Diamond AIRPLANE FLIGHT MANUAL DA 42 NG

FY Doc. #7.01.16-E | TR-OAM-42-383 16-Aug-2022 Cover Page DA 42 NG AFM Diamond Introduction AIRCRAFT FOREWORD We congratulate you on the acquisition of your new DIAMOND DA 42 NG. Skillful operation of an airplane increases both safety and the enjoyment of flying. Please take the time therefore, to familiarize yourself with your new DIAMOND DA 42 NG. This airplane may only be operated in accordance with the procedures and operating limitations of this Airplane Flight Manual. Before this airplane is operated for the first time, the pilot must familiarize himself with the complete contents of this Airplane Flight Manual. In the event that you have obtained your DIAMOND DA 42 NG second-hand, please let us know your address, so that we can supply you with the publications necessary for the safe operation of your airplane. This document is protected by copyright. All associated rights, in particular those of translation, reprinting, radio transmission, reproduction by photo-mechanical or similar means and storing in data processing facilities, in whole or part, are reserved. Copyright © by: DIAMOND AIRCRAFT INDUSTRIES GMBH N.A, Otto-Strasse 5 A-2700 Wiener Neustadt, Austria Phone. : +43-2622-26700 Fax © +43-2622-26780 E-Mail : office@diamond-air.at Doc. # 7.01.16-E Rev. 5 10-Jun-2021 Page 0-1 Introduction @ Diamond DA 42 NG AFM AIRCRAFT 0.1 APPROVAL The content of approved chapters is approved by EASA. All other content is approved by DAI under the authority of EASA DOA No. EASA.21J.052 in accordance with Part 21, 0.2 RECORD OF REVISIONS All revisions of this manual, with the exception of - + Temporary Revisions, + updates of the modification level (Section 1.1), + updated mass and balance information (Section 6.3), + updates of the Equipment Inventory (Section 6.5), and + updates of the List of Supplements (Section 9.2) must be recorded in the following table. The new or amended text is indicated by a vertical black line at the left hand side of the revised page, with the revision number and date appearing at the bottom of the page. If pages are revised which contain information valid for your particular serial number (modification level of the airplane, weighing data, Equipment Inventory, List of Supplements), then this information must be transferred to the new pages in hand-writing. The cover pages of Temporary Revisions, if applicable, are inserted behind the cover page of this manual. Temporary Revisions are used to provide information on systems or equipment until the next ‘permanent’ Revision of the Airplane Flight Manual. When a ‘permanent’ Revision covers a Mandatory or Optional Design Change Advisory (MAM or OAM), then the corresponding Temporary Revision is superseded. For example: If Revision 5 covers OAM 42-039, then the Temporary Revision TR OAM-42-039 is superseded by the 'permanent’ Revision 5. Page 0-2 Rev. 5 10-Jun-2021 Doc. # 7.01.16-E Diamond DA 42 NG AFM 9» Introduction AIRCRAFT Rev.| pion Coo: Paget) Date of EASA Approval Date Signature No. Revision [| Approval No. Date Inserted Revision 1of the AFM Doc. No. T0116-E ls 1 | FAA-Approval | © | 00,0-0a, 0:3, 0-4 | 19-Jun-2012 21-2012 approved by EASA under Project No. 0010016964. MAM 42650, 42.685, 42606, 42.701, 42757, 42-778, ke 2.785 pop km i 42.055, 42.056, > Sigs oi 42-004, 42-118, All except Cover is 2 |i innm | fie 28-Feb-2014 pai 18-Mar-2014 4219, 42-203, oh 4 422008 42 pest 1938, 42-213, EASA 241080 42-202, 42-224, 42.226, 42-251 Correchions Revision 3 of MAM the AFM 42-650, 42.678, Doc. No. 42.759 All except Cover 7.01.16:Eis 3 A 01-Apr-2014 05-tay-2014 0AM Page ie approved by ay 42253, 42.260 EASA with Comections Approval No.10048945. Doc. # 7.01.16-E Rev. 5 10-Jun-2021 Page 0-3 é Diamond Introduction DA 42 NG AFM AIRCRAFT Rev. Cha Data of EASA | Approval Dato No, | Romson | ter | Pegs) | poison ||ApprovalMo.| Date | Inserted | Snare MAM 42- 600, -744, +756, 828 8-760, 855, -868, -985, -936/b, +942, +973, 476, -978, -995, 100, -1030, Revision4 of OAM 42- the AFM 111/a&-158/a 8 Doc. No, 246, -15000 701.16-Eis 4 | as0070, | an | M pre 02002017 || approved | 27-0c12017 73,178,194, under the +208, -209,-213/a, authority of 218,228, -240, DOA No. -241,-247,-250, EASA21J.052 -265, - 251, -259, 267,270,273, 271,219, 281, -283,-287, -266, -298,-301,-304, Comections Page 0-4 Rev. 5 10-Jun-2021 Doc. # 7.01.16-E — » Diamond DA 42 NG AFM Introduction AIRCRAFT Rev, Chap: Date of EASA Approval Date No, | Reason Page(s) Revision || ApprovalNo.| Date Insertog | Siamature MAM 42- 600i, 1024, -1025,-1034, 1035, 1072, 1097, 1104, 1114, 41141, 1188, 1179, 1183, 1188, fe 1191, 1195, eT aap, Losi) -D56/a, -160/e, All except Cover oe 1 il Now-2021 5 A700, -2080a, Page 0-Jun-202 finn 02-Now-202 2280, 2400, kd 24113, -250a, pis 4 -251/a, -258, ) ripe, EASA21J.052 3dr, -312, 32418, 333, 33,397, 339, 20a, “343,349, Comections Doc. # 7.01.16-E Rev. 5 10-Jun-2021 Page 0-5 3-91°LO°L # 900 LZoZ-unr-0L G ney 9 - 0 ebed LE0g-unr-0l. i LZ0Z-unr-0L el Leog-unr-gL FA LZ0Z-unr-QL 92-1 Lz0z-unr-0L LL I L20Z-Unp-01 gl 8eq “abeg TE) L20Z-unr-oL vet LZ0Z-unr-0L ral LZoz-unr-ol ze L20z-unr-gi 91-0 LZ0Z-unp-pL 12-1 LZoz-unr-oL S10 LZ0Z-unp-gL 0z-L Legz-unr-oi vio LZ0Z-unp-gL BLL Lzoz-unr-gL £10 LZ0Z-unp-gi gL Lzoz-unr-gl ZL LZoz-unp-pL LL LZ0z-unr-QL L-0 LZ07-unr-01 aL 1zoz-unr-0L oo 1202-unf-01 Sit kzoz-unr-ol 50 1z0z-unr-o1 piel kzoz-unr-ol 80 LZ0Z-Un0-01 Il 1Z0z-un-gL 0 1202-01 Zi 1z0z-unr-o} 90 LZoz-unr-oL bt kzoz-unr-ok 0 LZ0Z-UNP-OL ob Lzoz-unr-oL 2] LZOZ-Unp-0L BL Lzz-unr-gl £0 LZ0Z-Unp-01 a LZ0Z-Unr-0L 0 LZ0Z-unr-0L 1-1 LZ0z-unr-gl 1-0 LZ0Z-unr-0L ol 1Z0Z-unr-0l 20-0 L202-unr-oi gi cLoz-unr-gL 0-0 0 eq obed ud. oieq lietmd) ER S§35Vd JAILSTI4TI0ISTT €0 W4V ON Z¥ va Bae Seok uonanpo.u| puouieiq Va RS MS SE SE WE RES SE EEN SEN EEN EEN EEN EES EES EES Emm EE — DA 42 NG AFM Dia Introduction AIRCRAFT Ch. | Page| Date Ch. Page _ Date 2 appr. 2-1 10-Jun-2021 2 appr. 2-28 10-Jun-2021 appr, 2:2 10-Jun-2021 appr. 2-29 10-Jun-2021 appr, 2-3 10-Jun-2021 appr. 2-30 10-Jun-2021 appr. 2-4 10-Jun-2021 appr. 2-31 10-Jun-2021 appr. 2-5 10-Jun-2021 appr. 2-32 10-Jun-2021 appr. 2-6 10-Jun-2021 appr. 2-33 10-Jun-2021 appr, 2-7 10-Jun-2021 appr. 2-34 10-Jun-2021 appr, 2-8 10-Jun-2021 appr. 2-35 10-Jun-2021 appr. 2-9 10-Jun-2021 appr. 2-36 10-Jun-2021 appr. 2-10 10-Jun-2021 appr. 2-37 10-Jun-2021 appr. 2-11 10-Jun-2021 appr. 2-38 10-Jun-2021 appr. 2-12 10-Jun-2021 appr. 2-39 10-Jun-2021 appr. 2-13 10-Jun-2021 appr. 2-40 10-Jun-2021 appr. 2-14 10-Jun-2021 appr. 2-41 10-Jun-2021 appr. 2-15 10-Jun-2021 appr. 2-42 10-Jun-2021 appr. 2-16 10-Jun-2021 appr. 2-43 10-Jun-2021 appr. 2-17 10-Jun-2021 appr. 2-44 10-Jun-2021 appr. 2-18 10-Jun-2021 appr. 2-45 10-Jun-2021 appr. 2-19 10-Jun-2021 appr. 2-46 10-Jun-2021 appr. 2-20 10-Jun-2021 appr. 2-47 10-Jun-2021 appr. 2-21 10-Jun-2021 appr. 2-48 10-Jun-2021 appr. 2-22 10-Jun-2021 appr. 2-23 10-Jun-2021 appr. 2-24 10-Jun-2021 appr. 2-25 10-Jun-2021 appr. 2-26 10-Jun-2021 appr. 2-27 10-Jun-2021 Doc. # 7.01.16-E Rev. 5 10-Jun-2021 Page 0-7 C—O EE EE RE SS SS RS RS SS — — — — “Diamond Introduction prides DA 42 NG AFM Ch. : Page Date | Ch. Page i Date 3 31 10-Jun-2021 3 3-28 10-Jun-2021 3-2 10-Jun-2021 3-29 10-Jun-2021 33 10-Jun-2021 3-30 10-Jun-2021 3-4 10-Jun-2021 3-31 10-Jun-2021 3-5 10-Jun-2021 3-32 10-Jun-2021 3-6 10-Jun-2021 3-33 10-Jun-2021 3-7 10-Jun-2021 3-34 10-Jun-2021 3-8 10-Jun-2021 3-35 10-Jun-2021 3.9 10-Jun-2021 3-36 10-Jun-2021 3-10 10-Jun-2021 3-37 10-Jun-2021 31 10-Jun-2021 3-38 10-Jun-2021 3-12 10-Jun-2021 3-39 10-Jun-2021 3-13 10-Jun-2021 3-40 10-Jun-2021 3-14 10-Jun-2021 3-41 10-Jun-2021 3-15 10-Jun-2021 3-42 10-Jun-2021 3-18 10-Jun-2021 3-43 10-Jun-2021 3-17 10-Jun-2021 3-44 10-Jun-2021 3-18 10-Jun-2021 3-45 10-Jun-2021 3-19 10-Jun-2021 3-46 10-Jun-2021 3-20 10-Jun-2021 3-47 10-Jun-2021 3-21 10-Jun-2021 3-48 10-Jun-2021 3-22 10-Jun-2021 3-49 10-Jun-2021 3-23 10-Jun-2021 3-50 10-Jun-2021 3.24 10-Jun-2021 3-51 10-Jun-2021 3-25 10-Jun-2021 3-52 10-Jun-2021 3-26 10-Jun-2021 3-53 10-Jun-2021 3-27 10-Jun-2021 3-54 10-Jun-2021 Page 0-8 Rev. 5 10-Jun-2021 Doc. # 7.01.16-E 6 - 0 abe LZog-unr-0l G ‘hoy 3-9L°1L0°L #000 LZ0zZ-unr-0L LZ0Z-unr-0L 1Z0Z-unr-0 1 Lzoz-unr-0L LZ0Z-unr-0L 120Z-unr-0L LZ0z-unr-L LZ0Z-unr-oL LZ0z-unr-gL VZ0Z-Unr-0k LZ0Z-unr-oL LZ0Z-unr-0L LZ0Z-unp-oL LZ0Z-UNr-0L LZ02-unr-0L LZ0g-unr-gL 120z-unr-ok 1202-unr-0L LZ0Z-unr-0L L202-Unr-0L LZ0Z-unr-0L L202-unr-gl LZ0zZ-unr-0i LZ0Z-unr-oL L202-Unr-0l LZoz-unp-0L LZoe-unr-gi 12Yy 92-vb SZvY vZ-yt £2-vr zZzvr LZ-vr 02-¥r GLY gL-¥p Livy 9L-vp Sl-vp rL-Yp El-p Zl-vr LYE 0L-vr 6-Y¥ evr Ly OVE Sv (aid evr ad bv wy eeq 8beg Uy Leoe-unr-oL Leoe-unr-gL Lege-unr-0L bzaz-unr-l 1Z0Z-unr-01 LZ02-unr-0L LZog-unr-gl L202-unr-glL LZ0Zg-unr-gL LZog-unp-oL L2oe-unr-gl LZOZ-unr-oL LZ0E-UNr-0l LZOZ-Unf-al LZ0Z-unr-0l LZ0g-unr-QL L20Z-unr-0l L20Z-unr-gL Lz20g-unr-ol LZ0g-unr-0i LZoZ-unr-gL Lzoe-unr-gi ejeq uononposu| 1AVHIHIY puoweiq é» W4vY ON Z¥ Va EE EE @ Diamond Introduction pried DA 42 NG AFM | ch. Page | Date Ch. Page | Date 4A 4A-28 10-Jun-2021 4A 47-55 10-Jun-2021 4A-29 10-Jun-2021 4A-56 10-Jun-2021 4A-30 10-Jun-2021 4A-67 10-Jun-2021 44-31 10-Jun-2021 4A-58 10-Jun-2021 44-32 10-Jun-2021 44-59 10-Jun-2021 4A-33 10-Jun-2021 44-60 10-Jun-2021 4A-34 10-Jun-2021 4A-61 10-Jun-2021 4A-35 10-Jun-2021 AA-62 10-Jun-2021 4A-36 10-Jun-2021 4A-63 10-Jun-2021 4A-37 10-Jun-2021 4A-64 10-Jun-2021 4A-38 10-Jun-2021 4A-65 10-Jun-2021 4A-39 10-Jun-2021 4A-66 10-Jun-2021 4A-40 10-Jun-2021 4A-67 10-Jun-2021 4A-41 10-Jun-2021 4A-68 10-Jun-2021 47-42 10-Jun-2021 4A-69 10-Jun-2021 4A-43 10-Jun-2021 44-70 10-Jun-2021 4A-44 10-Jun-2021 4A-45 10-Jun-2021 4A-48 10-Jun-2021 AA-47 10-Jun-2021 4A-48 10-Jun-2021 4A-49 10-Jun-2021 4A-50 10-Jun-2021 4A-51 10-Jun-2021 4A-52 10-Jun-2021 4A-53 10-Jun-2021 4A-54 10-Jun-2021 Page 0 - 10 Rev. 5 10-Jun-2021 Doc. # 7.01.16-E - DA 42 NG AFM Diamond Introduction AIRCRAFT Ch, Page Date | Ch. Page Date 4B 4B-1 10-Jun-2021 4B 4B-28 10-Jun-2021 48-2 10-Jun-2021 4B-29 10-Jun-2021 48-3 10-Jun-2021 4B-30 10-Jun-2021 4B-4 10-Jun-2021 48-31 10-Jun-2021 4B-5 10-Jun-2021 48-32 10-Jun-2021 4B-6 10-Jun-2021 4B-33 10-Jun-2021 4B-7 10-Jun-2021 4B-34 10-Jun-2021 4B-8 10-Jun-2021 48-35 10-Jun-2021 48-9 10-Jun-2021 4B-36 10-Jun-2021 4B-10 10-Jun-2021 48-37 10-Jun-2021 4B-11 10-Jun-2021 48-38 10-Jun-2021 4B-12 10-Jun-2021 48-39 10-Jun-2021 48-13 10-Jun-2021 48-40 10-Jun-2021 48-14 10-Jun-2021 48-41 10-Jun-2021 4B-15 10-Jun-2021 48-42 10-Jun-2021 4B-16 10-Jun-2021 48-43 10-Jun-2021 4B-17 10-Jun-2021 48-44 10-Jun-2021 4B-18 10-Jun-2021 4B-45 10-Jun-2021 4B-19 10-Jun-2021 48-46 10-Jun-2021 4B-20 10-Jun-2021 4B-21 10-Jun-2021 4B-22 10-Jun-2021 4B-23 10-Jun-2021 48-24 10-Jun-2021 48-25 10-Jun-2021 48.26 10-Jun-2021 4B-27 10-Jun-2021 Doc, #7.01.16-E Rev. 5 10-Jun-2021 Page 0-11 mn mm En Em mm mmm Em En EE Em EE mm Em Introduction rte DA 42 NG AFM Ch. Page Date _Ch. Page Date 5 51 10-Jun-2021 5 5-28 10-Jun-2021 5-2 10-Jun-2021 5-29 10-Jun-2021 53 10-Jun-2021 5-30 10-Jun-2021 5-4 10-Jun-2021 5-31 10-Jun-2021 5-5 10-Jun-2021 5-32 10-Jun-2021 5-6 10-Jun-2021 5-33 10-Jun-2021 57 10-Jun-2021 5-34 10-Jun-2021 5-8 10-Jun-2021 5-35 10-Jun-2021 59 10-Jun-2021 5-36 10-Jun-2021 5-10 10-Jun-2021 5-37 10-Jun-2021 5-11 10-Jun-2021 5-38 10-Jun-2021 5-12 10-Jun-2021 5-39 10-Jun-2021 5-13 10-Jun-2021 5-40 10-Jun-2021 5-14 10-Jun-2021 5-41 10-Jun-2021 5-15 10-Jun-2021 5-42 10-Jun-2021 5-16 10-Jun-2021 5-43 10-Jun-2021 5-17 10-Jun-2021 5-44 10-Jun-2021 5-18 10-Jun-2021 5-19 10-Jun-2021 5-20 10-Jun-2021 