# TCDS A50NM: Dassault Aviation

- Type: Type certificate data sheet
- Status: Current
- Holder: Dassault Aviation
- Revision: 17
- Revised: September 5, 2026
- Product: Aircraft, Large Airplane
- Certification basis: Part 25
- Registered aircraft: 485, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/76/10/761063b32623d500e9ed9fea35f0605813b5d4369cff1f972ca0fa4fb3235072
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118850921820261005154537.0001
- Page: https://openairdocs.org/tcds/A50NM

## Models (2)

As the data sheet lists them.

- FALCON 2000EX
- FALCON 2000

## 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 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 
Revision 17 - - 1 3 - 15 8 14 14 17 13 11 12 6 6 
Page 17 18 19 20 21 22           
Revision 12 9 17 16 14 14           
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
A50NM 
Revision 17 
DASSAULT AVIATION 
FALCON 2000 
FALCON 2000EX 
 
September 5, 2026 
 
TYPE CERTIFICATE DATA SHEET No. A50NM 
 
This data sheet which is part of Type Certificate No. A50NM prescribes conditions and limitations under which the 
product for which the Type Certificate was issued meets the airworthiness requirements of the US Federal Aviation 
Regulations. 
 
Type Certificate Holder Dassault Aviation  
9 rond Point des Champs Elysées 
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 Falcon 2000 (Transport Category) approved February 2, 1995 
 
(a) Basic Model Definition 
 
Engines 2 engines. CFE Company, Model CFE 738-1-1B 
(see NOTE 3b) 
 
Engine Limits Static, Standard, Sea Level 
Take-off (5 min)5,725 lb(2,547 daN) 
 
Maximum Continuous5,560 lb (2,474,daN) 
 
Maximum Steady State Rotor Speeds 
Low pressure rotor (N1)RPM 9,400 (96.7%) 
High pressure rotor (N2) 
5 minutesRPM 28,000 (106%) 
ContinuousRPM 27,709 (104.9%)

A50NM Page 2 of 23 Rev 17 
 
Engine Limits    (cont’d) 
Turbine Interstage Temperature Limits 
Ground starting815 °C 
Air starting864 °C 
Maximum take-off (5 min)877 °C 
Maximum take-off (2 min)890 °C 
Maximum continuous861 °C 
Airstart transient (10 sec)890 °C 
Airstart transient (2 sec)1000 °C 
 
Oil Temperature 
Maximum continuous138 °C 
Minimum continuous30 °C 
Maximum transient (3 min)155 °C 
 
Fuel Pump Inlet Pressure 
Minimum5 psi above true vapor pressure 
Maximum50 psig 
 
Oil Pressure 
Idle30-85 psig 
Normal operating range60-85 psig 
Maximum transient (3 min)100 psig (may be exceeded for 2.5 min. in case of a 
cold start (temp < 0 C)) 
 
Thrust Reversers Thrust reverser use is not approved, unless Dassault Aviation change M3B has 
been incorporated. 
 
APU Allied Signal Model GTCP36-150 (F2M) 
 
Limitation 
Maximum operating starting altitude35,000 ft 
Maximum N1 (%)110 
Exhaust gas temperature, Steady 746 °C 
Exhaust gas temperature, Starting 974 °C 
Maximum oil temperature163 °C 
Minimum oil pressure35 psi 
 
Operation of the APU with passengers in the cabin and without crew member 
monitoring is not authorized. 
 
Airspeed Limits Unless otherwise stated, speeds are indicated airspeeds 
 
VMO (Maximum Operating) 
350 kt at sea level, 370 kt at 10,000 ft with straight line variation between those 
points. 
370 kt from 10,000 to 25,000 ft 
 
MMO (Maximum Operating) 
M = 0.862 from 25,000 to 38,000 ft 
0.862 at 38,000 ft, 0.85 at 42,000 ft with straight line variation between those 
points 
0.85 above 42,000 ft

A50NM Page 3 of 23 Rev 17 
 
Airspeed Limits   (cont’d) 
VA (Maneuvering)198 kt 
 
VFE (Slat and Flap Speeds) 
Slats + Flaps 10°200 kt 
Slats + Flaps 20°160 kt 
Slats + Flaps 40°160 kt 
 
VLO (Landing Gear Operation)190 kt 
 
MLO0.70 
 
VLE (Landing Gear Extended)245 kt 
 
MLE0.75 
 
VMC (Minimum Control Speed) 
Flight90 kt 
 
Windshield Wiper Operation215 kt 
 
Direct Vision Window215 kt 
 
 
CG Range 
(Gear Extended) a. Without Option M57 
Weight (lb)Forward Limit (% MAC)Rearward Limit (% MAC) 
36,00016.7      26.2 
33,00014  - 
28,660 or less14 32.5 
 
b. With Option M57 
Weight (lb)Forward Limit (% MAC)Rearward Limit (% MAC) 
36,50017.2      25.8 
33,00014  - 
28,660 or less14 32.5 
 
Straight line variation between points. 
Gear retraction has negligible effect on CG range. 
 
Datum Datum is 25% of mean aerodynamic chord (MAC) which coincides with 
fuselage station FS + 400.43 in (Fuselage station reference +0 is the fo rward end 
of the airplane nose cone). 
 
Mean Aerodynamic chord (MAC) Length113.69 in 
Zero percent MAC is at FS +372.01 in 
 
Leveling Means Standard bubble type level to be installed on the passenger seat tracks

A50NM Page 4 of 23 Rev 17 
 
Weight Limitations Without Option M57 With Option M57 
Maximum ramp36,000 lb36,500 lb 
Maximum take-off35,800 lb36,500 lb 
Maximum landing33,000 lb33,000 lb 
Maximum zero fuel28,660 lb28,660 lb 
Minimum flight 
at 14% CG23,075 lb23,075 lb 
at 32.5% CG20,100 lb20,100 lb 
 
Minimum Crew 2 - Pilot and copilot 
 
Maximum Passenger Seats 19 - limited by emergency exit requirements of Federal Aviation Regulations § 
25.807(c) 
 
0 - Without passenger provision but incorporating Dassault Ferry flight configuration : 
 M0054. 
 
Maximum Baggage Baggage compartment1,600 lb 
(not to exceed 61.4 lb per sq ft) 
 
Fuel Capacity Nominal - Refer to weight and balance report of each airplane for exact capacity 
Refer to NOTE 1(b) for data on unusable system fuel and oil 
 
Usable FuelUS GallonsPoundsArm (in) 
LH outboard wing348.42,334 22.64 
LH inboard wing213.7 1,432-27.68 
LH center wing box216.91,453-37.76 
LH Feeder tank127851-16.34 
RH outboard349.22,340 22.64 
RH inboard wing214.11,435-27.68 
RH center wing box217.41,457 -37.76 
RH feeder tank127.3853-57.87 
Total Usable1,814.012,155 
Total Fuel1830.312,259 
 
Fuels Fuels conforming to General Electric specification No. D50TF2, current 
revision 
See NOTE 4 for fuel additives 
The above mentioned fuels and additives are also suitable for the APU 
 
Pressure Fueling Maximum50 psi 
 
Oil Capacity Refer to NOTE 1(b) for data on unusable system fuel and oil 
(each engine) Usable0.55 US gallon 
Total1.25 US gallon 
 
Oils Oil conforming to General Electric Specification No. D50TR1, or Allied Signal 
oil Specification EMS 53110, current revision 
See NOTE 5 
 
Maximum Operating Altitude 47,000 ft 
 
Control Surface Movements ElevatorDown 16°Up 20° 
RudderRight 29°Left 29° 
AileronUp 25°20´Down 24°50´ 
FlapsDown 40°

