# TCDS R0001RD: Airbus Helicopters - Type: Type certificate data sheet - Status: Current - Holder: Airbus Helicopters - Revision: 5 - Revised: February 8, 2022 - Product: Aircraft, Rotorcraft - Certification basis: Part 27, Part 21 - Registered aircraft: 73, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/88/aa/88aaaddf72dfe566da545797cd2ea534ca78fcb10c8b85f484351842d8fc6e15 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/EF6A06E33470F71D862587E9004E8164.0001 - Page: https://openairdocs.org/tcds/R0001RD ## Models (1) As the data sheet lists them. - EC120B ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text I I I I DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION R0001RD Revision 5 Airbus Helicopters EC120B February 8, 2022 TYPE CERTIFICATE DATA SHEET No. R0001RD This data sheet which is part of Type Certificate No. R0001RD 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: Airbus Helicopters Aeroport International Marseille Provence 13725-Marignane Cedex France TC Holder Record: Eurocopter France changed name to Airbus Helicopters on January 1, 2014. I. Model EC120B (Normal Category) Helicopter, Approved January 28, 1998 Engine. 1 Turbomeca Arrius 2F Fuel. See Rotorcraft Flight Manual Installed Engine Limits. Gas Generator Speed Ng % (RPM) Exhaust Gas Temperature T4 oC (oF) Takeoff Rating (5 min.) 101 (54658) Maximum Continuous 99.5 (53847) Maximum Transient (5 sec.) 103.6 (56065) 870 (1598) 830 (1526) 900 (1652) See Rotorcraft Flight Manual for other limitations including speed and temperature transients Transmission Torque Limits. Maximum Takeoff 100% Maximum Continuous 97% Maximum Transient 110% 100% = 300 Kw (402 SHP) at 406 RPM Rotor Limits. Min. Continuous (power on) 390 RPM Low NR aural warning: 370 RPM Max. Continuous (power on) 415 RPM High NR aural warning: 420 RPM Minimum (power off) 340 RPM Maximum (power off) 447 RPM Airspeed Limits (IAS). Max. VNE (power on) = 150 kts. at Hp= 0 ft. Max. VNE (power off) = 120 kts. at Hp= 0 ft. See Rotorcraft Flight Manual for airspeed limit decrease with altitude. Page No. 1 2 3 Rev. No. 5 3 5 2 of 3 R0001RD, Rev 5 C.G. Range. Longitudinal C.G. Limits max. forward range: at 1680 kg (3700 lb): 3870mm (152.2 in.) at 1400 kg (3086 lb): 3830mm (150.8 in.) at 1300 kg (2866 lb): 3830mm (150.8 in.) at 970 kg (2138 lb): 3890mm (153.1 in.) max. rearward range: at 1680 kg (3700 lb): 4100mm (161.4 in.) at 1300 kg (2866 lb): 4150mm (163.4 in.) at 970 kg (2138 lb): 4170mm (164.2 in.) Straight line variation between points given. Lateral C.G. Limits max. left CG: 80mm (3.15 in.) max. right CG: 80mm (3.15 in.) lateral CG varies with longitudinal CG position. Refer the Rotorcraft Flight Manual. Empty Weight C.G. Range. None Max. Weight. 1680kg (3700 lb) Min. Crew. 1 Pilot Passengers. 4 Max.Baggage/Cargo Loads. Baggage floor: 300kg/m2 (61.4 lb/ft2 ) Cockpit floor: 300kg/m2 (61.4 lb/ft2 ) Fuel Capacity. total: 416 liter (109.9 US gal.) usable: 411.5 liter (108.7 US gal.) Oil Capacity. Maximum engine oil capacity: 4.61 liter (1.22 US gal.) Max. Operating Altitude. 6096m (20000ft) pressure altitude Rotorblade and Control Movements. For rigging information refer to the EC120 Maintenance Manual. Datum. Longitudinal: 4m (157.5 in.) forward of main rotor head center line Lateral: Symetrical plane of the rotorcraft Leveling Means. Mechanical floor Serial Nos. Eligible. 