# TCDS A59NM: Dassault Aviation

- Type: Type certificate data sheet
- Status: Current
- Holder: Dassault Aviation
- Revision: 10
- Revised: July 2, 2025
- Product: Aircraft, Large Airplane
- Certification basis: Part 25
- Registered aircraft: 167, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/36/f9/36f967dd850b1b9dc6e3eb6de5caa5d13b16d949f88ae791fd9e347b82a3ef5f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198164259720250715215005.0001
- Page: https://openairdocs.org/tcds/A59NM

## Models (1)

As the data sheet lists them.

- Falcon 7X

## 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 
Revision 10 2 6 2 8 5 2 9 10 6 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
A59NM 
Revision 10 
DASSAULT AVIATION 
FALCON 7X 
 
July 2, 2025 
 
TYPE CERTIFICATE DATA SHEET No. A59NM 
 
This data sheet which is part of Type Certificate No. A59NM 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 Marcel Dassault 
        75008 PARIS 
        FRANCE 
 
The U.S. airworthiness certification basis for aircraft type certificated under FAR Section 21.29 and exported b y 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 7X (Transport Category) approved April 27, 2007 
 
(a) Basic Model Definition 
 
Engines 3 engines. PRATT & WHITNEY CANADA Corp. - Model PW307A 
(see NOTE 3b) 
 
Engine Limits Static, Standard, Sea Level 
Take-off (5 min)      6,405 lb  (2,849 daN) 
          6,725 lb  (2,910 daN)  with M1000 
 
Maximum Continuous    6,405 lb  (2,849 daN) 
          6,725 lb  (2,910 daN)  with M1000 
 
For other limits refer to engine TC Data Sheet E00071EN or the FAA approved 
Airplane Flight Manual  
 
Thrust Reversers Engine is approved for operation with thrust reverser p/n F7XC782140020  
 
APU Honeywell Model 36-150 (FN)

A59NM Page 2 of 10 Rev 8  
 
APU Limits APU is usable for ground operation only.  
 For other limits refer to the Airplane Flight Manual 
 
Airspeed Limits Unless otherwise stated, speeds are indicated airspeeds 
 
VMO  at sea level ..................................................................  350 kts 
VMO  straight line variation up to 10,000 ft .........................  370 kts 
VMO  from 10,000 ft to 28,000 ft  ........................................  370 kts 
MMO  from 28,000 to 51,000 ft  ............................................  0.9 
 
VA  .......... maneuvering speed  ....................................................  218 kts VFE SF1  ............................................................................  200 kts 
 SF2  ............................................................................  190 kts 
 SF3 .............................................................................  180 kts 
Note :  Above 20,000 ft, do not establish, nor maintain a configuration with the 
slats and the flaps extended 
 
VLO  Landing gear operation  ..............................................  200 kts 
MLO   ....................................................................................  0,70 
VLE  Landing gear extended  ..............................................  245 kts 
MLE   ....................................................................................  0,75 
VMCA  minimum control speed in flight ................................  80 kts (CAS) 
VMCG  minimum control speed on ground  .........................  81.3 kts (CAS) 
 
Maximum Operating Altitude 51,000 ft (15,544 m)  
 
Mean Aerodynamic chord (MAC) Mean aerodynamic chord (MAC): 131.793 in (3,347.54 mm) 
And Datum Datum is 25% of mean aerodynamic chord (MAC) 479.646 in (12,183 mm) from 
the forward end of the aircraft nose cone.  501.646 in (12741 mm) with M1000 
 
Leveling Means Aircraft is leveled in the longitudinal and lateral axis by means of a plumb bob and 
target in the left main landing gear bay 
 
Weight and CG Limitations  
 Weight FWD limit Aft limit Kg lbs % MAC % MAC 
Minimum flight - Aft 
Minimum flight - Forward  
Maximum zero fuel 
Maximum landing 
Maximum for aft CG at 38.5 % 
Maximum takeoff 
Maximum ramp 
 
14,696 
15,694 
18,597 
28,304 
25,890 
31,751 
31,842 
32,400 
34,600 
41,000 
62,400 
57,076 
70,000 
70,200 
N/A 
26.0 
19.5 
19.5 
19.5 
19.05 
19.5 
38.5 
N/A 
38.5 
37.35 
38.5 
33.65 
31.5

A59NM Page 3 of 10 Rev 8
  
          With modification M1000 installed 
 
 Weight FWD limit Aft limit Kg lbs % MAC % MAC 
Minimum flight - Aft 
Minimum flight - Forward  
Maximum zero fuel 
Maximum landing 
Maximum for aft CG at 38.5 % 
Maximum takeoff 
Maximum ramp 
 
