Diamond DA 62 Flight Manual

•Diamond

AIRCRAFT

AIRPLANE FLIGHT MANUAL

DA62

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  

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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.

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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Introduction DA 62 AFM

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Doc. # 11.01.05-E

DA 62 AFM Introduction

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

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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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Diamond DA 62 Flight Manual

Diamond DA 62 Flight Manual

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