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EMBRAER 170/190. Marketing Review. Nota Apresentação Resumida. Roll-Out Ceremony São José dos Campos - October 29 th , 2001. 2000. Jul. Sep. Mar. ERJ 170 FIRST ASSEMBLY. ERJ 190-200 PROGRAM START. ERJ 170 FIRST METAL CUT. Oct. ERJ 170 ROLL-OUT CEREMONY.

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Presentation Transcript
slide1

EMBRAER 170/190

Marketing Review

Nota Apresentação Resumida

Roll-Out Ceremony

São José dos Campos - October 29th, 2001

emb 170 190 program progress

2000

Jul

Sep

Mar

ERJ 170 FIRST ASSEMBLY

ERJ 190-200 PROGRAM START

ERJ 170 FIRST METAL CUT

Oct

ERJ 170

ROLL-OUT CEREMONY

EMB 170/190Program Progress

1999

Jan

Jun

Jul

INITIAL DEFINITION PHASE

  • START OF JOINT DEFINITION PHASE

GO-AHEAD & LAUNCH CUSTOMER

  • SELECTION OF PARTNERS

ON TARGET & ON SCHEDULE

2001

Apr

May

Jul

FUSELAGE

ASSEMBLY

S/N 0001

ERJ 170

WING STUB

ASSEMBLY

ERJ 190-200 FULL MOCK-UP

economics of regional jet

with

Mainline Cabin Comfort

Economics of Regional Jet

EMB170/190

embraer 170 190

EMBRAER 170

70 Seats

ERJ 170-100

70 Seats

EMBRAER 190

98 Seats

EMBRAER 195

108 Seats

EMBRAER 170/190

EMB 170/190

ERJ 190-100

98 Seats

ERJ 190-200

108 Seats

embraer 170 190 a new cabin concept

Actual mockup picture

  • Mainline jet comfort
  • Cabin features:
    • no middle seat
    • large headroom
    • easier access to bins and seats
    • faster boarding and unboarding
  • Cabin can accommodate roll-on bags up to 115% load factor
  • Superior ground service access and baggage handling
  • Highest total baggage volume and highest baggage volume per pax in its category

EMBRAER 170/190 – A New Cabin Concept

embraer 170 190 first class
EMBRAER 170/190First Class
  • Three abreast configuration
  • Wide seats (20.0 in/50.8 cm) and wide arm rest (8.0 in/20.3 cm)
  • Comfortable leg rest
  • Large overhead bins that accommodate all First Class passenger’s roll-on bags

PP17090IN033R1

slide7

Cross Section Comparison

EMBRAER 170/190

19

slide8

Cross Section Comparison

A320

EMBRAER 170/190

18.0 in

18.25 in

Slice Volume/Seat = A*P/n

A: Cabin cross section usefull area

P: Seat pitch (32”)

n: number of seats abreast

19.0 in

19.75 in

6.390 m2

5.194 m3

0.866 m3/seat

Baseline

4.280 m2

3.479 m3

0.870 m3/seat

+0.47%

Cabin X-Section Area:

Slice Volume @ 32” pitch:

Slice Volume/seat:

Comparison:

slide9

EMBRAER 170 New Developments

  • TheEMBRAER 170has an excelent mix of Cabin Comfort, Performance and Economics
  • Some potential customers, with less stringent environments, requested an aircraft with extra Payload in exchange for shorter range
  • Additional market surveys confirmed the opportunity for an aircraft with seating capacity between theEMBRAER 170and theEMBRAER 190
slide10

the EMBRAER 175

INTRODUCING …

78 Seats @ 32” pitch

slide11

EMBRAER 175 Interior Arrangements

High Standard Service Level

78 Pax @ 32”

Max Pax

86 Pax @ 31”

slide12

EMBRAER 175 External Configuration

EMBRAER 175

EMBRAER 170

1,78 m (70 in)

slide13

EMBRAER 175 Design Features

Enhanced Air Management System

BOW + 1000 kg

MTOW + 650 kg

MZFW + 2450 kg

Reinforced Wing

slide14

EMBRAER 175

78 Seats

EMBRAER 170

70 Seats

EMBRAER 175 & EMBRAER 170

A unique combined solution to maximize performance, economics and flexibility with same Type Rating and 95% commonality

slide15

EMBRAER 170

70 Seats

EMBRAER 175

78 Seats

EMBRAER 190

98 Seats

EMBRAER 195

108 Seats

EMBRAER 170/190 Family New Development Sequence

designed to exceed market requirements

Designed to Exceed Market Requirements

Passenger:

  • High passenger comfort and appeal

Operator:

  • Low operating costs
  • Easy maintenance
  • Operational flexibility and low turnaround time
  • Commonality within the family
  • High maturity from entry into service

Environment:

  • Exceed future environmental requirements
extensive customer partnership
Extensive Customer Partnership

A Customer driven Design...