14,696 
15,694 
18,597 
28,304 
25,890 
33,112 
33,203 
32,400 
34,600 
41,000 
62,400 
57,076 
73,000 
73,200 
N/A 
26.6 
19.5 
19.5 
19.5 
19.54 
19.62 
38.5 
N/A 
38.5 
37.35 
38.5 
27.73 
27.00 
For weight and balance calculation refer to the Falcon 7X Loading Manual (DGT 
108840) / Falcon 7X-M1000 Loading Manual (DGT 147688) - (See note 1) 
 
Minimum Crew 2 - Pilot and copilot 
 
Maximum Passenger Seats 19 - limited by emergency exit requirements of Federal Aviation Regulations § 
25.807(c).   (See note 2) 
Ferry flight configuration (0 passenger provisions) is defined by Dassault modifications 
M0272 and M0163 
 
Maximum Baggage Baggage compartment:  2004 lb (909 kg), not to exceed 61.4 lb/ft2 (300 kg per 
square meter) 
 
Exits 
 Type Size 
1 Passenger door I 0.800 x 1.72 m /(31.50 x 67.72 in) 
1 Emergency exit III 0.534 x 0.916 m /(21.02 x 36.06 in) 
 
Dimensions  
   With Modification M1000 
Length 920.47 in 23.38 m 24.46 m 
Span 1031.89 in 26.21 m 26.28 m 
Height 312.20 in 7.93 m 7.93 m 
Gross wing 
area 
761.008 ft2 70.7 m² 70.7 m 
 
Fuel Capacity   Numbers in ( ) indicate capacity associated with modification M1000  
USABLE 
FUEL 
Liters kg (*) US Gallons lbs (*) 
Left circuit 5944/(6359) 4773/(5106) 1570/(1680) 10522/(11257) 
Right circuit  5944/(6383) 4773/(5126) 1570/(1686) 10522/(11301) 
Center circuit 6154/(7108) 4942/(5708) 1626/(1878) 10896/(12583) 
Total usable  18042/(19850) 14488/(15940) 4766/(5244) 31940/(35141) 
UNUSABLE 
FUEL 
    
Drainable 65/(68) 52/(54) 17/(18) 115/(120) 
Undrainable  41/(48) 33/(39) 11/(13) 72/(85)

A59NM Page 4 of 10 Rev 8  
Total 
unusable 
106/(116) 85/(93) 28/(31) 187/(205) 
 * assuming a fuel density of 0,803 kg/liter 
Oil Capacity  
 Liters kg (**) US gallons lbs (**) 
Max oil level     
Left engine 7.87 7.67 2.08 16.90 
Right engine  7.87 7.67 2.08 16.90 
Center engine 7.87 7.67 2.08 16.90 
Total 23.61 23.01 6.24 50.70 
Min oil level     
Left engine 6.23 6.07 1.64 13.38 
Right engine  6.23 6.07 1.64 13.38 
Center engine 6.23 6.07 1.64 13.38 
Total  18.69 18.21 4.92 40.14 
(*) Tank quantities do not include undrainable oil or residual oil in the 
Accessory Gearbox, oil filter bowl or air-cooled oil cooler (ACOC) 
(**)  Based on specific gravity of 0.975 
 
Approved Fuel, oils and additives : 
 Refer to the Airplane Flight Manual.  
 
 
 
Control Surface Movements Elevator      Down 25°  Up 16° 
 Rudder      Right 29°  Left 29° 
Aileron      Up 25°   Down 25° 
Flaps       Down 40° 
Airbrakes     Inboard up 50° 
        Outboards up 30° 
Spoilers      up 80° 
Wing slats     Inboard down 20° 
        Median down 35° 
        Outboard down 35° 
Horizontal Stabilizer  Down 12°  Up 2° 
 
 
Serial Numbers Eligible Serial numbers 0001 through 0400. 
 
(b) Falcon 8X Definition (Approved June 27, 2016) 
 
The Falcon 8X does not correspond to a model designation.  The Falcon 8X is only a commercial designation for 
stretch version of the Falcon 7X airplanes that incorporates modifications M1000 and M1254 (EASy III) installed at 
production.  This Falcon 7X version incorporates Pratt & Whitney PW307D engines . 
 
M1000 is basic on all Falcon 7X aircraft starting with serial number 0401. 
 