1001 and subsequent. A French (DGAC) Certificate of Airworthiness endorsed as noted below under “Import Requirements” must be submitted for each individual rotorcraft for which application for FAA certification is made. Serial Nos. Ineligible The FAA has revoked the standard airworthiness certificate of serial number 1137 on an emergency basis, based on a determination of un-airworthiness sufficient to render the certificate ineffective. This serial number aircraft is not currently eligible for a Standard Certificate of Airworthiness. Inquiries regarding this aircraft should be directed to the FAA Rotorcraft Directorate Staff, Fort Worth, TX. Certification Basis. - FAR 21.29 - FAR 27, through Amendment 27-33 - FAR 36 Appendix J through Amendment 36-21 - Equivalent Level of Safety findings FAR 27.1027(b)(2) FAR 27.1549(b) The French Direction Generale de l’Aviation Civile (DGAC) originally type certificated this rotorcraft under its type certificate TC 189. The FAA validated 3 of 3 R0001RD, Rev 5 this product under U.S. Type Certificate Number R0001RD. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of the DGAC. Import Requirements. The FAA can issue a U.S. airworthiness certificate based on a National Aviation Authority (NAA) Export Certificate of Airworthiness (Export C of A) signed by a representative of the French Generale de l’Aviation Civile (DGAC) on behalf of the European Community. 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. The Export C of A should contain the following statement: “The aircraft covered by this certificate has been examined, tested, and found to comply with the type design approved under U.S. Type Certificate Number R0001RD and to be in a condition for safe operation.” Equipment. The minimum required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the respective helicopter for certification. DGAC-approved EC120B Rotorcraft Flight Manual, dated June 19, 1997, Revision 2, or later approved revision, as required. Service Information. Each of the documents listed below must state that it is approved by the European Aviation Safety Agency (EASA) or – for approvals made before September 28, 2003 – by the French Generale de l’Aviation Civile (DGAC). Any such documents are accepted by the FAA and are considered FAA approved.  Service Bulletin,  Structural repair manuals,  Vendor manuals,  Aircraft flight manuals, and  Overhaul and maintenance manuals. This applies only to the acceptance of the type design data. NOTES NOTE 1. Any alteration to the type design of this aircraft may require instructions for Continued Airworthiness. These instructions must be submitted and accepted by the Fort Worth Aircraft Evaluation Group Office prior to approval for return to service. NOTE 2 Effective January 1, 2014, Eurocopter France name was changed to Airbus Helicopters. - END - ``` ## ADs (41, in force first) - [AD 2026-20-03](https://openairdocs.org/ad/2026-20-03): Placards and Markings · Airbus Helicopters AS350B, AS350BA, AS350B1 and 11 more. Effective Nov 5, 2026 - [AD 2026-14-02](https://openairdocs.org/ad/2026-14-02): Indication/Recording System · Airbus Helicopters AS350B2, AS350B3, EC120B and 1 more. Effective Aug 14, 2026 - [AD 2026-04-07](https://openairdocs.org/ad/2026-04-07): Rotorcraft Flight Control · Airbus Helicopters EC120B. Effective Apr 7, 2026 - [AD 2025-20-10](https://openairdocs.org/ad/2025-20-10): Tail Rotor System · Airbus Helicopters EC120B. Effective Dec 30, 2025 - [AD 2025-17-02](https://openairdocs.org/ad/2025-17-02): Emergency Flotation Section · Airbus Helicopters EC120B, EC130B4 and EC130T2. Effective Sep 26, 2025 - [AD 2025-05-12](https://openairdocs.org/ad/2025-05-12): Main Rotor Head · Airbus Helicopters EC120B. Effective May 8, 2025 - [AD 2024-20-07](https://openairdocs.org/ad/2024-20-07): Emergency Equipment; Emergency Flotation Section · Apical Emergency Float Kit, P/N 20498 (STC SR00780LA or 12 