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28 Urban OperatiOns
31 blOck fUel advantage
35 ecOnOmics
39 envirOnmental fOOtprint
43 nOise redUctiOn
47 cOmfOrt
50 reliability / maintainability
08 technical specificatiOns
12 advanced technOlOgy
14 engine
17 advanced flight deck
18 dimensiOns
20 crOss sectiOns / cOnfigUratiOns
26 range capability
the wOrld has changed, and the CSerieS aircraft are the Only 100% newly designed aircraft fOr the 100- tO 149-seat market segment tO meet tOday’s OperatiOnal realities.
the CSeries aircraft family combines latest generation aerodynamics, optimal system integration and advanced structural materials, along with a game-changing engine, to deliver 20% fuel burn advantage and a 15% cash operating cost advantage over in-production aircraft in its class. the greenest single-aisle aircraft in their category, the CSeries aircraft also provide a 20% CO2 emissions advantage and 50% fewer NOx emissions. they can handle short, remote or hot and high runways while providing passengers with widebody cabin comfort and an exceptional flying experience. this all adds up to more profits, making the CSeries aircraft as profitable as they are responsible.
Changeis in
the air
CS
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05
the smaller Of the twO mOdels in the CSerieS aircraft family, the CS100 aircraft are designed fOr lOwer density, lOnger range, single-aisle markets. with their best-in-class shOrt field perfOrmance, the CS100 aircraft are the ideal sOlUtiOn fOr city centre airpOrt OperatiOns.
the Bombardier CS100 aircraft combine unmatched field performance along with transcontinental range, creating new business opportunities through currently unexploited routes and business models. beyond performance, the CS100 aircraft offer a variety of customized configurations, including dual-class and high density options. together, the CS100 and the CS300 aircraft offer 95% parts commonality, as well as the same type certification, range options, fuselage cross section, and engine–which all add up to tremendous flexibility.
Operators can look forward to reduced costs, increased margins and excellent returns. the CSeries aircraft’s advanced systems integration, lighter weight structure and advanced aerodynamics, coupled with the pratt & whitney purepower® pw1500g * engine, deliver a 20% fuel burn advantage and a 15% cash operating cost advantage over in-production aircraft in its class. in addition, the CSeries aircraft family offers airlines more than 25% direct maintenance cost advantage due to its optimized maintenance program. beyond maintenance savings, significant investment in upfront testing will ensure 99% reliability at entry-into-service, and 99.5% reliability two years after.
Introducing the
CS100
CS
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07
CS
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07
the larger Of the twO mOdels in the CSerieS aircraft family, the CS300 aircraft are designed fOr higher density, lOnger-range, single-aisle markets, Offering airlines the OptiOn tO cOnfigUre the aircraft tO accOmmOdate Up tO 160 passengers and drive seat-mile cOsts even lOwer.
the Bombardier CS300 aircraft provide a superior economic advantage compared to any aircraft in their class; they can even match the cost per seat of successful larger narrowbodies, unlocking a new level of profit potential with minimal risk. like the CS100 aircraft, the CS300 model offers a variety of customized configurations including dual-class and high density options.
regardless of the aircraft model, every CSeries aircraft interior configuration is designed to deliver widebody feel in a single-aisle aircraft and customer satisfaction that operators can rely on. the unprecedented operational flexibility of the CSeries aircraft allows operators to open new routes and increase network frequency being demanded by passengers, all at significantly lower operating costs. profitable, comfortable and responsible. providing a 20% cO2 emissions advantage, 50% less nOx emissions and dramatically reduced noise levels, the CSeries family of aircraft is the greenest single-aisle aircraft in its class.