 
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

A59NM Page 5 of 10 Rev 8
  
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 7X (basic model) 
 
 1. 14 CFR part 25, effective February 1, 1965, including Amendments 25 -1 
through 25-111 in entirety 
 
 2. The following special conditions in accordance with 14 CFR part 11 : 
 
(a) No. 25-343-SC  Pilot Compartment View – Hydrophobic Coatings in Lieu 
of Windshield Wipers 
(b) No. 25-346-SC  Interaction of System and Structure 
(c) No. 25-346-SC  Limit Pilot Forces 
(d) No. 25-346-SC  High Intensity Radiated Fields (HIRF) Protection 
(e) No. 25-349-SC  Side Stick Controllers 
(f) No. 25-349-SC  Electronic Flight Control System: Lateral-Directional and 
Longitudinal Stability and Low Energy Awareness 
(g) No. 25-349-SC  Electronic Flight Control System: Flight Control Surface 
Position Awareness 
(h) No. 25-349-SC  Electronic Flight Control System: Flight Characteristics 
Compliance Via Handling Qualities Rating Method (HQRM) 
(i) No. 25-349-SC  Flight Envelope Protection: General Limiting 
Requirements 
(j) No. 25-349-SC  Flight Envelope Protection: High Incidence Protection 
Function 
(k) No. 25-349-SC  Flight Envelope Protection: Normal Load Factor (G) 
Limiting 
(l) No. 25-349-SC  Flight Envelope Protection: Pitch, Roll And High Speed 
Limiting Functions 
(m) No. 25-350-SC  Sudden Engine Stoppage 
(n) No. 25-350-SC  Operation Without Normal Electrical Power 
(o) No. 25-350-SC  Dive Speed Definition with Speed Protection System 
(p) No. 25-351-SC  Design Roll Maneuvering Conditions 
(q) No. 25-410-SC  Enhanced Flight Visibility System 
(r) No. 25‐711‐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. 
  
NOTE:  The FAA Special Conditions referenced above may be accessed at internet 
location: 
http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgSC.nsf/MainFrame?Op
enFrameSet 
 
 
 3. Equivalent Level of Safety Findings according to the provisions of 14 CFR 
21.21(b)(1) for the following subjects: 
 
(a) Section 25.671:  Control Systems - General (documented in TAD ELOS 
Memo TC0030IB-T-A-6) 
(b) Section 25.331(c)(2):  Pitch Maneuver Conditions (documented in TAD 
ELOS Memo TC0030IB-T-A-8) 
(c) Section 25.811(d)(1), (d)(3):  Emergency Exit Marking (documented in 
TAD ELOS Memo TC0030IB-T-C-2)

A59NM Page 6 of 10 Rev 8  
(d) Section 25.1305 Powerplant Instruments (documented in TAD ELOS 
Memo TC0030IB-T-P-5) 
(e) Section 25.933(a)(1)(ii) Reversing Systems (documented in TAD ELOS 
Memo TC0030IB-T-P-7) 
(f) Section 25.971(a),(b):  Fuel Tank Sump (documented in TAD ELOS Memo 
TC0030IB-T-P-12) 
(g) Section 25.1549(b) – Powerplant and auxiliary power unit instruments 
(documented in TAD ELOS Memo TC0030IB-T-P-13) 
(h) Section 25.841(b)(6) – Pressurized Cabins (documented in TAD ELOS 
Memo TC0030IB-T-SE-13) 
(i) Section 25.831(g) - Ventilation (documented in TAD ELOS Memo 
TC0030IB-T-SE-20) 
(j) Section 25.1459(a)(2) – Flight Recorders (documented in TAD ELOS 
Memo TC0030IB-T-SE-22) 
(k) Section 25.809(b) - Emergency Exit Arrangement (documented in TAD 
ELOS Memorandum AT10010IB-T-CI-101) 
(l) Sections 25.809(b) and 25.813(c)(2)(ii) - Emergency Exit Access 
(documented in TAD ELOS Memorandum AT10010IB-T-CI-101) 
(m) Section 25.813(c)(2) “Emergency Exit Access” (documented in TAD ELOS 
Memo SP00843IB-T 
 
NOTE:  The FAA Equivalent Level of Safety memos referenced above may be accessed 
at internet location: 
http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgSC.nsf/MainFrame?Op
enFrameSet 
 
 4. Exemptions for the following requirement:  
 
(a) Exemption No. 8792, 14 CFR part 25, Section 25.785(b) Side Facing Sofas  
(b) Exemption No. 9117, 14 CFR part 25, Section 25.901(c) Uncontrolled High 
Engine Thrust 
(c) Exemption No. 9148, 14 CFR part 25, Section 25.981(a)(3) Fuel Tank 
Ignition Prevention 
(d) Exemption No. 9506A, 14 CFR part 25, Section 25813(e) Emergency Exit 
Access 
 
 
NOTE:  The FAA Exemptions referenced above may be accessed at internet location: 
http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgEX.nsf/MainFrame?Op
enFrameSet 
 
