# TCDS A46EU: Dassault Aviation - Type: Type certificate data sheet - Status: Current - Holder: Dassault Aviation - Revision: 24 - Revised: September 25, 2026 - Product: Aircraft, Large Airplane - Certification basis: Part 25, Part 21 - Registered aircraft: 484, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/dd/35/dd3574df40bb531df224dce822c7eca3839e1fedd21f8c7f3e4bf7e7efc90b05 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131757747520261005154406.0001 - Page: https://openairdocs.org/tcds/A46EU ## Models (3) As the data sheet lists them. - Mystere-Falcon 900 - Falcon 900EX - Mystere-Falcon 50 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 Rev. No. 23 8 10 13 13 24 9 10 10 12 9 10 22 22 14 20 24 20 Page No. 19 20 21 22 23 24 Rev. No. 21 23 23 22 22 22 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A46EU Revision 24 DASSAULT AVIATION MYSTERE-FALCON 50 MYSTERE-FALCON 900 FALCON 900EX September 5, 2026 TYPE CERTIFICATE DATA SHEET No. A46EU This data sheet which is part of Type Certificate No. A46EU prescribes conditions and limitations under which the product for which the Type Certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder. DASSAULT AVIATION (See NOTE 8) 9 Rond Point des Champs Elysees 75008 Paris France The U.S. airworthiness certification basis for aircraft type certificated under FAR Section 21.29 and exported by the country of manufacture is FAR Sections 21.183(c) or 21.185(c). The U.S. airworthiness certification basis for aircraft type certificated under FAR Section 21.29 exported from countries other than the country of manufacture (e.g. third party country) is FAR 21.183(d) or 21.185(b). Notwithstanding that the FAR referenced in the above paragraph does not specifically address or require a foreign civil airworthiness authority certification, such certification is the only practical way for an applicant to show, and the Federal Aviation Administration (FAA) to find conformity to the FAA -approved type design and conditions for safe operation. Additional guidance is contained in FAA Advisory Circular 21-23, Airworthiness Certification of Civil Aircraft, Engines, Propellers, and Related Products Imported into the United States. I. Model MYSTERE-FALCON 50 (Transport Category Airplane), approved March 7, 1979. (a) Basic Model Definition Engines. 3 engines - Allied Signal Engines, Model TFE 731-3-1C (see Note 3b). Engine Limits. Static, Standard Sea level Takeoff (5 min) lb 3,700 Maximum Continuous lb 3,700 Maximum normal operating rotor speeds Low pressure rotor (N1) RPM 21,000 percent 101.5% High pressure rotor (N2) RPM 29,692 percent 100% Transient Conditions* 1 Minute 5 Seconds Low pressure rotor (N1) 101.5% to 103% 103% to 105% High pressure rotor (N2) 100% to 103% 103% to 105% *(See NOTE 7) Interstage turbine temperature (ITT): During starting 907ºC (1,665ºF) A46EU 2 of 24 Rev. 24 Starting (10 sec. transient) 927ºC (1,700ºF)* Takeoff (5 minutes) 907ºC (1,665ºF) Takeoff (10 sec. transient) 939ºC (1,722ºF) Maximum Continuous 885ºC (1,625ºF) *(See NOTE 7) Oil temperature at fan gearbox inlet: Maximum (sea level to 30,000 ft) 127ºC (260ºF) Maximum (above 30,000 ft) 140ºC (284ºF) Maximum (2 minutes transient) 149ºC (300ºF) Minimum Continuous 30ºC ( 86ºF) Fuel Pressure Minimum fuel pressure warning, psig 4.5 Oil pressure limits: At idle, psig 25 to 46 Takeoff & maximum continuous, psig 38 to 46 APU (optional). Allied Signal Engines GTCP 36-100(A) (See NOTE 6) Limitation - Not operable in flight RATED MAX. ALLOWABLE EGT 680ºC 732ºC RP 100% 109% Fuel: See NOTE 4, and Airplane Flight Manual Oil: See NOTE 5b, and GTCP 36-100 Maintenance Manual. Airspeed Limits (IAS). Unless otherwise indicated, speeds are indicated airspeeds. VMO (Maximum Operating) 350 kts at sea level, 370 kts at 10,000 ft., with straight line variation between those points. 370 kts from 10,000 ft to 24,000 ft. MMO (Maximum Operating) M = 0.86 above 24,000 ft. VA (Maneuvering) 210 kts VFE (Slat and Flap Speeds) Slats 200 kts Slats + flaps 20º 190 kts Slats + flaps 48º 175 kts VLO (Landing Gear Operation) 190 kts MLO 0.70 VLE (Landing Gear Extended) 220 kts MLE 0.75 Windshield Wiper Operation 205 kts Cockpit Window Opening 180 kts VMC (Minimum Control Speed) In flight 82.5 kts (CAS) On ground 87.5 kts (CAS) C.G. Range. Weight (lb) Forward Limit (% MAC) Aft Limit (% MAC) (Gear Extended) 38,800 22.3 32 35,715 19.8 32 30,203 14 32 18,959 14 32 For aircraft incorporating AMD-BA Modification 1230 (Falcon 50 Service Bulletin Number 161), C.G. Range is modified as follows: Weight (lb) Forward Limit (% MAC) Aft Limit (% MAC) A46EU 3 of 24 Rev. 24 40,780 23.3 29.6 40,255 22.8 32 35,715 19.2 32 30,640 14 32 18,959 14 32 For aircraft incorporating AMD-BA Modification 1430 (Falcon 50 Service Bulletin Number 191), C.G. Range is modified as follows: Weight (lb) Forward Limit (% MAC) Aft Limit (% MAC) 40,780 20.9 29.6 40,255 20.6 32.0 35,715 17.3 32.0 32,624 14.0 32.0 18,959 14.0 32.0 Gear retraction has negligible effect on C.G. Range. Datum. Datum is 25% of mean aerodynamic chord (MAC) which is marked on aircraft and coincides with fuselage Station (FS) + 382.83 inches. (Fuselage Station + 0 is the forward end of the aircraft nose cone). Mean Aerodynamic Chord. Length 111.77 in. Zero % MAC is at FS + 354.89 in. Leveling Means. A bubble-type level, when placed on a special leveling rule which in turn is placed on the tops of 3 specific leveling pins on the floor of the fuselage rear compartment, facilitates leveling of the airplane in the longitudinal and lateral directions. Weight Limitations. Maximum Weights Maximum ramp 38,800 lb. Maximum takeoff (brake release) 38,800 lb. Maximum landing 35,715 lb. Maximum zero fuel 25,570 lb. Minimum weight 18,959 lb. For aircraft incorporating AMD-BA Modification 1230 or modification 1430 (Falcon 50 Service Bulletin Number 161 or 191), weight limitations are modified as follows: Maximum ramp 40,780 lb. Maximum takeoff (brake release) 40,780 lb. Maximum landing 35,715 lb. Maximum zero fuel 25,570 lb. Minimum weight 18,959 lb. Maximum Passengers. 19 maximum - limited by emergency exit requirement of FAR 25.807(c) (AMD memo DTM 800 identifies approved cabin interior for 8 or 9 passenger seats). 12 maximum - limited by cabin air ventilation requirements of FAR 25.831 when operated above 45,000 feet (AMD Falcon 50 Service Bulletin No. F50-0163 is applied (or AMD Mod. M17). 0 - Without passenger provision but incorporating Dassault Ferry flight configuration : M2133. Crew Seats. Third crew seat, installed in accordance with Option No. 25-11-02, may be occupied for takeoff and landing. Maximum Baggage. 2,200 lb in rear baggage compartment. Fuel Capacity. Nominal - (refer to weight and balance report of each individual airplane for exact capacity). A46EU 4 of 24 Rev. 24 Usable Fuel US Gallons Pounds Arm (in) Left wing 559 3,748 -0.94 Center wing 410 2,749 -38.82 Right wing 559 3,748 -0.94 Left fuselage 210 1,404 +51.3 Center fuselage 367 2,461 +51.85 Right fuselage 210 1,404 +51.3 TOTAL USABLE 2,315 15,514 TOTAL FUEL 2,329 15,607 Pressure Fueling 50 psi maximum. Oil Capacity. Usable, 0.5 US Gallons (Each Engine) Unusable, 2.25 US Gallons (drainable, and trapped oil) side engine arm + 80.9 in., center engine arm + 225.8 in. Maximum Operating Altitude. 45,000 ft. 49,000 ft. for serial No. 156 and on, or for aircraft incorporating AMD-BA Modification M17 (Falcon 50 Service Bulletin Number F50-0163). Control Surface Movements. Elevator: Down 16º Up 20º (Control stops) Rudder: Right 23º Left 23º Aileron: Up 25º20' Down 24º50' Flaps: Down 48º Airbrakes: Up 68º Wing Slats: internal 20º external 30º Stabilizer: Electrical stops: Nose down 1º Nose up 11º Mechanical stops:Nose down (max) 1º30' Nose up (max) 11º30' Structural stops: Nose down (min) 2º Nose up (min) 12º Rigging tolerances are included in Maintenance Manual. (b) Falcon 50EX Definition EX designation for Mystère Falcon 50 does not correspond to a model designation. This is only a commercial designation for airplanes on which 6 Major modifications are embodied. Those 6 modifications, listed below, are basic on any aircraft from serial number 253 and subsequent. M1200: Increase of rudder control authority M1810: new engines - assembly line configuration - TFE 731-40 M1890: new avionics M1939: new engine control EIED M1940: Bleed Air System Computer M2159: ADC new calibration The following associated retrofit modifications are available: M2017: New engines – retrofit – TFE 731-40-1C M1924: New avionics – retrofit Other modifications, as retrofit, have the same modification numbers as for new build aircraft. Engines. 