Introducing the
CS300
CS
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technical specificatio
ns
perfOrmance
Rangemax mtOw, normal cruise CS100: 110 pax. @ 225 lb. / 102 kg CS300: 135 pax. @ 225 lb. / 102 kg
2,950 NM 3,395 SM 5,463 km
Takeoff Field Lengthisa, sl, base mtOw, max. thrust
CS100 4,000 ft. CS300 5,000 ft. 1,219 m 1,524 m
Landing Field Lengthisa, sl, base mlw
CS100 4,400 ft. CS300 4,750 ft. 1,341 m 1,448 m
weights
CS100maximum takeoff weight Base 116,000 lb. / 52,617 kgMax 129,000 lb. / 58,513 kg
maximum landing weight Base 110,000 lb. / 49,895 kgMax 112,000 lb. / 50,802 kg
maximum payload Base 30,150 lb. / 13,676 kgMax 32,150 lb. / 14,583 kg
CS300maximum takeoff weight Base 129,000 lb. / 58,513 kgMax 144,000 lb. / 65,317 kg
maximum landing weight Base 121,500 lb. / 55,111 kgMax 127,000 lb. / 57,606 kg
maximum payload Base 35,900 lb. / 16,284 kgMax 40,900 lb. / 18,552 kg
Technical Specifications
general
Passengers
CS100Capacity 110 (up to 125)
CS300Capacity 135 (up to 160)
Cargo
CS100Volume 838 ft.3 / 23.7 m3
Weight 8,000 lb. / 3,629 kg
CS300Volume 1,116 ft.3 / 31.6 m3
Weight 10,700 lb. / 4,853 kg
CS
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technical specificatio
ns
speed (fl370, isa)
Maximum Cruise Speed 0.82 Mach 470 kts 541 mph 871 km/h
Normal Cruise Speed 0.78 Mach 447 kts 515 mph 829 km/h
advanced flight deck featUres
+ Advanced Fly-by-Wire with Full Envelope Protection & Speed Stabilization
+ Five large 15.1” LCD Displays + Side Stick Controls + Cat IIIa Autoland + Graphical Flight Management System
+ Advanced Multi-Scan Weather Radar
+ SATCOM Voice and Data Link + Full Format Printer + Controller Pilot Data Link Communication (CPDLC) Ready
+ CAT IIIb Autoland* + Single or Dual Head-Up Display System (HUD)*
+ Class 2 Electronic Flight Bag* + Integrated Flight Information System*
* Optional feature
engine
2 Pratt & Whitney PurePower ®PW1500G Engines
PW1519G Engines*Maximum Takeoff Thrust (MTOT) 18,900 lbf. / 84.1 kNFlat Rating ISA + 15.0°C
PW1521G EnginesMaximum Takeoff Thrust (MTOT) 21,000 lbf. / 93.4 kNFlat Rating ISA + 15.0°C
PW1524G EnginesMaximum Takeoff Thrust (MTOT) 23,300 lbf. / 103.6 kNFlat Rating ISA + 15.0°C
* PW1519G Engines applies only to the CS100 aircraft
Technical Specifications
CS
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13
advanced
technolo
gy
12,000lb. lighter *up
to
* Vs. in-production aircraft in 135-seat category and re-engined options.
Advanced Technology
advanced flight deck and fly-by-wire with side sticks
integrated aviOnics & Optimized systems
advanced alUminUm lithiUm fUselage
best-in-class cabin cOmfOrt and flexibility
advanced cOmpOsite wing, empennage and rear fUselage
electric brakes
sUperiOr field perfOrmance & range flexibility
pratt & whitney pUrepOwer® pw1500g engine
advanced On-bOard maintenance system
CS
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engine
Pratt & Whitney PurePower ® PW1500G EngineA Step Change in Technology Optimized for the CSeries Aircraft Family
high speed, advanced lOw pressUre cOmpressOr and tUrbine
advanced tUrbine aerOdynamics
talOn™ x cOmbUstOr
integrally bladed rOtOr (ibr)
highest by-pass ratiO Of any certified tUrbOfan engine in the wOrld
fan drive gear system (fdgs)
CS
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advanced
flight d
eck
Advanced Flight Deck
A integrated flight management system
B graphical flight planning
C sensed electrOnic checklist
D advanced mUlti-scan weather radar
E advanced fly-by-wire with side stick cOntrOls
F aUtO thrOttle (mOving thrUst levers)
G cat iiia aUtOland (cat iiib OptiOnal)
H cOntrOller pilOt data link cOmmUnicatiOn (cpdlc) ready
I data link with fUll fOrmat printer
J Optimized hUman-machine interface
K head Up displays (OptiOnal)
L class 2 electrOnic flight bags (OptiOnal)
M grOwth capability
A C
B
F
D
JH
E
GL
I
MK
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dim
ensions
wingspan
115 f t .1 i n .
