# TCDS 7A13: General Atomics AeroTec Systems GmbH - Type: Type certificate data sheet - Status: Current - Holder: General Atomics AeroTec Systems GmbH - Revision: 7 - Revised: September 28, 2021 - Product: Aircraft, Small Airplane - Certification basis: CAR 10 - Registered aircraft: 6, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/77/be/77bece012161c0b2515697b51439611429bb8a8e86899285ac34d5f56b86bf65 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1029027A43145C738625875D005DD9AC.0001 - Page: https://openairdocs.org/tcds/7A13 ## Models (2) As the data sheet lists them. - Do 28 B-1 - Do 28 A-1 ## 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 Rev. No. 7 4 6 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 7A13 Revision 7 General Atomics AeroTec Systems Do 28 A-1 Do 28 B-1 September 28, 2021 TYPE CERTIFICATE DATA SHEET NO. 7A13 This data sheet which is a part of type certificate No. 7A13 prescri bes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Civil Air Regulations. Type Certificate Holder: General Atomics AeroTec Systems GmbH Claude-Dornier-Strasse 1 D-82234 Wessling Germany Type Certificate Holder Record: Dornier-Werke G.M.b.H. Munich Federal Republic of Germany (Original type certificate holder; date(s) of transfer(s) to subsequent holder(s) not known. Intervening ownership until Dornier Luftfahrt GmbH not known.) DORNIER LUFTFAHRT GmbH D-8031 Wessling Federal Republic of Germany, transferred TC A16EU to Fairchild Dornier GmbH on June 1, 2000. Fairchild Dornier GmbH D-82230 Wessling, Germany, transferred TC A16EU to RUAG Aerospace Services GmbH on July 27, 2003. RUAG Aerospace Services GmbH transferred TC 7A13 to General Atomics AeroTec Systems GmbH on September 28, 2021. I - Model Do 28 A-1, 8 PCLM (Normal Category), Approved July 20, 1961 Engines 2 Lycoming O-540-A1D Fuel 91/96 Minimum grade aviation gasoline Engine limits For all operations, 2575 r.p.m. (250 hp.) Propeller and 2 Hartzell HC-A2XK-2/8433-2 propeller limits Diameter: 82 in. (No cutoff permitted) Pitch settings at 30 in. sta: Low 13°, High 52.7° Airspeed limits Vne (Never exceed) 204 m.p.h. (177 knots) Vno (Max. structural cruising) 160 m.p.h. (139 knots) Vp (Maneuvering) 117 m.p.h. (102 knots) Vfe (Flaps extended) 100 m.p.h. ( 87 knots) C.G. range (+128.5) to (+137.5) Empty weight C.G. range None Maximum weight 5400 lb. No. of seats 8. (2 at +120.8), (2 or 3* at +148.1), (2 or 3* at +189.7) *3 when seats 28.1.24/25 installed. Maximum baggage 132 lb. (+210.6) Fuel capacity 122 gal. (Two twin tanks 29 gal. and 13 gal. ea., two auxiliary tanks 19 gal. ea.) (+153.1) Oil capacity 6 gal. (Two engines with 3 gal. ea.) (+79.5) 2 7A13 Control surface movements Wing flaps Down 45° Outer aileron Up 21° Down 20° Inner aileron Up 18° Down 18° Elevator Up 28° Down 23° Rudder Right 25° Left 25° Stabilizer Up 9° Down 4° Serial Nos. eligible The Federal Republic of Germany Certificate of Airworthiness for Export endorsed as noted below under "Certification basis" must be submitted for each individual aircraft for which application for certification is made. II - Model Do 28 B-1, 7 PCLM (Normal Category), Approved June 1, 1964 Engines 2 Lycoming IO-540-A1A5 Fuel 100/130 Minimum grade aviation gasoline Engine limits For all operations, 2575 r.p.m. (290 hp.) Propeller and 2 Hartzell HC-A3VK-2 propeller limits Diameter: 80 in. (No cutoff permitted) Pitch settings at 30 in. sta: Low 12.5° Airspeed limits Vne (Never exceed) 207 m.p.h. (180 knots) Vno (Max. structural cruising) 167 m.p.h. (145 knots) Vp (Maneuvering) 121 m.p.h. (105 knots) Vfe (Flaps extended) 109 m.p.h. (95 knots) C.G. range (+129.2) to (+137.5) Empty weight C.G. range None Maximum weight 6000 lb. No. of seats 7. (2 at +120.8), (2 or 3 at +148.1), (2 at +189.7) Maximum baggage 132 lb. (+210.6) Fuel capacity 122 U.S. gal. (Two tank groups 29 gal. + 13 gal. + 19 gal. ea.) (+153.1) 40 US gal. (Two auxiliary tip tanks, optional equipment, 20 gal. ea.) (+142.9) Oil capacity 6 U.S. gal. (Two engines, 3 gal. ea.) (+79.5) Control surface movements Serial No. Serial No. 3062 to 3066 3067 and Up. Wing flaps Down 55° Down 55° + 1° Outer aileron Up 20° Down 20° Up 20.5° + 1.5° Down 20.5° + 1.5° Inner aileron Up 18° Down 18° Up 20.5° + 2° Down 20.5° + 2° (measured at zero flap) Elevator Up 32° Down 29° Up 32° + 1° Down 29° + 1° Rudder Right 30° Left 30° Right 30° + 1° Left 