3 engines - Allied Signal Engines, Model TFE 731-40 (FAA Data Sheet EINM-1 July 13, 1995) Engine Limits. Static, Standard Sea level Takeoff (5 min) lb 3,700 Maximum Continuous lb 3,700 A46EU 5 of 24 Rev. 24 Maximum normal operating rotor speeds Low pressure rotor (N1) RPM 21,021 percent 100.1% High pressure rotor (N2) RPM 31,485 percent 101% Transient Conditions* 5 Seconds Low pressure rotor (N1) 100.5% High pressure rotor (N2) 102.5 *(See NOTE 7) Interstage turbine temperature (ITT): During starting 991ºC (1,815ºF) Takeoff (5 minutes) 1013ºC (1,855ºF) Maximum Continuous 991ºC (1,815ºF) Oil temperature at fan gearbox inlet: Maximum (sea level to 30,000 ft) 127ºC (261ºF) Maximum (above 30,000 ft) 140ºC (284ºF) Maximum (2 minutes transient) 149ºC (300ºF) Minimum Continuous 40ºC ( 104ºF) Fuel Pressure Minimum fuel pressure warning, psig 4.5 Oil pressure limits: At idle, psig 50 to 80 Takeoff & maximum continuous, psig 65 to 80 APU (basic). Unchanged. Included as basic equipment on serial number 253 and subsequent. Airspeed Limits (IAS). Unchanged C.G. Range. Weight (lb) Forward Limit (% MAC) Aft Limit (% MAC) (Gear Extended) 39,700 22.96 32 30,179 14 32 18,959 14 32 After incorporation of Falcon 50 Service Bulletin Number 161, C.G. Range is modified as follows: Weight (lb) Forward Limit (% MAC) Aft Limit (% MAC) (Gear Extended) 40,785 23.3 29.57 40,300 22.99 32 30,618 14 32 18,959 14 32 Datum. Unchanged Mean Aerodynamic Chord. Unchanged Leveling Means. Unchanged Weight Limitations. Maximum Weights Maximum ramp 39,700 lb. Maximum takeoff (brake release) 39,700 lb. Weight Limitation (cont’d) Maximum landing 35,715 lb.(unchanged) Maximum zero fuel 25,570 lb.(unchanged) Minimum weight 18,959 lb.(unchanged) After incorporation of Falcon 50 Service Bulletin Number 161, weight limitations are modified as follows: Maximum ramp 40,785 lb.(unchanged) A46EU 6 of 24 Rev. 24 Maximum takeoff (brake release) 40,785 lb.(unchanged) Maximum landing 35,715 lb. (unchanged) Maximum zero fuel 25,570 lb. (unchanged) Minimum weight 18,959 lb. (unchanged) Maximum Passengers. Unchanged, except Ferry kit definition and installation (0 passenger provisions) is covered by Dassault modification M2133 Crew Seats. Unchanged Maximum Baggage. Unchanged Fuel Capacity. Unchanged Oil Capacity. Usable, 1.01 US Gallons (Each Engine) Unusable, 0.31 US Gallons Maximum Operating Altitude. Unchanged Control Surface Movements. Unchanged ,except Rudder (M1200): Right 29º Left 29º II. Model MYSTERE-FALCON 900 (Transport Category Airplane), approved March 21, 1986. (a) Basic Model Definition Engines. 3 engines - Allied Signal Engines, Model TFE 731-5AR-1C (See NOTE 3b). MF900 aircraft incorporating M1200 and M1548 (Service Bulletin F900-100) are equipped with 3 engines Allied Signal Engines, Model TFE 731-5BR-1C. Commercial name of Myatere-Falcon 900 airplanses fitted with M1200 and M1548 modificatiions is F900B. Engine Limits. A/C without SB100 A/C with SB100 Static, Standard Sea Level Takeoff (5 min.) lb 4,500 lb 4,750 Maximum continuous lb 4,500 lb 4,634 Maximum normal operating rotor speeds Low pressure rotor (N1) RPM 21,000 RPM 100% High pressure rotor (N2) RPM 29,989 RPM 101% 30,540 RPM 100.8% Transient Conditions* 5 seconds Low pressure rotor (N1) 100% to 103% High pressure rotor (N2) 101% to 103% 100.8% to 103% * (See NOTE 7) A46EU 7 of 24 Rev. 24 Interstage turbine temperature (ITT): During starting 952ºC (1,746ºF) 978ºC (1,793ºF) Starting (10 sec. transient) 974ºC (1,785ºF)* 996ºC (1,825ºF) Takeoff (5 minutes) 974ºC (1,785ºF) 996ºC (1,825ºF) (5 sec. transient) 984ºC (1,803ºF) 1006ºC (1,842ºF) (2 sec. transient) 994ºC (1,821ºF) 1016ºC (1,861ºF) Maximum continuous 924ºC (1,696ºF) 968ºC (1,775ºF) * (See NOTE 7) Oil temperature at fan gearbox inlet: Maximum (sea level to 30,000 ft) 127ºC (260ºF) Maximum (Above 30,000 ft) 140ºC (284ºF) Maximum transient (2 minutes) 149ºC (300ºF) Minimum Continuous 30ºC ( 86ºF) Fuel pressure: Minimum fuel pressure warning psig 4.5 Oil pressure limits: At idle, psig psig 25 to 46 Takeoff and maximum continuous psig 38 to 46 APU. Allied Signal Engines Model GTCP 36-150(F) Limitation - Not operable in flight RATED MAX. ALLOWABLE EGT 720ºC 973ºC RPM 102% 110% Fuel : See NOTE 4, and Airplane Flight Manual Oil : See NOTE 5b. Airspeed Limits. Unless otherwise indicated, speeds are indicated airspeeds. VMO (Maximum Operating) 350 kts at sea level; 370 kts at 10,000 ft., with straight line variation between those points. 370 kts from 10,000 ft to 25,000 ft. MMO (Maximum Operating) - Weight below 35,000 lbs. M = 0.87 from 25,000 ft. to 38,000 ft. 0.87 at 38,000 ft. to 0.84 at 42,000 ft., with straight line variation between other points. 0.84 above 42,000 ft. - Weight above 35,000 lbs. M = 0.87 from 25,000 ft. to 33,000 ft. 0.87 at 33,000 ft. to 0.84 at 37,000 ft. with straight line variations between those points. 0.84 above 37,000 ft. A46EU 8 of 24 Rev. 24 Aircraft Aircraft Without SB100 With SB100 VA (Maneuvering) VFE (Slat and Flap Speeds) Flaps 7º + Slats Flaps 20º + Slats Flaps 40º + Slats VLO (Landing Gear Operation) MLO VLE (Landing Gear Extended) MLE Windshield Wiper Operation Cockpit Window Opening VMC (Minimum Control Speed) In flight On ground 228 kts 200 kts 190 kts 180 kts 190 kts 0.70 245 kts 0.75 215 kts 215 kts 83 kts (CAS) 85.3 kts (CAS) 83.6 kts (CAS) 86 kts (CAS) C.G. Range. Weight (lb) Forward Limit (% MAC) Aft (Gear Extended) 45,500 14 31 42,000 14 31 20,700 14 31 For aircraft incorporating Modification 1196, C.G. range is modified as follows: Weight (lb) Forward Limit (% MAC) Aft Limit (% MAC) 20,700 14 31 42,000 14 31 46,500 14 31 Gear retraction has negligible effect on C.G. Range. Datum. Datum is 25% of mean aerodynamic chord (MAC) which is marked on aircraft and coincides with fuselage Station (FS) + 420.43 inches. (Fuselage Station + 0 is the forward end of the aircraft nose cone). Datum is marked on fuselage of A/C S/N's 1 through 11 only. Mean Aerodynamic Chord. Length 113.69 in. Zero % MAC is at FS + 392 in. Leveling Means. Standard bubble-type level to be installed on the passengers seats tracks. Weight Limitations. Maximum Weights Maximum ramp 45,700 lb Maximum takeoff (brake release) 45,500 lb Maximum landing 42,000 lb Maximum zero fuel 28,220 lb Minimum weight 20,700 lb For aircraft incorporating DASSAULT Modification 1196, Weight limitations are modified as follows: Maximum ramp 46,700 lb Maximum takeoff 46,500 lb Maximum landing 42,000 lb Maximum zero fuel 30,865 lb Minimum weight 20,700 lb A46EU 9 of 24 Rev. 24 Maximum Passengers. 19 maximum - limited by emergency exit requirement of FAR 25.807(c) (AMD memo (See Note 9) DTM 20164 identifies approved cabin interior for 12 passenger seats). Ferry flight configuration (0 passenger provisions) is defined by Dassault modification M3115 Crew Seats. The optional third crew seat may be occupied for takeoff and landing. Maximum Baggage. 2,866 lb in rear baggage compartment. Fuel Capacity. Nominal - (refer to weight and balance report of each individual airplane for exact capacity). Usable Fuel US Gallons Pounds Arm (in) wing and center wing, LH 904 6,058 -12.1 wing and center wing, RH 904 6,058 -12.1 Forward and aft fuselage 1,037 6,949 -28.2 TOTAL USABLE FUEL 2,845 19,065 TOTAL FUEL 2,863 19,184 Pressure Fueling 50 psi maximum. Oil Capacity. Usable, 0.375 US Gallons (Each Engine) Unusable, 2.86 US Gallons (drainable, and trapped oil) side engine arm + 136.7 in., center engine arm + 272.5 in. Maximum Operating Altitude. 51,000 ft. Control Surface Movements. Elevator: down 16º up 20º (Control Stops) Rudder: right 29º left 29º Aileron: up 25º20' down 24º50' Flaps: down 40º Airbrakes: up 68º Wing Slats: internal 20º external 30º Stabilizer: Electrical stops: Nose down 2º Nose up 10º Mechanical stops:Nose down (max) 2º30' Nose up (max) 10º30' Structural stops: Nose down (min) 2º40' Nose up (min) 11º Rigging tolerances are included in Maintenance Manual. (b) Falcon 900C Definition The 900C designation for the Mystere-Falcon 900 does not correspond to a model designation. It is only a commercial designation for Mystere-Falcon 900 airplanes on which one of the following major modifications are incorporated: M1975: Avionics upgrade - production M2695: Avionics upgrade – retrofit The M1975 and M2695 modifications consists of a complete upgrade of the basic Mystere-Falcon 900 avionics, by installation of a variant of the Honeywell Primus 2000 suite. M1975 is basic on all Mystere-Falcon 900 aircraft produced from serial number 179 and subsequent. All parameters listed in the preceding sub-section (a) for the basic Mystere-Falcon 900 remain valid for airplanes which incorporate M1975 or M2695. III. Model FALCON 900EX (Transport Category Airplane), approved July 19, 1996. A46EU 10 of 24 Rev. 24 (a) Basic Model Definition The Falcon 900EX is defined by Dassault modification M3000 and differs from the Mystere-Falcon 900 in the following major respects: (i) Allied Signal Engines TFE 731-60 replace TFE 731-5AR-1C or TFE 731-5BR-1C engines; (ii) A new aft fuel tank is added, and the forward central fuel tank is increased in capacity; (iii) The instrument panel is changed by the installation of a new avionics suite, including Honeywell Primus 2000 five tube EFIS including autothrottle; (iv) bleed air system is modified by the addition of a Bleed Air System Computer (BASC) and modification of HP flow control; (v) relocation of electrical system components, and use of Falcon 2000 type electrical wires; (vi) an increase in maximum weights. Engines. 