 5. Optional Design Regulations:   
 
 (a) Ditching Sections 25.801, 25.1411(d), (e), (f), (g) and 25.1415 
 (b) Ice Protection Section 25.141 
  
 6. Environmental Standards 
 
 14 CFR part 36, amendment 36-26. 
 14 CFR part 34, effective September 10, 1990, including amendment 34 -3. 
  
 (b) Falcon 7X airplanes incorporating M1000 (Falcon 8X definition) 
 
1)  The type certification basis, for the Model Falcon 7X 
M1000 project (commercially designated as the Model Falcon 8X),

A59NM Page 7 of 10 Rev 8
  
is the original certification basis for the Model Falcon 7X shown 
above, plus the following: 
 
Section No. Title Amdt 25- System/Area 
25.21(g) 
Proof of 
Compliance 135 
Falcon 7X 
M1000 airplane 
in Icing (except 
25.105(a), 
25.111(c), and 
25.121(b)(c)) 
25.107(c),(g),(h) Take-off Speeds 121 Falcon 7X M1000 airplane 
25.107(e) Take-off Speeds 135 Falcon 7X M1000 airplane 
25.111(c) Take-off Path 115 Falcon 7X M1000 airplane 
25.119 Landing Climb 121 Falcon 7X M1000 airplane 
25.121(d) Climb 121 Falcon 7X M1000 airplane 
25.123 En-route flight 
paths 121 Falcon 7X M1000 airplane 
25.125 Landing 121 Falcon 7X M1000 airplane 
25.143(c),(e),(f),(g),(h),(i) General 121 Falcon 7X M1000 airplane 
25.143(j) General 129 Falcon 7X M1000 airplane 
25.147(d) Directional and 
lateral control 115 Falcon 7X M1000 airplane 
25.161(c) Trim 115 Falcon 7X M1000 airplane 
25.207(b),(h),(i) Stall warning 129 Falcon 7X M1000 airplane 
25.207(e),(f),(g) Stall warning 121 Falcon 7X M1000 airplane 
25.237(a) Wind velocities 121 Falcon 7X 
M1000 airplane 
25.253 High-speed 
characteristics 
135 Falcon 7X 
M1000 airplane 
25.571(a),(b) Damage-
tolerance and 
fatigue 
evaluation of 
structure 
132 T34 Section 
frames 12 to 
12bis and frames 
28bis to 29 
25.613(b),(c),(d),(e),(f) Material strength 
properties and 
design values 
112 T34 Section 
frames 12 to 
12bis and frames 
28bis to 29 
25.677(b) Trim System 115 Horizontal Stabilizer 
25.729(a),(b),(e),(f) Retracting 
Mechanism 136 Main Landing Gear

A59NM Page 8 of 10 Rev 8  
25.812(g) Emergency 
Lighting 116 Cabin, Winglet 
25.812(h) Emergency 
Lighting 128 Cabin, Winglet 
25.973 Fuel Tank Filler 
Connection 115 Wing Fuel Tanks 
25.1322 (a), (e) Flight Crew 
Alerting 131 FalconEye System 
 
 
2.  Noise Standards 
 
14 CFR part 36 as amended by Amendments 36-1 through 36-28. 
 
3.  Fuel Venting and Exhaust Emissions Standards 
 
14 CFR Part 34 as amended by Amendments 34-1 through 34-5A. 
 
4.  Means of Compliance Issue Papers: In addition to the regulatory basis 
noted in the preceding sections, the FAA has established certain “means of 
compliance” in issue papers applicable to the Dassault Falcon 7X M1000 
certification program. 
 
The means of compliance issue papers applicable for Falcon 7X initial pro duct, 
supplemented by the certification bases of all other affected F7X major changes 
up to the M1000 project time of application, are considered to be applicable for 
F7X M1000 project. The list of these issue papers is amended by the following 
means of compliance raised for the specified F7X M1000 project subject areas. 
 
Airframe 
IP A-01 Fuel Tanks Emergency Landing Conditions 
 
Cabin Safety 
At this time, no new Cabin Safety subjects identified as potential means of 
compliance 
 
Flight 
A Cover IP to CRI B-09 “Landing Distance On Smooth Wet Runways” is to be 
addressed by FAA 
 
Noise 
IP N-01 Noise Level Evaluation Requirement 
 
Propulsion 
At this time, no new Propulsion subjects identified as potential means of 
compliance 
 
Systems & Software 
At this time, no new Systems & Software subjects identified as potential means 
of compliance 
Dassault document DGT131264 identifies the complete agreed upon 
certification basis for the F7X M1000 project