A50NM Page 5 of 23 Rev 17 
 
 
Control Surface Movements  (cont’d) 
 
AirbrakesInboard up 68° 
Center up 50° 
Outboards up 37° 
Wing slatsDown 30° 
StabilizerElectrical stops AND 2°ANU 10° 
Mechanical stopsAND Max 2°30´ANU Max 10°30´ 
Structural stopsAND Min 2°40´ANU Min 11° 
Rigging tolerances are included in Maintenance Manual 
 
 
II. Model FALCON 2000EX (Transport Category Airplane) approved March 21, 2003  
 
(a) Basic Model Definition 
 
The Falcon 2000EX is defined by Dassault modification M1802 and differs from the Falcon 2000 in the following 
major respects: (i) Pratt &Whitney Canada Engines PW308C replace CFE 738 -1-1B engines; (ii) New forward and 
aft fuel tanks are added, (iii) New main and nose landing gear, (iv) New tires  and brakes 
 
Engines 2 engines. (PRATT & WHITNEY Canada) Model PW308C Turbofan  
(see NOTE 3b) 
 
Engine Limits Static, Standard, Sea Level 
Take-off (5 min)6,998 lb(3,114 daN) 
 
Maximum Continuous6,998 lb (3,114 daN) 
 
Maximum Steady State Rotor Speeds 
Low pressure rotor (N1)RPM 10,660 (102.5%) 
High pressure rotor (N2)RPM 27,316 (102%) 
 
Turbine Interstage Temperature Limits 
Ground start950 °C 
Air start950 °C 
Normal Takeoff (5 min.)860 °C 
Maximum take-off (5 min)875 °C 
Maximum continuous860 °C 
Restarting Max. (air start/ground start)500 °C/ 340 °C 
Transient (20 sec)885 °C 
 
Oil Temperature 
Maximum135 °C 
Minimum takeoff/ in-flight27 °C/ 16 °C 
Maximum transient (90 sec.)143 °C 
Starting (minimum)-40 °C 
 
Fuel Pump Inlet Pressure 
Minimum(SEE ENGINE INSTALLATON 
MANUAL) 
Maximum(SEE ENGINE INSTALLATION 
MANUAL) 
 
 
Engine Limits  (cont’d)

A50NM Page 6 of 23 Rev 17 
 
 
Oil Pressure 
Operating Range36 to 100 psi 
Minimum at Idle20 psi 
Transient (20 sec.)0 to 220 psi 
Transient (90 sec.)10 to 220 psi 
Cold start:  during starting240 psi 
 
Thrust Reversers Thrust reverser use is approved only on the ground. 
 
APU Allied Signal Model GTCP36-150 (F2M) 
 
Limitation 
Maximum operating/starting altitude35,000 ft 
Maximum N1 (%)110 
Exhaust gas temperature, Steady 746 °C 
Exhaust gas temperature, Starting 974 °C 
Maximum oil temperature163 °C 
Minimum oil pressure35 psi 
 
Operation of the APU with passengers in the cabin and without crew member 
monitoring is not authorized. 
 
Airspeed Limits Unless otherwise stated, speeds are indicated airspeeds 
 
VMO (Maximum Operating): 
350 kt at sea level, 370 kt at 10,000 ft with straight line variation between those 
points. 
370 kt from 10,000 to 25,000 ft 
 
MMO (Maximum Operating): 
0.862 from 25,000 to 38,000 ft 
0.862 at 38,000 ft, 0.85 at 42,000 ft with straight line variation between those 
points 
0.85 above 42,000 ft 
 
VA (Maneuvering)198 kt 
 
VFE (Slat and Flap Speeds) 
Slats + Flaps 10°200 kt 
Slats + Flaps 20°190 kt 
Slats + Flaps 40°180 kt 
 
VLO (Landing Gear Operation)190 kt 
 
MLO0.70 
 
VLE (Landing Gear Extended)245 kt 
 
MLE0.75 
 
 
 
Airspeed Limits   (cont’d) 
VMC (Minimum Control Speed) 
Flight90 kt

A50NM Page 7 of 23 Rev 17 
 
 
Windshield Wiper Operation215 kt 
 
Direct Vision Window Opening215 kt 
 
CG Range 
(Gear Extended) Weight (lb)Forward Limit (% MAC)Rearward Limit (% MAC) 
40,90015.723.4 
38,30014 26.0 
28,660 or less14 32.5 
 
Straight line variation between points. 
Gear retraction has negligible effect on CG range. 
 
Datum Datum is 25% of mean aerodynamic chord (MAC) which coincides with 
fuselage station FS + 400.43 in (Fuselage station reference +0 is the forward end 
of the airplane nose cone). 
 
Mean Aerodynamic chord (MAC) Length113.69 in 
Zero percent MAC is at FS +372.01 in 
 
Leveling Means Standard bubble type level to be installed on the passenger seat tracks 
 
Weight Limitations Without M1826 (serial no.1 only)      with M1826       with M1826 and M1842  
(Maximums) Taxi and Ramp   40,900 lb                     41,500 lb                  42,400 lb 
Take-off             40,700 lb                     41,300 lb                  42,200 lb 
Landing              38,300 lb                     39,300 lb                  39,300 lb 
Zero fuel            29,700 lb                      29,700 lb                 29,700 lb 
Minimum flight 
at 14% CG23,444 lb23,444 lb 
at 32.5% CG21,149 lb21,149 lb 
 
Minimum Crew 2 - Pilot and copilot 
 
Maximum Passenger Seats 19 - limited by emergency exit requirements of Federal Aviation Regulations § 
25.807(c) 
 
Maximum Baggage Baggage compartment1,600 lb 
(not to exceed 61.4 lb per sq ft) 
 
Fuel Capacity Nominal - Refer to weight and balance report of each airplane for exact capacity 
Refer to NOTE 1(b) for data on unusable system fuel and oil 
 
Without M1826 applied (serial no. 1 only) 
 
Usable FuelUS GallonsPounds 
LH wing+1/2 center wing box9116,105 
RH wing+1/2 center wing box9116,105 
Rear Tank2441,630 
Front Tank3292,205 
Total Usable2,39516,045 
Total Fuel2,40716,127 
Fuel Capacity   (cont’d) 
With M1826 applied (serial no. 2 and on) 
 
Usable FuelUS GallonsPounds

A50NM Page 8 of 23 Rev 17 
 
LH wing+1/2 center wing box9096,092 
RH wing+1/2 center wing box9126,112 
Rear Tank2931,962 
Front Tank3832,564 
Total Usable2,49716,730 
Total Fuel2,50916,812 
 
 
Fuels Fuels and additives conforming with the specifications listed in the applicable 
P&WC Maintenance Manual are approved. 
See NOTE 4 for fuel additives. 
The above mentioned fuels and additives are also suitable for the APU 
 
Fuel anti-icing must be used for fuel temperature below –50 °C 
 
Pressure Fueling Maximum50 psi 
 
Oil Capacity Refer to NOTE 1(b) for data on unusable system fuel and oil 
(each engine) Usable0.49 US gallon 
Total2.4  US gallon 
 
Oils Oils conforming to the Specifications listed in the applicable P&WC 
Maintenance Manual (P/N 30C3882) are approved 
 
Maximum Operating Altitude 47,000 ft 
 
Control Surface Movements ElevatorDown 16°Up 20° 
RudderRight 29°Left 29° 
AileronUp 25°20´Down 24°50´ 
FlapsDown 40° 
AirbrakesInboard up 68° 
Center up 50° 
Outboards up 37° 
Wing slatsDown 30° 
StabilizerElectrical stops AND 2°ANU 10° 
Mechanical stopsAND Max 2°30´ANU Max 10°30´ 
Structural stopsAND Min 2°40´ANU Min 11° 
Rigging tolerances are included in Maintenance Manual 
 
(b) Falcon 2000EX EASy Definition (Approved June 21, 2004) 
 
EASy designation for Falcon 2000EX does not correspond to a model designation.  This is only a commercial 
designation for airplanes on which Major modification numbers M1691, M1745, and M1504 have been embodied. 
 
