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100% new aircrat

Change is in the air

Introducing the th e CS100

The world has changed,  a n d T h e c s e r i e s  a i r c r a  T i s T h e o n ly 100% newly designed  a i r c r a  T T o m e e T T o d ay ’ s operaTional realiTies. T cs * t  latest generation aerodynamics, system integration and advanced structural materials, materials,  t    , t     20% fuel burn benefit  -t t  t    15% cash operating costs advantage.. T t - advantage t  t t, t cs t t 20% fewer CO2  50% fewer NOx emissions emissions,,   4 times quieter t t tt. it   t, t  t       t widebody cabin comfort   t  . T    t  t,  t cs t  t  t  .

Introducing the CS300

08

Technical speciicaTions

22

range capabiliTy

46

Technical speciicaTions

60

range capabiliTy

12

advanced Technology

25

block uel  a d v an Ta g e

50

advanced Technology

63

block uel  a d va n Ta g e

14

engine

29

economics

52

engine

67

economics

16

advanced lighT deck 

33

environmenTal ooTprinT

54

advanced lighT deck 

71

environmenTal ooTprinT

18

dimensions

37

noise ooTprinT

56

dimensions

75

noise ooTprinT

20

cross secTions /  coniguraTions

40

reliabiliTy /  mainTainabiliTy

58

cross secTions /  coniguraTions

78

reliabiliTy /  mainTainabiliTy

Change is in the air

Introducing the th e CS100

The world has changed,  a n d T h e c s e r i e s  a i r c r a  T i s T h e o n ly 100% newly designed  a i r c r a  T T o m e e T T o d ay ’ s operaTional realiTies. T cs * t  latest generation aerodynamics, system integration and advanced structural materials, materials,  t    , t     20% fuel burn benefit  -t t  t    15% cash operating costs advantage.. T t - advantage t  t t, t cs t t 20% fewer CO2  50% fewer NOx emissions emissions,,   4 times quieter t t tt. it   t, t  t       t widebody cabin comfort   t  . T    t  t,  t cs t  t  t  .

Introducing the CS300

08

Technical speciicaTions

22

range capabiliTy

46

Technical speciicaTions

60

range capabiliTy

12

advanced Technology

25

block uel  a d v an Ta g e

50

advanced Technology

63

block uel  a d va n Ta g e

14

engine

29

economics

52

engine

67

economics

16

advanced lighT deck 

33

environmenTal ooTprinT

54

advanced lighT deck 

71

environmenTal ooTprinT

18

dimensions

37

noise ooTprinT

56

dimensions

75

noise ooTprinT

20

cross secTions /  coniguraTions

40

reliabiliTy /  mainTainabiliTy

58

cross secTions /  coniguraTions

78

reliabiliTy /  mainTainabiliTy

Introducing the th e CS100

Introducing the CS300

08

Technical speciicaTions

22

range capabiliTy

46

Technical speciicaTions

60

range capabiliTy

12

advanced Technology

25

block uel  a d v an Ta g e

50

advanced Technology

63

block uel  a d va n Ta g e

14

engine

29

economics

52

engine

67

economics

16

advanced lighT deck 

33

environmenTal ooTprinT

54

advanced lighT deck 

71

environmenTal ooTprinT

18

dimensions

37

noise ooTprinT

56

dimensions

75

noise ooTprinT

20

cross secTions /  coniguraTions

40

reliabiliTy /  mainTainabiliTy

58

cross secTions /  coniguraTions

78

reliabiliTy /  mainTainabiliTy

Introducing the th e CS100

 C    S    1     0     0   

The smaller o The Two models in The c s e r i e s  a m i l y, y, T h e 110-seaT cs100 aircraT is designed or lower densiTy, longer range, single-aisle markeTs. T b * cs100 * t  t    t ttt , t   tt t t t t   . b , t cs100 t   t  t t  -   t t. Tt,, t cs100  t cs300 * Tt t  95% t t t,,    t  t tt,  t,   t,  —    t t t.

ot    t  t,    t t. T cs t’  t tt, t t tt   ,  t t ptt & wt pp ® pw1500g** ,     20%   t   t t  t    15%  t t t. i t, t cs t    t 25% t t t   t t t t . b t , t tt  t tt   99% t t t t ,  99.5% t t t  t t t .

07

Introducing the th e CS100

 C    S    1     0     0   

The smaller o The Two models in The c s e r i e s  a m i l y, y, T h e 110-seaT cs100 aircraT is designed or lower densiTy, longer range, single-aisle markeTs. T b * cs100 * t  t    t ttt , t   tt t t t t   . b , t cs100 t   t  t t  -   t t. Tt,, t cs100  t cs300 * Tt t  95% t t t,,    t  t tt,  t,   t,  —    t t t.

ot    t  t,    t t. T cs t’  t tt, t t tt   ,  t t ptt & wt pp ® pw1500g** ,     20%   t   t t  t    15%  t t t. i t, t cs t    t 25% t t t   t t t t . b t , t tt  t tt   99% t t t t ,  99.5% t t t  t t t .

07

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Technical Specifcations general

Passengers

Capacity

perormance

weighTs

110 (up to 125)

Maximum Takeoff Weight

128,200 lb. 58,151 kg

Maximum Landing Weight

111,500 lb. 50,576 kg

Maximum Payload

Range

(MTOW, normal cruise, 110 pax @ 225 lb. /102 kg)

2,950 NM 3,395 SM 5,463 km

32,100 lb. 14,560 kg Takeoff Field Length

(ISA,SL, MTOW, max. thrust)

Cargo

4,950 ft. 1,509 m

 Volume Weight

819 ft. 3 / 23.2 m 3 8,190 lb. / 3,715 kg

Landing Field Length

(ISA, SL, MLW)

4,430 ft. 1,350 m

 t    e   c  h   n  i     c   a  l     s   p   e   c  i    f   i     c   a   t   i     o  n   s 

09

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Technical Specifcations general

perormance

weighTs

Passengers

Capacity

110 (up to 125)

Maximum Takeoff Weight

128,200 lb. 58,151 kg

Maximum Landing Weight

111,500 lb. 50,576 kg

Maximum Payload

Range

(MTOW, normal cruise, 110 pax @ 225 lb. /102 kg)

2,950 NM 3,395 SM 5,463 km

32,100 lb. 14,560 kg Takeoff Field Length

(ISA,SL, MTOW, max. thrust)

Cargo

4,950 ft. 1,509 m

 Volume Weight

Landing Field Length

819 ft. 3 / 23.2 m 3 8,190 lb. / 3,715 kg

(ISA, SL, MLW)

