CSeries Brochure En

8/2/2019 CSeries Brochure En

1/42

100%newaircrat


2/42

T h e w o r l d h a s c h a n g e d ,a n d T h e c s e r i e sa i r c r a T i s T h e o n ly1 0 0 % n e w l y d e s i g n e d

a i r c r a T T o m e e T T o d ay so p e r a T i o n a l r e a l i T i e s .

T cs * t

latest generation aerodynamics,

system integration and advancedstructural materials, t

, t

20% fuel burn benefit

-t t t

15% cash operating costs

advantage. T t -

t t t, t cs

t t 20% fewer CO2

50% fewer NOx emissions,

4 times quietert t tt.

it t, t t

t widebody cabin

comfort t

. T t

t, t cs t

t t .

Changeis in

the air


3/42

Introducingthe

CS100

Introducingthe

CS300

0 8 T e c h n i c a ls p e c i i c a T i o n s

4 6 T e c h n i c a ls p e c i i c a T i o n s

2 2 r a n g ec a p a b i l i T y

6 0 r a n g ec a p a b i l i T y

1 4 e n g i n e 5 2 e n g i n e

2 5 b l o c k u e la d v an Ta g e

6 3 b l o c k u e la d va n Ta g e

1 2 a d v a n c e dT e c h n o l o g y

5 0 a d v a n c e dT e c h n o l o g y

2 9 e c o n o m i c s 6 7 e c o n o m i c s

1 6 a d v a n c e d l i g h T d e c k

5 4 a d v a n c e d l i g h T d e c k

3 3 e n v i r o n m e n T a l o o T p r i n T

7 1 e n v i r o n m e n T a l o o T p r i n T

1 8 d i m e n s i o n s 5 6 d i m e n s i o n s

2 0 c r o s s s e c T i o n s / c o n i g u r a T i o n s

5 8 c r o s s s e c T i o n s / c o n i g u r a T i o n s

3 7 n o i s e o o T p r i n T

7 5 n o i s e o o T p r i n T

4 0 r e l i a b i l i T y / m a i n T a i n a b i l i T y

7 8 r e l i a b i l i T y /

m a i n T a i n a b i l i T y


4/42

07

CS100

T h e s m a l l e r o T h e T w o m o d e l s i n T h ec s e r i e s a m i l y, T h e1 1 0 - s e a T c s 1 0 0 a i r c r a Ti s d e s i g n e d o r l o w e rd e n s i T y , l o n g e r r a n g e ,s i n g l e - a i s l e m a r k e T s .

T b * cs100 * t

t t ttt ,

t tt

t t t t

. b ,

t cs100 t t

t t

- t t.

Tt, t cs100 t cs300 *

t 95% t t,

t t tt,

t, t,

t

t t.

ot t

t,

t t. T cs

t t

tt, t t tt

,

t t ptt & wt pp

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 tt t

tt 99% t t

t t , 99.5% t

t t t t .

Introducingthe

CS100


5/42

09

CS100

technicalspecifications

TechnicalSpecifcations

g e n e r a l

P a s s e n g e r s

Capacity 110 (up to 125)

C a r g o

Volume 819 ft. 3 / 23.2 m3Weight 8,190 lb. / 3,715 kg

p e r o r m a n c e

R a n g e ( M T O W , n o r m a lc r u i s e , 1 1 0 p a x @

2 2 5 l b . / 1 0 2 k g )

2,950 NM

3,395 SM

5,463 km

T a k e o f f ( I S A , S L , M T O W ,F i e l d L e n g t h m a x . t h r u s t )

4,950 ft.

1,509 m

L a n d i n g ( I S A , S L , M L W )F i e l d L e n g t h

4,430 ft.

1,350 m

w e i g h T s

Maximum Takeoff Weight 128,200 lb.

58,151 kg

Maximum Landing Weight 111,500 lb.

50,576 kg

Maximum Payload 32,100 lb.

