# TCDS TA4CH: Diamond Aircraft Industries Inc. - Type: Type certificate data sheet - Status: Current - Holder: Diamond Aircraft Industries Inc. - Revision: 17 - Revised: August 30, 2021 - Product: Aircraft, Small Airplane - Certification basis: Part 23, Part 21 - Registered aircraft: 364, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/c8/e6/c8e686042f5eb18ca38fd06fb47184915933bdc55b2aca121e3cbc40a66d3855 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8D693917BEF365F88625874A00475D16.0001 - Page: https://openairdocs.org/tcds/TA4CH ## Models (2) As the data sheet lists them. - DA20-A1 - DA20-C1 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TA4CH Revision 17 DIAMOND DA20-A1 DA20-C1 August 30, 2021 TYPE CERTIFICATE DATA SHEET NO. TA4CH This data sheet, which is part of Type Certificate No. TA4CH, 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: Diamond Aircraft Industries Inc. 1560 Crumlin Sideroad London, Ontario Canada N5V 1S2 I - Model DA20-A1 (Utility Category) Approved December 9, 1994 Engine Rotax 912 A3 or 912 F3 or 912 S3 Fuel AVGAS 100LL See Aircraft Flight Manual for other approved fuel types. Oil API System "SF" or "SG" multi grade (See Aircraft Flight Manual recommendations). Do not use aviation grade lubricants Engine Limits (912 A3 or 912 F3) Maximum Takeoff Power Maximum Continuous Power HP 80.0 78.0 Engine R.P.M. 5800 5500 Propeller R.P.M. 2550 2420 (912 S3) Maximum Takeoff Power Maximum Continuous Power 99.0 93.0 5800 5500 2385 2260 Propeller and Propeller Limits Hoffmann HO-V352F/170FQ or HO-V352F/C70FQ Reduced Propeller speed, step-down ratio: 1:2.2727 (compared to engine speed). Diameter 66.9 in (+0, -.39 in), 170 cm (+0, -10 m) No. of Blades: Two Pitch: 10o - 35o (75% station) Airspeed Limits Vne Never Exceed Speed 161 KCAS Vno Maximum Structural Cruising Speed 116 KCAS VA Maneuvering Speed 104 KCAS Maximum Flap Extended Speed 81 KCAS Vfe C.G. Range +9.84 in to +15.35 in (+250 mm to +390 mm) Empty Weight C.G. Range None Levelling Means Wedge 52:1000, 19.69 in (500 mm) in front of rudder fin. Maximum Weight 912 A3 or 912 F3 Engine: 1609 lbs (730 kg) 912 S3 Engine: 1653 lbs (750 kg) Minimum Crew One (1) Pilot. No. of Seats Two at +5.6 in (+143 mm) Maximum Baggage 44 lbs (20 kg) at +32.44 in (+824 mm). Only permissible with baggage harness Fuel Capacity 20.9 gal (79 liters) at +32.44 in (+824 mm) Usable: 20.3 gal (77 liters) (See Note 1) Oil Capacity 3.6 qt (3.4 liters) maximum, 3.2 qt (3 liters) minimum at -41.7 in (-1060 mm) Page No. 1 2 3 4 Rev. No. 16 16 16 15 TA4 CH 2 of 4 Coolant Capacity 2.6 qt (2.5 liters) maximum, 2.5 qt. (2.4 liters) minimum at -41.7 in (-1060 mm) Control Surface Movements AILERON 16o ± 1o UP 13o ± 1o DOWN ELEVATOR 16o ± 1o UP 14o ± 1o DOWN FLAP 15o ± 1o (T/O) 40.5o ± 1.5o (LDG) RUDDER 30o ± 1o left 30o ± 1o right Manufacturer's Serial Nos. Those aircraft shown to comply with Canadian DOT Aircraft Type Certificate A-191. The Canadian Department of Transport Certificate of Airworthiness for Export endorsed as noted under "Import Requirements" must be submitted for each individual aircraft for which application for certification is made (See Note 5 and 6). II - Model DA20-C1 (Utility Category) Approved April 6, 1998 Engine Continental Motors IO-240-B Fuel AVGAS 100LL Engine Limits Maximum Continuous Power 2800 r.p.m. (125 hp) Propeller and Propeller Limits 1. Hoffmann HO-14HM-175-157 Diameter 68.9 in (175 cm) No. of Blades: Two 2. Sensenich W69EK7-63 or W69EK7-63G or W69EK7-63GM Diameter 69 in (175.2 cm) No. of Blades: Two 3. Sensenich W69EK-63 (up to Aircraft S/N C0149) Diameter 69 in (175.2 cm) No. of Blades: Two Airspeed Limits Vne Never Exceed Speed 158.7 KCAS Vno Maximum Structural Cruising Speed 117.7 KCAS VA Maneuvering Speed 106.9 KCAS Maximum Flap Extended Speed Vfe Take-off position (15o) 100 KCAS Landing position (45o) 81 KCAS C.G. Range +8.07 in to +12.16 in (+205 mm to +309 mm) at 1764 lbs (800 kg) +7.95 in to +12.48 in (+202 mm to +317 mm) at 1653 lbs (750 kg) or less Straight line variation between points given Empty Weight C.G. Range None Levelling Means Wedge 55084:1000, 78.7 in (2000 mm) behind canopy. Maximum