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FALCON 900 AIRPLANE CHARACTERISTICSFOR AIRPORT PLANNINGFalcon 900 A / B / CFalcon 900EXFalcon 900EX EASyFalcon 900DXFalcon 900LXOriginal Issue - July 2006Revision 5 - Dec 2010Rev 5 - Dec 2010Pub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

TABLE OF CONTENTSTABLE OF CONTENTS . 21. PURPOSE . 32. AIRCRAFT CHARACTERISTICS - F900 ALL MODELS . 32.1 COMMON CHARACTERISTICS - F900 ALL MODELS . 33. PHYSICAL DESCRIPTION - F900 ALL MODELS . 53.1 WEIGHT AND LOADING . 53.2 DIMENSIONS. 73.2.1 F900 A / B / C / EX / EX EASy / DX . 73.2.2 F900LX . 83.3 MINIMUM TURN RADIUS . 93.3.1 F900A / B / C / EX / EX EASy / DX . 93.3.2 F900LX . 103.4 TIRE PRESSURE - F900 ALL MODELS . 104. PERFORMANCE - F900 ALL MODELS . 114.1 AIRPLANE CLASSIFICATION NUMBER (ACN) VALUES - FALCON 900A, B AND C . 114.2 AIRPLANE CLASSIFICATION NUMBER (ACN) VALUES - FALCON 900EX, EX EASY, DX, AND LX. 124.2 AIRPLANE CLASSIFICATION NUMBER (ACN) VALUES - FALCON 900EX, EX EASY, DX AND LX (CON'D) . 134.3 TAKEOFF - FALCON 900A. 144.4 TAKE-OFF - FALCON 900B AND C . 154.5 TAKE-OFF - FALCON 900EX, EX EASY, DX AND LX . 164.5 TAKE-OFF - FALCON 900EX, EX EASY, DX AND LX (CON'D) . 174.5 TAKE-OFF - FALCON 900EX, EX EASY, DX AND LX (CON'D) . 184.6 LANDING - F900 ALL MODELS . 194.6.1 Landing distance - F900 All models. 194.6.2 Approach speed - F900 All models . 204.7 NOISE - F900 ALL MODELS . 214.7.1 FALCON 900A . 214.7.2 FALCON 900B and C . 214.7.3 FALCON 900EX and EX EASy . 214.7.4 FALCON 900DX . 214.7.5 FALCON 900LX . 225. CRASH INFORMATION - F900 ALL MODELS . 236. HANDLING - F900 ALL MODELS. 23Rev 5 - Dec 2010Pub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

1. PURPOSEThis document provides, in a short manner, airplane characteristics data for general airportplanning.CautionThe information provided hereafter is for advisory purpose only and must not supersedeDassault official documentation (Airplane Flight Manual, Operating Manual, GroundServicing Manual) for any operational purpose.2. AIRCRAFT CHARACTERISTICS - F900 All modelsThe FALCON 900 is a long-range wide body business trijet airplane, with the capability to operateto or from less than 1,200 meters (4,000 ft) long runways.- Maximum airport pressure altitude: from – 1,000 to 14,000 ft.- Runway slope: from – 2.5% to 2.5%.- Maximum range: from 3,600 NM to 4,750 NM, according to the type.- Maximum tailwind component for takeoff and landing: 10 kt.- Maximum demonstrated crosswind component: 30 kt.The airplane is certified for CAT II operations. F900EX series are optionally certified for CAT IIIoperations.NOTE : For FALCON 900LX, HUD CAT III capability is not yet available.The family:FALCON 900A: initial version,FALCON 900B: higher performance due to upgraded engines,FALCON 900C: 900B upgraded with new avionics,FALCON 900EX: 900B upgraded with new avionics, and fitted with new engines and improvedfuel capacity,FALCON 900EX EASy: 900EX equipped with the new “Enhanced Avionics System”,FALCON 900DX: 900EX EASy with reduced fuel capacity,FALCON 900LX: 900EX EASy with installation of winglets (modification M5281).NOTE : Only the FALCON 900LX is still in production.2.1 Common characteristics - F900 All modelsThe main entry door also serves as an access stairway: the airplane is self-sufficient forpassenger boarding.The built-in auxiliary power unit (APU) provides, on ground only, the air conditioning, the electricalpower generation and the assistance for engines start.Rev 5 - Dec 2010Pub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

The airplane may be pressure- or gravity-refueled or defueled.The use of thrust reverser is approved for airplane back moving.All usual ground servicing operations are performed without any specific equipment.According to ICAO annex 14, the airplane is classified Rescue and Fire Fighting category 4.According to ICAO annex 14, Volume I, Chapter 3, the reference code of the Falcon 900 airplanesis 3B which corresponds to a minimum runway width of 30.0 m (98 ft).Minimum flight crew: 2 pilots.Rev 5 - Dec 2010Pub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

