DA20-C1 AIRPLANE FLIGHT MANUAL

DOT-appr 2-33 28-Feb-14 LIST OF EFFECTIVE PAGES Ch. Page Date 3 DOT-appr 3-1 15-May-12 DOT-appr 3-2 15-May-12 DOT-appr 3-3 15-May-12 DOT-appr 3-4 15-May-12 DOT-appr 3-5 15-May-12 DOT-appr 3-6 15-May-12 DOT-appr 3-7 15-May-12 DOT-appr 3-8 15-May-12 DOT-appr 3-9 15-May-12 DOT-appr 3-10 15-May-12 DOT-appr 3-11 15-May-12 DOT-appr 3-12 15-May-12 DOT-appr 3-13 15-May-12 DOT-appr 3-14 15-May-12 DOT-appr 3-15 12-Feb-13 DOT-appr 3-16 15-May-12 DOT-appr 3-17 15-May-12 DOT-appr 3-18 15-May-12 DOT-appr 3-19 15-May-12 DOT-appr 3-20 15-May-12 DOT-appr 3-21 15-May-12 DOT-appr 3-22 15-May-12 4 DOT-appr 4-1 15-May-12 DOT-appr 4-2 15-May-12 DOT-appr 4-3 15-May-12 DOT-appr 4-4 12-Feb-13 DOT-appr 4-5 15-May-12 LIST OF EFFECTIVE PAGES Ch. Page Date Introduction DA20-C1 Flight Manual Page 0 - 7 DOC # DA202-C1 Revision 28 February 28, 2014 4 DOT-appr 4-6 15-May-12 DOT-appr 4-7 15-May-12 DOT-appr 4-8 15-May-12 DOT-appr 4-9 12-Feb-13 DOT-appr 4-10 15-May-12 DOT-appr 4-11 15-May-12 DOT-appr 4-12 15-May-12 DOT-appr 4-13 15-May-12 DOT-appr 4-14 15-May-12 DOT-appr 4-15 15-May-12 DOT-appr 4-16 15-May-12 DOT-appr 4-17 15-May-12 DOT-appr 4-18 15-May-12 DOT-appr 4-19 15-May-12 DOT-appr 4-20 15-May-12 DOT-appr 4-21 15-May-12 DOT-appr 4-22 15-May-12 DOT-appr 4-23 15-May-12 DOT-appr 4-24 15-May-12 DOT-appr 4-25 12-Feb-13 DOT-appr 4-26 15-May-12 DOT-appr 4-27 15-May-12 DOT-appr 4-28 15-May-12 DOT-appr 4-29 15-May-12 DOT-appr 4-30 15-May-12 5 DOT-appr 5-1 12-Feb-13 DOT-appr 5-2 15-May-12 LIST OF EFFECTIVE PAGES Ch. Page Date 5 DOT-appr 5-3 15-May-12 DOT-appr 5-4 15-May-12 DOT-appr 5-5 15-May-12 DOT-appr 5-6 12-Feb-13 DOT-appr 5-7 12-Feb-13 DOT-appr 5-8 12-Feb-13 DOT-appr 5-9 12-Feb-13 DOT-appr 5-10 28-Feb-14 DOT-appr 5-11 12-Feb-13 DOT-appr 5-12 12-Feb-13 DOT-appr 5-13 12-Feb-13 DOT-appr 5-14 12-Feb-13 DOT-appr 5-15 12-Feb-13 DOT-appr 5-16 12-Feb-13 DOT-appr 5-17 12-Feb-13 DOT-appr 5-18 12-Feb-13 6 DOT-appr 6-1 15-May-12 DOT-appr 6-2 15-May-12 DOT-appr 6-3 15-May-12 DOT-appr 6-4 15-May-12 DOT-appr 6-5 15-May-12 DOT-appr 6-6 15-May-12 DOT-appr 6-7 15-May-12 DOT-appr 6-8 15-May-12 DOT-appr 6-9 15-May-12 DOT-appr 6-10 12-Feb-13 DOT-appr 6-11 15-May-12 LIST OF EFFECTIVE PAGES Ch. Page Date Introduction DA20-C1 Flight Manual Page 0 - 8 DOC # DA202-C1 February 28, 2014 Revision 28 6 DOT-appr 6-12 15-May-12 DOT-appr 6-13 15-May-12 DOT-appr 6-14 15-May-12 DOT-appr 6-15 28-Feb-14 DOT-appr 6-16 28-Feb-14 DOT-appr 6-17 28-Feb-14 DOT-appr 6-18 28-Feb-14 DOT-appr 6-19 28-Feb-14 DOT-appr 6-20 28-Feb-14 DOT-appr 6-21 28-Feb-14 DOT-appr 6-22 28-Feb-14 7 7-1 12-Feb-13 7-2 12-Feb-13 7-3 12-Feb-13 7-4 15-May-12 7-5 15-May-12 7-6 15-May-12 7-7 15-May-12 7-8 15-May-12 7-9 15-May-12 7-10 12-Feb-13 7-11 12-Feb-13 7-12 12-Feb-13 7-13 12-Feb-13 7-14 12-Feb-13 7-15 12-Feb-13 7-16 12-Feb-13 LIST OF EFFECTIVE PAGES Ch. Page Date 7 7-17 12-Feb-13 7-18 12-Feb-13 7-19 12-Feb-13 7-20 12-Feb-13 7-21 12-Feb-13 7-22 12-Feb-13 7-23 12-Feb-13 7-24 12-Feb-13 7-25 12-Feb-13 7-26 12-Feb-13 7-27 12-Feb-13 7-28 12-Feb-13 7-29 12-Feb-13 7-30 12-Feb-13 7-31 12-Feb-13 7-32 12-Feb-13 8 8-1 15-May-12 8-2 15-May-12 8-3 15-May-12 8-4 15-May-12 8-5 15-May-12 8-6 15-May-12 8-7 15-May-12 8-8 15-May-12 8-9 15-May-12 8-10 15-May-12 8-11 15-May-12 LIST OF EFFECTIVE PAGES Ch. Page Date Introduction DA20-C1 Flight Manual Page 0 - 9 DOC # DA202-C1 Revision 28 February 28, 2014 8 8-12 15-May-12 9 9-1 15-May-12 9-2 15-May-12 9-3 15-May-12 9-4 12-Feb-13 9-5 12-Feb-13 9-6 12-Feb-13 LIST OF EFFECTIVE PAGES Ch. Page Date Introduction DA20-C1 Flight Manual Intentionally Left Blank Page 0 - 10 DOC # DA202-C1 Revision 28 February 28, 2014 Introduction DA20-C1 Flight Manual Page 0 - 11 DOC # DA202-C1 Revision 27 February 12, 2013 SUPPLEMENTS LIST OF EFFECTIVE PAGES NOTE It is only necessary to maintain those Supplements which pertain to optional equipment that may be installed in your airplane. Refer to Page 9-2 for the Index of Supplements. LIST OF EFFECTIVE PAGES Supp Page Date S1 DOT-appr S1-1 15-May-12 DOT-appr S1-2 15-May-12 DOT-appr S1-3 15-May-12 DOT-appr S1-4 15-May-12 DOT-appr S1-5 15-May-12 DOT-appr S1-6 15-May-12 DOT-appr S1-7 15-May-12 DOT-appr S1-8 15-May-12 DOT-appr S1-9 15-May-12 DOT-appr S1-10 15-May-12 DOT-appr S1-11 15-May-12 DOT-appr S1-12 15-May-12 DOT-appr S1-13 15-May-12 DOT-appr S1-14 15-May-12 DOT-appr S1-15 15-May-12 DOT-appr S1-16 12-Feb-13 S2 DOT-appr S2-1 15-May-12 DOT-appr S2-2 15-May-12 DOT-appr S2-3 15-May-12 S2 DOT-appr S2-4 15-May-12 DOT-appr S2-5 15-May-12 DOT-appr S2-6 15-May-12 S3 DOT-appr S3-1 15-May-12 DOT-appr S3-2 15-May-12 DOT-appr S3-3 12-Feb-13 DOT-appr S3-4 15-May-12 DOT-appr S3-5 15-May-12 DOT-appr S3-6 15-May-12 S4 Supplement 4 Removed S5 DOT-appr S5-1 15-May-12 DOT-appr S5-2 15-May-12 DOT-appr S5-3 15-May-12 DOT-appr S5-4 15-May-12 DOT-appr S5-5 15-May-12 DOT-appr S5-6 15-May-12 DOT-appr S5-7 15-May-12 DOT-appr S5-8 15-May-12 DOT-appr S5-9 15-May-12 DOT-appr S5-10 12-Feb-13 DOT-appr S5-11 15-May-12 DOT-appr S5-12 15-May-12 DOT-appr S5-13 15-May-12 DOT-appr S5-14 15-May-12 LIST OF EFFECTIVE PAGES Supp Page Date Introduction DA20-C1 Flight Manual Page 0 - 12 DOC # DA202-C1 February 12, 2013 Revision 27 S6 DOT-appr S6-1 15-May-12 DOT-appr S6-2 15-May-12 DOT-appr S6-3 15-May-12 DOT-appr S6-4 15-May-12 DOT-appr S6-5 15-May-12 DOT-appr S6-6 12-Feb-13 DOT-appr S6-7 15-May-12 DOT-appr S6-8 15-May-12 DOT-appr S6-9 15-May-12 DOT-appr S6-10 15-May-12 S7 DOT-appr S7-1 15-May-12 DOT-appr S7-2 15-May-12 DOT-appr S7-3 15-May-12 DOT-appr S7-4 15-May-12 DOT-appr S7-5 15-May-12 DOT-appr S7-6 15-May-12 DOT-appr S7-7 12-Feb-13 DOT-appr S7-8 15-May-12 DOT-appr S7-9 15-May-12 DOT-appr S7-10 15-May-12 S8 DOT-appr S8-1 15-May-12 DOT-appr S8-2 15-May-12 DOT-appr S8-3 12-Feb-13 DOT-appr S8-4 15-May-12 LIST OF EFFECTIVE PAGES Supp Page Date S9 DOT-appr S9-1 15-May-12 DOT-appr S9-2 15-May-12 DOT-appr S9-3 15-May-12 DOT-appr S9-4 12-Feb-13 S10 DOT-appr S10-1 15-May-12 DOT-appr S10-2 15-May-12 DOT-appr S10-3 12-Feb-13 DOT-appr S10-4 15-May-12 S11 DOT-appr S11-1 15-May-12 DOT-appr S11-2 15-May-12 DOT-appr S11-3 15-May-12 DOT-appr S11-4 15-May-12 DOT-appr S11-5 15-May-12 DOT-appr S11-6 15-May-12 DOT-appr S11-7 12-Feb-13 DOT-appr S11-8 15-May-12 S12 DOT-appr S12-1 15-May-12 DOT-appr S12-2 15-May-12 DOT-appr S12-3 15-May-12 DOT-appr S12-4 15-May-12 DOT-appr S12-5 15-May-12 DOT-appr S12-6 15-May-12 DOT-appr S12-7 15-May-12 DOT-appr S12-8 15-May-12 LIST OF EFFECTIVE PAGES Supp Page Date Introduction DA20-C1 Flight Manual Page 0 - 13 DOC # DA202-C1 Revision 28 February 28, 2014 S12 DOT-appr S12-9 12-Feb-13 DOT-appr S12-10 15-May-12 S13 DOT-appr S13-1 15-May-12 DOT-appr S13-2 15-May-12 DOT-appr S13-3 15-May-12 DOT-appr S13-4 28-Feb-14 DOT-appr S13-5 15-May-12 DOT-appr S13-6 15-May-12 DOT-appr S13-7 15-May-12 DOT-appr S13-8 15-May-12 DOT-appr S13-9 15-May-12 DOT-appr S13-10 28-Feb-14 DOT-appr S13-11 28-Feb-14 DOT-appr S1-12 28-Feb-14 DOT-appr S13-13 28-Feb-14 DOT-appr S13-14 28-Feb-14 DOT-appr S13-15 28-Feb-14 DOT-appr S13-16 28-Feb-14 DOT-appr S13-17 28-Feb-14 DOT-appr S13-18 28-Feb-14 DOT-appr S13-19 28-Feb-14 DOT-appr S13-20 28-Feb-14 DOT-appr S13-21 28-Feb-14 DOT-appr S13-22 28-Feb-14 DOT-appr S13-23 28-Feb-14 DOT-appr S13-24 28-Feb-14 DOT-appr S13-25 28-Feb-14 LIST OF EFFECTIVE PAGES Supp Page Date S13 DOT-appr S13-26 28-Feb-14 DOT-appr S13-27 28-Feb-14 DOT-appr S13-28 28-Feb-14 S14 DOT-appr S14-1 15-May-12 DOT-appr S14-2 15-May-12 DOT-appr S14-3 15-May-12 DOT-appr S14-4 15-May-12 DOT-appr S14-5 15-May-12 DOT-appr S14-6 15-May-12 DOT-appr S14-7 12-Feb-13 DOT-appr S14-8 15-May-12 S15 DOT-appr S15-1 12-Feb-13 DOT-appr S15-2 12-Feb-13 DOT-appr S15-3 12-Feb-13 DOT-appr S15-4 12-Feb-13 DOT-appr S15-5 12-Feb-13 DOT-appr S15-6 12-Feb-13 DOT-appr S15-7 12-Feb-13 DOT-appr S15-8 12-Feb-13 DOT-appr S15-9 12-Feb-13 DOT-appr S15-10 12-Feb-13 DOT-appr S15-11 12-Feb-13 DOT-appr S15-12 12-Feb-13 DOT-appr S15-13 12-Feb-13 DOT-appr S15-14 12-Feb-13 LIST OF EFFECTIVE PAGES Supp Page Date Introduction DA20-C1 Flight Manual Page 0 - 14 DOC # DA202-C1 February 12, 2013 Revision 27 S16 DOT-appr S16-1 12-Feb-13 DOT-appr S16-2 12-Feb-13 S16 DOT-appr S16-3 12-Feb-13 DOT-appr S16-4 12-Feb-13 DOT-appr S16-5 12-Feb-13 DOT-appr S16-6 12-Feb-13 S17 DOT-appr S17-1 12-Feb-13 DOT-appr S17-2 12-Feb-13 DOT-appr S17-3 12-Feb-13 DOT-appr S17-4 12-Feb-13 DOT-appr S17-5 12-Feb-13 DOT-appr S17-6 12-Feb-13 LIST OF EFFECTIVE PAGES Supp Page Date Page 0 - 15 Introduction DA20-C1 Flight Manual DOC # DA202-C1 Revision 28 Febraury 28, 2014 RECORD OF REVISIONS Revisions and Temporary Revisions to this manual, with the exception of actual weighing data, are recorded in the following table. Revisions and Temporary Revisions of approved sections must be endorsed by the responsible airworthiness authority. In the Manual Revision, new or amended text will be indicated by a bold black vertical line in the left hand margin of a revised page. The Manual Revision number and Document number will be shown on the bottom right hand corner of the page on even pages and will be shown on the bottom left hand corner of the page on odd pages. Page numbers will show on the opposite corner of the pages. Temporary Revisions are used to provide information on systems or equipment until the next permanent Revision of the Airplane Flight Manual. The airplane may only be operated if the Flight Manual is up to date. Approved Rev. No. Affected Pages Date Name Rev 17 0-4, 0-5, 0-6, 0-9, 2 -7, 2-17, 4-16, 7-12, 7-13, S2-1, S2-2, S2-3, S2-4, S4-4. 19 Mar 04 W. Jupp Chief, Flight Test for Director, Aircraft Certification Transport Canada Rev 18 0-4, 0-5, 0-9 6-13, 6-14, 6-15, 6-16. 22 Mar 05 W. Jupp Chief, Flight Test for Director, Aircraft Certification Transport Canada Rev 19 0-4, 0-5, 0-9, 2-5, 7-15, 7-16. 24 Jun 05 W. Jupp Chief, Flight Test for Director, Aircraft Certification Transport Canada Rev 20 0-4, 0-6, 0-9, S4-1,S4-2, S4-3, S4-4, S4-5, S4-6, S4-7, S4-8, S4-9, S4-10, S4-11, S4-12, S4-13, S4-14, S4-15. 18 Aug 05 W. Jupp Chief, Flight Test for Director, Aircraft Certification Transport Canada Introduction DA20-C1 Flight Manual Page 0 - 16 DOC # DA202-C1 February 28, 2014 Revision 28 Rev 21 0-4, 0-5, 0-10 , 0-11, 0-12, 6-15, 6-16, 7-6. 05 Sep 06 W. Jupp Chief, Flight Test for Director, Aircraft Certification Transport Canada TR-1 0-10, 2-5. 02 Oct 07 W. Jupp Chief, Flight Test for Director, Aircraft Certification Transport Canada Rev 22 0-4, 0-5, 0-6, 0-10, 2-4, 2-7, 2-17, 4-14, 4-20, 5-20, S4-4, S4-12, S4-13. 02 Nov 07 W. Jupp Chief, Flight Test for Director, Aircraft Certification Transport Canada Rev 23 0-4, 0-6, 0-10, 0-11, 2-1, 2-4, 2-7, 2-8,2-9,2-10, 2-11, 2-12, 2-13, 2-14, 2-15, 2-16, 2-17, 2-18, 2-19, 4-14, 4-20, S4-1, S4-4, S4-5, S4-6, S4-7, S4-8, S4-9, S4-10, S4-11, S4-12, S4-13, S4-14, S4-15, S4-16. 11 Dec 07 W. Jupp Chief, Flight Test for Director, Aircraft Certification Transport Canada TR 08-01 0-10, 2-19, 4-5, 6-13, 6-14, 6-15, 6-16. 25 Aug 08 R. Walker A/Chief, Flight Test for Director, Aircraft Certification Transport Canada Rev 24 All 30 Apr 09 R. Walker A/Chief, Flight Test for Director, Aircraft Certification Transport Canada Approved Rev. No. Affected Pages Date Name Page 0 - 17 Introduction DA20-C1 Flight Manual DOC # DA202-C1 Revision 28 Febraury 28, 2014 TR 09-02 4-10, 4-11, 4-12. 