35.1 m
fUselage maximUm diameter
12 f t .2 i n .
3.7 m
height
37 f t .8 i n .
11.5 m
height
fUselage maximUm diameter
wingspanCS100 length
114 ft .9 in .
35.0 m
CS300 length
127 f t .0 i n .
38.7 m
wing area (net)
1,209 ft .2
112.3 m2
Dimensions
wing area (net)
wing area (net)
CS100 length
CS300 length
CS
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21
cross sectio
ns and co
nfiguratio
ns
Configurations CS100
dUal class
standard single class
high density single class
108 s e a t s
110 s e a t s
125 s e a t s
36 | 32 i n . s e a t p i t c h
32 i n . s e a t p i t c h
30 i n . s e a t p i t c h
bUsiness class ecOnOmy class
129.0 i n .| 3.28 m
83.0
in
.| 2.11
m
A Wide 20.0 in. / 0.51 m Business class seatB Wide 18.5 in. / 0.47 m seat C Oversized 19.0 in. / 0.48 m middle seat
ba aa a bc b b
59.0
in
.| 1.5
0 m 20.0 i n .| 0.51 m22.0 i n .| 0.56 m
122.0 i n .| 3.10 m
Cross Sections
Overhead bins (pivOt bins)
CS100Greater than 90 standard roller bags (22 x 14 x 9 in.)
CS300Greater than 110 standard roller bags (22 x 14 x 9 in.)
bin vOlUme per passenger
CS1002.4 ft.3 (0.07 m3) 110 pax. configuration
CS3002.5 ft.3 (0.07 m3) 135 pax. configuration
cabin windOws
Large 11 x 16 in. (28 x 41 cm) At least one window available at each seat row
CS
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cross sectio
ns and co
nfiguratio
ns
dUal class 130 s e a t s 36 | 32 i n . s e a t p i t c h
standard single class 135 s e a t s 32 i n . s e a t p i t c h
high density single class 150 s e a t s 30 i n . s e a t p i t c h
extra capacity 160 s e a t s 28 i n . s e a t p i t c h
Configurations CS300
extra capacity
the second overwing exit option makes it possible to increase the maximum seat capacity of the CS300 aircraft to 160 passengers, offering customers even more flexibility. this option is specifically designed for airlines wanting to increase the productivity of their aircraft beyond 145 passengers and driving seat-mile costs even lower.
Maximum capacity
up to
160passengers
secOnd Overwing exit OptiOn
(retrOfittable)
Up tO 15 extra passengers—making the best cOst-per-seat even better
CS
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cross sectio
ns and co
nfiguratio
ns
persOns with redUced mObility (prm) lavatOry
Configurations
the prm-designed lavatories of the CSeries aircraft set new standards in space utilization and occupant’s privacy without the need for supplementary partitions or curtains. it can be used independently of other lavatories in the cabin so able-bodied passengers will not need to wait for cabin crew to reconfigure doors or partitions.