3 engines - Allied Signal Engines TFE 731-60-1C (See Note 3b). Engine Limits. Static, Standard Sea Level Takeoff (5 min.) lb 5,000 Maximum Continuous lb 4,525 Maximum normal operating rotor speeds: Low pressure rotor (N1) rpm 21,000 percent 100% High pressure rotor (N2) rpm 31,485 percent 100% Transient conditions*: 1 second Low pressure rotor (N1) 100% to 100.5% High pressure rotor (N2) 100% to 101.5% * (See Note 7) Interstage Turbine Temperature (ITT): During starting 994C (1,821F) Takeoff (5 minutes) 1022C (1,872F) (10 sec. Transient*) 1032C (1,890F) Maximum Continuous 991C (1,816F) * (See Note 7) Oil temperature at fan gearbox inlet: Maximum: - Sea level to 30,000 ft 127C (260F) - Above 30,000 ft 140C (284F) Maximum transient (2 minutes) 149C (300F) Minimum Continuous 30C (86F) Fuel pressure: Minimum fuel pressure warning psig 4.5 Oil pressure limits: At idle psig 50 to 80 Takeoff and maximum continuous psig 65 to 80 Transient (3 minutes maximum) psig 100 APU. Allied Signal Engines GTCP 36-150(F) Limitation - Not operable in flight Rated Max.allowable EGT 720C 973C RPM 102% 110% Fuel: See NOTE 4, and Airplane Flight Manual Oil: See NOTE 5b Airspeed Limits. Unless otherwise indicated, speeds are indicated airspeeds. VMO (Maximum operating) Sea level 350 kt 10,000 ft 370 kt (linear variation from 0 to 10,000 ft) A46EU 11 of 24 Rev. 24 From 10,000 to 25,000 ft 370 kt MMO (Weight lower than 35,000 lb) From 25,000 to 38,000 ft Mach 0.87 From 38,000 to 42,000 ft Linear Variation from Mach 0.87 to 0.84 Above 42,000 ft Mach 0.84 MMO (Weight above 35,000 lb) From 25,000 to 33,000 ft Mach 0.87 From 33,000 to 37,000 ft Linear Variation from Mach 0.87 to 0.84 Above 37,000 ft Mach 0.84 VA (Maneuvering) 228 kt VFE (Slat and flaps speeds) flaps 7 + slats 200 kt flaps 20 + slats 190 kt flaps 40 + slats 180 kt Landing gear operation VLO 190 kt MLO Mach 0.70 Landing gear extended VLE 245 kt MLE Mach 0.75 Windshield wiper operation 215 kt Cockpit window opening 215 kt Minimum control speed In flight: VMCA 85.2 kt (CAS) On ground: VMCG 88.9 kt (CAS) Weight Limits & CG Range. Without M3020 (SB N 1) Weight Forward CG limit Rear CG limit kg lb % CMA % CMA Minimum weight Maximum zero fuel weight Maximum landing weight Maximum weight for 31% rear limit Maximum takeoff weight Maximum ramp weight 9 390 14 000 19 051 21 228 21 908 22 000 20 700 30 864 42 000 46 800 48 300 48 500 14 14 14 14 14 14 31 31 31 31 24,20 23,45 With M3020 (SB N 1) Weight Forward CG limit Rear CG limit kg lb % CMA % CMA Minimum weight Maximum zero fuel weight Maximum landing weight Maximum weight for 31% rear limit Maximum takeoff weight Maximum ramp weight 9 390 14 000 20 185 21 228 22 226 22 317 20 700 30 864 44 500 46 800 49 000 49 200 13 13 13 13 13 13 31 31 31 31 21,35 20,50 Datum. Datum is 25% of mean aerodynamic chord (MAC) and coincides with fuselage station +420.43 inches (Fuselage station +0 is the forward end of the aircraft nose cone). 13% MAC is 13.66 inches forward of the reference 14% MAC is 12.52 inches forward of the reference 31% MAC is 6.81 inches rear of the reference. A46EU 12 of 24 Rev. 24 Mean Aerodynamic Chord. Length 113.69 inches Zero % MAC is at FS + 392 inches Leveling Means. Standard bubble type level to be installed on the passengers seats tracks. Maximum Passengers. 19 maximum. (See Note 9) Ferry flight configuration (0 passenger provisions) is defined by Dassault modification M3116 Crew Seats. The optional third crew seat may be occupied for takeoff and landing. Maximum Baggage. 2,866 lb in rear baggage compartment. Fuel Capacity. Nominal - (refer to weight and balance report of each individual airplane for exact capacity). Usable fuel per engine* Liters kg* US gallons lb* Engine 1 Left wing and left front tank, left center tank and left feeder Engine 2 Front tank, rear tank, rear compartment tank and center feeder Engine 3 Right wing and right front tank, right center tank and right feeder 3 966 3 857 3 941 3 185 3 097 3 165 1 048 1 019 1 041 7 021 6 828 6 977 Usable – total 11 764 9 446 3 109 20 825 Fuel – total 11 854 9 519 3 133 20 986 * Fuel volumic mass: 0,803 kg/l Pressure fueling 50 psi max. Oil Capacity. Usable 1.01 U.S. Gallons (3.81 - 4.05 quarts) (Each engine) Total 1.823 U.S. Gallons (6,91 - 7,3 quarts) Unusable 0.317 U.S. Gallons (1,21 - 1,25 quart) Maximum Operating Altitude. 51,000 ft. Control Surface Movements. Elevator - up: 20 (Control stops) Elevator - down: 16 Rudder - right: 29 Rudder - left: 29 Aileron - up: 2520 Ailerons - down: 2450 Flaps - down: 40 Slats - internal: 20 Slats - external: 30 Airbrakes - up 68 Stabilizer Nose down Nose up Electrical stops Mechanical stops (maximum) Structural stops (minimum) 2 230 240 10 1030 11 Rigging tolerances are included in Maintenance Manual. (b) Falcon 900EX EASy Definition (Approved November 14, 2003) EASy designation for Falcon 900EX does not correspond to a model designation. This is only a commercial designation for airplanes on which a Major modification number M3083 has been embodied. Major Change Modification number M3083 to the Falcon 900EX consists of the installation of an Enhanced Avionics System (EASy) based on the Honeywell “Primus EPIC” product line. This system architecture is mainly built around 2 cabinets called A46EU 13 of 24 Rev. 24 Modular Avionics Units (MAU), 2 Modular Radio Cabinets (MRC), 2 Audio panels, 2 reversionary panels and 4 14.1 inch Liquid Crystal Displays. The pilots have access to the system using the 2 CCDs with multipurpose knob, menu pushbutton, display switch, action pushbuttons and trackball, 2 alphanumeric keyboards and the hard controls. M3083 is basic on all Falcon 900EX aircraft starting with serial number 97 and then continuing with serial number 120 through 600. All parameters listed in the preceding sub-section (a) for the basic Falcon 900EX remain valid for airplanes which incorporate M3083. (c) Falcon 900DX Definition (Approved November 3, 2005) The DX definition of the Falcon 900EX does not correspond to a model designation. The Falcon 900DX is only a commercial desgination for Falcon 900EX airplanes on which the following modifications are installed at production: Modification number Title Modification number Title M3083 + M3876 EASy Step 3 Configuration M4000 Definition of F900DX M3555 Rear Compartment mod M3755 Main Battery Relocation M5047 Feeder Routing in Rear Comp. M5012 Fastener Change in Longitudinal Beams M5046 FQMC Software Update M3987 Electronic Checklist for 900DX M3083, M3876, M4000, M3555, M3755, M5047, M5012, M5046 and M3987 are basic on all Falcon 900EX aiplanes starting with serial number 601 and subsequent. All parameters listed in the preceding sub-sections (a and b) for the Falcon 900EX and EASy designation remain valid for airplanes which incorporate M3083, M3876, M4000, M3555, M3755, M5047, M5012, M5046 and M3987, except for the following weight limits and CG changes: Weight Limits & CG Range for Falcon 900DX, except for s/n 621 and s/n 624 which incorporate M5051 and are the same as the Falcon 900EX: Falcon 900DX without M5051 Weight Forward CG limit Rear CG limit kg lb % CMA % CMA Minimum weight Maximum zero fuel weight Maximum landing weight Maximum weight for 31% rear limit Maximum takeoff weight Maximum ramp weight 9 390 14 000 19 142 21 228 21 183 21 273 20 700 30 864 42 200 46 800 46 700 46 900 14 14 14 14 14 14 31 31 31 31 24,20 23,45 . (d) Falcon 900LX Definition (Approved July 15, 2010) The LX definition of the Falcon 900EX does not correspond to a model designation. The Falcon 900LX is only a commercial designation for the Falcon 900EX on which modifications M5281 and M5535 (winglets) have been installed at production. All parameters listed in the preceding sub-section (b) above for the Falcon 900EX EASy remain valid for airplanes which incorporate M5281 and M5535. IV. DATA PERTINENT TO ALL MODELS. Fuel. - Fuels conforming to Allied Signal Engine Company Specifications: (See NOTE 4). EMS 53111 (Type JET A) EMS 53112 (Type JET A 1) EMS 53113 (Type JET B and JP4) EMS 53116 (Type JP5) Oil. - Oils conforming to Allied Signal Engine Company Specifications EMS 53110, A46EU 14 of 24 Rev. 24 Class B, Type 2. - (See NOTE 5a). Minimum Crew. 2 - Pilot and co-pilot. Serial Numbers Eligible. A French "Certificat de Navigabilite pour Exportation" endorsed as note under "Import Requirements" must be submitted for each individual aircraft for which application for US certification is made. Serial Numbers: For MYSTERE FALCON 50: Aircraft serial number 1 (s/n 2 See DGAC TCDS 163) through 250, and serial number 252. Serial number 251, 253 and subsequent are FALCON 50EX definition For MYSTERE FALCON 900: Aircraft serial number 1 (s/n 3 See DGAC TCDS 163) and Followings. Serial number 179 and subsequent include M1975 as standard (F900C definition). For FALCON 900EX: Aircraft serial number 1 through 119 except 97. Serial numbers 97, 120 through 600 include M3083 as standard (F900EX EASy definition). Aircraft serial number 601 and subsequent include M3083, M3876, M4000, M3555, M3755, M5047, M5012, M5046 and M3987 as standard (F900DX definition). Aircraft serial number 240 and subsequent include M5281 and M5535 as standard (F900LX definition). Import Requirements. Refer to the applicable bilateral agreement to verify eligibility for import into the United States of both new and used aircraft based on the scope of the agreement, to identify any required statements by the exporting authority on the export certificate of airworthiness (or equivalent document), and for procedures for coordinating exceptions to conformity statements on these documents. Refer to FAA Order 8130.2, Airworthiness Certification of Aircraft, for requirements for issuance of an airworthiness certificate for imported aircraft. Certification Basis. (a) For MYSTERE - FALCON 50 (basic model): FAR 21.29; FAR Part 25, dated February 1st, 1965, including amendments No. 25-1 through 25-34 and, Para 25.255 of amendment 25-42 Para 25.979 (d) and (e) as amended per amendment 25-38 Para 25.1013 (b)(1) as amended per amendment 25-36 Para 25.1351 (d) as amended per amendment 25-41 Para 25.1353 (c)(6) as amended per amendment 25-42 FAA Special Conditions No. 25-86-EU-24 dated March 6, 1979 Special Condition No. 25‐712‐SC, Non‐Rechargeable Lithium Batteries, effective to design changes applied for after January 18, 2018. See the applicability section of this special condition for more information on which design changes must meet it. FAR Part 36, through amendment 36-9 SFAR 27, through amendment SFAR 27-1 (fuel venting) Reference date of application for Type Certificate: 14 November 1973. (b) For MYSTERE - FALCON 50 airplanes incorporating Dassault modifications (Falcon 50EX definition): M1200: Increase of rudder control authority A46EU 15 of 24 Rev. 24 M1810: new engines - assembly line configuration - TFE 731-40 M1890: New Avionics M1939: new engine control EIED M1940: Bleed Air System Computer Or associated retrofit modifications: M2017: new engines – retrofit TFE 731-40-1C M1924: new avionics - retrofit (1) For parts of the airplane not changed or not affected by the modifications: Unchanged from basic Mystere-Falcon 50 (2) For those parts of the airplane that are changed or are affected by the modifications M1200, M1810, M1890, M1939, M1940, M2017, M1924: The certification basis includes, in addition to the certification basis of record indicated above in (b)(1), the following sections as amended by the indicated amendments: Section Amend. Title Section Amend. Title 25.2 25-72 Special retroactive req’mts 25.1143 25-57 Engine controls 25.207 25-42 Stall warning 25.1145 25-40 Ignition switches 25.305 25-77 Strength and deformation 25.1163 25.57 Powerplant accessories 25.307 25-54 Proof of structure 25.1165 25-72 Ignition systems 25.331 25-72 Maneuver and gust loads 25.1181 25-72 Fire zones 25.341 25-72 Gust loads 25.1183 25-57 Flammable fluid carrying components 25.343 25-72 Fuel and oil loads 25.1195 25-46 Fire extinguishing systems 25.345 25-72 High lift devices 25.1197 25-40 Fire extinguishing agents 25.351 25-72 Yawing conditions 25.1303 25-38 Flight and navigation instruments 25.361 25-72 Engine torque 25.1305 25-36 Powerplant instruments 25.1307 25-72 Miscellaneous equipment 25.571 25-72 Damage tolerance 24.1309 25-41 Equipment, systems and installations 25.1316 25-80 Lightning protection 25.603 25-46 Materials 25.1321 25-41 Instruments arrangement 25.605 25-46 Fabrication methods 25.1322 25-38 Warning, caution and advisory lights 25.613 25-72 Material strength properties 25.1323 25-57 Airspeed indicating system 25.693 25-72 Joints 25.1325 25-41 Static pressure systems 25.729 25-75 Retracting mechanism 25.1326 25-43 Pitot heating indicating systems 25.773 25-72 Pilot Compartment view 25.1329 25-46 Automatic pilot system 25.777 25-46 Cockpit controls 25.1331 25-41 Instruments using a power supply 25.779 25-72 Motion and effect of cockpit controls 25.1333 25-41 Instrument systems 25.781 25-72 Cockpit control knob shape 25.1335 25-41 Flight director systems 25.807 25-72 Passenger emergency exits 25.1337 25-40 Powerplant instruments 25.1381 25-72 Instrument lights 25.831(e) 25-41 Ventilation 25.1438 25-41 Pressurization systems 25.863 25-46 Flammable fluid fire protect. 25.1501 25-42 Operating limitations 25.869 25-72 Fire protection: systems 25.1521 25-72 Powerplant limitations 25.901 25-40 Powerplant installation 25.1529 25-54 Instructions for continued airworthiness 25.939 25-40 Engine operating characteristics 25.1543 25-72 Instrument markings 25.943 25-40 Negative acceleration 25.1551 25-72 Oil quantity indication 25.1013 25-72 Oil tanks 25.1557 25-72 Miscellaneous markings 25.1015 25-36 Oil tank tests 25.1581 25-72 Flight manual 25.1019 25-57 Oil strainer or filter 25.1583 25-72 Operating limitations 25.1021 25-57 Oil system drains 25.1585 25-46 Operating procedures 25.1041 25-38 Cooling - general 25.1091 25-57* Air induction A46EU 16 of 24 Rev. 24 25.1121 25-40 Exhaust system - general * NOTE: applicable for nacelles mounted on the fuselage sides 2. 14 CFR Part 36, effective December 1, 1969, as amended by Amendments 36-1 through 36-20. 3. 14 CFR Part 34, original issue. 4. Special Condition No. 25-ANM-115 HIRF Special Condition No. 25‐712‐SC, Non‐Rechargeable Lithium Batteries, effective to design changes applied for after January 18, 2018. See the applicability section of this special condition for more information on which design changes must meet it. 5. FAA Exemption No. 6451 for 25.571(e)(1), Amendment 25-72, Bird Strike Speed. 6. Equivalent safety findings for the following requirements: N2 Digital Only Indication (refer to Issue Paper P-6) 7. Compliance will be shown to the following optional requirements: - Ditching: § 25.801 Amendment 25-72 - Ice Protection : § 25.1419 Amendment 25-72 Reference date of application for design change is September 19, 1994. (c) For the MYSTERE - FALCON 900: - FAR Part 25, Amendment 25-1 through 25-56, except for the following sections which are complied with as amended through the noted Amendments. 25.107 - Amdt 25-38 - Take-off speeds 25.109 - Amdt 25-34 - Accelerate-stop distance 25.111 - Amdt 25-34 - Take-off path 25.149 - Amdt 25-34 - Minimum control speed 25.629 - Amdt 25-45 - Flutter, deformation and fail safe criteria 25.933 - Amdt 25-38 - Reversing systems 25.997 - Amdt 25-34 - Fuel strainer or filter 25.1019 - Amdt 25-34 - Oil strainer or filter 25.1093 - Amdt 25-34 - Induction system deicing and anti-icing provisions 25.1141 - Amdt 25-34 - Powerplant controls - General 25.1167 - Amdt 25-34 - Accessory gearboxes 25.1305 – Amdt 25-34 - Powerplant instruments - Special condition SC 25-ANM-8 High Altitude Operation - Special Condition No. 25‐712‐SC, Non‐Rechargeable Lithium Batteries, effective to design changes applied for after January 18, 2018. See the applicability section of this special condition for more information on which design changes must meet it. - SFAR 27, Amendments 27.1 through 27.5. (Fuel Venting) - FAR Part 36, Amendments 36.1 through 36.12. - Equivalent safety findings exist with respect to the following regulations: FAR Part 25.811(e)(3) Type III Exit Handle Illumination FAR Part 25.903(b) Engine Isolation - Advisory circular 120.29 change 3 criteria for approving Category I and Category II landing minima for FAR 121 operators. Compliance has been shown the following optional requirements. DITCHING; FAR 25.801 – Amdt 25-72 (overwater operation may be approved when the aircraft is equipped and installation approved to FAR 25.801). ICE PROTECTION; FAR 25.1419 – Amdt 25-72 A46EU 17 of 24 Rev. 24 For Mystere-Falcon 900 airplanes incorporating Dassault modification M-OPT0502 (Starlink Antenna Provisions): Equivalent Level of Safety Findings according to the provisions of 14 CFR 21.21(b)(1) for the following: Section 25.251: Vibration and Buffeting (documented in ELOS memo AT20750IB- T-ESF-B25.251-01) Reference date of application for Amendment to Type Certificate is Febuary 12, 1982 (d) For Mystere-Falcon 900 airplanes incorporating Dassault modifications M1975 or M2695 (Falcon 900C definition): (1) For parts of the airplane not changed or not affected by the modifications: Unchanged from basic Mystere-Falcon 900 certification basis (2) For those parts of the airplane that are changed or are affected by the modifications M1975 or M2695, the certification basis includes, in addition to the certification basis of record indicated above in (d)(1), the following sections as amended by the indicated amendments: - 14 CFR part 25, including Amendments 25-1 through 25-91, except for sections 25.1305(c)(8) and 