30 Jun 09 R. Walker A/Chief, Flight Test for Director, Aircraft Certification Transport Canada TR 09-03 0-9, 0-10, 6-13 thru 6-20, 9-1, 9-2 and 9-S13-1 thru 9-S13-24. 12 Nov 09 D. Stephen A/Chief, Flight Test for Director, Aircraft Certification Transport Canada TR 10-01 0-10, 6-3 and 6-5. 26 Feb 10 Jim Martin for Chief, Flight Test for Director, Aircraft Certification Transport Canada TR 10-02 0-10, 4-9, 7-11. 28 Feb 10 Jim Martin for Chief, Flight Test for Director, Aircraft Certification Transport Canada Rev 25 Cover Page, 0-1, 0-2, 0-5 thru 0-20, 1-1 thru 1-14, 2-1, 2-5, 2-10 thru 2-20, 4-9 thru 4-12, 4-14, 5-8, 5-10, 5-12, 6-3, 6-5, 6-16, 6-17, 7-1, 7-2, 7-9, 7-12 thru 7-24, 8-1 thru 8-10, 9-1, 9-2. S4-14, S4-16, S11-1 thru S11-6, S12-1 thru S12-8 S13-1 thru S13-22. 07 Apr 10 W. Istchenko Chief, Flight Test for Director, Aircraft Certification Transport Canada TR 10-03 0-13, 2-19, 3-5, 4-10 thru 4-12A, 7-14, S1-8 thru S1-11. 20 Dec 10 W. Istchenko Chief, Flight Test for Director, Aircraft Certification Transport Canada Approved Rev. No. Affected Pages Date Name Introduction DA20-C1 Flight Manual Page 0 - 18 DOC # DA202-C1 February 28, 2014 Revision 28 TR 11-01 0-13, 2-10, S4-13. 01 Aug 11 W. Istchenko Chief, Flight Test for Director, Aircraft Certification Transport Canada TR 11-02 0-13, 2-9, 2-10. 15 Aug 11 W. Istchenko Chief, Flight Test for Director, Aircraft Certification Transport Canada TR 11-03 0-13, S4-16. 20 Dec 11 W. Istchenko Chief, Flight Test for Director, Aircraft Certification Transport Canada Rev 26 ALL 03 Jul 12 W. Istchenko Chief, Flight Test for Director, National Aircraft Certification Transport Canada TR12-01 0-20, 2-5, 2-12, 6-15, and 6-19. 14 Aug 12 W. Istchenko Chief, Flight Test for Director, National Aircraft Certification Transport Canada TR12-02 0-20, 2-7 and 4-25. 23 Nov 12 W. Istchenko Chief, Flight Test for Director, National Aircraft Certification Transport Canada Approved Rev. No. Affected Pages Date Name Introduction DA20-C1 Flight Manual Page 0 - 20 DOC # DA202-C1 Intentionally left blank Revision 28 February 28, 2014 Page 0 - 21 Introduction DA20-C1 Flight Manual DOC # DA202-C1 Revision 26 May 15, 2012 REVISIONS LOG This Revisions Log should be used to record all Permanent Revisions issued and inserted into this manual. The affected pages of any revision must be inserted into the manual as well as the Record of Revisions upon receipt. The pages superseded by the revision must be removed and destroyed. The Revisions Log should be updated by hand. Changes are identified on those pages affected by a revision bar. Rev. No. Date Issued: Inserted On: Inserted By: Issue 1 19 Dec 97 19 Dec 97 Diamond Aircraft Rev 1 13 Aug 98 13 Aug 98 Diamond Aircraft Rev 2 28 Aug 98 28 Aug 98 Diamond Aircraft Rev 3 08 Dec 98 08 Dec 98 Diamond Aircraft Rev 4 05 Jan 99 05 Jan 99 Diamond Aircraft Rev 5 10 Mar 99 10 Mar 99 Diamond Aircraft Rev 6 07 Apr 99 07 Apr 99 Diamond Aircraft Rev 7 21 Jun 99 21 Jun 99 Diamond Aircraft Rev 8 07 Dec 99 07 Dec 99 Diamond Aircraft Rev 9 11 Apr 00 11 Apr 00 Diamond Aircraft Rev 10 14 Aug 00 14 Aug 00 Diamond Aircraft Rev 11 20 Mar 01 20 Mar 01 Diamond Aircraft Rev 12 16 Apr 01 16 Apr 01 Diamond Aircraft Rev 13 28 May 01 28 May 01 Diamond Aircraft Rev 14 09 Aug 01 09 Aug 01 Diamond Aircraft Rev 15 23 Apr 02 23 Apr 02 Diamond Aircraft Rev 16 18 Oct 02 18 Oct 02 Diamond Aircraft Rev 17 19 Mar 04 19 Mar 04 Diamond Aircraft Rev 18 22 Mar 05 22 Mar 05 Diamond Aircraft Introduction DA20-C1 Flight Manual Page 0 - 22 DOC # DA202-C1 Febraury 28, 2014 Revision 28 Rev 19 24 Jun 05 24 Jun 05 Diamond Aircraft Rev 20 18 Aug 05 18 Aug 05 Diamond Aircraft Rev 21 05 Sep 06 05 Sep 06 Diamond Aircraft Rev 22 02 Nov 07 02 Nov 07 Diamond Aircraft Rev 23 11 Dec 07 11 Dec 07 Diamond Aircraft Rev 24 16 Apr 09 26 Jun 09 Diamond Aircraft Rev 25 06 Apr 10 16 Apr 10 Diamond Aircraft Rev 26 15 May 12 10 Jul 12 Diamond Aircraft Rev 27 12 Feb 13 01 Apr 2013 Diamond Aircraft Rev 28 28 Feb 14 Rev. No. Date Issued: Inserted On: Inserted By: Page 0 - 23 Introduction DA20-C1 Flight Manual DOC # DA202-C1 Revision 28 February 28, 2014 REVISION HIGHLIGHTS GENERAL The table below highlights the changes that have been incorporated into Revision 28. CHAPTER PAGES HIGHLIGHTS Cover Page Cover page Cover Page revised to show Revision 28, dated February 28, 2014. 0 0-5 thru 0-10 and 0-13 List of Effective Pages (LOEP) and Supplements LOEP revised. Rev bars inserted adjacent to the changed pages. 0-15-0-20 Removed old revision information which reduced record of revision pages by 2 New Revision information added on page 0-19. 0-21 and 0-22 Pagination and Revision Log entries. 0-23 and 0-24 Pagination and Revision Highlights pages for Revision 28. 0-25 and 0-28 Pagination 2 2-28 and 2-29 Added new instrument panel graphics 2-30 thru 2-34 Pagination 5 5-9 Revised Take Off chart to correct wind component 6 6-15 thru 6-21 Revised equipment list Supplement 13 S13-4 Added new equipment software version S13-10 Added new instrument panel graphic S13-11 thru S13-22 Pagination S13-23 and S13-24 Added New Instrument panel graphic S13-25 and S13-26 GTN 650 Details Introduction DA20-C1 Flight Manual Page 0 - 24 DOC # DA202-C1 February 28, 2014 Revision 28 Supplement 13 S13-27 andS13- 28 Pagination CHAPTER PAGES HIGHLIGHTS Page 0 - 25 Introduction DA20-C1 Flight Manual DOC # DA202-C1 Revision 28 February 28, 2014 TEMPORARY REVISIONS LOG All Temporary Revisions (TRs) to this manual must be inserted and signed as being inserted into the manual in the following table. Temporary Revision Number Date Issued Inserted Date Name TR-1 02 Oct 07 02 Oct 07 Diamond Aircraft TR 08-01 25 Aug 08 25 Aug 08 Diamond Aircraft TR 09-02 30 Jun 09 30 Jun 09 Diamond Aircraft TR 09-03 12 Nov 09 12 Nov 09 Diamond Aircraft TR 10-01 26 Feb 10 26 Feb 10 Diamond Aircraft TR 10-02 28 Feb 10 28 Feb 10 Diamond Aircraft TR 10-03 20 Dec 10 20 Dec 10 Diamond Aircraft TR 11-01 01 Aug 11 01 Aug 11 Diamond Aircraft TR 11-02 15 Aug 11 15 Aug 11 Diamond Aircraft TR 11-03 20 Dec 11 20 Dec 11 Diamond Aircraft NOTE: All the Temporary Revisions above have been incorporated into the AFM at Rev 26. TR 12-01 01 Aug 12 14 Aug 12 Diamond Aircraft TR 12-02 09 Oct 12 23 Nov 12 Diamond Aircraft NOTE: The Temporary Revisions above have been incorporated into the AFM at Rev 27. Introduction DA20-C1 Flight Manual Page 0 - 26 DOC # DA202-C1 Febraury 28, 2014 Revision 28 Temporary Revision Number Date Issued Inserted Date Name Page 0 - 27 Introduction DA20-C1 Flight Manual DOC # DA202-C1 Revision 28 February 28, 2014 SUBSCRIPTION SERVICE Diamond Aircraft Publications Revision Subscription Contacts To ensure safe operation and maintenance of the DA20-C1 aircraft, it is recommended that operators verify that their documentation is at the correct revision levels. For revision and subscription service please contact the following: 1. DA20-C1 related manuals and publications. North America, Australia and Africa: Other: Diamond Aircraft Industries Inc. Diamond Aircraft Industries GmbH Customer Support Customer Support 1560 Crumlin Sideroad N.A. Otto-Strasse 5 London, Ontario A-2700 Wiener Neustadt Canada. Austria N5V 1S2 Phone: 519-457-4041 Phone: +43-(0) 2622-26700 Fax: 519-457-4060 Fax: +43-(0) 2622-26780 2. Teledyne Continental Motors IO 240B related manuals and publications. North America: Other: Teledyne Continental Motors Contact a Teledyne Continental P.O. Box 90 Motors distributor. Mobile, Alabama 36601 Phone: 334-438-3411 3. Sensenich Propeller Model W69EK7-63, W69EK7-63G, W69EK-63 related manuals and publications. North America: Sensenich Wood Propeller Company 2008 Wood Court Plant City, Florida USA Phone: 813-752-3711 Fax: 813-752-2818 Introduction DA20-C1 Flight Manual Page 0 - 28 DOC # DA202-C1 Intentionally left blank Revision 28 February 28, 2014 Page 1 - 1 General DA20-C1 Flight Manual DOC # DA202-C1 Revision 26 May 15, 2012 CHAPTER 1 GENERAL TABLE OF CONTENTS PAGE 1.1 INTRODUCTION .................................................................................. 3 1.2 CERTIFICATION BASIS ....................................................................... 3 1.3 WARNINGS, CAUTIONS AND NOTES ................................................ 4 1.4 THREE-VIEW-DRAWING OF THE AIRPLANE .................................... 5 1.5 DIMENSIONS ....................................................................................... 6 1.5.1 Overall Dimensions .................................................................. 6 1.5.2 Wing ......................................................................................... 6 1.5.3 Horizontal Stabilizer ................................................................. 6 1.5.4 Landing Gear ........................................................................... 6 1.6 ENGINE ................................................................................................ 7 1.7 PROPELLER ........................................................................................ 7 1.8 FUEL ..................................................................................................... 7 1.9 LUBRICANT AND COOLANT ............................................................... 8 1.9.1 Lubricant .................................................................................. 8 1.10 WEIGHT .............................................................................................. 10 1.11 LIST OF DEFINITIONS AND ABBREVIATIONS .................................11 1.11.1 Airspeeds ................................................................................11 1.11.2 Meteorological Terms ............................................................. 12 General DA20-C1 Flight Manual Page 1 - 2 DOC # DA202-C1 May 15, 2012 Revision 26 PAGE 1.11.3 Powerplant ..............................................................................12 1.11.4 Flight Performance and Flight Planning ..................................13 1.11.5 Weight and Balance ................................................................13 1.11.6 Equipment ...............................................................................14 1.11.7 Miscellaneous .........................................................................14 1.12 CONVERSION FACTORS ...................................................................15 1.12.1 Length or Altitude ....................................................................15 1.12.2 Speed ......................................................................................15 1.12.3 Pressure ..................................................................................15 1.12.4 Weight .....................................................................................15 1.12.5 Volume ....................................................................................16 Page 1 - 3 General DA20-C1 Flight Manual DOC # DA202-C1 Revision 26 May 15, 2012 1.1 INTRODUCTION The Airplane Flight Manual has been prepared to provide pilots and instructors with information for the safe and efficient operation of this airplane. This Manual includes the material required by JAR-VLA and Transport Canada Airworthiness Manual (AWM) Chapter 523-VLA. It also contains supplemental data supplied by the airplane manufacturer which can be useful to the pilot. The Flight Manual conforms to a standard equipped DA20-C1 airplane. Any optional equipment installed on request of the customer (COMM, NAV, etc.) is not considered. For the operation of optional equipment the Operation Manual of the respective vendor must be used. For permissible accessories refer to the Equipment List, Section 6.5. 