PHENOM 300 TYPE CERTIFICATE

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1 PHENOM 300 TYPE CERTIFICATE

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

3 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

4 DEVELOPMENT HIGHLIGHTS Phenom 300 First Flight April 2008

5 DEVELOPMENT HIGHLIGHTS Cold Soak Test at Eglin Air Force Base

6 DEVELOPMENT HIGHLIGHTS Water spray test at Embraer Gavião Peixoto facility

7 DEVELOPMENT HIGHLIGHTS Flying into known icing campaign

8 DEVELOPMENT HIGHLIGHTS Structural tests: Bird strike tests Wing ultimate loads tests Fatigue tests

9 DEVELOPMENT HIGHLIGHTS Cold weather and crosswind tests

10 SURPASSING EXPECTATIONS

11 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

12 SURPASSING EXPECTATIONS Targets achieved: 0.78 MMO Surpassed targets: % 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 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

13 SURPASSING EXPECTATIONS % 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 lb each, NBAA IFR reserves

14 SURPASSING EXPECTATIONS 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: Range out of (1) Initial Estimates Certified Performance Improvement Aspen 1,825 nm 2,011 nm 10 % Telluride (2) 1,393 nm 1,834 nm 32 % Toluca 1,777 nm 2,014 nm 13 % Riyadh 1,826 nm 1,985 nm 9 % Quito 1,603 nm 2,017 nm 26 % Angra dos Reis (Brazil) 863 nm 1,906 nm 121 % Lanseria (Johannesburg) 1,837 nm 1,996 nm 9 % (1) NBAA IFR reserves, LRC, ISA en-route, lb each, no winds, takeoff temperature 85% annual reliability; for Toluca it was considered ISA +20ºC (2) Telluride performance does not consider obstacles.

15 TELLURIDE (KTEX) - Initial estimates - Certified performance Assumptions 6 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

16 ANGRA DOS REIS (SDAG) - Initial estimates - Certified performance Assumptions 6 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

17 SURPASSING EXPECTATIONS 6. Direct climb to maximum ceiling of 45,000 MTOW Phenom 300 time to climb: 25.5 min CJ4 time to climb: 28 min 7. Up to 6.8% better block fuel Phenom 300 Block Fuel for Different Missions (1) Mission Initial Estimates Certified Phenom 300 Improvement 300 nm 1,100 lb 1,025 lb 6.8 % 600 nm 1,715 lb 1,607 lb 6.3 % 1,000 nm 2,564 lb 2,403 lb 6.3 % (1) 5 Occupants, ISA, SL, LRC, NBAA IFR Reserves

18 SURPASSING EXPECTATIONS 8. 5% higher thrust Thrust increased 160 lb, from 3,200 lb to 3,360 lb, keeping block fuel improvements. Phenom 300 CJ2+ CJ3 CJ4 Premier IA HW 400XP Engine Model PW535-E FJ44-3A-24 FJ44-3A FJ44-4A FJ44-2A JT15D-5 Thrust (lb) 3,360 2,490 2,820 3,400 2,300 2,965 Flat rating ( C) ISA+15 ISA+7 ISA+7 ISA+11 ISA+13 ISA+12 TBO (hours) 5,000 4,000 4,000 5,000 3,500 3,600

19 SURPASSING EXPECTATIONS 9. Low external noise levels - 24 EPNdB margin to ICAO stage IV limit EPNdB Takeoff Sideline Approach CJ3 Phenom 300 CJ4 data not available

20 SURPASSING EXPECTATIONS 10. Larger baggage compartment Total baggage compartment increased from 76 ft 3 to 79 ft 3 (4% increase) What was considered a best-in-class baggage compartment got even better after certification Phenom 300 CJ3 CJ4 Total baggage compartment 79 ft 3 65 ft 3 78 ft 3 8 ft 3 (230 l) 5 ft 3 (141 l) 66 ft 3 (1,869 l) 66 lb (30 kg) 463 lb (210 kg)

21 CERTIFIED PERFORMANCE DATA SUMMARY Range with IFR (1) reserves MMO Maximum Ceiling High Speed Cruise Landing Distance (2) Takeoff Distance (3) Engine Thrust Block Fuel for 1,000 nm External noise Total baggage compartment Initial estimates 1,800 nm ,000 ft 450 kt 2,950 ft 3,700 ft 3,200 lb 2,564 lb Stage IV 76 ft 3 ANAC / FAA Certified Phenom 300 1,971 nm ,000 ft 453 kt 2,621 ft 3,138 ft 3,360 lb 2,403 lb 24 EPNdB below Stage IV 79 ft 3 (1) NBAA IFR reserves (35 min) with 100 nm alternate; lb each (2) MLW, SL, ISA (3) MTOW, SL, ISA All targets achieved or exceeded! THE INFORMATION HEREIN IS SUBJECT TO THE DISCLAIMER PRESENTED 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 CONTAINED HEREIN IS SUBJECTED TO THE DISCLAIMER PRESENTED IN THE LAST PAGE OF THIS PRESENTATION.