5-21 10-Jun-2021 5-22 10-Jun-2021 5-23 10-Jun-2021 5-24 10-Jun-2021 5-25 10-Jun-2021 5-26 10-Jun-2021 5-27 10-Jun-2021 Page 0-12 Rev. 5 10-Jun-2021 Doc. # 7.01.16-E “Diamond DA 42 NG AFM prude Introduction Ch. Page Date ch. Page Date | 6 6-1 10-Jun-2021 6 6-28 10-Jun-2021 6-2 10-Jun-2021 6-29 10-Jun-2021 6-3 10-Jun-2021 6-30 10-Jun-2021 6-4 10-Jun-2021 6-31 10-Jun-2021 6-5 10-Jun-2021 6-32 10-Jun-2021 6-6 10-Jun-2021 6-33 10-Jun-2021 6-7 10-Jun-2021 6-34 10-Jun-2021 6-8 10-Jun-2021 6-9 10-Jun-2021 L_Ch. Page Date 6-10 10-Jun-2021 7 71 10-Jun-2021 6-11 10-Jun-2021 7-2 10-Jun-2021 6-12 10-Jun-2021 7-3 10-Jun-2021 6-13 10-Jun-2021 7-4 10-Jun-2021 6-14 10-Jun-2021 7-5 10-Jun-2021 6-15 10-Jun-2021 7-6 10-Jun-2021 6-16 10-Jun-2021 7-7 10-Jun-2021 6-17 10-Jun-2021 7-8 10-Jun-2021 6-18 10-Jun-2021 7-9 10-Jun-2021 6-19 10-Jun-2021 7-10 10-Jun-2021 6-20 10-Jun-2021 7-1 10-Jun-2021 6-21 10-Jun-2021 7-12 10-Jun-2021 6-22 10-Jun-2021 7-13 10-Jun-2021 6-23 10-Jun-2021 7-14 10-Jun-2021 6-24 10-Jun-2021 7-15 10-Jun-2021 6-25 10-Jun-2021 7-16 10-Jun-2021 6-26 10-Jun-2021 7-17 10-Jun-2021 6-27 10-Jun-2021 7-18 10-Jun-2021 Doc. #7.01.16-E Rev. 5 10-Jun-2021 Page 0-13 ~~ ~ 3-91°10°L # 200 LZog-unr-o} g roy ¥l - 0 afieg Lgoz-unr-ok ZL Lg0g-unr-oL (WI LZ0Z-UnP-0L 02-2 120Z-Unr-0b 69-2 LE20Z-unr-0k 89-4 LZ0Z-UNP-0L 194 LZ20Z-Unr-0L ag- LZ0Z-unr-0l 594 LZ0Z-unr-0L $01 LZ0Z-unr-0b £01 LEOZ-UNP-0L 292 LZ0Z-unr-01 19-1 LZ0Z-Unr-01 09-2 L202-unr-0L 65-2 LZ0z-unr-L 86-2 LZ0z-unr-gL 152 Lg0z-unr-gL aG-4 LZ0Z-Unr-01 56-2 LZ0Z-unp-0L GL LZ0Z-Unr-gL £64 LZoz-unr-0L 26-1 LZ0Z-Unr-0L LG Leog-unr-gl 05-2 LZ0z-unp-0L 6b-L LZ0z-unr-QL ab-L LZ0Z-unr-0l tL LEOZ-unr-0L ap=1 LZ0Z-UnP-0l LZ0Eg-unr-0L LZ0Z-UnP-01 LZ0g-unr-gL LZ0Z-unr-g1. LZ0g-unr-gL LZ0g-unr-gL LZ0g-unr-01 LZ0g-unr-oL VzZoz-unr-oL Lzoz-unr-oi LZog-unr-oi LZ0Z-unr-0i Lzog-unr-0l Leog-unr-gi Lzoz-unr-0i Lzoz-unr-0L L20Z-unr-0k LZ0Z-unr-0L LZOZ-unr-0l LZ0g-unr-0l LZ0Z-unr-0l LZ0Z-unr-oi LZ0Z-unr-0L LZ02-unr-oL Lzoz-unr-ol L LZ0Z-unr-0L Si=L bird Er-L [ATS WL or-L BE-L 8E-L LE-L ejeq [ eBed Ho ejeq WdY ON Z¥ va LAVHIUIV eIq é» uononposu) C—O EE EE EE ES EE SE ES — — — — - DA 42 NG AFM ¥» Diamond IntroductionAIRCRAFT ch | Page Date| [Ch | Page Date 7 7-73 10-Jun-2021 8 8-1 10-Jun-2021 7-74 10-Jun-2021 8-2 10-Jun-2021 7-75 10-Jun-2021 8-3 10-Jun-2021 7-76 10-Jun-2021 8-4 10-Jun-2021 7-17 10-Jun-2021 85 10-Jun-2021 7-78 10-Jun-2021 8-6 10-Jun-2021 7-19 10-Jun-2021 8-7 10-Jun-2021 7-80 10-Jun-2021 8-8 10-Jun-2021 7-81 10-Jun-2021 8-9 10-Jun-2021 7-82 10-Jun-2021 8-10 10-Jun-2021 7-83 10-Jun-2021 8-11 10-Jun-2021 7-84 10-Jun-2021 8-12 10-Jun-2021 7-85 10-Jun-2021 8-13 10-Jun-2021 7-86 10-Jun-2021 8-14 10-Jun-2021 7-87 10-Jun-2021 8-15 10-Jun-2021 7-88 10-Jun-2021 8-16 10-Jun-2021 7-89 10-Jun-2021 7-90 10-Jun-2021 Ch. Page Date | 9 9-1 10-Jun-2021 9-2 10-Jun-2021 9-3 10-Jun-2021 9-4 10-Jun-2021 9-5 10-Jun-2021 9-6 10-Jun-2021 Doc. #7.01.16-E Rev. 5 10-Jun-2021 Page 0-15 Introduction Diamond DA 42 NG AFM AIRCRAFT TABLE OF CONTENTS Chapter GENERAL (a non-approved chapter) ....... SR RR a a pr 1 OPERATING LIMITATIONS {(anapprovedchapter) ........ciiiiiiiiiiaiiinisiaiaiieis aes 2 EMERGENCY PROCEDURES {anon-approved chapter) ............ovreimiinionnrananeaciann 3 NORMAL OPERATING PROCEDURES {a non-approved chapter) «.....ocivii ie seas vases dias 4A ABNORMAL OPERATING PROCEDURES (a non-approved chapter) ........covivivuivnienniri inna iianan 4B PERFORMANCE {2 NOn-apPIOVET CREPIEEY: «sss ime ie ees ss emai Ss 49 sss 5 MASS AND BALANCE / EQUIPMENT LIST {anon-approved chapter) ........coevieniuiniriareniosninerinnsans 6 DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS {anon-approved chapter) ............. oii 7 AIRPLANE HANDLING, CARE AND MAINTENANCE {anon-approved chapter) ............coiiiiiiiiiiinaiiiieiaaaan 8 SUPPLEMENTS i. . ou iis ies vie aii a alii ie Sieve ainsi an : Page 0- 16 Rev. 5 10-Jun-2021 Doc. # 7.01.16-E DA 42 NG AFM Diamond AIRCRAFT General 1.1 INTRODUCTION 1.2 CERTIFICATION BASIS 1.3 WARNINGS, CAUTIONS AND NOTES 1.4 DIMENSIONS 1.7 THREE-VIEW DRAWING 1.8 G1000 AVIONICS SYSTEM 1.9 SOURCE DOCUMENTATION CHAPTER 1 GENERAL 1.5 DEFINITIONS AND ABBREVIATIONS 1.6 UNITS OF MEASUREMENT Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 1-1 General “Diamond DA 42 NG AFMAIRCRAFT 1.1 DUCTION This Airplane Flight Manual has been prepared in order to provide pilots and instructors with all the information required for the safe and efficient operation of the airplane. The Airplane Flight Manual includes all the data which must be made available to the pilot according to the JAR-23 requirement. Beyond this, it contains further data and operating instructions which, in the manufacturer's opinion, could be of value to the pilot. Equipment and modification level (design details) of the airplane may vary from serial number to serial number. Therefore, some of the information contained in this manual is applicable depending on the respective equipment and modification level. The exact equipment of your serial number is recorded in the Equipment Inventory in Section 6.5. The modification level is recorded in the following table (as far as necessary for this manual). Modification Source Installed Maximum Landing Mass 1999 kg MAM 42-659 Byes a no Maximum Take-Off Weight 1999 kg and Maximum Zero Fuel MAM 42-678 Ayes 0 no Mass 1835 kg Engine Software VC33_2_05_19" MAM 42-938 yes 0 no Garmin Hard- and Software Upgrade | (Garmin G1000 NXi) MAM 42-978 R yes ang Garmin Hard- and Software Upgrade II (Garmin G1000 NX) MAM 42-1072 |p yes il Ice Protection System OAM 42-053 yes o no Oxygen System OAM 42-055 O yes # no Auxiliary Fuel Tanks OAM 42-056 yes o no ont-Seats with Adjustable i 1 acres, OAM 42-067 oO yes Kono 0- #2. < | \ 8 — / Page Wa Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E DA 42 NG AFM Diamond General AIRCRAFT Modification Source Installed Electrical Rudder Pedal i Adjustment OAM 42-070 Pyes o no " OAM 42-101 OR Sun Visors OAM 42-142 Ayes oO no Garmin GWX 68 Weather Radar OAM 42-119 oO yes Pp no Ice Protection System OAM 42-160 Pyes o no Ice Protection System with TKS OAM 42-160 Tank in Rear Fuselage AND Hes Ano OAM 42-203 Garmin G1000, SBAS Operation OAM 42-179 yes 2 no Removal of Variable Elevator Stop OAM 42-199 O yes no Emergency Axe OAM 42-205 0 yes #Ano Short Baggage Extension OAM 42-207 O yes ® no Electronic Stability and Protection OAM 42-209 yes ono (ESP) Mission Alternator OAM 42-218 oO yes ® no Removal of Unfeathering ; Accumulator OAM 42-224 oO yes ® no Diesel Operation OAM 42-251 0 yes #£ no Garmin GTX 3X5R Transponders for ADS-B OAM 42-258 Eyes o no Front Seats with Adjustable Backrest - Hydrolok OAM 42-259 Kies Sl Maximum Take-Off Weight 2001 kg / 4411 Ib OAM 42-260 0 yes no Mid Continent MD302 Standby Attitude Module OAM 42-270 pee png Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 1-3 EN General @» Diamond DA 42 NG AFMAIRCRAFT Modification Source Installed Ghrmin GWX 70 Weather Radar OAM 42-273 oO yes no ‘Beat Warning Mute Function OAM 42-288 | A yes ono / Emergency Egress Hammer OAM 42-304 A yes 0 no “Or la tor approved software This Airplane Flight Manual must be kepton board the airplane atall times. Its designated place is the side bag of the forward left seat. The designated place for the Garmin G1000 Cockpit Reference Guide is the bag on the rear side of the forward left seat. This Airplane Flight Manual is applicable for DA 42 NG airplanes with design change MAM 42-600 installed. CAUTION The DA 42 NG is a twin engine airplane. When the operating limitations and maintenance requirements are complied with, it has the high degree of reliability which is required by the certification basis. Nevertheless, an engine failure is not completely impossible. For this reason it is highly recommended for flights during the night, on top, under IMC, or above terrain which is unsuitable for a landing, to select flight times and flight routes such that reduced performance in case of single engine operation does not constitutea risk. Page 1-4 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E Diamond TTYDA 42 NG AFM AIRCRAFT Garmin GWX 75 Weather Radar AFFECTED CHAPTERS: 1.1 INT The item is added to the Modification List: Modification Source Installed 1 Garmin GWX 75 Weather Radar | 0AM 42370 | ¥Cyes | © no Doc. # 7.01.16-E TR-OAM-42-370 11-Apr-2022 Page 1-4a DA 42 NG AFM DiamondAIRCRAFT General 1.2 RTIFICATION BASI S The certification basis is JAR-23, published on 11-Mar-1994, including Amdt. 1, and additional requirements as laid down in CRI A-01. 1.3 WARNING AUTIONS AND NOTES Special statements in the Airplane Flight Manual concerning the safety or operation of the airplane are highlighted by being prefixed by one of the following terms: in flight safety. WARNING means that the non-observation of the corresponding procedure leads to an immediate or important degradation CAUTION means that the non-observation of the corresponding procedure leads to a minor or to a more or less long term degradation in flight safety. NOTE draws the attention to any special item not directly related to safety but which is important or unusual. Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 1-5 General @ Diamond DA 42 NG AFMAIRCRAFT ENSIONS NOTE All dimensions shown below are approximate. Overall Dimensions Span $13.42 m 44 ft :13.55m 44.5 ft including ACL Length 8.56 m 28fi1in Height 249m 8ft2in Wing Airfoil : Wortmann FX 63-137/20 - W4 Wing Area 1 16.29 m? 175.3 sq.ft. Mean aerodynamic chord C1271 m 4ft2in Aspect ratio : 11.06 Dihedral + 6* Leading edge sweep a Alleron Area (total, left + right) : 0.66 m* 7.1s8q.ft. Page 1-6 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E DA 42 NG AFM Diamond GeneralAIRCRAFT Wing Flaps Area (total, left + right) Horizontal Tail Area Elevator area Angle of incidence Vertical Tail Area Rudder area Landing Gear Track Wheelbase Nose wheel Main wheel 1 218m? 23.5 sq.ft. :2.35m? 25.3 sq ft. : 0.66 m? 7.1 sq.ft. : -1.1° relative to longitudinal axis of airplane : 243m? 26.2 sq.ft. 0.78 m? 8.4 sq.ft. : 295m (9 ft8in) 1.735 m(5ft8in) : 5.00-5, for details refer to the AMM : 15x%6.0-6, for details refer to the AMM Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 1-7 Diamond DA 42 NG AFM General AIRCRAFT 1.5 DEFINITION BBREVIATIONS (a) Airspeeds CAS: Calibrated Airspeed. Indicated airspeed, corrected for installation and instrument errors. CAS equals TAS at standard atmospheric conditions (ISA) at MSL. IAS: Indicated Airspeed as shown on an airspeed indicator. KCAS: CAS in knots, KIAS: IAS 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. Vo! Operating Maneuvering Speed. Full or abrupt control surface movementis not permissible above this speed. Veg Maximum Flaps Extended Speed. This speed must not be exceeded with the given flap setting. Vig! Maximum Landing Gear Extended Speed. This speed may not be exceeded if the landing gear is extended. Vioe! Maximum Landing Gear Operating Speed for Extension. This speed may not be exceeded during the extension of the landing gear. Vior: Maximum Landing Gear Operating Speed for Retraction. This speed may not be exceeded during the retraction of the landing gear. Vicks Minimum Control Speed - Airborne. Minimum speed necessary to be able to control the airplane in case of one engine inoperative. Vie: Never Exceed Speed in smooth air. This speed must not be exceeded in any operation, Page 1-8 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E DA 42 NG AFM ¥p Diamond General AIRCRAFT Vio! Maximum