14,560 kg


6/42

CS100

11

technicalspecif

ications

e n g i n e

2 Pratt & Whitney PurePower

PW1500G Engines

P W 1 5 1 9 G E n g i n e s

Maximum Takeoff

Thrust (MTOT) 18,900 lbf. / 84.1 kN

Flat Rating ISA + 15.0C

P W 1 5 2 1 G E n g i n e s

Maximum Takeoff



P W 1 5 2 4 G E n g i n e sMaximum Takeoff



a d v a n c e d l i g h Td e c k e a T u r e s

+ 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 Surveillance-

Broadcast (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

s p e e d( l 3 7 0 , i s a )

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



7/42

13

CS100

advancedtec

hnology

AdvancedTechnology

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

a d v a n c e d c o m p o s i T e n a c e l l e

b e s T - i n - c l a s s c a b i n c o m o r T a n d l e x i b i l i T y

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

i n T e g r a T e d a v i o n i c s & o p T i m i z e d s y s T e m s

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

p r a T T & w h i T n e y p u r e p o w e r

p w 1 5 0 0 g e n g i n e

e l e c T r i c b r a k e s

s u p e r i o r i e l d p e r o r m a n c e & r a n g e l e x i b i l i T y


8/42

15

CS100

engine

Pratt & WhitneyPurePowerPW1500G Engine

h i g h s p e e d , a d v a n c e d l o w p r e s s u r e c o m p r e s s o r a n d T u r b i n e

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

i n T e g r a l l y b l a d e d r o T o r ( i b r )

h i g h b y p a s s a n

a n d r i v e g e a r s y s T e m ( d g s )

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

A S tep Change in Te chnology


9/42

17

CS100

advancedflig

htdeck

AdvancedFlight Deck

a c

b

d

Jh

e

gl

i

mk

A i n T e g r a T e d l i g h T m a n a g e m e n T s y s T e m

B g r a p h i c a l l i g h T p l a n n i n g

C s e n s e d e l e c T r o n i c c h e c k l i s T

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

F a u T o T h r o T T l e ( t t )

G c a T i i i a a u T o l a n d ( c a T i i i b o p T i o n a l )

H c o n T r o l l e r p i l o T d a T a l i n k c o m m u n i c a T i o n ( c p d l c ) r e a d y

I d a T a l i n k w i T h u l l o r m a T p r i n T e r

J o p T i m i z e d h u m a n - m a c h i n e i n T e r a c e

K h e a d u p d i s p l a y s ( t )

L c l a s s 2 e l e c T r o n i c l i g h T b a g s ( t )

M g r o w T h c a p a b i l i T y


10/42

19

CS100

dim

ensions

heighT

uselagemax imum d iameTer

wingspan

wing area (neT)

lengTh

l e n g T h

w i n g a r e a ( n e T )

w i n g s p a n

u s e l a g e m a x i m u md i a m e T e r

h e i g h T

1,209 t. 2 112.3 2

115 t .1 . 35.1

37 t .9 . 11.5

12 t .2 . 3.7

114 t .6 . 34.9

Dimensions


11/42

21

CS100

crosssectionsandconfigu

rations

d u a l c l a s s

s T a n d a r ds i n g l e c l a s s

h i g h d e n s i T ys i n g l e c l a s s

100 t

110 t

125 t

36 32 . t t

32 . t t

30 . t t

b u s i n e s s c l a s s e c o n o m y c l a s s

129.0 .|3.28

84.0.|2.13m

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

ba aa a bc b b

59.0.|1.50m

20.0 .|0.5122.0 . |0.56

121.9 . |3.10

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

ConfgurationsCrossSections


12/42

23

CS100

rangeca

pability

RangeCapability

a s s u m p T i o n s

++ 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)

a s i a pa c i i c / / h o n g k o n g / / h k ga m e r i c a s / / n e w y o r k / / J k m i d d l e e a s T / / d u b a i / / d x be u r o p e / / r a n k u r T / / r a

r a n g e

2,950 nm 3,395 sm 5,463

Beijing

Singapore

Chongqing

Brunei

ManilaBangkok

CalcuttaMumbai

Delhi

Shanghai

Kunming

Hochiminh

Xian

Chengdu

Tokyo

Ulaanbaatar

Lhasa

Urumqi

Darwin

Seoul

HONG KONGFRANKFURT

Rome

Paris

Athens

Oslo

Lisbon

MoscowStockholm

London

Kano

Dakar

CairoTripoli

Reykjavik

Riyadh

Casablanca

Las Palmas

Jeddah

Tehran

Ashgabat

Dubai

Tripoli

Mumbai

Rome

MoscowBerlin

Cairo

Antananarivo

Calcutta

Nairobi

Delhi

Addis Abeba

Athens

Tehran

Istanbul

Vienna

Stockholm

Riga

Almaty

Karaganda

JeddahDUBAI

Vancouver

Los Angeles

Mexico City

Denver

Dallas

St.Louis

Caracas

Bermuda Islands

St.Johns

Toronto

Houston

Bogota

Quito

Georgetown

NEW YORK


13/42

Block

ueladvantage25


14/42

27

CS100

blockfueladv

antage

o p T i m a l a i r c r a Ti n T e g r a T i o n + g a m ec h a n g i n g e n g i n e