Weight Ramp Weight 1770 lbs (803 kg) Take-off 1764 lbs (800 kg) Landing 1764 lbs (800 kg) Minimum Crew One (1) Pilot. No. of Seats Two at +5.6 in (+143 mm) Maximum Baggage 44 lbs (20 kg) at +32.44 in (+824 mm). Only permissible with baggage harness 3 of 4 TA4 CH Fuel Capacity S/N C0001 thru C0013: 25 gal (95 liters) at +32.44 in (+824 mm) Usable: 21.3 gal (80.5 liters) ( See Note 1) S/N C0014 and subsequent, and S/N C0001 thru C0013 if Service Bulletin DA C1-28-01 has been incorporated: 24.5 gal (93 liters) at +32.44 in (+824 mm) Usable: 24 gal (91 liters) (See Note 1) All S/N if 20 U.S. Gal. Fuel tank (Dwg. No. 22-2813-00-00) is installed: 20.5 gal (78 liters) at +32.44 in (+824 mm) Usable: 20 gal (76 liters) (See Note 1) Oil Capacity 6 qt (5.68 liters) maximum, 4 qt (3.79 liters) minimum at -39.6 in (-1005 mm) Control Surface Movements AILERON 15.5o ± 1o UP 13.5o ± 1o DOWN ELEVATOR 25o ± 1o UP 15o ± 1o DOWN FLAP 45o ± 1o (LDG) RUDDER 27o ± 1o left 27o ± 1o right Manufacturer's Serial Nos. Those aircraft shown to comply with Canadian DOT Aircraft Type Certificate A-191. The Canadian Department of Transport Certificate of Airworthiness for Export endorsed as noted under "Import Requirements" must be submitted for each individual aircraft for which application for certification is made. Data Pertinent to All Models Reference Datum The reference datum (RD) for the center of gravity (CG) is tangent to the leading edge of the wing at the root rib. Import Requirements A U.S. Airworthiness Certificate may be issued on the basis of the Canadian Certificate of Airworthiness for Export signed by a representative of Transport Canada Civil Aviation (TCCA), containing the following statement: "The aircraft covered by this certificate has been examined and/or tested and found to be in conformity with data forming the basis for DOT Type Certificate No. A-191, (FAA Type Certificate No. TA4CH) and to be in a condition for safe operation". Certification Basis FAR 21.29 and FAR 23 effective February 1, 1965, as amended by 23-1 through 23-42. JAR-VLA effective April 26, 1990, through Amendment VLA/92/1 effective January 1, 1992, used as a safety equivalence to FAR 23, as provided by AC 23-11. FAR 36 dated December 1, 1969, as amended by current amendment as of the date of type Certification. Model DA20-A1: Findings of Equivalent Level of Safety: FAR 23.903(a)(1) (ref. Finding ACE-95-1, dated December 2, 1994). Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. I n addition, the following equipment is also required: Transport Canada Approved Flight Manual DA20 Katana (DA20-A1 with Rotax 912 A3 or F3 engine) Document No. DA202 dated July 28, 1994 or later approved revision. Transport Canada Approved Flight Manual DA20/100 Katana (DA20-A1 with Rotax 912 S3 engine) Document No. DA202-100 Issue 1, dated June 19, 2000 or later approved revision. Transport Canada Approved Flight Manual DA20-C1 (DA20-C1) Document No. DA202-C1 Issue 1 dated Decemebr 19, 1997 or later approved revision. Fire Extinguisher. TA4 CH 4 of 4 Service Information Service Bulletins, structural repair manuals, vendor manuals, overhaul and maintenance manuals, and aircraft flight manuals which contain a statement that the document is Transport Canada approved or Transport Canada approved through the Manufacturers Design Approval Representative are accepted by the FAA and are considered FAA approved. (These approvals pertain to the design data only). NOTE 1 A current weight and balance report including list of equipment included in certificated empty weight must be providedwith each aircraft at the time of original certification. The certificated empty weight and corresponding center of gravity location must include for Model DA20 -A1, full oil and unusable fuel of 3.31 lbs (1.5 kg) at +32.44 in.; for Model DA20-C1, S/N C0001 thru C0013, full oil and unusable fuel of 22.2 lbs (10 kg) at +32.44 in.; and for Model DA20-C1, S/N C0014 and subsequent and S/N C0001 thru C0013 if Service Bulletin DA C1-28-01 has been incorporated, full oil and unusable fuel of 2.76 lbs (1.3 kg) at +32.44 in NOTE 2 All placards specified in the Transport Canada