25.1305(d)(3), which are complied with as amended through Amendments 25-1 through 25-34. - Special Condition 25-ANM-115 High Intensity Radiated Fields (HIRF) - Special Condition No. 25‐712‐SC, Non‐Rechargeable Lithium Batteries, effective to design changes applied for after January 18, 2018. See the applicability section of this special condition for more information on which design changes must meet it. - An equivalent level of safety finding was established with respect to the following regulation: Section 25.1549 Digital only display of engine high pressure rotor speed (issue paper P-1) - For precision approaches and landings, the applicable technical requirements are complemented by FAA advisory circulars AC 120-29 and AC 120-28C. - For the TCAS, the applicable technical requirements are complemented by FAA advisory circular AC 20-131A. Reference date of application for design change is February 8, 1998. (e) For the FALCON 900EX: 1. (a) For parts of the airplane not changed or not affected by the modification M3000 (Falcon 900EX definition): 14 CFR Part 25, effective February 1, 1965, including amendments 25-1through 25- 56, except for the following sections which are complied with as amended through the noted Amendments 25.629 Amdt. 25-45 Flutter, deformation and fail safe criteria 25.997 Amdt. 25-36 Fuel strainer or filter 25.1141 Amdt. 25-40 Powerplant controls - General (b) For those parts of the airplane that are changed or are affected by the modification M3000: 14 CFR Part 25, effective February 1, 1965, including amendments 25-1 through 25-77, except for the following sections which are complied with as amended through the indicated Amendments: A46EU 18 of 24 Rev. 24 25.109 Amdt. 25-0 Accelerate-stop distance 25.933 Amdt 25-38 Reversing system 25.1093 Amdt 25-0 Air intake system de-icing and anti-icing provisions 25.1316 Amdt. 25-80 Lightning Protection 2. 14 CFR Part 36 , effective December 1, 1969, as amended by Amendments 36-1 through 36-20. 3. 14 CFR Part 34, original issue. 4. Special Condition No. 25-ANM-8 High Altitude Operation Special Condition No. 25-ANM-115 HIRF Special Condition No. 25‐712‐SC Non‐Rechargeable Lithium Batteries, effective to design changes applied for after January 18, 2018. See the applicability section of this special condition for more information on which design changes must meet it. 5. FAA Exemption No. 6451 for 25.571(e)(1), Amendment 25-72, Bird Strike Speed. 6. Equivalent safety findings for the following requirements: Section 25.1549 N2 Digital Only Indication (refer to Issue Paper P-6) 7. Compliance is shown to the following optional requirements: - Ditching: § 25.801 Amendment 25-72 - Ice Protection : § 25.1419 Amendment 25-72 8. Miscellaneous - For precision approaches and landings, the applicable technical requirements are complemented by FAA Advisory Circular (AC) 120-29 and AC 120-28(c). - For the automatic flight control system, the applicable technical requirements are complemented by AC 25-1329-1A for cruise. Reference date of application for amendment to type certificate is March 3, 1993 (f) For FALCON 900EX airplanes incorporating Dassault modification M3083 (Falcon 900EX EASy definition): 1. (a) For parts of the airplane not changed or not affected by modification M3083: Unchanged from basic Falcon 900EX certification basis (b) For those parts of the airplane that are changed or are affected by the modification M3083: 14 CFR Part 25, effective February 1, 1965, including amendments 25-1 through 25-98, except for the following sections which are complied with as amended through the indicated Amendments: 25.1351 Amdt. 25-41 General 25.1353 Amdt. 25-42 Electrical Equipment and Installations 25.1355 Amdt. 25-38 Distribution System 2. 14 CFR Part 36 , effective December 1, 1969, as amended by Amendments 36-1 through 36-20. 3. 14 CFR Part 34, original issue. 4. Special Condition No. 25-ANM-8 High Altitude Operation A46EU 19 of 24 Rev. 24 Special Condition No. 25-ANM-115 HIRF Special Condition No. 25‐712‐SC Non‐Rechargeable Lithium Batteries, effective to design changes applied for after January 18, 2018. See the applicability section of this special condition for more information on which design changes must meet it. 5. FAA Exemption No. 6451 for 25.571(e)(1), Amendment 25-72, Bird Strike Speed. 6. Equivalent safety findings for the following requirements: Section 25.1549 N2 Digital Only Indication (refer to Issue Paper P-6) Section 25.813(c)(2) Emergency Exit Access (documented in TAD ELOS Memo AT10291IB-T-C-101) Section 25.809(b) and 25.813(c)(2)(ii) - Emergency Exit Access (documented in TAD ELOS Memorandum AT10010IB-T-CI-101) 25.813(c)(2) “Emergency Exit Access” (documented in TAD ELOS Memo SP00843IB-T) 7. Compliance is shown to the following optional requirements: - Ditching: § 25.801 Amendment 25-72 - Ice Protection : § 25.1419 Amendment 25-72 8. Miscellaneous - For precision approaches and landings, the applicable technical requirements are complemented by FAA Advisory Circular (AC) 120-29 and AC 120-28(c). - For the automatic flight control system, the applicable technical requirements are complemented by AC 25-1329-1A for cruise. Reference date of application for design change M3083 is November 8, 1999. (g) For Falcon 900EX airplanes incorporating Dassault modification M4000 (F900DX): See (f) above. (h) For Falcon 900EX airplanes incorporating Dassault modification M5281 (F900LX): 1. (a) For parts of the airplane not changed or not affected by modification M5281: Unchanged from basic Falcon 900EX certification basis (b) For those parts of the airplane that are changed or are affected by the modification M5281: Based on the application date of September 14, 2006, for Modification M5281, under the provisions of Federal Aviation Regulation 14 CFR 21.101, the applicable type certification standards for the modification to the Model Falcon 900EX series are as follows: 14 CFR Part 25, effective February 1, 1965, including amendments 25-1 through 25-119, except for the following sections which are complied with as amended through the indicated Amendments: • 14 CFR part 25 paragraphs at Amendment 34 25.1093 and 25.1141 (except (a) and (f)) • 14 CFR part 25 paragraphs at Amendment 38 25.933 • 14 CFR part 25 paragraphs at Amendment 45 A46EU 20 of 24 Rev. 24 25.629 • 14 CFR part 25 paragraphs at Amendment 56 25.361 to 25.367, 25.399 to 25.409, 25.495 to 25.511, 25.561, 25.562, 25.563, 25.621, 25.655, 25.657, 25.675, 25.679 to 25.697, 25.701, 25.721, 25.723, 25.729 (except (e)), 25.731 to 25.745, 25.772, 25.773(b)(c), 25.775, 25.779, 25.783(except (e)), 25.785, 25.787, 25.793, 25.801 to 25.811, 25.812 (except (f)), 25.813, to 25.833, 25.841 (except (b)(5)(6)), 25.843 to 25.859, 25.863 (except (c)), 25.871, 25.875, 25.901 (except (c)), 25.903 (except (d)(2)), 25.905 to 25.929, 25.934, 25.937, 25,939, 25.941 to 25.961, 25.963 (except (e)), 25.965 to 25.994, 25.999 to 25.1017, 25.1021 to 25.1027, 25.1041 (except (f)), 25.1043 to 25.1091, 25.1103 to 25.1127, 25.1143, 25.1145 (c), 25.1149 to 25.1165, 25.1181 to 25.1201, 25.1207, 25.1337 (except (b)(d)), 25.1351, 25.1353, 25.1362, 25.1363, 25.1383, 25.1403 to 25.1415, 25.1421, 25.1433, 25.1435 (except (a)(2)), 25.1436 to 25.1455, 25.1461, 25.1503 to 25.1521, 25.1525, 15.1527, 25.1531, 25.1533, 25.1557, 25.1561, 25.1583, and 25.1587 • 14 CFR part 25 paragraphs at Amendment 72 25.1419 • 14 CFR part 25 paragraphs at Amendment 77 25.145, 25.149, 25.201, 25.203, 25.233, 25.253, 25.901 (c), 25.963 (e), 25.997, 25.1019, 25.1167 • 14 CFR part 25 paragraphs at Amendment 98 25.1 to 25.33; 25.147; 25.171; 25.173; 25.175; 25.177; 25.181; 25.207; 25.231; 25.235; 25.237; 25.671; 25.672; 25.677; 25.699; 25.703; 25.729 (f); 25.771; 25.773 (a) (d); 25.783 (e); 25.789; 25.791; 25.812 (f); 25.841 (b)(5) (b)(6); 25.863 (c); 25.869; 25.899; 25.903 (d)(2); 25.1141 (a) (f); 25.1145 (a) (b); 25.1203; 25.1301; 25.1303; 25.1305; 25.1307; 25.1309;25.1321; 25.1322; 25.1323; 25.1325; 25.1326; 25.1327; 25.1329; 25.1331; 25.1333; 25.1335; 25.1337 (b) (d); 25.1351; 25.1353; 25.1355; 25.1357; 25.1360; 25.1381; 25.1435 (a)(2); 25.1457; 25.1459; 25.1501; 25.1523; 25.1529; 25.1541; 25.1543; 25.1545; 25.1547; 25.1549; 25.1551; 25.1553; 25.1555; 25.1563; 25.1585 • 14 CFR part 25 paragraphs at Amendment 144 25.773(e) : « Pilot compartment view » For FalconEye System Installations. 2. 14 CFR Part 36 , effective December 1, 1969, as amended by Amendments 36-1 through 36-28. 3. 14 CFR Part 34, original issue. 