others). Effective Dec 5, 2024 - [AD 2023-14-06](https://openairdocs.org/ad/2023-14-06): Main Landing Gear Strut, Axle, Truck · Airbus Helicopters EC120B, EC130B4 and EC130T2. Effective Sep 8, 2023 - [AD 2023-11-07](https://openairdocs.org/ad/2023-11-07): Ground Proximity System · Airbus Helicopters 47, 206, 210 and 237 more. Effective Jun 22, 2023 - [AD 2022-02-06](https://openairdocs.org/ad/2022-02-06): Tail Rotor Blades · Airbus Helicopters EC120B. Effective Mar 17, 2022 - [AD 2022-02-13](https://openairdocs.org/ad/2022-02-13): Rotorcraft Tail Boom · Airbus Helicopters EC120B. Effective Mar 17, 2022 - [AD 2021-24-08](https://openairdocs.org/ad/2021-24-08): Main Rotor System · Airbus Helicopters EC120B. Effective Jan 14, 2022 - [AD 2021-17-17](https://openairdocs.org/ad/2021-17-17): Cabin Equipment/Furnishings · Airbus Helicopters EC135P3, EC135T3, MBB-BK 117 C-2 and 32 more. Effective Nov 22, 2021 - [AD 2020-25-11](https://openairdocs.org/ad/2020-25-11): Doors · Airbus Helicopters EC120B and EC130B4. Effective Jan 21, 2021 - [AD 2020-12-02](https://openairdocs.org/ad/2020-12-02): Tail rotor blades · Airbus Helicopters EC120B. Effective Jul 13, 2020 - [AD 2017-26-04](https://openairdocs.org/ad/2017-26-04): Emergency Equipment · Airbus Helicopters EC120B. Effective Jan 24, 2018 - [AD 2017-06-11](https://openairdocs.org/ad/2017-06-11): failure of an air conditioner compressor drive pulley (pulley) or tail rotor output wheel (wheel) · Airbus Helicopters EC120B with STC SR00491DE. Effective May 8, 2017 - [AD 2016-12-13](https://openairdocs.org/ad/2016-12-13): Engine/Transmission Coupling--Coupling Tube, Engine Mount, and Engine Mount Base · Airbus Helicopters EC120B. Effective Jul 27, 2016 - [AD 2015-26-04](https://openairdocs.org/ad/2015-26-04): Cabin Equipment/Furnishings · Airbus Helicopters EC120B. Effective Feb 4, 2016 - [AD 2013-16-19](https://openairdocs.org/ad/2013-16-19): Emergency Flotation Section · Airbus Helicopters EC120B and EC130B4. Effective Sep 27, 2013 - [AD 2011-21-18](https://openairdocs.org/ad/2011-21-18): Cyclic Control Stick · Airbus Helicopters EC120B. Effective Dec 20, 2011 - [AD 2011-11-04](https://openairdocs.org/ad/2011-11-04): Contaminated Gas · Airbus Helicopters AS355E, AS355F, AS355F1 and 12 more. Effective Jun 17, 2011 - [AD 2005-09-05](https://openairdocs.org/ad/2005-09-05): Tail rotor drive shaft (drive shaft) · Airbus Helicopters EC120B. Effective Jun 13, 2005 - [AD 2003-22-10](https://openairdocs.org/ad/2003-22-10): Electrical bonding braid (bonding braid) that is installed on the left cyclic pitch control stick base · Airbus Helicopters EC120B. Effective Dec 10, 2003 - [AD 2003-08-04](https://openairdocs.org/ad/2003-08-04): Cyclic pitch flight control torque tube · Airbus Helicopters EC120B. Effective May 22, 2003 - [AD 2002-15-08](https://openairdocs.org/ad/2002-15-08): Cargo Hooks · Airbus Helicopters AS-365N2, AS-365N3, AS332C and 21 more. Effective Sep 6, 2002 - [AD 2001-24-08](https://openairdocs.org/ad/2001-24-08): Cabin Sliding Door Rail · Airbus Helicopters EC120B. Effective Jan 7, 2002 - [AD 2021-26-07](https://openairdocs.org/ad/2021-26-07) (historical): Tail rotor system · Airbus Helicopters EC120B. Effective Jan 27, 2022 - [AD 2021-23-13](https://openairdocs.org/ad/2021-23-13) (historical): Ground Proximity System · Airbus Helicopters K-225, K-190A, K-240 and 237 more. Effective Dec 9, 2021 - [AD 2021-04-21](https://openairdocs.org/ad/2021-04-21) (historical): Main Rotor System · Airbus Helicopters EC120B. Effective May 7, 2021 - [AD 2020-11-05](https://openairdocs.org/ad/2020-11-05) (historical): Tail rotor system · Airbus Helicopters