Major Change Modification number M1691 to the Falcon 2000EX 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 
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. 
 
M1745 installs an “Oxygen system electro-pneumatic altimetric controller" 
 
M1504 installs an "All falcon Common pressurization system" 
 
M1691, M1745, and M1504 are basic on all Falcon 2000EX aircraft serial numbers 6, 28 and subsequent.

A50NM Page 9 of 23 Rev 17 
 
All parameters listed in the preceding sub-section (a) for the basic Falcon 2000EX remain valid for airplanes which incorporate 
M1691, M1745 and M1504. 
 
(c) Falcon 2000DX Definition (Approved October 3, 2007) 
 
The DX definition of the Falcon 2000EX does not correspond to a model designation.  The Falcon 2000DX is only a commercial 
designation for Falcon 2000EX airplanes in the EASy configuration on which modifications M3000 and M3001 are installed at 
production.  Modification M3000 defines the airplane and reduces the fuel tank capacity.  Modification M3001 installs a new fuel 
quantity indication system. 
 
M3000 and M3001 are basic on all Falcon 2000EX airplanes in the EASy configuration starting with serial number 601 and 
subsequent. 
 
All parameters listed in the preceding sub-section (b) above for the Falcon 2000EX EASy remain valid for airplanes which 
incorporate M3000 and M3001, except for the following weight limits and useable fuel. 
 
Falcon 2000DX Weight (lb) 
Maximum landing weight 
Maximum takeoff weight 
Maximum taxi and ramp weight 
39 300 
41 000 
41 200 
 
Useable fuel 
Front Tank  189 US Gallons 1,268 lbs 
Rear Tank   183 US Gallons1,224 lbs 
 
(d) Falcon 2000LX Definition (Approved April 29, 2009) 
 
The LX definition of the Falcon 2000EX does not correspond to a model designation.  The Falcon 2000LX is only a commercial 
designation for Falcon 2000EX airplanes in the EASy configuration on which modifications M2846 and M3229 are installed.  
Modification M2846 incorporates winglets on the airplane and M3229 installs new slats. 
Major 
All parameters listed in the preceding sub-section (c) above for the Falcon 2000EX EASy remain valid for airplanes which 
incorporate M2846 and M3229, except for the following weight limits. 
 
Falcon 2000LX Without M3390 With M3390 
 Weight (lb) 
Maximum landing weight 
Maximum takeoff weight 
Maximum taxi and ramp weight 
39 300 
42 200 
42 400 
39 300 
42 800 
43 000 
 
 
(e) Falcon 2000LXS Definition (Approved March 25, 2013) 
 
The LXS definition of the Falcon 2000EX does not correspond to a model designation.  The Falcon 2000LXS is only a 
commercial designation for Falcon 2000EX airplanes in the EASy configuration on which modifications M2846, M3229, 
M3254, M3390, M3453, and M5000 are installed at production.  Modification M2846 installs winglets, M3254 incorporates the 
EASy Phase II, M3390, incorporates a weight and balance envelope increase for take-off, M3453 incorporates new FADEC 
software V9.03 for the PW308C engines and M5000 incorporates movable inboard leading edge slats. 
 
All parameters listed in the preceding sub-section (d) above for the Falcon 2000LX remain valid for airplanes which 
incorporate modification M5000, except for the following weight limits. 
 
 
 
Falcon 2000LXS Weight (lb) 
Maximum zero fuel weight 31 200

A50NM Page 10 of 23 Rev 17 
 
(f) Falcon 2000S Definition (Approved March 25, 2013) 
 
The S definition of the Falcon 2000EX does not correspond to a model designation.  The Falcon 2000S is only a 
commercial designation for Falcon 2000EX airplanes in the LXS configuration on which modifications M3000, 
M3001, and M5001 are installed at production.  Modification M5001 incorporates movable inboard leading edge 
slats. 
 
All parameters listed in the preceding sub-section (c) above for the Falcon 2000DX remain valid for airplanes which 
incorporate modifications M3000, M3001 and M5001, except for the following weight limits. 
 
Falcon 2000S Without M5031 With M5031 
 Weight (lb) 
Maximum takeoff weight 
Maximum taxi and ramp weight 
41 000 
41 200 
42 800 
43 000 
 
 
Data Pertinent to all Models 
 
Manufacturer Serial Number Eligible 
A French "Certificat de Navigabilité pour Exportation" endorsed as noted under 
"Import Requirements" must be submitted for each individual aircraft for which 
application for US certification is made. 
 
Serial Numbers: 
For FALCON 2000: Aircraft serial number 1 and up 
  
For FALCON 2000EX: Aircraft serial number 1 through 5 and 7 through 27.  
Serial numbers 6 and  28 through 217 include M1691, M1745, and M1504 as 
standard (F2000EX EASy definition).  Aircraft serial numbers 601 through 700 
include M3000 and M3001 as standard (F2000DX definition).  Aircraft serial 
numbers 218 through 262 include M2846 and M3229 (F2000LX definition).  
Aircraft serial number 263 and subsequent includes M2846, M3229, M3254, 
M3390, M3453, and M5000.  Aircraft serial numbers 701 and subsequent 
include M3000, M3001, and M5001. 
 
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 FALCON 2000 (basic model): 
 
1. FAR, Part 25 as amended by Amendment 25-1 through 25-69. 
In addition, Dassault Aviation has elected to comply with amendments 25 -71 for 
§ 25.365(e), 25-72 for §§ 25.783(g) and 25.177; 25-75 for § 25.729(e);  
25-79 for § 25.811(e)(2) and 25-80 for § 25.1316 
 
2. FAR Part 34, original issue (Fuel Venting and Exhaust Emissions) 
 
3. FAA, Part 36 as amended by amendment 36-1 through 36-20 
 
4. FAA, Special Conditions:

A50NM Page 11 of 23 Rev 17 
 
25-ANM-90 - High Altitude Operation 
25-ANM-91 - High -Intensity Radiated Fields 
25-ANM-94 - Automatic Takeoff Thrust Control System 
25‐713‐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. 7104A (for side facing sofa) 
 
For precision approach and landings, the applicable technical requirements are 
complemented by FAA Advisory Circulars (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. 
 