A59NM Page 9 of 10 Rev 8
  
(c) Falcon 7X or Falcon 8X airplanes incorporating M-OPT1238 (Starlink 
Antenna Provisions) 
 
1) The type certification basis, for the Model Falcon 7X or Falcon 8X 
incorporating M-OPT1238 (Starlink Antenna Provisions), is the original 
certification basis for the Model Falcon 7X and Falcon 8X shown above, 
plus the following: 
 
2) Equivalent Level of Safety Findings according to the provisions of 14 CFR 
21.21(b)(1) for the following subjects: 
 
Section 25.251:  Vibration and Buffeting (documented in ELOS Memo 
AT19534IB-T-ESF-B25.251-01) 
 
The European Aviation Safety Agency (EASA) originally type certificated this 
aircraft under its type certificate Number A.155. The FAA validated this product 
under U.S. Type Certificate Number A59NM issued April 27, 2007. 
 
Type Definition The type definition is defined by F7TC which is stored in an electronic format 
under the virtual product management tool ENOVIA/VPM©. The repository of 
the ENOVIA/VPM© database is located in Dassault Aviation facilities. 
 (See note 5) 
 
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 European Aircraft Safety Agency (EASA) are contained in the F7TC version 
stored in an electronic format under the virtual product management tool 
ENOVIA/VPM©. 
In addition, the aircraft must be operated in accordance with the FAA approved 
FALCON 7X Airplane Flight Manual, document DGT 105608. 
 
Service Information Each of the documents listed below that contain a statement that it is approved 
by the European Aviation Safety Agency (EASA) are accepted by the FAA and 
are considered FAA approved. 
 • Dassault Aviation Service Bulletins, except as noted below, 
• Structural repair manuals,  
• Vendor manuals referenced in Dassault Aviation service bulletins 
• Aircraft flight manuals, 
• Repair Instructions. 
Additionally, approvals issued by Dassault Aviation under the authority of 
EASA approved Design Organization DOA EASA.21J.051 are considered FAA 
approved.  These approvals pertain to the type certificate only such as changes 
to type design, repair/unrepair of damages. 
Note: Design changes that are contained in Dassault Aviation Service Bulletins 
and that are classified as Level 1 Major in accordance with US/France Bilateral 
Aviation Safety Agreement Implementation Procedures for Airworthiness must  
be approved by the FAA. 
 
FALCON 7X Operating and Service Instructions 
The aircraft must be operated according to the EASA approved Airplane Flight 
Manual DGT 105608 for the basic Falcon 7X.  The aircraft must be operated 
according to the EASA approved Airplane Flight Manual DGT 147681 for the 
Falcon 7X M1000 airplanes (Falcon 8X).

A59NM Page 10 of 10 Rev 8  
Instructions for Continued Airworthiness and Airworthiness Limitations, 
included in FIELD publications, that consist of: 
•        Airworthiness Limitation Section (Chapter 5-40 reference DGT 107838) 
•        Maintenance Planning Document (Chapter 5): 
− Reference: DGT 125953 applicable to S/N 001to S/N 400 (modification 
M1000 not included) 
− Reference: DGSM 151456 applicable to S/N 401 and up (modification 
M1000 included) 
•        Airplane Maintenance Manual  
•        Fault Isolation Manual 
•        Illustrated Parts Catalog (part list only) 
•        Structural Repair Manual (Part 1) 
•        Wiring Diagram Manual 
NOTES 
NOTE 1 - Weight and Balance 
(a) -  A current weight and balance report must be carried in the aircraft at all times from the moment the 
aircraft is originally certified. 
(b) -  Loading of the aircraft must be accomplished in a m anner that always maintains the center of gravity 
within the specified limits considering crew and passenger movements as well as fuel consumption and 
transfer. 
 
NOTE 2 -  Cabin interior and seating configuration must be approved. 
 
NOTE 3 -  Service Life Limits and required Maintenance/Inspections 
(a) Airframe components which are life limited, and associated retirement times, are presented in chapter 
5.40.00 of the FALCON 7X Maintenance Manual, approved by EASA, and must be replaced as 
indicated therein. 
(b) PW307A engine life limits, established for critical rotating components, are published in the approved 
PW307A Airworthiness limitation manual 30P0422 
(c) Required maintenance and inspections to maintain airworthiness based on involving reliability are 
presented in chapter 5.40.00 of the FALCON7X Maintenance Manuals approved by EASA. 
 
NOTE 4 - The FALCON 7X has been approved to operate in “Reduced Vertical Separation Minimum” (RVSM) 
airspace when the airplanes are operated in accordance with Airplane Flight Manual page 1-300-05.  
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 5 - The use of electronic technology and alternative methods of data storage for the type definition of the 
FALCON 7X is managed in accordance with the procedures and documents defined in EASA CRI A-02 
and Dassault document 00-113A-02, and is accepted by the FAA. 
 