EC120B. Effective Jun 8, 2020 - [AD 2014-12-12](https://openairdocs.org/ad/2014-12-12) (historical): Emergency Exits · Airbus Helicopters EC 130 B4 and EC120B. Effective Aug 4, 2014 - [AD 2010-05-51](https://openairdocs.org/ad/2010-05-51) (historical): Main rotor hub · Airbus Helicopters EC120B. Effective May 14, 2010 - [AD 2009-25-07](https://openairdocs.org/ad/2009-25-07) (historical): Emergency Floatation Gear Lighting and Ancillary Control Unit (LACU) · Airbus Helicopters EC120B. Effective Dec 28, 2009 - [AD 2008-10-01](https://openairdocs.org/ad/2008-10-01) (historical): Spherical thrust bearings · Airbus Helicopters EC120B. Effective May 21, 2008 - [AD 2002-13-11](https://openairdocs.org/ad/2002-13-11) (historical): Yaw control · Airbus Helicopters EC120B. Effective Aug 13, 2002 - [AD 2001-04-12](https://openairdocs.org/ad/2001-04-12) (historical): Main Gearbox Coupling Tube Assembly · Airbus Helicopters EC120B. Effective Mar 20, 2001 - [AD 2000-17-07](https://openairdocs.org/ad/2000-17-07) (historical): Cabin Sliding Door · Eurocopter France EC120B. Effective Sep 12, 2000 - [AD 2000-05-17](https://openairdocs.org/ad/2000-05-17) (historical): Engine Coupling Tube · Airbus Helicopters EC120B. Effective Mar 27, 2000 - [AD 99-19-23](https://openairdocs.org/ad/99-19-23) (historical): Engine Coupling Tube Inspection · Eurocopter France EC120B. Effective Oct 19, 1999 - [AD 2015-24-51](https://openairdocs.org/ad/2015-24-51) (historical): Air Comm Corporation (Air Comm) air conditioning kit · Airbus Helicopters EC120B with STC SR00491DE ## Registered aircraft by registry model (OpenAirDocs) - [Eurocopter EC120B](https://openairdocs.org/model/eurocopter-ec120b): 68 aircraft (registry code 8680987) - [Eurocopter COLIBRI EC 120B](https://openairdocs.org/model/eurocopter-colibri-ec-120b): 2 aircraft (registry code 8680985) - [Airbus Helicopters EC120B](https://openairdocs.org/model/airbus-helicopters-ec120b): 1 aircraft (registry code 868099C) - [Eurocopter EC120](https://openairdocs.org/model/eurocopter-ec120): 1 aircraft (registry code 8680986) - [Eurocopter France EC120B](https://openairdocs.org/model/eurocopter-france-ec120b): 1 aircraft (registry code 8680995) ## STCs approved under this data sheet (64, first 50) - [STC SR12074IB](https://openairdocs.org/stc/SR12074IB): Installation of halon free Umlaut fire extinguisher P/N P3APP003010D with extinguishing agent 2-BTP (Halotron® BrX). SABENA TECHNICS BGC - [STC SR03641AT](https://openairdocs.org/stc/SR03641AT): Replace the existing Eurocopter EC120-B windows with Tech-Tool Plastics, Inc. replacement windows. Tech-Tool Plastics Inc. - [STC SR00217IB](https://openairdocs.org/stc/SR00217IB): Installation of Skid Shoes. Airbus Helicopters Canada Limited - [STC SR09450RC](https://openairdocs.org/stc/SR09450RC): Installation of SAGEM ICDS-8 Integrated Cockpit Display System that includes a display for the pilot position and a second optional display for the copilot position.. Safran Electronics & Defense Avionics USA, LLC - [STC SR00182IB](https://openairdocs.org/stc/SR00182IB): Installation of the Avidyne Integrated Flight Display (IFD) Navigator(s). Horizon Design Services Ltd. - [STC SR04637CH](https://openairdocs.org/stc/SR04637CH): Replacement of existing main ship battery with Lithium Ion Battery and installation of Annunciator Control Panel. Airwolf Aerospace LLC - [STC SR02120SE](https://openairdocs.org/stc/SR02120SE): Installation of Garmin GTN 6XX/7XX Navigation System. Garmin International Inc. - [STC SH3319NM](https://openairdocs.org/stc/SH3319NM): Installation of Precise Flight Pulselite Control Unit in the Landing /Taxi Recognition