Equivalent safety findings exist with respect to the following requirements:  
•Design gust criteria, (refer to Issue Paper (IP) A-5) 
•Use of the 1-g stall speeds instead of minimum speed in the stall as a basis for 
determining compliance (refer to IP F-1) 
•Rejected take-off and landing performance (refer to IP F-3) 
•N2 Digital Indication (refer to IP P-10) 
•Flight Critical Thrust Reverser Certification (refer to IP P-7) 
 
Compliance has been shown to the following optional requirement: 
•Ditching, FAR § 25.801 
•Ice Protection FAR § 25.1419 
 
For Falcon 2000 airplanes incorporating modification M-OPT0413 (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 
AT20300IB-T-ESF-B25.251-01) 
 
Type Certificate A50NM issued February 2, 1995 
Reference date for type certification: November 30, 1989 
 
(b) For Falcon 2000EX 
 
(1) For parts of the airplane not changed or not affected by the modifications: 
        
Unchanged from basic Falcon 2000 
 
(2) For those parts of the airplane that are changed or are affected by the  
 modifications M1802, M1803, M1804, M1805: 
 
The following sections of 14 CFR 25 as amended by amendments 25 -1 through 
25-98 apply per the FAA derivative aircraft process FAA Order 8110.4B to the 
changes and areas affected by the changes for the Falcon 2000EX: 
 
Subpart B – Flight: 
 
All the paragraphs are applicable at amendment 25-98 except the following 
which are applicable as modified in Equivalent Level of Safety Finding Issue

A50NM Page 12 of 23 Rev 17 
 
Paper F-4 titled “Use of 1-g Stall Speeds Instead of Minimum Speed in the Stall 
as a Basis for Determining Compliance” 
 
25.103, 25.107, 25.111, 25.119, 25.121, 25.125, 25.143, 25.145, 25.147, 25.149, 
25.161, 25.175, 25.177, 25.181, 25.201, 25.207, 25.231, 25.233, 25.237 
 
Subpart C – Structure: 
 
All the paragraphs are applicable at amendment 25-98 
 
Subpart D – Design and Construction: 
 
The following paragraphs are applicable at amendment 25-98: 
 
25.601 to 25.703, 25.721, 25.723, 25.729, 25.801, 25.863 to 25.869 
 
The following paragraphs are applicable as modified by Equivalent Level of 
Safety Issue Paper F-4 titled “Use of 1-g Stall Speeds Instead of Minimum 
Speed in the Stall as a Basis for Determining Compliance”: 
 
25.735, 25.773 
 
Subpart E – Powerplant: 
 
All the paragraphs are applicable at amendment 25-98 except the following 
which is applicable as modified in Equivalent Level of Safety Finding Issue 
Paper F-4 titled “Use of 1-g Stall Speeds Instead of Minimum Speed in the Stall 
as a Basis for Determining Compliance” 
 
25.1001 
 
Subpart F – Equipment: 
 
The following paragraphs are applicable at amendment 25-98: 
 
25.1301, 25.1305 to 25.1322, 25.1337, 25.1431 
 
The following paragraphs are applicable as modified by Equivalent Level of 
Safety Issue Paper F-4 titled “Use of 1-g Stall Speeds Instead of Minimum 
Speed in the Stall as a Basis for Determining Compliance”: 
 
25.1323, 25.1325, 25.1587 
 
Subpart G – Operating Limitations and Information: 
 
All the paragraphs are applicable at amendment 25-98 except the following: 
 
25.1515, 25.1522, 25.1523, 25.1525, 25.1529, 25.1531, 25.1547, 25.1561  
 
(3) FAR Part 34, original issue (Fuel Venting and Exhaust Emissions) 
 
(4) FAA, Part 36 as amended by amendment 36-1 through 36-24 
 
(5) FAA, Special Conditions: 
25-ANM-90 - High Altitude Operation 
25-ANM-91 - High -Intensity Radiated Fields

A50NM Page 13 of 23 Rev 17 
 
25-ANM-94 - Automatic Takeoff Thrust Control System 
25‐713‐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. 
 
(6) FAA Exemption No. 8007A (for side facing sofa) 
 
(7) Equivalent safety findings according to 14 CFR 21.21(b)(1) for the following 
subjects: 
 
•§ 25.103 & related paragraphs, 1-G Stall Speeds (documented in TAD ELOS 
Memo AT0021IB-T-F-4) 
•Section 933(a)(1)(ii):  Reversing Systems (documented in TAD ELOS Memo 
AT0012IB-T-P-12) 
•§ 25.1203(a) Fire Detector System (documented in TAD ELOS Memo 
AT0021IB-T-P-15) 
•§§ 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) 
 
(8) Miscellaneous: 
For precision approach and landings, the applicable technical requirements 
are complemented by FAA Advisory Circulars (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 January 7, 
2000. 
 
(c) For FALCON 2000EX airplanes incorporating Dassault modifications M1691, 
M1745, and M1504 (Falcon 2000EX EASy definition): 
 
(1) For parts of the airplane not changed or not affected by the modifications: 
Unchanged from basic Falcon 2000EX 
 
(2) For those parts of the airplane that are changed or are affected by the 
modifications M1691, M1745, and M1504: 
 
The following sections of 14 CFR 25 as amended by amendments 25 -1 through 
25-98 apply per the FAA derivative aircraft process FAA Order 8110.4B to the 
changes and areas affected by the changes for the Falcon 2000EX EASy 
definition: 
 
Subpart B – Flight: 
 
25.207 : « Stall warning » 
 
Subpart C – Structure: 
 
25.581 : « Lightning protection» 
 
Subpart D – Design and Construction:

A50NM Page 14 of 23 Rev 17 
 
25.601 : « General » 
25.611 : « Accessibility provisions » 
25.631 : « Bird strike damage » 
25.671(b)(c) : « Control systems : general » 
25.672 : « Stability augmentation and automatic and power-operated systems » 
25.677(b) : « Trim systems » 
25.699 : « Lift and drag device indicator » 
25.703 : « Take-Off warning systems » 
25.729(e) : « Retracting mechanism » 
25.771 (a) (c) (e) : « Pilot compartment » 
25.773(a)(d) : « Pilot compartment view » 
25.777 (a)(b)(c)(d)(e)(f) : « Cockpit controls » 
25.783(e) : « Doors » 
25.789(a) : “Retention of items of mass in passenger and crew compartments 
and galleys” 
25.791(a)(b) : “ Passenger information signs and placards” 
25.812(f) : “Emergency lighting” 
25.841(b)(5)(b)(6) : « Pressurised cabins » 
25.863(c) : « Flammable fluid fire protection » 
25.869(a) : « Fire protection : systems » 
 
Subpart E – Powerplant: 
 
25.901 (c) : « Installation » 
25.903 (b) and (d)(2) : « Engines » 
25.1141(a) and (f) : « Powerplant controls- General» 
25.1143(a), (b) and (c) : « Engine controls» 
25.1145(a)(b) : « Ignition switches » 
25.1155 : « Reverse thrust and propeller pitch settings below the flight regime» 
25.1189(f) : « Shutoff means» 
25.1203 (b)(2)(b)(3)(d) : « Fire-detector system » 
Subpart F – Equipment: 
 
25.1301 : « Function and Installations » 
25.1303 : « Flight and Navigation Instruments » 
25.1305 : « Powerplant Instruments » 
25.1307(c)(d)(e) : « Miscellaneous equipments » 
25.1309 : « Equipment, systems and installations » 
25.1316 : « System lightning protection » 
25.1321 : « Arrangement and visibility » 
25.1322 : « Warning, Caution and advisory lights » 
25.1323 : « Airspeed indicating system » 
25.1325(a)(c)(d)(e)(f)(g) : « Static pressure systems » 
25.1326 : « Pitot heat indication systems » 
25.1327 : « Magnetic direction indicator » 
25.1329 : « Automatic pilot system » 
25.1331 : « Instruments using a power supply » 
25.1333 : « Instrument systems » 
25.1335 : « Flight director systems » 
25.1337(b)(d) : « Powerplant instruments » 
25.1351 : « Electrical Systems and Equipment - General » 
25.1353 : « Electrical equipment and installations » 
25.1355 : « Distribution system » 
25.1357 : « Circuit protective devices » 
25.1381 : « Instrument lights » 
25.1419(c) : « Ice protection »

A50NM Page 15 of 23 Rev 17 
 
25.1431 : « Electronic equipment » 
25.1435 (a)(2) : « Hydraulic systems »  
25.1457 : « Cockpit voice recorders » 
25.1459 : « Flight recorders » 
 
Subpart G – Operating Limitations and Information: 
 
25.1501(b)(c) : « General » 
25.1523 : « Minimum flight crew » 
25.1529 : « Instructions for continued airworthiness » 
25.1541 : « Markings and placards - General » 
25.1543(b) : « Instrument markings : General » 
25.1545 : « Airspeed limitation information » 
25.1547 : “Magnetic direction indicator” 
25.1549 : « Powerplant instruments » 
25.1551 : « Oil quantity indicator » 
25.1553 : « Fuel quantity indicator » 
25.1555 : « Control markings» 
25.1563 : « Airspeed placard » 
25.1581 : « Airplane flight manual – General » 
25.1585(a)(b)(d)(e) : « Operating procedures » 
 
 
Special Conditions 
25‐713‐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. 
 