22 OPERATIONAL WEIGHTS (lb) (kg) Maximum Ramp 18,078 8,200 Maximum Takeoff 17,968 8,150 Maximum Landing 16,865 7,650 Maximum Zero Fuel 13,999 6,350 Basic Operating (1) (2) 11,583 5,254 Available Payload w/ Max Fuel Maximum Payload (2) 2,416 1,096 Maximum Usable Fuel (3) 5,353 2,428 ( 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). THE INFORMATION HEREIN IS SUBJECT TO THE DISCLAIMER PRESENTED 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 CONTAINED HEREIN IS SUBJECTED TO THE DISCLAIMER PRESENTED IN THE LAST PAGE OF THIS PRESENTATION.

23 SURPASSING EXPECTATIONS 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.

24 COMPETITIVE ANALYSIS

25 PERFORMANCE COMPARISON vs. CJ3 Phenom 300 vs. CJ3 4ft 9in (1.45m) 4ft 11in (1.50m) Phenom 300 CJ3 4ft 11in (1.49m) 5ft 1in (1.55m) Source: Conklin & de Decker Aircraft Comparator 2009 Manufacturers web sites and promotional material

26 PERFORMANCE COMPARISON vs. CJ3 Range with IFR (1) reserves High speed cruise MMO Takeoff Distance (2) SL, ISA Takeoff Distance (2) Landing Distance (3) Maximum Ceiling Engine Thrust List Price (4) Phenom 300 1,971 nm 453 kt M ,138 ft 5,125 ft 2,621 ft 45,000 ft 3,360 lb US$ 8,140,000 (E.C. 2010) CJ3 (B&CA 2009) 1,727 nm 417 kt M ,180 ft 4,750 ft 2,770 ft 45,000 ft 2,820 lb US$ 8,119,000 (E.C. 2009) (1) NBAA IFR reserves (35 min) with 100 nm alternate; lb each (2) MTOW, SL, ISA (3) MLW, NBAA IFR reserves

27 PERFORMANCE COMPARISON vs. CJ4 Phenom 300 vs. CJ4 4ft 9in (1.45m) 4ft 11in (1.50m) Phenom 300 CJ4 4ft 10in (1.47m) 5ft 1in (1.55m) Source: Conklin & de Decker Aircraft Comparator 2009 Manufacturers web sites and promotional material

28 PERFORMANCE COMPARISON vs. CJ4 Range with IFR (1) reserves High speed cruise MMO Takeoff Distance (2) SL, ISA Takeoff Distance (2) Landing Distance (3) Maximum Ceiling Engine Thrust List Price (4) Phenom nm 453 kt M ,138 ft 5,125 ft 2,621 ft 45,000 ft 3,360 lb US$ 8,140,000 (E.C. 2010) CJ4 (Preliminary) 1963 nm 451 kt M ,300 ft 5,620 ft 2,665 ft 45,000 ft 3,400 lb US$ 8,750,000 (E.C. 2009) (1) NBAA IFR reserves (35 min) with 100 nm alternate; Phenom 300 considers 6 occupants (2) MTOW, SL, ISA (3) MLW, NBAA IFR reserves

29 OTHER PHENOM 300 ADVANTAGES

30 THE PHENOM 300 ADVANTAGE 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

31 THE PHENOM 300 ADVANTAGE It is never too much to remind that the Phenom 300 also delivers: 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 Smartprobes TM 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

32 THE PHENOM 300 ADVANTAGE It is never too much to remind that the Phenom 300 also delivers: 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 Components Exchange Expendable Parts Exchange Freight and Insurance Access to FlyEmbraer Web Portal Scheduled Maintenance Labor Unscheduled Maintenance Labor Bulk Consumables Mobile Recovery Service Standard Enhanced Engine Coverage Provided by P&WC through ESP Subscription to FlyEmbraer e-maintenance package is required first year included free of charge Engine coverage level depends on ESP Program selected

33 THE PHENOM 300 ADVANTAGE Phenom 300 schedule now joins for EIS the on Phenom 4Q 2009! 100 fleet! THE INFORMATION HEREIN IS IS SUBJECT TO TO THE DISCLAIMER PRESENTED IN IN THE LAST PAGE OF OF THIS DOCUMENT. THIS PRESENTATION IS IS THE PROPERTY OF OF EMBRAER AND SHALL NOT BE BE COPIED, OR OR USED IN IN ANY MANNER, EXCEPT WITH EMBRAER S PRIOR WRITTEN CONSENT.

34 Thank You!

35 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.

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