# TCDS A33EU: Dassault Aviation - Type: Type certificate data sheet - Status: Current - Holder: Dassault Aviation - Revision: 4 - Revised: March 2, 2010 - Product: Aircraft, Large Airplane - Certification basis: Part 25, Part 36 - Registered aircraft: 59, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/ab/70/ab701e9e6098599f2c15410a3fbd04df724f0c1816c7755e519a6cc7223ec02a - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/884F33EC030A8099862576E900493298.0001 - Page: https://openairdocs.org/tcds/A33EU ## Models (1) As the data sheet lists them. - Falcon 10 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 3 4 5 Rev.No. 4 2 2 3 3 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A33EU Revision 4 DASSAULT AVIATION Falcon 10 March 2, 2010 TYPE CERTIFICATE DATA SHEET NO. A33EU This data sheet which is a part of Type Certificate No. A33EU prescribes conditions and limitations under which the product for which the Type Certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder: DASSAULT AVIATION (See NOTE 6) 9 Rond Point des Champs Elysees 75008 Paris France I - MODEL FALCON 10 (Transport Category Airplane), Approved September 20, 1973 Engines 2 - Airesearch Manufacturing Company of Arizona, Model TPE731-2-1C (FAA Engine Type Certificate E6WE-1) Fuel Fuels conforming to Airesearch Manuf acturing Company of Arizona specifications: EMS 53111 (Type JET A) EMS 53112 (Type JET A 1) EMS 53113 (Type Jet B and JP4) EMS 53116 (Type JP5) Aviation gasoline, MIL-G-5572D, grades 80/87, 100/130 and 115/145, not in excess of 500 gallons per 100 hours of operation, may be used in emergencies. Shall ASA-3, anti-static additive, or e quivalent, in amounts to bring fuel up to 300 conductivity units, is permissible except that in no event shall the additive exceed 1 ppm. MIL-I-27686E inhibitor, icing, fuel system, or equivalent, is approved for use in fuel in amounts up to 0.15 percent by volume. If a different type of fuel is used, or a mixt ure of fuels is used, the engine computer must be adjusted (to adapt the computer to the de nsity of the fuel used) in order to preserve both the starting characteristics and the acceleration and deceleration characteristics of the engine. Oil Oils conforming to Airesearch Manufact uring Company of Arizona Specification EMS 53110, Class B. (Service Information letters of the Aires earch Manufacturing Company of Arizona give brand names of oils conforming to the above specification). A33EU 2 Engine Limits Maximum take off static thrust, up to 86°F Sea level conditions (5 minutes) lb. 3,230 Maximum continuous static thrust, up to 86 °F Sea level conditions lb. 2,966 Maximum permissible engine operating speeds (Takeoff and maximum continuous) Low pressure rotor (N 1) RPM 20,688 Percent 100% High pressure rotor (N 2) RPM 29,692 Percent 100% Maximum permissible interstage turbine temperature (ITT) During starting 860 °C (1,580°F) Takeoff (5 minutes) 860 °C (1,580°F) Maximum continuous 832 °C (1,530°F) Oil pressure limits At idle, psig 25 to 46 Takeoff and maximum continuous psig 38 to 46 Oil temperature Maximum from sea level up to 30,000 ft. 113 °C (235°F) Maximum above 30,000 ft. 132 °C (270°F) Minimum -40 °C ( -40°F) Fuel pressure Minimum fuel pressure warning, psi 4.5 Airspeed Limits V MO (Maximum Operating 350 kts at sea level; 370 kts at 10, 000 ft., with straight line variation between those points. 