NOTE 6 - The FAA has concluded that the occurrence of any uncontrollable high thrust failure condition, or any of 
the associated causal failures listed within Dassault Document DGT-DTC/CER 322496, may endanger the 
safe operation of an airplane. Consequently, the FAA recommends that operators be encouraged to report 
such failures in accordance with §§ 121.703(c), 125.409(c), and 135.415(c).  
 
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. 
 
......END.....
```

## ADs (59, first 50, in force first)

- [AD 2026-11-03](https://openairdocs.org/ad/2026-11-03): Flight Controls · Dassault Falcon 7X. Effective Jul 9, 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 2025-22-05](https://openairdocs.org/ad/2025-22-05): Navigation · Dassault Falcon 7X. Effective Jan 2, 2026
- [AD 2025-13-11](https://openairdocs.org/ad/2025-13-11): Flight Controls · Dassault Falcon 7X. Effective Aug 14, 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 2024-16-11](https://openairdocs.org/ad/2024-16-11): Wings · Dassault Falcon 7X. Effective Oct 23, 2024
- [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 2024-15-04](https://openairdocs.org/ad/2024-15-04): Time Limits/Maintenance Checks · Dassault Falcon 7X. Effective Oct 15, 2024
- [AD 2024-13-06](https://openairdocs.org/ad/2024-13-06): Pneumatic · Dassault Falcon 7X. Effective Sep 24, 2024
- [AD 2024-13-04](https://openairdocs.org/ad/2024-13-04): Powerplant · Dassault Falcon 7X. Effective Aug 16, 2024
- [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 2023-03-11](https://openairdocs.org/ad/2023-03-11): Electrical power · Dassault Falcon 7X. Effective Apr 4, 2023
- [AD 2022-17-10](https://openairdocs.org/ad/2022-17-10): Oxygen · Dassault Falcon 7X. Effective Oct 27, 2022
- [AD 2022-18-18](https://openairdocs.org/ad/2022-18-18): Flight controls · Dassault Falcon 7X. Effective Sep 19, 2022
- [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 2021-03-18](https://openairdocs.org/ad/2021-03-18): Oxygen · Dassault Falcon 7X. Effective Feb 22, 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 2020-05-10](https://openairdocs.org/ad/2020-05-10): Navigation · Dassault Falcon 7X. Effective Mar 26, 2020
- [AD 2018-03-19](https://openairdocs.org/ad/2018-03-19): Structure · Dassault Falcon 7X. Effective Mar 20, 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 2017-20-03](https://openairdocs.org/ad/2017-20-03): Standard Practices Airframe--Electrical Wiring · Dassault Falcon 7X. Effective Nov 6, 2017
- [AD 2017-18-07](https://openairdocs.org/ad/2017-18-07): Standard practices/structures · Dassault Falcon 7X. Effective Oct 5, 2017
- [AD 2017-17-11](https://openairdocs.org/ad/2017-17-11): Engine Controls · Dassault Falcon 7X. Effective Sep 29, 2017
- [AD 2017-13-02](https://openairdocs.org/ad/2017-13-02): Fuselage · Dassault Falcon 7X. Effective Jul 27, 2017
- [AD 2016-24-07](https://openairdocs.org/ad/2016-24-07): Fuel · Dassault Falcon 7X. Effective Jan 9, 2017
- [AD 2016-13-15](https://openairdocs.org/ad/2016-13-15): Fuselage · Dassault Falcon 7X. Effective Aug 16, 2016
- [AD 2016-08-01](https://openairdocs.org/ad/2016-08-01): Electrical power · Dassault Falcon 7X. Effective May 31, 2016
- [AD 2016-07-15](https://openairdocs.org/ad/2016-07-15): Fuel · Dassault Falcon 7X. Effective May 16, 2016
- [AD 2015-06-04](https://openairdocs.org/ad/2015-06-04): Navigation · Dassault Falcon 7X. Effective May 1, 2015
- [AD 2014-16-23](https://openairdocs.org/ad/2014-16-23): Flight Controls · Dassault Falcon 7X. Effective Oct 9, 2014
- [AD 2014-16-21](https://openairdocs.org/ad/2014-16-21): Main Landing Gear · Dassault Falcon 7X. Effective Oct 2, 2014
- [AD 2014-17-02](https://openairdocs.org/ad/2014-17-02): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Sep 9, 2014
- [AD 2014-15-10](https://openairdocs.org/ad/2014-15-10): Flight Controls · Dassault Falcon 7X. Effective Sep 2, 2014
- [AD 2013-16-02](https://openairdocs.org/ad/2013-16-02): Landing gear · Dassault Falcon 7X. Effective Aug 21, 2013