1.2 CERTIFICATION BASIS The DA20-C1 has been approved by Transport Canada in accordance with the Canadian Airworthiness Manual (AWM) Chapter 523-VLA., Type Certificate No. A-191. Category of Airworthiness: UTILITY Noise Certification Basis: (a) Canadian Airworthiness Manual Chapter 516 (b) FAA Part 36 (c) ICAO Annex 16. General DA20-C1 Flight Manual Page 1 - 4 DOC # DA202-C1 May 15, 2012 Revision 26 1.3 WARNINGS, CAUTIONS AND NOTES The following definitions apply to warnings, cautions, and notes used in the Flight Manual:: A WARNING MEANS THAT THE NON-OBSERVATION OF THE CORRESPONDING PROCEDURE LEADS TO AN IMMEDIATE OR IMPORTANT DEGRADATION IN FLIGHT SAFETY. A CAUTION MEANS THAT THE NON-OBSERVATION OF THE CORRESPONDING PROCEDURE LEADS TO A MINOR OR TO A LONG TERM DEGRADATION IN FLIGHT SAFETY. A Note draws the attention to any special item not directly related to safety but which is important or unusual. WARNING CAUTION NOTE Page 1 - 5 General DA20-C1 Flight Manual DOC # DA202-C1 Revision 26 May 15, 2012 1.4 THREE-VIEW-DRAWING OF THE AIRPLANE 1600 mm (5 ft 3 in) 2160 mm (7 ft 1 in) 1860 mm (6 ft 1 in) 7240 mm (23 ft 9 in) 10890 mm (35 ft 9 in) General DA20-C1 Flight Manual Page 1 - 6 DOC # DA202-C1 May 15, 2012 Revision 26 1.5 DIMENSIONS 1.5.1 Overall Dimensions Span: 35 ft 9 in (10.89 m) Length: 23 ft 9 in (7.24 m) Height: 7 ft 1 in (2.16 m) 1.5.2 WING Airfoil: Wortmann FX 63-137/20 HOAC Wing Area: 125 sq ft (11.6 m2) Mean Aerodynamic Chord (MAC): 3 ft 6.9 in (1.09 m) Aspect Ratio: 10.0 Dihedral: +4° nominal Sweep of Leading Edge: +1° nominal 1.5.3 HORIZONTAL STABILIZER Angle of Incidence : -4° ± 0.25° Span: 8 ft 9 in (2.66 m) 1.5.4 LANDING GEAR Track: 6 ft 1 in (1.86 m) Wheel Base: 5 ft 6 in (1.67 m) Tire Size: Nose: 5.00-4, 6 ply Main: 5.00-5, 6 ply Tire Pressure: Nose: 26 psi (1.8 bar) Main: 33 psi (2.3 bar) Page 1 - 7 General DA20-C1 Flight Manual DOC # DA202-C1 Revision 26 May 15, 2012 1.6 ENGINE Continental IO 240, naturally aspirated, 4 cylinder, 4 stroke-engine, fuel injected, horizontally opposed, air cooled. Propeller drive direct from engine crankshaft. Displacement: 239.8 cu.in. (3.9 liters) Output Power: 125 hp (93.2 kW) At 2800 RPM 1.7 PROPELLER Two-bladed fixed pitch propeller, manufactured by Sensenich: Model W69EK7-63, W69EK7-63G or W69EK-63 Diameter: 5 ft 9 in (1.752 m) 1.8 FUEL Approved Fuel Grades: AVGAS 100 or 100LL Total Fuel Capacity: 24.5 US gal. (93 liters) Usable Fuel: 24.0 US gal. (91 liters) Unusable Fuel: 0.5 US gal. (2 liters) General DA20-C1 Flight Manual Page 1 - 8 DOC # DA202-C1 May 15, 2012 Revision 26 1.9 LUBRICANT AND COOLANT 1.9.1 Lubricant Use only the lubricating oils conforming to TCM specifications listed in Service Information Letter SIL99-2B. See Table 1 below for approved brands. Table 1 Qualified Lubricating Oil – Ashless Dispersant (SAE J 1899) SUPPLIER BRAND (if applicable) TYPE (if applicable) BP Oil Corporation BP Aero Oil -- Castrol Castrol Aero AD Oil -- Castrol Limited ( Australia ) Castrol Aero AD Oil -- Chevron U.S.A. Chevron Aero Oil -- Continental Oil Conco Aero S -- Delta Petroleum Company Delta Avoil Oil -- Exxon Company, U.S.A. Exxon Elite -- Exxon Company, U.S.A. Exxon Aviation Oil EE -- Gulf Oil Company Gulfpride Aviation AD -- Mobil Oil Company Mobil Aero Oil -- NYCO SA Turbonycoil 3570 -- Pennzoil Company Pennzoil Aircraft Engine Oil -- Phillips Petroleum Company Phillips 66 Aviation Oil Type A 100AD, 120 AD Phillips Petroleum Company X/C Aviation Multiviscosity Oil SAE 20W-50, SAE 20W-60 Quaker State Oil & Refining Co. Quaker State AD Aviation OIL -- Red Ram Limited (Canada) Red Ram X/C Aviation Oil 20W-50 Shell Australia Aeroshell (R) W -- Shell Canada Limited Aeroshell Oil W, 15W-50 Anti-Wear Formulation Shell U.S.A. Aeroshell Oil W, 15W-50 Anti-Wear Formulation Shell U.S.A. Aeroshell Oil W100 Plus, W80 Plus -- Sinclair Oil Company Sinclair Avoil -- Texaco Inc. Texaco Aircraft Engine Oil- Premium AD -- Total France Total Aero DM 15W-50 Union Oil Company of California Union Aircraft Engine Oil HD -- Page 1 - 9 General DA20-C1 Flight Manual DOC # DA202-C1 Revision 26 May 15, 2012 The viscosity should be selected according to the various climatic conditions using Table 2. When selecting oil, the supplier’s documentation must be consulted to make sure that the oil is appropriate for the climactic conditions. Table 2 Use only the oils specified in TCM SIL99-2B. Oil Capacity: Maximum : 6.0 US qt (5.68 liters) Minimum : 4.0 US qt (3.78 liters) NOTE General DA20-C1 Flight Manual Page 1 - 10 DOC # DA202-C1 May 15, 2012 Revision 26 1.10 WEIGHT Maximum Ramp Weight : 1770 lbs (803 kg) Maximum Take-off Weight : 1764 lbs (800 kg) Maximum Landing Weight : 1764 lbs (800 kg) Empty Weight : See Chapter 6 Maximum Weight in Baggage Compartment : 44 lbs (20 kg) only if restraining devices available Wing Loading At Maximum Take-off Weight : 14.11 lbs/sq.ft. (68.96 kg/m2) Performance Load at Maximum Take-off Weight : 14.11 lbs/hp (8.58 kg/kW) Page 1 - 11 General DA20-C1 Flight Manual DOC # DA202-C1 Revision 26 May 15, 2012 1.11 LIST OF DEFINITIONS AND ABBREVIATIONS 1.11.1 Airspeeds CAS: Calibrated Airspeed. Indicated airspeed, corrected for installation and instrument errors. CAS equals TAS at standard atmospheric conditions (ISA) at MSL. GS: Ground Speed. Speed of the airplane relative to the ground. IAS: Indicated Airspeed as shown on an airspeed indicator. KCAS: CAS indicated in knots. KIAS: IAS indicated in knots. TAS: True Airspeed. The speed of the airplane relative to the air. TAS is CAS corrected for errors due to altitude and temperature. VA : Maneuvering Speed. Maximum speed at which the airplane is not overstressed at full deflection of control surfaces. Full or abrupt control surface movement is not permissible above this speed. VFE : Maximum Flaps Extended Speed. This speed must not be exceeded with the given flap setting. VNE : Never Exceed Speed in smooth air. This speed must not be exceeded in any operation. VNO: Maximum Structural Cruising Speed. This speed may be exceeded only in smooth air, and then only with caution. VR : Rotation Speed or Takeoff Speed VREF: Reference Speed VS : The power-off stall speed with the airplane in its standard configuration. VSO : The power-off stall speed with the airplane in landing configuration. VX : Best Angle-of-Climb Speed. VY : Best Rate-of-Climb Speed. General DA20-C1 Flight Manual Page 1 - 12 DOC # DA202-C1 May 15, 2012 Revision 26 1.11.2 Meteorological Terms 1.11.3 Powerplant AGL: Above Ground Level Indicated Pressure Altitude: Altitude reading with altimeter set to 1013.25 hPa (29.92 inHg). ISA: International Standard Atmosphere at which air is identified as a dry gas. The temperature at mean sea level is 15° C (59° F), the air pressure at sea level is 1013.25 mbar (29.92 inHg), the temperature gradient up to the altitude at which the temperature reaches -56.5° C (-67.9° F) is -0.0065° C/m (-0.0036° F/ft) and 0° C/m (0° F/ft) above. OAT: Outside Air Temperature. Pressure Altitude: Altitude measured at standard pressure at MSL (1013.25 mbar / 29.92 inHg) using a barometric altimeter. Pressure altitude is the indicated altitude corrected for installation and instrument errors. Within this manual the instrument errors are assumed to be zero. Aerodrome/Airport Pressure: Actual atmospheric pressure at the aerodrome/ airport altitude. Wind: The wind speeds used in the diagrams in this manual should be referred to as headwind or tailwind components of the measured wind. Take-off Power: Maximum engine power for take-off. Maximum Continuous Power: Maximum permissible continuous engine output power during flight. Page 1 - 13 General DA20-C1 Flight Manual DOC # DA202-C1 Revision 26 May 15, 2012 1.11.4 Flight Performance and Flight Planning 1.11.5 Weight and Balance Demonstrated Crosswind Component: The maximum speed of the crosswind component at which the manoeuvrability of the airplane during take-off and landing has been demonstrated during type certification test flights. Service Ceiling: The altitude at which the maximum rate of climb is 0.5 m/s (100 ft/min.) Reference Datum (RD): An imaginary vertical plane from which all horizontal distances for the center of gravity calculations are measured. It is the plane through the leading edge of the wing root rib, perpendicular to the longitudinal axis of the airplane. Station: A defined point along the longitudinal axis which is generally presented as a specific distance from the reference datum. Lever Arm: The horizontal distance from the reference datum to the center of gravity (of a component). Moment: The weight of a component multiplied by its lever arm. Center of Gravity (CG): Point of equilibrium for the airplane weight. CG position: Distance from the reference datum to the CG. It is determined by dividing the total moment (sum of the individual moments) by the total weight. Center of Gravity Limits: The CG range within which an airplane with a given weight must be operated. Usable Fuel: The amount of fuel available for the flight plan calculation. Unusable Fuel: The amount of fuel remaining in the tank, which cannot be safely used in flight. General DA20-C1 Flight Manual Page 1 - 14 DOC # DA202-C1 May 15, 2012 Revision 26 1.11.6 Equipment 1.11.7 Miscellaneous 1.12 CONVERSION FACTORS 1.12.1 Length or Altitude 1 [ft.] = 0.3048 [m] 1 [in.] = 25.4 [mm] 1.12.2 Speed 1 [kts] = 1.852 [km/h] 1 [mph] = 1.609 [km/h] 1.12.3 Pressure 1 [hPa] = 100 [N/m2] = 1 [mbar] 1 [in. Hg] = 33.865 [hPa] 1 [psi] = 68.97 [mbar] 1.12.4 Weight 1 [lbs] = 0.454 [kg] Empty Weight: Weight of the airplane including unusable fuel, all operating fluids and maximum amount of oil. Useful Load: The difference between take-off weight and empty weight. Maximum Take-off Weight: Maximum weight permissible for take-off. ACL: Anti collision light GFRP: Glass Fibre Reinforced Plastic CFRP: Carbon Fibre Reinforced Plastic Page 1 - 15 General DA20-C1 Flight Manual DOC # DA202-C1 Revision 26 May 15, 2012 1.12.5 Volume 1 [US gallon] = 3.785 [liters] 1 [Imperial gallon] = 4.546 [liters] CONVERSION CHART - LITERS/US GALLONS Liter US Gallon US Gallon Liter 5 1.3 1 3.8 10 2.6 2 7.6 15 4.0 4 15.1 20 5.3 6 22.7 25 6.6 8 30.3 30 7.9 10 37.9 35 9.2 12 45.4 40 10.6 14 53.0 45 11.9 16 60.6 50 13.2 18 68.1 60 15.9 20 75.7 70 18.5 22 83.3 80 21.1 24 90.9 90 23.8 26 98.4 100 26.4 28 106.0 General DA20-C1 Flight Manual Page 1 - 16 DOC # DA202-C1 Intentionally left blank Revision 26 May 15, 2012 Page 2 - 1 Operating Limitations DA20-C1 Flight Manual DOC # DA202-C1 Revision 27 February 12, 2013 DOT Approved CHAPTER 2 OPERATING LIMITATIONS TABLE OF CONTENTS PAGE 2.1 INTRODUCTION ................................................................................... 