4,430 ft. 1,350 m

 t    e   c  h   n  i     c   a  l     s   p   e   c  i    f   i     c   a   t   i     o  n   s 

09

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Technical Specifcations engine

2 Pratt & Whitney PurePower PW1500G Engines

 a d v a n c e d  l i g h T deck eaTures

speed (l370, 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

PW1519G Engines

Maximum Takeoff Thrust (MTOT) 18,900 lbf. / 84.1 kN Flat Rating ISA + 15.0°C

PW1521G Engines

Maximum Takeoff Thrust (MTOT) 21,000 lbf. / 93.4 kN Flat Rating ISA + 15.0°C

PW1524G Engines

Maximum Takeoff Thrust (MTOT) 23,300 lbf. / 103.6 kN Flat Rating ISA + 15.0°C

+ Five large 15.1” LCD Displays + Advanced Fly-by-Wire with Full Envelope Protection & Speed Stabilization + Side Stick Controls + Integrated Flight Management System + Advanced Multi-Scan Weather Radar + Data Link with Full Format Printer + Automatic Dependent SurveillanceBroadcast (ADS-B) Out + Controller Pilot Data Link  Communication (CPDLC) Ready + CAT IIIa Autoland + CAT IIIb Autoland* + Single / Dual Head-Up Display (HUD)* + Electronic Flight Bag (EFB)* * Optional feature

 t    e   c  h   n  i     c   a  l     s   p   e   c  i    f   i     c   a   t   i     o  n   s 

11

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Technical Specifcations engine

2 Pratt & Whitney PurePower PW1500G Engines

 a d v a n c e d  l i g h T deck eaTures

speed (l370, 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

PW1519G Engines

Maximum Takeoff Thrust (MTOT) 18,900 lbf. / 84.1 kN Flat Rating ISA + 15.0°C

PW1521G Engines

Maximum Takeoff Thrust (MTOT) 21,000 lbf. / 93.4 kN Flat Rating ISA + 15.0°C

PW1524G Engines

Maximum Takeoff Thrust (MTOT) 23,300 lbf. / 103.6 kN Flat Rating ISA + 15.0°C

+ Five large 15.1” LCD Displays + Advanced Fly-by-Wire with Full Envelope Protection & Speed Stabilization + Side Stick Controls + Integrated Flight Management System + Advanced Multi-Scan Weather Radar + Data Link with Full Format Printer + Automatic Dependent SurveillanceBroadcast (ADS-B) Out + Controller Pilot Data Link  Communication (CPDLC) Ready + CAT IIIa Autoland + CAT IIIb Autoland* + Single / Dual Head-Up Display (HUD)* + Electronic Flight Bag (EFB)* * Optional feature

 t    e   c  h   n  i     c   a  l     s   p   e   c  i    f   i     c   a   t   i     o  n   s 

11

 Advanced Technology

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 a d v a n c e d  l i g h T d e c k a n d  ly - b y- w i r e w i T h s i d e s T i c k s inTegraTed avionics & opTimized sysTems  a d v a n c e d a l u m i n u m l i T h i u m  u s e l a g e besT-in-class cabin comorT and lexibiliTy

 a d v a n c e d c o m p o s i T e w i n g , e m p e n n a g e a n d r e a r  u s e l a g e elecTric brakes superior ield perormance & range lexibiliTy praTT & whiTney purepower® pw1500g engine  a d v a n c e d c o m p o s i T e n a c e l l e

 a   d   v   a  n   c   e   d    t    e   c  h   n   o  l     o   g   y 

13

 Advanced Technology

 C    S    1     0     0   

 a d v a n c e d  l i g h T d e c k a n d  ly - b y- w i r e w i T h s i d e s T i c k s inTegraTed avionics & opTimized sysTems  a d v a n c e d a l u m i n u m l i T h i u m  u s e l a g e besT-in-class cabin comorT and lexibiliTy

 a d v a n c e d c o m p o s i T e w i n g , e m p e n n a g e a n d r e a r  u s e l a g e elecTric brakes superior ield perormance & range lexibiliTy praTT & whiTney purepower® pw1500g engine  a d v a n c e d c o m p o s i T e n a c e l l e

 a   d   v   a  n   c   e   d    t    e   c  h   n   o  l     o   g   y 

13

Pratt & Whitney PurePower ® PW1500G Engine

 C    S    1     0     0   

 A S t e p C h a n g e i n Te c h n o l o g y

high speed, advanced low pressure compressor and Turbine  a d v a n c e d T u r b i n e a e r o d y n a m i c s T a l o n Tm x c o m b u s T o r inTegrally bladed roTor (ibr)  a d v a n c e d n a c e l l e T e c h n o l o g y

high bypass an an drive gear sysTem (dgs)  e  n   g  i    n   e 

15

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Pratt & Whitney PurePower ® PW1500G Engine  A S t e p C h a n g e i n Te c h n o l o g y

high speed, advanced low pressure compressor and Turbine  a d v a n c e d T u r b i n e a e r o d y n a m i c s T a l o n Tm x c o m b u s T o r inTegrally bladed roTor (ibr)  a d v a n c e d n a c e l l e T e c h n o l o g y

high bypass an an drive gear sysTem (dgs)  e  n   g  i    n   e 

15

 Advanced Flight Deck

 C    S    1     0     0   

A inTegraTed lighT managemenT sysTem B graphical lighT planning

k 

C sensed elecTronic checklisT

m

D  a d va n c e d m u lT i - s c a n w e a T h e r r a d a r E  a d v a n c e d  ly - b y- w i r e w i T h s i d e s T i c k c o n T r o l s

h

F  a u T o T h r o T T l e (       t     t       )

i

J

G caT iiia auToland (caT iiib opTional)

g

d

e

b

H conTroller piloT daTa link communicaTion (cpdlc) ready I daTa link wiTh ull ormaT prinTer

  a

l

c

J opTimized human-machine inTerace K  h e a d u p d i s p l a y s (   t      ) L class 2 elecTronic lighT bags (t) M growTh capabiliTy

 a   d   v   a  n   c   e   d   f   l    i     g  h    t    d    e   c  k  

17

 C    S    1     0     0   

 Advanced Flight Deck A inTegraTed lighT managemenT sysTem B graphical lighT planning

k 

C sensed elecTronic checklisT

m

D  a d va n c e d m u lT i - s c a n w e a T h e r r a d a r E  a d v a n c e d  ly - b y- w i r e w i T h s i d e s T i c k c o n T r o l s

h

F  a u T o T h r o T T l e (       t     t       )

i

J

G caT iiia auToland (caT iiib opTional)

g

d

b

e

H conTroller piloT daTa link communicaTion (cpdlc) ready

l

 a

 a   d   v   a  n   c   e   d   f   l    i     g  h    t    d    e   c  k  

I daTa link wiTh ull ormaT prinTer

 c

J opTimized human-machine inTerace K  h e a d u p d i s p l a y s (   t      ) L class 2 elecTronic lighT bags (t) M growTh capabiliTy

17

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Dimensions

wingspan

lengTh

wingspan

lengTh

114 6 34.9 t.