(d) For FALCON 2000EX EASy airplanes incorporating Dassault modifications 
M3000 and M3001 (Falcon 2000DX definition): 
 
See (c) above. 
 
(e) For FALCON 2000EX EASy airplanes incorporating Dassault modification 
M2846 and M3229 (Falcon 2000LX definition): 
 
(1) For parts of the airplane not changed or not affected by the modifications: 
Unchanged from basic Falcon 2000EX EASy 
 
(2) For those parts of the airplane that are changed or are affected by the 
modification M2846: 
 
Based on the application date of September 14, 2006, for Modification M2846, under the 
provisions of Federal Aviation Regulation 14 CFR 21.101, the applicable type 
certification standards for the modification to the Model Falcon 2000EX series are as 
follows: 
 
14 CFR part 25, effective February 1, 1965, including Amendments 25-1 through 25-117.  
The following are the applicable regulations: 
 
Subpart A – General 
25.1Applicability. 
25.2Special retroactive requirements. 
 
Subpart B – Flight 
25.21Proof of compliance. 
25.23Load distribution limits. 
25.25Weight limits.

A50NM Page 16 of 23 Rev 17 
 
25.27Center of gravity limits. 
25.29Empty weight and corresponding center of gravity. 
25.31Removable ballast. 
25.101General. 
25.103Stall speed. 
25.105Takeoff. 
25.107Takeoff speeds. 
25.109Accelerate-stop distance. 
25.111Takeoff path. 
25.113Takeoff distance and takeoff run. 
25.115Takeoff flight path. 
25.117Climb: general. 
25.119Landing climb: All-engines-operative. 
25.121Climb: One-engine-inoperative. 
25.123En route flight paths. 
25.125Landing. 
25.143General. 
25.145Longitudinal control. 
25.147Directional and lateral control. 
25.149Minimum control speed. 
25.161Trim. 
25.171General. 
25.173Static longitudinal stability. 
25.175Demonstration of static longitudinal stability. 
25.177Static lateral-directional stability. 
25.181Dynamic stability. 
25.201Stall demonstration. 
25.203Stall characteristics. 
25.207Stall warning. 
25.237Wind velocities. 
25.251Vibration and buffeting. 
25.253High-speed characteristics. 
25.255Out-of-trim characteristics. 
 
Subpart C – Structure 
25.301Loads. 
25.303Factor of safety. 
25.305Strength and deformation. 
25.307Proof of structure. 
25.321General. 
25.331Symmetric maneuvering conditions. 
25.333Flight maneuvering envelope. 
25.335Design airspeeds. 
25.337Limit maneuvering load factors. 
25.341Gust and turbulence loads. 
25.343Design fuel and oil loads. 
25.345High lift devices. 
25.349Rolling conditions. 
25.351Yaw maneuver conditions. 
25.367Unsymmetrical loads due to engine failure. 
25.373Speed control devices. 
25.391Control surface loads: General. (d)(e) 
25.395Control system. 
25.427Unsymmetrical loads. 
25.445Auxiliary aerodynamic surfaces. (a) 
25.457Wing flaps. 
25.459Special devices. 
25.471General. (a)(b) 
25.473Landing load conditions and assumptions. (a)(b)(c)(e) 
25.479Level landing conditions. 
25.493Braked roll conditions. 
25.495Turning.

A50NM Page 17 of 23 Rev 17 
 
25.519Jacking and tie down provisions. (c) 
25.571Damage-tolerance and fatigue evaluation of structure. (a)(b)(e) 
25.581Lightning protection. 
 
Subpart D – Design and Construction 
25.601General. 
25.603Materials. 
25.605Fabrication methods. 
25.607Fasteners. 
25.609Protection of structure.  
25.611Accessibility provisions. 
25.613Material strength properties and material design values. 
25.619Special factors. 
25.621Casting factors. 
25.623Bearing factors. 
25.625Fitting factors. 
25.629Aeroelastic stability requirements. 
25.651Proof of strength. 
25.672Stability augmentation and automatic and power-operated systems. 
25.703Takeoff warning system. 
25.863Flammable fluid fire protection. (a)(b) 
25.869Fire protection: systems. (a)(4) 
 
Subpart E – Powerplant 
25.954Fuel system lightning protection. 
25.981Fuel Tank Ignition Prevention  (a)(b) 
25.1011 Oil Systems;General (b) 
 
Subpart F – Equipment 
25.1301Function and installation. 
25.1309Equipment, systems, and installations. 
25.1316System lightning protection. 
25.1327Magnetic direction indicator. 
25.1329Automatic pilot system. 
25.1351General. (a)(d) 
25.1353Electrical equipment and installations. (a)(b)(d) 
25.1357Circuit protective devices. (a) 
25.1385Position light system installation. 
25.1387Position light system dihedral angles. 
25.1389Position light distribution and intensities. 
25.1391 Minimum intensities in the horizontal plane of forward and rear position 
lights. 
25.1393Minimum intensities in any vertical plane of forward and rear position lights. 
25.1395Maximum intensities in overlapping beams of forward and rear position lights. 
25.1397Color specifications. 
25.1401Anticollision light system. 
25.1419Ice protection. (introduction paragraph only) 
25.1431Electronic equipment. (a)(c)(d) 
25.1443Minimum mass flow of supplement oxygen. (b)(c) 
 
Subpart G – Operating Limitations and Information 
25.1501General (b) 
25.1503Airspeed limitations: general. 
25.1505Maximum operating limit speed. 
25.1507Maneuvering speed. 
25.1511Flap extended speed. 
25.1513Minimum control speed. 
25.1515Landing gear speeds. 
25.1517Rough air speed, VRA. 
25.1519Weight, center of gravity, and weight distribution. 
25.1527Ambient air temperature and operating altitude. 
25.1529Instructions for Continued Airworthiness.

A50NM Page 18 of 23 Rev 17 
 
25.1531Maneuvering flight load factors. 
25.1533Additional operating limitations. 
25.1581General. 
25.1583Operating limitations. 
25.1585Operating procedures. 
25.1587Performance information. 
Appendix A(Sec 25.1) 
Appendix C(Sec 25.1) 
Appendix G(Sec 25.1) 
Appendix H(Sec 25.1) 
Appendix H(Sec 25.2) 
Appendix H(Sec 25.3) 
Appendix H(Sec 25.4) 
 
(3)  Special conditions:  The following Special Conditions are applicable to Modification 
M2846: 
 
a.Docket No. NM-100; Special Conditions No. 25-ANM-90 Dassault Aviation Model 
Falcon 2000 Airplane; High Altitude Operation.  
 
b.Docket No. NM-101; Special Conditions No. 25-ANM-91 Dassault Aviation Model 
Falcon 2000 Airplane; High Intensity Radiated Fields. 
 
c.Docket No. FAA-2017-1143; Special Conditions No. 25-713-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. 
 
