TCDS No. EASA.A.554 Issue 03 SIAT 223 13 Nov. 2018 TYPE-CERTIFICATE DATA SHEET NO. EASA.A.554 for SIAT 223 Type Certificate Holder Airbus Defence and Space GmbH Willy-Messerschmitt-Straße 1 82024, Taufkirchen Germany For models: SIAT 223 V SIAT 223 A1 SIAT 223 K1 TE.CERT.00048-001 European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 1 of 18
CONTENT SECTION A: SIAT 223 V A.I. General A.II. Certification Basis A.III. Technical Characteristics and Operational Limitations A.IV. Operating and Service Instructions A.V. Notes SECTION B: SIAT 223 A1 B.I. General B.II. Certification Basis B.III. Technical Characteristics and Operational Limitations B.IV. Operating and Service Instructions B.V. Notes SECTION C: SIAT 223 K1 C.I. General C.II. Certification Basis C.III. Technical Characteristics and Operational Limitations C.IV. Operating and Service Instructions C.V. Notes ADMINISTRATIVE SECTION I. Acronyms II. Type Certificate Holder Record III. Change Record TE.CERT.00048-001 European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 2 of 18
SECTION A: A.I. General SIAT 223 V 1. a) Type: b) Model: SIAT 223 SIAT 223 V 2. Airworthiness Category: Normal Utility 3. Type Certificate Holder: Airbus Defence and Space GmbH Willy-Messerschmitt-Straße 1 82024 Taufkirchen, Germany 4. Contracted DOA Holder: N/A 5. Manufacturer: Waggon- und Maschinenbau AG Siebelwerke ATG GmbH Donauwörth, Germany 6. (Reserved) 7. Type Certification in Federal Republic of Germany by Luftfahrt-Bundesamt 03 April 1968 The EASA TCDS is based on the LBA TCDS No. 679/SA for SIAT 223 V (at Issue 9, dated 12 April 2005) A.II. EASA Certification Basis 1. Airworthiness Requirements: FAR 23 incl. Amendment 23.1 and 23.2 2. Environmental Standards: ICAO Annex 16, Vol. I; for details see TCDSN.A.554 TE.CERT.00048-001 European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 3 of 18
A.III. Technical Characteristics and Operational Limitations 1. Description: Single-engine, cantilever low-wing aircraft, full metal construction, non-retractable landing gear in nose-wing configuration 2. Equipment: Minimum equipment pursuant to airworthiness requirements (see II.3) Details respecting minimum equipment as well as data on possible additional equipment may be found in the equipment list in the flight manual SIAT 223 dated 15 March 1968 3. Dimensions: Wing Span: 8,28 m Length: 7,43 m Height: 2,70 m 4. Engine: 4.1 Model: Engine 1: Lycoming IO-360-C1B Engine 2: Lycoming IO-360-C1D6 4.2 Type Certificate: Engine 1 & 2: EASA.IM.E.032 4.3 Limitations: Power 203 HP at 2700 rpm 5. Propeller: 5.1 Model: Hartzell HC-C2YK-1B()/()7666()-2 5.2 Type Certificate: EASA.IM.P.130 5.3 Number of blades: 2 5.4 Diameter: 1880 mm ± 0 mm (74 inch) 5.5 Sense of Rotation: Clockwise 6. Fluids: 6.1 Fuel: Aviation fuel 100/130 octane or 100 LL TE.CERT.00048-001 European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 4 of 18
