type-certificate data sheet...type-certificate data sheet no. easa.a.554 for siat 223 type...

TCDS No. EASA.A.554 SIAT 223

13 Nov. 2018 Issue 03

TE.CERT.00048-001 © European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. of 18 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.

An agency of the European Union

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



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



SECTION A: SIAT 223 V

A.I. General

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



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



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: 235,2 cm – 239,2 cm

@ 1000 kg 226,2 cm – 239,2 cm

@ 821 kg or less: 222,4 cm – 239,2 cm

Utility category

@ 980 kg 225,8 cm – 232,2 cm

@ 821 kg 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. 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 tabs

Up 18° Down 18°

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.



A.V. Notes:

1. Eligible Serial Numbers: 001 - 004



SECTION B: SIAT 223 A1

B.I. General

1. a) Type:

b) Model:

SIAT 223

SIAT 223 A1


Utility







La Hispano Aviacion S.A.

Sevilla, Spain

6. (Reserved)


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





B.III. Technical Characteristics and Operational Limitations


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


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



5. Propeller:






6. Fluids:




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°






7.2 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


Normal category

@ 1050 kg: 235,2 cm – 239,2 cm

@ 1000 kg 226,2 cm – 239,2 cm

@ 821 kg or less: 222,4 cm – 239,2 cm

Utility category

@ 980 kg 225,8 cm – 232,2 cm

@ 821 kg 222,4 cm – 232,2 cm









Up 18° Down 18°


Vertical trim tab Left 17° Right 17°



Tolerance for all rudders: +/- 1°

Control stick max. 4,6 mm


16. Minimum Flight Crew: 1 pilot







20. (Reserved):

B.IV. Operating and Service Instructions


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



a) Operations Manual SIAT 223 A1

b) Maintenance Manual SIAT 223 A1




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



SECTION C: SIAT 223 K1

C.I. General

1. a) Type:

b) Model:

SIAT 223

SIAT 223 K1


Utility

Aerobatic







La Hispano Aviacion S.A.

Sevilla, Spain

6. (Reserved)


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





C.III. Technical Characteristics and Operational Limitations


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, LBA-approved on 15 August 1968


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



5. Propeller:






6. Fluids:






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°




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


Normal category

At 1050 kg: 235,2 cm – 239,2 cm

At 1000 kg 226,2 cm – 239,2 cm

At 821 kg or less: 222,4 cm – 239,2 cm

Utility category

At 980 kg 225,8 cm – 232,2 cm

At 821 kg 222,4 cm – 232,2 cm

Aerobatic category

At 821 kg 222,4 cm – 226,6 cm












Up 18° Down 18°


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)




Aerobatic category: 0 passengers (only 1 Pilot)




20. (Reserved):

C.IV. Operating and Service Instructions


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



a) Operations Manual SIAT 223 A1/K1



b) Maintenance Manual SIAT 223 A1/K1




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



ADMINISTRATIVE SECTION

I. Acronyms

CAR Civil Aviation Regulations

DVL/PfL Deutsche Versuchsanstalt für Luftfahrt / Prüfstelle für Luftfahrtgerät

FAA Federal Aviation Administration

LBA Luftfahrt-Bundesamt

LSL Lärmschutzforderungen für Luftfahrzeuge

N/A Not applicable

SAE Society of Automotive Engineers

TCDS 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



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

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