b l o c k u e l a d v a n T a g ep e r s e a T

Block FuelAdvantage

* Compared to 110-seat class

in-production aircraft

20%cs100

ouT-of-

pro

ducTion

a

ircrafT*

>20%

>50%

uel burnadvantage

in-pro

ducTion

a

ircrafT*


15/42

Economics29


16/42

31

CS100

eco

nomics

cs100

average

in-producTion

aircrafT*

ouT-of-

producTion

aircrafT*

* 110-seat class aircraft @ 500 NM,

North American environment

>15%

c o c p e r s e a T

>30%

15%COCadvantage

CashOperating

CostsComparison

Per Seat


17/42

33

Unmatched

environmentalootprint


18/42

35

CS100

environmentalfo

otprint

cs100

in-producTion

aircrafT*

ouT-of-

producTion

aircrafT*



5 0 % l e s s n o xe m i s s i o n s

>50%

c a e p 6 n o q t

( J 2 0 0 8 )

NOxEmissions

2 0 % l e s s c o 2e m i s s i o n s p e r s e a T

GreenhouseGas

Emissions

cs100

in-producTion

aircrafT*

ouT-of-

producTion

aircrafT*

>20%

>50%


19/42

Noisereduction37


20/42

39

CS100

noisefo

otprint

CS100

110-seat capacity


c o m m u n i T yn o i s e l e v e l s ( e p n b )

7 0 b a n o i s e c o n T o u r

cs100

in-p

roducTion

aircrafT*

ouT-of-

p

roducTion

aircrafT*

NoiseFootprint

CommunityNoise

4quieterc h a p T e r 421e p n b


21/42

41

CS100

reliabilityandmaintain

ability

Aircrat HealthManagement System

e n h a n c e d d i a g n o s T i c

All Systems Central R eporting

Parameter snapshot on fault

Flight Deck Effect correlation

Automatic a nd / or Manual in -flight reporting

b i - d i r e c T i o n a l c o m m u n i c a T i o n

ACARS / Satcom

Ground Wireless

w e b b a s e d u s e r i n T e r a c e

Fleet Tracking

Enhanced troubleshooting

Event Monitoring

Prognostic / Usage Monitoring

d a T a s T o r a g e a n d m a n a g e m e n T

5,000 parameters for 100 Flights

Customizable reports

Diagnost ic and Prognost ic So lut ionsthrough a i r c ra f t in tegrat ion

reliabilityat entry

into service

99%99.5% reliability two years after entry into service

C

M i


22/42

43

CS100

reliabilityandmaintain

ability

MaintenanceIntervals

s e r v i c ec h e c k

c a l e n d a rc h e c k

a c h e c k

s T r u c T u r a li n s p e c T i o n

c c h e c k

100 t

3, 6 12

750 t

12

7,500 t

Changechangeseverything

C


23/42

45

CS300

T h e l a r g e r o T h e T w om o d e l s i n T h e c s e r i e s

a i r c r a T a m i ly , T h e1 3 0 - s e a T c s 3 0 0 a i r c r a Ti s d e s i g n e d o r h i g h e rd e n s i T y , l o n g e r - r a n g e ,s i n g l e - a i s l e m a r k e T s .

T b cs300 t

t

t t t ; t

t t t t

,

ft tt t

. l t cs100 t, t cs300

t t

ft -

t t.

r t t ,

cs t t t

t

- t t

tt tt t

. T t t

t t cs t

t t t

t q

,

t t t

t. pt, t

. p 20%

co2 , 50% no,

t ,

t cs t t

t - t

t .

Introducingthe

CS300

C

Technical


24/42

47

CS300

technicalspecific

ations

g e n e r a l

P a s s e n g e r s

Capacity 130 (up to 145)

C a r g o

Volume 1,058 ft. 3 / 30.0 m3

Weight 10,580 lb. / 4,799 kg

w e i g h T s

Maximum Takeoff Weight 139,600 lb.

63,322 kg

Maximum Landing Weight 122,000 lb.

55,339 kg

Maximum Payload 38,200 lb.