3 2.2 AIRSPEED LIMITATIONS...................................................................... 4 2.3 AIRSPEED INDICATOR MARKINGS .................................................... 4 2.4 POWER PLANT LIMITATIONS.............................................................. 5 2.4.1 Engine ....................................................................................... 5 2.4.2 Additional for aircraft equipped with altitude compensating fuel system......................................................... 6 2.4.3 Propeller.................................................................................... 6 2.5 POWER PLANT INSTRUMENT MARKINGS ........................................ 7 2.6 MISCELLANEOUS INSTRUMENT MARKINGS.................................... 8 2.7 WEIGHT................................................................................................. 8 2.8 CENTER OF GRAVITY.......................................................................... 9 2.9 APPROVED MANEUVERS ................................................................. 10 2.10 MANEUVERING LOAD FACTORS.......................................................11 2.11 MAXIMUM PASSENGER SEATING .....................................................11 2.12 FLIGHT CREW .....................................................................................11 2.13 KINDS OF OPERATION ...................................................................... 12 2.14 FUEL.................................................................................................... 13 2.15 PLACARDS.......................................................................................... 14 Operating Limitations DA20-C1 Flight Manual Page 2 - 2 DOC # DA202-C1 February 12, 2013 Revision 27 DOT Approved PAGE 2.16 DEMONSTRATED CROSSWIND COMPONENT ................................32 2.17 TEMPERATURE LIMITS ......................................................................32 Page 2 - 3 Operating Limitations DA20-C1 Flight Manual DOC # DA202-C1 Revision 26 May 15, 2012 DOT Approved 2.1 INTRODUCTION Chapter 2 of this Flight Manual comprises of the operating limitations, instrument markings, airspeed indicator markings, and the limitation placards which are necessary for the safe operation of the airplane, its engine, and standard systems and equipment. The operating limitations in this Chapter and Chapter 9 have been approved by the Department of Transport (DOT), and must be complied with for all operations. . ALL LIMITATIONS GIVEN IN THIS CHAPTER MUST BE COMPLIED WITH FOR ALL OPERATIONS. WARNING Operating Limitations DA20-C1 Flight Manual Page 2 - 4 DOC # DA202-C1 May 15, 2012 Revision 26 DOT Approved 2.2 AIRSPEED LIMITATIONS 2.3 AIRSPEED INDICATOR MARKINGS Speed KIAS Remarks VA Maneuvering Speed 106 Do not make full or abrupt control movement above this speed. Under certain conditions the airplane may be overstressed by full control movement. VFE Maximum Flap Extended Speed VFE (Takeoff) 100 Do not exceed this speed with flaps in take-off position. VFE (Landing) 78 Do not exceed this speed with flaps in landing position. VNO Maximum Structural Cruising Speed 118 Do not exceed this speed except in smooth air, and then only with caution. VNE Never Exceed Speed 164 Do not exceed this speed in any operation Marking KIAS Explanation White Arc 34 - 78 Operating range with flaps fully extended. Green Arc 42 - 118 Normal operating range. Yellow Arc 118 - 164 Maneuvers must be conducted with caution and only in smooth air. Red Line 164 Maximum permissable speed for all operating modes. Page 2 - 5 Operating Limitations DA20-C1 Flight Manual DOC # DA202-C1 Revision 27 February 12, 2013 DOT Approved 2.4 POWER-PLANT LIMITATIONS 2.4.1 Engine (a) Engine Manufacturer : Continental Motors (b) Engine Type Designation : IO-240-B (c) Engine Operating Limitations Max. T/O Power (5 min.) : 125 BHP / 93.2 kW Max. Permissible T/O RPM : 2800 RPM Max. Continuous Power : 125 BHP / 93.2 kW Max. Permissible Continuous RPM : 2800 RPM (d) Oil pressure Minimum : 10 psi (1.5 bar) Maximum : 100 psi (6.9 bar) Ambient temperature below 32°F (0°C), Full power operation oil pressure 70 psi max Normal Operating : 30 psi (2.1 bar) to 60 psi (4.1 bar) (e) Oil temperature Minimum : 75°F (24°C) Full power operation, oil temperature normal 100°F (38°C) Maximum : : 240°F (115°C) (f) Cylinder head temperature Maximum : 460°F (238°C) Minimum : 240°F (115°C) takeoff Operating Limitations DA20-C1 Flight Manual Page 2 - 6 DOC # DA202-C1 May 15, 2012 Revision 26 DOT Approved (g) Fuel Specifications Approved Fuel Grades : AVGAS 100LL or 100 (h) Oil Grades : Reference TCM IO-240-B operator and installation manual (form X30620) or TCM specification MHS-24. Refer to Chapter 1, Section 1.9.1. Lubricant, Table 1. 2.4.2 Additional for aircraft equipped with altitude compensating fuel system. (a) Mandatory Preflight Idle Mixture Rise : 50 RPM Minimum: See Normal Procedures-Before Takeoff (Section 4.4.6.) Less than 50 RPM Mixture Rise indicates an excessively lean idle mixture that can result in engine stoppage at idle. (b) Minimum Ground Idle Speed : 975 RPM Minimum Recommended minimum flight idle speed 1400 RPM, during idle power flight conditions and maneuvers. 2.4.3 Propeller (SENSENICH) (a) Propeller Manufacturer : Sensenich Propeller, Plant City/Florida (b) Propeller Type : Fixed Pitch W69EK7-63, W69EK7-63G or W69EK-63 (c) Propeller Diameter : 69.0 inches (1752mm) (d) Propeller Pitch (at 3/4 radius) : 62.8 inches (1595mm) NOTE NOTE Page 2 - 7 Operating Limitations DA20-C1 Flight Manual DOC # DA202-C1 Revision 27 February 12, 2013 DOT Approved 2.5 POWERPLANT INSTRUMENT MARKINGS Powerplant instrument markings and their color code significance are shown below: The allowable operating fuel pressure is greater than 32.5 psi. Operation to the top of the Red Line is permitted. This change is temporary pending installation of modified fuel pressure gauge. Powerplant instrument markings for instruments delivered after July 1999. Instrument Red Line/ Lower Limit Green Arc/ Normal Operating Range Yellow Arc/ Caution Range Red Line/ Upper Limit Tachometer - 700 - 2800 RPM - 2801 RPM Oil Temperature Indicator 75° F 170 - 220° F 75 - 170° F 220 - 240° F 240° F Cylinder Head Temperature Indicator - 360 - 420° F 240 - 360° F 420 - 460° F 460° F Oil Pressure Indicator 10 psi 30 - 60 psi RPM > 2100 10 - 30 psi 60 - 100 psi 100 psi Fuel Pressure Indicator 3.5 psi - - 16.5 psi 3.5 psi - - Top of Red Line (See NOTE) NOTE Instrument Red Line/ Lower Limit Green Arc/ Normal Operating Range Yellow Arc/ Caution Range Red Line/ Upper Limit Oil Temperature Indicator 75° F 170 - 220° F - 240° F Cylinder Head Temperature Indicator - 300 - 420° F 420 - 460° F 460° F Oil Pressure Indicator 10 psi 30 - 60 psi RPM > 2100 - 100 psi Operating Limitations DA20-C1 Flight Manual Page 2 - 8 DOC # DA202-C1 February 12, 2013 Revision 27 DOT Approved 2.6 MISCELLANEOUS INSTRUMENT MARKINGS 2.7 WEIGHT Maximum Ramp Weight : 1770 lbs (803 kg) Maximum permissible weight : 1764 lbs (800 kg) Maximum permissible weight in the : 44 lbs (20 kg) only permissable baggage compartment with baggage harness (including baggage extension) EXCEEDING WEIGHT LIMITATIONS MAY LEAD TO OVERLOADING OF THE AIRPLANE AND CAUSE LOSS OF CONTROL OF THE AIRPLANE AND/OR STRUCTURAL DAMAGE. Instrument Red Arc/ = Lower Limit Yellow Arc/ = Caution Range Green Arc/ = Normal Operating Range Red Line/ = Upper Limit Voltmeter 8 - 11 Volts 11 - 12.5 Volts 12.5 - 16.1 Volts 16.1 Volts WARNING Page 2 - 9 Operating Limitations DA20-C1 Flight Manual DOC # DA202-C1 Revision 26 May 15, 2012 DOT Approved 2.8 CENTER OF GRAVITY EXCEEDING THE CENTER OF GRAVITY LIMITATIONS REDUCES THE MANEUVERABILITY AND STABILITY OF THE AIRPLANE. The procedure used to determine the center of gravity is described in Chapter 6. Points Gross Weight Arm (aft of datum) (lbs) (kgs) (in) (m) A 1653 750 7.95 .202 B 1764 800 8.07 .205 C 1764 800 12.16 .309 D 1653 750 12.48 .317 WARNING Operating Limitations DA20-C1 Flight Manual Page 2 - 10 DOC # DA202-C1 February 12, 2013 Revision 27 DOT Approved 2.9 APPROVED MANEUVERS This airplane is certified in the UTILITY Category in accordance with Canadian Airworthiness Manual Chapter 523-VLA. Permissible Utility Category Maneuvers: (a) All normal flight maneuvers (b) The following maneuvers in which the angle of bank is not more than 60°: Lazy Eights Entry speed : 116 KIAS Chandelles Entry speed : 116 KIAS Steep turns (c) Spinning NOT approved for aircraft equipped with altitude compensating fuel system. (d) Spinning (with Wing Flaps UP) approved for aircraft NOT equipped with altitude compensating fuel system. Note removed. (e) Stalls NOT approved for aircraft equipped with altitude compensating fuel system and not in compliance with MSB DAC1-73-05 latest approved revision. (f) Stalls (except whip stalls) approved for aircraft NOT equipped with altitude compensating fuel system. (g) Stalls (except whip stalls) approved for aircraft equipped with altitude compensating fuel system in compliance with MSB DAC1-73-05 latest approved revision. (h) Intentional Side Slips, except as required for landings, NOT approved for aircraft equipped with altitude compensating fuel system and not in compliance with MSB DAC1-73-05 latest approved revision. Aerobatics are prohibited. NOTE Page 2 - 11 Operating Limitations DA20-C1 Flight Manual DOC # DA202-C1 Revision 26 May 15, 2012 DOT Approved 2.10 MANEUVERING LOAD FACTORS Table of structural maximum permissible load factors: EXCEEDING THE MAXIMUM LOAD FACTORS WILL RESULT IN OVERSTRESSING OF THE AIRPLANE. SIMULTANEOUS FULL DEFLECTION OF MORE THAN ONE CONTROL SURFACE CAN RESULT IN OVERSTRESSING OF THE STRUCTURE, EVEN AT SPEEDS BELOW THE MANEUVERING SPEED. 2.11 MAXIMUM PASSENGER SEATING Maximum Passenger Seating : one passenger. 