Structural Cruising Speed. This speed may be exceeded only in smooth air, and then only with caution. Vs Stalling Speed, or the minimum continuous speed at which the airplane is still controllable in the given configuration. Veo! Stalling Speed, or the minimum continuous speed at which the airplane is still controllable in the landing configuration. Vari Stalling Speed, or the minimum continuous speed at which the airplane is still controllable with flaps and landing gear retracted. Vssg Minimum Control Speed for Schooling. Minimum speed necessary in case of one engine intentionally inoperative / idle (training purposes). I'S Best Angle-of-Climb Speed. vy Best Rate-of-Climb Speed. Vyse: Best Rate of-Climb Speed for one engine inoperative. (b) Meteorological Terms ISA: International Standard Atmosphere. Conditions at which air is identified as an ideal dry gas. The temperatureat mean sea level is 15 °C (59 °F), air pressure at MSL is 1013.25 hPa (29.92 inHg); the temperature gradient up to the altitude at which the temperature reaches -56.5 °C (-69.7 °F) is -0.0065 °C/m (-0.00357 °F/ft), and above this 0 °C/m (0 °F/ft). MSL: Mean Sea Level, OAT: Outside Air Temperature, Doc. No, 7.01.16-E Rev. 5 10-Jun-2021 Page 1-9 General Diamond DA 42 NG AFM QNH: Theoretical atmospheric pressure at MSL, calculated from the elevation of the measuring point above MSL and the actual atmospheric pressure at the measuring point. Density Altitude: Altitude in ISA conditions at which the air density is equal to the current air density. Indicated Pressure Altitude: Altitude reading with altimeter set to 1013.25 hPa (29.92 inHg). Pressure Altitude: Altitude indicated by a barometric altimeter, which is setto 1013.25 hPa (29.92 inHg). The Pressure Altitude is the Indicated Pressure Altitude corrected for installation and instrument errors. In this Airplane Flight Manual altimeter instrument errors are regarded as zero. Wind: The wind speeds which are shown as variables in the diagrams and tables in this manual should be regarded as headwind or tailwind components of the measured wind. i Fli lannin AGL: Above Ground Level. Demonstrated Crosswind Component: The speed of the crosswind component at which adequate maneuverability for take-off and landing has been demonstrated during type certification. Page 1-10 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E DA 42 NG AFM ¥p Diamond General AIRCRAFT MET: Weather, weather advice. NAV: Navigation, route planning. RoC: Rate of Climb. (d) Mass and Balance CG: Center of Gravity, also called 'center of mass’. Imaginary point in which the airplane mass is assumed to be concentrated for mass and balance calculations. Its distance from the Datum Plane is equal to the Center of Gravity Moment Arm. Center of Gravity Moment Arm: The Moment Arm whichis obtained if one divides the sum of the individual moments of the airplane by its total mass. Center of Gravity Limits: The Center of Gravity range within which the airplane, at a given mass, must be operated. DP: Datum Plane; an imaginary vertical plane from which all horizontal distances for center of gravity calculations are measured. Empty Mass: The mass of the airplane including unusable fuel, all operating fluids and the maximum quantity of oil. Maximum Take-off Mass: The maximum permissible mass for take-off, Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 1-11 General @ Diamond DA 42 NG AFMAIRCRAFT Maximum Landing Mass: The highest mass for landing conditions atthe maximum descent velocity. This velocity was used in the strength calculations to determine the landing gear loads during a particularly hard landing. Moment Arm: The horizontal distance from the Datum Plane to the Center of Gravity of a component. Moment: The mass of a component multiplied by its moment arm, Usable fuel: The quantity of fuel available for fight planning. Unusable fuel: The quantity of fuel remaining in the tank which cannot be used for flight. Useful load: The difference between take-off mass and empty mass. (e} Engine EECU: Electr. Engine Control Unit RPM: Revolutions per minute (rotational speed of the propeller) Engine starting fuel temperature: Above this fuel temperature the engine may be started. Take-off fuel temperature: Above this fuel temperature take-off power setting is permitted. OELl: One engine inoperative Page 1-12 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E DA 42 NG AFM ¥p Diamond General AIRCRAFT f) Designation of the Circuit Breakers on the Instrument Panel LH MAIN BUS: com COM Radio No. 1 GPS/NAV1 Global Positioning System and NAV Receiver No. 1 XPDR Transponder ENG INST Engine Instruments PITOT Pitot Heating System XFER PUMP/DE-ICE Aux Fuel Pump / De-Icing System TAXIUMAP/ACL Taxi-, Map-, Anti Collision Light FLOOD Flood Light PFD Primary Flight Display ADC Air Data Computer AHRS Attitude Heading Reference System GEAR WRN/ELEV. LIMIT Landing Gear Annunciation / Variable Elevator Stop GEAR Landing Gear Control RH MAIN BUS: MFD Multi Function Display AH Artificial Horizon / Standby Attitude Module STALL WRN Stall Warning System FLAP Flap System LDG LT/START Landing Light / Start INST LT/ NAV LT Instrument-, Navigation (Position) Light AV/CDU/FAN Avionic-, CDU-Cooling Fans AVIONIC BUS Avionic Bus AV CONT./AP. WRN. Avionic Control / Autopilot Warning (not used) Doc. No, 7.01.16-E Rev. 5 10-Jun-2021 Page 1-13 r— “Diamond DA 42 NG AFMAIRCRAFT AVIONICS BUS: COM2 COM Radio No. 2 GPS/NAVZ Global Positioning System and NAV Receiver No, 2 AUDIO Audio Panel AUTO PILOT Auto Pilot System Wx 500 Stormscope ADF Automatic Direction Finder DME Distance Measuring Equipment Wx RDR Weather Radar TAS Traffic Advisory System DATA LINK GDL 69A Data Link System IRIDIUM GSR 56 Satellite Receiver LH ENG ECU BUS: ECU BUS LH ECU Bus ECUB LHECUB ECU A LHECU A LH BUS: ALT.LH LH Alternator BATT Battery FUEL PUMPS LH ENGINE: FUEL PUMP A LH ECU A Fuel Pump FUEL PUMP B LH ECU B Fuel Pump Page 1-14 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E DA 42 NG AFM “Diamond General AIRCRAFT RH ENG ECU BUS: ECU BUS RH ECU Bus ECUB RHECUB ECU A RHECUA RH BUS: ALT.RH RH Alternator BATT Battery FUEL PUMPS RH ENGINE: FUEL PUMP A RH ECU A Fuel Pump FUEL PUMP B RH ECU B Fuel Pump (a) Equipment ELT: Emergency Locator Transmitter (h) Design Change Advisories MAM: Mandatory Design Change Advisory OAM: Optional Design Change Advisory VAM: Variant Design Change Advisory Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 1-15 General Diamond DA 42 NG AFM AIRCRAFT (i) Miscellaneous ACG: ATC: CFRP: EASA: | EFB: EPU: GIA: GFRP: GPS: IFR: |] IPL: JAR: JC/VP: Austro Control GmbH (Austrian Airworthiness Autharity) Air Traffic Control Carbon Fiber Reinforced Plastic European Aviation Safety Agency Electronic Flight Bag External Power Unit Garmin Integrated Avionics Glass Fiber Reinforced Plastic Global Positioning System Instrument Flight Rules Interference Path Loss Joint Aviation Requirements Joint Certification/Validation Procedure Primary Certification Authority Portable Electronic Device Parts per Million (Dosage) Transmitting Portable Electronic Device Visual Flight Rules Page 1-16 Rev. § 10-Jun-2021 Doc. No. 7.01.16-E ¥p Diamond DA 42 NG AFM General AIRCRAFT 1.6 UNITS OF MEASUREMENT | T Dimension Sl-Units US Units Conversion Length [mm] millimeters | [in] inches [mm] / 25.4 = [in] [ml meters If feet [m]/ 0.3048 = [fi] [km] kilometers | [NM] nautical [km] / 1.852 = [NM] miles Volume 0} liters [US gal] USagallons |[l]/3.7854 = [US gal] [ats] US quarts [11 / 0.9464 = [gts] [ml] milliliter [oz] ounce [ml] x 0.033814 = [oz] Speed [km/h] kilometers [kts] knots [km/h] f 1.852 = [kts] perhour 1 imph] miles per | (km/h) / 1.609 = (mph) [m/s] par hour [m/s] x 196.85 = fom] fiom] feet por [fom] / 196.85 = [m/s]minute Speed of [RPM] revolutions per minute rotation . Mass [kg] kilograms [ib] pounds [kg] x 2.2046 = [Ib) Force, [N] newtons [Ibf] pounds [N] x 0.2248 = [Ibf] weight force Pressure [hPa] hecto- inHg] inches of [hPa] = [mbar] pascals mercury [hPa] / 33.86 = [inHg] [mbar] millibars [psi] pounds per b CE 4 ar] x 14.504 = (barf) bars square inch ar} x 14.504 = [ps] Tempera- [°C] degrees [°F] degrees [*Clx1.8 + 32 = [°F] ture Celsius Fahrenheit (I°F] - 32)/1.8 = [°C] Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 1-17 General Diamond DA 42 NG AFM Dimension Sl-Units US Units Conversion Intensity of electric current [A] amperes Electric charge (battery capacity) [Ah] ampére-hours Electric potential [V] volts Time [sec] seconds Page 1-18 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E DA 42 NG AFM Diamond General AIRCRAFT 1.6.2 CONVERSION CHART LITERS / US GALLONS Liters US Gallons US Gallons Liters 5 1.3 1 3.38 10 26 2 76 15 4.0 4 15.1 20 53 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 1.9 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 0 23.8 26 98.4 100 26.4 28 106.0 110 29.1 30 113.6 120 31.7 32 121.1 130 34.3 34 128.7 140 37.0 36 136.3 150 39.6 38 143.8 160 42.3 40 151.4 170 44.9 45 170.3 180 47.6 50 189.3 Doc. No. 7.01.16-E | Rew.5 10-Jun-2021 Page 1-19 General DA 42 NG AFM 1950 mm (6ftSin) 2205 mm (71 3in) lel 1735 mm (5 ft 8in) 8560 mm (28 ft 1in) 1900 mm Bft3in) 13420 mm (44 ft 0 in) 13550 mm (44 ft 6 in) including ACL | Page 1-20 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E DA 42 NG AFM Diamond General AIRCRAFT 18 &1 AVIONICS SYSTEM 1. The G1000 Integrated Avionics System is a fully integrated flight, engine, communication, navigation and surveillance instrumentation system. The system consists of a Primary Flight Display (PFD), Multi-Function Display (MFD), audio panel, Air Data Computer (ADC), Attitude and Heading Reference System (AHRS), engine sensors and processing unit (GEA), and integrated avionics (GIA) containing VHF communications, VHF navigation, and GPS (Global Positioning System). 2. The primary function of the PFD is to provide attitude, heading, air data, navigation, and alerting information to the pilot. The PFD may also be used for flight planning. The primary function of the MFD is to provide engine information, mapping, terrain information, autopilot operation, and for flight planning. The audio panel is used for selection of radios for transmitting and listening, intercom functions, and marker beacon functions. 3. The primary function of the VHF Communication portion of the G1000 is to enable external radio communication. The primary function of the VOR/ILS Receiver portion ofthe equipment is to receive and demodulate VOR, Localizer, and Glide Slope signals. The primary function of the GPS portion of the system is to acquire signals from the GPS satellites, recover orbital data, make range and Doppler measurements, and process this information in real-time to obtain the user's position, velocity, and time. Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 1-21 General @ Diamond DA 42 NG AFMAIRCRAFT 4. Ifthe Garmin GWX 68 or the GWX 70 weather radar system is installed, it can be used to aid the pilot in avoiding thunderstorms and associated turbulence or for ground mapping. The GWX 68 and the GWX 70 shall be used to avoid severe weather and not for penetrating severe weather. Pulse type weather radar systems like the GWX 68 and the GWX 70 detect precipitation only, not clouds or turbulence. The display may indicate clear areas between intense returns, but this does not necessarily mean it is safe to fly between them. As installed on the DA 42 NG, the Garmin GWX 68 and the GWX 70 has a demonstrated range of 160 nautical miles, Refer to Garmin G1000 Pilot's Guide for the DA 42 NG, P/N 190-00962-( ) for Garmin G1000 or P/N 190-02237-( ) for G1000 NXi (MAM 42-978) or P/N 190-02526+( ) for G1000 NXi (MAM 42-1072) in the latest effective issue for further information. 