17,327 kg

p e r o r m a n c e

R a n g e ( M T O W , n o r m a lc r u i s e , 1 3 0 p a x . @

2 2 5 l b . / 1 0 2 k g )

2,950 NM

3,395 SM

5,463 km

T a k e o f f ( I S A , S L , M T O W ,F i e l d L e n g t h M a x . T h r u s t )

6,200 ft.

1,890 m

L a n d i n g ( I S A , S L , M L W )

F i e l d L e n g t h

4,750 ft.

1,448 m


CSTechnical


25/42

49

technicalspecific

ations

S300

e n g i n e s p e e d( l 3 7 0 , i s a )

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

2 Pratt & Whitney PurePower

PW1500G Engines

P W 1 5 2 1 G E n g i n e s

Maximum Takeoff



P W 1 5 2 4 G E n g i n e s

Maximum Takeoff



a d v a n c e d l i g h Td e c k e a T u r e s

+ 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 Surveillance-

Broadcast (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


CS

Advanced


26/42

51

S300

advancedtechnology

AdvancedTechnology

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

a d v a n c e d c o m p o s i T e n a c e l l e

b e s T - i n - c l a s s c a b i n c o m o r T a n d l e x i b i l i T y

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

i n T e g r a T e d a v i o n i c s & o p T i m i z e d s y s T e m s

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

p r a T T & w h i T n e y p u r e p o w e r p w 1 5 0 0 g e n g i n e

e l e c T r i c b r a k e s

s u p e r i o r i e l d p e r o r m a n c e & r a n g e l e x i b i l i T y

12,000lb. lighter *up

to

* Vs. in-production aircraft of 130-seat

category and re-engined options.

Pratt & WhitneyCS


27/42

53

e

ngine

Pratt & WhitneyPurePowerPW1500G Engine

h i g h s p e e d , a d v a n c e d l o w p r e s s u r e c o m p r e s s o r a n d T u r b i n e

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

i n T e g r a l l y b l a d e d r o T o r ( i b r )

h i g h b y p a s s a n

a n d r i v e g e a r s y s T e m ( d g s )

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

S300

A S tep Change in Te chnology

CS3Advanced


28/42

55

advancedflightdeck

300

AdvancedFlight Deck

A i n T e g r a T e d l i g h T m a n a g e m e n T s y s T e m

B g r a p h i c a l l i g h T p l a n n i n g

C s e n s e d e l e c T r o n i c c h e c k l i s T

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

F a u T o T h r o T T l e ( t t )

G c a T i i i a a u T o l a n d ( c a T i i i b o p T i o n a l )

H c o n T r o l l e r p i l o T d a T a l i n k c o m m u n i c a T i o n ( c p d l c ) r e a d y

I d a T a l i n k w i T h u l l o r m a T p r i n T e r

J o p T i m i z e d h u m a n - m a c h i n e i n T e r a c e

K h e a d u p d i s p l a y s ( t )

L c l a s s 2 e l e c T r o n i c l i g h T b a g s ( t )

M g r o w T h c a p a b i l i T y

a c

b

d

Jh

e

gl

i

mk

CS3Dimensions


29/42

57

wing area (neT)

lengTh

l e n g T h

w i n g a r e a ( n e T )

heighT

uselagemax imum d iameTer

wingspan

w i n g s p a n

u s e l a g e m a x i m u md i a m e T e r

h e i g h Tdimen

sions

300

124 t .10 . 38.0

1,209 t . 2 112.3 2

115 t .1 . 35.1

37 t . 9 . 11.5

12 t . 2 . 3.7

Dimensions

CS3ConfgurationsCross


30/42

59

crosssectionsandconfigurations

300

d u a l c l a s s

s T a n d a r ds i n g l e c l a s s

h i g h d e n s i T ys i n g l e c l a s s

120 t

130 t

145 t

36 32 . t t

32 . t t

30 . t t

Confgurations

b u s i n e s s c l a s s e c o n o m y c l a s s

129.0 .|3.28

84.0.|2.13m

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

ba aa a bc b b

59.0.|1.50m

20.0 .|0.5122.0 . |0.56

121.9 . |3.10

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 m3) 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