- [AD 2013-07-13](https://openairdocs.org/ad/2013-07-13): Oxygen · Dassault Falcon 7X. Effective May 6, 2013
- [AD 2012-15-11](https://openairdocs.org/ad/2012-15-11): Oxygen · Dassault Falcon 7X. Effective Sep 11, 2012
- [AD 2012-12-18](https://openairdocs.org/ad/2012-12-18): Electrical Power · Dassault Falcon 7X. Effective Jul 30, 2012
- [AD 2011-27-06](https://openairdocs.org/ad/2011-27-06): Electrical Power · Dassault Falcon 7X. Effective Feb 7, 2012
- [AD 2011-14-04](https://openairdocs.org/ad/2011-14-04): Hydraulic Power · Dassault Falcon 7X. Effective Aug 10, 2011
- [AD 2011-09-18](https://openairdocs.org/ad/2011-09-18): Landing Gear · Dassault Falcon 7X. Effective Jun 6, 2011
- [AD 2010-24-02](https://openairdocs.org/ad/2010-24-02): Fuselage · Dassault Falcon 7X. Effective Dec 29, 2010
- [AD 2008-13-10](https://openairdocs.org/ad/2008-13-10): Secondary Power Distribution Boxes (SPDB) · Dassault Falcon 7X. Effective Jul 7, 2008
- [AD 2023-22-13](https://openairdocs.org/ad/2023-22-13) (historical): Time Limits/Maintenance Checks · Dassault Falcon 7X. Effective Dec 29, 2023
- [AD 2023-04-15](https://openairdocs.org/ad/2023-04-15) (historical): Time Limits/Maintenance Checks · Dassault Falcon 7X. Effective May 10, 2023
- [AD 2022-12-10](https://openairdocs.org/ad/2022-12-10) (historical): Navigation · Dassault Falcon 7X. Effective Sep 1, 2022
- [AD 2022-02-10](https://openairdocs.org/ad/2022-02-10) (historical): Standard Practices/Structures · Dassault Falcon 7X, Falcon 900EX and FALCON 2000EX. Effective Mar 15, 2022
- [AD 2021-19-20](https://openairdocs.org/ad/2021-19-20) (historical): Oxygen · Dassault Falcon 7X. Effective Sep 16, 2021
- [AD 2021-09-12](https://openairdocs.org/ad/2021-09-12) (historical): Time Limits/Maintenance Checks · Dassault Falcon 7X. Effective Jun 8, 2021
- [AD 2020-07-16](https://openairdocs.org/ad/2020-07-16) (historical): Time Limits/Maintenance Checks · Dassault Falcon 7X. Effective May 18, 2020

All 59: https://openairdocs.org/tcds/A59NM/ads.md

## Registered aircraft by registry model (OpenAirDocs)

- [Dassault FALCON 7X](https://openairdocs.org/model/dassault-falcon-7x): 167 aircraft (registry code 2730176)

## STCs approved under this data sheet (40)

- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST12403IB](https://openairdocs.org/stc/ST12403IB): Installation and maintenance of HAFEX (P/N P3APP003010D, Umlaut GmbH) and HBPE (P/N 351, Amerex) Halon-free handheld fire extinguishers. Q.C.M. DESIGN GmbH
- [STC ST03620NY](https://openairdocs.org/stc/ST03620NY): Installation of Gogo Galileo HDX System. Dassault Falcon Jet Corp.
- [STC ST03600NY](https://openairdocs.org/stc/ST03600NY): Installation of a GoGo AVANCE L5 system in Dassault Aviation Falcon 7X aircraft. Dassault Falcon Jet Corp.
- [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 ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc.
- [STC ST03616NY](https://openairdocs.org/stc/ST03616NY): Installation of SpaceX Starlink Aviation System i. Dassault Falcon Jet Corp.
- [STC ST03611NY](https://openairdocs.org/stc/ST03611NY): Installation of Garmin GI 275 Standby Flight Display System (SFDS). Dassault Falcon Jet Corp.
- [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 ST01973WI](https://openairdocs.org/stc/ST01973WI): Installation of Aviation Clean Air Ionization System. Dassault Falcon Jet Corp.
- [STC ST00136IB](https://openairdocs.org/stc/ST00136IB): Installation of Entryway & Aft Lavatory Vinyl Flooring, SATCOM ON/OFF Switch, & Galley Equipment. The Bank of Nova Scotia
- [STC ST00133IB](https://openairdocs.org/stc/ST00133IB): Installation of 4G LRU and ACM, Below Floor between FR 13-15, Structural Provision Only. The Bank of Nova Scotia
- [STC ST00101IB](https://openairdocs.org/stc/ST00101IB): Activation of WIFI Network. Dassault Falcon Service
- [STC ST03609NY](https://openairdocs.org/stc/ST03609NY): Installation of the Viassat Global Aero Terminal GAT-5510 Ka-Band Satelite Communication System. Dassault Aircraft Services (DAS)