5. IFOAM 42-257 (Garmin GTX 33 ES transponder) and MAM 42-828 (G1000 Software P/N 010-00670-12) are implemented, the installed ADS-B Out system is compliant to TSO-C166b / RTCA DO-206B. This constitutes no airworthiness approval. IFOAM 42-257 (Garmin GTX 33ES transponder) and MAM 42-1000 (G1000 Software P/N 010-00670-15) are implemented, the following functions are performed: - Transmission of ADS-B out data on 1090 extended squitter (1090 MHz) - Integration of data from internal and external sources to transmit the following data per 14 CFR 91.227: - GPS Position, Altitude, and Position Integrity - Ground Track and/or Heading, Ground Speed, and Velocity Integrity - Air Ground Status - Flight ID, Call Sign, ICAO Registration Number - Capability and Status Information - Transponder Squawk Codes between 0000-7777 - Emergency Status - IDENT - initiates SP! (special position identification) pulse for 18 seconds Page 1-22 Rev. § 10-Jun-2021 Doc. No. 7.01.16-E @p Diamond TRE SeDA 42 NG AFM AIRCRAFT Garmin GWX 75 Weather Radar 1.8 G1000 AVIONICS SYSTEM The Paragraph is amended to read: | 4. Ifthe Garmin GWX 68 or the GWX 70 / 75 weather radar system is installed, it can be used to aid the pilot in avoiding thunderstorms and associated turbulence or for 1 ground mapping, The GWX 68 and the GWX 70 / 75 shall be used to avoid severe weather and not for penetrating severe weather. Pulse type weather radar systems ® | like the GWX 68 and the GWX 70 / 75 detect precipitation only, not clouds or turbulence. The display may indicate clear areas between intense returns, but this does notnecessarily mean itis safe to fly between them. As installed on the DA 42 NG, | the Garmin GWX 68 and the GWX 70/75 has a demonstrated range of 160 nautical miles, Refer to Garmin G1000 Pilot's Guide for the DA 42 NG, P/N 190-00962-( ) for Garmin G1000or P/N 190-02237-() for G1000 NXi (MAM 42-978) or P/N 180-02526-( ) for G1000 NXi (MAM 42-1072) in the latest effective issue for further information. ® Doc #7.01.16-E | TR-OAM-42-370 11-Apr-2022 Page 1-224 DA 42 NG AFM ¥p Diamond General AIRCRAFT The Garmin GTX 33ES transponders for ADS-B meet the requirements in EASA AMC 20-24 for ADS-B (Automatic Dependent Surveillance-Broadcast) and ELS. 6. If a Garmin GTX 3X5R transponder for ADS-B (GTX 335R, GTX 345R) is installed the following functions are performed: - Transmission of ADS-B out data on 1090 extended squitter (1090 MHz) - Integration of data from internal and external sources to transmit the following data per 14 CFR 91.227: I 1 | I I I 1 | - GPS Position, Altitude, and Position Integrity | - Ground Track and/or Heading, Ground Speed, and Velocity Integrity 1 - Air Ground Status | - Flight ID, Call Sign, ICAO Registration Number | - Capability and Status Information | - Transponder Squawk Codes between 0000-7777 1 - Emergency Status | - IDENT - initiates SPI (special position identification) pulse for 18 seconds | I I I I | | | | The Garmin GTX 3X5R transponders for ADS-B meet the requirements in EASA AMC 20-24 for ADS-B (Automatic Dependent Surveillance-Broadcast) and ELS. 7. Referto Garmin G1000 Pilot's Guide for the DA 42 NG, P/N 190-00962-( } for Garmin G1000 or P/N 190-02237-( ) for G1000 NXi (MAM 42-978) or P/N 190-02526-( ) for G1000 NXi (MAM 42-1072) in the latest effective issue for further information. 8. The airplane has been assessed for back door coupling susceptibility in accordance with EUROCAE ED-239 Section 3 and found PED tolerant for back door coupling. The airplane has been assessed for front door coupling susceptibility in accordance with EUROCAE ED-130A Appendix A. No IPL determination was made. Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 1-23 General Diamond DA 42 NG AFM TION This section lists documents, manuals and other literature that were used as sources for the Airplane Flight Manual, and indicates the respective publisher. However, only the information given in the Airplane Flight Manual is valid. 1.9. INE Address: Austro Engine GmbH Rudolf Diesel-Str. 11 A-2700 Wiener Neustadt AUSTRIA Phone: +43-2622-23 000 Fax: +43-2622-23 000 - 2711 Internet: www.austroengine.at Documents: Operation Manual, E4.01.01, latest revision 1.9.2 PROPELLER Address: mt-propeller Airport Straubing Wallmiihle D-94348 Atting GERMANY Phone: +49-9429-9409-0 E-mail: sales@mt-propeller.com Website: www. .mt-propeller.de Documents: ~~ E-124, Operation and Installation Manual Hydraulically controlled variable pitch propeller MTV -5, -6, -9, -11, -12, 14, -15, -16, -21, -22, -25 Page 1-24 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E AIRCRAFT DA 42 NG AFM Diamond General 1.9.3 AVIONI EM Address: Garmin International, Inc. 1200 East 151 Street Olathe, Kansas 66062 USA Phone: +1-(913)-3978200 Fax: +1-(913)-3978282 Website: www .garmin.com Documents: ~~ G1000 Cockpit Reference Guide P/N 190-00963-( ), latest revision G1000 Pilot's Guide P/N 190-00962-( }, latest revision If MAM 42-978 is installed: G1000 NXi Cockpit Reference Guide P/N 190-02238-( ), latest revision G1000 NXi Pilot's Guide P/N 190-02237( ), latest revision If MAM 42-1072 is installed: G1000 NXi Cockpit Reference Guide P/N 180-02527( ), latest revision G1000 NXi Pilot's Guide P/N 190-02526-( ), latest revision Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 1-25 General DiamondAIRCRAFT DA 42 NG AFM Intentionally left blank. Page 1-26 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E DA 42 NG AFM Diamond Operating Limitations CHAPTER 2 OPERATING LIMITATIONS Page 24 INTRODUCTION iucisasssndiedsiaiaaaismisasnmas 2-3 22 AIREPEED wind evvienean Fe LR rr TE 2-4 2.3 AIRSPEED INDICATOR MARKINGS ......cvvininnninnnnnnn 2-5 24 POWER-PLANT LIMITATIONS ......... 00 0iitiiiineniannn 2-6 25 ENGINE INSTRUMENT MARKINGS .........cviivivnnnnnnn 2-12 2.6 WARNING, CAUTION AND ADVISORY ALERTS ............. 2-14 2.6.1 WARNING, CAUTION AND ADVISORY ALERTS ON THE GI000 tiie eee eae 2-14 2.6.2 OTHER WARNING ALERTS ........ciiviinnnnnnnnnn 2-18 ZT ASE DIVETGHT ccm arc sus swiss soins avs a ish sm dias dea swsc gan 2-19 28 CENTEROF GRAVITY ..vcuiviis sensor ss vim asiesasneis 2-21 29 APPROVED MANEUVERS wii imei asin sadam 2-23 2.10 MANEUVERING LOAD FACTORS ......0vvovvevrnnnnenrass 2-24 2.11 OPERATING ALTITUDE ..uviveiiwnisiesasssin sui nsii 2-25 22 FLIGHT GREW ovum e suas be aii ve aii 2-25 2.13 KINDS OF OPERATION .vvuiiw mimi iae ii vis eile wii 2-25 BH. PIER conn vein st ss oc at SR A 2-29 215 LIMITATIONPLACARDS ......coviiiininniennnseninninns 2-32 2.16 OTHERLIMITATIONS ....coiuveinnririnnsvnnsseninssass 2-38 216.1 FUELTEMPERATURE ......covvinivnnnnssnnsnsns 2-38 216.2 BATTERY CHARBE i. vvviviivi sen iindnis svn smness 2-38 2.16.3 EMERGENCY SWITCH .....0vvvrieninrinenieninnn 2-38 2.16.4 DOOR LOCKINGDEVICE .........c.cviiiennnnnnns 2-38 2.16.5 PORTABLE ELECTRONICDEVICES .........000uun 2-39 Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 RH Page 2-1 approved Operating Limitations Diamond DA 42 NG AFM 2.16.6 GARMIN G1000 AVIONICS SYSTEM ............... 2.40 2.16.7 AUTOPILOT LIMITATIONS 0. ovvvevnrsennienns 2-45 216.8 SMOKING «vee eee eee eee 2.47 2.16.9 GROUND OPERATION ©. o'er eee aera 2-47 2.16.10 USE OF THE SUN VISORS +. +o vveeeeennnnns 2-47 SE ET HRN 3 TH Se EA BRAS 2-47 Page 2-2 Rev. § 10-Jun-2021 EASA approved Doc. No. 7.01.16-E DA 42 NG AFM “Diamond Operating Limitations AIRCRAFT 2.1 INTRODUCTION Chapter 2 of this Airplane Flight Manual provides operating limitations, instrument markings and placards necessary for the safe operation of the airplane, its powerplants, standard systems and standard equipment. The limitations included in this Chapter are approved. WARNING Operation of the airplane outside of the approved operating limitations is not permissible. operation. NOTE Exceeding the operating limitations related to physical properties of the airplane (e.g. speeds, load factors, weights...) requires unscheduled maintenance priorto further Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 EASA approved Page 2-3 Operating Limitations ¥p Diamond DA 42 NG AFMAIRCRAFT 2.2 AIRSPEED Airspeed KIAS Remarks Vg Operating above 1800 kg 122 KIAS | Do not make full or maneuvering (3968 Ib) abrupt control surface movement above this speed above 1700 kg 119 KIAS | speed. (3748 |b) to 1800 kg (3968 Ib) up to 1700 kg 112 KIAS (3748 Ib) Vee Max. flaps LDG 113 KIAS | Do not exceed these extended speed speeds with the given APP 133 KIAS | flap setting. Vio | Max. landing Extension vy oe 188 KIAS | Do not operate the gear operating landing gear above this speed Retraction V, oq 152 KIAS | speed. Vie Max. landing gear extended speed 188 KIAS | Do not exceed this speed with the landing gear extended. Via | Minimum APP 68 KIAS | With one engine control speed inoperative, keep airborne uP 71 KIAS airspeed above this limit. Vo | Max. structural cruising speed 151 KIAS | Do not exceed this speed except in smooth air, and then only with caution. vue | Never exceed speed in smooth air 188 KIAS | Do not exceed this speed in any operation. EASA Page 2-4 Rev. 5 10-Jun-2021 Doc. No. 7.01,16-E approved DA 42 NG AFM ¥ Diamond Operating Limitations 2.3 AIRSPEED INDICATOR MARKINGS Marking KIAS Significance 62 - 113 KIAS If MAM 42-678 i White arc i i A Operating range with flaps fully extended. carried out: 64 - 113 KIAS 68 - 151 KIAS If MAM 42-678 is . Green arc 3 Normal operating range. carried out: 72-151 KIAS Yellow arc 151 - 188 KIAS ‘Caution’ range - "Only in smooth air". Blue radial 85 KIAS Best rate of climb speed, single engine. Red radial T1KIAS Minimum control speed, single engine. Red radial 188 KIAS Maximum speed for all operations - vy. EASA Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 2-5 approved Operating Limitations Diamond DA 42 NG AFMAIRCRAFT 2.4 POWER-PLANT LIMITATIONS a) Number of engines i 2 b) Engine manufacturer : Austro Engine c) Engine designation : E4-C d) RPM limitations {shown as propeller RPM) Maximum take-off (rpm) : 2300 RPM Maximum continuous (rpm) : 2300 RPM Maximum overspeed © 2500 RPM max. 20 sec e) Engine power Max. take-off power © 100% (123.5 kW) max. 5 min Max. continuous power to 92% (114 kW) f) Oil pressure (absolute) Minimum < 1500 RPM : 0.9 bar Minimum >= 1500 RPM : 2.5bar Maximum : 6.5bar Normal range : 2.5bar-6 bar g) Oil quantity Minimum : 5.01 Maximum FE 0 1 Maximum oil consumption © 0. liter/hr EASA Page 2-6 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E approved AIRCRAFT DA 42 NG AFM Diamond Operating Limitations h) Oil temperature Minimum : -30°C Maximum 140°C Normal range : 50°C-135°C Gearbox temperature Minimum : -30°C Minimum (full load) : 35°C Maximum © 120°C NOTE A cautionary (yellow) gearbox temperature range is not imposed by the engine manufacturer. However, there is a delay between power changes and gearbox temperature. Therefore, a cautionary range has been added to the G1000 gearbox temperature instrument solely to make the pilot attentive to the gearbox temperature approaching the maximum allowable limit. There is no specific time limit associated with operating in the cautionary gearbox temperature range. Coolant temperature Minimum (at start-up) : -30°C Minimum (full load) 1 60°C Maximum © 106°C EASA Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 approved Page2-7 Operating