Approved Airplane Flight Manual, and those listed in Chapter 11 of the Maintenance Manual, must be displayed in the airplane in the appropriate locations. NOTE 3 Components which are life limited are listed in Maintenance Manual, Document No. DA201, Chapter 04 for Model DA20-A1 and Document No. DA201-C1, Chapter 04 for Model DA20-C1. Revisions to the Airworthiness Limitations must be approved by Transport Canada on behalf of the FAA. NOTE 4 External colors are limited to those specified in Maintenance Manual, Document No. DA201, Chapter 04 for Model DA20-A1 and Document No. DA201-C1, Chapter 04 for Model DA20-C1. NOTE 5 DA20-A1 S/N 10002 through 10092 were produced with the Rotax 912 A3 engine. S/N 10093 and subsequent were produced with the Rotax 912 F3 engine. The finding of equivalent safety to FAR 23.903(a)(1) for the Rotax 912 A3 engine is applicable only to those serial numbers originally produced with the Rotax 912 A3 engine. NOTE 6 DA20-A1 S/N 10002 through 10092, originally equipped with the Rotax 912 A3 engine, may be retrofitted with the Rotax 912 F3 engine in accordance with Diamond Aircraft Service Bulletin DA20-73-01. DA20-A1 S/N 10002 through 10331, originally equipped with the Rotax 912 A3 or 912 F3 engine, may be retrofitted with the Rotax 912 S3 engine, by Diamond Aircraft Industries or its agents, in accordance with Diamond Aircraft Drawing No. 20-0100-00-00. -- END -- ``` ## ADs (15, in force first) - [AD 2026-15-18](https://openairdocs.org/ad/2026-15-18): Emergency Locator Beacon · Diamond Aircraft Industries DA20-C1. Effective Sep 8, 2026 - [AD 2026-16-11](https://openairdocs.org/ad/2026-16-11): Reciprocating Engine Front Section · BRP-Rotax 912 F2, 912 F3, 912 F4 and 16 more. Effective Aug 28, 2026 - [AD 2023-17-13](https://openairdocs.org/ad/2023-17-13): Reciprocating Engine Front Section · BRP-Rotax 912 F2, 912 F3, 912 F4 and 16 more. Effective Sep 20, 2023 - [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022 - [AD 2018-03-05](https://openairdocs.org/ad/2018-03-05): Reciprocating Engine · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-200 (Super Ximango), HK 36 R SUPER DIMONA, HK 36 TC and 5 more. Effective Mar 20, 2018 - [AD 2016-23-06](https://openairdocs.org/ad/2016-23-06): Engine--Fuel and Control · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-200 (Super Ximango), HK 36 R SUPER DIMONA, HK 36 TC and 5 more. Effective Dec 23, 2016 - [AD 2016-12-02](https://openairdocs.org/ad/2016-12-02): Engine Reciprocating · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-200 (Super Ximango), HK 36 R SUPER DIMONA, HK 36 TC and 5 more. Effective Jul 15, 2016 - [AD 2013-17-04](https://openairdocs.org/ad/2013-17-04): Engine Reciprocating · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-200 (Super Ximango), HK 36 R SUPER DIMONA, HK 36 TC and 5 more. Effective Sep 24, 2013 - [AD 2012-01-01](https://openairdocs.org/ad/2012-01-01): Engine · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-200 (Super Ximango), HK 36 R SUPER DIMONA, HK 36 TC and 5 more. Effective Jan 26, 2012 - [AD 2011-14-09](https://openairdocs.org/ad/2011-14-09): Ignition · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-200 (Super Ximango), HK 36 R SUPER DIMONA, HK 36 TC and 5 more. Effective Jul 25, 2011 - [AD 2010-23-17](https://openairdocs.org/ad/2010-23-17): Engine · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-200 (Super Ximango), HK 36 R SUPER DIMONA, HK 36 TC and 5 more. Effective Dec 22, 2010 - [AD 2010-17-08](https://openairdocs.org/ad/2010-17-08): Engine Fuel and Control · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-200 (Super Ximango), HK 36 R SUPER DIMONA, HK 36 TC and 5 more. Effective Sep 22, 2010 - [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005 - [AD 97-13-02](https://openairdocs.org/ad/97-13-02): Placard - Spins Prohibited · Diamond Aircraft Industries DA20-A1. Effective Jul 14, 1997 - [AD 96-09-05](https://openairdocs.org/ad/96-09-05): Aileron Pushrod Fairings and Aft Wing Cavities · Diamond Aircraft Industries DA20-A1. Effective May 17, 1996 ## Registered aircraft by registry model (OpenAirDocs) - [Diamond Aircraft Ind