4. Special Condition No. 25-ANM-8 High Altitude Operation Special Condition No. 25-ANM-115 HIRF Special Condition No. 25‐712‐SC Non‐Rechargeable Lithium Batteries, effective to design changes applied for after January 18, 2018. See the applicability section of this special condition for more information on which design changes must meet it. 5. FAA Exemptions: Existing exemptions apply and No. 109332 for 25.629(d)(9) Amdt 25-45 and 25.671(c)(2) Amdt 25-56. A46EU 21 of 24 Rev. 24 6. Equivalent safety findings for the following requirements: Section 25.1419 – Ice Protection (documented in TAD ELOS Memo TD0710IB-T- S-101) Reference date of application for design change M5281 is September 14, 2006. (i) For FALCON 900EX series airplanes incorporating M-OPT0501 (Starlink Antenna Provisions: See (e),(f), (g), and (h) above. Equivalent Level of Safety Findings according to the provisions of 14 CFR 21.21(b)(1) for the following: Section 25.251: Vibration and Buffeting (documented in ELOS memo AT20750IB-T-ESF- B25.251-01) The Direction Generale de l'Aviation Civile (D.G.A.C.) of France originally type certificated this aircraft under its type certificate Number 163. The FAA validated this product under U.S. Type Certificate Number A46EU. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of the D.G.A.C.. Type Definition For the Mystere-Falcon 50, the type definition is in Note DTM 800, Revision G For the Mystere-Falcon 900, the type definition is in Note DTM 20.078, Revision C For the Falcon 900EX, the type definition is in Modification M3000, Revision B3 of Mystere-Falcon 900 Equipment. The basic required equipment as prescribed in the applicable airworthiness regulations (See Certification Basis) must be installed on the aircraft for certification. The lists of all equipment as well as optional equipment approved by Direction Generale de l'Aviation Civile (DGAC) of France are contained: For the MYSTERE - FALCON 50, in the AMD-BA memos No. DTM 380075/91 and DTM 4510/78 For the MYSTERE - FALCON 900, in the AMD-BA memos No. DTM 5100/84 and DTM 5257/84 For the FALCON 900EX, in the Dassault Aviation memo No. DTM 35-3287/95 In addition, the following is required: (a) For the MYSTERE - FALCON 50: DGAC approved FALCON 50 Airplane Flight Manual, Document DTM-813 approved September 9, 1988, as of revision 24 and subsequent - It supersedes DTM 884 which must no longer be used. For the MYSTERE - FALCON 50, s/n 253 and subsequent (Falcon 50 EX definition): DGAC approved FALCON 50 Airplane Flight Manual, Document DTM-813EX revision 1 approved December 20, 1996 For the MYSTERE - FALCON 900: DGAC approved FALCON 900 Airplane Flight Manual, Document DTM 20103 approved June 6, 1986. For the Mystere-Falcon 900, s/n 179 and subsequent (F900C definition): DGAC approved Falcon 900 Airplane Flight Manual, Document FM900C approved 15 June 1999 A46EU 22 of 24 Rev. 24 For the FALCON 900EX s/n 1 through 119 except 97: DGAC approved Airplane Flight Manual, Document DTM 561 Revision 1, approved July 16, 1996. For the FALCON 900EX serial numbers 97, 120 and subsequent (F900EX EASy definition): DGAC approved Airplane Flight Manual, Document DGT84972 approved November 13, 2003. (b) Nose wheel must be equipped with a chined tire. Service Information. Each of the documents listed below that contain a statement that it is approved by the European Aviation Safety Agency (EASA) - or for approvals made before September 28, 2003 - by the the Direction Generale de l'Aviation Civile (D.G.A.C.) of France, are accepted by the FAA and are considered FAA approved. Additionally, approvals issued by Dassault Aviation under the authority of EASA approved Design Organization EASA.21J.051 - or for approvals made before September 28, 2003 - under the authority of DGAC Design Organization Approval No. No. F.JA.03 are considered FAA approved. These approvals pertain to the type certificate only such as changes to type design and repair/unrepair of damages. • Dassault Aviation Service Bulletins, except as noted below, • Structural repair manuals, • Vendor manuals referenced in Dassault Aviation service bulletins • Aircraft flight manuals, • Repair Instructions. Note: Design changes that are contained in Dassault Aviation Service Bulletins and that are classified as Level 1 Major in accordance with either the US/Direction Generale de l'Aviation Civile (D.G.A.C.) of France or US/EASA Bilateral Aviation Safety Agreement Implementation Procedures for Airworthiness must be approved by the FAA. NOTES. NOTE 1. Weight and Balance (a) Current weight and balance report, including list of equipment in certified empty weight and loading instructions must be provided for each aircraft at delivery. (b) The following must be included in the airplane empty weight: (1)For the MYSTERE - FALCON 50: The total unusable fuel (92.6 lb) listed as follows, plus unusable oil (54 lb), plus hydraulic fluid (106 lb at + 93.3 in.) UNUSABLE FUEL US GALLONS POUNDS ARM (in) Drainable: Left Wing 0.8 5.3 -7.87 Center Wing 0.5 3.5 -7.87 Right Wing 0.8 5.3 -7.87 Left fuselage 0.7 4.4 +70.87 Center fuselage 0.5 3.5 +70.87 Right fuselage 0.7 4.4 +70.87 UNUSABLE FUEL US GALLONS POUNDS ARM (in) Trapped Fuel: Tanks and fuel lines: 9.8 65.4 +14.77 TOTAL UNUSABLE FUEL 13.8 91.8 A46EU 23 of 24 Rev. 24 (2) For the MYSTERE - FALCON 900: The total unusable fuel 119 (lbs.) listed as follows, plus unusable oil 73.6 (lbs.), plus hydraulic fluid (106 lbs. at +79.57 in.). UNUSABLE FUEL US GALLONS POUNDS ARM (in) Drainable: Wing and center wing, LH 3.03 20.3 -35.33 Wing and center wing, RH 2.34 15.7 -35.33 Forward and aft fuselage 2.30 15.4 +20.20 Trapped Fuel: Tanks and fuel lines: 10.20 68.3 -44.13 TOTAL UNUSABLE FUEL 17.86 119.7 (3) For the FALCON 900EX: The total unusable fuel (114 lbs, at -21.2 in.), plus the unusable oil (42 lbs), plus hydraulic Fluid (106 lbs. At + 79.57 in. Unusable fuel per engine Liters Kg US Gallons lb Drainable: Engine 1 (left circuit) Engine 2 (center circuit) Engine 3 (right circuit) Non drainable: Tanks and pipes 21.4 19.8 23 26 17.2 15.9 18.5 21 6 5 6 7 38 35 41 46 Unusable – total 90 73 24 160 (c) The airplane must be loaded in accordance with the Falcon 50 Performance Manual, Section 2, or the Falcon 900 Loading Manual, Loading Instructions, as applicable, and the C.G. must be within the specified limits at all times. NOTE 2. Reserved. NOTE 3. Service Life Limits and required Maintenance/Inspections. a. Airframe components which are life limited, and associated retirement times, are presented in DGAC approved Chapter 5.40.00 of the FALCON 50 or FALCON 900 and 900EX Maintenance Manual, and must be replaced as indicated therein. b. Engine Life Limited parts are listed in FAA-approved Allied Signal Service Bulletin TFE 731 72-3001. c. Required Maintenance and Inspections to maintain airworthiness based on/involving reliability are presented in DGAC approved Chapter 5.40.00 of the Falcon 50 or Falcon 900 and 900EX Maintenance Manual. Chapter 5-40 references: MF50/F50EX : Airworthiness Limitation Section (Chapter 5-40, reference: DGT 113872) MF900/F900C : Airworthiness Limitation Section (Chapter 5-40, reference: DGT113873) F900EX : Airworthiness Limitation Section (Chapter 5-40, reference: DGT113874) F900EX Easy/DX/LX: Airworthiness Limitation Section (Chapter 5-40, reference: DGT113875) NOTE 4. Fuel Specifications and Additives: a. For information concerning equivalent fuel specifications see Airplane Flight Manual. If a different type of fuel is used, or a mixture of fuels are used, the engine computer must be adjusted in accordance with the TFE 731-3,or TFE 731-5, or TFE 731-40, or TFE 731- 60 Maintenance Manual (as applicable) to adapt the computer to the density of the fuel used in order to preserve both the starting, and the acceleration deceleration characteristics of the engine. b. ADDITIVES A46EU 24 of 24 Rev. 24 For the TFE 731 engine, the GTCP 36-100 and GTCP 36-150 auxiliary power unit the following additives limitations are approved: - Anti-Icing Additive, conforming to AIR 3652 or - MIL-I-27686D or E, (JP-4/JP-8) or to MIL-I-85470 (JP-5) or equivalent are approved for use in fuel in amounts up to 0.15 percent by volume. - SOHIO Biobor JF biocide additive, or equivalent, is approved for use in the fuel at a concentration not to exceed 270 PPM - - Antistatic additive, provided the quantity added does not exceed 1 PPM for SHELL ASA 3 and 3 PPM for STADIS 450. NOTE 5. Qualified Oils: a. Allied Signal Turbine Engine Company Service Information Letters give brand names of oils conforming to Specification EMS 53110, Class B, Type 2. b. Brand names of oils approved for use in the APU are listed in the GTCP 36-100 or GTCP 36-150 Maintenance Manual as applicable. NOTE 6. For the MYSTERE - FALCON 50, Installation of the AiResearch Model GTCP 36-100(A) turbine auxiliary power unit is an approved optional installation and may be installed subsequent to airplane delivery in accordance with AMD-BA Service Bulletin No. FALCON 50-0002. NOTE 7. If these transient limits are exceeded refer to engine Maintenance Manual for corrective action. NOTE 8. Effective June 19, 1990 the name of AVIONS MARCEL DASSAULT-BREGUET AVIATION changed to DASSAULT AVIATION. The new name will appear as of this date on all documents and nameplates. However, documents bearing the old name remain valid and will be updated when and where necessary. NOTE 9. The