(4)  Equivalent Safety Findings:  According to the provisions of 14 CFR 21.21(b)(1), 
the following subject has been identified as an equivalent safety findings. 
 
a.  Section 25.1419 – Ice Protection (documented in TAD ELOS Memo 
TD0592IB-T-S-101) 
 
(5)  Exemptions: FAA Exemption No. 5991 (for side facing sofa). 
 
(f) For FALCON 2000EX EASy airplanes incorporating Dassault modification 
M2846, M3229, M3254, M3390, M3453, and M5000 (Falcon 2000LXS definition): 
 
(1)Airworthiness & Environmental Standards for components and areas not 
affected by the change  
 
See (e) above. 
 
(2)Airworthiness and Environmental Standards for components and areas affected 
by the change 
 
Based on the application date of November 18, 2008, for Modification M5000, under the 
provisions of Federal Aviation Regulation 14 CFR 21.101, the applicable type certification 
standards for the modification to the Model Falcon 2000EX series are as follows: 
 
14 CFR part 25, effective February 1, 1965, including Amendments 25-1 through 25-125, 
except for the sections which are complied with as amended through the indicated 
Amendments:  
 
a)  14 CFR part 25 paragraphs at Amendment 125 
25.21 to 25.27, 25.31, 25.101, 25.109, 25.113 to 25.117, 25.145 to 25.203, 25.231 to 235, 
251(e), 25.301 to 25.351, 25.367, 25.391(d),(e), 25.393 to 25.397, 25.409 to 25.427, 
25.457 to 25.495, 25.499, 25.507 to 25.519, 25.561 to 25.625, 25.631, 25.651, 25.657, 
25.671, 25.675, 25.685, 25.693 to 25.701, 25.801, 25.863(a),(d), 25.1316, 25.1333, 
25.1501, 25.1519, 25.1533, 25.1581, 25.1583(a),(c), 1585(a),(c),(d), 25.1587(b)

A50NM Page 19 of 23 Rev 17 
 
b)  14 CFR part 25 paragraphs at Amendment 122 
25.1701 to 25.1731 (i.e. before EWIS implementation)  
 
c)  14 CFR part 25 paragraphs at Amendment 120 
25.21(g), 25.103, 25.105, 25.107, 25.111, 25.119, 25.121, 25.123, 25.125, 25.143, 25.207, 
25.237, 25.253, 25.1419  
d)14 CFR part 25 paragraphs at Amendment 108 
25.735  
 
e)  14 CFR part 25 paragraphs at Amendment 98: 
25.503, 25.655, 25.672, 25.677 to 25.683, 25.689, 25.703, 25.721, 25.729, 25.771, 25.773, 
25.777, 25.783, 25.789, 25.791, 25.841, 25.865, 25.867, 25.899 to 25.1182, 25.1185 to 
25.1315, 25.1321 to 25.1357, 25.1360, 25.1363, 25.1365, 25.1381, 25.1423 to 25.1431, 
25.1435, 25.1457, 25.1459, 25.1529 
 
f)  14 CFR part 25 paragraphs at Amendment 79: 
25.811(e)(2)  
 
g)  14 CFR part 25 paragraphs at Amendment 69:  
25.725, 25.727, 25.731, 25.733, 25.772, 25.779, 25.781, 25.785, 25.787, 25.793, 25.795, 
25.803,25.805, 25.807, 25.809 to 25.820 (except 25.811(e)(2)), 25.832, 25.831, 25.833, 
25.843 to 25.859, 25.871, 25.875, 25.1362, 25.1383 to 25.1403, 25.1411, 25.1413, 
25.1415, 25.1421, 25.1433, 25.1436 to 25.1450, 25.1453, 25.1455, 25.1461  
 
h)  14 CFR part 25 paragraphs at Amendment 144 
25.733(e): « Pilot compartment view »  For FalconEye System Installations 
 
 
SSDs / SRDs and NSSDs / NSRDs are identified in the F2000EX M5000 CPR analysis 
DGT 118921.  
 
3) Special Conditions 
 
Special Conditions No. 25-713-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.. 
 
4) Equivalent Safety Findings 
 
No new equivalent safety findings (existing equivalent safety findings for unchanged 
airplane still apply). 
 
5) Exemptions 
 
No new exemptions (existing exemptions for unchanged airplane still apply). 
 
 
6) Optional Design Regulations 
 
The follow approvals are unaffected by the modification:  
 
Ditching §§ 25.801, 25.1411(d), (e), (f), (g) & 25.1415  
Ice Protection § 25.1419  
 
7) Noise Standards 
 
14 CFR part 36 at Amdt 28 
 
8) Fuel Venting and Exhaust Emissions Standards 
 
14 CFR Part 38, Airplane Fuel Efficiency Certification, Amendment 38-1, Paragraph 
38.17(b)(X).

A50NM Page 20 of 23 Rev 17 
 
 
9) 14 CFR 26 
 
No Impact 
 
(g) For FALCON 2000EX EASy airplanes incorporating Dassault modification 
M3000, M3001 and M5001 (Falcon 2000S definition): 
 
See (f) above. 
 
(h) For FALCON 2000EX series airplanes incorporating M-OPT0408 (Starlink 
Antenna Provisions: 
 
See (b),(c), (d),(e), (f) and (g) 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 AT20300IB-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 185. The FAA 
validated this product under U.S. Type Certificate Number A50NM. 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 Falcon 2000, the type definition is DASSAULT AVIATION Drawing 
List 01-130 Ref. DGT 21172 Issue A 
 
For the Falcon 2000EX, the type definition is DASSAULT AVIATION 
document M1802-01-130 (DGT-F/NAV89793) – Master Drawing Lists 
 
Definition of Falcon 2000EX results of the addition of Falcon 2000 definition 
plus application of M1802, M1803, M1804, M1805, M1820, M1838 and 
M2233. 
From aircraft s/n 2 and on, modification M1826 is applied resulting in an 
increase in fuel capacity and maximum weights. 
 
Definition of the Falcon 2000EX EASy is the result of the basic Falcon 2000EX 
definition plus application of M1691, M1745, and M1504. 
 
Definition of the Falcon 2000DX is the result of the basic Falcon 2000EX in the 
EASy definition plus application of M3000 and M3001. 
 
Definition of the Falcon 2000LX is the result of the basic Falcon 2000EX in the 
EASy definition plus application of M2846 and M3229. 
 
 
 
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 Générale de l'Aviation Civile (DGAC) of France are contained in 
the documents:

A50NM Page 21 of 23 Rev 17 
 
For the FALCON 2000, in memos Nos.: 
 
•DTM 38-2000/90 (01-940) - Equipment list of the basic airplane 
•DTM 38-0735/91 (01-941) - Equipment list of the standard option and other 
options 
 
In addition, the aircraft must be operated in accordance with the DGAC 
approved FALCON 2000 Airplane Flight Manual, document DTM 537 
approved February 2, 1995 
 
For the FALCON 2000EX: 
 
M1802-01-940 (DGT-DTF/NAV81711) – Equipment List – Basis Aircraft 
 
In addition, the aircraft must be operated in accordance with the DGAC 
approved FALCON 2000EX Airplane Flight Manual, Document No. 
DGT84278 
 
For the Falcon 2000EX EASy: 
 
M1691-01-101 (DGT-DTF/NAV 96502) - Equipment list for F2000EX EASy 
 
In addition, the aircraft must be operated in accordance with the Falcon 2000EX 
EASy Airplane Flight Manual, document DGT88898. 
 
For the Falcon 2000LX, the aircraft must be operated in accordance with the 
Falcon 2000EX EASy Flight Manual, document DGT88898. 
 
