DA 42 AFM

Diamond DA42 VI · Parts Catalog

Free account — keep the POHs & checklists you reference in one place.

Overview

This document is the Airplane Flight Manual (AFM) for the Diamond DA42 aircraft equipped with the Garmin GFC700 Autopilot System. It provides essential information regarding the operation, procedures, and limitations necessary for safe flight.

The AFM is valid for Diamond DA42 airplanes with Garmin GFC700.
Pilots must familiarize themselves with the entire manual before first operation.
The manual includes approved chapters by EASA.
Revisions must be recorded in the manual.
Temporary revisions provide interim information until permanent updates.
The document is protected by copyright.

Document

Source

Originally published by acaeronautics.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

View original at acaeronautics.com

Report a problem or request removal

Document details

Type: Parts Catalog
Year: 2024
File size: 11 MB
Publisher: acaeronautics.com
Language: en

About this document

What is the DA 42 AFM?

The DA 42 AFM is a parts catalog for the Diamond DA42 VI, dated 2024.

Where does the DA 42 AFM come from?

This copy of the DA 42 AFM was originally published by acaeronautics.com and is hosted on Sprinkle as a free, searchable reference copy.

What year was the DA 42 AFM published?

The DA 42 AFM — the Diamond DA42 VI parts catalog on file — is dated 2024.

Documentation completeness

6/7

Most owners only have the POH. Here's the essential set for the Diamond DA42 VI.

More Diamond DA42 VImanuals & documents

See all 31 →

In this document

Approval

The content of approved chapters is approved by EASA, while other content is approved by DAI under EASA DOA No. EASA.21J.052.

Record of Revisions

All revisions must be recorded, and new text is indicated by a vertical black line on the revised page.

List of Effective Pages

A list of effective pages is provided, indicating the date of each page's revision.

Full document text

Introduction DA 42 AFM with OÄM 42-102 Garmin GFC 700 NOTE This Airplane Flight Manual is valid for DIAMOND DA 42 Airplanes with a Garmin GFC700 Autopilot System in accordance with OÄM 42-102 installed. Page 0 - 0a Rev. 0 20-Dec-2007 Doc. No. 7.01.06-E DA 42 AFM with OÄM 42-102 Garmin GFC 700 Introduction FOREWORD We congratulate you on the acquisition of your new DIAMOND DA 42 enquired with Garmin GFC700 Autopilot. 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. 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 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@diamondaircraft.com Doc. No. 7.01.06-E Rev. 5 25-Nov-2024 Page 0 - 1 Introduction DA 42 AFM with OÄM 42-102 Garmin GFC 700 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; the following pages of the Temporary Revision are inserted in front of the corresponding pages of this AFM. 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 (MÄM or OÄM), then the corresponding Temporary Revision is superseded. Example: If Revision 3 covers OÄM 42-XXX, then the Temporary Revision TR-OÄM-42-XXX is superseded by the 'permanent' Revision 3. Page 0 - 2 Rev. 5 25-Nov-2024 Doc. No. 7.01.06-E DA 42 AFM with OÄM 42-102 Garmin GFC 700 Introduction Rev. No. Reason Chap- ter Page(s) Date of Revision Approval Note Date of Approval Date Inserted Signature 1 MÄM 42- -268/a, -270, -272, -284, -292, -294, -301, -304, -336, -347, -377, -405, -405/a, -443, OÄM 42- -053/e & -054/e, -056/e, -107/d, -108/a, -111& -158, -125, -127, -134, -141/a, -142, -146/a, -175, -188, -195, - 205, -208, corrections all all except cover page 30-Apr-2011 Revision No. 1 of the AFM Doc. No. 7.01.06-E is approved under the authority of DOA No. EASA.21J. 052 Doc. No. 7.01.06-E Rev. 5 25-Nov-2024 Page 0 - 3 Introduction DA 42 AFM with OÄM 42-102 Garmin GFC 700 Rev. No. Reason Chap- ter Page(s) Date of Revision Approval Note Date of Approval Date Inserted Signature 2 MÄM 42- -529, -542, -545/a, -546, -575, -584, -641, -685, -716, -756, -764/d, -814, -861, OÄM 42- -053/f & -054/f, -055/b, -056/f, -094, -107/f, -111/a& -158/a&-246, -119, -178, -185, -215, -252, -253, -259, -279, -280, -283, corrections all all except cover page 30 Nov 2015 Revision No. 2 of the AFM Doc. No. 7.01.06-E is approved under the authority of DOA No. EASA.21J. 052 3 OÄM 42- -222, -252/b, -304/a, corrections all all except cover page 15 Dec 2017 Revision No. 3 of the AFM Doc. No. 7.01.06-E is approved under the authority of DOA No. EASA.21J. 052 09 Feb 2018 Page 0 - 4 Rev. 5 25-Nov-2024 Doc. No. 7.01.06-E DA 42 AFM with OÄM 42-102 Garmin GFC 700 Introduction Rev. No. Reason Chap- ter Page(s) Date of Revision Approval Note Date of Approval Date Inserted Signature 4 MÄM 42- -983, -1024, -1025, -1034, -1111, -1114, -1186, -1191, -1199, -1200, OÄM 42- -053/g & -054/g, -055/c, -324/a, -334, -339, corrections all all except cover page 14 Feb 2022 Revision No. 4 of the AFM Doc. No. 7.01.06-E is approved under the authority of DOA No. EASA.21J. 052 17 Feb 2022 5 | MÄM 42- | -1265, | -1310, | -1325, | | OÄM 42- | -134/a, | -179, | -211, | -252/c, | -280/a, | | corrections | all | all | except | cover page | 25 Nov 2024 | Revision | No. 5 of the | AFM Doc. | No. | 7.01.06-E | is approved | under the | authority of | DOA ref. | EASA.21J. | 052 | 28 Nov | 2024 ||| Doc. No. 7.01.06-E Rev. 5 25-Nov-2024 Page 0 - 5 Introduction DA 42 AFM with OÄM 42-102 Garmin GFC 700 Rev. No. Reason Chap- ter Page(s) Date of Revision Approval Note Date of Approval Date Inserted Signature Page 0 - 6 Rev. 5 25-Nov-2024 Doc. No. 7.01.06-E DA 42 AFM with OÄM 42-102 Garmin GFC 700 Introduction 0.3 LIST OF EFFECTIVE PAGES Ch. Page Date 0 0-0 20 Dec 2007 0-0a 20 Dec 2007 0-1 25 Nov 2024 | 0-2 25 Nov 2024 | 0-3 25 Nov 2024 | 0-4 25 Nov 2024 | 0-5 25 Nov 2024 | 0-6 25 Nov 2024 | 0-7 25 Nov 2024 | 0-8 25 Nov 2024 | 0-9 25 Nov 2024 |

