phenom 300 type certificate - embraer jet /...

PHENOM 300 TYPE CERTIFICATE

THE INFORMATION HEREIN IS SUBJECT TO THE DISCLAIMER PRESENTED IN THE LAST PAGE OF THIS DOCUMENT. THIS PRESENTATION IS THE PROPERTY OF EMBRAER AND SHALL NOT BE COPIED, OR USED IN ANY MANNER, EXCEPT WITH EMBRAER´S PRIOR WRITTEN CONSENT.


PROGRAM UPDATE AND DEVELOPMENT HIGHLIGHTS


PHENOM 300 PROGRAM UPDATE

� 5 aircraft used for certification

� Over 1,200 flight test hours performed

� Static tests successfully completed

� RVSM tests accomplished

� IFR operations (day and night) certification accomplished

� Campaign for flying into known and forecasted icing conditions accomplished

� Function and Reliability campaign accomplished

� Performance goals achieved or surpassed


Phenom 300 First Flight – April 2008

DEVELOPMENT HIGHLIGHTS


Cold Soak Test at Eglin Air Force Base



Water spray test at Embraer Gavião Peixoto facility



Flying into known icing campaign



Structural tests:

� Bird strike tests

� Wing ultimate loads tests

� Fatigue tests



Cold weather and crosswind tests



SURPASSING EXPECTATIONS



“After three years of rigorous research and development I’m delighted to let you know that the Phenom 300 is now fully certified.

This achievement marks the final stage of a completely new concept in executive aviation. Through a combination of cutting-edge design and technical innovation we have produced a jet that is truly ahead of its time, and boasts an unrivalled level of comfort, performance and reliability.

In fact, not only have we met our design goals but we have surpassed them. The result is a jet that has exceeded all expectations and sets a new standard in the Light Jet category.”

Luís Carlos Affonso, Embraer Executive Vice President, Executive Jets


� Targets achieved:

� 0.78 MMO

� Surpassed targets:

1. 9.5% more range: 1,971 nm

2. High speed cruise: 453 kt

3. 15% better takeoff performance

4. 11% better landing performance

5. Improved range from restrictive airports

6. Direct climb to maximum ceiling of 45,000 ft @ MTOW

7. Up to 6.8% better block fuel

8. 5% higher thrust

9. Low external noise levels - 24 EPNdB margin to ICAO stage IV limit

10. Larger total baggage compartment



1. 9.5% more range: 1,971 nm

� CJ3: 1,727 nm(1)

� CJ4: 1,963 nm(2)

2. High speed cruise: 453 kt

� Phenom 300 is faster than CJ3 and CJ4

� CJ3: 417 kt (1)

� CJ4: 451 kt (2)

3. 15% better takeoff performance

� At MTOW, takeoff distance improved from 3,700 ft to 3,138 ft

4. 11% better landing performance

� At MLW(3), landing distance improved from 2,950 ft to 2,621 ft

� For a typical executive mission landing weight(4) the landing distance is 2,252 ft


(1) B&CA May/2009(2) Preliminary data(3) SL, ISA, non-factored(4) SL, ISA, 6 occ@200 lb each, NBAA IFR reserves



5. Improved range from restrictive airports

� TOFL at MTOW/SL/ISA is 3,138 ft

� Overall takeoff performance was improved and provided a greater range from restrictive airports. See examples:

121 %1,906 nm863 nmAngra dos Reis (Brazil)

1,996 nm

2,017 nm

1,985 nm

2,014 nm

1,834 nm

2,011 nm

Certified Performance

9 %

26 %

9 %

13 %

32 %

10 %

Improvement

1,777 nmToluca

1,826 nmRiyadh

1,393 nmTelluride (2)

1,603 nmQuito

1,837 nm

1,825 nm

Initial Estimates

Lanseria (Johannesburg)

Aspen

Range out of (1)

(1) NBAA IFR reserves, LRC, ISA en-route, 6 occ. @ 200 lb each, no winds, takeoff temperature 85% annual reliability; for Toluca it was considered ISA +20ºC(2) Telluride performance does not consider obstacles.


TELLURIDE (KTEX)

Assumptions

� 6 Occupants @ 200lb

� LRC speed

� ISA temperature en route

� 85% annual takeoff temperature

� 85% annual winds

� 3% airways allowance

� NBAA IFR Reserves – 100nm alternate airport, 35min holding at 5,000ft

� FAA Baseline

� No obstacles considered

- Initial estimates

- Certified performance


ANGRA DOS REIS (SDAG)

Assumptions

� 6 Occupants @ 200lb

� LRC speed

� ISA temperature en route

� 85% annual takeoff temperature

� 85% annual winds

� 3% airways allowance

� NBAA IFR Reserves – 100nm alternate airport, 35min holding at 5,000ft

� FAA Baseline

- Initial estimates

- Certified performance



7. Up to 6.8% better block fuel

2,403 lb

1,607 lb

1,025 lb

Certified Phenom 300

6.3 %

6.3 %

6.8 %

Improvement

1,000 nm

600 nm

300 nm

Mission

1,100 lb

1,715 lb

2,564 lb

Initial Estimates

(1) 5 Occupants, ISA, SL, LRC, NBAA IFR Reserves

Phenom 300 Block Fuel for Different Missions(1)

6. Direct climb to maximum ceiling of 45,000 ft @ MTOW

� Phenom 300 time to climb: 25.5 min

� CJ4 time to climb: 28 min


8. 5% higher thrust

� Thrust increased 160 lb, from 3,200 lb to 3,360 lb, keeping block fuel improvements.