2.12 FLIGHT CREW Minimum Flight Crew : one pilot. at VA V NE with flaps in T/O or LDG position Positive + 4.4 + 4.4 + 2.0 Negative - 2.2 - 2.2 0 WARNING Operating Limitations DA20-C1 Flight Manual Page 2 - 12 DOC # DA202-C1 February 12, 2013 Revision 27 DOT Approved 2.13 KINDS OF OPERATION Flights are permissible in accordance with visual flight rules. Minimum Equipment, Flight and Navigation Instruments: Airspeed Indicator Altimeter Attitude Gyro (Artificial Horizon) (not mandatory for Day-VFR only) Outside Air Temperature Indicator (mandatory for Night-VFR only) Vertical Speed Indicator (mandatory for Night-VFR only) Magnetic Compass Turn and Bank Indicator (not mandatory for Day-VFR only) Directional Gyro (not mandatory for Day-VFR only) Minimum Equipment, Powerplant Instruments: Fuel Quantity Indicator Fuel Pressure Indicator Oil Pressure Indicator Oil Temperature Indicator Cylinder Head Temperature Indicator Tachometer Voltmeter Ammeter Generator Warning Light Minimum Equipment, Lighting: Instrument Lighting (not mandatory for Day-VFR only) Instrument Panel and Map Lighting (mandatory for Night-VFR only) Landing Light (mandatory for Night-VFR only) Position and Anti-Collision Lights (mandatory for Night-VFR only) Illuminated Placards (mandatory for Night-VFR operations in EASA member countries) Additional equipment may be required for compliance with specific operational or specific national requirements. It is the operators responsibility to ensure compliance with any such specific equipment requirements. NOTE Page 2 - 13 Operating Limitations DA20-C1 Flight Manual DOC # DA202-C1 Revision 27 February 12, 2013 DOT Approved 2.14 FUEL Fuel Capacity Total Fuel Quantity: : 24.5 US gal. (93.0 liters) Usable Fuel: : 24.0 US gal. (91.0 liters) Unusable Fuel: : 0.5 US gal. (2.0 liters) Operating Limitations DA20-C1 Flight Manual Page 2 - 14 DOC # DA202-C1 February 12, 2013 Revision 27 DOT Approved 2.15 PLACARDS The following placards must be installed on the airplane: (a) On the exterior of the airplane - Upper surfaces placards and markings. DO NOT CLOSE CANOPY IN LOCKED POSITION LOCK UNLOCK TO LIFT CANOPY UNLATCH BOTH SIDES AND LIFT UP CANOPY UNLATCH LATCH OPEN OPEN BOTH SIDES TO OPEN CANOPY 1. OPEN WINDOW, UNLOCK HANDLE 2. UNLOCK OPPOSITE SIDE AND LIFT UP CANOPY TO OPEN CANOPY: STEP BELOW LOCK UNLOCK DO NOT PUSH ON SPINNER 93L/24.5 US gal. AVGAS 100LL 95L/25 US gal. AVGAS 100LL 77L/20.3 US gal. AVGAS 100LL USABLE 91L/24.0 US gal. USABLE 80.5L/21.3 US gal. USABLE 75L/19.8 US gal. Fuel Drains Located Underneath. Ground Aircraft before Refueling. EXTERNAL 14 VOLTS POWER REFUELING GROUND NOTE: One of the Placards is installed on the airplane NOTE: One of the Placards is installed on the airplane Page 2 - 15 Operating Limitations DA20-C1 Flight Manual DOC # DA202-C1 Revision 27 February 12, 2013 DOT Approved (b) On the exterior of the airplane - Upper surfaces placards and markings. TO LIFT CANOPY UNLATCH BOTH SIDES AND LIFT UP CANOPY UNLATCH LATCH OPEN OPEN BOTH SIDES TO OPEN CANOPY 1. OPEN WINDOW, UNLOCK HANDLE 2. UNLOCK OPPOSITE SIDE AND LIFT UP CANOPY TO OPEN CANOPY: STEP BELOW LOCK UNLOCK INLET AND OUTLET BAFFLES MUST BE REMOVED ABOVE 12.5 0 0 C/54.5 F 12.5 0 0 C/54.5 F FOR TEMPERATURES BETWEEN 0 0 0 C/32 F AND INSTALL EITHER INLET BAFFLES ONLY OR OUTLET BAFFLES ONLY CAUTION USE ONLY AVIATION GRADE OIL! FLIGHT MANUAL OIL SAE 20W-50 6.0 US Qts. 5.68 I OR ACCORDING TO EMERGENCY LOCATOR TRANSMITTER INSTALLED HERE ELT EMPLACEMENT HERE DE LA RADIOBALISE DE DETRESSE ICIL’ (BAFFLE SHOULD BE INSTALLED BELOW -5°C /+23°F) WINTER KIT MUST BE REMOVED ABOVE 12.5°C /+54.5°F) Operating Limitations DA20-C1 Flight Manual Page 2 - 16 DOC # DA202-C1 February 12, 2013 Revision 27 DOT Approved (c) On the exterior of the airplane - Lower surfaces placards and markings. NOTE: The Placards and Markings shown are on the lower surfaces of the airplane. Page 2 - 17 Operating Limitations DA20-C1 Flight Manual DOC # DA202-C1 Revision 27 February 12, 2013 DOT Approved (d) On the exterior of the airplane - Lower surfaces placards and markings. NOTE: The Placards and Markings shown are on the lower surfaces of the airplane. Operating Limitations DA20-C1 Flight Manual Page 2 - 18 DOC # DA202-C1 February 12, 2013 Revision 27 DOT Approved (e) On the instrument panel - Up to airplane serial number C0149. Maneuvering speed V = 106kts A No smoking! NOSE UP NEUTRAL NOSE DOWN TRIM Usable Usable 91 L/24 US gal. 80.5 L/21.3 US gal. This aeroplane i s class ified as a v ery light aeroplane approved for day and night VFR only, in non-icing conditions. All aerobatic manoeuvres except for intentinal spinning which is permitted with flaps UP only, are prohibited. See Flight Manual for other limitations. This airplane is class ifi ed as a v ery light airplane ap pr ov ed for V i s u a l M e t e o r o l o gical Conditions only, in non-icing conditions. All aerobatic maneuvers, except for intentional spinning which is permitted with flaps UP only, are prohibited. See Flight Manual for other limitations. L ELEC. D.C. TURN COORDINATOR INFORMATIO N NO PITCH 2 MIN. R INSTRUMENT EPU TAXI STROBE PITOT LANDING POSITION MAP LIG HTS BRIGHT DIM OFF ON Maneuvering speed V = 104kts GPS limited for VFR only. No smoking! 12 S 51 NOSE UP NEUTRAL NOSE DOWN TRIM INDENT BENDIX/KING TST ALT OFF SBY ON 0 1 KT 76A TSO 2 3 VDO AMPS 60 - 0 HOURS 1/10 VDO 0 0 0 0 0 OUTSIDE AIR TEMP . FAHRENHEIT A309F + 60 8 VDO 1412 16 10 VOLT GEN. GEN. CONTROL BATTERY ELECTRICAL ADF DME AVIONICS MARKER HSI 240 Cylinder Head 100 460 600 °F 360 420 VDO Temp. VDO FUEL/FLOW US.GAL/HR LITERS/HR 35 4 5 0 0 2 8 25 15 6 45 12 40 10 75 240 OIL VDO 220 °F 170 Usable 74L/19.5 US gal. VDO 0 1 1 2 1 43 41 FUEL 80 10 VDO OIL lbs./sq.inch 03 06 8 10 6 4 2 16 VDO EGT x100°F 14 2 2 2 5 1 2 10 10 2 1 50 3 3 3 5 5 25 50 ENGINE OIL PRESS OIL TEMP FUEL PRESS START SLIP FUEL QTY. SYSTEM O.A.T. TRIM FLAPS & FUEL PUMP PITOT HEAT TURN MIC Flaps ON OFF PUMP MASTER AVIONIC FUEL GEN/BAT Push-On Volu me ALL ISO PM 501 Squelch 100 80 KNOTS 60 AIRSPEED 160 40 140 120 12:45 CONTROL DAVTR ON SELECT GMT LT ET CHRONOMETER M800 4 5 6 C US O IT N 20 2 0 15 UP 5 1 0 VERTICAL SPEED 100 FEET PER MINUTE 15 10 DOWN 5 0 05 3 10 15 1 10 30 0 0 0 HOURS 35 0 1 HUNDREDS 25 20 RPM OBS N E W S B S PULL TEST TSO OFF KX 125 BENDIX/KING COMM PULL 25K



OBS PULL PULL IDENT NAV S B Y OBS S FLAG TO FR S B B Y N 3 3 3 0 W 2 4 2 1 S 1 5 1 2 E 6 3 PUSH This airplane is classified as a very light airplane approved for VFR only, in non-icing conditions. All aerobatic maneuvers, except for intentional spinning which is S T A R T G E N C A N O P Y E P U EG T LANDING TAXI/MAP LIG HTS STROBE POSITIO N INST. PULSE LIGHT 3 3 3 5 5 AVIONICS CONTROL MASTER ICS MASTER ATC NAV/CO M 1 GPS Note: The content of this label changes for different countries. For aircraft operated in EASA member countries only. Page 2 - 19 Operating Limitations DA20-C1 Flight Manual DOC # DA202-C1 Revision 27 February 12, 2013 DOT Approved (f) On the instrument panel - Up to airplane serial number C0149. INS EPU TAXI STROBE LANDING POSITION MAP LIGHTS BRIGHT DIM OFF ON GPS limited for VFR only. ON OFF PUMP MASTER AVIONIC FUEL GEN/BAT Flaps MIC CRUISE T/O LDG CRUISE T/O LDG PITOT HEAT L ELEC. D.C. TURN COORDINATOR INFORMATIO N NO PITCH 2 MIN. R INSTRUMENT EPU TAXI STROBE PITOT LANDING POSITION MAP LIG HTS BRIGHT DIM OFF ON Maneuvering speed V = 104kts GPS limited for VFR only. No smoking! 12 S 51 NOSE UP NEUTRAL NOSE DOWN TRIM INDENT BENDIX/KING TST ALT OFF SBY ON 0 1 KT 76A TSO 2 3 VDO AMPS 60 - 0 HOURS 1/10 VDO 0 0 0 0 0 OUTSIDE AIR TEMP . FAHRENHEIT A309F + 60 8 VDO 1412 16 10 VOLT GEN. GEN. CONTROL BATTERY ELECTRICAL ADF DME AVIONICS MARKER HSI 240 Cylinder Head 100 460 600 °F 360 420 VDO Temp. VDO FUEL/FLOW US.GAL/HR LITERS/HR 35 4 5 0 0 2 8 25 15 6 45 12 40 10 75 240 OIL VDO 220 °F 170 Usable 74L/19.5 US gal. VDO 0 1 1 2 1 43 41 FUEL 80 10 VDO OIL lbs./sq.inch 03 06 8 10 6 4 2 16 VDO EGT x100°F 14 2 2 2 5 1 2 10 10 2 1 50 3 3 3 5 5 25 50 ENGINE OIL PRESS OIL TEMP FUEL PRESS START SLIP FUEL QTY. SYSTEM O.A.T. TRIM FLAPS & FUEL PUMP PITOT HEAT TURN MIC Flaps ON OFF PUMP MASTER AVIONIC FUEL GEN/BAT Push-On Volu me ALL ISO PM 501 Squelch 100 80 KNOTS 60 AIRSPEED 160 40 140 120 12:45 CONTROL DAVTR ON SELECT GMT LT ET CHRONOMETER M800 4 5 6 C US O IT N 20 2 0 15 UP 5 1 0 VERTICAL SPEED 100 FEET PER MINUTE 15 10 DOWN 5 0 05 3 10 15 1 10 30 0 0 0 HOURS 35 0 1 HUNDREDS 25 20 RPM OBS N E W S B S PULL TEST TSO OFF KX 125 BENDIX/KING COMM PULL 25K



OBS PULL PULL IDENT NAV S B Y OBS S FLAG TO FR S B B Y N 3 3 3 0 W 2 4 2 1 S 1 5 1 2 E 6 3 PUSH This airplane is classified as a very light airplane approved for VFR only, in non-icing conditions. All aerobatic maneuvers, except for intentional spinning which is S T A R T G E N C A N O P Y E P U EG T LANDING TAXI/MAP LIG HTS STROBE POSITIO N INST. PULSE LIGHT 3 3 3 5 5 AVIONICS CONTROL MASTER ICS MASTER ATC NAV/CO M 1 GPS Note: The content of this Placard changes for different installed equipment. Optional VM 1000 MicroVision Installation EGT/CHT EGT/CHT GRAPH DIGITAL AUTOTRACK ON/OFF FUEL/COMP MODE FLIGHT DATA Operating Limitations DA20-C1 Flight Manual Page 2 - 20 DOC # DA202-C1 February 12, 2013 Revision 27 DOT Approved (g) On the instrument panel - Airplane serial number C0150 and subs. Note: The content of this label changes for different countries. CAUTION! GROUND OPERATION. DO NOT ENGAGE STARTER WHEN PROPELLER IS MOVING. SERIOUS ENGINE DAMAGE MAY RESULT. No smoking! GPS limited for VFR only. PRIME OFF OFF FOR NORMAL FLIGHT Maneuvering speed V = 106kts A NOSE UP NEUTRAL NOSE DOWN TRIM Usable 91 L/24 US gal. This airplane is classified as a very light airplane approved for Visual Meteorological Conditions only, in non-icing conditions. All aerobatic maneuvers, except for intentional spinning which is permitted with flaps UP only, are prohibited. See Flight Manual for other limitations. This aeroplane is class ified as a v ery light aeroplane approved for day and night VFR only, in non-icing conditions. All aerobatic manoeuvres except for intentinal spinning which is permitted with flaps UP only, are prohibited. See Flight Manual for other limitations. For aircraft operated in EASA member countries only. Page 2 - 21 Operating Limitations DA20-C1 Flight Manual DOC # DA202-C1 Revision 27 February 12, 2013 DOT Approved (h) On the instrument panel - Airplane serial number C0150 and subs. Note: The content of this Placard changes for different installed equipment. Optional VM 1000 MicroVision Installation AUTOPILOT MAX. OPERATING SPEED 148 KIAS A/P OPS PROHIBITED FOR T/O & LDG MAX FLAP T/O (15 ) WITH A/P ON PULSE EPU AUTO PILOT LANDING TAXI STROBE POSITION MAP INSTRUMENT FLOOD LIGHTS ON OFF ON OFF PUMP MASTER AVIONIC FUEL GEN/BAT CRUISE T/O LDG Flaps EGT/CHT EGT/CHT GRAPH DIGITAL AUTOTRACK ON/OFF FUEL/COMP MODE FLIGHT DATA For Idle Power Operation: 1. Fuel Pump 2. Mixture 3. Throttle ON FULL RICH IDLE VFE (T/O) 100 KTS. V FE (LDG) 78 KTS. 14VDC ACCESSORY PWR. GROUND OPS. ONLY 2A MAX NOTE: Only installed if Auto Pilot is installed. Operating Limitations DA20-C1 Flight Manual Page 2 - 22 DOC # DA202-C1 February 12, 2013 Revision 27 DOT Approved (i) On the instrument panel - Circuit Breakers. ENGINE OIL PRESS OIL TEMP FUEL PRESS START EGT TACH . L ELEC. D.C. TURN COORDINATOR INFORMATIO N NO PITCH 2 MIN. R INSTRUMENT EPU TAXI STROBE PITOT LANDING POSITIO N MAP LIG HTS BRIGHT DIM OFF ON Maneuvering speed V = 104kts GPS limited for VFR only. No smoking! 12 S 51 NOSE UP NEUTRAL NOSE DOWN TRIM INDENT BENDIX/KING TST ALT OFF SBY ON 0 1 KT 76A TSO 2 3 VDO AMPS 60 - 0 HOURS 1/10 VDO 0 0 0 0 0 OUTSIDE AIR TEMP. FAHRENHEIT A309F + 60 8 VDO 1412 16 10 VOLT GEN. GEN. CONTROL BATTERY ELECTRICAL ADF DME AVIONICS MARKER HSI 240 Cylinder Head 100 460 600 °F 360 420 VDO Temp. VDO FUEL/FLOW US.GAL/HR LITERS/HR 35 4 5 0 0 2 8 2515 6 45 12 40 10 75 240 OIL VDO 220 °F 170 Usable 74L/19.5 US gal. VDO 0 1 1 2 1 4 3 41 F UEL 80 10 VDO OIL lbs./sq.inch 03 06 8 10 6 4 2 16 VDO EGT x100°F 14 2 2 2 5 1 2 10 10 2 1 50 3 3 3 5 5 25 50 SLIP FUEL QTY. SYSTEM O.A.T. TRIM FLAPS & FUEL PUMP PITOT HEAT TURN MIC Flaps ON OFF PUMP MASTER AVIONIC FUEL GEN/BAT Push-On Volu me ALL ISO PM 501 Squelch 100 80 KNOTS 60 AIRSPEED 160 40 140 120 12:45 CONTROL DAVTRON SELECT GMT LT ET CHRONOMETER M800 4 5 6 CUS OIT N 20 2 0 15 UP 5 1 0 VERTICAL SPEED 100 FEET PER MINUTE 15 10 DOWN 5 0 05 3 10 15 1 10 30 0 0 0 HOURS 35 0 1 HUNDREDS 25 20 RPM OBS N E W S B S PULL TEST TSO OFF KX 125 BENDIX/KING COMM PULL 25K