370 kts from 10,000 ft. to 25,000 ft. M MO (Maximum Operating) M = 0.87 above 25,000 ft. V A (Maneuvering) 220 kts V FE (Slat and Flap Speed) Slats 200 kts Slats + Flaps 15 ° 190 kts Slats + Flaps 30 ° 165 kts Slats + Flaps 52 ° 165 kts V LO (Landing Gear Operation) 190 kts V LE (Landing Gear Extended) 220 kts Windshield Wiper Operation 190 kts V MC (Minimum Control Speed) In flight 97 kts On ground 100 kts C.G.Range (Gear Extended) Forward limit % MAC Weight(lb) Takeoff En Route Landing Aft limit % MAC 18,300 25 25 -- 31 17,200 21.2 21.2 21.2 31 15,720 16 16 16 31 13,230 16 14 14 31 9,920 16 14 14 31 Straight-line variation between points shown. Gear retraction moment is + 1750 in.lb. 3 A33EU Datum Datum is 25% of mean aerodynamic chor d (MAC) which is marked on aircraft and coincides with Fuselage Station (FS) + 268.28 inches. (Fuselage station +0 is the forward end of the aircraft nose cone.) Mean Aerodynamic Chord. Length 80.54 in. Zero % MAC is at FS +248.15 in. Leveling Means A bubble-type level, when placed on the top of bolt heads (with locknuts) on the floor of the fuselage rear compartment, facilitates le veling of the airplane in the longitudinal and lateral directions. Weight Limitations Maximum Weights Maximum ramp 18,300 lb. Maximum takeoff (brake rel ease) 18,300 lb.(See NOTE 3 and 4) Maximum landing 17,200 lb. Maximum zero fuel 12,460 lb (See NOTE 3) Minimum weight 9,920 lb Minimum Crew 2 - Pilot and co-pilot Maximum Passengers 9 with appr opriate approved passenger provisions for cabin interior and approved seating arrangement. (AMD Production Memo No. 1908 iden tifies approved passenger provisions and seating arrangement fo r a maximum of 7 passengers). 0 - without passenger provisions for cabin interior but incorporating AMD Ferry Kit per Production Memo No. 751. Maximum Baggage Compartment Weight (lb) Arm*(in) In the coat rack - without galley, with retainer 180 -110.0 - with galley 90 -102.5 On the rear tank 500 +44.5 On the folded back of the three-people divan 500 + 9.5 * Arm is taken from 25% MAC. Fuel Capacity (Average - Refer to weight and balan ce report of each individual airplane for exact capacity). U.S. Gallons Pounds Arm (in) USABLE FUEL in both wings 470.0 3,150 -7 in both fuselage tanks 412.0 2,762 +47 TOTAL USABLE 882.0 5,912 +18 UNUSABLE FUEL - Drainable unusable fuel in both wings 1.0 7 -7 in both fuselage tanks 3.5 24 -47 - Tank trapped fuel in both wings 1.0 7 -7 in both fuselage tanks - - - - Line trapped fuel 0.5 4 +50 - Engine trapped fuel 1.5 10 +55 TOTAL FUEL in both wings 472 3,164 -7 in both fuselage tanks 415.5 2,786 +47 in lines and engines 2.0 14 +54 TOTAL 889.5 5,964 +18 Pressure Fueling Maximum pressure for pr essure fueling is 50 psi. A33EU 4 Oil Capacity Usable, 0.5 U.S. gallon (at Arm + 75 in.) (each engine) Unusable, 2.25 U.S. gallon (at Arm + 75 in.) Maximum Operating Altitude 45,000 feet Control Surface Movements (Control Stops) Elevator Up 18 °30’(±10’) Down 12 ° (± 10’) Rudder Right 35 ° (± 10’) Left 35 ° (± 10’) Aileron Up 15 °30’ (+0°10’ -0°30’) Down 13 °30’(+0°10’-0°30’) Flaps Down 52 ° (±30’) Airbrakes Up 50 ° Wing slats Internal 20 ° (+30’ -0) External 31 °10’ (+30’ -0) Stabilizer: Electrical stops: Nose down 0 °14’ (±10’) Nose up 12 °16’ (±10’) Mechanical stops: Nose down (max) 0 °35’ Nose up (max) 12 °55’ Structural stops: Nose down (min) 1 ° Nose up (min) 13 °15’ Serial Numbers Eligible A French “Certificat de navi gabilite pour Exportation” endorsed as noted under “Import Requirements”, must be submitted for each i ndividual aircraft for which application for U.S. Certification is made. Import Requirements The FAA can issue a U.S. airwor thiness certificate based on an NAA Export Certificate of Airworthiness (Export C of A) signed by a representative of the Direction Générale de l'Aviation Civile (DGAC) of France on behalf of the European Community. The Export C of A should contain the following statement: ‘The aircraft covered by this certificate has been examined, tested, and found to conform with Type Design approved under U.S. Type Certificate No. A33EU and to be in a condition for safe operation.’ Certification Basis FAR Part 25 dated February 1, 1964, including Amendment Nos. 25-1 through 25-20. FAR Part 36, including Amendment 36-1. FAA Special Conditions No. 25-49-EU-14, dated April 16, 1973. Type Certificate A33EU issued September 20, 1973. Date of Application for Type Certificate: June 18, 1969. The Direction Générale de l'Aviation Civile (DGAC) of France originally type certificated this aircraft under its type certificate Number 142. The FAA validated this product under U.S. Type Certificate Number A33EU. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of the Direction Générale de l'Aviation Civile (DGAC) of France. Equipment The basic required equipm ent as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installe d on the aircraft for Certification. The equipment list for Falcon 10 contains lists of all equipment as well as optional equipment approved by Secretariat Gene ral a l’Aviation Civile (SGAC) of France. In addition, the following is required: (a) SGAC or FAA-approved Falcon 10 Airplane Flight Manual, approved October 17, 1973 (b) Nose wheel must be equipped with a chined tire. Service Information Each of the doc uments 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 Générale de l'Aviation Civile (DGAC) 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. F.JA.03 are considered FAA approved. These approvals pertain to the type design only. • Dassault Aviation Service Bulletins, except as noted below, 5 A33EU • 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/France or US/EASA Bilateral Aviation Safety Agreement Implementation Procedures for Airworthiness must be approved by the FAA. NOTES NOTE 1. Weight and Balance. a. Current weight and balance report, including list of equipment in certificated empty weight and loading instructions must be provided for each aircraft at delivery. b. The airplane must be loaded so that the CG is w ithin the specified limits at all times with the effect of fuel used and a movement of crew and pa ssengers from their assigned position being considered. c. The following must be included in the airplane empty weight: The total Unusable Fuel (52 lb.) listed unde r Fuel Capacity, plus unusable oil (36 lb. at +75 inches), plus hydraulic fluid (77 lb. at +45 inches). NOTE 2. Service Life Limits. Service life limits for airframe structural components wh ich are fatigue critical, if any, are listed in the FAA- approved Airplane Fli ght Manual for Falcon 10. NOTE 3. Airplane S/N 55 and subsequent , and prior serial numbers incorporating AMD/BA Modification No. 150 or Service Bulletin No. F10-0052, are eligible for ope ration at a maximum takeoff weight of 18,743 lbs. (8500 kg) in accordance with SGAC-approved Falcon 10 Airplane Flight Manual Revision No. 7 and at maximum zero fuel weight of 13,560 lbs (6150 kg) in accordance with DGAC-approved Falcon 10 Airplane Flight Manual Revision 10 on behalf of FAA. NOTE 4. Airplane S/N 212 and subsequent , and prior serial numbers incorporating AMD-BA Modification M151 or Service Bulletin No. F10-238, are eligible for opera tion with the following maximum weights, in accordance with DGAC-approved Falcon 10 Airplane Fli ght Manual Revision 23 