Limitations @ Diamond DA 42 NG AFMAIRCRAFT k) Fuel temperature Minimum Maximum I} Fuel pressure Minimum Maximum -30°C 60°C 4 bar 7 bar NOTE The fuel pressure is not indicated on the G1000; a fuel pressure warning will illuminate on the PFD if the pressure is below limit. m)Voltage Minimum Maximum n) Amperage Maximum 0) Propeller manufacturer p) Propeller designation q) Propeller diameter r) Prop. pitch angle (@ 0.75 R) 241V 32.0V TOA mi-Propeller MTV-6-R-C-F / CF 190-69 190 cm 13°+£0.2° (low pitch) 80° + 1° (feathered position) s) Governor mt-Propeller P-877-16 electrical governor with feather position EASA Page 2-8 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E approved DA 42 NG AFM Diamond Operating Limitations AIRCRAFT t) Oil specification SAE Grade 5W-30: SHELL HELIX ULTRA ADDINOL SUPER POWER MV 0537 BP VISCO 5000 REPSOL ELITE COMMON RAIL GULF FORMULA GMX AEROSHELL Oil Diesel Ultra CASTROL Edge 5W-30 A3 CASTROL Edge Professional A3 G-Energy F Synth TOTAL Quartz 9000 Energy SAE Grade 5W-40: SHELL HELIX ULTRA LIQUI MOLY LEICHTLAUF HIGH TECH MEGOL MOTORENOEL HIGH CONDITION PETRONAS Syntium 3000 LUKOIL LUXE SYNTHETIC CASTROL Edge Professional A3 CASTROL Magnatec Professional A3 VALVOLINE SynPower HST VALVOLINE SynPower GULF Formula GX AUSTRO ENGINE Aero produced by Liqui Moly recommended by Austro Engine GmbH SAE Grade OW-40: CASTROL SLX PROFESSIONAL LONGTEC CASTROL Edge 0W-40 A3/B4 CASTROL Edge Professional A3 SHELL Helix Ultra Doc. No. 7.01.16-E Rev. 5 EASA 10-Jun-2021 Page 2-8 approved Operating Limitations Diamond DA 42 NG AFMAIRCRAFT CAUTION Only engine oils conforming to MB 229.5 specification are approved by Austro Engine GmbH to be used for operation. Use only one type of approved E4 engine oil for an il change. NOTE It is not recommended to mix different SAE grades. u) Gearbox oil (propeller gearbox) : SHELL SPIRAX GSX 75W-80 SHELL SPIRAX S6 GXME 75W-80 v) Coolant : Distilled water / cooler protection (BASF Glysantin Protect Plus / G48) 1/1. The freezing point of the coolant is - 38°C. CAUTION If the coolant or gearbox oil level is low the reason must be determined and the problem must be corrected by authorized personnel. EASA Page 2 - 10 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E approved rN - DA 42 NG AFM Diamond Operating LimitationsAIRCRAFT w) Maximum restart altitude 1 18,000 ft pressure altitude for immediate restarts 10,000 ft pressure altitude for restarts within two minutes If MAM 42-938 (engine software VC33_2 05_19 or later approved 7 software) is installed © 15,000 ft pressure altitude for immediate restarts Up to 10,000 ft pressure altitude: OAT Max. engine OFF time re [Fl [minutes] below -15 | below 5 2 -15t0-5 510 23 5 above -5 | above 23 10 x) Restart airspeed (starter) © max. 100 KIAS or airspeed for a stationary propeller, whichever is lower ~~ Restart airspeed (windmilling) © 125 KIAS to 145 KIAS y) No intentional shutdown below 3,000 ft AGL and above 10,000 ft pressure altitude. EASA Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 2-11 approved Operating Limitations Diamond DA 42 NG AFM 2.5 ENGINE INSTRU KINGS Engine instrument markings and their color code significance are shown in the tables below. Indi- Red Yellow Green Yellow Red cation arc/bar arc/bar arc/bar arc/bar arc/bar = = = = = ; lower caution normal caution upper prohibited range operating range prohibited range range range RPM BN i» up to . above 2300 RPM 2300 RPM Oil pressure below 0.9 bar | 0.9 to 2.5 bar | 2.5 to 6.0 bar | 6.0 to 6.5 bar |above 6.5 bar Qil 135° to below -30°C | -30° to 135°C bove 140°C temp. low -30°C | -30° to 50°C | 50° to 13 140°C above orig below -30°C | -30° 10 60°C | 60° to 95°C | 95° to 105°C | above 105°C 115° to Gearbox | ow 30°C | -30° to 36°C | 35° 10 115°C S| hove 120°C temp. 120°C Load - -- up to 92% 92 - 100% - Fuel “9, °C |-30° to -20°C | -20° to 55°C | 55° 10 60°C | above 60°C temp. elow -30 -30° to - -20% to to ahove 6 Fuel *% " - - , oc | ab o temp. below -30°C - -30° to 55°C | 55° to 60’ above 60°C Ammeter - - up to 60A 60 to 70A above 70A sl below 24.1V | 24.11025V | 25t030V | 301032V | above 32v EASA Page 2 - 12 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E approved Diamond DA 42 NG AFM Operating Limitations AIRCRAFT Indi- Red Yellow Green Yellow Red cation arc/bar arc/bar arc/bar arc/bar arc/bar = = = = = lower caution normal caution upper prohibited range operating range prohibited range range range Fuel qty. below 1to 25 1 US gal US gal 1 |f G1000 system software prior to P/N 010-00670-12 is installed. *2) |f G1000 system software P/N 010-00670-12 or later is installed. EASA Doc. No. 7.01.16-E Rev. § 10-Jun-2021 Page 2 - 13 approved Operating Limitations Diamond DA 42 NG AFMAIRCRAFT 2.6 WARNING, CAUTION AND ADVISORY ALERTS 2.6.1 WARNING, CAUTION AND ADVISORY ALERTS ON THE G1000 NOTE The alerts described in the following are displayed on the Garmin G1000. Section 7.10 includes a detailed description of the alerts. The following tables show the color and significance of the warning, caution and advisory alerts lights on the G1000. Color and Significance of the Warning Alerts on the G1000 Yarming sects Meaning / Cause (red) WARNING One of the warnings listed below is being indicated. Left / Right engine coolant temperature is in the upper red L/RENG TEMP range (too high / =105 °C). Left / Right engine oil temperature is in the upper red range LROILTEMP | 400 high / >140 °C). L/R OIL PRES Left / Right engine oil pressure is in the lower red range (too low / <0.9 bar). L/R FUEL TEMP Left / Right fuel temperature is in the upper red range (too high / =60 °C). L/R GBOX TEMP | Left / Right engine gearbox temperature is in the upper red range (too high / >120 °C). L/R FUEL PRESS | Left/Right engine fuel pressure is low. EASA Page 2-14 Rev, 5 10-Jun-2021 Doc. No. 7.01.16-E approved Diamond o.caing Limitations DA 42 NG AFM phobic Amig Mers Meaning / Cause (red) L/R ALTN AMPS | Left / Right engine alternator output is in the upper red range (too high / >70 Amps). L/R ENG FIRE Left / Right engine fire detected. L/R STARTER Left / Right engine starter is engaged. DOOR OPEN Front and/or rear canopy and/or baggage door arefis not closed and locked. ATTITUDE FAIL The display system is not receiving attitude reference information from the AHRS. AIRSPEED FAIL The display system is not receiving airspeed input from the air data computer. ALTITUDE FAIL The display system is not receiving altitude input from the air data computer. VERT SPEED The display system is not receiving vertical speed input fram FAIL the air data computer. HDG The display system is not receiving valid heading input from the AHRS. WARN RAIM position warning. The nav deviation bar is removed. Red X or yellow X A red or yellow (if Garmin G1000 NXi is installed) X through any display field, such as com frequencies, nav frequencies, or engine data, indicates that the display field is not receiving valid data. Doc. No. 7.01.16-E EASA Rev. 5 10-Jun-2021 Page 2-15 approved Operating Limitations Diamond AIRCRAFT DA 42 NG AFM Color and Significance of the Caution Alerts on the G1000 Caution alerts Meaning / Cause (amber) A fault has occurred in the left/right engine ECU A (one reset of minor faults is possible) L/R ECU A FAIL or ECU A is being tested during FADEC-test procedure during the ‘Before Take-Off Check’. A fault has occurred in the left/right engine ECU B (one reset of minor faults is possible) L/R ECU B FAIL or ECU B is being tested during FADEC-test procedure during the 'Before Take-Off Check’. L/R FUEL LOW Left / Right main tank fuel quantity is low. L/R ALTN FAIL Left / Right engine alternator has failed. L/R VOLTS LOW Left / Right engine bus voltage is too low (< 25 Volts). L/R COOL LVL Left / Right engine coolant level is low. PITOT FAIL Pitot heat has failed. PITOT HT OFF Pitot heat is OFF. STAL HT FAIL Stall warning heat has failed. STAL HT OFF Stall warning heat is OFF. STICK LIMIT Control stick limiting system (variable elevator stop) has failed. LOI GPS integrity is insufficient for the current phase of flight. AHRS ALIGN: The AHRS (Attitude and Heading Reference System) is Keep Wings Level | aligning, L/R AUX FUEL E Left / Right auxiliary fuel tank empty (if installed). EASA Page 2-16 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E approved Operating Limitations DA 42 NG AFM Diamond AIRCRAFT Caution alerts Meaning / Cause (amber) CHECK GEAR Landing gear is not down and locked. DEICE LVL LO De-icing fluid level is low (if installed). DEIC PRES HI De-icing pressure is high (if installed). DEIC PRES LO De-icing pressure is low (if installed). lor ignifi f th Advisory alerts Meaning / Cause (white) L/R GLOW ON Left / Right engine glow plug active. L/R AUXPUMP Fuel transfer from auxiliary to main tank is in progress ON (if installed). PFD FAN FAIL Cooling fan for the PFD is inoperative. MFD FAN FAIL Cooling fan for the MFD is inoperative. GIA FAN FAIL Cooling fan for the GlAs is inoperative. EASA Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 2-17 approved Operating Limitations Diamond DA 42 NG AFMAIRCRAFT 2.6.2 OTHER WA ALERT Warning Alerts on the Instrument Panel Warning alert (red) Meaning / Cause GEAR UNSAFE WARNING LIGHT lNluminates if the landing gear is neither in the final up nor in the down & locked position. Audible Warning Alerts Audible warning Meaning / Cause alert GEAR R dsi ; ; i ql RETRACTED Resounds if the landing gear is retracted while the aps move CHIME TONE into position LDG or when the power lever is placed in a : position below approx. 20 %. (repeating) EASA Page 2-18 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E approved DA 42 NG AFM @ Diamond AIRCRAFT Operating Limitations 2.7 MASS (WEIGHT Value Mass (Weight) Minimum flight mass 1450 kg 3197 Ib Maximum take-off mass 1900 kg 4189 Ib Maximum take-off mass (if MAM 42-678 is carried out) 1999 kg 4407 Ib Maximum zero fuel mass 1765 kg 3891 Ib Maximum zero fuel mass (if MAM 42-659 is carried out) 1835 kg 4045 Ib Maximum landing mass 1805 kg 3979 Ib Maximum landing mass (if MAM 42-659 is carried out) 1999 kg 4407 Ib Max. load in nose baggage compartment 30 kg 66 Ib (in fuselage nose) Max. load in cabin baggage compartment 45 kg 100 Ib (behind rear seats) Max. load in baggage extension 18 kg 40 1b (behind cabin baggage compartment) Max. load, cabin baggage compartment and baggage 45 kg 100 Ib extension together if OAM 42-207 is carried out: Max. load in standard baggage compartment 30 kg 66 Ib (between rear seats and baggage bulkhead) Max. load in short baggage extension 15 kg 33 1b WARNING Exceeding the mass limits will lead to overstressing of the airplane as well as to degradation of flight characteristics and flight performance. Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 EASA approved Page 2-19 Operating Limitations @ DiamondAIRCRAFT DA 42 NG AFM be exceeded. NOTE In some countries the beginning of a flight is defined by starting the powerplant. In those countries a ramp mass of maximal MTOM + 8 kg (MTOM + 18 Ib) is approved. At the time of lift-off the maximum permitted take-off mass must not Page 2 - 20 Rev. 5 10-Jun-2021 EASA approved Doc. No. 7.01.16-E DA 42 NG AFM Diamond Operating Limitations 28 CENTER VITY Datum Plane The datum plane (DP) is a plane which is normal to the airplane’s longitudinal axis and in front of the airplane as seen from the direction of flight. The airplane’s longitudinal axis is parallel with the floor of the nose baggage compartment. When the floor of the nose Fat baggage compartmentis aligned horizontally, the datum planeis vertical. The datum plane is located 2.196 meters (86.46 in) forward of the most forward point of the root rib on the stub wing (refer to figure in Section 6.2). Center of Gravity Limitations The center of gravity (CG position) for flight conditions must be between the following limits: Most forward flight CG: 2.350 m (92.52 in) aft of datum plane at 1450 kg (3197 Ib) 2.350 m (92.52 in) aft of datum plane at 1468 kg (3236 Ib) 2.418 m (95.20 in) aft of datum plane at max. take-off mass 1900 kg (4189 Ib) If MAM 42-678 is carried out: 2.434 m (95.83 in) aft of datum plane at max. take-off mass 1999 kg (4407 Ib) linear variation in between Pan } Most rearward flight CG: 2.454 m (96.61 in) aft of datum plane at 1450 kg (3197 Ib) 2.480 m (97.64 in) aft of datum plane at 1700 kg (3748 Ib) 2.480 m (97.64 in) aft of datum plane at max, take-off mass (see Section 2.7) linear variation in between Refer to Section 6.4.4 for a graphical illustration of the CG limitations. ff \ EASA Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 2 - 21 approved Operating Limitations Diamond DA 42 NG AFM AIRCRAFT WARNING Exceeding the center of gravity limitations reduces the controllability and stability of the airplane. Page 2 - 22 EASA Rev. § 10-Jun-2021 Doc. No. 7.01.16-E approved “’ DA 42 NG AFM Diamond Operating LimitationsAIRCRAFT 2. PPROVED MANEUVERS The airplane is certified in the Normal Category in accordance with JAR-23. Approved Maneuvers 1) All normal flight maneuvers; 2) Stalling (with the exception of dynamic stalling); and 3) Lazy Eights, Chandelles, as well as steep turns and similar maneuvers, in which an angle of bank of not more than 60° is attained. CAUTION Aerobatics, spinning and flight maneuvers with more than 60° of bank are not permitted in the Normal Category. Stalling with asymmetric power or one engine inoperative is not permitted. CAUTION Intentional negative g - maneuvers are not permitted. EASA Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 2-23 approved Operating Limitations Diamond DA 42 NG AFM 2.10 EUVERING LOAD FACTO NOTE The tables below show structural limitations. The load factor limits for the engine must also be observed. Refer to the corresponding Operation Manual for the engine. atvy at vye with flaps in APP or LDG position Positive 38 3.8 2.0 Negative -1.52 -1.52 0.0 WARNING Exceeding the maximum structural load factors will lead to overstressing of the airplane. CAUTION Intentional negative g- maneuvers are not permitted. EASA Page 2 - 24 Rev, 5 10-Jun-2021 Doc. No. 7.01.16-E approved DA 42 NG AFM ¥p Diamond Operating LimitationsAIRCRAFT .11 OPERATING ALTITUDE The maximum operating altitude is 18,000 ft (5,486 m) pressure altitude. 2.12 FLIGHT CREW Minimum crew : 1 (one person) Maximum number of occupants: 4 (four persons) 2.13 KINDS OF OPERATION Provided that national operational requirements are met, the following kinds of operation are approved: + daytime flights according to Visual Flight Rules (VFR) + with the appropriate equipment: night flights according to Visual Flight Rules (NVFR) + with the appropriate equipment: flights according to Instrument Flight Rules (IFR) + take-off and landing on paved surfaces + take-off and landing on grass surfaces Flights into known or forecast thunderstorms are prohibited. Minimum Operational Equipment (Serviceable The following table lists the minimum serviceable equipment required by JAR-23. Additional minimum equipment for the intended operation may be required by national operating rules and also depends on the route to be flown. EASA Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 2 - 25 approved Operating Limitations Diamond DA 42 NG AFM NOTE Many of the items of minimum equipment listed in the following table are integrated in the G1000. for daytime in addition for in addition for VFR flights night VFR flights IFR flights Flight & * airspeed indicator | * vertical speed * second airspeed navigation (on G1000 PFD or indicator (VSI) indicator (both, on instruments backup) * attitude gyro his Fro and * altimeter(on G1000 | (artificial horizon; on P PFD or backup) G1000 PFD or * second altimeter “ backu| both, on G1000 Mmagnsiic.compass $ oy and backup) * 1 headset, used by | 1 & bank ilot i H hid y indicator (on G1000 |* second attitude pret: CommaY PFD) gyro (both, on * direci G1000 PFD and irectional gyro backup) * VHF radio (COM) |. with speaker and ry VHF adi microphone * VOR receiver hoa * transponder i second GPS rsd he A receiver (part of G1000) * GPS receiver (part of G1000) EASA Page 2 - 26 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E approved DA 42 NG AFM ¥ Diamond Operating Limitations AIRCRAFT for daytime in addition for in addition for VFR flights night VFR flights IFR flights Engine * fuel qty. (2x) * ammeter INSTOMENG: |» oil press. (2x) * voltmeter * oil temp. (2x) * coolant temp. (2x) * coolant level indicator (2x) * gearbox temp. (2x) * load (2x) * prop. RPM (2x) * fuel temp. left & right tank * fuel flow (2x) * fuel px warning Lighting * position lights * strobe lights (anti collision lights) * landing light * instrument lighting * flood light * flashlight Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 EASA Page 2 - 27 approved stop * alternate means for fuel quantity indication (see Section 7.9) * safety belts for each occupied seat * Airplane Flight Manual valve Operating Limitations “¥»D mond DA 42 NG AFMAIRCRAFT for daytime in addition for in addition for VFR flights night VFR flights IFR flights Other * stall warning * Pitot heating * emergency battery operational system system (for backup attitude minimum aid x ? gyro and flood light) equipment variable elevator alternate static NOTE A list of approved equipment can be found in Chapter 6. Engine Systems and Equipment All engine systems and equipment must be functional prior to airplane take-off. Any engine system or equipment failure must be corrected before next flight. Page 2-28 Rev. § EASA approved 10-Jun-2021 Doc. No. 7.01.16-E DA 42 NG AFM ¥p Diamond Operating Limitations AIRCRAFT 2.14 FUEL Approved fuel grades: JET A, JET A-1 (ASTM D 1655) TS-1 (Russia, GOST 10227-86) TS-1 (Ukraine, GSTU 320.00149943.011-99) RT (Russia, GOST 10227-86) RT (Ukraine GSTU 320.00149943.007-97) f No. 3 Jet Fuel (China, GB 6537-2006) JP-8 (F34) (USA, MIL-DTL-83133G-2010) and blends of the above listed fuel grades. NOTE A minimum cetane number of 36 determined acc. to EN ISO 5165/ASTM D613 is recommended. NOTE Use only uncontaminated fuel from reliable sources. Auxiliary Tanks Main Tanks (if installed) Total \ USgal | liters | USgal | liters | US gal liters Total fuel quantity | 2x 26.0 | 2x98.4 | 2x 13.7 | 2x 52.0 | 2x 39.7 | 2x 150.4 Usable fuel 2%x250 [2x946 |2x13.2 | 2x50.0 | 2x38.2 | 2x 144.6 Max. permissible difference LHRH | >0 15:0 f EASA Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 2-29 approved Operating Limitations Diamond AIRCRAFT DA 42 NG AFM Any mixture of the different types of fuel additives is not permitted. PERATION WITH ANTI-MICROBIAL LIFE FUEL ADDITIVE The application of the following additives is permitted: - KATHON FP 1.5 - BIOBOR JF max. 100 ppm CAUTION max. 270 ppm for initial treatment max. 135 ppm for permanent use after initial treatment In case of an unknown or an over dosage of the fuel additives the fuel system must be purged until the dosage is within the permitted limits. NOTE The specified additives are qualified for the operation with the certified fuel grades. To clean the fuel system of the airplane a higher dosage of the specified additive is allowed under consideration of the instructions of the additive supplier. During cleaning the engine must not be operated. NOTE The instructionsof the fuel additive supplier must be followed. Page 2 - 30 Rev. 5 10-Jun-2021 EASA approved Doc. No. 7.01.16-E DA 42 NG AFM Diamond Operating AIRCRAFT Limitations OPERATION WITH ANTI-ICING FUEL ADDITIVES The application of the following additive is permitted: - PRIST Hi-Flash © max. 1500 ppm CAUTION The use of PRIST Hi-Flash fuel additive is only permitted with JET A, JET A-1 (ASTM D 1655) and JP-8 (F34). NOTE The instructions of the fuel additive supplier must be followed. EASA Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 approved Page 2-31 Operating Limitations Diamond DA 42 NG AFMAIRCRAFT 215 L ARD All limitation placards are shown below. A list of all placards is included in the Airplane Maintenance Manual (Doc. No. 7.02.15), Chapter 11. Limitations for GFC 700 Autopilot System: Autopilot / Yaw Damper DISC during take-off and landing. Do not use AP during single engine operation. Maximum speed for autopilot operation is 180 KIAS. Minimum speed for autopilot operation is 90 KIAS. Minimum Altitude for Autopilot Operation: Cruise, Climb, Descent and Maneuvering : 800 feet AGL Approach : 200 feet AGL Departure : 200 feet AGL This airplane may only be operated in accordance with the Airplane Flight Manual in the "Normal" category. Provided that national operational requirements are met and the appropriate equipment is Installed and operational, this airplane is approved for the following kinds of operation; day VFR, night VFR, IFR and flight into known or forecast icing conditions. All aerobatic maneuvers including spinning are prohibited. For further operational limitations refer lo the Airplane Flight Manual. Operaling maneuvering speed vo = 122 KIAS (above 1800 kg / 3968 Ib) Vo = 119 KIAS (above 1700 kg / 3748 Ib to 1800 kg / 3968 Ib) vo = 112 KIAS (up to 1700 kg / 3748 1b ) EASA Page 2 - 32 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E approved DA 42 NG AFM DiamondAIRCRAFT Operating Limitations LANDING GEAR Vie I Vor = 188 KIAS Vion = 152 KIAS If OAM 42-179 is not incorporated: © GPS NOT APPROVED FOR WAAS OPERATIONS 1 | EMERGENCY Gear Extension Max. 152 KIAS On the Emergency Landing Gear Extension Lever: On the Instrument Panel: Standard Tank: Auxiliary Tank (if installed): max. usable fuel: 2 x 25 US gal max. difference LH/RH tank: 5 US gal max. usable fuel main tank: 2x25US gal auxiliary tank: 2x13 US gal max. difference LH/IRH malin tank: 5 US gal Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 EASA approved Page 2 - 33 Operating Limitations “Diamond DA 42 NG AFM AIRCRAFT (a) Next to Each of the Two Fuel Filler Necks: (b) In Addition Next to Each of the Two Auxiliary Fuel Filler Necks (if installed): WARNING APPROVED FUEL JET-A1 or see Airplane Flight Manual h Cowling, on the Door for the Oil Filler Neck: OIL OIL AUSTRO ENGINE SHELL HELIX Aero ULTRA 5W-40 OR 5W30 or see Airplane of see Airplane Flight Menual Flight Manual EASA Page 2 - 34 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E approved DA 42 NG AFM Diamond Operating Limitations Next to the Flap Selector Switch: Flaps BL APP O 133 KIAS LDG O 113 KiAS Next to the Cabin B mpartment: CABIN BAGGAGE BAGGAGE COMPARTMENT EXTENSION MAX. 45 kg [100 Ib] ARM: 3,89 m [153.1"] MAX. 18 kg [40 Ib] ARM: 4.54 m [178.7"] MAX, BAGGAGE TOTAL (CABIN BAGGAGE COMPARTMENT & EXTENSION) 45 kg [100 Ib] CAUTION: OBSERVE WEIGHT AND BALANCE LIMITATIONS SEE AIRPLANE FLIGHT MANUAL CHAPTER 6 EASA Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 2 - 35 approved - ing Limitati Diamond Operating Limitations 9» CHART DA 42 NG AFM If OAM 42-207 is carried out: ARM: 3.65 m [143.7 in] STANDARD BAGGAGE — SHORT BAGGAGE COMPARTMENT EXTENSION MAX 30 kg [68 Ib) MAX 15 kg (33 Ib] ARM; 3.97 m [156.3 in] CAUTION: OBSERVE WEIGHT AND BALANCE LIMITATIONS SEE AIRPLANE FLIGHT MANUAL CHAPTER 6 In thi in, on i li: Alternate Static OPEN CLOSED If Alternate Static Is open Emergency Window and Cockpit Vent must be closed EASA Page 2 - 36 Rev. 5 10-Jun-2021 approved Doc. No. 7.01.16-E DA 42 NG AFM DiamondAIRCRAFT Operating Limitations In the Nose Bagga artment: Max. Baggage: 30 kg [66 Ib] ide the Door Locking Device Installed in the Passengers’ Door: EMERGENCY EXIT: The keylock must be unlocked during flight On the Right-Hand Side of the Instrument Panel Above the Circuit Breakers: —— NO SMOKING — Doc. No, 7.01.16-E Rev. 5 10-Jun-2021 EASA approved Page 2 - 37 Operating Limitations ‘¥#p Diamond DA 42 NG AFMAIRCRAFT 2.16 OTHER LIMITATIONS 2.16.1 FUEL TEMPERATURE From -30 °C to 60 °C (from -22 °F to 140 °F). 