Visual Control Light system,. Precise Flight Inc - [STC SR02028SE](https://openairdocs.org/stc/SR02028SE): Fabrication of Onboard Systems International Model 200-351-00, Cargo Hook Kit,. Onboard Systems International LLC - [STC SR01673SE](https://openairdocs.org/stc/SR01673SE): Installation of Chelton Flight Systems Electronic Flight Instrument System (EFIS) and associated equipment. Genesys Aerosystems Inc. - [STC SR02704SE](https://openairdocs.org/stc/SR02704SE): Installation and maintenance of the Sunspot 36 and 46 series lights. AeroLED's Holdings LLC - [STC SR02622SE](https://openairdocs.org/stc/SR02622SE): Installation of Garmin G500H TXi Display System (Primary Flight Display (PDF), Multi-Function Display (MFD)). Garmin International Inc - [STC SR04453CH](https://openairdocs.org/stc/SR04453CH): Installation of Appareo Systems LLC Stratus ES & Stratus ESG ADS-B transponder. Appareo Systems LLC - [STC SR02124SE](https://openairdocs.org/stc/SR02124SE): Installation functionality. of Data Garmin Required: transponders: (1) Garmin GTX Master 345/345R Drawing with List ADS-B (MDL), Out and In 005-00734-A4, functionality;. Garmin International Inc - [STC SR00359BO](https://openairdocs.org/stc/SR00359BO): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies - [STC SR02487AK](https://openairdocs.org/stc/SR02487AK): Installation of L-3 Communications Avionics Systems ESI-500 Standby Instrument System. ADS-B Technologies, LLC - [STC SR02478AK](https://openairdocs.org/stc/SR02478AK): Installation of the L-3 Aviation Products Lynx multilink surveillance system model NGT-9000() part number 9029000-20000 or Garmin GTX-345 ADS-B transponder part number 011-03302-40. Vector Aerospace Helicopter Services USA Inc. - [STC SR09263RC-D](https://openairdocs.org/stc/SR09263RC-D): Installation of a SFIM VFR Autopilot System. Safran Electronics & Defense Avionics USA, LLC - [STC SR11230SC](https://openairdocs.org/stc/SR11230SC): Installation of HeliSAS Stability Augmentation System and Autopilot (SAS/AP). S-TEC Corporation - [STC SR02475AK](https://openairdocs.org/stc/SR02475AK): Installation of the Lexavia Integrated Systems LFS3500 Enhanced Vision System (EVS) on Part 27 Airbus Helicopters equipped with a panel-mounted Multi-Function Display (MFD), primary navigational display or dedicated display with the ability to display video imagery. Lexavia Integrated Systems - [STC SR02470AK](https://openairdocs.org/stc/SR02470AK): Installation of the L-3 Communications NGT -1000/2000/2500 ADS-B System. ADS-B Technologies, LLC - [STC SR02471AK](https://openairdocs.org/stc/SR02471AK): Installation of the L-3 Communications NGT -9000/9000R ADS-B System. ADS-B Technologies, LLC - [STC SR03676NY](https://openairdocs.org/stc/SR03676NY): Installation of Aspen EFD 1000H Pro Primary Flight Display and associated components. Motorflug Baden-Baden GmbH - [STC SR03539NY](https://openairdocs.org/stc/SR03539NY): Installation of Garmin G500H Flight Display System.. Maxcraft Avionics Ltd. - [STC SR03524NY](https://openairdocs.org/stc/SR03524NY): Installation of a MD302 Standby Attitude Module. Maxcraft Avionics Ltd. - [STC SR01130NY-D](https://openairdocs.org/stc/SR01130NY-D): Installation of NS Microwave Antenna Installation. Sikorsky Aircraft Corporation - [STC SR00491DE](https://openairdocs.org/stc/SR00491DE): Installation of cabin air conditioning system.. Air Comm Corporation - [STC SR00549DE](https://openairdocs.org/stc/SR00549DE): Installation of Bleed Air Cabin Heater/Defroster System.. Air Comm Corporation - [STC SR09427RC](https://openairdocs.org/stc/SR09427RC): Installation of Night Vision Goggle (NVG) Compatible