5,000

ISA+11

3,400

FJ44-4A

CJ4

3,600

ISA+12

2,965

JT15D-5

HW 400XP

3,500

ISA+13

2,300

FJ44-2A

Premier IA

4,000

ISA+7

2,820

FJ44-3A

CJ3

4,000

ISA+7

2,490

FJ44-3A-24

CJ2+

PW535-EEngine Model

Phenom 300

5,000

ISA+15

3,360

TBO (hours)

Flat rating (°C)

Thrust (lb)



9. Low external noise levels - 24 EPNdB margin to ICAO stage IV limit

65

70

75

80

85

90

Takeoff Sideline Approach

EP

NdB

CJ3 Phenom 300 CJ4 data not available



10. Larger baggage compartment

� Total baggage compartment increased from 76 ft3 to 79 ft3 (4% increase)

� What was considered a best-in-class baggage compartment got even better after certification

78 ft3

CJ4

65 ft3

CJ3

79 ft3Total baggage compartment

Phenom 300

66 ft3 (1,869 ℓ)

463 lb (210 kg)

8 ft3 (230 ℓ)

66 lb (30 kg)

5 ft3 (141 ℓ)


CERTIFIED PERFORMANCE DATA SUMMARY

0.780.78MMO

45,000 ft45,000 ftMaximum Ceiling

79 ft376 ft3Total baggage compartment

3,360 lb3,200 lbEngine Thrust

24 EPNdB below Stage IV

Stage IVExternal noise

ANAC / FAA Certified Phenom 300

Initial estimates

453 kt450 ktHigh Speed Cruise

2,403 lb2,564 lbBlock Fuel for 1,000 nm

3,138 ft3,700 ftTakeoff Distance (3)

2,621 ft2,950 ftLanding Distance(2)

1,971 nm1,800 nmRange with IFR(1) reserves

(1) NBAA IFR reserves (35 min) with 100 nm alternate; 6 occupants @ 200 lb each(2) MLW, SL, ISA (3) MTOW, SL, ISA

All targets achieved or exceeded!THE INFORMATION CONTAINED HEREIN IS SUBJECTED TO THE DISCLAIMER PRESENTED IN THE LAST PAGE OF THIS PRESENTATION.

�

�

�

�

�

�

�

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OPERATIONAL WEIGHTS

THE INFORMATION CONTAINED HEREIN IS SUBJECTED TO THE DISCLAIMER PRESENTED IN THE LAST PAGE OF THIS PRESENTATION.

(1) BOW considering 1 crew (200 lb / 91 kg each)(2) Standard configuration (weights may vary according to optional equipment installed or interior layouts).(3) Adopted fuel density 6.70 lb/US gal (0.803 kg/l).

5181142Available Payload w/ Max Fuel

(kg)(lb)

7,65016,865Maximum Landing

2,4285,353Maximum Usable Fuel (3)

1,0962,416Maximum Payload (2)

5,25411,583Basic Operating (1) (2)

6,35013,999Maximum Zero Fuel

8,15017,968Maximum Takeoff

8,20018,078Maximum Ramp



� All performance figures in this presentation are based on the Basic Operating Weight for Standard FAA equipped aircraft. No options considered, unless otherwise stated.

� BOW may vary according to local regulations requirements and options selected by the client.

� Performance figures for EASA may vary.


COMPETITIVE ANALYSIS


PERFORMANCE COMPARISON vs. CJ3

5ft 1in (1.55m)

4ft 9in(1.45m)

4ft 11in (1.49m)

� Phenom 300 vs. CJ3

4ft 11in(1.50m)

Phenom 300 CJ3

Source: Conklin & de Decker Aircraft Comparator 2009 – Manufacturers’ web sites and promotional material



4,750 ft5,125 ftTakeoff Distance(2) 5,000’ @25ºC

US$ 8,119,000

(E.C. 2009)

US$ 8,140,000

(E.C. 2010)List Price(4)


CJ3 (B&CA 2009)Phenom 300

417 kt453 ktHigh speed cruise


3,180 ft3,138 ftTakeoff Distance(2) SL, ISA

M 0.74M 0.78MMO

1,727 nm1,971 nmRange with IFR(1) reserves

(1) NBAA IFR reserves (35 min) with 100 nm alternate; 6 occupants @ 200 lb each(2) MTOW, SL, ISA(3) MLW, NBAA IFR reserves