6.2 Oil: unalloyed alloyed SAE 50 SAE 40 or 50 above 16 C SAE 40 SAE 40-1 C to +32 C SAE 30 SAE 40 or 20W-30-18 C to +21 C SAE 20 20W-30 below -12 7. Fluid capacities: 7.1 Fuel: Max. fuel: 220 l Usable fuel quantity: 216 l 7.2 Oil: 7,6 l 8. Air Speeds: Normal Utility Max. permissible - Speed V NE: 165 kt 177 kt - Manoeuvring speed VA: 122 kt 126 kt - Cruising speed VNO: 131 kt 131 kt - Flaps extended VFE: 110 kt 110 kt 9. (Reserved) 10. Load factors: Normal category: -1,52 g to 3,8 g Utility category: -1,76 g to 4,4 g 11. Maximum Weights: Normal Utility Max. permissible: -Takeoff mass 1050 kg 980 kg 12. Centre of Gravity Range: Normal category @ 1050 kg: @ 1000 kg @ 821 kg or less: Utility category @ 980 kg @ 821 kg 235,2 cm 239,2 cm 226,2 cm 239,2 cm 222,4 cm 239,2 cm 225,8 cm 232,2 cm 222,4 cm 232,2 cm 13. Datum: Reference plane: 200 cm forward of leading edge of wing Attitude: top chord of cockpit dome horizontal TE.CERT.00048-001 European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 5 of 18
14. Levelling Means: Refer to Maintenance Manual 15. Control surface deflections: Landing flaps Down 40 Ailerons Up 22 Down 22 Rudder Left 25 Right 25 Elevator Up 25 Down 30 Transverse trim Up 18 Down 18 tabs Elevator trim tabs Up 17 Down 17 Vertical trim tab Left 17 Right 17 Tolerance for all rudders: +/- 1 Control stick max. 4,6 mm 16. Minimum Flight Crew: 1 pilot 17. Maximum Passenger Seating Capacity: Normal category: 2 passengers Utility category: 1 passenger 18. Baggage/Cargo Compartments: Max. payload weight on rear bench: 77 kg 19. Wheels and Tyres: Refer to Maintenance Manual 20. (Reserved): A.IV. Operating and Service Instructions 1. Manual for Operation: a) Flight Manual SIAT 223 V, LBA-approved edition of 15 March 1968 with Annex, mass and balance statement, loading plan and equipment list b) Checklist SIAT 223 I and II c) Labelling as per Flight Manual 2. Technical Manual: a) Operations Manual SIAT 223 V b) Maintenance Manual SIAT 223 V c) Lycoming Operator s Manual, Model IO-360 Series Aircraft Engines d) Hartzell Propeller Owner s Manual The listed documents can be obtained from the holder of type approval. TE.CERT.00048-001 European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 6 of 18
A.V. Notes: 1. Eligible Serial Numbers: 001-004 TE.CERT.00048-001 European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 7 of 18
SECTION B: B.I. General SIAT 223 A1 1. a) Type: b) Model: SIAT 223 SIAT 223 A1 2. Airworthiness Category: Normal Utility 3. Type Certificate Holder: Airbus Defence and Space GmbH Willy-Messerschmitt-Straße 1 82024 Taufkirchen, Germany 4. Contracted DOA Holder: N/A 5. Manufacturer: Waggon- und Maschinenbau AG Siebelwerke ATG GmbH Donauwörth, Germany La Hispano Aviacion S.A. Sevilla, Spain 6. (Reserved) 7. Type Certification in Federal Republic of Germany by Luftfahrt-Bundesamt 12 April 1968 The EASA TCDS is based on the LBA TCDS No. 679/SA for SIAT 223 A1 (at Issue 9, dated 12 April 2005) B.II. EASA Certification Basis 1. Airworthiness Requirements: FAR 23 incl. Amendment 23.1 and 23.2 2. Environmental Standards: ICAO Annex 16, Vol. I; for details see TCDSN.A.554 TE.CERT.00048-001 European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 8 of 18
