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DA 62 AFM Introduction
FOREWORD
We congratulate you on the acquisition of your new DIAMOND DA 62.
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 62.
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 62 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 INC.
1560 Crumlin Sideroad,
London, Ontario, Canada N5V 1S2
Phone. : +1 519 457 4000
E-Mail : Techpubs@diamondair.com
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Introduction DA 62 AFM
0.1 APPROVAL
The content of approved chapters is approved by Transport Canada Civil Aviation.
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.
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 Design Change Advisory or Optional Design Change Advisory (MÄM
or OÄM), then the corresponding Temporary Revision is superseded. For example: If
Revision 1 covers OÄM 62-039, then the Temporary Revision TR OÄM-62-039 is
superseded by the 'permanent' Revision 1.
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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
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DA 62 AFM General
CHAPTER 1
GENERAL
Page
1.1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-2
1.2 CERTIFICATION BASIS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-4
1.3 WARNINGS, CAUTIONS AND NOTES . . . . . . . . . . . . . . . . . . . . . . 1-4
1.4 DIMENSIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-5
1.5 DEFINITIONS AND ABBREVIATIONS . . . . . . . . . . . . . . . . . . . . . . . 1-7
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. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-21
1.9.1 ENGINE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-21
1.9.2 PROPELLER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-21
1.9.3 AVIONICS SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-22
Doc. No. 11.01.05-E Rev. 0 11-Jan-2019 Page 1 - 1
General DA 62 AFM
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.
The Airplane Flight Manual includes all the data which must be made available to the
pilot according to the AWM 523 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
MTOM 2300 kg/5071 lb MÄM 62-001 9 yes 9 no
Maximum Zero Fuel Mass
2200 kg (4850 lb)
MÄM 62-063 9 yes 9 no
Engine Software
VC33_2P_05_19*
MÄM 62-168 9 yes 9 no
Garmin Hard- and Software
Upgrade I (Garmin G1000 NXi)
MÄM 62-254 9 yes 9 no
Auxiliary Fuel Tanks OÄM 62-001 9 yes 9 no
Continuous Flow Oxygen System
(77 cuft cylinder)
OÄM 62-004 9 yes 9 no
Garmin GWX 70 Weather Radar OÄM 62-009 9 yes 9 no
Avidyne TAS 600 Series OÄM 62-011 9 yes 9 no
MTOM 1999 kg/4407 lb OÄM 62-018 9 yes 9 no
7 Seated Configuration OÄM 62-019 9 yes 9 no
Page 1 - 2 Rev. 0 11-Jan-2019 Doc. No. 11.01.05-E
DA 62 AFM General
Modification Source Installed
WX-500 Storm Scope OÄM 62-021 9 yes 9 no
Continuous Flow Oxygen
System (50 cuft cylinder)
OÄM 62-028 9 yes 9 no
Removal of Unfeathering
Akkumulator
OÄM 62-030 9 yes 9 no
Heated Static Ports OÄM 62-037 9 yes 9 no
On Top Exhaust System OÄM 62-038 9 yes 9 no
28V Power Outlet Option OÄM 62-1002 9 yes 9 no
* Or later approved software
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 right seat.
CAUTION
The DA 62 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.
Doc. No. 11.01.05-E Rev. 0 11-Jan-2019 Page 1 - 3
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