115 1 35.1

 .

t.



.



uselage maximum diameTer wing area  (neT)

wing area (neT)

1,209 112.3

uselage maximum diameTer t. 2

12 2 3.7

heighT

t.

2

.



heighT

37 9 11.5 t.

 .



 d   i    m  e  n   s  i     o  n   s 

19

 C    S    1     0     0   

Dimensions

wingspan

lengTh

wingspan

lengTh

114 6 34.9 t.

115 1 35.1

 .

t.



.



uselage maximum diameTer wing area  (neT)

wing area (neT)

1,209 112.3

uselage maximum diameTer t. 2

12 2 3.7

heighT

t.

2

.



heighT

37 9 11.5 t.

 .



 d   i    m  e  n   s  i     o  n   s 

19

 C    S    1     0     0   

Confgurations

Cross Sections bus in ess c la ss

dual class

economy class

100

t

36 32

. t t

   m

   0    5  .    1

    |  .         

   3    1  .    2

22.0  . | 0.56 

   m

20.0  . | 0.51 

    |  a

 a

a 

   0  .    9    5

121.9  . | 3.10  129.0  . | 3.28 

a

 .         

   0  .    4    8

b

c

b

b

b sTandard single class

110

t

32

. t t

30

. t t

 A - Wide 20.0 in. / 0.51 m Business class seat B - Wide 18.5 in. / 0.47 m seat C - Oversized 19.0 in. / 0.48 m middle seat

OVERHEAD BINS (pivot bins)

Greater than 90 standard roll aboards (22 in. x 14 in. x 9 in.)

BIN VOLUME PER PASSENGER

2.4 ft. 3 (0.07 m3) 110 pax. configuration

CABIN WINDOWS

Large 11 in. x 16 in. (27.9 cm x 40.6 cm)  At least on e window available a t each sea t row

high densiTy single class

125

t

 c  r    o   s   s   s   e   c   t   i     o  n   s   a  n   d    c   o  n  f   i     g   u  r    a   t   i     o  n   s 

21

 C    S    1     0     0   

Confgurations

Cross Sections bus in ess c la ss

100

dual class

economy class

t

36 32

. t t

   m

   0    5  .    1

    |  .         

   3    1  .    2

22.0  . | 0.56 

   m

20.0  . | 0.51 

    |  a

 a

a 

a

   0  .    9    5

121.9  . | 3.10 

 .         

   0  .    4    8

b

c

b

b

b

110

sTandard single class

t

32

. t t

30

. t t

 c  r    o   s   s   s   e   c   t   i     o  n   s   a  n   d    c   o  n  f   i     g   u  r    a   t   i     o  n   s 

 A - Wide 20.0 in. / 0.51 m Business class seat B - Wide 18.5 in. / 0.47 m seat C - Oversized 19.0 in. / 0.48 m middle seat

129.0  . | 3.28 

OVERHEAD BINS (pivot bins)

Greater than 90 standard roll aboards (22 in. x 14 in. x 9 in.)

BIN VOLUME PER PASSENGER

2.4 ft. 3 (0.07 m3) 110 pax. configuration

CABIN WINDOWS

Large 11 in. x 16 in. (27.9 cm x 40.6 cm)  At least on e window available a t each sea t row

125

high densiTy single class

t

21

 C    S    1     0     0   

Range Capability  a m e r i c a s / / n e w y o r k / / J  k  

europe // rankurT // ra 

 a s i a pa c i  i c / / h o n g k o n g / / h k g

middle easT // dubai // dxb

Stockholm Riga Berlin Ulaanbaatar

Toronto

London Paris

NEW YORK

St.Louis

Seoul

Stockholm Moscow

Lhasa Mumbai

FRANKFURT

Tokyo

Xian

Delhi Chengdu

Calcutta

Chongqing

 Almaty

Istanbul

Beijing

Oslo

St.Johns Denver Los Angeles

Karaganda

Rome

Reykjavik 

 Vancouver

Moscow

 Vienna

Urumqi

Shanghai

 Athens Tripoli

Tehran Cairo

Delhi

Kunming HONG KONG

 Ashgabat

DUBAI

Dallas Bermuda Islands

Houston

Lisbon

Las Palmas

Mumbai

 Athens Tripoli

Manila

Bangkok 

Rome

Casablanca Mexico City

Hochiminh

Dubai Cairo

 Addis Abeba Brunei

Riyadh Singapore

Jeddah Caracas Bogota Quito

Calcutta

Jeddah

Tehran

Nairobi

Dakar Darwin

Georgetown Kano

 Antananarivo

 a s s u m p T i o n s range

2,950

nm

3,395 sm 5,463 

++ Type Spec Aircraft Configuration ++ 110 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)

r    a  n   g   e   c   a   p   a   b   i    l    i     t    y 

23

 C    S    1     0     0   

Range Capability  a m e r i c a s / / n e w y o r k / / J  k  

europe // rankurT // ra 

 a s i a pa c i  i c / / h o n g k o n g / / h k g

middle easT // dubai // dxb

Stockholm Riga Berlin Ulaanbaatar

Toronto

London Paris

NEW YORK

St.Louis

Seoul

Stockholm Moscow

Lhasa Mumbai

FRANKFURT

Tokyo

Xian

Delhi Chengdu

Calcutta

Chongqing

 Almaty

Istanbul

Beijing

Oslo

St.Johns Denver Los Angeles

Karaganda

Rome

Reykjavik 

 Vancouver

Moscow

 Vienna

Urumqi

Shanghai

 Athens Tripoli

Tehran Cairo

Delhi

Kunming HONG KONG

 Ashgabat

DUBAI

Dallas Bermuda Islands

Houston

Lisbon

Las Palmas

Mumbai

 Athens Tripoli

Manila

Bangkok 

Rome

Casablanca Mexico City

Hochiminh

Dubai Cairo

 Addis Abeba Brunei

Riyadh Singapore

Jeddah Caracas Bogota Quito

Calcutta

Jeddah

Tehran

Nairobi

Dakar Darwin

Georgetown Kano

 Antananarivo

 a s s u m p T i o n s range

2,950

nm

3,395 sm 5,463 

++ Type Spec Aircraft Configuration ++ 110 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)

r    a  n   g   e   c   a   p   a   b   i    l    i     t    y 

23

Block uel advantage

25

Block uel advantage

25

 C    S    1     0     0   

Block Fuel  Advantage

block uel advanTage per seaT

50%

>

20%

>

20%

opTimal aircraT inTegraTion + game changing engine

uel burn advantage    0    0    1     s     c

   n   *     o   T    i    f    T   a     c   r    u    c    d   r     o   i    a    r    p      n    i

 b   l     o   c  k   f    u   e  l     a   d   v   a  n   t    a   g   e 

  -    n   *    f    o   T     o   i    f   -    T   a    T    c   r    u   u    c     o   d   r    i     o   a    r    p