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc.
- [STC ST04594NY](https://openairdocs.org/stc/ST04594NY): Installation of cabin 14 pax configuration. Dassault Falcon Service
- [STC ST04574NY](https://openairdocs.org/stc/ST04574NY): Installation of Interior Reconfiguration. Elisen & Associes Inc
- [STC ST04469NY](https://openairdocs.org/stc/ST04469NY): Activation of DLU TrueNorth Satcom. Dassault Falcon Service
- [STC ST04509NY](https://openairdocs.org/stc/ST04509NY): Installation of Interior Refurbishment. Elisen & Associes Inc
- [STC ST02672LA](https://openairdocs.org/stc/ST02672LA): Installation of Honeywell DU-1310-2 Display Unit in accordance. Honeywell International Inc
- [STC ST01921WI](https://openairdocs.org/stc/ST01921WI): Interior reconfiguration. Duncan Aviation Inc
- [STC ST04379NY](https://openairdocs.org/stc/ST04379NY): Installation of LH Galley Bulkhead and aircraft curtains modification. Dassault Falcon Service
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST04384CH](https://openairdocs.org/stc/ST04384CH): Reconfiguration of the Cabin Interior in accordance with StandardAero Master Data List 1035953, Revision (A), dated April 5, 2019 or later FAA approved revision.. StandardAero Business Aviation Services LLC
- [STC ST00391BO](https://openairdocs.org/stc/ST00391BO): Installation of a Honeywell CNX-900 Cabin Network Accelerator and PED tolerance certification. Pro Star Aviation LLC
- [STC ST00383BO](https://openairdocs.org/stc/ST00383BO): Installation of a Honeywell DLMU-W. Pro Star Aviation, LLC
- [STC ST01886WI](https://openairdocs.org/stc/ST01886WI): 3-Place 16G Divan Installation. Duncan Aviation Inc
- [STC ST00833DE](https://openairdocs.org/stc/ST00833DE): Demonstration of Aircraft Compatibility to Wireless Fidelity (WiFi) Data Transmissions (Ground & Flight). West Star Aviation LLC
- [STC ST04296CH](https://openairdocs.org/stc/ST04296CH): Reconfiguration of the cabin floor plan arrangement. StandardAero Business Aviation Services, LLC
- [STC ST04278CH](https://openairdocs.org/stc/ST04278CH): Reconfiguration of the cabin floor plan arrangement. StandardAero Business Aviation Services, LLC
- [STC ST11071SC](https://openairdocs.org/stc/ST11071SC): Demonstration of aircraft critical equipment and antenna systems tolerance of radio frequency interference (RFI) from intentional or spurious transmissions from certain Portable Electronic Devices (PEDs). Liberty Partners Inc
- [STC ST04170CH](https://openairdocs.org/stc/ST04170CH): Activation of an 802.11 b/g/n/ac WiFi System. StandardAero Business Aviation Services, LLC
- [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS
- [STC ST04273AT](https://openairdocs.org/stc/ST04273AT): Replace Original Main Battery Connector with Concorde Connector, Part Number 4000. Concorde Battery Corporation
- [STC ST04185AT](https://openairdocs.org/stc/ST04185AT): Replacement of the original equipment valve regulated sealed Lead-acid batteries with Concorde valve regulated sealed Lead-acid batteries with associated hardware. Concorde Battery Corporation
- [STC ST03384CH](https://openairdocs.org/stc/ST03384CH): Reconfiguration of cabin floor Plan Arrangement in accordance with Standard Aero Master Data List 1026983, Revision (F), dated October 02, 2014 or later FAA approved revision.. StandardAero Business Aviation Services LLC
- [STC ST11036SC](https://openairdocs.org/stc/ST11036SC): Installation of a window shade assembly. A & C Products
- [STC ST02146NY](https://openairdocs.org/stc/ST02146NY): Installation of EMS Technologies Ltd. Cabin Network Xcelerator (CNX).. EMS Technologies Canada Ltd
- [STC ST02893AT](https://openairdocs.org/stc/ST02893AT): Installation of a Boom Beam Taxi/Landing Light System. Whelen Aerospace Technologies

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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.