Show full text

0-10 25 Nov 2024 | 0-11 25 Nov 2024 | 0-12 25 Nov 2024 | 0-13 25 Nov 2024 | 0-14 25 Nov 2024 | 0-15 25 Nov 2024 | 0-16 25 Nov 2024 | Ch. Page Date 1 1-1 25 Nov 2024 | 1-2 25 Nov 2024 | 1-3 25 Nov 2024 | 1-4 25 Nov 2024 | 1-5 25 Nov 2024 | 1-6 25 Nov 2024 | 1-7 25 Nov 2024 | 1-8 25 Nov 2024 | 1-9 25 Nov 2024 | 1-10 25 Nov 2024 | 1-11 25 Nov 2024 | 1-12 25 Nov 2024 | 1-13 25 Nov 2024 | 1-14 25 Nov 2024 | 1-15 25 Nov 2024 | 1-16 25 Nov 2024 | 1-17 25 Nov 2024 | 1-18 25 Nov 2024 | 1-19 25 Nov 2024 | 1-20 25 Nov 2024 | 1-21 25 Nov 2024 | 1-22 25 Nov 2024 | 1-23 25 Nov 2024 | 1-24 25 Nov 2024 | Doc. No. 7.01.06-E Rev. 5 25-Nov-2024 Page 0 - 7 Introduction DA 42 AFM with OÄM 42-102 Garmin GFC 700 Ch. Page Date 2 appr. 2-1 25 Nov 2024 | appr. 2-2 25 Nov 2024 | appr. 2-3 25 Nov 2024 | appr. 2-4 25 Nov 2024 | appr. 2-5 25 Nov 2024 | appr. 2-6 25 Nov 2024 | appr. 2-7 25 Nov 2024 | appr. 2-8 25 Nov 2024 | appr. 2-9 25 Nov 2024 | appr. 2-10 25 Nov 2024 | appr. 2-11 25 Nov 2024 | appr. 2-12 25 Nov 2024 | appr. 2-13 25 Nov 2024 | appr. 2-14 25 Nov 2024 | appr. 2-15 25 Nov 2024 | appr. 2-16 25 Nov 2024 | appr. 2-17 25 Nov 2024 | appr. 2-18 25 Nov 2024 | appr. 2-19 25 Nov 2024 | appr. 2-20 25 Nov 2024 | appr. 2-21 25 Nov 2024 | appr. 2-22 25 Nov 2024 | appr. 2-23 25 Nov 2024 | appr. 2-24 25 Nov 2024 | appr. 2-25 25 Nov 2024 | appr. 2-26 25 Nov 2024 | appr. 2-27 25 Nov 2024 | appr. 2-28 25 Nov 2024 | appr. 2-29 25 Nov 2024 | appr. 2-30 25 Nov 2024 | appr. 2-31 25 Nov 2024 | appr. 2-32 25 Nov 2024 | appr. 2-33 25 Nov 2024 | Ch. Page Date 2 appr. 2-34 25 Nov 2024 | appr. 2-35 25 Nov 2024 | appr. 2-36 25 Nov 2024 | appr. 2-37 25 Nov 2024 | appr. 2-38 25 Nov 2024 | appr. 2-39 25 Nov 2024 | appr. 2-40 25 Nov 2024 | Page 0 - 8 Rev. 5 25-Nov-2024 Doc. No. 7.01.06-E DA 42 AFM with OÄM 42-102 Garmin GFC 700 Introduction Ch. Page Date 3 3-1 25 Nov 2024 | 3-2 25 Nov 2024 | 3-3 25 Nov 2024 | 3-4 25 Nov 2024 | 3-5 25 Nov 2024 | 3-6 25 Nov 2024 | 3-7 25 Nov 2024 | 3-8 25 Nov 2024 | 3-9 25 Nov 2024 | 3-10 25 Nov 2024 | 3-11 25 Nov 2024 | 3-12 25 Nov 2024 | 3-13 25 Nov 2024 | 3-14 25 Nov 2024 | 3-15 25 Nov 2024 | 3-16 25 Nov 2024 | 3-17 25 Nov 2024 | 3-18 25 Nov 2024 | 3-19 25 Nov 2024 | 3-20 25 Nov 2024 | 3-21 25 Nov 2024 | 3-22 25 Nov 2024 | 3-23 25 Nov 2024 | 3-24 25 Nov 2024 | 3-25 25 Nov 2024 | 3-26 25 Nov 2024 | 3-27 25 Nov 2024 | 3-28 25 Nov 2024 | 3-29 25 Nov 2024 | 3-30 25 Nov 2024 | 3-31 25 Nov 2024 | 3-32 25 Nov 2024 | 3-33 25 Nov 2024 | Ch. Page Date 3 3-34 25 Nov 2024 | 3-35 25 Nov 2024 | 3-36 25 Nov 2024 | 3-37 25 Nov 2024 | 3-38 25 Nov 2024 | 3-39 25 Nov 2024 | 3-40 25 Nov 2024 | 3-41 25 Nov 2024 | 3-42 25 Nov 2024 | 3-43 25 Nov 2024 | 3-44 25 Nov 2024 | 3-45 25 Nov 2024 | 3-46 25 Nov 2024 | 3-47 25 Nov 2024 | 3-48 25 Nov 2024 | 3-49 25 Nov 2024 | 3-50 25 Nov 2024 | 3-51 25 Nov 2024 | 3-52 25 Nov 2024 | 3-53 25 Nov 2024 | 3-54 25 Nov 2024 | 3-55 25 Nov 2024 | 3-56 25 Nov 2024 | 3-57 25 Nov 2024 | 3-58 25 Nov 2024 | Doc. No. 7.01.06-E Rev. 5 25-Nov-2024 Page 0 - 9 Introduction DA 42 AFM with OÄM 42-102 Garmin GFC 700 Ch. Page Date 4A 4A-1 25 Nov 2024 | 4A-2 25 Nov 2024 | 4A-3 25 Nov 2024 | 4A-4 25 Nov 2024 | 4A-5 25 Nov 2024 | 4A-6 25 Nov 2024 | 4A-7 25 Nov 2024 | 4A-8 25 Nov 2024 | 4A-9 25 Nov 2024 | 4A-10 25 Nov 2024 | 4A-11 25 Nov 2024 | 4A-12 25 Nov 2024 | 4A-13 25 Nov 2024 | 4A-14 25 Nov 2024 | 4A-15 25 Nov 2024 | 4A-16 25 Nov 2024 | 4A-17 25 Nov 2024 | 4A-18 25 Nov 2024 | 4A-19 25 Nov 2024 | 4A-20 