OBS PULL PULL IDENT NAV S B Y OBS S FLAG TO FR S B B Y N 3 3 3 0 W 2 4 2 1 S 1 5 1 2 E 6 3 PUSH This airplane is classified as a very light airplane approved for VFR only, in non-icing conditions. All aerobatic maneuvers, except for intentional spinning which is S T A R T G E N C A N O P Y E P U LANDING TAXI/MAP LIG HTS STROBE POSITIO N INST. PULSE LIGHT 3 3 3 5 5 AVIONICS CONTROL MASTER ICS MASTER ATC NAV/CO M 1 GPS Note: The content of the Avionics Placard changes depending on installed equipment. Note: The content of the Avionics Placard changes depending on installed equipment. ENGINE START FUEL PRESS OIL PRESS EGT OIL TEMP TACH. SYSTEM FLAPS TRIM FUEL/QTY. O.A.T. TURN & SLIP FUEL PUMP PITOT HEAT LIGHTS STROBE LANDING MAP/TAXI INST. POSITION PULSE LIGHT ELECTRICAL BATTERY GEN. GEN. CONTROL ELECTRICAL BATTERY GEN. GEN. CONTROL AUX POWER Page 2 - 23 Operating Limitations DA20-C1 Flight Manual DOC # DA202-C1 Revision 27 February 12, 2013 DOT Approved (j) Reversed instrument panel installation. Usable 76 L / 20 US gal. For Idle Power Operation: 1. Fuel Pump 2. Mixture 3. Throttle ON FULL RICH IDLE NOSE UP NEUTRAL NOSE DOWN TRIM Maneuvering speed V = 106kts A CAUTION! GROUND OPERATION. DO NOT ENGAGE STARTER WHEN PROPELLER IS MOVING. SERIOUS ENGINE DAMAGE MAY RESULT. No smoking! GPS limited for VFR only. PRIME OFF OFF FOR NORMAL FLIGHT Operating Limitations DA20-C1 Flight Manual Page 2 - 24 DOC # DA202-C1 February 12, 2013 Revision 27 DOT Approved (k) Reversed instrument panel installation. This airplane is classified as a very light airplane approved for Visual Meteorological Conditions only, in non-icing conditions. All aerobatic maneuvers, except for intentional spinning which is permitted with flaps UP only, are prohibited. See Flight Manual for other limitations. V FE (T/O) 100 KTS. V FE (LDG) 78 KTS. CRUISE T/O LDG Flaps ON OFF ON OFF FUEL PUMP MASTER AVIONIC GEN/BAT LIGHTS INSTRUMENT MAP STROBE POSITION TAXI LANDING EPU Page 2 - 25 Operating Limitations DA20-C1 Flight Manual DOC # DA202-C1 Revision 27 February 12, 2013 DOT Approved (l) Reversed instrument panel installation - Circuit Breakers. ENGINE START FUEL PRESS OIL PRESS EGT OIL TEMP TACH. SYSTEM FLAPS TRIM FUEL/QTY. O.A.T. TURN & SLIP FUEL PUMP PITOT HEAT LIGHTS STROBE LANDING TAXI/MAP INST. POSITION HORIZON DG SYSTEM ELECTRICAL BATTERY GEN. GEN. CONTROL AVIONICS AVIONICS MASTER MASTER CONTROL ICS ATC COM1 GPS/NAV 1 COM2 GPS2 CDI EQUIP COOLING Operating Limitations DA20-C1 Flight Manual Page 2 - 26 DOC # DA202-C1 February 12, 2013 Revision 27 DOT Approved (m) Instrument panel with Garmin G500 installation. Refer to Supplement 13. N O S M O K I N G This airplane is classified as as very light airplane a p p r o v e d f o r V i s u a l M e t e o r o l o g i c a l C o n d i t i o n s o n l y, i n n o n - i c i n g c o n d i t i o n s . A l l a e r o b a t i c maneuvers, except for intentional spinning which i s p e r m i t t e d w i t h f l a p s U P o n l y, a r e p r o h i b i t e d . S e e f l i g h t M a n u a l f o r o t h e r I i m i t a t i o n s . NOSE UP NEUTRAL NOSE DN T R I M MANEUVERING SPEED V = 106kts 15 OIL VDO °F 75 170 220 240 VDO FUEL 3.5 0 6 16.5 9 12 PSI 60 25 45 65 165 x10 EGT °F 145 125 85 105 8 9 0 1 2 6 7 3 4 5 GARMIN A GARMIN EC 119.80 VOL COMM PULL SQUELCH s121.50 MEMRCL MON SL40 APOLLO 165 NAV ALT R IDENT ALT GARMIN ON VFR OFF STBY 1200 GPS CDI C/V PUSH OBS MSG ft START FUNC STOP PRESSURE ALT 12300 CRSR GTX 330 CLR t FPL PROC CRSR PUSH VLOC 118.000 136.975 TERM 108.00 117.95 COS C C VOL PWR PUSH / SQ VOL ID / PUSH V COM/ VLOC V KHPN O HI COM MUTEM MRK COM1 MIC PILOT VOL SENS LO OFF/ COM1 COM3 COM2 NAV1 1/2 COM3 COM2 MIC MIC COM RNG D CLR n m K NAV DEFAULT WPT DIS KHPN 4.85 GS 000° TKE GNS 430 MENU ENT GPS COM PASS VOL VOLPULL DME CREW PILOT ICS ISOLATION ADF NAV2 PA CABIN AUDIO SPKR GMA 340 TEST COPILOT L GROUND DO NOT ENGAGE PILOT AUTO INSTRUMENT LT. R STROBE MAP EPU PULSE LANDING TAXI POSITION STARTER WHEN CAUTION! LIGHTS OFF ON OFF PUMP MASTER AVIONIC FUEL GEN/BAT BOTH FUEL PRIME NORMAL FLIGHT - OFF OFF PROP IS MOVING. START OPS. ON AMPS FLAP SPEEDS + VDO 60 - VFE (T/O) 100 KTS. VFE (LDG) 78 KTS. Flaps NEUTRAL T R I M NOSE DN NOSE UP 9 1 05 3 10 15 110 30 000HOURS 35 0 1 HUNDREDS 25 20 RPM KNOTS AIRSPEED 100 120 140 ON P Y E G N A C T R U S T A P E 160 21 S TO 6 5 20.000 FEET 4 3 28.8 ALT CALIBRATED 2 28.7 28.6 IN.Hg 60 80 mb 7 970 8 975 40 100 0 FEET Usable VOLT 81L/21.4 US gal. VDO OIL lbs./sq.inch VDO 10 30 100 60 1210 14 8 VDO 16 FUEL 1 0 1 24 1 1 34 VDO 460 Cylinder Head 200 100 Temp. 300 420 °F 600 MANEUVERING SPEED V = 106kts COM2 OIL TEMP AHRS EGT AVIONICS COOLING EQUIP LINK DATA TAS AVIONICS GPS/NAV PUMP FUEL ATC COM1 10 X X ELECTRICAL POWER PFD AUX. 1 X X X ENGINE ADC OIL PRESS START FUEL PRESS X X 7.5 2 5 2 5 5 ICS 2 X GEN. FLAPS TRIM CONTROL MASTER MASTER 3 5 20 2 BATTERY GEN. 2 50 50 SYSTEM FUEL/QTY. CONTROL NO SMOKING This airplane is classified as a very light airplane approved for Visual Meteorological Conditions only, in non-icing conditions. All aerobatic maneuvers, except for intentional spinning which is permitted with flaps UP only, are prohibited. See Flight Manual for other limitations. STROBE POSITION 10 LANDING INST. TAXI/MAP LIGHTS 5 5 5 5 14VDC ACCESSORY PWR. GROUND OPS. ONLY 2A MAX 0 VDO HOURS 1/10 0 00 03 2 Usable 91L / 24 US gal. This aeroplane is classified as a very light aeroplane approved for day and night VFR only, in non-icing conditions. All aerobatic maneuvers except for intentional spinning which is permitted with flaps UP only, are prohibited. See Flight Manual for other limitations. NO SMOKING For aircraft operated in European Aviation Safety Agency (EASA) member countries only. For aircraft operated in EASA member countries G500 with Backup Artificial Horizon 2 X X X X X X X X X X X X X X X X X X X X X X X X X X X 0 VDO HOURS 1/10 0 00 03 X F C A G E P L TO L U F O AH SYSTEM 14VDC ACCESSORY PWR. GROUND OPS. ONLY 2A MAX AVIONICS COOLING EQUIP LINK DATA TAS STROBE POSITION LANDING INST. TAXI/MAP LIGHTS COM2 OIL TEMP AHRS EGT AVIONICS GPS/NAV PUMP FUEL ATC COM1 ELECTRICAL POWER PFD AUX. 1 ENGINE ADC OIL PRESS START FUEL PRESS ICS GEN. FLAPS TRIM CONTROL MASTER MASTER BATTERY GEN. SYSTEM FUEL/QTY. CONTROL This aeroplane is classified as a very light aeroplane approved for day and night VFR only, in non-icing conditions. All aerobatic maneuvers except for intentional spinning which is permitted with flaps UP only, are prohibited. See Flight Manual for other limitations. NO SMOKING This aeroplane is classified as a very light aeroplane approved for day and night VFR only, in non-icing conditions. All aerobatic maneuvers except for intentional spinning which is permitted with flaps UP ony, are prohibited. See Flight Manual for other limitations. Page 2 - 27 Operating Limitations DA20-C1 Flight Manual DOC # DA202-C1 Revision 27 February 12, 2013 DOT Approved (n) Instrument panel with Garmin G500 installation. Refer to Supplement 13. PULSE EPU AUTO LANDING TAXI STROBE POSITION ON MAP INSTRUMENT LT. OFF OFF ON R L BOTH FUEL PRIME GEN / BAT NORMAL FLIGHT AVIONIC MASTER FUEL PUMP FLAP SPEEDS Vrs (T/O) 100 KTS. VRS (LDG) 75 KTS. OFF START CAUTION GROUND OPS DO NOT ENGAGE STARTER WHEN PROP IS MOVING OFF FOR IDLE POWER OPS. FUEL PUMP MIXTURE THROTTLE ON FULL RICH IDLE LIGHTS INST. POSITION MASTER FLAPS BATTERY TRIM GEN. PFD ADC AHRS 14VDC ACCESSORY PWR. GROUND OPS. ONLY 2A MAX GEN. CONTROL AUX. POWER START FUEL PRESS OIL PRESS EGT OIL TEMP FUEL PUMP FUEL/QTY. MASTER CONTROL STROBE LANDING TAXI/MAP AVIONICS DATA LINK TAS ICS ATC COM1 COM2 GPS/NAV 1 EQUIP COOLING SYSTEM ENGINE AVIONICS AVIONICS 15 OIL VDO °F 75 170 220 240 VDO FUEL 3.5 0 6 16.5 9 12 PSI 60 25 45 65 165 x10 EGT °F 145 125 85 105 8 9 0 1 2 6 7 3 4 5 GARMIN A GARMIN EC 119.80 VOL COMM PULL SQUELCH s121.50 MEMRCL MON SL40 APOLLO 165 NAV ALT R IDENT ALT GARMIN ON VFR OFF STBY 1200 GPS CDI C/V PUSH OBS MSG ft START FUNC STOP PRESSURE ALT 12300 CRSR GTX 330 CLR t FPL PROC CRSR PUSH VLOC 118.000 136.975 TERM 108.00 117.95 COS C C VOL PWR PUSH / SQ VOL ID / PUSH V COM/ VLOC V KHPN O HI COM MUTEM MRK COM1 MIC PILOT VOL SENS LO OFF/ COM1 COM3 COM2 NAV1 1/2 COM3 COM2 MIC MIC COM RNG D CLR n m K NAV DEFAULT WPT DIS KHPN 4.85 GS 000° TKE GNS 430 MENU ENT GPS COM PASS VOL VOLPULL DME CREW PILOT ICS ISOLATION ADF NAV2 PA CABIN AUDIO SPKR GMA 340 TEST COPILOT L GROUND DO NOT ENGAGE PILOT AUTO INSTRUMENT LT. R STROBE MAP EPU PULSE LANDING TAXI POSITION STARTER WHEN CAUTION! LIGHTS OFF ON OFF FULL RICH FOR IDLE POWER OPS. FUEL PUMP THROTTLE MIXTURE IDLE ON PUMP MASTER AVIONIC FUEL GEN/BAT BOTH FUEL PRIME NORMAL FLIGHT - OFF OFF PROP IS MOVING. START OPS. ON AMPS FLAP SPEEDS + VDO 60 - VFE (T/O) 100 KTS. VFE (LDG) 78 KTS. Flaps NEUTRAL T R I M NOSE DN NOSE UP 9 1 05 3 10 15 110 30 000 HOURS 35 0 1 HUNDREDS 25 20 RPM KNOTS AIRSPEED 100 120 140 ON P Y E G N A C T R U S T A P E 160 21 S TO 6 5 20.000 FEET 4 3 28.8 ALT CALIBRATED 2 28.7 28.6 IN.Hg 60 80 mb 7 970 8 975 40 100 0 FEET Usable VOLT 81L/21.4 US gal. VDO OIL lbs./sq.inch VDO 10 30 100 60 1210 14 8 VDO 16 FUEL 1 0 1 24 1 1 34 VDO 460 Cylinder Head 200 100 Temp. 300 420 °F 600 MANEUVERING SPEED V = 106kts COM2 OIL TEMP AHRS EGT AVIONICS COOLING EQUIP LINK DATA TAS AVIONICS GPS/NAV PUMP FUEL ATC COM1 10 X X ELECTRICAL POWER PFD AUX. 1 X X X ENGINE ADC OIL PRESS START FUEL PRESS X X 7.5 2 5 2 5 5 ICS 2 X GEN. FLAPS TRIM CONTROL MASTER MASTER 3 5 20 2 BATTERY GEN. 2 50 50 SYSTEM FUEL/QTY. CONTROL NO SMOKING NO SMOKING This airplane is classified as a very light airplane approved for Visual Meteorological Conditions only, in non-icing conditions. All aerobatic maneuvers, except for intentional spinning which is permitted with flaps UP only, are prohibited. See Flight Manual for other limitations. STROBE POSITION 10 LANDING INST. TAXI/MAP LIGHTS 5 5 5 5 14VDC ACCESSORY PWR. GROUND OPS. ONLY 2A MAX 0 VDO HOURS 1/10 0 00 03 2 Spinning is prohibited Operations in IMC are prohibited Operations by night are prohibited Operations is known or forcasting icing conditions are prohibited Operating Limitations DA20-C1 Flight Manual Page 2 - 28 DOC # DA202-C1 February 28, 2014 Revision 28 DOT Approved (o) Instrument panel with Garmin G500, UMA engine instruments and Garmin GTN 650/GTR 225installed Page 2 - 29 Operating Limitations DA20-C1 Flight Manual DOC # DA202-C1 Revision 28 February 28, 2014 DOT Approved (p) Instrument panel with Garmin G500, UMA engine instruments and Garmin GTN 650/GTR 225installed Operating Limitations DA20-C1 Flight Manual Page 2 - 30 DOC # DA202-C1 February 28, 2014 Revision 28 DOT Approved (q) Airplane interior - General placards and markings. HEADSET HEADSET HEADSET HEADSET MIC HEADSET MIC MIC HEADSET MIC PILOT CO-PILOT ON ON OFF OFF ARM MAX BAGGAGE - 44 lbs (20kg) ONLY WITH BAGGAGE NET RESCUE HAMMER TO OPEN CANOPY UNLOCK BOTH HANDLES TO LIFT CANOPY OPEN BOTH SIDES CLOSE CLOSE OPEN OPEN LOCK UNLOCK NOTE: One of the Placards is installed on the airplane NOTE: One of the Placards is installed on the airplane Page 2 - 31 Operating Limitations DA20-C1 Flight Manual DOC # DA202-C1 Revision 28 February 28, 2014 DOT Approved (r) Airplane interior - General placards and markings. TO OPEN CANOPY UNLOCK BOTH HANDLES CLOSE OPEN LOCK UNLOCK TO LIFT CANOPY OPEN BOTH SIDES CLOSE OPEN THROTTLE TENSION NOTE: One of the Placards is installed on the airplane NOTE: One of the Placards is installed on the airplane Operating Limitations DA20-C1 Flight Manual Page 2 - 32 DOC # DA202-C1 February 28, 2014 Revision 28 DOT Approved (s) Airplane interior - General placards and markings. Hydraulic Fluid Hydraulic Fluid 4 MIL-H-5606 MIL-H-5606 OFF FULL RICH OFF FULL RICH OFF FULL RICH OFF FULL RICH ALTERNATE AIR POWER FUEL MIXTURE 55 55 (Leather Seats) (Sheepskin Seats) Page 2 - 33 Operating Limitations DA20-C1 Flight Manual DOC # DA202-C1 Revision 28 February 28, 2014 DOT Approved (t) Around the ignition switch on Optional Ignition Switch the instrument panel. (Push-to-Start Feature) (u) On the instrument panel. If equipped with an altitude compensating fuel pump. (v) On the instrument panel. If equipped with an altitude compensating fuel pump. (w) On the instrument panel. If equipped with an altitude compensating fuel pump. A C S Operating Limitations DA20-C1 Flight Manual Page 2 - 34 DOC # DA202-C1 February 28, 2014 Revision 28 DOT Approved 2.16 DEMONSTRATED CROSSWIND COMPONENT The maximum demonstrated crosswind component is 20 kts. (37 km/h). 