* Compared to 110-seat class

27

 C    S    1     0     0   

Block Fuel  Advantage

block uel advanTage per seaT

50%

>

20%

>

20%

opTimal aircraT inTegraTion + game changing engine

uel burn advantage    0    0    1     s     c

   n   *     o   T    i    f    T   a     c   r    u    c    d   r     o   i    a    r    p      n    i

 b   l     o   c  k   f    u   e  l     a   d   v   a  n   t    a   g   e 

  -    n   *    f    o   T     o   i    f   -    T   a    T    c   r    u   u    c     o   d   r    i     o   a    r    p

* Compared to 110-seat class in-productionaircraft

Economics

27

29

Economics

29

 C    S    1     0     0   

15%

COC advantage

Cash Operating Costs Comparison Per Seat

coc per seaT

30%

>

15%

>

   0    0    1     s     c

   e   n   *     g    o   T    a   i    f    r   T   a    e    c   r    v   u    c    a   d   r    i     o    r   a    p      n    i

  -    n   *    f    o   T     o   i    f   -    T   a    T    c   r    u   u    c     o   d   r    i     o    r   a    p

* 110-seat class aircraft @ 500 NM,

 e   c   o  n   o  m i     c   s 

31

 C    S    1     0     0   

15%

COC advantage

Cash Operating Costs Comparison Per Seat

coc per seaT

30%

>

15%

>

   0    0    1     s     c

   e   n   *     g    o   T    a   i    f    r   T   a    e    c   r    v   u    c    a   d   r    i     o    r   a    p      n    i

  -    n   *    f    o   T     o   i    f   -    T   a    T    c   r    u   u    c     o   d   r    i     o    r   a    p

* 110-seat class aircraft @ 500 NM, North American environment

Unmatched environmental ootprint

 e   c   o  n   o  m i     c   s 

31

33

Unmatched environmental ootprint

33

 C    S    1     0     0   

Greenhouse Gas Emissions

20% less co2 emissions per seaT

NOx Emissions

50% less nox emissions

50%

>

20%

caep6 no qt (J 2008)

>

50%

>



   0    0    1     s     c

   n   *     o   T    i    f    T   a     c   r    u    c    d   r    i     o    r   a    p      n    i

  -    n   *    f    o   T     o   i    f   -    T   a    T    c   r    u   u    c     o   d   r    i     o    r   a    p

   0    0    1     s     c

   n   *     o   T    i    f    T   a     c   r    u    c    d   r    i     o    r   a    p      n    i

  -    n   *    f    o   T     o   i    f   -    T   a    T    c   r    u   u    c     o   d   r    i     o    r   a    p

* 110-seat class aircraft @ 500 NM,

 e  n  v  i    r    o  n  m  e  n   t    a  l    f    o   o   t    p  r   i    n   t  

35

 C    S    1     0     0   

Greenhouse Gas Emissions

20% less co2 emissions per seaT

NOx Emissions

50% less nox emissions

50%

>

20%

caep6 no qt (J 2008)

>

50%

>



   0    0    1     s     c

   n   *     o   T    i    f    T   a     c   r    u    c    d   r    i     o    r   a    p      n    i

  -    n   *    f    o   T     o   i    f   -    T   a    T    c   r    u   u    c     o   d   r    i     o    r   a    p

   0    0    1     s     c

   n   *     o   T    i    f    T   a     c   r    u    c    d   r    i     o    r   a    p      n    i

  -    n   *    f    o   T     o   i    f   -    T   a    T    c   r    u   u    c     o   d   r    i     o    r   a    p

* 110-seat class aircraft @ 500 NM, North American environment

Noise reduction

 e  n  v  i    r    o  n  m  e  n   t    a  l    f    o   o   t    p  r   i    n   t  

35

37

Noise reduction

37

 C    S    1     0     0   

Community Noise

Noise Footprint

communiTy noise levels (epnb)

70 ba noise conTour

4

quieter

chapTer 4

21 epnb 

   0    0    1     s     c

   n   *     o   T    i    f    T   a     c   r    u    c    d   r     o   i    a    r    p      n    i

  -    n   *    f    o   T     o   i    f   -    T   a    T    c   r    u   u    c     o   d   r     o   i    a    r    p

CS100 110-seat capacity

n   o  i     s   e  f    o   o   t    p  r   i    n   t  

39

 C    S    1     0     0   

Community Noise

Noise Footprint

communiTy noise levels (epnb)

70 ba noise conTour

4

quieter

chapTer 4

21 epnb 

   0    0    1     s     c

   n   *     o   T    i    f    T   a     c   r    u    c    d   r     o   i    a    r    p      n    i

n   o  i     s   e  f    o   o   t    p  r   i    n   t  

  -    n   *    f    o   T     o   i    f   -    T   a    T    c   r    u   u    c     o   d   r     o   i    a    r    p

CS100 110-seat capacity in-production aircraft

 Aircrat Health Management System

39

 C    S    1     0     0   

Diagnostic and Prognostic Solutions through aircraft integration

99% reliability

at entry into service 99.5% reliability two years after entry into service

enhanced diagnosTic  All Systems Central R eporting Parameter snapshot on fault Flight Deck Effect correlation  Automatic a nd / or Manual in -flight reporting

web based user inTerace Fleet Tracking Enhanced troubleshooting Event Monitoring Prognostic / Usage Monitoring

bi-direcTional communicaTion  ACARS / Satcom Ground Wireless

daTa sTorage and managemenT 5,000 parameters for 100 Flights Customizable reports

r    e  l    i     a   b   i    l    i     t    y   a  n   d   m  a  i    n   t    a  i    n   a   b   i    l    i     t    y 