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 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 a list of equipment included in certificated empty weight, 
and loading instructions when necessary must be provided for each aircraft at its delivery.

A50NM Page 22 of 23 Rev 17 
 
 
(b)The following must be included in the airplane empty weight: 
•The total unusable fuel, 82 lb, plus 
•The unusable engine oil, 4.1 US gallons, 34 lb, (drainable and trapped oil) at arm + 150 in, and  
•The hydraulic fluid 83 lb at are + 127 in 
 
(c) The airplane must be loaded in accordance with the FALCON 2000 Loading Manual (DTM 541) or 
the FALCON 2000EX Loading Manual (DGT 65), as applicable and the CG 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 2000 and Falcon 2000EX Maintenance Manual, a nd must 
be replaced as indicated therein. 
(b) For the Falcon 2000:  CFE 738-1-1B engine life limits, established for critical rotating components, are 
published in the approved Engine Light Maintenance Manual, Report Number 72.08.03, Airworthiness 
Limitation Section. 
For the Falcon 2000EX:  PW308C engine life limits are listed in the Airworthiness Limitation Section 
of P&WC Maintenance Manual P/N  30C3882. 
(c) Required maintenance and inspections to maintain airworthiness based on involving reliability are 
presented in DGAC approved chapter 5.40.00 of the FALCON 2000 and Falcon 2000EX Maintenance 
Manuals. 
 
Chapter 5-40 references : 
F2000 : Airworthiness Limitation Section (Chapter 5-40, reference: DGT113876) 
F2000EX : Airworthiness Limitation Section (Chapter 5-40, reference: DGT113877 
 
NOTE 4 - Fuel Specifications and Additives 
(a)For information concerning equivalent fuel specifications, see Airplane Flight Manual  
(b)Additives 
For the CFE 738 engines; PW308C engines; and GTCP 36-150 auxiliary power unit, the following 
additive limitations are approved. 
•Anti-icing additives, conforming to AIR 3652 of MIL-I 27686 D or E (JP-4/JP-8) or to MIL-I  85470 (JP-
5) or equivalent are approved for use in the fuel in amounts up to 0.15 per cent by volume. 
•SOHIO BIOBOR JF biocide additive, or equivalent, is approved for use in fuel at a concentration  not 
exceeding 270 PPM 
•Anti-static additive is approved for use in fuel at a concentration not exceeding 1 PPM for SHELL ASA 3; 
and 3 PPM for STADIS 450 
 
NOTE 5 - Qualified Oils 
(a) Engine: See CFE 738 Engine Installation Manual IM 75 550 for specific oils approved per the subject 
specification. 
(b) APU: Brand names of oils approved for use in the APU are listed in the GTCP36 -150 Maintenance 
Manual 
 
NOTE 6 - The Model Falcon 2000 (incorporating M1251), Falcon 2000EX, and Falcon 2000EX EASy have been 
approved to operate in “Reduced Vertical Separation Minimum” (RVSM) airspace when the airplanes are 
operated in accordance with Airplane Flight Manual page 1-160-1 (for F2000/2000EX) or page 1-300-05 
(for F2000EX EASy).  Continued airworthiness and operational approval aspects of RVSM must be 
constructed according to Advisory Circular (AC) 91-RVSM, titled “Approval of Aircraft and Operators 
for Flight in Airspace Above Flight Level (FL) 290 Where a 1,000 Foot Vertical Separation Minimum is 
Applied.” 
 
NOTE 7 - 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.