25 Nov 2024 | 4A-21 25 Nov 2024 | 4A-22 25 Nov 2024 | 4A-23 25 Nov 2024 | 4A-24 25 Nov 2024 | 4A-25 25 Nov 2024 | 4A-26 25 Nov 2024 | 4A-27 25 Nov 2024 | 4A-28 25 Nov 2024 | 4A-29 25 Nov 2024 | 4A-30 25 Nov 2024 | 4A-31 25 Nov 2024 | 4A-32 25 Nov 2024 | 4A-33 25 Nov 2024 | Ch. Page Date 4A 4A-34 25 Nov 2024 | 4A-35 25 Nov 2024 | 4A-36 25 Nov 2024 | 4A-37 25 Nov 2024 | 4A-38 25 Nov 2024 | 4A-39 25 Nov 2024 | 4A-40 25 Nov 2024 | 4A-41 25 Nov 2024 | 4A-42 25 Nov 2024 | 4A-43 25 Nov 2024 | 4A-44 25 Nov 2024 | 4A-45 25 Nov 2024 | 4A-46 25 Nov 2024 | 4A-47 25 Nov 2024 | 4A-48 25 Nov 2024 | 4A-49 25 Nov 2024 | 4A-50 25 Nov 2024 | 4A-51 25 Nov 2024 | 4A-52 25 Nov 2024 | 4A-53 25 Nov 2024 | 4A-54 25 Nov 2024 | 4A-55 25 Nov 2024 | 4A-56 25 Nov 2024 | 4A-57 25 Nov 2024 | 4A-58 25 Nov 2024 | 4A-59 25 Nov 2024 | 4A-60 25 Nov 2024 | Page 0 - 10 Rev. 5 25-Nov-2024 Doc. No. 7.01.06-E DA 42 AFM with OÄM 42-102 Garmin GFC 700 Introduction Ch. Page Date 4B 4B-1 25 Nov 2024 | 4B-2 25 Nov 2024 | 4B-3 25 Nov 2024 | 4B-4 25 Nov 2024 | 4B-5 25 Nov 2024 | 4B-6 25 Nov 2024 | 4B-7 25 Nov 2024 | 4B-8 25 Nov 2024 | 4B-9 25 Nov 2024 | 4B-10 25 Nov 2024 | 4B-11 25 Nov 2024 | 4B-12 25 Nov 2024 | 4B-13 25 Nov 2024 | 4B-14 25 Nov 2024 | 4B-15 25 Nov 2024 | 4B-16 25 Nov 2024 | 4B-17 25 Nov 2024 | 4B-18 25 Nov 2024 | 4B-19 25 Nov 2024 | 4B-20 25 Nov 2024 | 4B-21 25 Nov 2024 | 4B-22 25 Nov 2024 | 4B-23 25 Nov 2024 | 4B-24 25 Nov 2024 | 4B-25 25 Nov 2024 | 4B-26 25 Nov 2024 | 4B-27 25 Nov 2024 | 4B-28 25 Nov 2024 | 4B-29 25 Nov 2024 | 4B-30 25 Nov 2024 | 4B-31 25 Nov 2024 | 4B-32 25 Nov 2024 | 4B-33 25 Nov 2024 | Ch. Page Date 4B 4B-34 25 Nov 2024 | 4B-35 25 Nov 2024 | 4B-36 25 Nov 2024 | 4B-37 25 Nov 2024 | 4B-38 25 Nov 2024 | 4B-39 25 Nov 2024 | 4B-40 25 Nov 2024 | 4B-41 25 Nov 2024 | 4B-42 25 Nov 2024 | 4B-43 25 Nov 2024 | 4B-44 25 Nov 2024 | 4B-45 25 Nov 2024 | 4B-46 25 Nov 2024 | 4B-47 25 Nov 2024 | 4B-48 25 Nov 2024 | Doc. No. 7.01.06-E Rev. 5 25-Nov-2024 Page 0 - 11 Introduction DA 42 AFM with OÄM 42-102 Garmin GFC 700 Ch. Page Date 5 5-1 25 Nov 2024 | 5-2 25 Nov 2024 | 5-3 25 Nov 2024 | 5-4 25 Nov 2024 | 5-5 25 Nov 2024 | 5-6 25 Nov 2024 | 5-7 25 Nov 2024 | 5-8 25 Nov 2024 | 5-9 25 Nov 2024 | 5-10 25 Nov 2024 | 5-11 25 Nov 2024 | 5-12 25 Nov 2024 | 5-13 25 Nov 2024 | 5-14 25 Nov 2024 | 5-15 25 Nov 2024 | 5-16 25 Nov 2024 | 5-17 25 Nov 2024 | 5-18 25 Nov 2024 | 5-19 25 Nov 2024 | 5-20 25 Nov 2024 | 5-21 25 Nov 2024 | 5-22 25 Nov 2024 | 5-23 25 Nov 2024 | 5-24 25 Nov 2024 | 5-25 25 Nov 2024 | 5-26 25 Nov 2024 | 5-27 25 Nov 2024 | 5-28 25 Nov 2024 | 5-29 25 Nov 2024 | 5-30 25 Nov 2024 | 5-31 25 Nov 2024 | 5-32 25 Nov 2024 | 5-33 25 Nov 2024 | Ch. Page Date 5 5-34 25 Nov 2024 | Page 0 - 12 Rev. 5 25-Nov-2024 Doc. No. 7.01.06-E DA 42 AFM with OÄM 42-102 Garmin GFC 700 Introduction Ch. Page Date 6 6-1 25 Nov 2024 | 6-2 25 Nov 2024 | 6-3 25 Nov 2024 | 6-4 25 Nov 2024 | 6-5 25 Nov 2024 | 6-6 25 Nov 2024 | 6-7 25 Nov 2024 | 6-8 25 Nov 2024 | 6-9 25 Nov 2024 | 6-10 25 Nov 2024 | 6-11 25 Nov 2024 | 6-12 25 Nov 2024 | 6-13 25 Nov 2024 | 6-14 25 Nov 2024 | 6-15 25 Nov 2024 | 6-16 25 Nov 2024 | 6-17 25 Nov 2024 | 6-18 25 Nov 2024 | 6-19 25 Nov 2024 | 6-20 25 Nov 2024 | 6-21 25 Nov 2024 | 6-22 25 Nov 2024 | 6-23 25 Nov 2024 | 6-24 25 Nov 2024 | 6-25 25 Nov 2024 | 6-26 25 Nov 2024 | 6-27 25 Nov 2024 | 6-28 25 Nov 2024 | 6-29 25 Nov 2024 | 6-30 25 Nov 2024 | Ch. Page Date 7 7-1 25 Nov 2024 | 7-2 25 Nov 2024 | 7-3 25 Nov 2024 | 7-4 25 Nov 2024 | 