CrossSections

RangeCS30


31/42

61

gCapability

a s i a pa c i i c / / h o n g k o n g / / h k g m i d d l e e a s T / / d u b a i / / d x b

r a n g ea s s u m p T i o n s

++ 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)

a m e r i c a s / / n e w y o r k / / J k e u r o p e / / r a n k u r T / / r a

rangecapability

00

2,950nm

3,395 sm 5,463

Beijing

Singapore

Chongqing

Brunei

ManilaBangkok

CalcuttaMumbai

Delhi

Shanghai

Kunming

Hochiminh

Xian

Chengdu

Tokyo

Ulaanbaatar

Lhasa

Urumqi

Darwin

Seoul

HONG KONG

Tripoli

Mumbai

Rome

MoscowBerlin

Cairo

Antananarivo

Calcutta

Nairobi

Delhi

Addis Abeba

Athens

Tehran

Istanbul

Vienna

Stockholm

Riga

Almaty

Karaganda

JeddahDUBAI

Vancouver

Los Angeles

Mexico City

Denver

Dallas

St.Louis

Caracas

Bermuda Islands

St.Johns

Toronto

Houston

Bogota

Quito

Georgetown

NEW YORK FRANKFURT

Rome

Paris

Athens

Oslo

Lisbon

MoscowStockholm

London

Kano

Dakar

CairoTripoli

Reykjavik

Riyadh

Casablanca

Las Palmas

Jeddah

Tehran

Ashgabat

Dubai


32/42

Block

ueladvantage63

CS30


33/42

o p T i m a l a i r c r a Ti n T e g r a T i o n + g a m ec h a n g i n g e n g i n e

b l o c k u e l a d v a n T a g ep e r s e a T

Block FuelAdvantage

* Compared to 130-seat class


20%uel burnadvantage blo

ckfueladva

ntage

65

00

cs300

in-p

roducTion

aircrafT*

ouT-of-

p

roducTion

aircrafT*

r

e-engined

aircrafT

>20%

>50%

>12%


34/42

Economics67

CS300


35/42

69

econo

mics

0

COCadvantage

cs300

average

in-producTion

aircrafT*

re-engined

aircrafT

ouT-of-

producTion

aircrafT*



>15%>12%

c o c p e r s e a T

>30%

CashOperating

CostsComparisonPer Seat15%


36/42

Unmatched

environmentalootprint71

CS300


37/42

environmentalfootprint

cs300

in-producTion

aircrafT*

ouT-of-

producTion

aircrafT*



5 0 % l e s s n o xe m i s s i o n s

>50%

c a e p 6 n o q t

( J 2 0 0 8 )

NOxEmissions

73

environmentalfootprint

cs300

in-producTion

aircrafT*

ouT-of-

producTion

aircrafT*

2 0 % l e s s c o 2e m i s s i o n s p e r s e a T

GreenhouseGas

Emissions

re-engined

aircrafT

>20%

>50%

>12%


38/42

75

Noisereduction

CS300


39/42

77

noisefootprint

c o m m u n i T yn o i s e l e v e l s ( e p n b )

CS300

130-seat capacity


4quieter

7 0 b a n o i s e c o n T o u r

cs300

CommunityNoise

NoiseFootprint

in

-producTion

aircrafT*

ouT-of-

producTion

aircrafT*

c h a p T e r 4

20e p n b

CS300

Aircrat HealthManagement System


40/42

79

reliabilityandmaintaina

bility

Management System

e n h a n c e d d i a g n o s T i c

All Systems Central R eporting

Parameter snapshot on fault

Flight Deck Effect correlation

Automatic a nd / or Manual in -flight reporting

b i - d i r e c T i o n a l c o m m u n i c a T i o n

ACARS / Satcom

Ground Wireless

w e b b a s e d u s e r i n T e r a c e

Fleet Tracking

Enhanced troubleshooting

Event Monitoring

Prognostic / Usage Monitoring

d a T a s T o r a g e a n d m a n a g e m e n T

5,000 parameters for 100 Flights

Customizable reports

reliabilityat entry

into service

99%99.5% reliability two years after entry into service

Diagnost ic and Prognost ic So lut ionsthrough a i r c ra f t in tegrat ion

CS300

MaintenanceIntervals


41/42

s e r v i c e

c h e c k

c a l e n d a r

c h e c k

a c h e c k

s T r u c T u r a li n s p e c T i o n

c c h e c k

100 t

3, 6 12

750 t

12

7,500

t

81

reliabilityandmaintainability

BombardierCustomer ServicesGlobally. Locally.We put

p e o p l e , p a s s i o n a n d p e r o r m a n c e . .


42/42

A newchoice or

a changedworld

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