B.III. Technical Characteristics and Operational Limitations 1. Description: Single-engine, cantilever low-wing aircraft, full metal construction, non-retractable landing gear in nose-wing configuration 2. Equipment: Minimum equipment pursuant to airworthiness requirements (see II.3) Details respecting minimum equipment as well as data on possible additional equipment may be found in the equipment list in the flight manual SIAT 223 A1 dated 15 March 1968 3. Dimensions: Wing Span: 8,28 m Length: 7,43 m Height: 2,70 m 4. Engine: 4.1 Model: Engine 1: Lycoming IO-360-C1B Engine 2: Lycoming IO-360-C1D6 4.2 Type Certificate: Engine 1 & 2: EASA.IM.E.032 4.3 Limitations: Power 203 HP at 2700 rpm 5. Propeller: 5.1 Model: Hartzell HC-C2YK-1B()/()7666()-2 5.2 Type Certificate: EASA.IM.P.130 5.3 Number of blades: 2 5.4 Diameter: 1880 mm ± 0 mm (74 inch) 5.5 Sense of Rotation: Clockwise 6. Fluids: 6.1 Fuel: Aviation fuel 100/130 octane or 100 LL 6.2 Oil: unalloyed alloyed SAE 50 SAE 40 or 50 above 16 C SAE 40 SAE 40-1 C to +32 C SAE 30 SAE 40 or 20W-30-18 C to +21 C SAE 20 20W-30 below -12 TE.CERT.00048-001 European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 9 of 18
7. Fluid capacities: 7.1 Fuel: Max. fuel: 170 l Usable fuel quantity: 166 l 7.2 Oil: 7,6 l 8. Air Speeds: Normal Utility Max. permissible - Speed V NE: 165 kt 177 kt - Manoeuvring speed VA: 122 kt 126 kt - Cruising speed VNO: 131 kt 131 kt - Flaps extended VFE: 100 kt 100 kt 9. (Reserved) 10. Load factors: Normal category: -1,52 g to 3,8 g Utility category: -1,76 g to 4,4 g 11. Maximum Weights: Normal Utility Max. permissible: -Takeoff mass 1050 kg 980 kg 12. Centre of Gravity Range: Normal category @ 1050 kg: @ 1000 kg @ 821 kg or less: Utility category @ 980 kg @ 821 kg 235,2 cm 239,2 cm 226,2 cm 239,2 cm 222,4 cm 239,2 cm 225,8 cm 232,2 cm 222,4 cm 232,2 cm 13. Datum: Reference plane: 200 cm forward of leading edge of wing Attitude: top chord of cockpit dome horizontal 14. Control surface deflections: Landing flaps Down 40 Ailerons Up 22 Down 22 Rudder Left 25 Right 25 Elevator Up 25 Down 30 Transverse trim Up 18 Down 18 tabs Elevator trim tabs Up 17 Down 17 Vertical trim tab Left 17 Right 17 TE.CERT.00048-001 European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 10 of 18
Tolerance for all rudders: +/- 1 Control stick max. 4,6 mm 15. Levelling Means: Refer to Maintenance Manual 16. Minimum Flight Crew: 1 pilot 17. Maximum Passenger Seating Capacity: 18. Baggage/Cargo Compartments: Normal category: 2 passengers Utility category: 1 passenger Max. payload weight on rear bench: 77 kg 19. Wheels and Tyres: Refer to Maintenance Manual 20. (Reserved): B.IV. Operating and Service Instructions 1. Manual for Operation: a) Flight Manual SIAT 223 A1, LBA-approved edition of 15 March 1968 with Annex, mass and balance statement, loading plan and equipment list b) Checklist SIAT 223 A1/K1 I and II c) Labelling as per Flight Manual 2. Technical Manual: a) Operations Manual SIAT 223 A1 b) Maintenance Manual SIAT 223 A1 c) Lycoming Operator s Manual, Model IO-360 Series Aircraft Engines d) Hartzell Propeller Owner s Manual The listed documents can be obtained from the holder of type approval. B.V. Notes: 1. Eligible Serial Numbers: Siebelwerke ATG GmbH, 885 Donauwörth, Germany : 011 to 050 LaHispano Aviacion S.A., San Jacinto 68-76, Seville, Spain: 051 and subsequent TE.CERT.00048-001 European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 11 of 18