on behalf of FAA. Maximum ramp 19,405 lb Maximum takeoff (brake release) 19,305 lb Maximum landing 17,640 lb Maximum zero fuel 14,420 lb Minimum flight weight 9,920 lb The associate CG range (gear extended) is then as follows: Forward limit % MAC Weight(lb) Takeoff En Route Landing Aft limit % MAC 9,920 16 14 14 31 13,230 16 14 14 31 15,720 16 16 16 31 17,640 21.8 21.8 21.8 31 19,305 26.6 26.6 31 19,405 27 31 NOTE 5. Airplanes incorporating AMD-BA Service Bulle tin No. F10-0082 are eligible for operation on unpaved runways in accordance with DGAC approved Falcon 10 Airplane Flight Manual Supplement No 1 and F10 Flight Manual Revision 9, on behalf of FAA. NOTE 6. Effective June 19, 1990 the name of AVI ONS MARCEL DASSAULT-BREGUET AVIATION changed to DASSAULT AVIATION. The new name will appear as of this date on all documents and nameplates. However, documents bearing the old name remain valid and will be updated when and where necessary. ...END... ``` ## ADs (43, in force first) - [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026 - [AD 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 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 - [AD 2021-04-20](https://openairdocs.org/ad/2021-04-20): Time Limits/Maintenance Checks · Dassault Falcon 10. Effective Apr 9, 2021 - [AD 2021-03-12](https://openairdocs.org/ad/2021-03-12): Ice and rain protection · Dassault Falcon 10. Effective Mar 31, 2021 - [AD 2020-17-14](https://openairdocs.org/ad/2020-17-14): Flight Controls · Dassault Falcon 10. Effective Oct 8, 2020 - [AD 2016-19-07](https://openairdocs.org/ad/2016-19-07): Ice and Rain Protection · Dassault Falcon 10. Effective Oct 21, 2016 - [AD 2013-25-01](https://openairdocs.org/ad/2013-25-01): Flight controls · Dassault Falcon 10. Effective Dec 24, 2013 - [AD 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 2008 - [AD 2008-04-14](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 2005-04-02](https://openairdocs.org/ad/2005-04-02): Airplane flight manual (AFM) · Dassault Falcon 10. Effective Mar 25, 2005 - [AD 2002-13-07](https://openairdocs.org/ad/2002-13-07): Inertial Reference Units (IRU) · Dassault Falcon 10, Falcon 900EX, Fan Jet Falcon and 8 more. Effective Aug 9, 2002 - [AD 2001-13-11](https://openairdocs.org/ad/2001-13-11): Dual Non-return Valves of the Fire Extinguishing System · Dassault Falcon 10. Effective Jul 12, 2001 - [AD 2001-01-05](https://openairdocs.org/ad/2001-01-05): Parking Brake · Dassault Falcon 10, Mystere-Falcon 50, Falcon 10 and 1 more. Effective Feb 22, 2001 - [AD 2000-05-20](https://openairdocs.org/ad/2000-05-20): Passenger Oxygen Masks · Dassault Falcon 10, Falcon 900EX, Fan Jet Falcon and 13 more. Effective Apr 18, 2000 - [AD 97-05-03 R1](https://openairdocs.org/ad/97-05-03-R1): Global Positioning Systems · BAE Systems Avro 146-RJ100A, BAe 146-200A, Jetstream Model 4101 and 27 more. Effective Apr 20, 1999 - [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998 - [AD 95-22-01](https://openairdocs.org/ad/95-22-01): Fluorescent Lighting System · Aerospace Lighting Fluorescent lighting systems, A310-203, A310-204 and 74 more. Effective Dec 4, 1995 - [AD 90-07-08 R1](https://openairdocs.org/ad/90-07-08-R1): Fluorescent Lighting and Remote Power Units · British Aerospace Regional Jetstream 3201, Jetstream Series 3101, Falcon 10 and 10 more. Effective Jul 2, 1990 - [AD 87-24-10](https://openairdocs.org/ad/87-24-10): Air Conditioning Freon Compressor Motor · Dassault Falcon 10. Effective Dec 29, 1987 - [AD 86-15-06](https://openairdocs.org/ad/86-15-06): Rudder Servo Actuator