DA20-C1](https://openairdocs.org/model/diamond-aircraft-ind-da20-c1): 335 aircraft (registry code 2990001) - [Diamond Aircraft Ind DA20-A1](https://openairdocs.org/model/diamond-aircraft-ind-da20-a1): 29 aircraft (registry code 2990000) ## STCs approved under this data sheet (90, first 50) - [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).. Garmin International Inc. - [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.. TCW Technologies, LLC - [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC - [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies - [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC - [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc. - [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder.. Garmin International Inc. - [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc. - [STC SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation - [STC SA12066IB](https://openairdocs.org/stc/SA12066IB): Installation of the MT-Propeller Entwicklung GmbH model MTV-21-A/170-05 propeller. MT-Propeller Entwicklung GmbH - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc. - [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc. - [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd. - [STC SA11838IB](https://openairdocs.org/stc/SA11838IB): Installation of the MT-Propeller Entwicklung GmbH model MTV-21-A/170-05. MT-Propeller Entwicklung GmbH - [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc. - [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc. - [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio.. Peregrine - [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc. - [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC - [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc. - [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King) - [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc. - [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation - [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation - [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc - [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc - [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems.. Garmin International Inc - [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation - [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies - [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine - [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine - [STC SA04112CH](https://openairdocs.org/stc/SA04112CH): Installation of Appareo Systems, LLC Stratus ESG ADS-B transponder. Appareo Systems LLC. - [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation - [STC SA01435SE](https://openairdocs.org/stc/SA01435SE): Installation of J.P. Instruments (JPI) Primary Engine Data Management System. J. P. Instruments - [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc. - [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation - [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine - [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC - [STC SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems.. J P Instruments - [STC SA02428SE](https://openairdocs.org/stc/SA02428SE): Installation of an Air Stream Switch for an electric time recording device on non-pressurized aircraft. Henry F Rogers/David E Polley - [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation - [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation - [STC SA11172SC](https://openairdocs.org/stc/SA11172SC): Installation of an ADS600-B Automatic Dependent Surveillance-Broadcast (ADS-B) Universal Access Transceiver (UAT) and Global Positioning System (GPS) antenna. NavWorx Inc - [STC SA02119SE PAGE 1](https://openairdocs.org/stc/SA02119SE%20PAGE%201): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc - [STC SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc - [STC SA02442AK PAGE 1](https://openairdocs.org/stc/SA02442AK%20PAGE%201): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC - [STC SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc All 90: https://openairdocs.org/tcds/TA4CH/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.