7-5 25 Nov 2024 | 7-6 25 Nov 2024 | 7-7 25 Nov 2024 | 7-8 25 Nov 2024 | 7-9 25 Nov 2024 | 7-10 25 Nov 2024 | 7-11 25 Nov 2024 | 7-12 25 Nov 2024 | 7-13 25 Nov 2024 | 7-14 25 Nov 2024 | 7-15 25 Nov 2024 | 7-16 25 Nov 2024 | 7-17 25 Nov 2024 | 7-18 25 Nov 2024 | 7-19 25 Nov 2024 | 7-20 25 Nov 2024 | 7-21 25 Nov 2024 | 7-22 25 Nov 2024 | 7-23 25 Nov 2024 | 7-24 25 Nov 2024 | 7-25 25 Nov 2024 | 7-26 25 Nov 2024 | 7-27 25 Nov 2024 | 7-28 25 Nov 2024 | 7-29 25 Nov 2024 | 7-30 25 Nov 2024 | 7-31 25 Nov 2024 | 7-32 25 Nov 2024 | 7-33 25 Nov 2024 | Doc. No. 7.01.06-E Rev. 5 25-Nov-2024 Page 0 - 13 Introduction DA 42 AFM with OÄM 42-102 Garmin GFC 700 Ch. Page Date 7 7-34 25 Nov 2024 | 7-35 25 Nov 2024 | 7-36 25 Nov 2024 | 7-37 25 Nov 2024 | 7-38 25 Nov 2024 | 7-39 25 Nov 2024 | 7-40 25 Nov 2024 | 7-41 25 Nov 2024 | 7-42 25 Nov 2024 | 7-43 25 Nov 2024 | 7-44 25 Nov 2024 | 7-45 25 Nov 2024 | 7-46 25 Nov 2024 | 7-47 25 Nov 2024 | 7-48 25 Nov 2024 | 7-49 25 Nov 2024 | 7-50 25 Nov 2024 | 7-51 25 Nov 2024 | 7-52 25 Nov 2024 | 7-53 25 Nov 2024 | 7-54 25 Nov 2024 | 7-55 25 Nov 2024 | 7-56 25 Nov 2024 | 7-57 25 Nov 2024 | 7-58 25 Nov 2024 | 7-59 25 Nov 2024 | 7-60 25 Nov 2024 | 7-61 25 Nov 2024 | 7-62 25 Nov 2024 | 7-63 25 Nov 2024 | 7-64 25 Nov 2024 | 7-65 25 Nov 2024 | Ch. Page Date 7 7-66 25 Nov 2024 | 7-67 25 Nov 2024 | 7-68 25 Nov 2024 | 7-69 25 Nov 2024 | 7-70 25 Nov 2024 | 7-71 25 Nov 2024 | 7-72 25 Nov 2024 | 7-73 25 Nov 2024 | 7-74 25 Nov 2024 | 7-75 25 Nov 2024 | 7-76 25 Nov 2024 | 7-77 25 Nov 2024 | 7-78 25 Nov 2024 | 7-79 25 Nov 2024 | 7-80 25 Nov 2024 | 7-81 25 Nov 2024 | 7-82 25 Nov 2024 | 7-83 25 Nov 2024 | 7-84 25 Nov 2024 | 7-85 25 Nov 2024 | 7-86 25 Nov 2024 | 7-87 25 Nov 2024 | 7-88 25 Nov 2024 | 7-89 25 Nov 2024 | 7-90 25 Nov 2024 | Page 0 - 14 Rev. 5 25-Nov-2024 Doc. No. 7.01.06-E DA 42 AFM with OÄM 42-102 Garmin GFC 700 Introduction Ch. Page Date 8 8-1 25 Nov 2024 | 8-2 25 Nov 2024 | 8-3 25 Nov 2024 | 8-4 25 Nov 2024 | 8-5 25 Nov 2024 | 8-6 25 Nov 2024 | 8-7 25 Nov 2024 | 8-8 25 Nov 2024 | 8-9 25 Nov 2024 | 8-10 25 Nov 2024 | 8-11 25 Nov 2024 | 8-12 25 Nov 2024 | 8-13 25 Nov 2024 | 8-14 25 Nov 2024 | 8-15 25 Nov 2024 | 8-16 25 Nov 2024 | Ch. Page Date 9 9-1 25 Nov 2024 | 9-2 25 Nov 2024 | 9-3 25 Nov 2024 | 9-4 25 Nov 2024 | 9-5 25 Nov 2024 | 9-6 25 Nov 2024 | Doc. No. 7.01.06-E Rev. 5 25-Nov-2024 Page 0 - 15 Introduction DA 42 AFM with OÄM 42-102 Garmin GFC 700 0.4 TABLE OF CONTENTS Chapter GENERAL (a non-approved chapter) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 OPERATING LIMITATIONS (an approved chapter) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 EMERGENCY PROCEDURES (a non-approved chapter) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 NORMAL OPERATING PROCEDURES (a non-approved chapter) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4A ABNORMAL OPERATING PROCEDURES (a non-approved chapter) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4B PERFORMANCE (a non-approved chapter) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 MASS AND BALANCE / EQUIPMENT LIST (a non-approved chapter) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6 DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS (a non-approved chapter) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7 AIRPLANE HANDLING, CARE AND MAINTENANCE (a non-approved chapter) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8 SUPPLEMENTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 Page 0 - 16 Rev. 5 25-Nov-2024 Doc. No. 7.01.06-E DA 42 AFM with OÄM 42-102 Garmin GFC 700 General CHAPTER 1 GENERAL Page 1.1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-2 1.2 CERTIFICATION BASIS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-5 1.3 WARNINGS, CAUTIONS AND NOTES . . . . . . . . . . . . . . . . . . . . . . 