SECTION C: C.I. General SIAT 223 K1 1. a) Type: b) Model: SIAT 223 SIAT 223 K1 2. Airworthiness Category: Normal Utility Aerobatic 3. Type Certificate Holder: Airbus Defence and Space GmbH Willy-Messerschmitt-Straße 1 82024 Taufkirchen, Germany 4. Contracted DOA Holder: N/A 5. Manufacturer: Waggon- und Maschinenbau AG Siebelwerke ATG GmbH Donauwörth, Germany 6. (Reserved) La Hispano Aviacion S.A. Sevilla, Spain 7. Type Certification in Federal Republic of Germany by Luftfahrt-Bundesamt 28 August 1968 The EASA TCDS is based on the LBA TCDS No. 679/SA for SIAT 223 A1 (at Issue 9, dated 12 April 2005) C.II. EASA Certification Basis 1. Airworthiness Requirements: FAR 23 incl. Amendment 23.1 and 23.2 2. Environmental Standards: ICAO Annex 16, Vol. I; for details see TCDSN.A.554 TE.CERT.00048-001 European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 12 of 18
C.III. Technical Characteristics and Operational Limitations 1. Description: Single-engine, cantilever low-wing aircraft, full metal construction, non-retractable landing gear in nose-wing configuration 2. Equipment: Minimum equipment pursuant to airworthiness requirements Details respecting minimum equipment as well as data on possible additional equipment may be found in the equipment list in the flight manual SIAT 223 K, LBAapproved on 15 August 1968 3. Dimensions: Wing Span: 8,28 m Length: 7,43 m Height: 2,70 m 4. Engine: 4.1 Model: Engine 1: Lycoming AIO-360-A1A Engine 2: Lycoming AIO-360-A1B 4.2 Type Certificate: Engine 1 & 2: EASA.IM.E.032 4.3 Limitations: Power 203 HP at 2700 rpm 5. Propeller: 5.1 Model: Hartzell HC-C2YK-1B()/()7666()-2 5.2 Type Certificate: EASA.IM.P.130 5.3 Number of blades: 2 5.4 Diameter: 1880 mm ± 0 mm (74 inch) 5.5 Sense of Rotation: Clockwise 6. Fluids: 6.1 Fuel: Aviation fuel 100/130 octane or 100 LL TE.CERT.00048-001 European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 13 of 18
6.2 Oil: unalloyed alloyed SAE 50 SAE 40 or 50 above 16 C SAE 40 SAE 40-1 C to +32 C SAE 30 SAE 40 or 20W-30-18 C to +21 C SAE 20 20W-30 below -12 7. Fluid capacities: 9.1 Fuel: Max. fuel: 170 l Usable fuel quantity: 166 l 9.2 Oil: 7,6 l 8. Air Speeds: Normal Utility Aerobatic Max. permissible - Speed V NE: 165 kt 177 kt 183 kt - Manoeuvring speed VA: 122 kt 126 kt 135 kt - Cruising speed VNO: 131 kt 131 kt 131 kt - Flaps extended VFE: 100 kt 100 kt 100 kt 9. (Reserved) 10. Load factors: Normal category: -1,52 g to 3,8 g Utility category: -1,76 g to 4,4 g Aerobatic category: -4,0 g to 6,0 g 11. Maximum Weights: Normal Utility Aerobatic Max. permissible: -Takeoff mass 1050 kg 980 kg 821 kg 12. Centre of Gravity Range: Normal category At 1050 kg: At 1000 kg At 821 kg or less: Utility category At 980 kg At 821 kg Aerobatic category At 821 kg 235,2 cm 239,2 cm 226,2 cm 239,2 cm 222,4 cm 239,2 cm 225,8 cm 232,2 cm 222,4 cm 232,2 cm 222,4 cm 226,6 cm TE.CERT.00048-001 European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 14 of 18