+ Large entryway for maneuverability + Full ingress of aisle chair + Optimized PRM ergonomics
Beijing
Singapore
Chongqing
Brunei
Manila Bangkok
Calcutta Mumbai
Delhi Shanghai
Kunming
Ho Chi Minh
Xian Chengdu
Tokyo
Ulaanbaatar
Lhasa
Urumqi
Darwin
Seoul
HONG KONG
Tripoli
Mumbai
Rome
Moscow Berlin
Cairo
Antananarivo
Calcutta
Nairobi
Delhi
Addis Abeba
Athens
Tehran
Istanbul
Vienna
StockholmRiga
Almaty
Karaganda
Jeddah DUBAI FRANKFURT
Rome
Paris
Athens
Oslo
Lisbon
Moscow
Stockholm
London
Kano
Dakar
Cairo Tripoli
Reykjavik
Riyadh Casablanca
Las Palmas
Jeddah
Tehran
Ashgabat
Dubai
Vancouver
Los Angeles
Mexico City
Denver
Dallas
St.Louis
Caracas
Bermuda Islands
St.Johns
Toronto
Houston
Bogota
Quito
Georgetown
NEW YORK
CS
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27
range cap
ability
assUmptiOns
+ + Type Spec Aircraft Configuration (CS100: 110 Pax, CS300: 135 Pax)+ + Passengers with Bags @ 225 lb. (102 kg) each+ + 85% Annual Wind / Enroute Temperature ISA+ + Typical Mission Rules with Reserves (100 NM diversion,
45 min. hold @ Cruise Altitude, 5% Flight Fuel Contingency)
asia pacific // hOng kOng // hkg middle east // dUbai // dxb
Range Capability
americas // new yOrk // Jfk eUrOpe // frankfUrt // fra
range
2,950 n m
3,395 s m
5,463 k m
Athènes + Rome +
Varsovie +
Tripoli +
+
+ Kiev
+ Oulu
+ + Reykjavik
Ibiza +Faro +
Ankara ++ Genève
+
+ Las Palmas
+ Açores
+
Stockholm +
LONDRES CITY
Moscou
St-Petersbourg
Benghazi
Djanet
CS
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29
urban o
peratio
ns
cOnnect the dOts
+ The CS100 aircraft offers best-in-class airfield performance and increased range
+ With a takeoff field length as low as 4,000 ft. (1,219 m), the CS100 aircraft is the ideal solution for city centre airport operations
+ The CS100 aircraft expands the range of business opportunities
QUiet fOr a change
+ The CSeries aircraft family: designed from the outset with the community in mind
+ The noise signature of the CSeries aircraft is comparable to other urban sounds
Take-Off Run Available (TORA): 3,934 ft. (1,199 m) Take-Off Distance Available (TODA) / Accelerate-Stop Distance Available (ASDA): 4,327 ft. (1,319 m)
range 1,700 nm
1,956 sm
3,148 km
Meet the community-
friendly aircraft
Urban Operations
the CSeries aircraft is the ideal aircraft for urban operations, with an unmatched environmental scorecard, including the lowest noise levels of any commercial aircraft in-production.
get to your destination faster with the airport at your doorstep. avoid traffic and reduce local cO2 automobile emissions that contribute to city smog.
CS
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33
blo
ck fuel advantag
e
Optimal aircraft integratiOn + game-changing engine
* Compared to competitors in the same category
20%fuel burn
advantage
blOck fUel advantage per seat
Block Fuel Advantage
>20%
>50%
up to
12%
in-p
rO
dU
ct
iOn
a
irc
ra
ft
*
OU
t-O
f-
pr
Od
Uc
tiO
n
air
cr
af
t
*
re
-en
gin
ed
a
irc
ra
ft
cs
er
ies
CS
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37
econo
mics
>15%
cOc per seat
>30%
Cash Operating
Costs (COC) Comparison
Per Seat
* Compared to competitors in the same category
in-p
rO
dU
ct
iOn
a
irc
ra
ft
*
OU
t-O
f-
pr
Od
Uc
tiO
n
air
cr
af
t
*
re
-en
gin
ed
a
irc
ra
ft
cs
er
ies
up to
12%15%COC
advantage
CS
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41
environm
ental foo
tprint
50% less nOx emissiOns
>50% margin
caep6 nOx requirement (January 2008)
NOx Emissions
in-p
rO
dU
ct
iOn
a
irc
ra
ft
*
OU
t-O
f-
pr
Od
Uc
tiO
n
air
cr
af
t
*
cs
er
ies
* Compared to competitors in the same category
20% cO2 emissiOns advantage per seat
Greenhouse Gas
Emissions>20%
>50%
up to
12%
in-p
rO
dU
ct
iOn
a
irc
ra
ft
*
OU
t-O
f-
pr
Od
Uc
tiO
n
air
cr
af
t
*
re
-en
gin
ed
a
irc
ra
ft
cs
er
ies
CS