1-5 1.4 DIMENSIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-6 1.5 DEFINITIONS AND ABBREVIATIONS . . . . . . . . . . . . . . . . . . . . . . . 1-8 1.6 UNITS OF MEASUREMENT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-16 1.6.1 CONVERSION FACTORS. . . . . . . . . . . . . . . . . . . . . . . . . . . 1-16 1.6.2 CONVERSION CHART LITERS / US GALLONS . . . . . . . . . 1-18 1.7 THREE-VIEW DRAWING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-19 1.8 G1000 AVIONICS SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-20 1.9 SOURCE DOCUMENTATION. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-23 1.9.1 ENGINE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-23 1.9.2 PROPELLER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-23 1.9.3 AVIONICS SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-24 Doc. No. 7.01.06-E Rev. 5 25-Nov-2024 Page 1 - 1 General DA 42 AFM with OÄM 42-102 Garmin GFC 700 1.1 INTRODUCTION 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 with the Garmin GFC 700 Autopilot System installed. 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. This Airplane Flight Manual is valid for serial numbers equipped with the Garmin GFC 700 Autopilot System. 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 Firmware 2.7, Mapping O28V273DA42 MÄM 42-284 yes no Firmware 2.91, Mapping O28V291DA42 MÄM 42-304 yes no Firmware 2.91, Mapping O28V294DA42 MÄM 42-529 yes no Ice Protection System OÄM 42-053 yes no Ice Protection System (Known Icing) OÄM 42-054 yes no Oxygen System OÄM 42-055 yes no Auxiliary Fuel Tanks OÄM 42-056 yes no Page 1 - 2 Rev. 5 25-Nov-2024 Doc. No. 7.01.06-E DA 42 AFM with OÄM 42-102 Garmin GFC 700 General Modification Source Installed Front Seats with Adjustable Backrest OÄM 42-067 yes no Electrical Rudder Pedal Adjustment OÄM 42-070 yes no Mission Power Supply System OÄM 42-074 yes no Removable Fuselage Nose Cone OÄM 42-077 yes no Operator Desk (Full CFRP Version) OÄM 42-111 yes no Operator Desk (CFRP Version with Aluminum Joint) OÄM 42-111/a yes no Garmin GWX 68 Weather Radar OÄM 42-119 yes no ECU Backup Battery OÄM 42-129 yes no Operator Desk (Full Aluminum Version) OÄM 42-158 yes no Increase of Maximum Zero Fuel Mass OÄM 42-188 yes no Maximum Landing Mass 1785 kg OÄM 42-195 yes no Emergency Axe OÄM 42-205 yes no TAE 125-02-114 Engine OÄM 42-252/c yes no Front Seats with Adjustable Backrest - Hydrolok OÄM 42-259 yes no Emergency Egress Hammer OÄM 42-304 yes no Doc. No. 7.01.06-E Rev. 5 25-Nov-2024 Page 1 - 3 General DA 42 AFM with OÄM 42-102 Garmin GFC 700 NOTE The use of ECU Mapping O28V273DA42, ECU Mapping O28V291DA42 and ECU Mapping O28V294DA42 is limited to TAE 125-02-99 engines (MÄM 42-198, latest revision carried out). This Airplane Flight Manual must be kept on board the airplane at all 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. CAUTION The DA 42 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 constitute a risk. Page 1 - 4 Rev. 5 25-Nov-2024 Doc. No. 7.01.06-E DA 42 AFM with OÄM 42-102 Garmin GFC 700 General 1.2 CERTIFICATION BASIS 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 WARNINGS, CAUTIONS 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: WARNING means that the non-observation of the corresponding procedure leads to an immediate or important degradation in flight safety. 