System · Dassault Falcon 10. Effective Aug 25, 1986 - [AD 86-13-03](https://openairdocs.org/ad/86-13-03): Automatic Leading Edge Slat Extension System · Dassault Falcon 10. Effective Jul 24, 1986 - [AD 84-02-02](https://openairdocs.org/ad/84-02-02): Wing Leading Edge Slat Anti-Icing System · Dassault Falcon 10. Effective Jan 31, 1984 - [AD 83-24-02](https://openairdocs.org/ad/83-24-02): Eexterior Emergency Lighting · Dassault Falcon 10. Effective Dec 23, 1983 - [AD 83-15-02](https://openairdocs.org/ad/83-15-02): Passenger Door Latches · Dassault Falcon 10. Effective Aug 1, 1983 - [AD 82-25-02](https://openairdocs.org/ad/82-25-02): Landing Gear Retraction System · Dassault Falcon 10. Effective Dec 6, 1982 - [AD 81-19-06](https://openairdocs.org/ad/81-19-06): Seat Belt Attachments · Dassault Falcon 10. Effective Oct 14, 1981 - [AD 81-05-02](https://openairdocs.org/ad/81-05-02): Compressor Starting Circuit · Dassault Falcon 10. Effective Mar 2, 1981 - [AD 80-15-04](https://openairdocs.org/ad/80-15-04): Passenger Door Microswitch · Dassault Falcon 10. Effective Aug 11, 1980 - [AD 78-14-02](https://openairdocs.org/ad/78-14-02): Oxygen Pressure · Dassault Falcon 10. Effective Jul 11, 1978 - [AD 78-01-10](https://openairdocs.org/ad/78-01-10): Fire Extinguishing System · Dassault Falcon 10. Effective Jan 19, 1978 - [AD 77-23-04](https://openairdocs.org/ad/77-23-04): Total-Pressure Probes · Dassault Falcon 10. Effective Dec 10, 1977 - [AD 77-15-08](https://openairdocs.org/ad/77-15-08): Pilot or Copilot Seats · Dassault Falcon 10. Effective Aug 22, 1977 - [AD 77-07-09](https://openairdocs.org/ad/77-07-09): Tailpipes · Dassault Falcon 10. Effective Apr 18, 1977 - [AD 76-11-08](https://openairdocs.org/ad/76-11-08): Electrical Power · Dassault Falcon 10. Effective Jun 15, 1976 - [AD 2019-03-27](https://openairdocs.org/ad/2019-03-27) (historical): Ice and rain protection · Dassault Falcon 10. Effective Mar 8, 2019 - [AD 2018-24-03](https://openairdocs.org/ad/2018-24-03) (historical): Time Limits/Maintenance Checks · Dassault Falcon 10. Effective Jan 4, 2019 - [AD 2010-26-05](https://openairdocs.org/ad/2010-26-05) (historical): Air Conditioning · Dassault Falcon 10, Falcon 900EX, Fan Jet Falcon and 14 more. Effective Jan 25, 2011 - [AD 2008-19-08](https://openairdocs.org/ad/2008-19-08) (historical): Airplane flight manual · Dassault Falcon 10. Effective Oct 27, 2008 - [AD 2007-18-08](https://openairdocs.org/ad/2007-18-08) (historical): Airplane flight manual (AFM) · Dassault Falcon 10. Effective Oct 11, 2007 - [AD 2005-18-14](https://openairdocs.org/ad/2005-18-14) (historical): Airplane flight manual (AFM) · Dassault-Aviation Falcon 10. Effective Sep 26, 2005 - [AD 2005-07-23](https://openairdocs.org/ad/2005-07-23) (historical): Airplane flight manual (AFM) · Dassault-Aviation Falcon 10. Effective Apr 26, 2005 - [AD 2000-12-15](https://openairdocs.org/ad/2000-12-15) (historical): Overwing Emergency Exit · Dassault-Aviation Falcon 10, FALCON 2000, Falcon 900EX and 12 more. Effective Jul 20, 2000 ## Registered aircraft by registry model (OpenAirDocs) - [Dassault-Breguet FALCON 10](https://openairdocs.org/model/dassault-breguet-falcon-10): 56 aircraft (registry code 2730101) - [Avion Marcel Dassault Breguet FALCON 10](https://openairdocs.org/model/avion-marcel-dassault-breguet-falcon-10): 2 aircraft (registry code 2730122) - [Avions Marcel Dassault Breguet FALCON 10](https://openairdocs.org/model/avions-marcel-dassault-breguet-falcon-10): 1 aircraft (registry code 2730114) - [Dassault FALCON 10](https://openairdocs.org/model/dassault-falcon-10): 