3. PHYSICAL DESCRIPTION - F900 All models3.1 Weight and loadingF900A, B and CF900A, B and CWithout SB 139With SB 139Maximum Ramp Weight20,730 KgMaximum Takeoff WeightKgF900EXF900EXEASyF900DXF900LX21,183 Kg22,317 Kg22,317 Kg21,274 Kg22,317 Kg20,639 Kg21,092 Kg22,226 Kg22,226 Kg21,183 Kg22,226 KgMaximum LandingWeight19,051 Kg19,051 Kg20,185 Kg20,185 Kg19,142 Kg20,185 KgMaximum Zero FuelWeight12,800 Kg14,000 Kg14,000 Kg14,000 Kg14,000 Kg14,000 KgFuel Capacity8,647.5 Kg8,647.5 Kg9,526 Kg9,526 Kg8,545 Kg9,483 Kg14% to 31% MAC14% to 31% MAC13% to 31% MAC13% to 31% MAC13% to 31% MAC13% to 31%MAC*Center of Gravity Limits*cf. specific F900LX Center of Gravity Limits in the last revision of flight documentation.Rev 5 - Dec 2010Pub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

F900A, B and CF900A, B and CWithout SB 139With SB 139Maximum Ramp Weight45,700 lbMaximum Takeoff WeightlbF900EXF900EXEASyF900DXF900LX46,700 lb49,200 lb49,200 lb46,900 lb49,200 lb45,500 lb46,500 lb49,000 lb49,000 lb46,700 lb49,000 lbMaximum LandingWeight42,000 lb42,000 lb44,500 lb44,500 lb42,200 lb44,500 lbMaximum Zero FuelWeight28,220 lb30,870 lb30,864 lb30,864 lb30,864 lb30,864 lbFuel Capacity19,065 lb19,065 lb21,000 lb21,000 lb18,830 lb20,907 lb14% to 31% MAC14% to 31% MAC13% to 31% MAC13% to 31% MAC13% to 31% MAC13% to 31% MAC*Center of Gravity Limits*cf. specific F900LX Center of Gravity Limits in the last revision of flight documentation.Loading - F900 All modelsMaximum passenger19Maximum cargo in baggage compartment2,866 lbRev 5 - Dec 20101,300 KgPub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

3.2 Dimensions3.2.1 F900 A / B / C / EX / EX EASy / DXRev 5 - Dec 2010Pub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

3.2.2 F900LXRev 5 - Dec 2010Pub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

3.3 Minimum turn radius3.3.1 F900A / B / C / EX / EX EASy / DXSteering uncoupled(towing)Steering coupledA : r 10.2 m / 33.4 ftB : r 14.5 m / 47.6 ftC : 4.6 m / 15 ftNOTE: The towing bar is specific to the airplane. Towing with a towbarless vehicle is approvedprovided the appropriate interface tool is used.Rev 5 - Dec 2010Pub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

3.3.2 F900LX3.4 Tire Pressure - F900 All modelsMain gearNose gearFalcon 900A, B, C13.3 bars / 193 psi10.2 bars / 148 psiFalcon 900EX, EX EASy, DX, LX13.8 bars / 200 psi10.4 bars / 151 psiRev 5 - Dec 2010Pub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

4. PERFORMANCE - F900 All models4.1 Airplane Classification Number (ACN) values - FALCON 900A,B and CRev 5 - Dec 2010Pub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

4.2 Airplane Classification Number (ACN) values - FALCON900EX, EX EASy, DX, and LXRev 5 - Dec 2010Pub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

4.2 Airplane Classification Number (ACN) values - FALCON900EX, EX EASy, DX and LX (Con'd)Rev 5 - Dec 2010Pub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

4.3 Takeoff - FALCON 900ARev 5 - Dec 2010Pub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

4.4 Take-off - FALCON 900B and CRev 5 - Dec 2010Pub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

4.5 Take-off - FALCON 900EX, EX EASy, DX and LXRev 5 - Dec 2010Pub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

4.5 Take-off - FALCON 900EX, EX EASy, DX and LX (Con'd)Rev 5 - Dec 2010Pub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

4.5 Take-off - FALCON 900EX, EX EASy, DX and LX (Con'd)Rev 5 - Dec 2010Pub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

4.6 LANDING - F900 All models4.6.1 Landing distance - F900 All modelsRev 5 - Dec 2010Pub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

4.6.2 Approach speed - F900 All modelsRev 5 - Dec 2010Pub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

4.7 Noise - F900 All models4.7.1 FALCON 900AReference pointNoise levelsNoise limits(EPNdB)(EPNdB)81.989.591.7899498Noise levelsNoise limits(EPNdB)(EPNdB)79.891.291.7899498Noise levelsNoise limits(EPNdB)(EPNdB)79.890.592.3899498Noise levelsNoise alApproach4.7.2 FALCON 900B and CReference pointFlyoverLateralApproach4.7.3 FALCON 900EX and EX EASyReference pointFlyoverLateralApproach4.7.4 FALCON 900DXReference pointFlyoverLateralApproachRev 5 - Dec 2010Pub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

4.7.5 FALCON 900LXReference pointFlyoverLateralApproachRev 5 - Dec 2010Noise levelsNoise limits(EPNdB)(EPNdB)78.290.392.1899498Pub 926This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.