41

 Aircrat Health Management System

 C    S    1     0     0   

Diagnostic and Prognostic Solutions through aircraft integration

99% reliability

at entry into service 99.5% reliability two years after entry into service

enhanced diagnosTic  All Systems Central R eporting Parameter snapshot on fault Flight Deck Effect correlation  Automatic a nd / or Manual in -flight reporting

web based user inTerace Fleet Tracking Enhanced troubleshooting Event Monitoring Prognostic / Usage Monitoring

bi-direcTional communicaTion  ACARS / Satcom Ground Wireless

daTa sTorage and managemenT 5,000 parameters for 100 Flights Customizable reports

r    e  l    i     a   b   i    l    i     t    y   a  n   d   m  a  i    n   t    a  i    n   a   b   i    l    i     t    y 

41

 C    S    1     0     0   

Maintenance Intervals

service check 

100

t 

“a ” check 

750 t 

“c” check 

7,500 t 

calendar check 

3, 6 12 



sTrucTural inspecTion

12



Change changes everything

r    e  l    i     a   b   i    l    i     t    y   a  n   d   m  a  i    n   t    a  i    n   a   b   i    l    i     t    y 

43

 C    S    1     0     0   

Maintenance Intervals

service check 

100

t 

“a ” check 

750 t 

“c” check 

calendar check 

3, 6 12 



sTrucTural inspecTion

12



7,500 t 

Change changes everything

r    e  l    i     a   b   i    l    i     t    y   a  n   d   m  a  i    n   t    a  i    n   a   b   i    l    i     t    y 

43

Introducing the CS300 The larger o The Two models in The cseries  a i r c r a  T  a m i ly , T h e 130-seaT cs300 aircraT is designed or higher densiTy, longer-range, single-aisle markeTs. T b cs300 t     t  t  t  t ; t   t t t  t    ,      ft tt t  . l t cs100 t, t cs300    t  t ft  -   t t.

 C    S     3     0     0   

r  t t ,  cs t t t   t      - t  t tt tt t   . T t t t  t cs t  t t   t   t q    ,  t t  t t. pt, t…  . p 20%  co 2 , 50%  no,  t   , t cs   t  t t - t  t .

45

 C    S     3     0     0   

Introducing the CS300 The larger o The Two models in The cseries  a i r c r a  T  a m i ly , T h e 130-seaT cs300 aircraT is designed or higher densiTy, longer-range, single-aisle markeTs. T b cs300 t     t  t  t  t ; t   t t t  t    ,      ft tt t  . l t cs100 t, t cs300    t  t ft  -   t t.

r  t t ,  cs t t t   t      - t  t tt tt t   . T t t t  t cs t  t t   t   t q    ,  t t  t t. pt, t…  . p 20%  co 2 , 50%  no,  t   , t cs   t  t t - t  t .

45

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Technical Specifcations weighTs

general

Passengers

Capacity

130 (up to 145)

perormance

Maximum Takeoff Weight

139,600 lb. 63,322 kg

Maximum Landing Weight

122,000 lb. 55,339 kg

Maximum Payload

Range

(MTOW, normal cruise, 130 pax. @ 225 lb. /102 kg)

2,950 NM 3,395 SM 5,463 km

38,200 lb. 17,327 kg Takeoff Field Length

(ISA,SL, MTOW, Max. Thrust)

Cargo

6,200 ft. 1,890 m

 Volume Weight

1,058 ft. 3 / 30.0 m 3 10,580 lb. / 4,799 kg

Landing Field Length

(ISA, SL, MLW)

4,750 ft. 1,448 m

 t    e   c  h   n  i     c   a  l     s   p   e   c  i    f   i     c   a   t   i     o  n   s 

47

 C    S     3     0     0   

Technical Specifcations weighTs

general

Passengers

Capacity

130 (up to 145)

perormance

Maximum Takeoff Weight

139,600 lb. 63,322 kg

Maximum Landing Weight

122,000 lb. 55,339 kg

Maximum Payload

Range

(MTOW, normal cruise, 130 pax. @ 225 lb. /102 kg)

2,950 NM 3,395 SM 5,463 km

38,200 lb. 17,327 kg Takeoff Field Length

(ISA,SL, MTOW, Max. Thrust)

Cargo

6,200 ft. 1,890 m

 Volume Weight

1,058 ft. 3 / 30.0 m 3 10,580 lb. / 4,799 kg

Landing Field Length

(ISA, SL, MLW)

4,750 ft. 1,448 m

 t    e   c  h   n  i     c   a  l     s   p   e   c  i    f   i     c   a   t   i     o  n   s 

47

 C    S     3     0     0   

Technical Specifcations engine

2 Pratt & Whitney PurePower PW1500G Engines

speed (l370, isa)

®

 a d v a n c e d  l i g h T deck eaTures

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

PW1521G Engines

Maximum Takeoff Thrust (MTOT) 21,000 lbf. / 93.4 kN Flat Rating ISA + 15.0°C

PW1524G Engines

Maximum Takeoff Thrust (MTOT) 23,300 lbf. / 103.6 kN Flat Rating ISA + 15.0°C

+ Five large 15.1” LCD Displays + Advanced Fly-by-Wire with Full Envelope Protection & Speed Stabilization + Side Stick Controls + Integrated Flight Management System + Advanced Multi-Scan Weather Radar + Data Link with Full Format Printer + Automatic Dependent SurveillanceBroadcast (ADS-B) Out + Controller Pilot Data Link  Communication (CPDLC) Ready + CAT IIIa Autoland + CAT IIIb Autoland* + Single / Dual Head-Up Display (HUD)* + Electronic Flight Bag (EFB)* * Optional feature

 t    e   c  h   n  i     c   a  l     s   p   e   c  i    f   i     c   a   t   i     o  n   s 

49

 C    S     3     0     0   

Technical Specifcations engine

2 Pratt & Whitney PurePower PW1500G Engines

speed (l370, isa)

®

 a d v a n c e d  l i g h T deck eaTures

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

PW1521G Engines

Maximum Takeoff Thrust (MTOT) 21,000 lbf. / 93.4 kN Flat Rating ISA + 15.0°C

PW1524G Engines

Maximum Takeoff Thrust (MTOT) 23,300 lbf. / 103.6 kN Flat Rating ISA + 15.0°C

+ Five large 15.1” LCD Displays + Advanced Fly-by-Wire with Full Envelope Protection & Speed Stabilization + Side Stick Controls + Integrated Flight Management System + Advanced Multi-Scan Weather Radar + Data Link with Full Format Printer + Automatic Dependent SurveillanceBroadcast (ADS-B) Out + Controller Pilot Data Link  Communication (CPDLC) Ready + CAT IIIa Autoland + CAT IIIb Autoland* + Single / Dual Head-Up Display (HUD)* + Electronic Flight Bag (EFB)* * Optional feature

 t    e   c  h   n  i     c   a  l     s   p   e   c  i    f   i     c   a   t   i     o  n   s 

