TCDS No.: EASA.A.069 SAAB 2000 Issue: 10 Date: 27 June 2018 TYPE-CERTIFICATE DATA SHEET No. EASA.A.069 for SAAB 2000 Type Certificate Holder: Saab AB 581 88 Linköping SWEDEN For Models: SAAB 2000 TE.CERT.00051-001 © European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 1 of 14 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union Intentionally left blank TE.CERT.00051-001 © European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 2 of 14 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union TCDS No.: EASA.A.069 SAA Issue: 10 Date: 27 June 2018 TABLE OF CONTENTS SECTION 1: SAAB 2000 .................................................................................................................. 5 I. General ............................................................................................................................. 5 1. Type/ Model/ Variant .............................................................................................................. 5 2. Performance Class ................................................................................................................... 5 3. Certifying Authority ................................................................................................................. 5 4. Manufacturer .......................................................................................................................... 5 5. State of Design Authority Certification Application Date........................................................ 5 6. EASA Type Certification Application Date ............................................................................... 5 7. State of Design Authority Type Certificate Date ..................................................................... 5 8. EASA Type Certification Date .................................................................................................. 5 9. Production conditions ............................................................................................................. 5 II. Certification Basis .............................................................................................................. 6 1. Reference Date for determining the applicable requirements ............................................... 6 2. State of Design Airworthiness Authority Type Certification Data Sheet No. .......................... 6 3. State of Design Airworthiness Authority Certification Basis ................................................... 6 4. EASA Airworthiness Requirements ......................................................................................... 6 5. Special Conditions ................................................................................................................... 6 6. Exemptions .............................................................................................................................. 7 7. Deviations ................................................................................................................................ 7 8. Equivalent Safety Findings....................................................................................................... 7 9. Elect To Comply ....................................................................................................................... 7 11. Environmental Protection ................................................................................................... 8 III. Technical Characteristics and Operational Limitations .................................................... 8 1. Type Design Definition ............................................................................................................ 8 2. Description .............................................................................................................................. 8 3. Equipment ............................................................................................................................... 8 4. Dimensions .............................................................................................................................. 8 5. Engines .................................................................................................................................... 8 6. Auxiliary Power Unit ................................................................................................................ 9 7. Propellers ................................................................................................................................ 9 8. Fluids (Fuel, Oil, Additives, Hydraulics) ................................................................................... 9 9. Fluid Capacities ........................................................................................................................ 9 10. Airspeed Limits .................................................................................................................... 9 11. Flight Envelope .................................................................................................................. 10 12. Operating Limitations ........................................................................................................ 10 13. Maximum Certified Masses ............................................................................................... 10 14. Centre of Gravity Range .................................................................................................... 11 15. Datum ................................................................................................................................ 11 16. Mean Aerodynamic Chord (MAC) ..................................................................................... 11 17. Levelling Means ................................................................................................................. 11 18. Minimum Flight Crew ........................................................................................................ 11 19. Minimum Cabin Crew ........................................................................................................ 11 20. Maximum Seating Capacity and Exit configuration........................................................... 11 21. Baggage/ Cargo Compartment .......................................................................................... 11 22. Wheels and Tyres .............................................................................................................. 12 23. ETOPS ................................................................................................................................ 12 IV. Operating and Service Instructions ............................................................................... 12 TE.CERT.00051-001 © European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 3 of 14 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union TCDS No.: EASA.A.069 SAAB 2000 Issue: 10 Date: 27 June 2018 1. Aeroplane Flight Manual (AFM) ............................................................................................ 12 2. Instructions for Continued Airworthiness and Airworthiness Limitations ............................ 12 V. Operational Suitability Data (OSD) ................................................................................... 12 VI. Notes .......................................................................................................................... 13 SECTION: ADMINISTRATIVE ........................................................................................................ 14 I. Acronyms and Abbreviations ........................................................................................... 14 II. Type Certificate Holder Record ........................................................................................ 14 III. Change Record ............................................................................................................ 14 TE.CERT.00051-001 © European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 4 of 14 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union TCDS No.: EASA.A.069 SAAB 2000 Issue: 10 Date: 27 June 2018 SECTION 1: SAAB 2000 I. General 1. Type/ Model/ Variant SAAB 2000 2. Performance Class A 3. Certifying Authority European Aviation Safety Agency (EASA) Postfach 101253 D-50452 Köln Deutschland 4. Manufacturer Saab AB 581 88 Linköping SWEDEN 5. State of Design Authority Certification Application Date 28 April 1989 6. EASA Type Certification Application Date N/A 7. State of Design Authority Type Certificate Date 31 March 1994 Note: Original LFV TC A 1/94 was replaced by the EASA TC EASA.A.069 8. EASA Type Certification Date N/A 9. Production conditions N/A TE.CERT.00051-001 © European Aviation Safety Agency, 2018. All rights reserved. ISO9001 Certified. Page 5 of 14 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union TCDS No.: EASA.A.06 SAAB 2000 Issue: 10 Date: 27 June 2018 II. Certification Basis 1. Reference