0 aircraft (registry code 2730166) ## STCs approved under this data sheet (231, 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 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 ST11216DS](https://openairdocs.org/stc/ST11216DS): Installation of automatic dependent surveillance-broadcast (ADS-B) out on Part 25 aircraft. BHE & Associates Ltd. - [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc. - [STC 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 ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC - [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC - [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc. - [STC ST02004WI](https://openairdocs.org/stc/ST02004WI): Installation of the Garmin GI-275 Instantaneous Vertical Speed Indicators (IVSI). Peregrine - [STC ST01930LA](https://openairdocs.org/stc/ST01930LA): Installation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI). Sandel Avionics LLC - [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc. - [STC SA1223CE](https://openairdocs.org/stc/SA1223CE): Install King KFC-300 dual flight director flight control system(Category I configuration).. Honeywell International Inc - [STC SA1224CE](https://openairdocs.org/stc/SA1224CE): Installation of King KFC-300 dual flight director flight control system (Category II configuration).. Honeywell International Inc - [STC ST02635LA](https://openairdocs.org/stc/ST02635LA): Modification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC ST00652SE](https://openairdocs.org/stc/ST00652SE): Installation of emergency medical stretcher and base, oxygen and electrical systems.. LifePort LLC - [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 ST00835DE](https://openairdocs.org/stc/ST00835DE): Installation of Automatic Dependent Surveillance - Broadcast (ADS-B) Out and In functionality using the Garmin GTX 335R and GTX 345R Transponders plus qualified position sensor. Peregrine - [STC ST02395CH](https://openairdocs.org/stc/ST02395CH): Install air ambulance conversion.. Spectrum Aeromed LLC dba Spectrum Aeromed - [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC ST00373BO](https://openairdocs.org/stc/ST00373BO): Installation of Rockwell Collins TDR-94D Transponders with ADS-B Out. Pro Star Aviation, LLC - [STC SA2217SW](https://openairdocs.org/stc/SA2217SW): Installation of Collins Dual FD-109 Y and Z Flight Directors and associated sensors for Category II operation. Textron Aviation Inc - [STC SA2218SW](https://openairdocs.org/stc/SA2218SW): Installation of single Collins NCS-31 Area Navigation System with mechanical back-up controls. Textron Aviation Inc - [STC SA2219SW](https://openairdocs.org/stc/SA2219SW): Installation of Intercontinental Dynamics Corporation Servo/Pneumatic, Pneumatic, Flight Instruments. Textron Aviation Inc - [STC SA2221SW](https://openairdocs.org/stc/SA2221SW): Revision of existing Inverter Control System. Textron Aviation Inc - [STC SA2222SW](https://openairdocs.org/stc/SA2222SW): Installation of additional nose cone mounted landing lights. Textron Aviation Inc - [STC SA2223SW](https://openairdocs.org/stc/SA2223SW): Installation of wing inspection lights. Textron Aviation Inc - [STC SA2224SW](https://openairdocs.org/stc/SA2224SW): Installation of Long Range/RNAV System. Textron Aviation Inc - [STC SA2227SW](https://openairdocs.org/stc/SA2227SW): Installation of Canadian Marconi CMA-730 Engine and Fuel Quantity Instrumentation. Textron Aviation Inc - [STC SA2228SW](https://openairdocs.org/stc/SA2228SW): Installation of Fairchild Flight Data Recorder and