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45
noise red
uction
CSERIES
In-production aircraft
Noise Footprint 4x
smaller footprint
up toCommunity Noise
cUrrent(margin to stage 4)
fUtUre(margin to stage 5)
0
nOise margin tO cUrrent and fUtUre regUlatiOns
cs
300
cs
100
cO
mp
et
itO
r
av
er
ag
e *
cs
100
cs
300
cO
mp
et
itO
r
av
er
ag
e *
21epndbmargin
up to
15epndbmargin
QU
iete
r
20epndbmargin
up to
14epndbmargin
* Compared to competitors in the same category
CS
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49
com
fort
+ Greatest seat width, shoulder and foot space per passenger in a single-aisle aircraft
+ Wider middle seat, up to 1 ½ in. larger than the competition
+ More personal space without compromising aisle width
+ Extra large windows measuring 1 1 x 16 in. (28 x 41 cm)
+ Positioned high on the sidewall to provide an optimal viewing angle and natural light
+ A window at every seat row
best view in the sky
Unrivaled passenger living space
Comfort
+ Up to 18 more carry-on bags than its competitors
+ Capacity to stow oversized carry-on bags measuring 24 x 17 x 1 1 in. (61 x 43 x 28 cm), wheels first
+ Lower bin access bringing storage and security checks within easy reach
largest stOwage in its class
the CSeries aircraft cabin was intentionally designed from inside out to provide space where it matters most to passengers and crew members. it is a 100% new aircraft that delivers a superior and unrivaled passenger experience, with increased comfort, service efficiency and safety. the CSeries aircraft is an innovation airlines can rely on.
A higher levelof comfort
CS
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51
reliability and
maintainab
ility
Aircraft Health Management SystemDiagnostic and Prognostic Solutions Through Aircraft Integration
enhanced diagnOsticAll Systems Central ReportingParameter snapshot on faultFlight Deck Effect correlationAutomatic and / or Manual in-flight reporting
bi-directiOnal cOmmUnicatiOnACARS / SatcomGround Wireless
web-based User interfaceFleet TrackingEnhanced troubleshootingEvent MonitoringPrognostic / Usage Monitoring
data stOrage and management5,000 parameters for 100 FlightsCustomizable reports
99%reliability at entry-
into-service99.5% reliability two years after entry-into-service
CS
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53
reliability and
maintainab
ility
Bombardier Customer ServicesGlobally. Locally.We put
peOple, passiOn and perfOrmancewww.iflybombardier.com
Maintenance Intervals
service check
100 f l i g h t h o u r s
“a” check
850 f l i g h t h o u r s
“c” check
8,500 f l i g h t h o u r s
strUctUral inspectiOn
12 y e a r s
Bombardier Commercial AircraftTelephone: +1 450-476-5795www.aero.bombardier.comwww.cseries.com
Bombardier, CSeries, CS100, CS300 and The Evolution of Mobility are trademarks of Bombardier Inc. or its subsidiaries.
* PurePower ® PW1500G, PW1519G, PW1521G and PW1524G Engines are trademarks of United Technologies Corp. – Pratt & Whitney or its subsidiaries.
disclaimer The information in this document is PROPRIETARY to Bombardier Inc. or its subsidiaries. This document does not constitute an offer, commitment, representation, guarantee or warranty of any kind and the configuration and performance of any aircraft shall be determined in a final purchase agreement. The CSeries aircraft is in development phase and, as such is subject to changes in family strategy, branding, capacity, performance, design and / or systems. The actual aircraft and configuration may differ from images shown. This document must not be reproduced or distributed in whole or in part to or by a third party. Bombardier Aerospace shall be notified in writing of all requests for permission to disclose.
All rights reserved © 2014 Bombardier Inc.
Printed in Canada, May 2014