2.17 TEMPERATURE LIMITS FOR AIRCRAFT WITH OTHER THAN WHITE UNDERSIDES. PARKING THE AIRCRAFT OVER A LIGHT COLOURED OR REFLECTIVE SURFACE IN CONDITIONS OF BRIGHT SUNLIGHT, PARTICULARLY AT HIGH OAT, IS NOT RECOMMENDED. Temperature limit of the structure for the operation of the airplane: Maximum T/O Temperature : 131°F (55°C) Structural Temperature CAUTION Page 3 - 1 Emergency Procedures DA20-C1 Flight Manual DOC # DA202-C1 Revision 26 May 15, 2012 DOT Approved CHAPTER 3 EMERGENCY PROCEDURES TABLE OF CONTENTS PAGE 3.1 INTRODUCTION ..................................................................................... 3 3.2 AIRSPEEDS DURING EMERGENCY PROCEDURES............................3 3.3 EMERGENCY PROCEDURES - CHECKLISTS.......................................4 3.3.1 Engine Failures ....................................................................... 4 3.3.2 Gliding ..................................................................................... 9 3.3.3 Emergency Landing ................................................................ 9 3.3.4 Fire ........................................................................................ 12 3.3.5 Icing ...................................................................................... 15 3.3.6 Recovery from Unintentional Spin ........................................ 16 3.3.7 Landing with Defective Tire on Main Landing Gear .............. 16 3.3.8 Electrical Power Failure ........................................................ 17 3.3.9 Flap System Failure .............................................................. 19 3.3.10 Starter Relay Failure ............................................................. 19 3.3.11 Avionics System Failure ........................................................ 20 3.3.12 Trim System Failure .............................................................. 21 3.3.13 Instrument Panel Lighting Failure ......................................... 22 Emergency Procedures DA20-C1 Flight Manual Page 3 - 2 DOC # DA202-C1 Intentionally left blank Revision 26 May 15, 2012 DOT Approved Page 3 - 3 Emergency Procedures DA20-C1 Flight Manual DOC # DA202-C1 Revision 26 May 15, 2012 DOT Approved 3.1 INTRODUCTION The following chapter contains check-lists as well as descriptions of the recommended procedures in case of an emergency. However, engine failure or other airplane related emergency situations will most likely never occur if the mandatory pre-flight check and maintenance are performed properly. In the event that an emergency situation does appear, the procedures presented in this manual should be used to rectify such problems. Since it is impossible to present in the Flight Manual all emergency situations which may occur, knowledge of the airplane and experience of the pilot are essential in rectifying any problems. 3.2 AIRSPEEDS DURING EMERGENCY PROCEDURES KIAS Engine failure after take-off with flaps in T/O position 60 Maneuvering Speed 106 Airspeed for best glide angle Maximum Gross Weight – 1764 lbs (800 kg) Wing Flaps in CRUISE position 73 Precautionary Landing (with power and Wing Flaps in landing position) 55 Emergency landing with engine off (Wing Flaps in T/O position) 60 Emergency landing with engine off (Wing Flaps in LDG position) 55 Emergency landing with engine off (Wing Flaps CRUISE) 64 Emergency Procedures DA20-C1 Flight Manual Page 3 - 4 DOC # DA202-C1 May 15, 2012 Revision 26 DOT Approved 3.3 EMERGENCY PROCEDURES - CHECKLISTS 3.3.1 Engine Failures (a) Engine Failure during Take-off Run (1) Throttle........................................................ IDLE (2) Brakes .........................................................as required (3) Flaps ...........................................................CRUISE (4) Mixture ........................................................IDLE CUT-OFF (5) Ignition Switch .............................................OFF (6) GEN/BAT Master Switch .............................OFF (b) Engine Failure after Take-Off INSUFFICIENT ENGINE POWER (1) Airspeed ..................................................... 60 KIAS (2) Throttle ........................................................FULL (3) Mixture ........................................................FULL RICH (4) Alternate Air ................................................OPEN (5) Fuel Shut-off Valve ......................................OPEN (6) Ignition Switch .............................................BOTH (7) Fuel Pump ..................................................ON IF ADEQUATE ENGINE PERFORMANCE CANNOT BE RESTORED IMMEDIATELY, PREPARE FOR AN EMERGENCY LANDING. IF POSSIBLE, LAND STRAIGHT AHEAD, AVOIDING OBSTACLES. WARNING Page 3 - 5 Emergency Procedures DA20-C1 Flight Manual DOC # DA202-C1 Revision 26 May 15, 2012 DOT Approved SHORTLY BEFORE LANDING (8) Mixture ....................................................... IDLE CUTOFF (9) Fuel Shut-off Valve ..................................... CLOSED (10)Ignition Switch ............................................ OFF (11)Flaps .......................................................... as required (12)GEN/BAT Master Switch ............................ OFF ENGINE INOPERATIVE Perform emergency landing according to paragraph 3.3.3. (c) Engine Failure during Flight ENGINE RUNNING ROUGHLY (1) Mixture ....................................................... FULL RICH (2) Alternate Air ............................................... OPEN (3) Fuel Shut-off .............................................. OPEN (4) Fuel Pump .................................................. ON (5) Ignition Switch ............................................ cycle L - BOTH - R - BOTH (6) Throttle ....................................................... at present position (7) No Improvement ........................................ reduce throttle to minimum required power, land as soon as possible. Emergency Procedures DA20-C1 Flight Manual Page 3 - 6 DOC # DA202-C1 May 15, 2012 Revision 26 DOT Approved LOSS OF OIL PRESSURE (1) Oil Temperature ......................................... check (2) If Oil Pressure drops below .........................land at the nearest suitable Green Arc above 2100RPM. .......................airport. (3) If Oil Pressure drops below .........................reduce throttle to minimum Green Arc and oil temperature ....................required power and land as is rising ........................................................soon as possible. Be prepared ....................................................................for engine failure and ....................................................................an emergency landing. LOSS OF FUEL PRESSURE (1) Fuel Pump ................................................. ON, and land at the nearest suitable airport. (2) If fuel pressure is not restored. ...................Land at nearest suitable airport. Be prepared for engine failure and an emergency landing. Page 3 - 7 Emergency Procedures DA20-C1 Flight Manual DOC # DA202-C1 Revision 26 May 15, 2012 DOT Approved DO NOT ENGAGE STARTER IF PROPELLER IS WINDMILLING. ENGINE DAMAGE MAY RESULT. The propeller will continue to windmill as long as the airspeed is at least 60 KIAS. RESTARTING THE ENGINE WITH PROPELLER WINDMILLING (1) Airspeed (VIAS) ......................................... 73 kts (2) Mixture ....................................................... FULL RICH (3) Fuel Shut-off Valve ..................................... OPEN (4) Ignition Switch ............................................ BOTH (5) Fuel Pump .................................................. ON (6) Fuel Prime .................................................. ON (7) Throttle ....................................................... 3/4 in (2cm) forward AFTER SUCCESSFUL RE-START: (8) Oil Pressure ............................................... check (9) Oil Temperature ......................................... check (10)Fuel Prime .................................................. OFF (11)Electrically Powered Equipment ................ ON if required CAUTION Emergency Procedures DA20-C1 Flight Manual Page 3 - 8 DOC # DA202-C1 May 15, 2012 Revision 26 DOT Approved RESTARTING THE ENGINE WITH PROPELLER AT FULL STOP (1) Airspeed ..................................................... 73 kts. (2) Electrically Powered Equipment .................OFF (3) GEN/BAT Master Switch .............................ON (4) Mixture ........................................................FULL RICH (5) Fuel shut off valve .......................................OPEN (6) Fuel Pump ..................................................ON (7) Fuel Prime ..................................................ON (8) Throttle ........................................................3/4 in (2 cm) forward (9) Ignition Switch .............................................START (10)Ignition Switch with Push-to-Start (Optional) START (TURN then PUSH) The engine may also be re-started by increasing the airspeed by pushing the airplane into a descent. A loss of 1000 ft/300 m altitude must be taken into account. AN AIRSPEED OF 137 KIAS IS REQUIRED TO RESTART THE ENGINE. AFTER SUCCESSFUL RE-START: (11)Oil Pressure ................................................check (12)Oil Temperature ..........................................check (13)Fuel Prime ..................................................OFF (14)Electrically Powered Equipment .................ON if required NOTE Page 3 - 9 Emergency Procedures DA20-C1 Flight Manual DOC # DA202-C1 Revision 26 May 15, 2012 DOT Approved 3.3.2 Gliding (a) Wing Flaps .........................................................CRUISE (b) Airspeed at 1764 lbs (800 kg) ............................73 KIAS (c) Glide Ratio 11:1 Example: For every 1000 feet of altitude the aircraft can move forward 11,000 feet or 1.8 NM (3.4 km). 3.3.3 Emergency Landing (a) Emergency Landing with Engine off (1) Airspeed (Flaps in T/O position) ................ 