2.16.2 BATTERY CHARGE Taking off for a Night VFR or IFR flight with an empty battery is not permitted. The use of an external power supply for engine starting with an empty airplane battery is also not permitted if the subsequent flight is intended fo be a Night VFR or IFR flight. In this case the airplane battery must first be charged. 2.16.3 EMERGENCY SWITCH IFR flights are not permitted when the seal on the emergency switch is broken. 2.16.4 D DEVICE The canopy and the passenger door must not be blocked by the key lock during operation of the airplane. EASA Page 2 - 38 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E approved DA 42 NG AFM Diamond Operating Limitations AIRCRAFT B L| ONIC DEVICE! | The useof Portable Electronic Devices (PED) during low visibility approaches is prohibited. NOTE Refer to EASA AMC 20-25 or FAA AC 120.76A for the use of PED associated to electronic flight bag (EFB) operation. The use of any device as an EFB may require separate approvals. EASA Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 2 - 39 approved Operating Limitations @ Diamond DA 42 NG AFMAIRCRAFT 2.16.6 GARMIN G1000 AVIONICS SYSTEM 1. The Garmin G1000 Cockpit Reference Guide, P/N 190-00863-( ) or Garmin G1000 NXi (MAM 42-978) Cockpit Reference Guide, P/N 190-02238-( ) or Garmin G1000 NXi (MAM 42-1072) Cockpit Reference Guide, P/N 190-02527-( ), appropriate revision must be immediately available to the flight crew. 2. The G1000 must utilize the software Garmin 010-00670-( ), the Garmin G1000 NXi must utilize the software Garmin 010-01916-( ), approved software in accordance with the mandatory service bulletin DAI MSB 42-003, latest approved version. Software Part Number Approved Function Version System (G1000) 010-00670-( ) System (G1000 NXi) - 010-01916-() 8 Manifest £ 006-B0093-( ) g GPS1, GPS2 006-B0172-( ) a GTX1-GIA1, GTX1-GIA2 006-B0190-( ) = GIA1, GIAZ 006-B0193-( ) 2 GEA1-GIA1; GEA1-GIAZ 006-B0203-( ) © GMA1-GIA1, GMA1-GAI2 006-B0223-( ) 8 GRS1-GIA1, GRS1-GIA2 006-B0224-( ) B GMUA1 006-B0319-( ) 2 PFD1, MFD1 006-B0328-( ) B t= 006-B0329-( ) 5 5 006-C0048-( ) a = GMU1 FPGA 006-C0049-( ) 5 3 GRS1 FPGA 006-C0055-( ) GDC1 FPGA 006-D0159-( ) GRS1 MV DB 006-D0202-( ) EASA Page 2 - 40 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E approved DA 42 NG AFM Diamond Operating LimitationsAIRCRAFT Software Part Number Approved Function Version 006-80261-( ) GDC1-GIA1 006-80081-( ) COM1, COM? 006-B0083-( ) GS1, GS2 006-B0082-( ) NAV1, NAV2 NOTE The database version is displayed on the MFD power-up page immediately after system power-up and must be acknowledged. The remaining system software versions can be verified on the AUX group sub-page 5, "AUX-SYSTEM STATUS". 3. IFR enroute, oceanic and terminal navigation predicated upon the G1000 GPS Receiver is prohibited unless the pilot verifies the currency of the database or verifies each selected way point for accuracy by reference to current approved data. 4. Instrument approach navigation predicated upon the G1000 GPS Receiver must be accomplished in accordance with approved instrument approach procedures that are retrieved from the GPS equipment database. The GPS equipment database must incorporate the current update cycle. NOTE Not all published approaches are in the FMS database. The pilot must ensure that the planned approach is in the database. (a) Instrument approaches utilizing the GPS receiver must be conducted in the approach mode and Receiver Autonomous Integrity Monitoring (RAIM) must be available at the Final Approach Fix. EASA Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 2 - 41 approved Operating Limitations “Diamond DA 42 NG AFMAIRCRAFT (b) () (d) (e) (9 Accomplishment of ILS, LOC, LOC-BC, LDA, SDF, MLS or any other type of approach not approved for GPS overlay with the G1000 GPS receiver is not authorized. Use of the G1000 VOR/ILS receiver to fly approaches not approved for GPS require VORJ/ILS navigation data to be present on the display. When an alternate airport is required by the applicable operating rules, it must be served by an approach based on other than GPS or Loran-C navigation, the airplane must have the operational equipment capable of using that navigation aid, and the required navigation aid must be operational. NAV information may be utilized for advisory information only. Use of VNAV information for Instrument Approach Procedures does not guarantee step-down fix altitude protection, or arrival at approach minimums in normal position to land. RNAV (GPS) approaches must be conducted utilizing the GPS sensor. RNP RNAV operations are not authorized, except as noted in Chapter 1 of this AFM. EA Page 2 - 42 Rev. § 10-Jun-2021 Doc. No. 7.01.16-E SA approved DA 42 NG AFM Diamond Operating Limitations AIRCRAFT 5. Ifnot previously defined, the following default settings must be madein the "SYSTEM SETUP" menu of the G1000 prior to operation (refer to Pilot's Guide for procedure if necessary): (a) DIS, SPD :nm, kt (sets navigation unitsto "nautical miles” and "knots") (b) ALT, VS ft, fpm (sets altitude units to "feet" and "feet per minute") (¢) POSITION : deg-min (sets navigation grid units to decimal minutes) NOTE Navigation Information is referenced to WGS-84 reference system, and should only be used where the Aeronautical Information Publication (including electronic data and aeronautical charts) conforms to WGS-84 or equivalent. 6. When AHRS is required to meet the items listed in the minimum operational equipment (serviceable) table in Section 2.13 of this AFM, operation is prohibited in the following areas! (a North of 72° N latitude at all longitudes. South of 70° S latitude at all longitudes. North of 65” N latitude between longitude 75° W and 120° W (Northern Canada). North of 70° N latitude between longitude 70° Wand 128° W (Northern Canada). North of 70° N latitude between longitude 85° E and 114° E (Northern Russia). South of 55° § latitude between longitude 120° E and 165° E (Region south of Australia and New Zealand). When day VFR operations are conducted in the above areas, the MFD must be in a non-heading up orientation. Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 2-43 EASA approved Operating Limitations Diamond DA 42 NG AFM 7. The fuel quantity, fuel required, and fuel remaining functions of the FMS are supplemental information only and must be verified by the flight crew. 8. The GPS is not approved for WAAS operations: (a) The G1000 integrated avionics system is NOT approved for GPS WAAS operations including GPS WAAS approach procedures such as "LPV", "LNAV/VNAV", and "LNAV +V", (b) SBAS (WAAS & MSAS) functionality must be disabled on the G 1000 GPS Status page (refer to the G1000 Pilot's Guide for procedure). 9. The availability of SafeTaxi®, ChartView, or FliteCharts® in electronic form on the G1000 is for information purposes only, itis still mandatory to carry another source of charts on-board the airplane. EASA Page 2 - 44 Rev, 5 10-Jun-2021 Doc. No. 7.01.16-E approved Fa DA 42 NG AFM Diamond Operating Limitations AIRCRAFT 16.7 AUTOPILOT LIMITATION 1. Itis the responsibility of the pilot in command to monitor the autopilot when it is engaged. The pilot should be prepared to immediately disconnect the autopilot and to take prompt corrective action in the event of unexpected or unusual autopilot behavior. 2. The autopilot and yaw damper must be disconnected (using the DISC button) during take-off, landing and single engine operation. 3. Following an autopilot or electric trim malfunction, reengaging the autopilot or manual electric trim, or resetting the AFCS / ESP / USP circuit breaker is prohibited until the cause of the malfunction has been determined and corrected. 4. The Garmin G1000 Cockpit Reference Guide for the Diamond DA 42 NG, P/N 010-00963-( ) or Garmin G1000 NXi (MAM 42-978) Cockpit Reference Guide for the Diamond DA 42 NG, P/N 010-02238-( ) or Garmin G1000 NXi (MAM 42-1072) Cockpit Reference Guide for the Diamond DA 42 NG, P/N 010-02527-( ) approved revision must be immediately available to the flight crew. 5. ILS approaches using the GFC700/ flight director are limited to Category | approaches only. 6. Autopilot maximum airspeed: 180 KIAS Autopilot minimum airspeed: 90 KIAS 7. Altitude select captures below 1200 feet AGL are prohibited. 8. The autopilot must be disengaged: - below 200 ft AGL during approach, - below 200 ft AGL during departure, - below 800 ft AGL for all other phases of flight, - during single engine operation. 9. Overriding the autopilot to change pitch or roll attitude is prohibited. (Disengage or EASA Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 2 - 45 approved Operating Limitations DiamondAIRCRAFT DA 42 NG AFM press CWS while maneuvering.) 10. The GFC 700 components must utilize the following or later approved software versions: Sub-System Software Version GDhuU v9.03 GDC 74 v3.02 GEA 7X v2.07 GPS v3.03 GIA 6X v5.65 GIA Audio v2.03 GMAX347 v4.01 GMU44 v2,01 GRS 77 v2.11 GTX 33X v5.01 GDL 69 v3.20.00 GSA 8X v2.20 GFC 700 v2.00 The system software versions can be verified on the AUX group sub-page 5, "AUX - SYSTEM STATUS". 11. The GFC 700 AFCS pre-flight test must be successfully completed prior to use of the autopilot, flight director, yaw damper or manual electric trim. 12. Apilotwith the seat belt fastened must occupy the left pilot's seat during all operations. 13. The yaw damper is an integral part of the autopilot system and must not be used separately. Page 2 - 46 Rev. 5 10-Jun-2021 EASA approved Doc. No. 7.01.16-E Ad Temporary Revision Garmin GWX 75 Weather Radar 2.16 OTHER LIMITAT! The Paragraph is amended to read: | 2.16.11 GARMIN GWX 68 / GWX 70 / 75 WEATHER RADAR OPERATION WARNING The Garmin GWX 68 and the GWX 70 / 75 Weather Radar System (if installed) must not be operated on ground. If the system is transmitting, it may result in bodily injury if persons are within the minimum safe distance of 3.7 m (12 ft). Never operate the radar in a hangar or other enclosure as radiation can be reflected throughout the area. Doc. #7.01.16-E | TR-OAM-42-370 | 11-Apr-2022 approved A EAS Page 2-47a DA 42 NG AFM Diamond Operating LimitationsAIRCRAFT 2.16.8 SMOKING Smoking in the airplane is not permitted. 2.16.9 GROUND OPERATION Take-off and landing has been demonstrated on hard paved surfaces (asphalt, concrete, etc.) and grass runways. 2.16.10 USE OF THE SUN V| The sun visors (ifinstalled, OAM 42-101 or OAM 42-142) may only be used during cruise. During all other phases of flight the sun visors must be locked in the fully upward position. 