49

 C    S     3     0     0   

 Advanced Technology  a d v a n c e d  l i g h T d e c k a n d  ly - b y- w i r e w i T h s i d e s T i c k s inTegraTed avionics & opTimized sysTems  a d v a n c e d a l u m i n u m l i T h i u m  u s e l a g e besT-in-class cabin comorT and lexibiliTy

 a d v a n c e d c o m p o s i T e w i n g , e m p e n n a g e a n d r e a r  u s e l a g e elecTric brakes superior ield perormance & range lexibiliTy praTT & whiTney purepower® pw1500g engine  a d v a n c e d c o m p o s i T e n a c e l l e

12,000

  o    t

  p   u

lb. lighter *

* Vs. in-production aircraft of 130-seat

 a   d   v   a  n   c   e   d    t    e   c  h   n   o  l     o   g   y 

51

 C    S     3     0     0   

 Advanced Technology  a d v a n c e d  l i g h T d e c k a n d  ly - b y- w i r e w i T h s i d e s T i c k s inTegraTed avionics & opTimized sysTems  a d v a n c e d a l u m i n u m l i T h i u m  u s e l a g e besT-in-class cabin comorT and lexibiliTy

 a d v a n c e d c o m p o s i T e w i n g , e m p e n n a g e a n d r e a r  u s e l a g e elecTric brakes superior ield perormance & range lexibiliTy praTT & whiTney purepower® pw1500g engine  a d v a n c e d c o m p o s i T e n a c e l l e

12,000

  o    t

  p   u

lb. lighter *

* Vs. in-production aircraft of 130-seat category and re-engined options.

Pratt & Whitney PurePower ® PW1500G Engine

 a   d   v   a  n   c   e   d    t    e   c  h   n   o  l     o   g   y 

51

 C    S     3     0     0   

 A S t e p C h a n g e i n Te c h n o l o g y

high speed, advanced low pressure compressor and Turbine  a d v a n c e d T u r b i n e a e r o d y n a m i c s T a l o n Tm x c o m b u s T o r inTegrally bladed roTor (ibr)  a d v a n c e d n a c e l l e T e c h n o l o g y

high bypass an an drive gear sysTem (dgs)  e  n   g  i    n   e 

53

 C    S     3     0     0   

Pratt & Whitney PurePower ® PW1500G Engine  A S t e p C h a n g e i n Te c h n o l o g y

high speed, advanced low pressure compressor and Turbine  a d v a n c e d T u r b i n e a e r o d y n a m i c s T a l o n Tm x c o m b u s T o r inTegrally bladed roTor (ibr)  a d v a n c e d n a c e l l e T e c h n o l o g y

high bypass an an drive gear sysTem (dgs)  e  n   g  i    n   e 

53

 Advanced Flight Deck

 C    S     3     0     0   

A inTegraTed lighT managemenT sysTem B graphical lighT planning

k 

C sensed elecTronic checklisT

m

D  a d va n c e d m u lT i - s c a n w e a T h e r r a d a r E  a d v a n c e d  ly - b y- w i r e w i T h s i d e s T i c k c o n T r o l s

h

F  a u T o T h r o T T l e (       t     t       )

i

J

G caT iiia auToland (caT iiib opTional)

g

d

e

b

H conTroller piloT daTa link communicaTion (cpdlc) ready I daTa link wiTh ull ormaT prinTer

  a

l

c

J opTimized human-machine inTerace K  h e a d u p d i s p l a y s (   t      ) L class 2 elecTronic lighT bags (t) M growTh capabiliTy

 a   d   v   a  n   c   e   d   f   l    i     g  h    t    d    e   c  k  

55

 C    S     3     0     0   

 Advanced Flight Deck A inTegraTed lighT managemenT sysTem B graphical lighT planning

k 

C sensed elecTronic checklisT

m

D  a d va n c e d m u lT i - s c a n w e a T h e r r a d a r E  a d v a n c e d  ly - b y- w i r e w i T h s i d e s T i c k c o n T r o l s

h

F  a u T o T h r o T T l e (       t     t       )

i

J

G caT iiia auToland (caT iiib opTional)

g

d

b

e

H conTroller piloT daTa link communicaTion (cpdlc) ready

l

 a

 a   d   v   a  n   c   e   d   f   l    i     g  h    t    d    e   c  k  

I daTa link wiTh ull ormaT prinTer

 c

J opTimized human-machine inTerace K  h e a d u p d i s p l a y s (   t      ) L class 2 elecTronic lighT bags (t) M growTh capabiliTy

55

 C    S     3     0     0   

Dimensions

wingspan

lengTh

wingspan

lengTh

124 10 38.0 t.

115 1 35.1

 .

t.



.



uselage maximum diameTer wing area  (neT)

1,209 112.3

uselage maximum diameTer t.2

12 2 3.7

heighT

t.

2

.



wing area (neT) heighT

37 9 11.5 t.

.



 d   i    m  e  n   s  i     o  n   s 

57

 C    S     3     0     0   

Dimensions

wingspan

lengTh

wingspan

lengTh

124 10 38.0 t.

115 1 35.1

 .

t.



.



uselage maximum diameTer wing area  (neT)

1,209 112.3

uselage maximum diameTer t.2

12 2 3.7

heighT

t.

2

.



wing area (neT) heighT

37 9 11.5 t.

.



 d   i    m  e  n   s  i     o  n   s 

57

 C    S     3     0     0   

Confgurations

Cross Sections bus in ess c la ss

dual class

economy class

120

t

36 32

. t t

   m

   0    5  .    1

    |  .         

   3    1  .    2

22.0  . | 0.56 

   m

20.0  . | 0.51 

    |  a

 a

a 

   0  .    9    5

121.9  . | 3.10  129.0  . | 3.28 

a

 .         

   0  .    4    8

b

c

b

b

b sTandard single class

130

t

32

. t t

 A - Wide 20.0 in. / 0.51 m Business class seat B - Wide 18.5 in. / 0.47 m seat C - Oversized 19.0 in. / 0.48 m middle seat

OVERHEAD BINS (pivot bins)

Greater than 100 standard roll aboards (22 in. x 14 in. x 9 in.)