30° + 1° For further details see Rigging Diagram in Maintenance Manual Do 28 B-1 Page 3.31. Serial Nos. eligible The Federal Republic of Germany Certificate of Airworthiness for Export endorsed as noted below under "Certification basis" must be submitted for each individual aircraft for which application for certification is made. Specifications Pertinent to All Models Datum 118.11 in. forward of wing leading edge slat Leveling means Longeron in cabin horizontal Certification basis CAR 10. Type Certificate No. 7A13 issued July 20, 1961 Date of Application for Type Certificate March 8, 1960 U.S. Civil Air Regulation Part 3, dated May 15, 1956, including Amendments 3-1, 3-2, 3- 3, 3-4 and 3-5, (Do 28 B-1: including Amendments 3-1 through 3-7). Each aircraft and any replacement part manufactured in Germany must be clearly identified as imported. 3 7A13 Certification basis, contd. The Luftfahrt Bundesamt originally type certificated this aircraft under its type certificate Number 613. The FAA validated this product under U.S. Type Certificate Number 7A13. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of Germany. The EASA type certificate is EASA.A.360. Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. In addition, the following items of equipment are required: (a) Luftfahrt-Bundesamt approved Airplane Flight Manual (b) Stall warning indicator Import Requirements The FAA can issue a U.S. airworthiness certificate based on an NAA Export Certificate of Airworthiness (Export C of A) signed by a representative of the Luftfahrt Bundesamt 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 comply with U.S. Civil Air Regulation Part 3 approved under U.S. Type Certificate No. 7A13 and to be in a condition for safe operation.’ 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. 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 Luftfahrt Bundesamt. • Service bulletins, • Structural repair manuals, • Vendor manuals, • Aircraft flight manuals, and • Overhaul and maintenance manuals. The FAA accepts such documents and considers them FAA-approved unless one of the following conditions exists: • The documents change the limitations, performance, or procedures of the FAA approved manuals; or •The documents make an acoustical or emissions changes to this product’s U.S. type certificate as defined in 14 CFR § 21.93. The FAA uses the post type validation procedures to approve these documents. The FAA may delegate on case-by-case to EASA to approve on behalf of the FAA for the U.S. type certificate. If this is the case it will be noted on the document. NOTE 1. Current weight and balance report, including list of equipment included in certificated empty weight, and loading instructions when necessary, must be provided for each aircraft at the time of original certification. NOTE 2. The following placard must be displayed on the instrument panel in full view of the pilot: "THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE IN COMPLIANCE WITH THE OPERATING LIMITATIONS OF THE AIRPLANE FLIGHT MANUAL. NO ACROBATIC MANOEUVERS, INCLUDING SPINS APPROVED." .....END..... ``` ## ADs (5, in force first) - [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 77-14-17 R1](https://openairdocs.org/ad/77-14-17-R1): Fuel and Oil Hose · Dornier-Werke Do 27 Q-6, Do 28 A-1, Do 28 B-1 and 2 more. Effective Mar 22, 1985 - [AD 66-30-03](https://openairdocs.org/ad/66-30-03): Stabilizer Hinge Bracket · Dornier-Werke Do 28 B-1. Effective Dec 26, 1966 - [AD 64-14-04](https://openairdocs.org/ad/64-14-04): Control Flap Lever · Dornier-Werke Do 27 Q-6 and Do 28 A-1. Effective Jul 17, 1964 - [AD 64-14-03](https://openairdocs.org/ad/64-14-03): Electrical Installation · Dornier-Werke Do 28 A-1, Do 28 B-1, Do 28 D and 1 more. Effective Jul 13, 1964 ## Registered aircraft by registry model (OpenAirDocs) - [Dornier DO28 A-1](https://openairdocs.org/model/dornier-do28-a-1): 3 aircraft (registry code 2990102) - [Dornier DO28 B-1](https://openairdocs.org/model/dornier-do28-b-1): 3 aircraft (registry code 2990202) ## STCs approved under this data sheet (43) - [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 SA12428CH](https://openairdocs.org/stc/SA12428CH): Installation of the Lycoming Engines Electronic Ignition System (EIS). Lycoming Engines, An Operating Division of AVCO Corporation - [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc. - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [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 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 SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC - [STC SA4503NM](https://openairdocs.org/stc/SA4503NM): Remove original cloth covering and install Ceconite covering. Ceconite Division of Poly-Fiber Inc. - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display 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 SA01435LA](https://openairdocs.org/stc/SA01435LA): Installation of engines modified with Firewall Forward Technologies LLC modified camshaft. Centri-Lube Technologies LLC - [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc. - [STC SA04776NY](https://openairdocs.org/stc/SA04776NY): The HIPEC Covering and Finishing System must be performed and maintained. HIPEC Aircraft Coatings 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 SA03819NY](https://openairdocs.org/stc/SA03819NY): Installation and maintenance of Oratex 6000 Covering and Coating System. Lanitz-Prena Folien Factory GmbH - [STC SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King) - [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 SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation 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 SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation - [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation - [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 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 SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine - [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 SA02283SE PAGE 2](https://openairdocs.org/stc/SA02283SE%20PAGE%202): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc. - [STC SA02402SE PAGE 1](https://openairdocs.org/stc/SA02402SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc. - [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc - [STC SA02015SE-D](https://openairdocs.org/stc/SA02015SE-D): Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System.. Garmin International Inc - [STC SA02016SE-D](https://openairdocs.org/stc/SA02016SE-D): Installation of Garmin GTS 800, GTS 820 or GTS 850 Traffic System. Garmin International Inc - [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc. - [STC SA01988SE](https://openairdocs.org/stc/SA01988SE): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.. Electronics International Inc. - [STC SA00769CH](https://openairdocs.org/stc/SA00769CH): Installation of Champion Limited Authority Spark Advance Regulator (LASARTM) ignition system with Cylinder Head Temperature (CHT) monitoring capability on airframes with FAA approved installations of Textron Lycoming model IO-540, AEIO-540 and HIO-540 engines.. Champion Aerospace LLC - [STC SA593CH](https://openairdocs.org/stc/SA593CH): Install Champion SlickSTART magneto booster system.. Champion Aerospace LLC - [STC SA01157LA](https://openairdocs.org/stc/SA01157LA): Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument.. Electronics International Inc. - [STC SA489EA](https://openairdocs.org/stc/SA489EA): Installation of ARP Inc. carburetor ice detection system. Aircraft & Rotorcraft Products (ARP) Inc - [STC SA308EA](https://openairdocs.org/stc/SA308EA): Installation of carburetor ice detection system 105AP in single and twin engine aircraft and single engine helicopters powered by Continental, Franklin, and Lycoming type engines equipped with Marvel-Schebler MA-2, MA-3, MA-4, MA-4-5, MA-6 and HA-6 series carburetors. (Normal,Utility and Acrobatic Category airplanes and helicopters equipped with engines and carburetors as described.). Alfred R Puccinelli - [STC SA00765DE PAGE 1](https://openairdocs.org/stc/SA00765DE%20PAGE%201) (historical): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine - [STC SA02153LA-D](https://openairdocs.org/stc/SA02153LA-D) (historical): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc - [STC SA01435DE](https://openairdocs.org/stc/SA01435DE) (historical): Installation of engines, modified with a Firewall Forward Technologies.. Centri-Lube Technologies LLC - [STC SA02153LA](https://openairdocs.org/stc/SA02153LA) (historical): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System.. Garmin AT Inc. --- 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.