2.16.11 GA 70 WEATHER RAD. P T WARNING The Garmin GWX 68 and the GWX 70 weather radar system (if installed) must not be operated on ground. If the system is transmitting, it may result in bodily injury If persons are within the minimum safe distance of 2.8 m (9.16 ft) for the GWX 68. For the GWX 70 the minimum safe distanceis 2.3m (7.4 ft). Never operate the radar in a hangar or other enclosure as radiation can be reflected throughoutthe area. 12 MID CONTINEN BY ATTITUDE MODULE The Mid Continent MD302 Standby Attitude Module Pilot's Guide, P/N 9017846, latest effective issue must be immediately available to the flight crew. EASA Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 2 - 47 approved Operating Limitations Diamond DA 42 NG AFM Intentionally left blank. Page 2 - 48 Rev. 5 10-Jun-2021 EASA approved Doc. No. 7.01.16-E DA 42 NG AFM ¥p Diamond SORA AIRCRAFT Procedures CHAPTER 3 EMERGENCY PROCEDURES Page 31 NFRGDUCTION = coovuis esis dbsisisrs bdandays sv 3-4 BA: GENERAL (i oiiiviivs sms ons sims mem oime ne erie sis mints anim 3-4 3.1.2 CERTAIN AIRSPEEDS INEMERGENCIES .............. 3-6 3.1.3 SELECTING EMERGENCY FREQUENCY .............. 35 3.2 AIRPLANE-RELATED G1000 WARNINGS ................... 3-6 3.21 WARNINGS / GENERAL ...\..vviviiniiiiiiiniennnans 3-6 322 LIRENGTEMP . LL. iii ie iran 3-6 323 LIROILTEMP otter ineine aarti eineannas 3-8 3 LIP OME PRES ow m amen goss is) cmc 1 i 0 BTA LE We 39 3.2.5 LAR GBOX TEMP «\ ovmmsmvms ss mass oe ssa 3-10 B20 LR PUBL TEMP «moins wimerivom wis im od a oie anes ssa 3-11 JZ TLR PUBL PRESS wie vm ie aries oo sorb o hoes 55 ma aiiati a 3-12 S28 LIRALTN AMPS ios vows ives dsm bails. od savas ate 3-12 F229 LMENG FIRE. i viiwmmvionse seid ies se ise in 3-13 FRAOURSTARTER wovvi wow sm smi ni imate oo shai odio vie 3-14 SZ1T DOOR OPEN ivi vv avid via van cies o Sanda 3-14 3.3 AIRPLANE-RELATED G1000 CAUTIONS ............c00uvnn 3-15 FF LIRALTN FAIL ova mmmdmin ee on viva ie saliii bio ia 3-15 3.4 GI000SYSTEMWARNINGS . ..... ovineeins 3-16 34 RED XIYELLOWX on osvsias enim eninidaimeiy 3-16 S42 ATTITUDE FAIL iii vapsmaminasvimmisae seria ene 3-18 343 AIRSPEED FAIL .......covvvivvnnnrrvrinrrrnnnsenns 3-16 BAA ALTITUDE FAIL cons sas ss nim rm aa a 3-16 3,5 VERT SPEED FAIL (ie aie eas names bens ws ioe deans oe 3-17 BB HDG Lottie ceri as 317 Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 3-1 Fehérgenoy » Diamond DA 42 NG AFMProcedures AIRCRAFT 35 GIO FAILURES coves sw mms wns sive Seems so% 3-18 3.5.1 NAVIGATION INFORMATION FAILURE .............. 3-18 3.52 PFDORMFD DISPLAY FAILURE .......... count. 3-18 3.53 AHRSFAILURE ....uiiiiininiininaraninnnsivnns 3-19 3.5.4 AIR DATA COMPUTER (ADC)FAILURE .............. 3-20 3.5.5 ERRONEOUS OR LOSS OF ENGINE AND FUEL DISPLAYS EE A AE RE MA No SA CG HAE 3-20 3.5.6 ERRONEOUS OR LOSS OF WARNING/CAUTION ANNUNCGIATORS oo ooos vs smeimis sameness sass 3-21 3.6 ABNORMAL ENGINE BEHAVIOUR ........ccvveiinvnnnns 3-22 3.7 ONE ENGINE INOPERATIVE PROCEDURES ............... 3-23 3.7.1 DETECTING THE INOPERATIVE ENGINE ............ 3-24 3.7.2 ENGINE TROUBLESHOOTING ....0ovvrvnrianrrvans 3-25 3.7.3 ENGINE SECURING (FEATHERING) PROCEDURE .... 3-28 3.7.4 UNFEATHERING & RESTARTING THE ENGINE IN FLIGHT Ce EI ST ee 3-29 3.7.5 ENGINE FAILURE DURING TAKE-OFF ............... 3-33 3.7.6 ENGINE FAILURES INFLIGHT ......coviiianininnns 3-36 3.7.7 LANDING WITH ONE ENGINE INOPERATIVE ......... 3-38 3.7.8 GO-AROUND / BALKED LANDING WITH ONE ENGINE INOPERATIVE .......0iiiiiniiiiniiennnennnn 3-41 3.7.9 FLIGHT WITH ONE ENGINE INOPERATIVE ........... 3-44 28, ENGINES OUT LANDING . coves amass psmes wan sass 3-46 3.9 LANDING GEAR SYSTEM FAILURES ........coviivnnnnnns 3-48 3.9.1 LANDING GEAR UNSAFE WARNING ................ 3-48 3.9.2 MANUAL EXTENSION OF THE LANDING GEAR ....... 3-50 3.9.3 LANDINGWITHGEARUP ........ccovvvnnrnninnnnss 3-52 3.9.4 LANDING WITH A DEFECTIVE TIRE ON THE MAIN LANDING EREAR © oo assis mesa ds se ER 8 ATS 3-53 3.9.5 LANDING WITH DEFECTIVEBRAKES ............... 3-54 3.10 FAILURES IN THE ELECTRICAL SYSTEM .........c00vuunn 3-585 Page 3-2 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E DA 42 NG AFM “Diamond Emergency AIRCRAFT Procedures 3.12 3.10.1 COMPLETE FAILURE OF THE ELECTRICAL SYSTEM .. 3-55 SAC HIGH CURRENT, wineries a driinins vain mma tie 3-56 3.10.3 STARTER MALFUNCTION ..........cvviinnnnnn... 3-57 SMOKE AND FIRE ....cuintieiiiiaiiniiiiiienieanns 3-58 3.11.1 ENGINEFIREONGROUND ............c.covvinunnn 3-58 3.11.2 ENGINE FIRE DURING TAKE-OFF .................. 3-59 3.11.3 ENGINE FIRE INFLIGHT cvvive nmin sn vsmsamsmasws 3-60 3.11.4 ELECTRICALFIREONGROUND ........ovvvuvunnnn 3-61 3.11.5 ELECTRICAL FIRE INFLIGHT ........covvvvvinnn.. 3-62 OTHER EMERGENCIES ............... AA SE 3-63 3.12.1 SUSPICION OF CARBON MONOXIDE CONTAMINATION IN THE CABIN» ose iaaiaii iain svnihing RES Cr TE 3-63 3.12.2 UNLOCKEDDOORS .........cvviiiinncnniannanes 3-64 3.12.3 DEFECTIVE PROPELLER RPM REGULATING SYSTEM Ty Cu 3-66 3.12.4 UNINTENTIONAL FLIGHT INTOICING ............... 3-69 3.125 FUEL SUPPLY FAILURE ..............coviviiiann. 3-70 3.12.6 RECOVERY FROM AN UNINTENTIONAL SPIN ........ 3-7 3.12.7 EMERGENCY DESCENT ....vvvvvenmaivvsrinenanin 3-73 3.12.8 EMERGENCY EXIT ... otter 3-73 3.12.9 AUTOPILOT OR ELECTRIC TRIM MALFUNCTION / FAILURE EAE BAA AES HT SC OF SEE SU FE 3-74 NOTE Procedures for uncritical system faults are given in Chapter 4B - ABNORMAL OPERATING PROCEDURES. Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 3-3 po Diamond DA 42 NG AFMProcedures 3.1 INTRODUCTION 3.1.1 GENERAL This chapter contains checklists as well as the description of recommended procedures to be followed in the event of an emergency. Engine failure or other airplane-related emergencies are most unlikely to occur if the prescribed procedures for pre-flight checks and airplane maintenance are followed. If, nonetheless, an emergency does arise, the guidelines given in this chapter should be followed and applied in order to clear the problem. As it is impossible to foresee all kinds of emergencies and cover them in this Airplane Flight Manual, a thorough understanding of the airplane by the pilot is, in addition to his knowledge and experience, an essential factor in the solution of any problems which may arise. WARNING In each emergency, control over the flight attitude and the preparation of a possible emergency landing have priority over attempts to solve the current problem (“first fly the airplane”). Prior to the flight the pilot must consider the suitability of the terrain for an emergency landing for each phase of the flight. For a safe flight the pilot must constantly keep a safe minimum flight altitude. Solutions for various adverse scenarios should be thought over in advance. This should prevent a situation where the pilot is faced with an emergency he cannot handle calmly and with determination. Page 3 - 4 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E r Emergency DA 42 NG AFM DiamondAIRCRAFT Procedures I EEDS IN EMERGENCIE Event One engine inoperative minimum Flaps UP 71 KIAS | g conkiol speed (i) Vie Flaps APP 68 KIAS One engine inoperative speed for best rate of climb vyee EERAS 3.1. ELECTING EM ENCY In an in-flight emergency, depressing and holding the Com transfer button +=# on the G1000 for 2 seconds will tune the emergency frequency of 121.500 MHz. If the display is available, it will also show it in the "Active" frequency window. Doc. Ne. 7.01.16-E Rev. 5 10-Jun-2021 Page 3-5 Emergency Diamond DA 42 NG AFMProcedures AIRCRAFT 3.2 AIRPLANE- TED WARNINGS 3.21 WARNINGS / GENERAL "Warning" means that the non-observation of the corresponding procedure leads to an immediate or important degradation in flight safety. The warning text is displayed in red color. Awarning chime tone of 1.5 seconds duration will sound and repeat without delay until the alarm is acknowledged by the crew, ENG TEMP L/R ENG TEMP Left / Right engine coolant temperature is in the upper red range (too high / above 105 °C) Coolant temperatures above the limit value of 105 °C can lead to a total loss of power due to engine failure. - Check G1000 for L/R COOL LVL caution message (low coolant level) L/R COOL LVL caution message not displayed: During climb: - Reduce power on affected engine by 10 % or more as required. - Increase airspeed by 10 KIAS or more as required. - If the coolant temperature does not reach the green range within 60 seconds, reduce power on affected engine as far as possible and increase airspeed. CONTINUED Page 3-6 Rev. 5 10-Jun-2021 Doe. No. 7.01.16-E DA 42 NG AFM Diamond AIRCRAFT Emergency Procedures During cruise: - Reduce power on affected engine. - Increase airspeed. - Check coolant temperature in green range. CAUTION f \ If high coolant temperature is indicated and the L/R COOL LVL caution message is not displayed, it can be assumed that thereis no technical defect in the cooling system and that the above mentioned procedure can decrease the temperature(s). This might not be the case if the coolant temperature does not return to the green range. In this case perform a precautionary landing on the nearest suitable airfield. Prepare for an engine failure in accordance with 3.7.6 - ENGINE FAILURES IN FLIGHT. END OF CHECKLIST L/R COOL LVL caution message displayed: - Reduce power on affected engine. FY - Expect loss of coolant. WARNING Afurther increase in coolant temperature mustbe expected. Prepare for an engine failure in accordance with 3.7.6 - ENGINE FAILURES IN FLIGHT. END OF CHECKLIST 27 \ Doc. No, 7.01.16-E Rev. 5 10-Jun-2021 Page 3-7 E - margahay @ Diamond DA 42 NG AFMProcedures AIRCRAFT 3.2.3 LIR OIL TEMP L/R OIL TEMP Left / Right engine oil temperature is in the upper red range (too high / above 140 °C). Oil temperatures above the limit value of 140 °C can lead to a total loss of power due to engine failure. - Check oll pressure. If the oil pressure is outside of the green range (lower limit): - Reduce power on affected engine. - Expect loss of engine oil, WARNING A further increase in oil temperature must be expected. Prepare for an engine failure in accordance with 3.7.6 - ENGINE FAILURES IN FLIGHT. If the oil pressure is within the green range: - Reduce power on affected engine. - Increase airspeed. CONTINUED Page 3-8 Rev. 5 10-Jun-2021 Doc. No. 7.01.16-E DA 42 NG AFM Diamond Esreegancy! AIRCRAFT Procedures CAUTION If high oil temperature is announced and the oil pressure indication is within the green range, it can be assumed that there is no technical defect in the engine oil system and that the above mentioned procedure can decrease the temperature(s). This might not be the case if the oil temperature does not return to the green range. In this case perform a precautionary landing on the nearest suitable airfield. Prepare for an engine failure in accordance with 3.7.6 - ENGINE FAILURES IN FLIGHT. END OF CHECKLIST 3.24 LIR OIL PRES L/R OIL PRES Left / Right engine oil pressure is in the lower red range (too low [ below 0.9 bar). Oil pressures below the limit value of 0.9 bar can lead to a total loss of power due to engine failure. - Reduce power on affected engine. - Expect loss of oil. WARNING Land at the nearest suitable airfield. Prepare for an engine failure in accordance with 3.7.6 - ENGINE FAILURES IN FLIGHT. END OF CHECKLIST Doc. No. 7.01.16-E Rev. 5 10-Jun-2021 Page 3-9 Emergency @ Diamond DA 42 NG AFM Procedures AIRCRAFT 3.2.5 L/IR GBOX TEMP Left / Right engine gearbox temperature is in the L/R GBOX TEMP upper red range (too high / above 120 °C). Gearbox temperatures above the limit value of 120 °C can lead to a total loss of power due to engine failure. - Reduce power on affected engine. - Increase