cabin interior arrangements must comply with the FAA certification basis. General specification for cabin interior completions are covered by the document DTM 802-30 for Mystere-Falcon 50 airplanes, and by DTM 20-167 for Mystere-Falcon 900 and Falcon 900EX airplanes. These specifications mainly cover the gust and forced landing load factors. For the Mystere-Falcon 900 and Falcon 900EX, DGAC France has granted an equivalent safety finding for FAR 25.813(e) to allow cabin interior doors. This equivalent safety finding is not included in the FAA certification basis and is therefore not valid for US registered airplanes. NOTE 10. The modifications MF50 M2210 (from serial number 263), MF900 M2440 (from serial number 165), F900EX M2458 (from serial number 015) have been approved to operate in "Reduced Vertical Separation Minimun" airspace. Continued airworthiness and operational approval aspects of RVSM must be constructed according to advisory circular 91- RVSM. Aircraft RVSM capability remains valid after further incorporation of any DGAC approved Dassault Aviation Modification. NOTE 11. An approved change to the AFM and ALS can be released either through a full revision of the manual or through a Change Project (CP) number bearing the same reference as the related manual. .....END..... ``` ## ADs (146, first 50, in force first) - [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026 - [AD 2025-06-05](https://openairdocs.org/ad/2025-06-05): Information systems · Dassault Falcon 7X, Falcon 900EX and FALCON 2000EX. Effective May 2, 2025 - [AD 2024-14-09](https://openairdocs.org/ad/2024-14-09): Standard Practices/Structures · Dassault Falcon 7X, Falcon 900EX and FALCON 2000EX. Effective Oct 15, 2024 - [AD 2024-15-01](https://openairdocs.org/ad/2024-15-01): Time Limits/Maintenance Checks · Dassault Falcon 900EX. Effective Oct 15, 2024 - [AD 2024-15-02](https://openairdocs.org/ad/2024-15-02): Time Limits/Maintenance Checks · Dassault Mystere-Falcon 900. Effective Oct 15, 2024 - [AD 2024-14-02](https://openairdocs.org/ad/2024-14-02): Time Limits/Maintenance Checks · Dassault Falcon 900EX. Effective Sep 25, 2024 - [AD 2010-26-05 R1](https://openairdocs.org/ad/2010-26-05-R1): Air conditioning · Dassault Falcon 10, Fan Jet Falcon, Fan Jet Falcon Series C and 14 more. Effective Dec 6, 2023 - [AD 2023-18-08](https://openairdocs.org/ad/2023-18-08): Ice and Rain Protection · Dassault Mystere-Falcon 900, Falcon 900EX, FALCON 2000 and 1 more. Effective Nov 7, 2023 - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 - [AD 2023-05-15](https://openairdocs.org/ad/2023-05-15): Time Limits/Maintenance Checks · Dassault Mystere-Falcon 50. Effective May 18, 2023 - [AD 2021-20-14](https://openairdocs.org/ad/2021-20-14): Equipment/Furnishings · Dassault Falcon 7X, Falcon 900EX and FALCON 2000EX. Effective Nov 18, 2021 - [AD 2020-20-01](https://openairdocs.org/ad/2020-20-01): Instruments · Dassault Falcon 7X, Falcon 900EX and FALCON 2000EX. Effective Oct 21, 2020 - [AD 2020-17-12](https://openairdocs.org/ad/2020-17-12): Equipment/furnishings · Dassault Falcon 900EX, FALCON 2000, FALCON 2000EX and 1 more. Effective Sep 9, 2020 - [AD 2019-23-18](https://openairdocs.org/ad/2019-23-18): Fire protection · Dassault Falcon 900EX, FALCON 2000, FALCON 2000EX and 2 more. Effective Jan 17, 2020 - [AD 2019-23-17](https://openairdocs.org/ad/2019-23-17): Flight controls · Dassault Falcon 900EX and FALCON 2000EX. Effective Dec 27, 2019 - [AD 2019-05-14](https://openairdocs.org/ad/2019-05-14): This AD removes AD 2012-02-18 · Dassault Mystere-Falcon 50. Effective Mar 28, 2019 - [AD 2018-24-02](https://openairdocs.org/ad/2018-24-02): Wings · Dassault Falcon 900EX, Mystere-Falcon 50 and Mystere-Falcon 900. Effective Jan 2, 2019 - [AD 2018-19-06](https://openairdocs.org/ad/2018-19-06): Flight Controls · Dassault Falcon 900EX. Effective Nov 13, 2018 - [AD 2018-11-10](https://openairdocs.org/ad/2018-11-10): Doors · Dassault Fan Jet Falcon, Fan Jet Falcon Series C, Fan Jet Falcon Series D and 9 more. Effective Jul 9, 2018 - [AD 2018-05-05](https://openairdocs.org/ad/2018-05-05): Wings · Dassault Falcon 900EX, FALCON 2000, FALCON 2000EX and 1 more. Effective Apr 11, 2018 - [AD 2018-02-06](https://openairdocs.org/ad/2018-02-06): Navigation · Dassault Falcon 7X, Falcon 900EX and FALCON 2000EX. Effective Feb 5, 2018 - [AD 2017-23-10](https://openairdocs.org/ad/2017-23-10): Ice and rain protection · Dassault Falcon 900EX and FALCON 2000EX. Effective Dec 1, 2017 - [AD 2017-16-09](https://openairdocs.org/ad/2017-16-09): Landing gear · Dassault FALCON 2000 and Mystere-Falcon 50. Effective Sep 25, 2017 - [AD 2016-19-13](https://openairdocs.org/ad/2016-19-13): Lights · Dassault Falcon 900EX, FALCON 2000, FALCON 2000EX and 2 more. Effective Nov 22, 2016 - [AD 2016-15-05](https://openairdocs.org/ad/2016-15-05): Flight Controls · Dassault Falcon 900EX and FALCON 2000EX. Effective Sep 8, 2016 - [AD 2016-10-16](https://openairdocs.org/ad/2016-10-16): Operations Information · Dassault Falcon 900EX, FALCON 2000EX and Mystere-Falcon 900. Effective Jun 27, 2016 - [AD 2016-09-03](https://openairdocs.org/ad/2016-09-03): Equipment/Furnishings · Dassault Falcon 900EX, FALCON 2000, FALCON 2000EX and 1 more. Effective Jun 6, 2016 - [AD 2016-04-09](https://openairdocs.org/ad/2016-04-09): Wings · Dassault Falcon 900EX and FALCON 2000EX. Effective Apr 5, 2016 - [AD 2015-08-02](https://openairdocs.org/ad/2015-08-02): Electrical Power · Dassault Mystere-Falcon 50. Effective Apr 29, 2015 - [AD 2012-26-15 R1](https://openairdocs.org/ad/2012-26-15-R1): Navigation · Agusta AW139, A318-111, A318-112 and 70 more. Effective Dec 3, 2014 - [AD 2014-18-01](https://openairdocs.org/ad/2014-18-01): Navigation · Bombardier ATR42-200, ATR42-300, ATR42-320 and 23 more. Effective Oct 14, 2014 - [AD 2013-09-03](https://openairdocs.org/ad/2013-09-03): Wings · Dassault Falcon 900EX, FALCON 2000, FALCON 2000EX and 2 more. Effective Aug 14, 2013 - [AD 2013-11-06](https://openairdocs.org/ad/2013-11-06): Electrical Power · Dassault Falcon 900EX and Mystere-Falcon 900. Effective Jul 9, 2013 - [AD 2012-06-21](https://openairdocs.org/ad/2012-06-21): Fuel · Dassault Mystere-Falcon 900. Effective May 4, 2012 - [AD 2011-10-14](https://openairdocs.org/ad/2011-10-14): Landing Gear · Dassault Mystere-Falcon 50. Effective Jun 17, 2011 - [AD 2011-07-11](https://openairdocs.org/ad/2011-07-11): Fire protection · Dassault Mystere-Falcon 50. Effective Apr 18, 2011 - [AD 2010-07-02](https://openairdocs.org/ad/2010-07-02): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 26 more. Effective May 3, 2010 - [AD 2010-04-01](https://openairdocs.org/ad/2010-04-01): Oxygen · Dassault Falcon 900EX. Effective Mar 19, 2010 - [AD 2009-08-01](https://openairdocs.org/ad/2009-08-01): Honeywell FMSs · Bombardier CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R), CL-600-2B16 (CL-604) and 11 more. Effective May 14, 2009 - [AD 2008-25-04](https://openairdocs.org/ad/2008-25-04): Valve boxes · Dassault Mystere-Falcon 50. Effective Jan 15, 2009 - [AD 2008-22-05](https://openairdocs.org/ad/2008-22-05): Control panel reading light · Dassault FALCON 2000, Falcon 900EX and Mystere-Falcon 900. Effective Dec 19, 2008 - [AD 2008-12-19](https://openairdocs.org/ad/2008-12-19): Feeder bundle and the right side partition wall separating the cabin from the lavatory · Dassault Falcon 900EX and Mystere-Falcon 900. Effective Jul 24, 2008 - [AD 2008-12-15](https://openairdocs.org/ad/2008-12-15): Oxygen controller · Dassault FALCON 2000EX and Falcon 900EX. Effective Jul 23, 2008 - [AD 2008-12-18](https://openairdocs.org/ad/2008-12-18): Primary flight unit (PDU) · Dassault FALCON 2000EX and Falcon 900EX. Effective Jul 23, 2008 - [AD 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 2008 - [AD 2008-09-21](https://openairdocs.org/ad/2008-09-21): Electrical feeder bundle and a bus bar · Dassault Mystere-Falcon 50. Effective Jun 12, 2008 - [AD 2008-05-08](https://openairdocs.org/ad/2008-05-08): Life raft · Dassault Mystere-Falcon 50. Effective Apr 8, 2008 - [AD 2008-04-14](https://openairdocs.org/ad/2008-04-14): Overwing emergency exit · Dassault Falcon 10, Falcon 900EX, Fan Jet Falcon and 14 more. Effective Apr 1, 2008 - [AD 2007-26-11](https://openairdocs.org/ad/2007-26-11): High-pressure oxygen cylinder · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 45 more. Effective Jan 28, 2008 - [AD 2007-25-10](https://openairdocs.org/ad/2007-25-10): Trailing edge flap · Dassault Falcon 900EX, FALCON 2000, FALCON 2000EX and 2 more. Effective Jan 14, 2008 All 146: https://openairdocs.org/tcds/A46EU/ads.md ## Registered aircraft by registry model (OpenAirDocs) - [Dassault FALCON 900EX](https://openairdocs.org/model/dassault-falcon-900ex): 140 aircraft (registry code 2730013) - [Dassault FALCON 900 EX](https://openairdocs.org/model/dassault-falcon-900-ex): 115 aircraft (registry code 2730009) - [Dassault MYSTERE-FALCON 50](https://openairdocs.org/model/dassault-mystere-falcon-50): 