BIN VOLUME PER PASSENGER

2.4 ft. 3 (0.07 m 3) 130 pax. configuration

CABIN WINDOWS

Large 11 in. x 16 in. (27.9 cm x 40.6 cm)  At least on e window available at each se at row

high densiTy single class

145

t

30

. t t

 c  r    o   s   s   s   e   c   t   i     o  n   s   a  n   d    c   o  n  f   i     g   u  r    a   t   i     o  n   s 

59

 C    S     3     0     0   

Confgurations

Cross Sections bus in ess c la ss

120

dual class

economy class

t

36 32

. t t

   m

   0    5  .    1

    |  .         

   3    1  .    2

22.0  . | 0.56 

   m

20.0  . | 0.51 

    |  a

 a

a 

a

   0  .    9    5

121.9  . | 3.10 

 .         

   0  .    4    8

b

c

b

b

b

130

sTandard single class

t

32

 c  r    o   s   s   s   e   c   t   i     o  n   s   a  n   d    c   o  n  f   i     g   u  r    a   t   i     o  n   s 

. t t

 A - Wide 20.0 in. / 0.51 m Business class seat B - Wide 18.5 in. / 0.47 m seat C - Oversized 19.0 in. / 0.48 m middle seat

129.0  . | 3.28 

OVERHEAD BINS (pivot bins)

Greater than 100 standard roll aboards (22 in. x 14 in. x 9 in.)

BIN VOLUME PER PASSENGER

2.4 ft. 3 (0.07 m 3) 130 pax. configuration

CABIN WINDOWS

Large 11 in. x 16 in. (27.9 cm x 40.6 cm)  At least on e window available at each se at row

145

high densiTy single class

t

30

. t t

59

 C    S     3     0     0   

Range Capability  a m e r i c a s / / n e w y o r k / / J  k  

europe // rankurT // ra 

 a s i a pa c i  i c / / h o n g k o n g / / h k g

middle easT // dubai // dxb

Stockholm Riga Berlin Ulaanbaatar

Toronto

London Paris

NEW YORK

St.Louis

Seoul

Stockholm Moscow

Lhasa Mumbai

FRANKFURT

Tokyo

Xian

Delhi Chengdu

Calcutta

Chongqing

 Almaty

Istanbul

Beijing

Oslo

St.Johns Denver Los Angeles

Karaganda

Rome

Reykjavik 

 Vancouver

Moscow

 Vienna

Urumqi

Shanghai

 Athens Tripoli

Tehran Cairo

Delhi

Kunming HONG KONG

 Ashgabat

DUBAI

Dallas Bermuda Islands

Houston

Lisbon

Las Palmas

Mumbai

 Athens Tripoli

Manila

Bangkok 

Rome

Casablanca Mexico City

Hochiminh

Dubai Cairo

 Addis Abeba Brunei

Riyadh Singapore

Jeddah Caracas Bogota Quito

Calcutta

Jeddah

Tehran

Nairobi

Dakar Darwin

Georgetown Kano

 Antananarivo

 a s s u m p T i o n s range

2,950

nm

3,395 sm 5,463 

++ Type Spec Aircraft Configuration ++ 130 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)

r    a  n   g   e   c   a   p   a   b   i    l    i     t    y 

61

 C    S     3     0     0   

Range Capability  a m e r i c a s / / n e w y o r k / / J  k  

europe // rankurT // ra 

 a s i a pa c i  i c / / h o n g k o n g / / h k g

middle easT // dubai // dxb

Stockholm Riga Berlin Ulaanbaatar

Toronto

London Paris

NEW YORK

St.Louis

Seoul

Stockholm Moscow

Lhasa Mumbai

FRANKFURT

Tokyo

Xian

Delhi Chengdu

Calcutta

Chongqing

 Almaty

Istanbul

Beijing

Oslo

St.Johns Denver Los Angeles

Karaganda

Rome

Reykjavik 

 Vancouver

Moscow

 Vienna

Urumqi

Shanghai

 Athens Tripoli

Tehran Cairo

Delhi

Kunming HONG KONG

 Ashgabat

DUBAI

Dallas Bermuda Islands

Houston

Lisbon

Las Palmas

Mumbai

 Athens Tripoli

Manila

Bangkok 

Rome

Casablanca Mexico City

Hochiminh

Dubai Cairo

 Addis Abeba Brunei

Riyadh Singapore

Jeddah Caracas Bogota Quito

Calcutta

Jeddah

Tehran

Nairobi

Dakar Darwin

Georgetown Kano

 Antananarivo

 a s s u m p T i o n s range

2,950

nm

3,395 sm 5,463 

++ Type Spec Aircraft Configuration ++ 130 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)

r    a  n   g   e   c   a   p   a   b   i    l    i     t    y 

61

Block uel advantage

63

Block uel advantage

63

 C    S     3     0     0   

Block Fuel  Advantage

block uel advanTage per seaT

50%

>

12%

>

   0    0    3     s     c

   d   T    e   f    n   a    i    r     g    c    n   r    e   i   -    a    e    r

20%

>

20%

opTimal aircraT inTegraTion + game changing engine

uel burn advantage    n   *     o   T    i    f    T   a     c   r    u    c    d   r    i     o   a    r    p      n    i

 b   l     o   c  k   f    u   e  l     a   d   v   a  n   t    a   g   e 

  -    n   *    f    o   T     o   i    f   -    T   a    T    c   r    u   u    c     o   d   r    i     o   a    r    p

* Compared to 130-seat class

65

 C    S     3     0     0   

Block Fuel  Advantage

block uel advanTage per seaT

50%

>

12%

>

   0    0    3     s     c

   d   T    e   f    n   a    i    r     g    c    n   r    e   i   -    a    e    r

20%

>

20%

opTimal aircraT inTegraTion + game changing engine

uel burn advantage    n   *     o   T    i    f    T   a     c   r    u    c    d   r    i     o   a    r    p      n    i

 b   l     o   c  k   f    u   e  l     a   d   v   a  n   t    a   g   e 

  -    n   *    f    o   T     o   i    f   -    T   a    T    c   r    u   u    c     o   d   r    i     o   a    r    p

* Compared to 130-seat class in-productionaircraft

Economics

65

67

Economics

67

 C    S     3     0     0   

15%

COC advantage

Cash Operating Costs Comparison Per Seat

coc per seaT

30%

>

12%

>

   0    0    3     s     c

   d   T    e   f    n   a    i    r     g    c    n   r    e   i   -    a    e    r

15%

>

   e   n   *     g    o   T    a   i    f    r   T   a    e    c   r    v   u    c    a   d   r    i     o    r   a    p      n    i