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. 7.01.06-E Rev. 5 25-Nov-2024 Page 1 - 5 General DA 42 AFM with OÄM 42-102 Garmin GFC 700 1.4 DIMENSIONS NOTE All dimensions shown below are approximate. Overall Dimensions Span : 13.42 m 44 ft : 13.55 m 44.5 ft including ACL Length : 8.56 m 28 ft 1 in Height : 2.49 m 8 ft 2 in Wing Airfoil : Wortmann FX 63-137/20 - W4 Wing Area : 16.29 m² 175.3 sq.ft. Mean aerodynamic chord : 1.271 m 4 ft 2 in Aspect ratio : 11.06 Dihedral : 5° Leading edge sweep : 1° Aileron Area (total, left + right) : 0.66 m² 7.1 sq.ft. Page 1 - 6 Rev. 5 25-Nov-2024 Doc. No. 7.01.06-E DA 42 AFM with OÄM 42-102 Garmin GFC 700 General Wing Flaps Area (total, left + right) : 2.18 m² 23.4 sq.ft. Horizontal Tail Area : 2.35 m2 25.3 sq.ft. Elevator area : 0.66 m² 7.1 sq.ft. Angle of incidence : -1.1° relative to longitudinal axis of airplane Vertical Tail Area : 2.43 m² 26.2 sq.ft. Rudder area : 0.78 m² 8.4 sq.ft. Landing Gear Track : 2.95 m (9 ft 8 in) Wheelbase : 1.735 m (5 ft 8 in) Nose wheel : 5.00-5* Main wheel : 15x6.0-6* * for details refer to the Airplane Maintenance Manual, Doc. No. 7.02.01, latest revision Doc. No. 7.01.06-E Rev. 5 25-Nov-2024 Page 1 - 7 General DA 42 AFM with OÄM 42-102 Garmin GFC 700 1.5 DEFINITIONS AND ABBREVIATIONS (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. vA: Maneuvering Speed. 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. vLO: Maximum Landing Gear Operating Speed. This speed may not be exceeded during the extension or retraction of the landing gear. vLE: Maximum Landing Gear Extended Speed. This speed may not be exceeded if the landing gear is extended. vMC: Minimum Control Speed. Minimum speed necessary to be able to control the airplane in case of one engine inoperative. 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. Page 1 - 8 Rev. 5 25-Nov-2024 Doc. No. 7.01.06-E DA 42 AFM with OÄM 42-102 Garmin GFC 700 General vS: Stalling Speed, or the minimum continuous speed at which the airplane is still controllable in the given configuration. vS0: Stalling Speed, or the minimum continuous speed at which the airplane is still controllable in the landing configuration. vS1: Stalling Speed, or the minimum continuous speed at which the airplane is still controllable with flaps and landing gear retracted. vSSE: Minimum Control Speed for Schooling. Minimum speed necessary in case of one engine intentionally inoperative / idle (training purposes). vx: 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 temperature at 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. 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. Doc. No. 7.01.06-E Rev. 5 25-Nov-2024 Page 1 - 9 General DA 42 AFM with OÄM 42-102 Garmin GFC 700 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 set to 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 in this manual should be regarded as headwind or tailwind components of the measured wind. (c) Flight Performance and Flight Planning 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. MET: Weather, weather advice. NAV: Navigation, route planning. RoC: Rate of Climb. Page 1 - 10 Rev. 5 25-Nov-2024 Doc. No. 7.01.06-E DA 42 AFM with OÄM 42-102 Garmin GFC 700 General (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 