite TechnologyResin Transfer Molding (RTM)General CharacteristicsCRJ900 General CharacteristicsGeneral ArrangementCRJ900Aircraft Design WeightsCRJ900Turnaround ServicingCRJ900Competitive Turnaround TimeCRJ900Jetway / Airbridge CompatibilityCRJ900Door LocationsCRJ900Cargo Compartment CharacteristicsCRJ900Main Baggage CompartmentCRJ900Secondary Under-Floor Baggage CompartmentCRJ900InteriorsPassenger Experience - New Interior Bigger. Brighter. Better.Passenger Experience - Latest Interior Look and FeelPassenger ExperienceProven Passenger Appeal Now Even BetterPassenger ExperienceFlexible Passenger Cabin Meets Airlines RequirementsPassenger Experience - Larger Cabin Windows24% More Viewing AreaPassenger Experience - LED Cabin LightingOverall Improved AestheticsPassenger Experience - Business ClassEnhanced Passenger Experience Passenger ExperienceOptional In-Flight Entertainment AvailablePassenger ExperienceCabin In-Seat Power System AvailableInterior ConfigurationsCRJ900Interior Layouts - Single ClassCRJ900Interior Layouts - Dual ClassCRJ900Standard 88 Seat ConfigurationCRJ900Optional 86 Seat ConfigurationCRJ900Optional 86 Seat Mixed Class ConfigurationCRJ900Optional 90 Seat ConfigurationCRJ900Optional 75 Dual Class ConfigurationCRJ900Optional 77 Dual Class ConfigurationCRJ900Passenger ExperienceCabin Cross SectionPassenger Experience - Larger Overhead Bins up to 27% more roller bags storedCRJ900 - Interiors G1 Galley OptionsCRJ900G2 Galley OptionsCRJ900G3 Galley OptionsCRJ900Additional Galley OptionsCRJ900Customized Galley FeaturesCRJ900Slide Number 58MaintenanceCRJ900Advanced Technology UtilizationCRJ900Flight DeckCRJ900Avionics and Cockpit SystemsCRJ900APU AssemblyCRJ900APU SystemCRJ900Cabin Temperature Control SystemCRJ900Flight Controls - Flaps and SlatsCRJ900Electrical PowerCRJ900Landing GearCRJ900Hydraulic SystemCRJ900Fuel System SchematicCRJ900PropulsionGeneral Electric CF34-8C5 EnginePowerplant Commonality CRJ700/900/1000Common Right and Left (CRL) Powerplant DesignCRJ900Clamshell Design Facilitates Improved CF34-8C5 Core and LRU AccessOn-Wing Maintenance for Reduced CostsCRJ900Environmental CompatibilityCRJ900 - Certified Emission LevelsEnvironmental CompatibilityCRJ900 LR - Chapter IV Certified Noise LevelsSlide Number 79Performance EFB, CAFM and CIFPNominal PerformanceCRJ900Nominal PerformanceNominal PerformancePayload Range CRJ900 NextGenBlock Time CRJ900 NextGenBlock Fuel CRJ900 NextGenRange from MinneapolisCRJ900 NextGenRange from FrankfurtCRJ900 NextGenRange from DubaiCRJ900 NextGenRange from Hong KongCRJ900 NextGenEconomicsEconomics500 nm, Jan 09US$, North American EnvironmentEconomics500 nm, Jan 09 US$, European EnvironmentCommonalityCommonality Design PhilosophyCRJ900 General RequirementsFlight Crew CommonalityCRJ SeriesTraining CommonalityCRJ SeriesMaintenance CommonalityCRJ SeriesSpares CommonalityCRJ SeriesTotal Commonality SavingsSample Fleet* 10 + 10 AircraftLarge Commonality Savings with CRJ FamilyCommonality AssumptionsSlide Number 103