88 aircraft (registry code 2730173) - [Dassault-Breguet MYSTERE FALCON 900](https://openairdocs.org/model/dassault-breguet-mystere-falcon-900): 73 aircraft (registry code 2730160) - [Dassault MYSTERE FALCON 900](https://openairdocs.org/model/dassault-mystere-falcon-900): 52 aircraft (registry code 2730172) - [Dassault FALCON 900](https://openairdocs.org/model/dassault-falcon-900): 9 aircraft (registry code 2730102) - [Avions Marcel Dassault MYSTERE FALCON 900](https://openairdocs.org/model/avions-marcel-dassault-mystere-falcon-900): 4 aircraft (registry code 2730161) - [Avions Marcel Dassault Breguet MYSTERE FALCON 50](https://openairdocs.org/model/avions-marcel-dassault-breguet-mystere-falcon-50): 2 aircraft (registry code 2730199) - [Dassault FALCON 900LX](https://openairdocs.org/model/dassault-falcon-900lx): 1 aircraft (registry code 2730015) ## STCs approved under this data sheet (991, first 50) - [STC ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.. Rockwell Collins Inc - [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center - [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc. - [STC ST03619NY](https://openairdocs.org/stc/ST03619NY): Installation of SpaceX Starlink Aviation System. Dassault Falcon Jet Corp. - [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc. - [STC ST11282DS](https://openairdocs.org/stc/ST11282DS): Installation of a wireless cabin management system. Cabin Management Solutions - [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS).. VisionSafe LLC - [STC ST03598NY](https://openairdocs.org/stc/ST03598NY): Installation of a GoGo AVANCE L5 system. Dassault Falcon Jet Corp. - [STC ST03606NY](https://openairdocs.org/stc/ST03606NY): Installation of Mid-Continent Instruments and Avionics MD302 Standby Attitude Module. Dassault Falcon Jet Corp. - [STC ST04591CH](https://openairdocs.org/stc/ST04591CH): Installation of SmartSky System. Apcela IFC JV, LLC dba Apcela ATG - [STC ST03594NY](https://openairdocs.org/stc/ST03594NY): Installation of Honeywell Primus Elite SVS Upgrade. Dassault Falcon Jet Corp. - [STC ST11216DS](https://openairdocs.org/stc/ST11216DS): Installation of automatic dependent surveillance-broadcast (ADS-B) out on Part 25 aircraft. BHE & Associates Ltd. - [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc. - [STC ST11033SC](https://openairdocs.org/stc/ST11033SC): Installation of upgraded hardware to the Rockwell Collins Pro Line IV FMS-6100 to provide Localizer Performance with Vertical Guidance (LPV). BHE & Associates LTD - [STC ST11040SC](https://openairdocs.org/stc/ST11040SC): Installation of upgraded hardware to the Rockwell Collins Pro Line 21 FMS-6100 to provide Localizer Performance with Vertical Guidance (LPV). BHE & Associates LTD - [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc. - [STC ST04533CH](https://openairdocs.org/stc/ST04533CH): Installation of Universal Avionics InSight (TM) Display System, UNS-1Fw SBAS FMS, Future Air Navigation System (FANS) with UniLink® UL-801 Communications Management Unit and options for a Cockpit Voice Recorder for Datalink Recording, Mid-Continent Instruments MD302 Standby Instrument, PS Engineering Audio Panels, LED Cockpit Lighting upgrade, and Latitude Technologies SkyNode 200 Iridium for Satellite Voice Safety Services in accordance with Chicago Jet Group LLC, Master Data List, Document No. DB2004004, Revision F, dated August 30, 2021, or later FAA approved revision.. Chicago Jet Group LLC - [STC ST11834CH](https://openairdocs.org/stc/ST11834CH): Installation of Gogo L5 System with MB13 Antenna. StandardAero Business Aviation Services LLC - [STC ST03610NY](https://openairdocs.org/stc/ST03610NY): Installation of Universal InSight Displays. Dassault Falcon Jet Corp. - [STC ST03612NY](https://openairdocs.org/stc/ST03612NY): Installation of Garmin (Standby Flight Display System). Dassault Falcon Jet Corp - [STC ST02586AK](https://openairdocs.org/stc/ST02586AK): Approval of the Thomas Global Systems TFD-4000/4100 Active Matrix Liquid Crystal Display. ADS-B Technologies - [STC ST01833WI](https://openairdocs.org/stc/ST01833WI): Modification of a Rockwell Collins Global Positioning System (GPS) installation. Rockwell Collins Inc. - [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC - [STC ST04666CH](https://openairdocs.org/stc/ST04666CH): Installation of Gogo MB13 Antennas. PREMIER AIR CENTER LLC d/b/a WEST STAR AVIATION - [STC ST03615NY](https://openairdocs.org/stc/ST03615NY): Installation of Honeywell CC-701 Cursor Control Device. Dassault Falcon Jet Corp - [STC ST01066DE](https://openairdocs.org/stc/ST01066DE): Installation of the Aviation Clean Air Airborne Air & Surface Purification System. Lee Aerospace, Inc . - [STC ST04159CH](https://openairdocs.org/stc/ST04159CH): Upgrade of Honeywell Primus II Communications Units RCZ-8XX Transponders to support Certification of Automatic Dependent Surveillance -Broadcast (ADS-B) Out. CMD Flight Solutions LLC - [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC - [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc. - [STC ST00928DE](https://openairdocs.org/stc/ST00928DE): Installation of a Datalink Communications System supporting Air Traffic Services (ATS) using a Universal UniLink UL-801 Communications Management Unit (CMU). West Star Aviation LLC - [STC ST11289DS](https://openairdocs.org/stc/ST11289DS): An update to the Communication Management Unit (CMU) to add or update the 3rd VHF Datalink to support Controller Pilot Data Link Communication (CPDLC). Dassault Falcon Jet Corp. - [STC ST04556AT](https://openairdocs.org/stc/ST04556AT): Installation of a cabin interior. Walkabout Air Inc. - [STC ST04607CH](https://openairdocs.org/stc/ST04607CH): Reconfiguration of a Cabin Floor Plan. Standard Aero Business Aviation Services LLC - [STC ST01985WI](https://openairdocs.org/stc/ST01985WI): Installation of the Garmin GI-275 I Electronic Standby Instrument (ESI). Peregrine - [STC ST02004WI](https://openairdocs.org/stc/ST02004WI): Installation of the Garmin GI-275 Instantaneous Vertical Speed Indicators (IVSI). Peregrine - [STC ST03607NY](https://openairdocs.org/stc/ST03607NY): Installation of Honeywell RDR-7000 Weather Radar. Dassault Aircraft Services (DAS) - [STC ST04582CH](https://openairdocs.org/stc/ST04582CH): INSTALLATION OF A CENTER-WING EXTERNAL REPAIR DOUBLER IAW FAA APPROVED MDL LP5223-1002, REV. B, DTD 9/27/22 OR LATER FAA APPROVED REVISION.. BRANDIS AIRCRAFT LLC - [STC ST11285DS](https://openairdocs.org/stc/ST11285DS): An update to the existing Collins Aerospace Integrated Flight Information System (IFIS) FSU-5010 and upgrade the existing XMWR-1000 to a XMWR-1000S (Sirius XM) in Part 25.. BHE & Associates Ltd. - [STC ST04281AT](https://openairdocs.org/stc/ST04281AT): Installation for the Upgrade of the NZ-2000 FMS computer for software version NZ6.. Chippewa Aerospace Inc - [STC ST04470CH](https://openairdocs.org/stc/ST04470CH): Installation of a Honeywell RDR-7000 Weather Radar System. Honeywell International Inc - [STC ST01974WI](https://openairdocs.org/stc/ST01974WI): Installation of Aviation Clean Air Ionization System. Dassault Falcon Jet Corp - [STC ST02715SE](https://openairdocs.org/stc/ST02715SE): Installation of the Honeywell RDR-7000 Volumetric Buffer Weather Radar System. Honeywell International Inc - [STC ST01930LA](https://openairdocs.org/stc/ST01930LA): Installation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI). Sandel Avionics LLC - [STC ST04521CH](https://openairdocs.org/stc/ST04521CH): Reconfiguration of a Cabin Floor Plan in accordance with StandardAero Master Data List 1039747, Revision (B), Dated April 30, 2021 or later FAA approved revision.. StandardAero Business Aviation Services LLC - [STC ST04526CH](https://openairdocs.org/stc/ST04526CH): Installation of Thermal/Acoustic kits in accordance with Skandia Master Data List, Document Number 7803-051MDL, Revision A, dated January 5, 2021 or later FAA approved revisions.. Skandia Inc - [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc. - [STC ST02400NY-D](https://openairdocs.org/stc/ST02400NY-D): Installation of Universal Avionics Corporation MFD-640 with upgraded Honeywell EGPWS. Chicago Jet Group LLC - [STC ST04265CH](https://openairdocs.org/stc/ST04265CH): Installation of a cabin LED lighting system. Bigorre Aerospace Corporation - [STC ST548CH-D](https://openairdocs.org/stc/ST548CH-D): lnstallation of a B.F. Goodrich, GH-3000 Standby Instrument System in accordance with Garrett Aviation Services, drawing list DL548, dated November 5, 1996, no revision, or later FAA approved revision.. GARRETT AVIATION SERVICES - [STC ST03604NY](https://openairdocs.org/stc/ST03604NY): Installation of a Honeywell MCS8000 KA Band SATCOM in Dassault Aviation Mystere-Falcon 900 and Falcon 900EX airplanes. Dassault Aircraft Services (DAS) All 991: https://openairdocs.org/tcds/A46EU/stcs.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.