which is 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. Maximum Landing Mass: The highest mass for landing conditions at the 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. Doc. No. 7.01.06-E Rev. 5 25-Nov-2024 Page 1 - 11 General DA 42 AFM with OÄM 42-102 Garmin GFC 700 Usable fuel: The quantity of fuel available for flight 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. Aux. tanks: Auxiliary tanks. (e) Engine ECU: Engine Control Unit FADEC: Full Authority Digital Engine Control 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. Page 1 - 12 Rev. 5 25-Nov-2024 Doc. No. 7.01.06-E DA 42 AFM with OÄM 42-102 Garmin GFC 700 General (f) Designation of the Circuit Breakers on the Instrument Panel LH MAIN BUS: COM1 COM Radio No. 1 GPS/NAV1 Global Positioning System and NAV Receiver No. 1 XPDR Transponder ENG INST Engine Instruments PITOT Pitot Heating System XFR PUMP/DE-ICE Fuel Transfer Pump / De-Icing System TAXI/MAP/ACL Taxi-, Map-, Anti Collision Light FLOOD/OXY Flood Light / Oxygen System 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 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. Avionic Control Doc. No. 7.01.06-E Rev. 5 25-Nov-2024 Page 1 - 13 General DA 42 AFM with OÄM 42-102 Garmin GFC 700 AVIONICS BUS: COM2 COM Radio No. 2 GPS/NAV2 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 LH ENG ECU BUS: ECU BUS LH ECU Bus ECU B LH ECU B ECU A LH ECU A LH BUS: ALT.LH LH Alternator BATT Battery RH BUS: ALT.RH RH Alternator BATT Battery RH ENG ECU BUS: ECU BUS RH ECU Bus ECU B RH ECU B ECU A RH ECU A Page 1 - 14 Rev. 5 25-Nov-2024 Doc. No. 7.01.06-E DA 42 AFM with OÄM 42-102 Garmin GFC 700 General (g) Equipment ELT: Emergency Locator Transmitter (h) Design Change Advisories MÄM: Mandatory Design Change Advisory OÄM: Optional Design Change Advisory VÄM: Variant Design Change Advisory (i) Miscellaneous ACG: Austro Control GmbH ATC: Air Traffic Control CFRP: Carbon Fiber Reinforced Plastic EASA: European Aviation Safety Agency EFB: Electronic Flight Bag EPU: External Power Unit GIA: Garmin Integrated Avionics GFRP: Glass Fiber Reinforced Plastic IPL: Interference Path Loss JAR: Joint Aviation Requirements JC/VP: Joint Certification/Validation Procedure PCA: Primary Certification Authority PED: Portable Electronic Device T-PED: Transmitting Portable Electronic Device Doc. No. 7.01.06-E Rev. 5 25-Nov-2024 Page 1 - 15 General DA 42 AFM with OÄM 42-102 Garmin GFC 700 1.6 UNITS OF MEASUREMENT 1.6.1 CONVERSION FACTORS Dimension SI-Units US Units Conversion Length [mm] millimeters [m] meters [km] kilometers [in] inches [ft] feet [NM] nautical miles [mm] / 25.4 = [in] [m] / 0.3048 = [ft] [km] / 1.852 = [NM] Volume [l] liters [US gal] US gallons [qts] US quarts [l] / 3.7854 = [US gal] [l] / 0.9464 = [qts] Speed [km/h] kilometers per hour [m/s] meters per second [kts] knots [mph] miles per hour [fpm] feet per minute [km/h] / 1.852 = [kts] [km/h] / 1.609 = [mph] [m/s] x 196.85 = [fpm] Speed of rotation [RPM] revolutions per minute -- Mass [kg] kilograms [lb] pounds [kg] x 2.2046 = [lb] Force, weight [N] newtons [lbf] pounds force [N] x 0.2248 = [lbf] Pressure [hPa] hecto- pascals [mbar] millibars [bar] bars [inHg] inches of mercury [psi] pounds per square inch [hPa] = [mbar] [hPa] / 33.86 = [inHg] [bar] x 14.504 = [psi] Tempera- ture [°C] degrees Celsius [°F] degrees Fahrenheit [°C]x1.8 + 32 = [°F] ([°F] - 32)/1.8 = [°C] Page 1 - 16 Rev. 5 25-Nov-2024 