CJ4Phenom 300

4ft 9in(1.45m)

5ft 1in (1.55m)

4ft 11in(1.50m)

4ft 10in (1.47m)

� Phenom 300 vs. CJ4

Source: Conklin & de Decker Aircraft Comparator 2009 – Manufacturers’ web sites and promotional material




5,620 ft5,125 ftTakeoff Distance(2) 5,000’ @25ºC

US$ 8,750,000

(E.C. 2009)

US$ 8,140,000

(E.C. 2010)List Price(4)


CJ4 (Preliminary)Phenom 300

451 kt453 ktHigh speed cruise


3,300 ft3,138 ftTakeoff Distance(2) SL, ISA

M 0.77M 0.78MMO

1963 nm1971 nmRange with IFR(1) reserves

(1) NBAA IFR reserves (35 min) with 100 nm alternate; Phenom 300 considers 6 occupants(2) MTOW, SL, ISA(3) MLW, NBAA IFR reserves


OTHER PHENOM 300 ADVANTAGES


It is never too much to remind that the Phenom 300 also delivers:

� Clean sheet design

� Oval Lite cross section concept

� Interior designed in partnership between BMW DesignworksUSA and Embraer

� Most flexible interior among the Light Jets

� Largest windows in class

� Unique Air Stair among the Light Jets

� Largest baggage compartment in class

THE PHENOM 300 ADVANTAGE



� Designed for High Utilization: 35,000 hours. Favors residual value

� New standards for Light Jets in terms of systems:

� Externally serviced lavatory

� Single point refueling

� SmartprobesTM

� Brake-by-wire with carbon breaks

� Bleed anti-ice on horizontal stab (boot free aircraft)

� Central Maintenance Computer

� Synthetic Vision System

� Lower DOC than a Turboprop




� Optional pay by the hour programs. The Embraer Executive Care (EEC) offers:

� Budget planning predictability

� Peace of mind

� Quality Embraer Maintenance

� Aircraft enhanced resale value


●●Access to FlyEmbraer Web Portal

●Bulk Consumables

●Mobile Recovery Service

Provided by P&WC through ESP®Engine Coverage

●

●

●

Standard

●

●

●

●

●

Enhanced

Unscheduled Maintenance Labor

Scheduled Maintenance Labor

Freight and Insurance

Expendable Parts Exchange

Components Exchange

●●Access to FlyEmbraer Web Portal

●Bulk Consumables

●Mobile Recovery Service

Provided by P&WC through ESP®Engine Coverage

●

●

●

Standard

●

●

●

●

●

Enhanced

Unscheduled Maintenance Labor

Scheduled Maintenance Labor

Freight and Insurance

Expendable Parts Exchange

Components Exchange

Subscription to FlyEmbraer “e-Maintenance” package is required – first year included free of charge

Engine coverage level depends on ESP® Program selected

THE INFORMATION HEREIN IS SUBJECT TO THE DISCLAIMER PRESENTED IN THE LAST PAGE OF THIS DOCUMENT. THIS PRESENTATION IS THE PROPERTY OF EMBRAER AND SHALL NOT BE COPIED, OR USED IN ANY MANNER, EXCEPT WITH EMBRAER´S PRIOR WRITTEN CONSENT. THE INFORMATION HEREIN IS SUBJECT TO THE DISCLAIMER PRESENTED IN THE LAST PAGE OF THIS DOCUMENT. THIS PRESENTATION IS THE PROPERTY OF EMBRAER AND SHALL NOT BE COPIED, OR USED IN ANY MANNER, EXCEPT WITH EMBRAER´S PRIOR WRITTEN CONSENT.

schedule for EIS on 4Q 2009!Phenom 300 now joins the Phenom 100 fleet!



Thank You!

Embraer reserves the right to revise this document whenever occasioned by product improvements, governmental regulations or other good cause.

All figures, finishing materials and colors are for illustration purpose only, and may not represent the real and final product accurately.

Some features are optional items not included in the baseline aircraft and are subject to price increase and lead-time analysis.

ALL DATA PRESENTED SHALL NOT BE USED AS GUARANTEE. GUARANTEED SPECIFICATIONS ARE LISTED IN CHAPTER 1 – SECTION 5 OF THE PRELIMINARY TECHNICAL DESCRIPTION AND REPRESENT THE ONLY BINDING GUARANTEE.

In the event of any conflict between this presentation and the Embraer Phenom 300 preliminary technical description, the preliminary technical description shall govern. The information contained herein is the property of Embraer S.A. and it shall not be copied, in whole or in part, or used in any manner except with Embraer’s written consent.

phenom 300 type certificate - embraer jet /...

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