60 KIAS (2) Airspeed (Flaps in LDG position) ............... 55 KIAS (3) Airspeed (Flaps CRUISE) .......................... 64 KIAS (4) Fuel Shut-off Valve ..................................... CLOSED (5) Mixture ....................................................... IDLE CUTOFF (6) Ignition Switch ............................................ OFF (7) Safety Belts ................................................ secured (8) Radio .......................................................... Transmit, 121.5 Mhz, giving location and intentions (9) Flaps .......................................................... as required (10)GEN/BAT Master Switch ............................ OFF (11)After Touch – Down .................................... Apply brakes Emergency Procedures DA20-C1 Flight Manual Page 3 - 10 DOC # DA202-C1 May 15, 2012 Revision 26 DOT Approved (b) Precautionary Landing with Engine Power Available A precautionary landing would be required if continuing the flight would endanger the aircraft or its occupants. Circumstances, including mechanical defects, low fuel quantity or deteriorating weather conditions could require a precautionary landing. (1) Search for a suitable place to land. Special attention must be given to wind direction and obstacles in the approach path. (2) Safety Belts .................................................secured (3) Initiate Descent (4) Mixture ........................................................FULL RICH (5) Throttle ........................................................as required (6) Trim .............................................................as required (7) Wing Flaps ..................................................as required (observe permissable speed) (8) Over fly selected landing area (not below 500 ft / 150 m above ground) to confirm suitability and that approach route is free of obstacles. (9) Climb up to pattern altitude. (10)Low pass over flight at a safe altitude to observe any possible obstacles, such as cables, fences, ditches. (11)Climb up to pattern altitude. (12)Radio ..........................................................Transmit, giving location and intentions. NOTE Page 3 - 11 Emergency Procedures DA20-C1 Flight Manual DOC # DA202-C1 Revision 26 May 15, 2012 DOT Approved (13)Final Approach: (A) Mixture ................................................. FULL RICH (B) Throttle ................................................ as required (C) Fuel Pump ........................................... ON (D) Wing Flaps .......................................... LDG (E) Airspeed .............................................. 55 KIAS (14)Touch-down is to be made with minimum airspeed, nose wheel should be kept above ground as long as possible. (15)After Touch-down: (A) Brake ................................................... as required (B) Fuel Shut-off Valve .............................. CLOSED (C) Mixture ................................................. IDLE CUT-OFF (D) Ignition Switch ..................................... OFF (E) GEN/BAT Master Switch ..................... OFF If no suitable level landing area can be found, an up-hill landing should be performed, if possible. NOTE Emergency Procedures DA20-C1 Flight Manual Page 3 - 12 DOC # DA202-C1 May 15, 2012 Revision 26 DOT Approved 3.3.4 Fire (a) Engine Fire during Engine-Start-Up on the Ground (1) Fuel Shut-off Valve ..................................... CLOSED (2) Cabin Heat ..................................................CLOSED (3) Mixture ........................................................IDLE CUTOFF (4) GEN/BAT Master Switch .............................OFF (5) Ignition Switch .............................................OFF (6) Evacuate Airplane immediately (b) Engine Fire during Flight (1) Fuel Shut-off Valve ..................................... CLOSED (2) Cabin Heat ..................................................CLOSED (3) Airspeed ......................................................73 KIAS Airspeed is for best glide with flaps in CRUISE position. If a suitable landing area is available and can be safely reached, airspeed can be increased in an attempt to extinguish the fire. Do not exceed airspeeds given for structural limitations. (4) Fuel Pump ..................................................OFF (5) Perform emergency landing with engine off according to paragraph 3.3.3. NOTE Page 3 - 13 Emergency Procedures DA20-C1 Flight Manual DOC # DA202-C1 Revision 26 May 15, 2012 DOT Approved (c) Electrical Fire including Smoke during Flight (1) GEN/BAT Master Switch ............................ OFF (2) Cabin Air .................................................... OPEN (3) Fire Extinguisher ........................................ use only if smoke development continues. IF FIRE EXTINGUISHER IS USED, THE CABIN MUST BE VENTILATED. In case the fire is extinguished and electric power is required for continuation of the flight: (4) Avionics Master Switch .............................. OFF (5) Electrically Powered Equipment ................ OFF Restore electrical power systematically allowing time to monitor the system voltmeter and amp meter between the reconnection of loads. Watch carefully for smoke. (6) Circuit Breakers ......................................... Push all circuit breakers (7) Circuit Breakers ......................................... Push BATTERY (8) GEN/BAT Master Switch ............................ ON BAT 1/2 only (9) Circuit Breakers ......................................... Push GEN & GEN CONTROL (10)GEN/BAT Master Switch ............................ ON (11)Circuit Breakers ......................................... Push AVIONICS and AVIONICS MASTER (12)Avionics Master Switch .............................. ON CAUTION NOTE Emergency Procedures DA20-C1 Flight Manual Page 3 - 14 DOC # DA202-C1 May 15, 2012 Revision 26 DOT Approved (13)Circuit Breakers ..........................................Push to activate systems as required. (14)Radio ..........................................................ON (15)Land as soon as possible. (d) Electrical Fire including Smoke on the Ground (1) GEN/BAT Master Switch ............................ OFF IF ENGINE IS RUNNING: (2) Throttle ........................................................IDLE (3) Mixture ........................................................IDLE CUTOFF (4) Fuel Shut-off Valve ......................................CLOSED (5) Ignition Switch .............................................OFF (6) Canopy .......................................................open (7) Fire Extinguisher .........................................discharge as required (e) Cabin Fire during Flight (1) GEN/BAT Master Switch ............................ OFF (2) Cabin Air .....................................................OPEN (3) Cabin Heat ..................................................CLOSED (4) Fire Extinguisher .........................................discharge as required (5) Land as soon as possible IF THE FIRE EXTINGUISHER IS USED, THE CABIN MUST BE VENTILATED. CAUTION Page 3 - 15 Emergency Procedures DA20-C1 Flight Manual DOC # DA202-C1 Revision 27 February 12, 2013 DOT Approved 3.3.5 Icing Unintentional Flight Into Icing Area (a) Leave icing area (through change of altitude or change of flight direction to reach area with higher outside air temp). (b) Continue to move control surfaces to maintain their moveability. (c) Alternate Air ........................................................ON (d) Increase RPM to avoid icing of propeller blades (observe maximum RPM). (e) Cabin Heat .........................................................ON DEFROST IN CASE OF ICING ON THE LEADING EDGE OF THE WING, THE STALL SPEED WILL INCREASE. IN CASE OF ICING ON THE LEADING EDGE OF THE WING, ERRONEOUS INDICATING OF THE AIRSPEED, ALTIMETER, RATE OF CLIMB AND STALL WARNING SHOULD BE EXPECTED. CAUTION CAUTION Emergency Procedures DA20-C1 Flight Manual Page 3 - 16 DOC # DA202-C1 May 15, 2012 Revision 26 DOT Approved 3.3.6 Recovery from Unintentional Spin (a) Throttle ............................................................... IDLE (b) Rudder ............................................................... fully applied opposite to direction of spin (c) Control Stick ....................................................... ease forward (d) Rudder ............................................................... neutral, after rotation has stopped (e) Wing Flaps ......................................................... CRUISE (f) Elevator .............................................................. pull cautiously. Bring airplane from descent into level flight position. Do not exceed maximum permissible speed (VNE ). 3.3.7 Landing with Defective Tire on Main Landing Gear (a) Final approach with wing flaps in landing position. (b) Land airplane on the side of runway opposite to the side with the defective tire to compensate for change in direction which is to be expected during final rolling. (c) Land with wing slightly tipped in the direction of the non-defective tire. To increase the maneuverability during rolling, the nose-wheel should be brought to the ground as soon as possible after touch-down. (d) To ease the load on the defective tire, the aileron should be fully applied in the direction of the non-defective tire. Page 3 - 17 Emergency Procedures DA20-C1 Flight Manual DOC # DA202-C1 Revision 26 May 15, 2012 DOT Approved 3.3.8 Electrical Power Failure (a) Total Electrical Power Failure (1) Battery Circuit Breaker ............................... If tripped, reset (2) GEN/BAT Master Switch ............................ check ON (3) Master Switch ............................................ OFF if power not restored (4) If Unsuccessful ........................................... Land at nearest suitable airport (b) Generator Failure GEN. ANNUNCIATOR ILLUMINATED (1) GEN/BAT Master Switch ............................ Cycle Generator Master Switch OFF - ON (2) Generator Circuit Breaker .......................... If tripped, reset (3) Generator CONTROL Circuit Breaker ....... If tripped, reset (4) If Generator can not be brought on-line ..... Switch OFF all non-flight essential electrical consumers. Monitor Ammeter and Voltmeter. Land at nearest suitable airport. There is 30 minutes of battery power at a discharge load of 20 amperes when the battery is fully charged and properly maintained. NOTE Emergency Procedures DA20-C1 Flight Manual Page 3 - 18 DOC # DA202-C1 May 15, 2012 Revision 26 DOT Approved (c) Low Voltage Indication (needle in yellow Arc) LOW VOLTAGE INDICATION (NEEDLE IN YELLOW ARC) WHILE AIRPLANE IS ON THE GROUND (1) Engine RPM ............................................... Increase RPM until needle is in the Green Arc. This should occur before exceeding 1100 RPM. (2) Non-flight essential electrical consumers ....Switch OFF consumers until needle is in the Green Arc. (3) If needle remains in the yellow arc ..............Discontinue any planned flight and the ammeter is indicating to the activity left of center (discharge). LOW VOLTAGE INDICATION (NEEDLE IN YELLOW ARC) DURING FLIGHT (1) All non-f