13. Datum: Reference plane: 200 cm forward of leading edge of wing Attitude: top chord of cockpit dome horizontal 14. Levelling Means: Refer to Maintenance Manual 15. Control surface deflections: Landing flaps Down 40 Ailerons Up 22 Down 22 Rudder Left 25 Right 25 Elevator Up 25 Down 30 Transverse trim Up 18 Down 18 tabs Elevator trim tabs Up 20 Down 20 Vertical trim tab Left 17 Right 17 Tolerance for all rudders: +/- 1 Control stick max. 4,6 mm 16. Minimum Flight Crew: 1 pilot (in Normal/Utility/Aerobatic categories) 17. Maximum Passenger Seating Capacity: Normal category: 2 passengers Utility category: 1 passenger Aerobatic category: 0 passengers (only 1 Pilot) 18. Baggage/Cargo Compartments: Max. payload weight on rear bench: 77 kg 19. Wheels and Tyres: Refer to Maintenance Manual 20. (Reserved): C.IV. Operating and Service Instructions 1. Manual for Operation: a) Flight Manual SIAT 223 K1, LBA-approved edition of 15 August 1968 with Annex, mass and balance statement, loading plan and equipment list b) Checklist SIAT 223 A1/K1 I and II c) Labelling as per Flight Manual 2. Technical Manual: a) Operations Manual SIAT 223 A1/K1 TE.CERT.00048-001 European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 15 of 18
b) Maintenance Manual SIAT 223 A1/K1 c) Lycoming Operator s Manual, Model IO-360 Series Aircraft Engines d) Hartzell Propeller Owner s Manual The listed documents can be obtained from the holder of type approval. C.V. Notes: 1. Eligible Serial Numbers: Siebelwerke ATG GmbH, 885 Donauwörth, Germany : 011 to 050 LaHispano Aviacion S.A., San Jacinto 68-76, Seville, Spain: 051 and subsequent 2. Type certification was issued on 28 August 1968 on application of Siebelwerke ATG GmbH Donauwörth, Germany and expanded to include Spanish production on 12 April 1972 TE.CERT.00048-001 European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 16 of 18
ADMINISTRATIVE SECTION I. Acronyms CAR DVL/PfL FAA LBA LSL N/A SAE TCDS Civil Aviation Regulations Deutsche Versuchsanstalt für Luftfahrt / Prüfstelle für Luftfahrtgerät Federal Aviation Administration Luftfahrt-Bundesamt Lärmschutzforderungen für Luftfahrzeuge Not applicable Society of Automotive Engineers Type Certificate Data Sheet II. Type Certificate Holder Record Day of Entry Company name (Legal Entity) 18.11.1952 Siebel-Werke-ATG GmbH (09.12.1964 Taken over by Bölkow Entwicklungen KG) (01.01.1966 Contract with SIAT WMD) 29.06.1972 Messerschmitt-Bölkow-Blohm GmbH * 01.04.1992 Messerschmitt-Bölkow-Blohm AG 30.09.1992 Deutsche Aerospace AG 02.01.1995 Daimler-Benz Aerospace AG 17.11.1998 Daimler Chrysler Aerospace AG 10.07.2000 EADS Deutschland GmbH 01.07.2014 Airbus Defence and Space GmbH *Siebel-Werke ATG GmbH ceased to exist as a legal entity by amalgamation into Messerschmitt-Bölkow-Blohm GmbH on June 29, 1972 TE.CERT.00048-001 European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 17 of 18
III. Change Record Issue Date Changes TC Issue No. & Date 1 02/02/2015 Initial issue after TC transfer 1, 02/02/2015 2 22/06/2015 Type Certificate Holder Record revised 1, 02/02/2015 3 13/11/2018 Change of TC holder address 2, 13/11/2018 TE.CERT.00048-001 European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 18 of 18