Interior Lighting System. REB Technologies Inc - [STC SR00780LA](https://openairdocs.org/stc/SR00780LA): Installation of Apical Emergency Float Kit, P/N 20498.. Apical Industries Inc. dba Dart Aerospace - [STC SR01191SE](https://openairdocs.org/stc/SR01191SE): Installation of an engine air filter.. Aerometals - [STC SR03383NY](https://openairdocs.org/stc/SR03383NY): Installation of a Latitude Technologies IONODE Flight Data Monitoring (FDM). Latitude Technologies Corporation - [STC SR03364NY](https://openairdocs.org/stc/SR03364NY): Installation of a Garmin G500H Flight Display System. Kitchener Aero Avionics Ltd - [STC SR03243NY](https://openairdocs.org/stc/SR03243NY): Installation of Right-Hand Door Handle. Eurocopter Canada Limited - [STC SR03152NY](https://openairdocs.org/stc/SR03152NY): The installation of the Brite Saver 2 Data Monitoring System. ECT Industries - [STC SR02232LA](https://openairdocs.org/stc/SR02232LA): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin AT Inc. - [STC SR02939NY](https://openairdocs.org/stc/SR02939NY): Installation of a SkyTrac ISAT-200 Airborne Position/Data Communicator in accordance with Avionics Design Services Ltd. Master Drawing List MDL10033, Revision C, dated February 02, 2011, Transport Canada approved February 02, 2011, or later Transport Canada approved revision.. SkyTrac Systems Ltd. - [STC SR09371RC-D](https://openairdocs.org/stc/SR09371RC-D): Cabin Floor Protector Kits in accordance with Aeronautical Accessories, Inc. Drawing List, Report No. AA-03084, Revision A, dated February 16, 2004, or later DAS approved revisions; and installation per Report No. AA-03082, No Revision, dated November 12, 2003, and/or AA-03083, Revision A, dated February 16, 2004, or later DAS approved revisions.. Bell Helicopter Textron Inc. - [STC SR01609SE](https://openairdocs.org/stc/SR01609SE): Installation of a Supplemental Lighting System.. Aviation Specialties Unlimited Inc. - [STC SR02189NY](https://openairdocs.org/stc/SR02189NY): Iinstallation of SkyTrac ISAT-100 Airborne Position/Data Communicator System.. SkyTrac Systems Ltd. - [STC SR01892NY](https://openairdocs.org/stc/SR01892NY): Installation of an Improved Heating System.. Eurocopter Canada Limited - [STC SR09466RC](https://openairdocs.org/stc/SR09466RC): Installation of Night Vision Goggle Compatible Interior Lighting System and Red Position Light.. Aero Dynamix Inc. - [STC SR01701NY](https://openairdocs.org/stc/SR01701NY): Installation of SX-16 Nightsun Searchlight System. Exterior mount must be installed per STC SR01302LA.. Eurocopter Canada Limited - [STC SR02244NY](https://openairdocs.org/stc/SR02244NY): Installation of FLIR 8000 series System.. Eurocopter Canada Limited - [STC SR01245NY](https://openairdocs.org/stc/SR01245NY): Installation of Settling Protectors.. Eurocopter Canada Limited - [STC SR01302LA](https://openairdocs.org/stc/SR01302LA): Installation of side utility mount.. Airfilm Camera Systems - [STC SR00811NY](https://openairdocs.org/stc/SR00811NY): Installation of Technisonic Industries Limited TFM-138 series transceiver models.. Technisonic Industries Limited - [STC SR01842NY](https://openairdocs.org/stc/SR01842NY): Installation of Air Cruisers emergency flotation system.. Air Cruisers Company - [STC SR09136RC-D](https://openairdocs.org/stc/SR09136RC-D): Installation of a Forward L/H External Mount.. American Eurocopter Corporation - [STC SR09108RC-D](https://openairdocs.org/stc/SR09108RC-D): Installation of a left or right pilot instrument panel.. American Eurocopter Corporation All 64: https://openairdocs.org/tcds/R0001RD/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.