Doc. No. 7.01.06-E DA 42 AFM with OÄM 42-102 Garmin GFC 700 General Dimension SI-Units US Units Conversion Intensity of electric current [A] ampères -- Electric charge (battery capacity) [Ah] ampère-hours -- Electric potential [V] volts -- Time [sec] seconds -- Doc. No. 7.01.06-E Rev. 5 25-Nov-2024 Page 1 - 17 General DA 42 AFM with OÄM 42-102 Garmin GFC 700 1.6.2 CONVERSION CHART LITERS / US GALLONS Liters US Gallons US Gallons Liters 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 28 106.0 110 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 Page 1 - 18 Rev. 5 25-Nov-2024 Doc. No. 7.01.06-E DA 42 AFM with OÄM 42-102 Garmin GFC 700 General 1.7 THREE-VIEW DRAWING Doc. No. 7.01.06-E Rev. 5 25-Nov-2024 Page 1 - 19 General DA 42 AFM with OÄM 42-102 Garmin GFC 700 1.8 G1000 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 of the 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. 4. Provided a Garmin G1000 GPS receiver is receiving adequate usable signals, it has been demonstrated capable of and has been shown to meet the accuracy specifications for: (a) VFR/IFR enroute, oceanic, terminal, and non-precision instrument approach (GPS, Loran-C, VOR, VOR-DME, TACAN, NDB, NDB-DME, RNAV) operation within the U.S. National Airspace System in accordance with AC 20-138A. Page 1 - 20 Rev. 5 25-Nov-2024 Doc. No. 7.01.06-E DA 42 AFM with OÄM 42-102 Garmin GFC 700 General (b) The systems meets RNP5 airspace (BRNAV) requirements of AC 90-96 and in accordance with AC 20-138A, and FAA Order 8110.60 for oceanic and remote airspace operations, provided it is receiving useable navigation information from the GPS receiver. The system meets the accuracy requirements of EASA AMC 20-4 for Basic RNAV. (c) The Garmin GNSS navigation system as installed in this airplane complies with the equipment requirements of FAA AC 90-100A for RNAV 2 and RNAV 1 operations. (d) The Garmin GNSS navigation system as installed in this airplane complies with the equipment requirements of FAA AC 90-105 and meets the equipment performance and functional requirements to conduct RNP terminal departure and arrival procedures and RNP approach procedures without RF (radius to fix) legs. (RNP1, RNP APCH0.3 LNAV). (e) The Garmin GNSS navigation system as installed in this airplane has been found to comply with the requirements for primary means of Class II navigation in oceanic and remote navigation (RNP-10) without time limitations in accordance with FAA AC 20-138A and FAA Order 8400.12A. The Garmin GNSS navigation system can be used without reliance on other long-range navigation system. Navigation is accomplished using the WGS-84 (NAD-83) coordinate reference datum. GPS navigation data is based upon use of only the GPS operated by the United States of America. Doc. No. 7.01.06-E Rev. 5 25-Nov-2024 Page 1 - 21 General DA 42 AFM with OÄM 42-102 Garmin GFC 700 5. If the Garmin GWX 68 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 shall be used to avoid severe weather and not for penetrating severe weather. Pulse type weather radar systems like the GWX 68 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, the Garmin GWX 68 has a demonstrated range of 160 nautical miles. Refer to Garmin G1000 Pilot’s Guide for the DA 42, P/N 190-00649-( ), latest effective issue for further information. 6. 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. Page 1 - 22 Rev. 5 25-Nov-2024 Doc. No. 7.01.06-E

All Diamond DA42 VI parts catalog