Collins Cockpit Voice Recorder. Textron Aviation Inc - [STC SA2301SW](https://openairdocs.org/stc/SA2301SW): Modification of Dassault installed main cabin door counterbalance system. Textron Aviation Inc - [STC ST02632LA](https://openairdocs.org/stc/ST02632LA): Modification to replace the existing Mode S Transponder system with ACSS NXT-700 Mode S Transponder with ADS-B Out and optionally install ACSS NXG-900 GPS as a position source for ADS-B Out. Aviation Communications and Surveillance Systems - [STC ST02609LA](https://openairdocs.org/stc/ST02609LA): Modification to replace the existing Mode S Transponder system with ACSS NXT-700 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC SA2225SW](https://openairdocs.org/stc/SA2225SW): Passenger compartment interior.. Textron Aviation Inc - [STC SA2226SW](https://openairdocs.org/stc/SA2226SW): Pressurization of nose cone to improve avionics reliability.. Textron Aviation Inc - [STC SA3650SW](https://openairdocs.org/stc/SA3650SW): Installation of No. 2 Global GNS-500A, Series 4, VLF/Omega Navigation System.. Textron Aviation Inc - [STC SA3651SW](https://openairdocs.org/stc/SA3651SW): Installation of Lockheed flight data recorder, Model 650/1/14040/001.. Textron Aviation Inc - [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 ST00881WI-D](https://openairdocs.org/stc/ST00881WI-D): Modification of a TCAS II system installation to Change 7.0 or Change 7.1. Rockwell Collins Inc - [STC ST00800DE](https://openairdocs.org/stc/ST00800DE): Modification of a TCAS II system installation to Change 7.1. West Star Aviation Inc - [STC ST00774LA](https://openairdocs.org/stc/ST00774LA): Installation of Two Concorde Battery Model No. RG-390E Batteries.. Concorde Battery Corporation - [STC ST01474WI-D](https://openairdocs.org/stc/ST01474WI-D): Modication of a Rockwell Collins Weather Radar System installation.. Rockwell Collins Inc - [STC SA2846WE](https://openairdocs.org/stc/SA2846WE): Installation of Hoskins Pulstar Twilight Supplemental Lighting System in accordance with FAA sealed Hoskins Top Drawing No. 10-202864.. BF Goodrich Aerospace - [STC ST01202WI-D](https://openairdocs.org/stc/ST01202WI-D): Modification of an existing FAA approved Collins TPR-720, TPR-900 or TPR-901 Mode S transponder installation in Part 25 Aircraft using Collins Drawing Index as listed on AML No. ST01202WI-D, latest FAA approved revision.. Rockwell Collins Inc - [STC ST00673WI-D](https://openairdocs.org/stc/ST00673WI-D): Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System installation.. Rockwell Collins Inc - [STC ST00682WI-D](https://openairdocs.org/stc/ST00682WI-D): Modification of Collins VHF-20/VHF-20A/VHF-20B VHF COMM Receiver Transmitter with CTL-20 Control Pro Line I System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation in accordance with Collins Installation Instructions as listed on AML No. ST00682WI-D, Revision -, or later FAA approved revisions.. Rockwell Collins Inc - [STC ST00632WI-D](https://openairdocs.org/stc/ST00632WI-D): Installation of an Allied Signal MK VI GPWS System.. Duncan Aviation Inc - [STC ST01131WI-D](https://openairdocs.org/stc/ST01131WI-D): Installation of Honeywell MK-VIII Enhanced Ground Proximity Warning System (EGPWS).. Duncan Aviation Inc - [STC ST02760CH](https://openairdocs.org/stc/ST02760CH): Installation of a single Universal Avionics Systems Corporation UNS-1Lw Flight Management System and an LP/LPV Monitor. Elliott Aviation Technical Products All 231: https://openairdocs.org/tcds/A33EU/stcs.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.