crj900 product overview
DESCRIPTION
CRJ900TRANSCRIPT
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Proprietary August 2009 1
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Program Planning, Development & Customer Requirements Bombardier Commercial Aircraft
CRJ900 NextGen Product OverviewAugust 2009
W1522308
7/23/2009
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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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7/20/2009
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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
J7115548
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Change Summary - Family-Driven Concept CRJ700 - CRJ900
New Winglets for CRJ900
T2557296
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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
7/23/2009
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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
EIS May 2007
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EVOLUTION
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EIS July 1992
Economics
Comfort
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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
$30
$40
$50
$60
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
+35%Up to
+30%
Competitor CompetitorCompetitorOlder
CompetitorsOlder
CompetitorsOlder
Competitors
70-80SEATS
80-90SEATS
90-110SEATS
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Environmentally Friendly Less Exterior Noise
260
270
280
1 2 3 4 5 6 7 8 9 10 11
70-80SEATS
80-90SEATS
90-110SEATS
Competitor CompetitorCompetitorOlder
CompetitorsOlder
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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
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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)
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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*
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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
Minutes
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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
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Jetway / Airbridge Compatibility CRJ900
The CRJ Series design features ensure compatibility with current jetways and airbridges
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Door Locations CRJ900
* Sill height 68 (1.73 m)I8100862
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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)
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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
Q4211676
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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
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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
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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
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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
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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
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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
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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
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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
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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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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
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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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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
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Proprietary August 2009 48
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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
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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
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Passenger Experience Cabin Cross Section
P3717541
7/20/2009
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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
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CRJ900 - Interiors
Forward flight attendant seat Aft flight attendant seatV2448660
7/23/2009
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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
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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
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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
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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
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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
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Proprietary August 2009 58
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Systems
S1723507
7/15/2009
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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
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Proprietary August 2009 60
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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Proprietary August 2009 72
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General Electric CF34-8C5 Engine
One engine for the whole NextGen family
Relative to the GE CF34-3B1 engine
O7369361
7/20/2009
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Proprietary August 2009 73
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Powerplant Commonality CRJ700/900/1000
CRJ700 provides engine normal take-off power optionsto match operational requirements
P8235042
7/20/2009
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Proprietary August 2009 74
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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
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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
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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
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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
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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
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L
e
v
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l
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P
N
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B
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Margin (ICAO Annex 16 Chapter III )Noise Level (Chapter IV)
6.3
265.4
255
260
265
270
275
280
Cumulative
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Margin (ICAO Ch IV)Acc. Noise Level
Environmental Compatibility CRJ900 LR - Chapter IV Certified Noise Levels
Y6879575
7/23/2009
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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
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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
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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
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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.
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
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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
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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
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15000
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0 500 1000 1500 2000 2500 3000Range (nm)
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CRJ900 CRJ900 ER CRJ900 LR
88 pax
A2795587
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.
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
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H4867197
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.
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
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G4322285
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.
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
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Proprietary August 2009 88
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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
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Proprietary August 2009 89
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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
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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.
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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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Proprietary August 2009 102
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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
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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