  • 5 Airline Advisory Board Meetings
  • 3 Steering Groups for Design Reviews
  • 4 Man-Machine Interface Conferences

...Involving 27 Airlines and 154 Airline Representatives

extensive suppliers partnership
Extensive Suppliers Partnership

SYSTEMS:

HAMILTON SUNDSTRAND (USA)

HONEYWELL (USA)

PARKER (USA)

C & D (USA)

LIEBHERR (GERMANY)

GEAE (USA)

GAMESA (SPAIN)

HAMILTON SUNDSTRAND

(USA)

EMBRAER (LEADER)

KAWASAKI (JAPAN)

SONACA (BELGIUM)

LATECOERE (FRANCE)

LATECOERE

(FRANCE)

EMBRAER

(BRAZIL)

GEAE (USA)

EMBRAER

(BRAZIL)

a joint design teaming effort

300 partner members

at Embraer

All partners co-located at Embraer in early design

A Joint Design Teaming Effort

1999

integration supported by a world wide portal
Integration Supported by a World-Wide Portal

800 people

1800 people

400 people

1500 people

... A virtual team co-location for detailed design and manufacturing

highly integrated tools

Engineering Development Simulator

Virtual Reality Center

Systems Integration Test Station

Iron Bird

Highly Integrated Tools

Electronic mock-up

... reducing development cycle and leading to an optimized product

new facilities and tools
New Facilities and Tools

Final Assembly Hangar

Painting Shop

NCM for Sheet Metal Cutting

investment breakdown embraer 170 190

Material

7%

Partners

R & D

34%

Labor

33%

Building

& Equipment

12%

Other

14%

Investment Breakdown (EMBRAER 170/190)

US$ 850 Million

embraer 170 190 program progress

Feb

Mar

Jul

Sep

Dec

Partners

EMBRAER 170/190Program Progress

1999

Jan

Jun

Jul

  • SELECTION OF PARTNERS

INITIAL DEFINITION PHASE

  • START OF JOINT DEFINITION PHASE

GO-AHEAD & LAUNCH CUSTOMER

2000

EMBRAER 170 FIRST ASSEMBLY

EMBRAER 195 PROGRAM START

EMBRAER 175

BOARD APPROVAL

END OF JOINT DEFINITION PHASE

EMBRAER 170 FIRST METAL CUT

embraer 170 190 program progress1

Partners

EMBRAER 170/190Program Progress

2001

Apr

May

Jul

Aug

EMBRAER 195 JOINT DEFINITION PHASE START-UP

S/N 0001

FULL FUSELAGE WITH WINGS

EMBRAER 195 FULL MOCK-UP

FUSELAGE

ASSEMBLY

S/N 0001

EMBRAER 170

WING STUB

ASSEMBLY

slide27

July 23th

Forward

Fuselage

(Embraer)

Central

Fuselage I

(Latecoere)

Central

Fuselage II

(Embraer)

Central

Fuselage III

(Latecoere)

Rear Fuselage

(Gamesa)

slide29

August 11th

Wing  Fuselage

Junction

slide30

October

Cockpit

slide31

EMBRAER 170

Ready for Roll out

On Schedule

first flight robust certification strategy

S/N 0001

Fatigue Test Setup

S/N 0005

S/N 0003

Oct 01

Nov 01

Dec 01

Jan 02

Feb 02

Mar 02

Apr 02

May 02

Jun 02

Jul 02

Aug 02

Sep 02

Oct 02

Nov 02

Dec 02

S/N 0006

S/N 0002

S/N 0004

Static Test Setup

First Flight & Robust Certification Strategy
  • Functional Tests/
  • Flight Preparation
  • First Flight

Fatigue Test Completion

1st Delivery (Crossair)

Static Test Completion

Roll Out

OCT29 2001

Certification

a family of embraer jets that will meet customer expectations on time

4th quarter/02

2nd quarter/04

4th quarter/04

4th quarter/05

A Family of Embraer Jets that will meet customer expectations – ON TIME