  -    n   *    f    o   T     o   i    f   -    T   a    T    c   r    u   u    c     o   d   r    i     o    r   a    p

* 130-seat class aircraft @ 500 NM,

 e   c   o  n   o  m i     c   s 

69

 C    S     3     0     0   

15%

COC advantage

Cash Operating Costs Comparison Per Seat

coc per seaT

30%

>

12%

>

   0    0    3     s     c

   d   T    e   f    n   a    i    r     g    c    n   r    e   i   -    a    e    r

15%

>

   e   n   *     g    o   T    a   i    f    r   T   a    e    c   r    v   u    c    a   d   r    i     o    r   a    p      n    i

  -    n   *    f    o   T     o   i    f   -    T   a    T    c   r    u   u    c     o   d   r    i     o    r   a    p

* 130-seat class aircraft @ 500 NM, North American environment

Unmatched environmental ootprint

 e   c   o  n   o  m i     c   s 

69

71

Unmatched environmental ootprint

71

 C    S     3     0     0   

Greenhouse Gas Emissions

NOx Emissions

20% less co2 emissions per seaT

50% less nox emissions

50%

>

20%

>

12%

>

   0    0    3     s     c

   d   T    e   f    n   a    i    r     g    c    n   r    e   i   -    a    e    r

caep6 no qt (J 2008)

50%

>



   n   *     o   T    i    f    T   a     c   r    u    c    d   r    i     o    r   a    p      n    i

  -    n   *    f    o   T     o   i    f   -    T   a    T    c   r    u   u    c     o   d   r    i     o    r   a    p

   0    0    3     s     c

   n   *     o   T    i    f    T   a     c   r    u    c    d   r    i     o    r   a    p      n    i

  -    n   *    f    o   T     o   i    f   -    T   a    T    c   r    u   u    c     o   d   r    i     o    r   a    p

* 130-seat class aircraft @ 500 NM,

 e  n  v  i    r    o  n  m  e  n   t    a  l    f    o   o   t    p  r   i    n   t  

73

 C    S     3     0     0   

Greenhouse Gas Emissions

NOx Emissions

20% less co2 emissions per seaT

50% less nox emissions

50%

>

20%

>

12%

>

   0    0    3     s     c

   d   T    e   f    n   a    i    r     g    c    n   r    e   i   -    a    e    r

caep6 no qt (J 2008)

50%

>



   n   *     o   T    i    f    T   a     c   r    u    c    d   r    i     o    r   a    p      n    i

  -    n   *    f    o   T     o   i    f   -    T   a    T    c   r    u   u    c     o   d   r    i     o    r   a    p

   0    0    3     s     c

   n   *     o   T    i    f    T   a     c   r    u    c    d   r    i     o    r   a    p      n    i

  -    n   *    f    o   T     o   i    f   -    T   a    T    c   r    u   u    c     o   d   r    i     o    r   a    p

* 130-seat class aircraft @ 500 NM, North American environment

Noise reduction

 e  n  v  i    r    o  n  m  e  n   t    a  l    f    o   o   t    p  r   i    n   t  

73

75

Noise reduction

75

 C    S     3     0     0   

Community Noise

Noise Footprint

communiTy noise levels (epnb)

70 ba noise conTour

4

quieter

chapTer 4

20 epnb 

   0    0    3     s     c

   n   *     o   T    i    f    T   a     c   r    u    c    d   r     o   i    a    r    p      n    i

  -    n   *    f    o   T     o   i    f   -    T   a    T    c   r    u   u    c     o   d   r     o   i    a    r    p

CS300 130-seat capacity

n   o  i     s   e  f    o   o   t    p  r   i    n   t  

77

 C    S     3     0     0   

Community Noise

Noise Footprint

communiTy noise levels (epnb)

70 ba noise conTour

4

quieter

chapTer 4

20 epnb 

   0    0    3     s     c

   n   *     o   T    i    f    T   a     c   r    u    c    d   r     o   i    a    r    p      n    i

  -    n   *    f    o   T     o   i    f   -    T   a    T    c   r    u   u    c     o   d   r     o   i    a    r    p

CS300 130-seat capacity in-production aircraft

 Aircrat Health Management System

n   o  i     s   e  f    o   o   t    p  r   i    n   t  

77

 C    S     3     0     0   

Diagnostic and Prognostic Solutions through aircraft integration

99% reliability

at entry into service 99.5% reliability two years after entry into service

enhanced diagnosTic  All Systems Central R eporting Parameter snapshot on fault Flight Deck Effect correlation  Automatic a nd / or Manual in -flight reporting

web based user inTerace Fleet Tracking Enhanced troubleshooting Event Monitoring Prognostic / Usage Monitoring

bi-direcTional communicaTion  ACARS / Satcom Ground Wireless

daTa sTorage and managemenT 5,000 parameters for 100 Flights Customizable reports

r    e  l    i     a   b   i    l    i     t    y   a  n   d   m  a  i    n   t    a  i    n   a   b   i    l    i     t    y 

79

 Aircrat Health Management System

 C    S     3     0     0   

Diagnostic and Prognostic Solutions through aircraft integration

99% reliability

at entry into service 99.5% reliability two years after entry into service

enhanced diagnosTic  All Systems Central R eporting Parameter snapshot on fault Flight Deck Effect correlation  Automatic a nd / or Manual in -flight reporting

web based user inTerace Fleet Tracking Enhanced troubleshooting Event Monitoring Prognostic / Usage Monitoring

bi-direcTional communicaTion  ACARS / Satcom Ground Wireless

daTa sTorage and managemenT 5,000 parameters for 100 Flights Customizable reports

r    e  l    i     a   b   i    l    i     t    y   a  n   d   m  a  i    n   t    a  i    n   a   b   i    l    i     t    y 

79

 C    S     3     0     0   

Maintenance Intervals

service check 

100

t 

“a ” check 

750 t 

“c” check 

7,500 t 

calendar check 

3, 6 12 



sTrucTural inspecTion

12

Bombardier Customer Services Globally. Locally. We put



people, passion and perormance ..

r    e  l    i     a   b   i    l    i     t    y   a  n   d   m  a  i    n   t    a  i    n   a   b   i    l    i     t    y 

81

 C    S     3     0     0   

Maintenance Intervals

service check 

100

t 

“a ” check 

750 t 

“c” check 

7,500 t 

calendar check 

3, 6 12 



sTrucTural inspecTion

12

Bombardier Customer Services Globally. Locally. We put



people, passion and perormance ..

r    e  l    i     a   b   i    l    i     t    y   a  n   d   m  a  i    n   t    a  i    n   a   b   i    l    i     t    y 

81