A50NM Page 23 of 23 Rev 17 
 
 
           ………………………………………………. END………………………………………………………
```

## ADs (92, first 50, in force first)

- [AD 2026-18-02](https://openairdocs.org/ad/2026-18-02): Time Limits/Maintenance Checks · Dassault FALCON 2000. Effective Oct 16, 2026
- [AD 2026-18-05](https://openairdocs.org/ad/2026-18-05): Time Limits/Maintenance Checks · Dassault FALCON 2000EX. Effective Oct 16, 2026
- [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 2026-07-02](https://openairdocs.org/ad/2026-07-02): Electrical power · Dassault FALCON 2000EX. Effective May 11, 2026
- [AD 2025-15-06](https://openairdocs.org/ad/2025-15-06): Navigation · Dassault FALCON 2000EX. Effective Sep 3, 2025
- [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 2023-22-12](https://openairdocs.org/ad/2023-22-12): Time Limits/Maintenance Checks · Dassault FALCON 2000. Effective Dec 27, 2023
- [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 2022-27-05](https://openairdocs.org/ad/2022-27-05): Landing gear · Dassault FALCON 2000 and FALCON 2000EX. Effective Feb 3, 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 2021-14-04](https://openairdocs.org/ad/2021-14-04): Equipment/Furnishings · Dassault Falcon 7X and FALCON 2000EX. Effective Aug 26, 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 2018-25-13](https://openairdocs.org/ad/2018-25-13): Electrical power · Dassault FALCON 2000. Effective Jan 18, 2019
- [AD 2018-19-14](https://openairdocs.org/ad/2018-19-14): Ice and Rain Protection · Dassault FALCON 2000 and FALCON 2000EX. Effective Nov 1, 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 2017-25-11](https://openairdocs.org/ad/2017-25-11): Ice and Rain Protection · Dassault FALCON 2000EX. Effective Jan 22, 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 2017-18-08](https://openairdocs.org/ad/2017-18-08): Ice and Rain Protection · Dassault FALCON 2000 and FALCON 2000EX. Effective Oct 5, 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 2015-13-08](https://openairdocs.org/ad/2015-13-08): Ice and Rain Protection · Dassault FALCON 2000EX. Effective Jun 30, 2015
- [AD 2014-25-08](https://openairdocs.org/ad/2014-25-08): Equipment/Furnishings · Dassault FALCON 2000 and FALCON 2000EX. Effective Jan 20, 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 2014-12-02](https://openairdocs.org/ad/2014-12-02): Flight Controls · Dassault FALCON 2000 and FALCON 2000EX with STC ST01987SE. Effective Aug 4, 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 2010-10-24](https://openairdocs.org/ad/2010-10-24): Landing gear · Dassault FALCON 2000 and FALCON 2000EX. Effective Jun 25, 2010
- [AD 2009-14-09](https://openairdocs.org/ad/2009-14-09): Fuselage · Dassault FALCON 2000EX. Effective Aug 12, 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 2008-22-15](https://openairdocs.org/ad/2008-22-15): Crew System Alerting (CAS) · Dassault FALCON 2000EX. Effective Dec 11, 2008
- [AD 2008-16-08](https://openairdocs.org/ad/2008-16-08): 4 Electronic Flight Instrumentation System (EFIS) · Dassault FALCON 2000EX. Effective Sep 9, 2008
- [AD 2008-13-31](https://openairdocs.org/ad/2008-13-31): Engine cowlings · Dassault FALCON 2000. Effective Aug 12, 2008
- [AD 2008-12-14](https://openairdocs.org/ad/2008-12-14): Wings' anti-ice valve · Dassault FALCON 2000EX. Effective Jul 23, 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 2008-08-20](https://openairdocs.org/ad/2008-08-20): Wing anti ice telescopic tubes · Dassault FALCON 2000. Effective May 27, 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 2007-25-10](https://openairdocs.org/ad/2007-25-10): Trailing edge flap · Dassault Falcon 900EX, FALCON 2000, FALCON 2000EX and 2 more. Effective Jan 14, 2008
- [AD 2007-12-16](https://openairdocs.org/ad/2007-12-16): Skin panels · Dassault Falcon 900EX and FALCON 2000EX. Effective Jul 19, 2007

All 92: https://openairdocs.org/tcds/A50NM/ads.md

## Registered aircraft by registry model (OpenAirDocs)

- [Dassault FALCON 2000EX](https://openairdocs.org/model/dassault-falcon-2000ex): 332 aircraft (registry codes 2730110, 2730012)
- [Dassault FALCON 2000](https://openairdocs.org/model/dassault-falcon-2000): 153 aircraft (registry code 2730170)
- [Dassault FALCON 2000LX](https://openairdocs.org/model/dassault-falcon-2000lx): 0 aircraft (registry code 2730124)

## STCs approved under this data sheet (252, 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 ST03597NY](https://openairdocs.org/stc/ST03597NY): Installation of a GoGo AVANCE L5 system in Dassault Aviation Falcon 2000EX Aircraft. Dassault Falcon Jet Corp.
- [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc.
- [STC ST03613NY](https://openairdocs.org/stc/ST03613NY): Installation of Garmin GI Standby Flight Display 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 ST03617NY](https://openairdocs.org/stc/ST03617NY): Installation of Gogo Galileo HDX System. Dassault Falcon Jet Corp.
- [STC ST04099NY](https://openairdocs.org/stc/ST04099NY): Installation of Satcom Direct Plane Simple. Delta Engineering Corporation
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS).. VisionSafe LLC
- [STC ST04610CH](https://openairdocs.org/stc/ST04610CH): Installation of SmartSky Flagship System. Apcela IFC JV, LLC dba Apcela ATG
- [STC ST03618NY](https://openairdocs.org/stc/ST03618NY): Installation of SpaceX Starlink Aviation System. Dassault Falcon Jet Corp.
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc.
- [STC ST10978SC](https://openairdocs.org/stc/ST10978SC): 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 ST11044SC](https://openairdocs.org/stc/ST11044SC): Installation of a third Rockwell Collins AHC-3000 Attitude Heading Reference System (AHRS). 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 ST01117DE](https://openairdocs.org/stc/ST01117DE): Installation of the Gogo ATG C1.. Peregrine
- [STC ST11845CH](https://openairdocs.org/stc/ST11845CH): Installation of Gogo MB13 Antennas. Premier Air Center LLC. d/b/a West Star Aviation
- [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 ST01972WI](https://openairdocs.org/stc/ST01972WI): Installation of Aviation Clean Air Ionization System. Dassault Falcon Jet Corp.
- [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 ST04726NY](https://openairdocs.org/stc/ST04726NY): Installation of Universal Insight EFIS with UNS-1Fw FMS. TAI Acquisition Corp. Dba Trimec Aviation
- [STC ST00178IB](https://openairdocs.org/stc/ST00178IB): Installation of the Galley Modification. The Bank of Nova Scotia
- [STC ST04727NY](https://openairdocs.org/stc/ST04727NY): Installation of FANS-1/A+ & CPDLC with Universal Kapture CVR. TAI Acquisition Corp. Dba Trimec Aviatio
- [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc.
- [STC ST00135IB](https://openairdocs.org/stc/ST00135IB): Relocation of Aircell Axxess Equipment, Speaker AMP, FCMS Port Controller, Data Interface Unit, WiFi and Cellular Antenna. The Bank of Nova Scotia
- [STC ST11233DS](https://openairdocs.org/stc/ST11233DS): Installation of a Mission System. L-3 Communications Integrated Systems LP
- [STC ST9769SC](https://openairdocs.org/stc/ST9769SC): Installation of provisions for a mission equipment interior and exterior antenna and radome shapes. L-3 Communications Integrated Systems L.P.
- [STC ST11286DS](https://openairdocs.org/stc/ST11286DS): To update the Communication Management Unit (CMU) and to add or update the 3rd VHF Datalink to 
support Controller Pilot Data Link Communication (CPDLC). Dassault Aircraft Services
- [STC ST01706WI](https://openairdocs.org/stc/ST01706WI): Installation of Aircell Universal Communications System (UCS). Gogo Business Aviation LLC
- [STC ST00050IB](https://openairdocs.org/stc/ST00050IB): Installation, Collins Aerospace Venue Cabin Management System and Miscellaneous Interior Modifications. Sky Service F.B.O. Inc
- [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 ST00032IB](https://openairdocs.org/stc/ST00032IB): Interior Refurbishment modification. Skyservice Business Aviation Inc.
- [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 ST04717NY](https://openairdocs.org/stc/ST04717NY): The Installation of the Cabin Management System (CMS) Venue, USB Outlet, and Coffee Maker. B/E Aerospace Limited
- [STC ST04697NY](https://openairdocs.org/stc/ST04697NY): Installation of Importation Modification (Interior and Avionics). DECA Aviation Engineering Limited
- [STC ST02397CH](https://openairdocs.org/stc/ST02397CH): Installation of GDS Aero Tail Cone APU Firewall Assembly, P/N GF2APU-FW1.. GDS Aero LLC
- [STC ST03608NY](https://openairdocs.org/stc/ST03608NY): Installation of Satcom Direct (SD) HUB 2.0 WiFi Hub and Wi-Fi antennas. Dassault Aircraft Services (DAS)
- [STC ST02779CH](https://openairdocs.org/stc/ST02779CH): Installation of dual Universal Avionics Systems Corporation UNS-1Ew Flight Management Systems. West Star Aviation Inc
- [STC ST04467CH](https://openairdocs.org/stc/ST04467CH): Installation of a Universal Avionics UL-801 Datalink System and Latitude DL150 Iridium Satellite Communication System to meet airworthiness requirements for FANS 1/A+ and ATN B1 capability in accordance with Premier Air Center LLC STC Master Data List, Doc. No. A21311L-241, Revision A, dated June 4, 2021, or later FAA-approved revision.. Premier Air Center LLC
- [STC ST04516CH](https://openairdocs.org/stc/ST04516CH): Installation of a Universal Avionics CVR-120A Cockpit Voice Recorder in accordance with Premier Air Center LLC STC Master Data List, Doc. No. A21336L-242, Revision A, dated June 3, 2021, or later FAA-approved revision.. Premier Air Center LLC
- [STC ST04639NY](https://openairdocs.org/stc/ST04639NY): Installation of Cabin Interior Modification. Flying Colours Corp
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc.
- [STC ST04062CH](https://openairdocs.org/stc/ST04062CH): Installation of Cabin LED Lighting System. Bigorre Aerospace Corporation
- [STC ST04394CH](https://openairdocs.org/stc/ST04394CH): Weather Radar Upgrade in accordance with StandardAero Master Data List 1035391, Revision (B), dated December 13, 2019 or later FAA approved revision.. Dassault Aircraft Services (DAS)
- [STC ST04469NY](https://openairdocs.org/stc/ST04469NY): Activation of DLU TrueNorth Satcom. Dassault Falcon Service
- [STC ST03595NY](https://openairdocs.org/stc/ST03595NY): Installation of Honeywell Laseref IV Upgrade. Dassault Aircraft Services (DAS)
- [STC ST02886CH-D](https://openairdocs.org/stc/ST02886CH-D): Installation of an Interior Floorplan Reconfiguration in Accordance with StandardAero Master Data List 1019035, Revision (K), dated August 13, 2020 or later FAA approved revision.. StandardAero
- [STC ST01270WI-D](https://openairdocs.org/stc/ST01270WI-D): Installation of Honeywell MK V and MK VII EGPWS Runway Awareness and Advisory System (RAAS).  This approval is limited to specifically idenitfied aircraft.. Duncan Aviation Inc

All 252: https://openairdocs.org/tcds/A50NM/stcs.md

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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.